20010502000602001050200060CE 2001 5 2 00114 120010318G711045A350271 COWLING BEECH BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE LT ENGINE BENT E DJFAO OTHER O OTHER CRCRUISE 1 EA23456CW4448 RK56 COWLING ON LEFT HAND ENGINE BOTTOM INBOARD SIDE WAS BENT BACK DURING FLIGHT. THE CAUSE IS UNKNOWN, THESE COWLINGS ARE KNOWN TO HAVE THIS TYPE OF PROBLEM. 2H72 4F4 FRTA16SW E25EA 20010802002482001080200248CE 2001 8 2 010204 120010723G7713C4820020108 RELIEF VALVE CESSNA210 T210N 2073456CE CONT O520 TSIO520R 17040SO MCAULYD3A34 D3A34C402 GL INDUCTION SYSTEMFAILED B R8RRK NONE O OTHER ININSP/MAINT 1 SW996506G 21064406 294271R 001099 A TCM REBUILT ENGINE WAS INSTALLED INTO THIS AIRCRAFT WITH ALL THE ASSOIATED NEW PARTS. THE AIRCRAFT COULD NOT ACHIVE 36.5 IN. AT 2700 RPM FOR TAKEOFF POWER. ALL INDICATING INSTRUMENTS WERE VERIFIED FOR CALIBRATION. WE INSTALLED THE OLD ABSOLUTE PRESSURE RELIEF VALVE AND OBTAINED 36.5 IN. EASILY. 1H71 3O3 O 3A21 E8CE 5 CP47GL 20010802002502001080200250CE 2001 8 2 010726 120010726G7713C4820020108 RELIEF VALVE CESSNA210 T210N 2073456CE CONT O520 TSIO520R 17040SO MCAULYD3A34 D3A34C402 GL INDUCTION SYSTEMMALFUNCTIONED B R8RRK NONE O OTHER ININSP/MAINT 1 SW996506G 21064406 294271R 001099 AFTER A REBUILT TCM ENGINE WAS INSTALLED INTO THIS AIRFRAME A SECOND REBUILT ABSOLUTE PRESSURE RELIEF VALVE FROM CONSOLIDATED FUEL SYSTEMS, INC. WAS INSTALLED AND THE ENGINE WOULD NOT PRODUCE 36.5 IN OF MANIFOLD PRESSURE REQUIRED FOR TAKEOFF. REINSTALLED THE ORIGINAL RELIEF VALVE AND THE ENGINE PRODUCED 36.5 IN OF MANIFOLD PRESSURE. 1H71 3O3 O 3A21 E8CE 5 CP47GL 20011002000062001100200006WP 2001 10 2 0109 120010906G5552 STOP DOUG DC8 DC862 3021970WP RT ELEVATOR TAB LOOSE H O OTHER F FLT CONT AFFECTED CRCRUISE 1 SW99VP-BH 46111 AUTO PILOT PORPOSING IN LEVEL FLIGHT. DURING RT ELEVATOR CABLE ADJUSTMENT CHECKED TRAVEL TAB IN BOTH DIRECTION. WITH STICK FULL FORWARD THE LEFT ELEVATOR TAB ONLY GOES UP. THE RIGHT ELEVATOR TAB STAYS AT THE SAME POSITION. AFTER TROUBLE SHOOTING WE FOUND THE STOP SCREW (THE UPPER ONE ) COMPLETELY LOOSE ON RIGHT SYSTEM, CAUSING THE RESTRICTING TRAVEL OF TAB IN TRAILING EDGE UP. AFTER CORRECTING ACTION, THE TRAVEL CHECK IS NORMAL 2L74 4F 4A25 20011126000032001112600003NE 2001 11 26 0115 220011115G7200 ENGINE AMD FALC50FALCON50MYST2730106EU GARRTTTFE731TFE73131C 01518NE NR 1 FLAMED OUT H K NONE X ENGINE FLAMEOUT CRCRUISE 1 SW99BSA 196 APPROX 30 MINUTES INTO FLIGHT AT FL 390 COCKPIT HEAT CONTROL WAS MOVED FROM MANUAL TO AUTO. SHORTLY AFTER NR 1 ENG FLAMED OUT. NO WARNING LIGHTS, NO VIBRATION. AN IMMEDIATE RELIGHT WAS PERFORMED AND SUCCESSFUL. ALL ENGINE PARAMETERS WERE NORMAL, FLIGHT CONTINUED TO DESTINATION. 2L73 4F4 F A46EU E6WE 20020124000952002012400095SO 2002 1 24 0116 120011116G7830 LOCK GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU THRUST REVERSER FAULTY H A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW99VPBSF 1058 16171 WHILE PASSING THROUGH 2,500 FT MASTER WARNING RT THRUST REVERSER UNLOCKED. IMMEDIATELY REDUCED THROTTLES MESSAGE CLEARED. CONTINUED ON. WHEN PASSING THROUGH 4000 FT SAME WARNING AGAIN. RETURN TO BLOCKS. NORMAL APPROACH AND LANDING MADE. MAINTENANCE INSPECTION REVEILED FAULTY THRUST REVERSER INTERNAL LOCK . BOTH ACTUATORS REPLACED 2L72 4F4 FRTA12EA E25NE 20010424002772001042400277WP 2001 4 24 01FDEA00289 120010419G3260 TARGET DOUG DC10 DC1010 3022110WP RT MLG DOOR INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25389FE 46623 01-124 RT MLG RED LIGHT ILLUMINATED ON BOTH PANELS AFTER TAKE OFF. RECYCLED PER RED TABS, REMAIN ILLUMINATED. R/R TARGET PER EO 8-3260-7-3304-B. AC OK FOR SERVICE. 2L73 4F A22WE 20010702000362001070200036WP 2001 7 2 01FDEA00398 120010605G3260 WARNING LIGHT DOUG DC10 DC1010 3022110WP COCKPIT ILLUMINATED A FDEAO OTHER J WARNING INDICATION DEDESCENT 1 SO25389FE 46623 ON DESCENT RT MLG RED LIGHT ILLUM ON BOTH PANELS. ACCOMP RED TAB PROC. FERRIED A/C TO IND. 2L73 4F A22WE 20020124000962002012400096CE 2002 1 24 040521239 120011204G3211501202015 SUPPORT BEECH 200 A200 1152921CE MLG CRACKED H K NONE O OTHER ININSP/MAINT 1 SO211546 11996 BC58 LEFT HAND AND RIGHT HAND MAIN LANDING GEAR DRAG LEG SUPPORTS FOUND TO BE CRACKED DURING FLUORESCENT PENETRANT INSPECTION. INSPECTION ORDERED BY U.S. CUSTOMS SERVICE BASED ON REPORTS FROM U.S. ARMY OPERATORS. 1L72 4T A24CE 20020124000972002012400097CE 2002 1 24 040521239A 120011204G3211501202015 SUPPORT BEECH 200 A200 1152921CE MLG CRACKED H K NONE O OTHER ININSP/MAINT 1 SO217247012534 BC04 LEFT HAND MAIN LANDING GEAR DRAG LEG SUPPORT FOUND TO BE CRACKED DURING FLUORESCENT PENETRANT INSPECTION. INSPECTION ORDERED BY U.S. CUSTOMS SERVICE BASED ON REPORTS BY U.S. ARMY OPERATORS. 1L72 4T A24CE 20010802002532001080200253NE 2001 8 2 1 220010712G7261642790041 TRANSMITTER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE OIL PRESSURE INOPERATIVE B S88RED ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO215202Y 3085 9564 NO ENGINE OIL PRESSURE INDICATION DURIN ENGINE START SEQUENCE.THE OIO PRESSURE TRANSMITTER WAS REPLACED ON MORE THAN ONE TIME, BUT THE NEW TRANSMITTER WERE BAD FROM OVERHAULED FACILITY. 1G71 3U3 U H9EU E19EU 20010802002562001080200256SO 2001 8 2 100000 220010801G7414 WIRE PIPER J3 J3F65 7100536SO CONT A65 A658 17003SO MAGNETO CHAFED G O OTHER YJ ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 GL0740782 7496 DURING TAKE-OFF THE ENGINE QUIT. THE AIRCRAFT WAS DESTROYED. INVESTIGATION BY THE FAA INSPECTOR PROVED THAT THE PROBABLE CAUSE OF THE ENGINE FAILURE WAS ATTRIBUTED TO BOTH MAGNETO P-LEAD WIRES BEING GROUNDED OUT AGAINST A SCREW THAT SECURED THE LEFT-HAND INNER AND OUTER WINDOW TRIM PIECES. 1H71 3O3 O A692 E205 20011026000092001102600009CE 2001 10 26 1024016 120011022G3040265318202071 WINDSHIELD RKWELLNA265 NA26565 7630107CE GARRTTTFE731TFE7313R1D 01518WP COCKPIT ARCED B RE3RK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM016NR 1834 46529 PILOTS NOTICED INTERNAL ARCING IN WINDSHIELD AT UPPER EDGE ALONG HEAT ELEMENT BUS STRIP. ARCING CONTINUED FROM ONE SIDE AND PROGRESSED TO OPPOSITE SIDE AND BURNED BUS STRIP PARTIALLY THROUGH. WINDSHIELD CONTINUED TO HEAT UNTIL BUS STRIP BURNED COMPLETELY THROUGH WIDTH AT ONE LOCATION. WINDSHIELD WAS REPLACED PRIOR TO NEXT FLIGHT. REASON FOR ARCING IS MOST LIKELY DELAMINATION IN UPPER EDGE OF WINDSHIELD IN BUS STRIP AREA. RECOMMEND PRE-FLIGHT VISUAL INSPECTION OF THIS AREA FOR DELAMINATION AND EVIDENCE OF INTERNAL ARCING STARTING TO HAPPEN IN ANY AREA. IF REPLACEMENT IS REQUIRED, REPLACE WITH PPG BRAND WINDSHIELD. 2L72 4J4 F A2WE E6WE 20020719000812002071900081CE 2002 7 19 102401868 120010923G3340S13605L CIRCUIT BREAKER CESSNA172 172R 2072401CE EXTERIOR LIGHTS FAILED D S1XBA UNSCHED LANDING A FLAME/FIRE CLCLIMB 1 SO172458G 17280893 THE TAIL LIGHT POSITIVE LEAD SHORTED TO GROUND BY CONTACT WITH A TINNERMAN NUT IN THE RUDDER. THERE WAS NO EVIDENCE OF TRAUMA TO THE WIRE. ONLY A PINPOINT OF CONTACT WAS EVIDENT THE NAV LIGHT BREAKER DID NOT TRIP AND THE WIRING BURNED FROM THE TAIL TO THE CIRCUIT BREAKER PANEL, TAKING OUT HALF THE BUS WITH IT. THE FIRST WIRE BURNING STARTED A CASCADE OF SHORT CIRCUITS. THIS DOMINO EFFECT SEQUENTIALLY TOOK OUT ADDITIONAL CIRCUITS UNTIL THE MAIN BUSS BREAKER OPENED. 1H71 3O NT3A12 20010802002592001080200259CE 2001 8 2 2 120010727G323299810057652 ACTUATOR BEECH 200 C12C CE PWA PT6 PT6* 52043EA HARTZLHCB3T HCB3TN3 GL MLG DAMAGED B S88RK NONE O OTHER ININSP/MAINT 1 SO211547 1091 BC50 DURING A LANDING GEAR RETRACTION CHECK THE L/H LANDING GEAR WHENT FROM THE UP POSITION TO THE DOWN AND LOCK POSITION BY OT SELF. AFTER FURTHER INVESTIGATION FOUND THA THE L/H ACTUATOR SHAFT NUT HAD FAILED AND COMPLETLY CAME OF THE SHAFT, CAUSING THE LANDING GEAR TO DROP TO THE DOWN AND LOCK POSITION. 1L72 4T3 T A24CE E2NE 6 CP15EA 20010409001642001040900164CE 2001 4 9 20010124CW003 120010103G712010191012253 MOUNT BEECH B300 B300 1159232CE PWA PT6 PT6* 52043EA ENGINE CRACKED D K NONE O OTHER ININSP/MAINT 1 EA23309M FL48 COWL ATTACH LUGS CRACKED ON ENGINE MOUNT. ALSO, CORROSION FOUND AT MOUNT TO FUSELAGE ATTACH POINT BOLTS AND SPACING WASHERS. 2L72 4T3 TRTA24CE E2NE 20010410000022001041000002CE 2001 4 10 20010124CW006 220010124G7420M750272 IGNITION LEAD PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360RB 17025CE RT ENGINE SHORTED D K NONE O OTHER ININSP/MAINT 1 NM074166R 3449185 322077 NR2 AND NR6 CYLINDER IGNITION LEADS ON BOTTOM PLUGS SHORTED OUT, BEHIND IGNITION LEAD SPRING ASSEMBLY. 1L72 3O3 O A7SO E9CE 20010417000972001041700097SO 2001 4 17 20010124CW007 220010124G8520 BEARING CESSNA180 180B 2072606CE CONT O520 IO520D 17032SO CRANKCASE FAILED D K NONE O OTHER CRCRUISE 1 SW999283R 18802211 22145373D BEARING FAILURE ON NR2 MAIN BEARING. CAUSED DAMAGE TO CRANKCASE, OIL PRESSURE DROPPED 20 PSI IN FLIGHT WITH NO OTHER INDICATION. 1H71 3O3 O 5A6 E5CE 20010502000012001050200001EU 2001 5 2 20010124CW008 120010109G6520365A33600501 BEARING AEROSPSA365 SA365N1 8680668EU TAIL ROTOR GRBX FAILED D K NONE O OTHER ININSP/MAINT 1 EA0389SM 6282 MANUFACTURER TEARDOWN OF GEARBOX, FOUND PITCH CHANGE SHAFT DUPLEX BEARING FAILURE AND SHAFT SHEAR T/R BLADES IN-NEG-PITCH WITH NO CONTROL OF TAIL ROTOR.NOTE: NO T/R GEARBOXES INSTALLED ON ANY 365 IN OUR FLEET HAVE ELECTRONIC CHIP DETECTOR. 1G72 3U H10EU 20010502000022001050200002CE 2001 5 2 20010124CW009 120010124G2720 RUDDER CESSNA182 182S 2072701CE TAIL INTERFERENCE D K NONE O OTHER ININSP/MAINT 1 SW99162TC 80164 WHEN CHECKING RUDDER TRAVEL, ELEVATOR WAS IN NEUTRAL POSITION. WHILE THE RUDDER WAS DEFLECTED FULL IN EITHER DIRECTION, THE ELEVATOR WOULD HIT THE RUDDER WHEN THE ELEVATOR WAS RAISED. THE RUDDER TRAVEL WAS RIGGED CORRECTLY PER MAINTENANCE MANUAL. THIS COULD CAUSE THE RUDDER AND ELEVATOR TO JAM IN FLIGHT. 1H71 3O NT3A13 20010301000792001030100079EU 2001 3 1 20010124CW010 120010109G65203655A33600501 GEARBOX AEROSPAS365 AS365N2 8680815EU TAIL ROTOR FAILED D K NONE O OTHER ININSP/MAINT 1 EA03365DU955 955 6425 GEARBOX REMOVED DUE TO FAILING SOAP/OIL ANALYSIS/ OF IRON-18.0 AND MAGNESIUM/ 73.2/SAMPLE TAKEN 12-18-00. PREVIOUS SAMPLE TAKEN 12-5-00 HAD IRON AT /3.8/ AND MAGNESIUM AT /10.9/ ALL VALVES ARE IN PARTS PER MILLION. 1G72 3U RTH10EU 20010502000052001050200005SO 2001 5 2 20010125CW002 120010102G2140A23D04 REGULATOR PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA FWD HEATER LEAKING G WVBAK NONE K FLUID LOSS ININSP/MAINT 1 SW9959764 317652037 PILOT REPORTED HEATER INOPERATIVE. UPON INSPECTION, FOUND FUEL PRESSURE REGULATOR LEAKING. UNIT WAS REPLACED, OPS GOOD. 1L72 3O3 O A20SO E14EA 20010502000062001050200006SO 2001 5 2 20010125CW003 120010102G2140A23D04 REGULATOR PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA FWD HEATER LEAKING G WVBAK NONE K FLUID LOSS ININSP/MAINT 1 SW9927755 317852148 PILOT REPORTED HEATER OUTPUT DECREASES AFTER ABOUT 20 MIN. UPON INSPECTION, FOUND FUEL PRESSURE REGULATOR LEAKING. UNIT WAS REPLACED. OPS CHECK GOOD 1L72 3O3 O A20SO E14EA 20010502000072001050200007SO 2001 5 2 20010125CW004 120010102G214044008 VALVE ELECTROSYS PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA MCAULY3DF36CB3DF36C526 GL HEATER COMP LEAKING G K NONE K FLUID LOSS ININSP/MAINT 1 SW993527U2346 2346 A98030019 317952141 DURING ROUTINE INSPECTION, FUEL WAS OBSERVED LEAKING FROM FUEL SOLENOID SHUT OFF VALVE. PART WAS REMOVED FROM SERVICE. 1L72 3O3 O A20SO E14EA 5 C 20010502000082001050200008SO 2001 5 2 20010125CW006 120010109G282335640023564001 SELECTOR VALVE PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA HARTZLHCE2Y HCE2YR2 GL FUEL SYSTEM LEAKING D K NONE K FLUID LOSS ININSP/MAINT 1 SW9917WE 3615 277854118 AC WAS PUT IN UNHEATED HANGER WITH FULL FUEL TANKS, FOUND FUEL ON FLOOR UNDER BOTH WINGS, WAS FOUND TO BE LEAKING FROM OVERFLOW TUBES OF BOTH INBOARD FUEL TANKS WHICH WERE FULL. OUTBOARD TANKS WERE DOWN, ONLY CONNECTION BETWEEN IB AND OB TANKS IS THROUGH FUEL SELECTOR VALVES. FUEL SELECTOR VALVES WERE FOUND, WHEN IN OFF POSITION, FUEL FLOW WAS NOT COMPLETELY SHUT OFF TO ENG SIDE OF VLV. AC HAD RECENT ANNUAL INSP. ALL OPS CHECKED GOOD. VALVE LOCATION IN IB AFT OF FIREWALLS. VALVES REMOVED AND SENT TO DUKES, VALVE MFG. SUSPECT ENVIRONMENTAL CHANGE OF AC TO FIND DEFECT OF VALVES. 1L72 3O3 O 1A10 1E4 5 CP9EA 20010502000112001050200011CE 2001 5 2 20010125CW009 120010125G270135524656 CLIP BEECH 35 S35 1151532CE CONTROL YOKE MISSING D K NONE O OTHER ININSP/MAINT 1 SW99354D D7659 DURING ANNUAL INSPECTION OF AC A VISUAL INSPECTION WAS PERFORMED ON CHAIN INSIDE THE DUAL CONTROL YOKE. CHAIN MASTER LINK PLATE AND CLIP WERE MISSING FROM LOWER LEFT CHAIN ATTACH POINT TO FITTING. RECOMMEND MORE ATTENTION IN THIS AREA UPON ANNUAL INSPECTION/ 100 HOUR INSPECTION 1L71 3O 3A15 20010418002822001041800282NM 2001 4 18 20010125CW010 120010105G291065447821 HOUSING BOEING BOEING737 737 UTILSYSNM HYDRAULIC MODULECRACKED B K NONE O OTHER ININSP/MAINT 1 NM01 1110 HOUSING WAS NOTED TO BE CRACKED AT BOTH THE A AND B PORTS, DURING NON-DESTRUCTIVE INSPECTION. 2L72 4F RTA16WE 20010417001092001041700109NM 2001 4 17 20010125CW011 120010104G278269358521 SLEEVE BOEING BOEING737 737 UTILSYSNM SLAT ACTUATOR FRACTURED B K NONE O OTHER ININSP/MAINT 1 NM01 7649K SLEEVE /145/ OF BLOCKING VALVE ASSEMBLY IS FRACTURED. PROBABLE CAUSE/ FATIGUE 2L72 4F RTA16WE 20010417001102001041700110NM 2001 4 17 20010125CW012 120010104G291065447821 HOUSING BOEING BOEING737 737 UTILSYSNM HYDRAULIC MODULELEAKING B K NONE K FLUID LOSS ININSP/MAINT 1 NM01 4312743127 1134 UNIT NOTED TO HAVE A PIN HOLE LEAK ADJACENT TO OUTLET PORT NR4 AS PRESSURE WAS APPLIED DURING PROOF TEST. 2L72 4F RTA16WE 20010502000152001050200015EA 2001 5 2 20010129CW004 220010104G855006B26072 GASKET PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA OIL FILTER CUT B K NONE O OTHER ININSP/MAINT 1 SW993580561 318052090 L663461A GASKET FOUND CUT UPON REMOVAL. POSSIBLY DUE TO INSTALLATION PROCEDURE. RECOMMEND MORE CARE IN INSTALLING ADAPTER PLATE TO PREVIENT COCKING ON INSTALLATION. MAKE SURE GASKET IS CENTERED ON PLATE. 1L72 3O3 O A20SO E14EA 20010418003482001041800348EA 2001 4 18 20010129CW008 120010129G5330 SKIN CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE FUSELAGE CORRODED B K NONE O OTHER ININSP/MAINT 1 WP07604WB 5125 AFTER REMOVAL OF SATCOMM ANTENNAS FROM FUSELAGE STATION 349, CORROSION WAS DISCOVERED UNDER ANTENNAS ON AIRCRAFT FUSELAGE SKIN SURFACE. AFTER REMOVAL OF CORROSION DAMAGE WAS BEYOND LIMITS, RESULTING IN SKIN REPLACEMENT ON BOTH SIDES. 2L72 4F4 FRTA21EA E15NE 20010502000212001050200021CE 2001 5 2 20010129CW013 120010105G5210 DOOR CESSNA182 182P 2075816CE RT DOOR CRACKED D K NONE O OTHER ININSP/MAINT 1 SW997220H 18263011 FORWARD DOOR POST, INSPECT AND MOD. FOUND CRACK ON RT SIDE. THE SEB CALLS FOR INITIAL INSPECTION AT 4000 HOURS. I HAVE FOUND THIS CONDITION ON 3 AC. 2 OF THE 3 HAD LESS THAN 2000 HRS T/S. HISTORY ON BOTH IS NORMAL SERVICE AND NO PASST DAMAGE OR ABUSIVE USE. SUSPECT CRACKS ARE DUE TO STRESS RELIEVE FROM STRAINS APPLIED DURING ASSEMBLY MORE THAT TYPE OF USE. 1H71 3O NTTA13 20010502000222001050200022CE 2001 5 2 20010129CW014 120010108G5210504300431273 DOOR FRAME BEECH 200 200BEECH 1152920CE AFT DOOR CRACKED B K NONE O OTHER ININSP/MAINT 1 EA05383JP8204 BB615 REMOVED AND REPLACED AFT CABIN DOOR FRAME PRESSURATION PROBLEM. 1L72 4T A24CE 20010307005812001030700581CE 2001 3 7 20010129CW016 120010108G2710 TORQUE TUBE CESSNA560 560XL CE PWA 545 PW545A NE AILERON CORRODED B DXTAK NONE O OTHER ININSP/MAINT 1 SW99690QS564 5605090 AFT AILERON SECTOR TORQUE TUBE CORRODED THE LENGTH OF THE TUBE BETWEEN THE UPPER AND LOWER BELLCRANKS. 2L72 4F4 FRTA22CE E00059EN 20010418003702001041800370SO 2001 4 18 20010129CW018 120010109G32421331317 STATOR BFGOODRICH EMB 120 EMB120 3260201SO BRAKE ASSY CRACKED B XC4RK NONE O OTHER ININSP/MAINT 1 SO05 0814A BRAKE ASSEMBLY PN 21661 FAILED PREMATURELY. NR2 STATOR CRACKED AT RELIEF HOLES. 25 PERCENT OF STATOR MISSING. HEAT STACK WARPED AND UNEVEN WEAR.NOTE OEM PARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION PN 21661. 2L72 4T RTA31SO 20010418003722001041800372 2001 4 18 20010129CW020 420010102G2565 SLIDE RAFT BFGOODRICH DOUG DC10 DC10 N/A-SDRNM CABIN MISINSTALLED B K NONE O OTHER ININSP/MAINT 1 SO19 DD041 FOUND 8 FT LONG BY 2 INCHES WIDE, RED WEBBING STRAP TIED AROUND THE FOLDED INFLATABLE SLIDE/RAFT. IF THE UNIT WERE TO BE USED IN AN EMERGENCY, THE SLIDE WOULD NOT HAVE DEPLOYED PROPERLY. 2L73 4F RTA22WE 20010502000292001050200029GL 2001 5 2 20010129CW025 320010106G6114HCE2YR2RBSF HUB HARTZL PIPER PA23 PA23250 7102308SO LYC O540 IO540* 41532EA HARTZLHCE2Y HCE2YR2 GL PROPELLER LEAKING B K NONE K FLUID LOSS ININSP/MAINT 1 SW9911JD 7841 860 BP6961 277405395 RL1279248A BP6961 PROPELLER WAS RECEIVED FOR NON-SCHEDULE REPAIR, OIL LEAK. DURING PRELIMINARY PROPELLER INSPECTION, PROPELLER WAS NOTED LEAKING BETWEEN HUB/PN D24772R/ AND CYLINDER/PN B24231. CYLINDER LIFTED OFFTHE HUB. PROPELLER ASSEMBLY WAS DISASSEMBLED, VISUALLY INSPECTED, HUB AND CYLINDER REPLACED, REASSEMBLED AND BALANCED. PROPELLER GOVERNOR WAS REQUESTED FOR INSP. WOODWARD GOVERNOR MODEL NR A210721 WITH SERIAL NR 2455904 WAS RECEIVED FOR INSP.GOVERNOR PRESSURE RELIEF VALVE WAS INSP. AND GOVERNOR ASSY WAS BENCH CKD W/NO DEFECTS.REPAIRED PROPELLER AND GOVERNOR WAS REINSTALLED. PROPELLER AND GOV OPS CK GOOD. 1L72 3O3 O 1A10 1E4 5 CP9EA 20010307005902001030700590EU 2001 3 7 20010130CW004 120010115G6321L635M1025229 BRAKE UROCOPEC135 EC135P1 8680990EU TRANSMISSION CRACKED B K NONE O OTHER ININSP/MAINT 1 EA03511ME138 0143 ROTOR BRAKE CHATTERING FOUND CRACKED ROTOR BRAKE DISC./ THIS IS SECOND EVENT. 1G72 3U O H88EU 20010307005922001030700592SW 2001 3 7 20010130CW005 120010116G6220430010101101 YOKE BELL 430 430 1182150SW MAIN ROTOR CRACKED B GS1RK NONE O OTHER ININSP/MAINT 1 sw99430TX 49005 H.A.S. REPLACED WITH NEW YOKE FROM BELL HELICOPTER. A 1.5 LONG CRACK WAS FOUND ON TOP OF THE YOKE AT STATION 31. 1G72 3U RTH9SW 20010307006182001030700618SW 2001 3 7 20010130CW006 120010108G6510407340339103 BEARING BELL BELL 407 407 SW T/R DRIVE SHAFT FAILED B K NONE O OTHER ININSP/MAINT 1 sw99407JR 53245 T/ROTOR, D/SHAFT BEARING PN 407340339101 FAILED. RESULTING IN THE LOSS OF BALL BEARINGS, SEALS AND GREASE. DAMAGE TO THE FOLLOWING ITEMS WAS CAUSED BY BEARING FAILURE. BEARING WAS INSTALLED IN NR1 POSITION OF TAIL ROTOR HANGER BEARINGS. DAMAGED ITEMS TO FOLLOW: IMPELLER ASSY, FER OIL COOLER BLOWER, HOUSING, COVER , HANGER SUPPORT, BOTH BEARINGS, BOTH ADAPTERS ON FWD AND AFT END OF SHAFT.IMPROVEMENTS NEED TO BE MADE IN BEARING DURABILITY AND ABILITY TO RETAIN GREASE FROM BEING FORCED OUT BY SUCTION CAUSED FROM IMPELLER ROTATION. 1G71 3U O H2SW 20010307006202001030700620GL 2001 3 7 20010130CW008 120010116G5310 TUBE ENSTRMF28 280F 3300550GL GEARBOX MOUNTS CRACKED D K NONE O OTHER ININSP/MAINT 1 CE01199TV5503 1510 4130 TUBING WAS FOUND CRACKED BETWEEN LEFT FORWARD GEARBOX MOUNT AND LEFT REAR GEARBOX MOUNT. PROBABLE CAUSE, METAL FATIGUE. AC IS 20 YR OLD WITH 5503 HRS. AC DID HAVE HARD LANDING YEARS AGO AT LESS THAN 1000 HRS ON AIRFRAME. POSSIBLE FRAME WAS SUBJECTED TO ADDITIONAL STRESS FROM THE HARD LANDING. RECOMMEND OPERATORS TO INSPECT AIRFRAME TUBING IN THIS AREA FOR POSSIBLE CRACKS. 1G71 3O H1CE 20010307006222001030700622EU 2001 3 7 20010130CW009 120010105G6520365A33600501 GEARBOX AEROSPSA365 SA365N1 8680668EU TMECA ARRIELARRIEL1C 60030NE TAIL ROTOR FAILED B E ENGINE SHUTDOWN O OTHER ININSP/MAINT 1 SW07911UF M539 6338 5065 INITIAL GRND RUN-UP, AFTER MJR INSP, A T/R GBX FAILURE WAS EXPERIENCED AFTER APPROX 15-20 MINUTES. AC JERKED SEVERAL TIMES ALONG THE YAW AXIS, WITH NR1 ENG RUNNING AT 68%NG AND NR2 AT 65%NG AN UNUSUAL NOISE WAS HEARD FRM TAIL ROTOR, SHUT DOWN WAS INITIATED, NOISE WORSENED. ROTOR BREAK WAS APPLIED WITHIN 10 REV OF COMING TO COMPLETE STOP FRM COAST DWN WITH ROTOR BREAK APPLIED, LOUD SQUEALING AND GRINDING NOISE WAS EMITTING FROM THE TAIL ROTOR AND COAST DWN CAME TO A RAPID BUT NOT SUDDEN STOP. INITIAL INSP REVEALED METAL PARTICLES ON TAIL ROTOR CHIP PLUG, OIL AND SPREAD FLEX COUPLING AT THE TAIL ROTOR OUTPUT FLNG FROM MAIN GBX. AFTER TR DWN & INSP, OUTER BRG OF INPUT HSG WAS DRY, GBX OIL LEVEL WAS FULL. 1G72 3U3 U H10EU E19EU 20010409001112001040900111 2001 4 9 20010202CW002 420010112G31004059013 PANEL DOUG MD11 MD11 3023602NM COCKPIT INOPERATIVE D JA DUMP FUEL UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP03105EV 48544 PILOT REPORTED ELECTRICAL BURNING ODOR DURING CLIMB, A IL 300, SMOKE APPEARED IN THE COCKPIT CAUSED FUEL DUMPED AND AIR RETURNED TO LAX. MAINTENANCE AND INSPECTION COCKPIT INDICATORS ALL C/B ARE CLOSED OPEN OVHD PANEL, MAINT PANEL AND AVIONICS PANEL, EXAMINED ALL COMPARTMENT, IND ALL CONDITIONS ARE NORMAL, NO BURN SIGN WAS FOUND. REVIEW LAST FLIGHT FAULT, REPLACED SYSTEM CONTROL PANEL FOR SAFETY AND MAINTENANCE PREVENTION. 2L73 4F RTA22WE 20010502000332001050200033CE 2001 5 2 20010205CW004 120010105G574050110231 FITTING CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C505 GL WING SPAR CORRODED D K NONE O OTHER ININSP/MAINT 1 NE05401TJ3000 402C0109 AFT SPAR REAR TOP WING ATTACH FITTING CORRODED. INSTALLED NEW FITTING. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010502000342001050200034SO 2001 5 2 20010205CW005 220010205G8530637837 VALVE SPRING CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO NR 4 CYLINDER BROKEN D K NONE O OTHER ININSP/MAINT 1 SW99305AT 1354 402C0030 519128 DURNING DETAILED INSPECTION OF LEFT ENGINE, COMPRESSION CHECK OF NR4 CYLINDER REVEALED LOW COMPRESSION. APPROX 80/20, UPON FURTHER INSPECTION THE OUTER SPRING OF THE INTAKE VALVE WAS FOUND TO BE BROKEN. 1L72 3O3 O A7CE E8CE 20010502000352001050200035CE 2001 5 2 20010205CW006 120010205G7714C6680160107 TACHOMETER CESSNA402 402C 207590RCE INSTRUMENT PANELMALFUNCTIONED D K NONE O OTHER ININSP/MAINT 1 SW012711X 94 402C0116 LEFT ENGINE TACH NEEDLE WOULD NOT PROCEED BEYOND 2300 RPM WHEN ENGINE WAS ACTUALLY AT 2700 RPM. 1L72 3O A7CE 20010502000362001050200036CE 2001 5 2 20010205CW007 120010116G2434OHC315E ALTERNATOR CESSNA172 172M 2072418CE LYC O320 AEIO320E1B 41508EA ENGINE SEPARATED D K NONE O OTHER ININSP/MAINT 1 SW019627Q400 17265711 OHC ALTERNATOR, BOLTS HOLDING HOUSING TOGETHER, 2 BACKED OUT, LEFT HANGING BY INTACT SAFETY TO 3RD BOLT. 1H71 3O3 ONT3A12 1E12 20010502000372001050200037SO 2001 5 2 20010205CW008 220010115G7414 ROTOR SLICK CESSNA210 210L 2073448CE CONT O520 IO520L 17032SO MAGNETO BROKEN D K NONE O OTHER ININSP/MAINT 1 SO1593111637 637 99061927 21060266 295010R ROTOR BROKE AT CAM AND GEAR LOCATION/DRIVE GEAR. 1H71 3O3 O 3A21 E5CE 20010502000392001050200039SO 2001 5 2 20010205CW010 120010110G716087327002 VALVE PIPER PA28 PA28161 7102803SO CARB AIR BOX WORN D K NONE O OTHER ININSP/MAINT 1 NM13514MS 288316099 AIR VALVE IN CARB AIR BOX HAS BEEN REPLACED 3 TIMES WITH T/S : 1/327.3, 2/622.7, 3/186.4 ALL 3 REPLACEMENTS DUE TO WORN OR BROKEN ACTUATOR LEVER. THIS LEVER WAS ORIGINALLY A STEEL PART THAT SEEMED TO LAST FOREVER. THE AL APPEARS TO BE TOO SOFT. SUSPECT WHEN IT IS WELDED TO THE FHAFT ANY HEAT TREATMENT PRESENT, IS LOST. 1L71 3O 2A13 20010307006902001030700690 2001 3 7 20010205CW011 420010104G2210761039 TRIM SWITCH CENTURY PIPER PA31 PA31310 7103103SO LYC O540 TIO540A2B 41532EA PILOT YOLK SHORTED D A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CE019007Y 3111 RL55061 AFTER TAKEOFF AUTOPILOT TRIM PITCHED UP. PILOT RETURNED TO AIRPORT AND HAD SAFE LANDING. FOUND TRIM SWITCH IN PILOTS YOLK SHORTED OUT. FOUND TWO WIRES TOUCHING, CAUSING PITCH UP. RESOLDERED CONNECTOR AND INSULATED FROM OTHER TERMINALS. 1L71 3O3 ORTA20SO E14EA 20010307005712001030700571SW 2001 3 7 20010205CW012 120010117G5302206033004143 MOUNT BELL 206 206L3 1182108SW TAIL BOOM CRACKED D K NONE O OTHER ININSP/MAINT 1 SW9964PJ 6177 51100 CRACK FOUND UNDER TAIL ROTOR GEARBOX AT AFT, RIGHT, MOUNT HOLE. CRACK WAS NOT SEEN UNTIL GEARBOX WAS REMOVED TO PERFORM ASBCRACK WAS ONE INCH LONG, GOING FOR AND AFT THRU HOLE. 1G71 3U H2SW 20010306000712001030600071CE 2001 3 6 20010205CW013 120010109G29102407003487 HYDRAULIC LINE LEAR 25 25D 5170514CE GE CJ610 CJ6108 30006NE TAILCONE CHAFED D K NONE O OTHER ININSP/MAINT 1 SW0525HF 295 PILOT LOST HYDRAULIC PRESSURE IN FLIGHT. INSPECTION REVEALED HYDRAULIC PRESSURE LINE FROM LEFT ENGINE TO AUXILLARY HYDRALUIC PUMP MANIFOLD LINE, CHAFFED AT CLAMP, RECOMMENDED REMOVING CLAMPS ON THIS SPECIFIC HYDRAULIC LINE ON AIRCRAFT WITH THE SAME HYDRAULIC SYSTEM SETUP. 2L72 4J4 J A10CE 1E16 20010322001172001032200117 2001 3 22 20010205CW014 420010115G2561KS9P0101105 LIFE VEST CELLS WORN B KQ1RK NONE O OTHER ININSP/MAINT 1 EA07 LIFE VEST FAILED TO MEET MFG RECOMMENDED TWO SDI CELL TEST. LIFE VEST DATE OF MFG JUNE 1983. FAIR WEAR AND TEAR 20010322001182001032200118 2001 3 22 20010205CW015 420010105G2561KS9P0101 LIFE VEST CELLS WORN B KQ1RK NONE O OTHER ININSP/MAINT 1 EA07 LIVE VEST FAILED MFG RECOMMENDED PSI TEST.NOVEMBER 1982/ FAIR WEAR AND TEAR. 20010307005732001030700573CE 2001 3 7 20010205CW016 120010104G55312707 RIB BBAVIA8 8KCAB 2110612CE VERTICAL STAB CRACKED B K NONE O OTHER ININSP/MAINT 1 GL2168ND 2760 2760 66892 DURNING ANNUAL INSPECTION , TAIL FIN FABRIC WAS FOUND BUCKLING APPROX 1 INCH AFT OF TOP LEADING EDGE. UPON FABRIC REMOVAL FOR HIDDEN DAMAGE INSPECTION THE FIN RIB WAS FOUND TO BE CRACKED AND BUCKLED AT FWD ATTACHING WELD. FURTHER INSPECTION REVEALED AFT ATTACHING WELD TO BE CRACKED ALSO, SUSPECTED CAUSE TO BE EXCESSIVELY TIGHTENED DRAG WIRES. 1H71 3O A21CE 20010307005762001030700576SO 2001 3 7 20010205CW019 120010116G5753 BEARING GULSTMG1159 G1159B 3953535SO LT FLAP TRACK BROKEN B K NONE O OTHER ININSP/MAINT 1 CE014NR 185 255 NOTICED INBOARD ROLLER BEARING ON LEFT FLAP TRACK, B, WAS MISSING THE OUTER CASING AND BEARING...ONLY STUD REMAINED, CAUSE IS UNKNOWN. RECOMMEND THAT ROLLER BEARINGS ARE VISUALLY INSP AT EACH PRE-FLIGHT INSPECTION AND MOVED WITH FINGERS TO CHECK FOR BINDING. NEW ROLLER/PN 1159SCC22821 WHICH SUPERCEEDS THE 1159CC2289 PURGED STOCK OF -9 BEARINGS. 2L72 4F RTA12EA 20010307005822001030700582CE 2001 3 7 20010206CW003 120010108G3720C6685090101 INDICATOR CESSNA182 182R 2072731CE INSTRUMENT PANELREADS LOW B K NONE O OTHER ININSP/MAINT 1 EA214776T4169 R18201762 WHILE COMPLYING WITH AD, 3.5 MINIMUM VACUUM COULD NOT BE OBTAINED, EVEN AT SEA LEVEL. TROUBLESHOOTING REVEALED VACUUM INDICATOR WAS 2-2 1/2 IN HG LOW AND REGULATOR HAD BEEN MIS-ADJUSTED. INSTALLED NEW GAGE, WHICH WAS CALIBRATED, AND RESET REGULATOR DOWN. STANDBY SYSTEM RETESTED, OK. 1L71 3O NT3A13 20010307006782001030700678CE 2001 3 7 20010206CW005 120010112G5330101120108601 SKIN BEECH 200 200BEECH 1152920CE LT WING DEBONDED B K NONE O OTHER ININSP/MAINT 1 GL2325KA BB783 LEFT WING UPPER INBOARD SKIN, ABOVE AUX. FUEL TANK, DEBONDING. INSTALLED DOUBLER. 1L72 4T A24CE 20010307005852001030700585EA 2001 3 7 20010206CW006 220010111G8530LW16740 EXHAUST VALVE LYC BEECH 80 65A80 1152808CE LYC O720 IO720A1B 41546EA CYLINDER BROKEN B K NONE O OTHER ININSP/MAINT 1 GL15134BA 216 LD202 147554A EXHAUST VALVE BROKEN IN HALF. 1L72 3O3 O 3A20 1E15 20010307005872001030700587WP 2001 3 7 20010206CW007 220010115G7320254911842 FUEL CONTROL GARRTT GULSTM690TP 690A 0141722SW GARRTTTPE331TPE33110 01514WP RT ENG MALFUNCTIONED B K NONE O OTHER ININSP/MAINT 1 SO0381448 337 11327 P79656 WHILE DOING OVERSPEED GOVERNOR CHECK, ENGINE RPM STAYS ABOVE TAKEOFF, PROP GOVERNOR HIGH, AND WILL NOT REDUCE WHEN POWER LEVER AND CONDITION LEVER ARE RETARDED. THIS CONDITION ALSO PREVENTS THE PROP FROM COMING OFF THE LOCKS. TROUBLE SHOOTING HAS DETERMINED THAT THE INLET SENSOR AND THE PROP GOVERNOR ARE NOT THE CAUSE OF THIS MALFUNCTION ANDTHE FUEL CONTROL IS, INDEED THE PROBLEM. REPLACED FUEL CONTROL, RAN AND ADJUSTED AS REQUIRED. 1H72 3T4 T 2A4 E4WE 20010307005912001030700591SO 2001 3 7 20010206CW008 120010111G32421331317 STATOR EMB 120 EMB120 3260201SO BRAKE ASSY CRACKED B K NONE O OTHER ININSP/MAINT 1 SO05 2579 BRAKE ASSEMBLY PN2-1661 FAILED PREMATURELY. NR 2 STATOR CRACKED THROUGH AT 1 RELIEF HOLE, BINDING ON TORQUE TUBE.NOTE: OEM PARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION PN 2-1661. 2L72 4T RTA31SO 20010322001192001032200119 2001 3 22 20010206CW010 420010113G2564 LIFE RAFT HOOVERIND DEFECTIVE B K NONE O OTHER ININSP/MAINT 1 SO19 L301 LIFE RAFT RECEIVED IN PACKAGED CONDITION. THE PACKAGE WAS OPENED AND FOUND THAT THE MOORING LINE WAS NOT CONNECTED TO THE INFLATION VALVES PULL CABLE. WITHOUT MOORING LINE BEING CONNECTED TO THE INFLATION VALVES PULL CABLES, INFLATION OF THE LIFE RAFT WOULD NOT BE POSSIBLE, IF THE MOORING LINE WAS PULLED DURING A DEPLOYMENT. MAINTENANCE MANUALS SHOULD HAVE ATTENTION OF WORKING PERSONNEL. 20010410000052001041000005EU 2001 4 10 20010206CW012 120010115G6730AC67244 SERVO DUNLOP AEROSPAS355 AS355F1 8680810EU TAIL ROTOR CRACKED B K NONE O OTHER ININSP/MAINT 1 NM07 658 CRACKED DETECTED ON LOWER END OF SERVO BODY ABOVE END. CAP EDDY CURRENT TESTING. 1G72 3U H11EU 20010307005722001030700572EA 2001 3 7 20010206CW014 120010108G2752 BEARING EATON CNDAIRCL600 CL6002B19 EA FLAP ACTUATOR FAILED B K NONE O OTHER ININSP/MAINT 1 GL09 1385 THRUST BEARING FAILURE DUE TO LACK OF LUBRICATION AND POSSIBLE PRE-LOAD CONDITION. 2L72 4F RTA21EA 20010307005972001030700597SW 2001 3 7 20010207CW001 120010119G5320206033110189 STIFFENER BELL 206 206L4 1182110SW FUSELAGE CRACKED D K NONE O OTHER ININSP/MAINT 1 SW192036F1169 52123 CRACK IN TOP OF RIGHT AFT VERTICAL TUNNEL FWD OF BOX BEAM. CRACK WAS FOUND IN THE RADIUS OF THE 206033110189 STIFFENER. MAY BE PRELOAD PROBLEM. 1G71 3U NCH2SW 20010307005982001030700598EA 2001 3 7 20010207CW002 220010122G7414BL68291013 SHAFT D6LN3200 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA MAGNETO LOOSE B K NONE O OTHER ININSP/MAINT 1 SO1559905 364 J199901GR 317652135 THE GEAR AND SHAFT WERE FOUND LOOSE AND RETAINER WASHER WAS LOOSE AND RUBBING ON COIL FINGER. 1L72 3O3 O A20SO E14EA 20010307006262001030700626CE 2001 3 7 20010209CW007 120010111G541205530311 FIREWALL CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA FUSELAGE CRACKED D K NONE O OTHER ININSP/MAINT 1 SW999421Z882 17280267 FOUND 1.8 IN LONG CRACK IN FIREWALL. CRACK IS LOCATED BEHIND COWL SHOCKMOUNT BRACKET AT RIGHT FIREWALL STEP. REPAIRED CRACK IN ACCORDANCE WITH SB. 1H71 3O3 ONT3A12 1E10 20010409004972001040900497CE 2001 4 9 20010209CW009 120010209G5410505403042 BEAM CESSNA421 421C 2076016CE NACELLE CRACKED D K NONE O OTHER ININSP/MAINT 1 SW9926603 0862 AC TOTAL TIME 4800 HRS , CRACK NOTED ON BOTH BEAMS RIGHT AND LEFT OUTBOARD SIDE OF EACH ENGINE. BOTH CRACKS APPROX 1.5 IN LONG. CRACKS IN RADIUS OF BEND OF TOP STRAP OF BEAM ASSEMBLY NEAR JUNCTION OF FORE AND AFT RUNNING ENGINE MOUNT BEAMS. 1L72 3O A7CE 20010322001212001032200121EU 2001 3 22 20010212CW002 120010102G5600F10AZ60200AZ WINDSHIELD AMD FALC10FALCON10 2730101EU GARRTTTFE731TFE731* 01518WP RT FWD WINDSHLD CRACKED G O OTHER O OTHER CRCRUISE 1 GL1987TH 5660 178 AIRCRAFT DEPARTED CMI IN VFR CONDITIONS AND DURING CLIMB OUT THROUGH 15,000 FT, THE CO-PILOT''S FWD WINDSHIELD OUTER PANE CRACKED. PILOT ELECTED TO RETURN TO CMI. AIRCRAFT LANDED WITHOUT INCIDENT. 2L72 4F4 F A33EU E6WE 20010409004472001040900447 2001 4 9 20010212CW003 420010108G3423 WIRE BEECH 36 A36 1151604CE COMPASS CHAFED D K NONE O OTHER ININSP/MAINT 1 SW99128JG E3332 AC FROM FACTORY WITH 18.4 HRS, DURING AN AVIONICS INSTALLATION, DISCOVERED WIRES FOR THE MAGNETIC COMPASS THAT PASS BETWEEN THE GLARESHIELD AND TOP OF INSTRUMENT PANEL ROUTED SO THEY WERE SANDWICHED AND CHAFING BETWEEN THE TWO. RELIEF SPOT IN TOP OF INSTRUMENT PANEL TO ROUTE OTHER WIRING THAT GOES TO GLARESHIELD, BELIEVE TO BE NEEDED ROUTING FOR COMPASS. DUE TO LENGTH OF THE WIRES BEING SHORT, COMPASS WIRES WILL NOT MAKE IT THROUGH THE RELIEFAND BE ABLE TO BE CONNECTED. WE FEEL THESE WIRES WERE MISROUTED DUE TO A MANUFACTURING ERROR. SUSPECT THE WIRE LOOM TO BE TOO SHORT. 1L71 3O 3A15 20010306000782001030600078EA 2001 3 6 20010213CW005 120010105G2752601RR9310318 ACTUATOR CNDAIRCL600 CL6002B19 EA TE FLAPS LACK OF LUBE B K NONE O OTHER ININSP/MAINT 1 GL09 THRUST BEARING FAILURE DUE TO LACK OF LUBRICATION AND POSSIBLE PRE-LOAD CONDITION. 2L72 4F RTA21EA 20010322001262001032200126CE 2001 3 22 20010214CW001 120010118G2140FR81D943ELB4500 HEATER BEECH 58 58 1152740CE CONT O520 IO520* 17032SO ERODED B DFZRO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA09922DN11500 TH922 PILOT SMELLED CABIN HEATER GASES IN AIRCRAFT. INSPECTED FOUND CABIN HEATER(B4500) CERMA KOTE, COMBUSTION CAN WITH HOLE IN AFT AREA OF CAN BY REAR DRAIN. INSTALLED REBUILT HEATER. 1L72 3O3 O 3A16 E5CE 20010327001962001032700196GL 2001 3 27 20010214CW002 320010122G6114A24182 ROD HARTZL HARTZLHCC2Y HCC2YK1 GL PITCH ROD CRACKED B W59RK NONE O OTHER ININSP/MAINT 1 WP07 AW696 AW696 OBSERVED CRACK-LINE INDICATION DURING MAG PARTICLE TESTING. INDICATION APPEARS TO BE A LAMINATION IN MATERIAL DUE TO STRAIGHTNESS OR INDICATION. 5 CP920 20010327001972001032700197 2001 3 27 20010215CW002 420010109G34215546257001 CONNECTOR COLLINS OUTER SHELL CORRODED D K NONE O OTHER ININSP/MAINT 1 GL13 2193 EXCESSIVE CORROSION BUILDS UP ON PINS OF CONNECTOR, SPECIFICALLY PINS N AND P, WHICH RESULTS IN FLAGGING. 20010326003282001032600328EA 2001 3 26 20010215CW003 220010116G8530AEL6510212 CYLINDER PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA HEAD UNSERVICEABLE B MW2RK NONE O OTHER ININSP/MAINT 1 GL174350G1081 288490058 L2749236A A CRACK RUNS FROM TOP SPARKPLUG HOLE AROUND OUTSIDE EXHAUST SEAT TO TOP SPARKPLUG AND CYLINDER WILL SPLIT IN TWO PIECES. 1L71 3O3 O 2A13 E286 20010307006392001030700639SW 2001 3 7 20010215CW004 120010123G5320206040338009 HANGER ASSY BELL BELL 206 206B3 1181506SW TAILBOOM BEARINGMISALIGNED B K NONE O OTHER ININSP/MAINT 1 SO0967330 BP36 5138 MOUNTING HOLES MISALIGNED. PART MUST BE JIG DRILLED AND INSTALLED. THE JIG WAS MISALIGNED AT INSTALLATION. 1G71 3U H2SW 20010321000952001032100095CE 2001 3 21 20010215CW005 120010119G52101144002369 DOOR BEECH 1900 1900C 1154161CE PWA PT6 PT6* 52043EA BOTTOM AT HING CRACKED B S1FRK NONE O OTHER ININSP/MAINT 1 SO33500PR5682 UC139 BOTTOM OF DOOR .5 INCH FROM HINGE ATTACH POINT 3.5IN CRACK. 2L72 4T3 TRTA24CE E2NE 20010326001542001032600154SO 2001 3 26 20010215CW007 120010122G2910166 SNAP RING ELECTROL 166 GULSTMG44 G44 3951502SO FCD 6440 6440* 26003EA CYL PISTON BROKEN D O OTHER O OTHER NRNOT REPORTED 1 NM1069058 105 1291 SNAP RINGS RETAINING PISTONS IN PLACE SNAPED OFF. ONE RING SHOWS SIGNS OF RUST DAMAGE. PARTS LODGED IN CYLINDER-STOPPING PROPER OPERATION. RESULTING IN TOTAL FAILURE OF HYDRAULIC SYSTEM AND EMERGENCY SYSTEMS.CYLINDERS WERE MODIFIED TO ACCEPT ORINGS INSTEAD OF CHEVRON TYPE SEALS. SUSPECT ORING FAILURE, RESULTING IN OVER PSI AGAINST ORING ON RETURN PISTON, FORCING SNAP RING TO FAIL. 1H72 3I3 IO A734 E216 20010326003112001032600311WP 2001 3 26 20010220CW001 120010107G610054H6077 PROPELLER CVAC 340 340CVAC 242270AWP ALLSN 501D 501D22 03005GL HAMSTD54H 54H60 NE VLV 2 HOUSING BLOWN G O OTHER K FLUID LOSS TOTAKEOFF 1 GL23391FL841 278 550640 239764 AIRCRAFT WAS COLD SOAKED, OUTSIDE TEMPERATURE BEFORE DEPARTURE WAS 15 DEGREES. SUBMITTER FEELS THIS WAS A CONTRIBUTING FACTOR TO THIS SEAL BEING DEFECTIVE. COMPANY INITIATED PROCEDURES NOT TO CHANGE PROP BLADE ANGLE UNTIL MINIMUM OF 40 DEGREE OIL TEMPERATURE IS OBTAINED, DEFECTIVE SEAL REPLACED. AC RETURNED TO SERVICE. 2L72 4R4 T 6A6 E282 6 CP906 20010326003272001032600327CE 2001 3 26 20010222CW001 120010125G7602S12345 LEVER CESSNA177 177B 2073708CE LYC O360 O360* 41514EA PANEL BROKEN D K NONE O OTHER ININSP/MAINT 1 SW01160213292 17702479 MIXTURE CONTROL BROKE ON GROUND RUN UP. BREAK APPEARS TO BE DEFECT IN MATERIAL. 1H71 3O3 O A13CE E286 20010410000072001041000007SO 2001 4 10 20010222CW002 120010123G2410635796 COUPLER CONT PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360EB 17025SO RT ENGINE FAILED D O OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 SW99304CW170 306527H 347870153 306527H RT ALTERNATOR FAILED IN FLIGHT AT NIGHT. ALTERNATOR FAILURE CAUSED BY DRIVE COUPLER FAILURE. 1L72 3O3 O A7SO E9CE 20010326003292001032600329EU 2001 3 26 20010222CW003 120010118G79203033356 FUEL FILTER PILATSPC12 PC1245 EU PWA PT6 PT6A66 52043NE DISCHG FUEL FLTRUNBONDED G K NONE O OTHER ININSP/MAINT 1 CE05302PB 302 UPON 100 HOUR INSPECTION, REPLACEMENT OF ENGINE DISCHARGE FUEL FILTER. NEW FILTER FROM 100 HR KIT WAS NOT GLUED TOGETHER. THE TOP AND BOTTOM OF FILTER WERE LOOSE AND COULD BE PULLED OFF. 1L71 3T4 TRTA78EU E26NE 20010410000082001041000008EA 2001 4 10 20010222CW005 220010109G7414103571651 COIL 56LSC200 GULSTM500 500B 0141106SW LYC O540 IO540* 41532EA MAGNETO DAMAGED G K NONE O OTHER ININSP/MAINT 1 SW15411JF 387 H279909ER 101435 269118 MAGNETO REMOVED FROM UNSERVICEABLE ENGINE. DURING INSPECTION TO DETERMINE SERVICEABILITY, FOUND COIL WIRE BROKEN AT POINTS END JUST BEFORE SPADE CONNECTOR. 1H72 3O3 O 6A1 1E4 20010322001292001032200129GL 2001 3 22 20010222CW006 120010110G2750F659 TUBE AMTR VANS VANSRV6 05605AZGL LYC O320 IO320* 41508EA BELOW FLAP BROKEN D K NONE O OTHER ININSP/MAINT 1 CE073891P117 23736 L1220627 FLAP ROD BROKE JUST BELOW UPPER BALL JOINT CAUSING FLAP TO RETRACT ON LANDING. THIS PART IS .3125 X .058 6061 T6 ALUMINUM TUBING AND APPEARS TO BE WEAK AFTER THREADS ARE CUT IN ENDS. 1L71 3O3 O EXPA1L711E12 20010322001302001032200130CE 2001 3 22 20010222CW009 120010108G8011PM2401 STARTER CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA ENGINE INOPERATIVE D O OTHER O OTHER ININSP/MAINT 1 NM03949SP773 773 172S8145 L2812051A PILOT ATTEMPTED ENGINE START, STARTER WOULD NOT ROTATE. MAINTENANCE FOUND STARTER HAD TWO TERMINALS MELTED WHERE THAT ATTACH TO COMMUTATOR BRUSHES. REPLACED STARTER, OPERATIONAL CHECKED SAT. 1H71 3O3 ONT3A12 1E10 20010322001312001032200131 2001 3 22 20010222CW010 420010119G2310551202621 STRINGER CESSNA500 550 2076604CE AFT BAG COMPT CRACKED C U1CMK NONE O OTHER ININSP/MAINT 1 SW17264965215 5500607 DURING SCHEDULED INSPECTION, IT WAS FOUND THAT SUPPORT PN1455078519 HAD CAUSED THE STRINGER AT/FS428.5/ TO CRACK AND PULL ATTACHING RIVETS LOOSE. THE AC, AT FACTORY, HAD ADDITIONAL EQUIPMENT RACKS INSTALLED. IT SHOULD BE NOTED THAT CLOSER ATTENTION SHOULD BE PLACED ON INSPECTING THESE ATTACHMENT POINTS AS THEY MAY OR MAY NOT BE INCLUDED IN AREAS TO LOOK AT DURING SCHEDULED TIMES. 1L72 4F A22CE 20010322001332001032200133SW 2001 3 22 20010223CW001 120010117G5711 SPAR BBAVIA7 7AC 2110102SW CONT C90 C9012F 17009SO MCAULY1B90 1B90* GL 7TH RIB IB END CRACKED D K NONE O OTHER ININSP/MAINT 1 GL151205E4262 7AC4762 45450712 CM7343 DURING INSPECTION, CRACK FOUND ORIGINATING FROM RIB NAIL RUNNING HORIZONTAL. SPAR INSTALLED 5/17/59 1H71 3O3 O A759 E252 5 NP842 20010322001342001032200134EA 2001 3 22 20010223CW002 220010105G732225765362 SERVO CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA FUEL SERVO VAPOR LOCK D O OTHER R PARTIAL RPM/PWR LOSS CRCRUISE 1 NM03567JW163 70217008 172S8187 L2822651A ENGINE START, RUN UP AND TAKEOFF NORMAL, WHEN THROTTLE WAS RETARDED, ENGINE BEGAN TO RUN ROUGH WITH POPPING OUT EXHAUST. MIXTURE WAS READJUSTED WITH NO CHANGE. ADVANCED THROTTLE AND RETURNED TO HOME STATION. LANDING UNEVENTFUL. ENGINE RUN UP AFTER ENGINE HAD COOLED COMPLETELY INDICATED NO DEFECTS, ALL OPERATION NORMAL. MAINTENANCE INSPECTION OF ENGINE FOUND NO DEFECTS. CONCLUDED THAT FUEL VAPORIZATION CAUSED ROUGHNESS AT IDLE IN FLIGHT WITH INCREASED TEMPS, RETARDED THROTTLE AND REDUCED AIRFLOW THRU ENG AS THIS HAS BEEN CONTINUING PROBLEM. COOLING MODIFICATIONS HAVE BEEN ACCOMPLISHED ON AC ENGINE TO INCLUDE INVERTING FUEL FLOW DIVIDER. 1H71 3O3 ONT3A12 1E10 20010322001432001032200143SO 2001 3 22 20010223CW003 120010131G322189137041 MOUNT PIPER PA46 PA46350P SO DRAGLNK FT AREA BROKEN B HE4RK NONE O OTHER ININSP/MAINT 1 SO11 DRAGLINK FITTING AT ENGINE MOUNT BROKEN LOOSE DUE TO HARD LANDING. NEEDS VISUAL INSPECTION OFTEN, POSSIBLE REINFORCEMENT FROM MFG. 1L71 3O RTA25SO 20010322001972001032200197CE 2001 3 22 20010223CW005 120010123G77222870 PROBE BEECH 58 58P 1152744CE CONT O520 TSIO520LB 17040SO NR1 CYL BROKEN D K NONE O OTHER ININSP/MAINT 1 NE014269S650 TJ96 237296R CUSTOMER REPORTED NR1 EGT ON HIS GEM 1200, INOPERATIVE. UPON REMOVAL OF EGT PROBE, ABOUT HALF OF THE PROBE TIP WAS BROKEN OFF AND MISSING. THE ONLY PATH OF EXIT IS THROUGH THE TURBO CHARGER. FURTHER INSPECTION OF THE TURBO CHARGER REVEALED FOD DAMAGE TO THE VANES OF THE EXHAUST TURBINE. THE PROBE WAS REPLACED WITH NEW. THE TURBO WAS REPLACED WITH AN O/H UNIT.NOTE: THESE TURBOS NOT ONLY SUPPLY BOOST TO ENGINE, BUT ALSO PRESSURIZE CABIN AT ALTITUDE. RECOMMEND AN INSPECTION INTERVAL OR TIME/LIFE LIMIT. 1L72 3O3 O A23CE E8CE 20010322002022001032200202SO 2001 3 22 20010227CW005 120010124G2913HYC5005 POWERPACK PIPER PA28 PA28R201 7102816SO LYC O360 IO360C1C 41514EA MOTOR INOPERATIVE B PAIDO OTHER O OTHER LDLANDING 1 EA136320C6861 28R7837157 WHEN LANDING GEAR WAS SELECTED DOWN, GEAR DID NOT EXTEND. EXTENDED LANDING GEAR USING EMERGENCY PROCEDURES. GEAR EXTENDED AND LOCKED. LANDING MADE WITHOUT INCIDENT. FOUND HYDRAULIC POWER PAK MOTOR INOPERATIVE. INSTALLED OVERHAULED HYDRAULIC POWER PAK. GEAR RETRACTION TEST COMPLETED SATISFACTORY. 1L71 3O3 O 2A13 1E10 20010322002052001032200205CE 2001 3 22 20010227CW007 120010202G8010S1577 SOLENOID CESSNA210 210N 2073453CE CONT O520 TSIO520* 17040SO STARTER SHORTED B BOE2K NONE O OTHER ININSP/MAINT 1 GL197235F 21063038 AIRCRAFT CAME IN WITH DEAD BATTERY, FOUND BATTERY OVERHEATED. PUT TEST BATTERY IN AND IMMEDIATELY WENT HIGH DISCHARGE. WHEN STARTER WIRE REMOVED DISCHARGED STOPPED. STARTER WAS SHORTED OUT. UPON FURTHER INVESTIGATION, FOUND STARTER SOLENOID CONTACTS WERE WELDED TOGETHER, CAUSING STARTER TO ALWAYS BE ON THUS SHORTING IT OUT. INSTALLED NEW STARTER RELAY, OVERHAULED STARTER AND INSTALLED NEW BATTERY. AIRCRAFT RUNUP AND ALTERNATOR CHECK OK. 1H71 3O3 O 3A21 E8CE 20010320001042001032000104SO 2001 3 20 20010227SG001 220010129G7414BL3492606 MAGNETO BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO ENGINE FAILED B K NONE L NO TEST ININSP/MAINT 1 SW99931E 256 TC1009 1553646L PILOT REPORTED THAT THE MAGNETO WOULD FAIL ON RUN UP. TROUBLESHOT THE SYSTEM AND FOUND THE MAGNETO INTERIOR COATED IN BRONZE LIKE METAL FLAKES. DETERMINED THAT THE BLOCK BEARING HAD FAILED AND THE ROTOR HAD CHAFED THE POINTS DOWN. THE MAGNETOS HAD BEEN OVERHAULED BY TCM UNDER THEIR WO NO P53955. DISTRIBUTOR BLOCK PN 10-391586 1L72 3O3 ORT3A16 3E1 20010502000302001050200030SO 2001 5 2 20010227SG002 220010131G73146467681A1R PUMP TSIO520M CESSNA206 TU206G 2073357CE CONT O520 TSIO520M 17040SO ENGINE LEAKING D K NONE K FLUID LOSS ININSP/MAINT 1 SW997PAAL451 818076R U20604718 818076R ENGINE DRIVEN FUEL PUMP BEGAN LEAKING FROM SHAFT SEAL. 1H71 3O3 O A4CE E8CE 20010502000322001050200032SO 2001 5 2 20010227SG004 220010115G73146467681A1 PUMP TSIO520M CESSNA206 TU206G 2073357CE CONT O520 TSIO520M 17040SO ENGINE LEAKING D K NONE K FLUID LOSS ININSP/MAINT 1 SW99HCBXK15 U20604404 FUEL LEAK FROM PUMP DRAIN 1H71 3O3 O A4CE E8CE 20010409001352001040900135NE 2001 4 9 20010227SG005 220010201G731431042681 PUMP CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE ENGINE FAILED B K NONE O OTHER ININSP/MAINT 1 SW992GG 1848 PC 5500286 PCE70020 ENGINE OIL PUMP PN: 3104268-1 SN; A1178 WITH 1848.2 HOURS SINCE INSTALLATION FAILED. THE PUMP SEIZED AND CAUSED SHAFT TO SHEAR. PUMP WAS REPALCED WITH OVERHAULED UNIT. 1L72 4F4 F A22CE E1NE 20010322002092001032200209CE 2001 3 22 20010228CW001 120010206G2840535942 RESISTOR CESSNA172 172R 2072401CE LYC O360 IO360A1C 41514EA RT SENDER DEFECTIVE B K NONE O OTHER ININSP/MAINT 1 SO15434ER244 17280655 DURING PHASE 1 INSPECTION, RT FUEL QUANTITY READING WAS ERRATIC. THE SHAFT BEARING OR SEAL WAS FOUND TO BE DEFECTIVE ON THE RT SENDER. THIS APPARENTLY ALLOWED GASOLINE INTO THE SENDER. 1H71 3O3 ONT3A12 1E10 20010409002292001040900229EA 2001 4 9 20010228CW002 220010201G8520LW11026 CRANKCASE PIPER PA30 PA30 7103002SO LYC O320 IO320B1A 41508EA ENGINE CRACKED B K NONE K FLUID LOSS ININSP/MAINT 1 SO0687CW 5168 301639 L349755A DURING ANNUAL INSPECTION, OIL LEAK NOTED AT CRANKCASE AREA FORWARD OF NR2 CYLINDER. AFTER CLEANING AN OBVIOUS 1.5 IN CRACK WAS NOTED. ENGINE WAS REMOVED FOR REPAIRS. LT ENGINE TSMOH 1098.41, 1992 FIREWALL FORWARD, INC. 1L72 3O3 O A1EA 1E12 20010322002102001032200210SO 2001 3 22 20010228CW003 220010201G8520629288 CRANKCASE BEECH 35 M35 1151526CE CONT O470 IO470C 17026SO LT TOP CTR CRKCSCRACKED D K NONE K FLUID LOSS ININSP/MAINT 1 SO069748R5874 D6229 DURING ANNUAL INSP, OIL LEAK NOTED AT TOP OF CRANKCASE, CLEANING AND RERUN, OIL LEAK RETURNED. FOUND 1.25 IN CRACK EXTENDING FROM TOP CENTER CASE BOLT HOLE AT AREA WHERE FUEL FLOW DIVIDER BRACKET ATTACHES. CRACK IN NON-CRITICAL AREA AND WITHIN CRACK LIMITATIONS EXCEPT OIL LEAK IN EXCESS. ENGINE REMOVED FOR REPAIRS/ CRANKCASE RECONDITIONED. 1L71 3O3 O 3A15 E273 20010307006232001030700623SW 2001 3 7 20010228CW005 120010124G6420 YOKE BELL 407 407 SW ALLSN 250C 250C47B GL TAIL ROTOR OUT OF POSITION B K NONE O OTHER ININSP/MAINT 1 NM03407LR1854 53279 INBOARD BEARINGS 2EA WERE FOUND TO HAVE SHIFTED IN YOKE APPROXIMATELY .050 IN OFF CENTER. ONE YOKE BORE WAS WORN BEYOND LIMITS. 1G71 3U3 UO H2SW E1GL 20010409004532001040900453SO 2001 4 9 20010228CW008 120010124G2140A23D047 REGULATOR PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HEATER LEAKING B FFSAK NONE O OTHER ININSP/MAINT 1 AL014501B 318052168 THIS FUEL REGULATOR WAS INSTALLED NEW, AND WHILE PRESSURE TESTING STATIC ON GROUND, IT WAS FOUND TO BE LEAKING FROM SCREW ON TOP OF UNIT. 1L72 3O3 O A20SO E14EA 20010321001322001032100132SO 2001 3 21 20010228CW010 120010116G326067411002 SWITCH PIPER PA28 PA28R201 7102816SO LYC O360 IO360A1A 41514EA LT LANDING GEAR INOPERATIVE B EASRO OTHER N FALSE WARNING LDLANDING 1 EA236320C563 28R783757 UPON EXTENSION OF LANDING GEAR, NO DOWN & LOCKED INDICATION NOTED ON LEFT LANDING GEAR. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LEFT LANDING GEAR DOWN LIMIT SWITCH INTERMITTENT. INSTALLED NEW SWITCH. RETRACTION TEST COMPLETED SATISFACTORY 1L71 3O3 O 2A13 1E10 20010409001742001040900174 2001 4 9 20010228CW011 420010201G2562MN1300LR20 BATTERY ACK CESSNA182 R182 2072734CE LYC O540 IO540* 41532EA ELT CORRODED B AMVRK NONE L NO TEST ININSP/MAINT 1 CE054135C 022105 R18200326 UPON INSPECTION OF ELT AND BATTERIES, WERE FOUND TO BE CORRODED AND SWELLING, THE BATTERY COMPARTMENT IS WET WITH A LIQUID. COMPOSITION OF LIQUID UNKNOWN. ELT IS INSIDE TAIL SECTION OF AC AND NOT SUBJECT TO WATER EXPOSURE. 1H71 3O3 ORT3A13 1E4 20010409002282001040900228EA 2001 4 9 20010301CW001 220010126G8520SL13790A SHAFT CESSNA177 177A 2073706CE LYC O360 O360* 41514EA ENGINE ROCKERS DAMAGED D K NONE O OTHER ININSP/MAINT 1 SO1470847123 17701356 L1992336A ROUGH GRIND FINISH CAUSED ALMOST ALL 8 ROCKER ARM BUSHINGS TO WEAR AND CONTAMINATE OIL WITH BRASS, METAL PARTICLES. BUSHINGS AND ROCKER SHAFTS WERE DEFECTIVE FROM WEAR AND WERE REPLACED. 1H71 3O3 O A13CE E286 20010307005692001030700569 2001 3 7 20010301CW004 420010301G2562E01 ELT BELL 206 206B3 1181506SW ALLSN 250C 250C20 03013GL CABIN CRACKED E AWTAK NONE O OTHER ININSP/MAINT 1 WP2567PJ 300 3966 INSPECTING ELT, FOUND CASE TO BE IN MANY PIECES WITH CRACKS THROUGHOUT ENTIRE UNIT. PLASTIC SEEMS TO BE VERY SOFT AND BRITTLE. THIS IS SECOND ELT OF THIS MAKE AND MODEL THAT HAS BEEN FOUND IN THIS CONDITION DURING TESTING FOR NON OPERATION. 1G71 3U3 U H2SW E4CE 20010321001352001032100135CE 2001 3 21 20010301CW006 120010130G3250HM6 ROD END BEECH 90 65A90 1152908CE PWA PT6 PT6* 52043EA NOSE GEAR STRNG DISCONNECTED D O OTHER O OTHER TXTAXI/GRND HDL 1 SO1711FL 12250 LJ301 NOSE GEAR STEERING ARM BECAME DISCONNECTED DURING TAXI, SENDING AC INTO HARD RIGHT TURN. ROD END BALL AND BUSHING SEPARATED FROM ROD END EYELET. NO ABNORMAL WEAR WAS NOTED. RECOMMEND INSTALLING LARGE DIAMETER WASHER UNDER HEAD OF BOLT FOR RETAINING ROD END EYELET IN CASE OF FAILURE. ROD END IS NOT PART OF NOSE GEAR OVERHAUL, SHOULD BE INSPECTED. 1L72 3T3 T 3A20 E2NE 20010410000102001041000010CE 2001 4 10 20010301CW008 120010301G7920CH48108 OIL FILTER CESSNA210 210L 2073448CE CONT O520 IO520* 17032SO OIL SUMP DEFECTIVE G K NONE O OTHER ININSP/MAINT 1 EA232170S 21061131 PIECES OF SEALANT USED TO SEAL THE INLET AND OUTLET OF THE FILTER, INSIDE THE FILTER FLAKING OFF AND GOING DOWNSTREAM IN THE OIL SYSTEM. PIECES COULD GET INTO THE PRESSURE SYSTEM AND STARVE A BEARING FOR OIL. 1H71 3O3 O 3A21 E5CE 20010327002312001032700231SO 2001 3 27 20010301CW009 120010301G7920CH48110 OIL FILTER PIPER PA38 PA38112 7103812SO LYC O320 O320* 41508EA OIL SUMP FLAKING G K NONE O OTHER ININSP/MAINT 1 EA232602B 3879A0146 FOUND SEALANT MATERIAL IN OIL SUMP DURING NORMAL 50 HR OIL CHANGE. FOUND ON SUCTION SCREEN. SEALANT CAME FROM THE OIL FILTER. AREA THAT SEALS THE INLET TO THE OUTLET AREA OF THE FILTER IS FLAKING OFF AND GETTING STUCK IN THE FILTER AND ON THE OIL SUCTION SCREEN. 1L71 3O3 O A18SO E274 20010327002322001032700232SO 2001 3 27 20010301CW010 120010301G7920CH48110 OIL FILTER PIPER PA38 PA38112 7103812SO LYC O235 O235* 41505EA OIL SUMP DEFECTIVE G K NONE O OTHER ININSP/MAINT 1 EA232596E 3878A0483 SEALANT USED IN MANUFACTURE OF FILTER TO SEAL THE INLET AND OUTLET TO THE FILTER APPEARS TO BE FLAKING OFF. PIECES ARE BEING FOUND INSIDE THE FILTER ON THE PLEATS AND ON THE OIL SUMP SUCTION SCREEN. THESE PIECES COULD GET INTO THE PRESSURE SYSTEM AND STARVE A BEARING FOR OIL. 1L71 3O3 O A18SO E223 20010327002332001032700233CE 2001 3 27 20010301CW011 120010301G7920CH48108 OIL FILTER CESSNA210 T210N 2073456CE OIL SUMP FLAKING G K NONE O OTHER ININSP/MAINT 1 EA235201A 21063305 PIECES OF THE SEALANT USED TO SEPARATE INLET AND OUTLET CHAMBERS INSIDE THE OIL FILTER ARE BREAKING OFF AND ARE BEING FOUND IN THE FILTER PLEATS AND IN THE SUMP ON THE SUCTION SCREEN. THESE PIECES COULD BLOCK AN OIL PASSAGE IN THE PRESSURE SYSTEM AND STARVE A BEARING FOR OIL. 1H71 3O 3A21 20010305000032001030500003CE 2001 3 5 20010302AP001 120010103G571212210624 BULKHEAD CESSNA210 T210M 2073451CE RT WING CRACKED B K NONE O OTHER ININSP/MAINT 1 sw99 6193 FOUND RIGHT WING INBOARD FLAP BELLCRANK BULKHEAD STA.54.75 CRACKED. CRACK WAS LOCATED LEFT LOWER CORNER OF BULKHEAD (LOOKING FWD) AND APPROX. 1.5 INCHES LONG. AIRCRAFT HAS ROBERTSON STOL KIT INSTALLED. SUSPECT HIGHER CABLE TENSIONS BECAUSE OF STOL KIT CONTRIBUTED TO THE CRACKING. THIS IS THE THIRD AIRCRAFT FOUND WITH THIS PROBLEM, ALL WITH SIMILAR AIRFRAME TOTAL TIME. 1H71 3O 3A21 20010302000592001030200059 2001 3 2 20010302AP003 420010104G2215275 MOUNT BEECH 36 36BEECH 1151602CE SERVO MISINSTALLED G K NONE O OTHER ININSP/MAINT 1 SO13111LJ E1822 SERVO MOUNT (KM-275) WAS FOUND INSTALLED INCORRECTLY NOT ALLOWING FULL ENGAGMENT WITH THE SERVO (KS-270). SERVO MOUNT WAS FOUND INSTALLED ON TOP OF SERVO MOUNTING SHELF AND SERVO WAS INSTALLED UNDERNEATH SERVO MOUNTING BRACKET. THE SERVO MOUNTING BRACKET (SHELF) WAS FOUND BETWEEN THE SERVO AND SERVO MOUNT. INSTALLATION INSTRUCTIONS CALLS FOR SERVO (KS-270) AND SERVO MOUNT (KS-270) BE INSTALLED UNDERNEATH SHELF. RESEARCH OF AIRCRAFT RECORDS DID NOT SHOW ANY MAINTENANCE THAT WOULD HAVE RESULTED IN THIS IMPROPER CONFIGURATION. SUSPECT INCORRECT INSTALLATION WAS DONE AT INITIAL INSTALLATION OF THE AUTOPILOT SYSTEM. 1L71 3O 3A15 20010302000602001030200060CE 2001 3 2 20010302AP007 120010109G812098510441 CHECK VALVE ALIDSG CESSNA206 206CESSNA 2073302CE TURBO INLET LEAKING D O OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW99PKMPP704 704 BLO26610 U20603719 TURBO CHARGER OIL INLET DRAINS OIL INTO TURBOCHARGER AT SHUTDOWN. UPON REMOVAL AND INSPECTION, THE CHECH VALVE WAS FOUND TO TAKE ONLY LIGHT AIR PRESSURE TO UNSEAT THE CHECK VALVE AND BLOW BOTH DIRECTIONS THROUGH THE CHECK VALVE. 1H71 3O A4CE 20010409002492001040900249CE 2001 4 9 20010302CW001 120010302G32103450A LANDING GEAR CESSNA206 T206H CE MAINS COLLAPSED G O OTHER O OTHER NRNOT REPORTED 1 AL017255T4 T20608065 MAIN GEARS COLLAPSED ON FLOAT POND ENTRY / EXIT RAMP. INSPECTION FOUND RT AND LT MAIN GEAR ACTUATING CONTROL SHAFTS BROKEN. REPLACED RT AND LT ACTUATING CONTROL SHAFTS ON MAIN GEAR ASSEMBLY. GEAR RETRACTION TESTS COMPLETED SATISFACTORY. 1H71 3O A4CE 20010409002542001040900254SO 2001 4 9 20010302CW003 220010108G7414 DRIVE GEAR CESSNA150 150A 2071804CE CONT O200 O200A 17020SO MAGENTO BROKEN C K NONE W INADEQUATE Q C ININSP/MAINT 1 WP177141X600 15059241 51063AR MAGNETO DRIVE GEAR BROKEN. BROKEN PIECE LODGED BETWEEN CAM GEAR AND GENERATOR GEAR, BREAKING GENERATOR SHAFT, DESTROYING GENERATOR, CAM GEAR AND OIL PUMP COVER. BOTH MAGNETO DRIVE GEARS WERE UNAPPROVED PARTS. PARTS INSTALLED. 1H71 3O3 O 3A19 E252 20010409000772001040900077CE 2001 4 9 20010305CW004 120010212G3110 POTENTIOMETER CESSNA172 172S 2072439CE INSTRUMENT PANELMISINSTALLED B ESMRK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11563SP 172S8416 REPORT THAT RADIO INDICATOR BACKLIGHTING AND RADIO CONTROL BACKLIGHTING HAD NOT WORKED SINCE DELIVERY OF AC. TROUBLESHOOTING, FOUND THAT PIN 1 OF JC005 WAS AT GROUND POTENTIAL, PREVENTING DIMMER POTENTIOMETER FROM FUNCTIONING PROPERLY. REMOVED WIRE FROM CIRCUIT, WIRE THAT HOOKS INTO WARNING / CAUTION ANNUNCIATOR. RADIO LIGHTING WORKED CORRECTLY. THE WAY SWITCH WAS INTERGRATED INTO SYSTEM WAS CAUSING HARD GROUND CONDITION. 1H71 3O NT3A12 20010322002152001032200215SO 2001 3 22 20010305CW011 120010123G7714640925 ADAPTER PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360EB 17025SO 90 TACH DR ADPT FAILED B O OTHER O OTHER NRNOT REPORTED 1 NE012240D88 347970032 807536L 90 DEGREE TACH DRIVE ADAPTER PUT ON AIRCRAFT. WHEN ADAPTER FAILS, THERE IS NO RPM INDICATION TO TACH. PROBLEM APPARENTLY VIBRATION INDUCED. SOME PROVISION SHOULD BE MADE TO REINFORCE UNIT OR RELOCATE IT TO AN AREA NOT AS PRONE TO VIBRATIONS. 1L72 3O3 O A7SO E9CE 20010322002162001032200216SO 2001 3 22 20010305CW012 120010125G7714640925 ADAPTER PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360EB 17025SO 90 TACH ADAPTER FAILED B O OTHER O OTHER NRNOT REPORTED 1 NE012240D121 347970032 807536R 90 DEGREE TACH DRIVE ADAPTER PUT ON AIRCRAFT. WHEN ADAPTER FAILS, THERE IS NO RPM INDICATION TO TACH. PROBLEM, APPARENTLY VIBRATION INDUCED. SOME PROVISIONS SHOULD BE MADE TO REINFORCE UNIT , OR RELOCATE IT TO AN AREA NOT AS PRONE TO VIBRATIONS. 1L72 3O3 O A7SO E9CE 20010409000192001040900019SO 2001 4 9 20010305CW013 120010123G7714640925 ADAPTER PIPER PA34 PA34200T 7103406SO TMECA ARRIELARRIEL1 60030NE TACH GENERATOR FAILED B K NONE O OTHER ININSP/MAINT 1 NE012240D274 347970032 807536R 90 DEGREE TACH ADAPTER PUT ON AIRCRAFT. WHEN ADAPTER FAILS, THERE IS NO RPM INDICATION TO TACH. PROBLEMS APPARENTLY VIBRATION INDUCED. SOME PROVISION SHOULD BE MADE TO REINFORCE UNIT, OR RELOCATE IT TO AN AREA NOT AS PRONE TO VIBRATION. 1L72 3O3 U A7SO E19EU 20010409000522001040900052EA 2001 4 9 20010305CW014 220010305G8550CH48110 OIL FILTER CESSNA172 172 2072402CE LYC O320 O320* 41508EA ENGINE FLAKING D K NONE O OTHER ININSP/MAINT 1 EA23737MP 17269524 UPON INSPECTION OF OIL FILTER AFTER 50 HRS USAGE, FILTER HOUSING DISASSEMBLED FOR INSPECTION AND GASKET / GLUE TYPE MATERIAL NOTED AT MATING FLANGES INSIDE. THIS MATERIAL NOTED IN FILTER ASSEMBLIES NUMBEROF TIMES AND ALSO DRAINED FROM OIL SUMPS, RECOMMEND MFG CHECK AMOUNT OF SEALANT USED AND DESIGN CRUSH TYPE SEAL USED INSTEAD OF MATERIAL THAT CAN FLAKE AWAY AND GO THROUGH OIL SYSTEM. 1H71 3O3 ONT3A12 E274 20010306000222001030600022SO 2001 3 6 20010306AP001 120010112G282067700322 FUEL LINE PIPER PA32 PA32301T 7103209SO BAGGAGE AREA LEAKING D O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW9981573 328024004 PILOT REPORTED STRONG FUEL ODOR IN CABIN. INVESTIGATION REVEALED FUEL LEAKING FROM FLARELESS FITTING SLEEVE AT BULKHEAD FITTING AFT OF FIREWALL BELOW THE NOSE BAGGAGE AREA FLOOR. FUEL WAS CARRIED BACK INTO THE CABIN AREA INSIDE THE PLASTIC CHAFF SLEEVE COVERING THE LINE. THE PLASTIC CHAFF COVER WAS SPLIT IN THE CABIN AREA AND FUEL DRIPPED BEHIND THE SIDE PANEL. REPLACED LINE ASSEMBLY. SUSPECT FLARELESS FITTING SLEEVE BECAME LOOSE DUE TO VIBRATION AND AGE. 1L71 3O A3SO 20010306000232001030600023CE 2001 3 6 20010306AP002 120010112G7160BA4106 AIR FILTER CESSNA150 150L 2071826CE CONT O200 O200A 17020SO ENGINE DAMAGED C K NONE O OTHER ININSP/MAINT 1 SW9918033 15073748 669917A DURING ANNUAL INSPECTION THE AIR FILTER ASSEMBLY WAS REMOVED TO FACILITATE INSPECTION OF CARB AIRBOX AND HEAT VALVE. UPON REMOVAL, IT WAS NOTED THAT THE AIR FILTER FRAME DID NOT HAVE THE GASKET RETAINER LIPS AS REQUIRED BY AD 96-09-06. THE FILTER FRAME WAS MARKED WITH A MANUFACTURERS DATA LABEL IDENTIFYING IT AS A BA-4106 REVISION D. REVISION D IS TERMINATING ACTION FOR THIS AD AND INDICATES THE PRESENCE OF THE GASKET RETAINING LIPS ON THE FRAME. THE MANUFACTURER, WHEN CONTACTED, STATED THAT ALL REV. D FRAME ASSEMBLIES HAD A LETTER L METAL STAMPED IN THE LOWER FLANGE BEFORE ANODIZEING. THIS IDENTIFICATION WAS MISSING.THE SUBMITTER SPECULATES THAT AN UNSCRUPULOUS MISCREANT OBTAINED A REVISION D LABEL IN O 1H71 3O3 O 3A19 E252 20010409001382001040900138CE 2001 4 9 20010306CW001 120010101G2720071230916AGW BELLCRANK CESSNA188 A188B 2073005CE CONT O520 IO520* 17032SO RUDDER WORN D K NONE O OTHER ININSP/MAINT 1 NM094877Q7758 18802613T RUDDER BELLCRANK PN 0712309-16AGW HAD EXTREME WEAR SEVERAL PLACES, BOTH SIDES. WHERE THEY ARE LOCATED THEY ARE DIFFICULT TO INSPECT AND LUBERCATE. MADE INSPECTION PANEL TO BE ABLE TO GAIN ACCESS TO THIS VITAL AREA. FAILURE OF THIS PART WOULD POTENTIALLY CAUSE GROUND LOOP. 1L71 3O3 O A9CE E5CE 20010409002162001040900216 2001 4 9 20010312CW001 420010212G2562ELT910 ELT LKHEEDP3A P3A 5260103NM CABIN UNSTABLE D K NONE O OTHER ININSP/MAINT 1 SW99927AU 151369 ELT SELF ACTIVATED. THIS UNIT WAS SENT TO THE FACTORY FOR WARRANTY REPAIR FOR THE SAME DEFECT 2 MOS EARLIER. AIRCRAFT WAS SITTING ON RAMP WITH NO POWER. ELT WENT OFF AT 2AM. UNITS HAVE A POOR SELF ACTIVATION RATE. 2L74 4T RTA32NM 20010409002222001040900222SO 2001 4 9 20010312CW002 120010213G3244217K221 TIRE GULSTMGV GV SO NLG FAILED B K NONE O OTHER ININSP/MAINT 1 EA11 NOSEWHEEL TIRE HAS SEPARATION OF TREAD FROM CARCUS. BONDING BETWEEN TREAD AND CARCUS DEBONDED. 2L72 4F RTA12EA 20010409002272001040900227NE 2001 4 9 20010312CW003 220010205G72502A0851 SEAL IAE V2500 V2500A1 NE NR 4 BEARING CRACKED B K NONE O OTHER ININSP/MAINT 1 NE03 PART RECEIVED FROM REPAIR STATION FOR PENETRANT INSPECTION. PART REJECTED 2ND TIME AT PENETRANT INSPECTION FOR INDICATIONS AS MARKED IN RADIUS ADJACENT TO MACHINED FACES OF OIL PASSAGES. 4 F E311NE 20010409002252001040900225NE 2001 4 9 20010312CW004 220010130G72502A0847 SEAL IAE V2500 V2500A1 NE NR4 BEARING CRACKED B K NONE O OTHER ININSP/MAINT 1 NE03 PART RECEIVED FOR PENETRANT INSPECTION. PART REJECTED AT PENETRANT INSPECTION FOR TWO INDICATIONS AT BOTTOM OF COUNTERBORES ON ID OF PART. 4 F E311NE 20010409002262001040900226NE 2001 4 9 20010312CW005 220010130G72502A0851 SEAL IAE V2500 V2500A1 NE NR4 BEARING CRACKED B K NONE O OTHER ININSP/MAINT 1 NE03 PART RECEIVED FOR PENETRANT INSPECTION. PART REJECTED AT PENETRANT INSPECTION FOR INDICATIONS AS MARKED IN RADIUS ADJACENT TO MACHINED FACES OF OIL PASSAGES. 4 F E311NE 20010409001022001040900102EU 2001 4 9 20010312CW009 120010129G5540 BRACKET EIRVON20 PIK20D 5760206EU RUDDER HINGE CRACKED D K NONE O OTHER ININSP/MAINT 1 NM017820D 20602 VIBRATION OF A HARD RUBBER TAIL DOLLY TIRE ASSISTS IN THE FORMATION OF THESE CRACKS. THIS STATEMENT MAY GIVE FALSE SENSE OF SECURITY TO OWNERS WHO ONLY USE PNEUMATIC TIRES, AS WAS THE CASE WITH THIS AIRCRAFT. THREE OF THE FOUR FLANGES WERE CRACKED AND WERE VERY HARD TO SEE, EVEN WITH A 5X MAGNIFICATION. CRACKS WERE HIDDEN UNDER EPOXI RESIN THAT HAD BEEN IN PLACE SINCE NEW. ANY RESIN AND USE OF DYE PENETRANT INSPECTION. 1K00 G31EU 20010405001112001040500111EU 2001 4 5 20010314CW001 120010218G2612B332M FIRE DETECTOR BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL NR 1 ENGINE SHORTED E ALGAK NONE O OTHER ININSP/MAINT 1 SW035416F 794 836063 DURING PRESTART CHECK. AFT PROBE SHORTED TO ELBOW ON ENGINE AIR SYSTEM. 1G72 3U3 UNCH3EU E4CE 20010405001122001040500112SW 2001 4 5 20010314CW002 120010217G6510206061432121 HOUSING BELL 407 407 SW ALLSN 250C 250C47B GL BLOWER CRACKED E ALGAK NONE O OTHER ININSP/MAINT 1 SW03577AL 53247 CAE847167 FOUND DURING ROUTINE MAINTENANCE. BLOWER HOUSING HAD CRACKED. 1G71 3U3 UO H2SW E1GL 20010405001132001040500113SW 2001 4 5 20010314CW003 120010201G5320NAS6606D70 BOLT BELL 214 214ST 1182106SW GE CT7TS CT71 30030NE FUSELAGE BROKEN E ALGAK NONE O OTHER ININSP/MAINT 1 SO03392AL 28114 DURING DAILY INSPECTION, FOUND UPPER RETAINER BOLT, PN NAS6606D70, ON THE FWD NODAL BEAM ASSY HELPER SPRING BROKE, CRACKING THE HELPER SPRING SIDE PLATE AND CAUSING CONTACT DAMAGE TO THE RIGHT TORSION ARM ASSEMBLY. NEED SCHEDULED INSPECTION OR RETIREMENT OF BOTH UPPER AND LOWER BOLTS DUE TO THE HIGH STRESS LOAD ON THESE PARTS. 2G72 4U4 U H10SW E8NE 20010405001142001040500114EU 2001 4 5 20010314CW004 120010126G6520365A33619721 FLANGE AEROSPAS365 AS365N2 8680815EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR G/B WORN E EGRAK NONE O OTHER ININSP/MAINT 1 EA17272NE M538 6435 DURING T INSPECTION, FOUND BOLTS ATTACHING SLIDING FLANGE TO FLEXIBLE COUPLING HAVE LOW TORQUE. COTTER KEYS WERE INSTALLED. SLIDING FLANGE AND FLEXIBLE COUPLING HAVE GROOVES WORN ON ATTACHING SURFACE. REPLACED SLIDING FLANGE, FLEXIBLE COUPLING, AND ATTACH HARDWARE WITH NEW. 1G72 3U3 URTH10EU E19EU 20010322002212001032200221EU 2001 3 22 20010319CW005 120010222G2720 BRACKET PDP 503 SZD503 8821647EU ATTACH BOLT CRACKED G K NONE O OTHER ININSP/MAINT 1 WP01191CM B2198 RUDDER PULLEY CONTROL BRACKET CRACKED AT ATTACH BOLT LOCATIONS. THIS WAS DUE TO LACK OF VARNISH OF THE BRACKETS AND POSSIBLE SHRINKAGE OF MATERIAL. PRIOR TO INSPECTION OF AREA, PILOT REPORTED RUDDER FLUTTER AND STICKING. RECOMMEND INSPECTION OF ALL AIRCRAFT FOR SIMILAR CONDITION. 1K00 RCG02CE 20010405001372001040500137SW 2001 4 5 20010319CW006 120010216G631047620669S CLUTCH BELL BELL 47 47G3B1 1181028SW LYC O435 TVO435B1A 41516EA M/R TRANSMISSIONDAMAGED H ARUAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP1148020 369 B123119 2812 67452C AIRCRAFT IN CRUISE AT 300 FT AGL CLUTCH SLIPPED AUTOROTATION PERFORMED DISASSEMBLED FOUND PARTIAL CONTACT OF CLUTCH/DRUM FACE. DRUM AT MAX LIMITS. MORE CAUTIOUS MEASUREMENT DURING OVERHAUL AND REQUIRED INSPECTION. 1G71 3O3 O 2H3 1E13 20010320000012001032000001SO 2001 3 20 20010320AP001 120010119G2140A23D047 REGULATOR PIPER PA31 PA31350 7103110SO HEATER LEAKING C H DEACTIVATE SYST/CIRCUITS K FLUID LOSS ININSP/MAINT 1 SW99 318152176 THE PROBLEM THAT WE ARE HAVING IS WITH THE HEATER FUEL PRESSURE REGULATORS P/N A23D04-7.5 THEY START LEAKING FUEL AROUND THE HOUSEING. THE FIRST ONE STARTED LEAKING AFTER 180.9 HOURS OF HEATER OPERATION. INSTALLED NEW IN STOCK UNIT, AND IT LEAKED ON FIRST TEST FIRING. WE ALSO JUST HAD ANOTHER UNIT START LEAKING ON ONE OF OUR OTHER PIPER NAVIJO HEATER. THIS UNIT HAD 834.1 HEATER HOURS ON IT WHEN IT STARTED LEAKING. 1L72 3O A20SO 20010320001872001032000187 2001 3 20 20010320AP002 420010215G6113055032110 BULKHEAD CESSNA172 172I 2072426CE SPINNER BROKEN D K NONE O OTHER ININSP/MAINT 1 SW9946230 17257123 SPINNER BULKHEAD WAS FOUND BROKEN AT END NEAR BLADE, WHERE LAST NUTPLATE IS LOCATED. THE BULKHEAD WAS REMOVED AND A NEW ONE ORDERED THROUGH API. THIS PART HAD BEEN REPLACED LESS THAN ONE YEAR EARLIER, APPROX 300 HOURS WERE ON THE PART. WHEN WE RECIEVED THE FACTORY NEW PART WE FOUND A CRACK/DEFECT IN THE EXACT SAME AREA AS WHERE THE BULKHEAD WE WERE REPLACING HAD BROKE. CESSNA PRODUCT SUPPORT WAS NOTIFIED BY US OF THIS PROBLEM, BUT THEY DID NOT SEE THAT IT WAS OF ANY CONCERN. WE STRONGLY FEEL DIFFERENTLY, AND WE BELIEVE THAT THE MACHINARY USED TO MAKE THIS PRODUCT COULD BE INDUCING DAMAGE THAT WILL CAUSE THE PART TO FAIL IN THE FUTURE. 1H71 3O NT3A12 20010409002532001040900253GL 2001 4 9 20010321CW005 320010213G6114C50462 PLATE MCAULY CESSNA182 R182 2072734CE LYC O540 O540* 41532EA MCAULY2D34C B2D34C214 GL PROPELLER HUB MISSING B W59RK NONE O OTHER ININSP/MAINT 1 WP072280T 776894 R18200016 L1928840A 776894 WHILE IN FLIGHT, THE C50462 SPINNER MOUNTING PLATES FAILED, RELEASING THE SPINNER FROM THE AIRCRAFT. THE PROPELLER BECAME LOOSE ON THE CRANKSHAFT DUE TO THE MISSING PLATES. WAS DAMAGED BEYOND REPAIR DUE TO SEVERE FRETTING. A NUMBER OF THE ATTACHING STUDS WERE SKIPPED AS WERE THE CRANKSHAFT BUSHINGS FROM THE SEVERE ABNORMAL LOADS IMPOSED UPON THEM. COMMON TO FIND THE C50462 PLATES CRACKED DURING OVERHAUL OR MINOR REPAIRS. HOWEVER, THIS IS FIRST OF IN-FLIGHT FAILURE KNOWN. 1H71 3O3 ORT3A13 E295 5 CP7EA 20010409002572001040900257GL 2001 4 9 20010321CW006 320010212G6111A2202B RETAINER HARTZL PIPER PA23 PA23250 7102308SO HARTZLHCE2Y HCE2YK2 GL PROP BLADE CRACKED B W59RK NONE O OTHER ININSP/MAINT 1 WP07 C23534 1537 MT INSPECTION REVIELD A CRACK APPROX .1250 INCH LONG ON BOTH SIDES OF RACE MATERIAL. PROPELLER WAS PURCHASED AS A OVERHAULED PROPELLER WITHOUT RECORDS. REPORTED LOST. PURCHASER SUBMITTED PROPELLER FOR OVERHAUL. IN ADDITION TO THIS CRACKED PART, THE BLADES WERE FOUND TO BE 2 INCHES UNDER MINIMUM DIAMETER FOR THE INTENDED APPLICATION. 1L72 3O 1A10 5 CP9EA 20010409004662001040900466GL 2001 4 9 20010322CW012 120010219G273010680009 CARTRIDGE CIRRUSSR SR20 05628AJGL CONT O360 IO360E 17025SO HARTZLHCJ3Y PHCJ3YF1 GL ELEV CONTROL JAMMED B YDSRO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL15109CD1195 1009 357116 JC13A ON RUN UP & PREPARING FOR FLIGHT, ELEVATOR DOWN AUTHORITY COULD NOT BE ACHIEVED UNDER NORMAL CONTROL PRESSURE. PILOT RETURNED AND GROUNDED THE AIRCRAFT FOR MAINTENANCE. INVESTIGATION IDENTIFIED BINDING TO BE LOCATED WITHIN THE PITCH TRIM CARTRIDGE ASSEMBLY PN 10681004. DUE TO FOREIGN OBJECT INTRUSION INTO THE PITCH TRIM CARTRIDGE CUTOUT OPENING IN THE FORM OF A SINGLE DISCARDED COTTER PIN TAILING. WHILE THE PRE-TAKEOFF PITCH TRIM TEST WAS BEING PERFORMED, AND THE ELEVATOR PLACED IN THE NOSE UP ATTITUDE, THE COTTER PIN LODGED. THE AFT SPRING RETAINER IN THE PLACE NOT ALLOWING IT TO RETURN WHEN TRIM WAS COMMANDED DOWN. 1H71 3O3 ONCA00009CHE1CE 5 CP36EA 20010409004672001040900467SW 2001 4 9 20010322CW013 120010202G33402061531 CONNECTOR MOONEYM20 M20R 5870225SW TAIL STROBE SHORTED B K NONE O OTHER ININSP/MAINT 1 NE0591678650 290129 DURING ANNUAL INSPECTION TAIL STROBE LIGHT WAS INOPERATIVE, ELECTRICAL ARCING ACROSS PINS IN CONNECTOR. CONNECTOR WAS LOCATED AT THE PIVOT POINT OF THE TAIL. (TAIL TO FUS MOUNTING AREA), REPLACED BURNT CONNECTOR. SYSTEM NO LONGER AS STROBE SNAP SOUND AT THIS LOCATION. 1L71 3O RT2A3 20010409004762001040900476EA 2001 4 9 20010322CW014 220010206G7414M3548 ROTOR SLICK 4370 PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA MAGNETO SHEARED B UC2RO OTHER R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 GL1941487 98030708 2843179 L3628536A PILOT REPORTED RT MAGNETO TO BE INOPERATIVE DURING GROUND RUNUP. THE ASSIGNED TECHNICAN REMOVED THE RIGHT MAGNETO AND FOUND THE CAM SLOT ON THE ROTOR SHAFT COMPLETELY SHEARED OFF. CAUSE UNKNOWN POSSIBLE PART DEFECT. THIS MAGNETO WAS INSPECTED EVERY 500 HOURS. 1L71 3O3 O 2A13 E286 20010409004772001040900477EU 2001 4 9 20010322CW015 120010216G6510E230397911 SPLINE ADAPTER AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20F 03013GL GEARBOX CRACKED B Y3ARK NONE O OTHER ININSP/MAINT 1 SW03911NW555 555 5082 CAEC20F REMOVED ENGINE ASSEMBLY FOR OIL LEAKS. REMOVED COMPRESSOR AND TURBINE FROM GEAR BOX TO REPLACE SEALS AND ORINGS. INSPECTION OF SPLINE ADAPTOR FOUND CRACK RUNNING APPROX 340 DEGREES AROUND ADAPTOR. TOTAL TIME ON PART IS 555.3 SINCE LAST OVERHAUL AT WHICH TIME THE ADAPTOR WAS REPLACED. CAUSE OF CRACK UNKNOWN AT THIS TIME. 1G72 3U3 U H11EU E4CE 20010409004922001040900492EA 2001 4 9 20010323CW001 220010219G8530AEL651024 CYLINDER PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA ENGINE CRACKED B MW2RK NONE O OTHER ININSP/MAINT 1 GL17 778 778 287916130 L1017539A CYLINDER CRACKED SAME AS PREVIOUS CYLINDERS FROM TOP SPARK PLUG HOLE AROUND OUTSIDE EX SEAT TO BOTTOM SPARK PLUG HOLE. 1L71 3O3 O 2A13 E274 20010409000782001040900078EA 2001 4 9 20010323CW002 220010126G741456LSC200 MAGNETO GULSTM500 500B 0141106SW LYC O540 IO540* 41532EA ENGINE FAILED D K NONE O OTHER ININSP/MAINT 1 SW15667CA 721 1468166 L328148 ENGINE WAS REMOVED FOR TBO DUE WHEN INSPECTED MAGS FOR SERVICEABLILITY. CAN HEAR CLICK INTERNALLY. DETERMIND MAG TO BE UNSERVICEABLE. PREVIOUS EXPERIENCE, SUSPECT LOOSE COIL DUE TO COIL WEAR AT POLAR SHOES. 1H72 3O3 O 6A1 1E4 20010409000822001040900082CE 2001 4 9 20010323CW004 120010227G32521693800297 SHIMMY DAMPENER BEECH 23 B19 1151215CE LYC O320 O320* 41508EA MLG DEFECTIVE D O OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 NM022048A 106 MB904 FOUND MULITUDE OF (AIR) POCKETS AND AIRCRAFT SHIMMIED EXCESSIVELY ON LANDING AND TAXI. 1L71 3O3 O A1CE E274 20010409002002001040900200CE 2001 4 9 20010323CW005 120010214G282063B22623 VALVE CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA FUEL DISTRIBUTIOINOPERATIVE D K NONE O OTHER ININSP/MAINT 1 NM1174GW 665 665 172S8143 62813751A SERVO WAS CLEANED AND RECERTIFIED, WHICH PARTIALLY IMPROVED ENGINE PERFORMANCE. ENGINE STILL BACKFIRED AT 1300-1500 RPM. CLEANED INJECTORS, WITH NO CHANGE. REMOVED AND INSPECTED FUEL DISTRIBUTION VALVE. FOUND SMALL AMOUNT OF LINT PARTIALLY BLOCKING PASSAGES AT NR3 CYLINDER PORT. CLEANED AND REASSEMBLED VALVE. RUNUP AND OPS CHECKS NORMAL. 1H71 3O3 ONT3A12 1E10 20010409002242001040900224CE 2001 4 9 20010323CW011 120010228G2510C1650310101 CYLINDER CESSNA182 182S 2072701CE LYC O540 IO540* 41532EA PILOT SEAT BROKEN H VPFGK NONE O OTHER ININSP/MAINT 1 SO0763CE 1450 18280357 SEAT LOCK CYLINDER PN C1650310101 ON PILOTS SEAT. THE SHAFT ON CYLINDER BROKE WHERE IT GOES INTO THE FORK THAT ATTACHES TO SEAT BACK. 1H71 3O3 ONT3A13 1E4 20010409005052001040900505EU 2001 4 9 20010323CW014 120010215G55211090200059 RIB AGUSTAA109 A109A 0260109EU ALLSN 250C 250C28 03013GL LT ELEVATOR CRACKED D K NONE O OTHER ININSP/MAINT 1 SW9925RX 2526 2526 7220 DURING A WIRING REPAIR TO THE LEFT NAVIGATION LIGHT, A CRACK WAS FOUND UNDER THE VIBRATION DAMPER WEIGHT. NO UNUSUAL VIBRATION HAD BEEN REPORTED PRIOR TO THE CRACK BEING DETECTED. A DAILY INSPECTION OF THE SYNCH ELEVATOR WOULD NOT HAVE REVEALED THIS CRACK, UNTIL THE VIBRATION WEIGHT SEPERATES FROM THE ATTACHING RIB. RECOMMENDED AN INSPECTION BE INCLUDED IN THE MFG INSP PROGRAM TO REMOVE THE SYNCH ELEVATOR TIP CAP AND VISUALLY INSPECT THIS AREA. 1G72 3U3 U H7EU E1GL 20010409002822001040900282CE 2001 4 9 20010323CW015 120010215G5347161102105 LOCK CESSNA172 172S 2072439CE PILOTS SEAT BROKEN D K NONE O OTHER ININSP/MAINT 1 NM03949SP431 172S8145 PILOT REPORTED HIS SEAT LOCK PINS WOULD NOT RELEASE. MAINTENANCE FOUND THE PILOTS SEAT LOCK CONTROL WAS BROKEN. THIS SAME CONTROL WAS REPLACED 431.0 HOURS PRIOR FOR THE SAME PROBLEM. BOTH CONTROL ASSEMBLYS HAVE PN 1611020-05 REPLACE CONTROL ASSEMBLY, OPERATIONAL CHECK SATISFACTORY. 1H71 3O NT3A12 20010409002832001040900283CE 2001 4 9 20010323CW016 120010124G2510161102105 CONTROL UNIT CESSNA172 172S 2072439CE COPILOT SEAT BROKEN D K NONE O OTHER ININSP/MAINT 1 SW99494SP981 981 172S8035 CO-PILOTS SEAT LOCK CONTROL ASSEMBLY WOULD NOT RELEASE SEAT LOCK PIN. MAINTENANCE FOUND THE RIGHT LOCK PIN CABLE BROKEN. REPLACED CONTROL ASSEMBLY PN161102105. THIS HAS BEEN A REOCCURRING PROBLEM ON NEW SEATS. 1H71 3O NT3A12 20010409002932001040900293CE 2001 4 9 20010323CW017 120010108G801185009614 STARTER CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA ENGINE INOPERATIVE D O OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW99949SP773 773 172S8145 L2812051A PILOT ATTEMPTED ENGINE START. FIRST FLIGHT OF THE DAY, STARTER WOULD NOT ROTATE. MAINTENANCE FOUND STARTER HAD TWO TERMINALS MELTED WHERE THEY ATTACH TO COMMUTATOR BRUSHES. REPLACED STARTER, OPERATIONAL CHECKED SAT. 1H71 3O3 ONT3A12 1E10 20010409003062001040900306SO 2001 4 9 20010323CW019 220010223G8520653129 CRANKSHAFT CONT O360 IO360DB 17025SO ENGINE CRACKED H K NONE O OTHER ININSP/MAINT 1 SW99 1863 808785R SUBJECT CRANKSHAFT HAS A 1.5 INCH CRACK IN NR6 ROD JOURNAL AT A 45 DEGREE ANGLE. ENGINE WAS REBUILT PRIOR TO MSB005C APPLICABILITY. CRANKSHAFT NOT APPLICABLE PER SN. 3 O E1CE 20010327004252001032700425CE 2001 3 27 20010326AP001 120010323G76025038901223 CONTROL UNIT BEECH 58 58 1152740CE RIGHT MALFUNCTIONED B O OTHER O OTHER NRNOT REPORTED 1 SW997MG 60 TH513 PILOT REPORTED THAT THE CONTROL WAS HARD TO MOVE. FOUND IN THE LOGS THAT THE INSTALLER HAD LUBED THE CONTROL. LUBRICATION WILL GUM UP THE DRY LUBE AND MAKE IT HARD TO MOVE. 1L72 3O 3A16 20010409000552001040900055EU 2001 4 9 20010326CW003 120010130G5711D21200380 SPAR CAP WSK M18A M18A EU WSK ASZ62 ASZ62IRM18 NE WING CENTER BOX CRACKED B K NONE O OTHER ININSP/MAINT 1 SO09518094229 1Z00915 DURING REPAIRS OF THE WING CENTER SECTION FOR CORROSION DAMAGE TO THE TRAILING EDGE SECTION OF THE WING AND DURING HIDDEN DAMAGE INSPECTION, FOUND .1250 INCH DEEP CRACK IN THE FORWARD LOWER SPAR CAP. THE CRACK RAN APPROX 24 INCHES INBOARD IN A SPANWISE DIRECTION FROM THE LEFT LOWER WING ATTACH FITTING. CRACK PASSED THROUGH 2 BOLT HOLES IN THE SPAR THAT ATTACH THE LOWER WING ATTACH FITTING. CRACK IN SPAR CAP WAS CONFIRMED BY NDI INSP USING EDDIE CURRENT, AND DYE PENETRANT METHODS. LOWER SPAR CAP WAS REPLACED WITH NEW PZL PART AND WING CENTER SECTION WAS RETURNED TO SERVICE. RECOMMEDN A CLOSE INSPECTIONOF ALL WING ATTACH FITTINGS AND SPAR CAPS DURING ANY INSPECTION ON THIS AC. 1L71 3O3 RNCA47EU E10NE 20010409000592001040900059SW 2001 4 9 20010326CW005 120010326G5711 SPAR BBAVIA7 7EC 2110120SW CONT C90 C90* 17009SO RT WING CRACKED D K NONE O OTHER ININSP/MAINT 1 GL0370824 7EC337 DURING ANNUAL INSPECTION, FOUND COMPRESSION CRACKS ON THE RIGHT WING REAR SPAR AT TOP LOCATION ON TOP SIDE OF SPAR. THIS COMPRESSION CRACK WAS HIDDEN UNDER OLD SPAR VARNISH AND WOULD HAVE BEEN MISSED IF TOP INSPECTION HOLES WERE NOT INSTALLED. 1H71 3O3 O A759 E252 20010409003952001040900395CE 2001 4 9 20010327CW009 120010108G2842 TRANSMITTER CESSNA150 150A 2071804CE CONT O200 O200A 17020SO LT FUEL TANK DEFECTIVE D K NONE O OTHER ININSP/MAINT 1 NM038067F4757 15064167 661557A AC LANDED SHORT OF RUNWAY AFTER ENGINE QUIT. AC HAD SUBSTANTIAL DAMAGE NO INJURIES. DETERMINED AC RAN OUT OF FUEL DUE TO FAULTY FUEL GUAGE. REMVD FUEL QUANTITY TRANSMITTER TO FUNCTION TEST. FOUND TWO RUB SPOTS ON FLOAT, REASON FOR CONTACT BETWEEN FLOAT AND TANK APPEARS TO BE MISALIGNMENT OF FLOAT ARM. FOUND CONTACTOR DIMPLE HAD WORN THROUGH. CAUSE OF FUEL GUAGE TO STICK AT HALF TANK INDICATED COMBINATION OF FLOAT CONTACTING INSIDE OF FUEL TANK AND CONTACTOR BEING WORN THROUGH. RESEARCHING LOG FOUND SENDING UNIT HAD BEEN REMOVED 1 YEAR PRIOR & NEW GASKET INSTALLED. RECOMMEND FOR RECURRENCE PREVENTION: KNOWING SERVICE LIFE OF TRANSMITTERS & VERIFICATION OF NO INTERFERENCE OF FLOAT & INSIDE OF FUEL TANK.1H71 3O3 O 3A19 E252 20010409004072001040900407CE 2001 4 9 20010327CW010 120010129G7910047051 ENGINE CESSNA182 182P 2075816CE CONT O470 O470S 17026SO MCAULY2A34C 2A34C203 GL NACELLE DEFECTIVE H K NONE L NO TEST ININSP/MAINT 1 NM1196118 18263409 464601 744427 FACTORY NEW ENGINE GROUND TESTED ONLY. PROPELLER WILL NOT CYCLE. HAVE RECHECKED PROPELLER AND GOVERNOR. PROBLEM APPEARS TO BE ENGINE OIL PRESSURE, INSUFFICIENT TO CYCLE PROPELLER. WARRANTY RETURN. 1H71 3O3 ONTTA13 E273 5 CP3EA 20010409004822001040900482SO 2001 4 9 20010327CW011 120010208G8011 BRACKET PIPER PA28 PA28R201 7102816SO LYC O360 IO360C1C6 41514EA STARTER UNSECURE D K NONE O OTHER ININSP/MAINT 1 WP07962PA 2844022 L2858251A THE FORWARD 1 FT STARTER ATTACH BOLT WHICH HOLDS THE ALTERNATOR BRACELET IS STRIPPING THE CASE OUT DUE TO VIBRATION. HELICOILS ARE BEING INSTLLED BUT ARE NOT HOLDING. A SHELF NEEDS TO BE CUT INTO THE CASE TO SEAT A BOLT HEAD SO A NUT AND LOCK WASHER CAN BE INSTALLED. 1L71 3O3 O 2A13 1E10 20010409005372001040900537NE 2001 4 9 20010328CW001 220010130G73225704931 CARBURETOR PWA R985 R985* 52008NE HARTZLHCB3R HCB3R304 GL ENGINE LEAKING H K NONE K FLUID LOSS ININSP/MAINT 1 AL05 489 ENGINE FLOODED WITH FUEL AND DIED. FUEL LEAKING FROM CARBURETOR WHEN FUEL SELECTOR VALVE TURNED TO ON. 3 R 5E1 5 CP28EA 20010409005422001040900542EU 2001 4 9 20010328CW002 120010125G3213AIR131368 PISTON JETAIRJETSTMJETSTM4101 1500501EU MLG STRUT DAMAGED D FW1RK NONE O OTHER ININSP/MAINT 1 NE03 MLG STRUT RECEIVED WITH INTERNAL DAMAGE. UNIT RECEIVED W/O 5606 OIL BUT NO APPARENT DISASSEMBLY OF THE GEAR HAD OCCURED. (GLAND NUT AND FILL PLUGS INTACT). INTERNAL PARTS WERE DRY. THE FLUTTER VALVE WAS FOUND LOOSE IN THE TOP OF THE CYLINDER WITH THE UPPER CARRIER BEARING HELD IN PLACE BY THE CYLINDER LINER. THE CYLINDER LINER HAD TO BE MACHINED TO BE REMOVED FROM THE CYLINDER. THE UNIT WAS SHIPPED FOR OVERHAUL AFTER THE AXLE WAS OVERHEATED WITH A WHEEL BEARING FAILURE. 2L72 4T RTA41NM 20010409004962001040900496CE 2001 4 9 20010328CW006 120010222G562010243016215 WINDOW BEECH 58 58P 1152744CE CONT O520 TSIO520* 17040SO CABIN FAILED B MQ3RA UNSCHED LANDING O OTHER CRCRUISE 1 WP1140PG 2666 TJ309 AIRCRAFT HAD BEEN CRUISING AT FL240 FOR 1 HOUR PLUS TEMP-40 DEGREE. ON DESCENT OUT OF FL200 THE LEFT MID CABIN WINDOW BLEW OUT OF AIRCRAFT, CABIN DEPRESSURIZATION. PILOT CONTINUED DESCENT TO LOWER ALTITUDE AND LANDED WITHOUT FURTHER INCIDENT. WINDOWS WEW INSPECTED IN NOVEMBER, 2000 AT 2636.9 HRS. AND WERE FOUND TO BE IN GOOD CONDITION. 1L72 3O3 O A23CE E8CE 20010409003752001040900375EU 2001 4 9 20010328CW012 120010308G2913704A33690004 BELT SNIAS 350 AS350BA 8680817EU LYC LTS101LTS101600A3 41560NE HYD SYSTEM SEPARATED D O OTHER J WARNING INDICATION NRNOT REPORTED 1 WP1957717237 1334 L43402CE HYDRAULIC BELT FAILED AT BOND LINE DURING FLIGHT WHICH LEAD TO PRECAUTIONARY LANDING. BELT CONDITION AND TENSION APPEARED NORMAL DURING PREFLIGHT. 1G71 3U3 UNCH9EU E5NE 20010409003022001040900302NE 2001 4 9 20010328CW013 120010228G65107610105101041 BLADE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL TAIL ROTOR DELAMINATED D MV1RK NONE O OTHER ININSP/MAINT 1 EA1738 2436 760087 ON PRE-FLIGHT INSPECTION FOUND AN AREA OF DELAMINATION AT TAIL ROTOR BLADE STATION 27.00, 4.5 INCHES FROM LEADING EDGE OF TAIL ROTOR BLADE. ITS SIZE ABOUT .7500 INCH. BLADE REMOVED AND SENT FOR REPAIR. 1G72 3U3 U H1NE E1GL 20010409002452001040900245EA 2001 4 9 20010402CW001 220010205G7414S6LN1258 MAGNETO PIPER PA60 PA60602P 7106015NM LYC O540 IO540* 41532EA RT ENGINE BROKEN D K NONE L NO TEST ININSP/MAINT 1 WP01858CH124 608265006 RT ENGINE, LT MAGNETO POINT CAM FOLLOWER ARM BROKE AFTER 124.9 HOURS USE. MAGNETO OVERHAULED. INSTALLED 6-2-99 AT 2180.1 HOURS. FAILED AND REMOVED AT 2305.0 HOURS. 1M72 3O3 ORTA17WE 1E4 20010409003342001040900334CE 2001 4 9 20010403CW004 120010308G243523080005 STARTER GEN RAYTHNDH125 HAWKER800XP CE GARRTTTFE731TFE731* 01518WP LT ENGINE DESTROYED H A UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW019292X1081 563 258315 AT FLIGHT LEVAL 390, CREW FELT A VIBRATION IN THE AIRCRAFT, AIRCRAFT DIVERTED. MAINTENANCE FOUND LEFT ENGINE STARTER GENERATOR DESTROYED. GENERATOR WAS REPLACED, GROUND CHECK NORMAL. THE GENERATOR CARRIES A TBO OF 1000 HOURS. THIS TIME IS RARELY ACHIEVED. 2L72 4F4 FRTA3EU E6WE 20010409003362001040900336SO 2001 4 9 20010403CW006 120010131G2432455211 CONTACTOR PIPER PA34 PA34220T 7103420SO CONT O360 TSIO360* 17025SO BATTERY DAMAGED B SO5RK NONE O OTHER ININSP/MAINT 1 NE03292CA543 3449017 BATTERY MASTER CONTACTOR INTERMITTANT. REMOVED AND INSPECTED CONTACTOR. FOUND BOTTOM COVER FULL OF WATER AND CONTACTS RUSTED. INSTALLED NEW CONTACTOR, OPERATIONAL CHECK SATISFACTORY. INSPECTED AFT BAGGAGE DOOR SEAL AND SURROUNDING SKIN SEAMS FOR SOURCE OF WATER LEAK ONTO RELAY SHELF LOCATED BENEATH BAGGAGE FLOOR. NO LEAKS NOTED, CARPET AND INTERIOR DRY. SUSPECT GPU PLUG DOOR JUST FORWARD OF RELAY SHELF TO BE PROBABLE CAUSE FOR WATER INFILTERATION. 1L72 3O3 O A7SO E9CE 20010409003382001040900338SO 2001 4 9 20010403CW008 120010315G3230492303 VALVE PIPER PA44 PA44180 7104402SO LYC O360 O360A1D 41514EA MLG MALFUNCTIONED D O OTHER J WARNING INDICATION NRNOT REPORTED 1 SO15243AT100 100 4496042 PILOTS REPORTED THAT LANDING GEAR WOULD NOT EXTEND, THEY THEN PULLED THE EMERGENCY EXTENSION VALVE AND THE GEAR LOWERED WITH THREE GREEN. UPON INSPECTION FOUND THE EMERGENCY GEAR EXTENSION VALVE TO BE, SPRAYING HYDRAULIC FLUID IN NOSE BELOW HEATER. THIS IN TURN DEPLENISHED ALL FLUID IN RESERVOIR AND BURNED UP HYDRAULIC POWERPAK. SUSPECT INCORRECT ORING IN VALVE. 1L72 3O3 O A19S0 E286 20010409003432001040900343SO 2001 4 9 20010403CW012 220010224G8520 ROD CESSNA421 421B 2076014CE CONT O520 TSIO520H 17040SO RT ENGINE DEPARTED D K NONE O OTHER ININSP/MAINT 1 GL155988M 421B0231 AIRCRAFT ARRIVED WITH RIGHT ENGINE OIL LEAK. FOUND OIL LINE TO BE LEAKING. REPAIRED OIL LINE AND SERVICED BACK UP WITH OIL. ENGINE WAS RERUN AND A ROD CAME LOOSE AND PENETRATED THE CRANKCASE. NO OTHER INFORMATION WAS RECEIVED, EXCEPT THAT THE ENGINE RAN OUT OF OIL DURING FLIGHT, WHICH PROBABLY CAUSED THE ROD TO SEPERATE. AN OVERHAULED ENGINE WAS RECEIVED AND INSTALLED. 1L72 3O3 O A7CE E8CE 20010409003442001040900344SO 2001 4 9 20010403CW013 120010222G324616105800 WHEEL PIPER PA23 PA23250 7102308SO LYC O540 IO540* 41532EA MLG BROKEN B K NONE O OTHER ININSP/MAINT 1 GL09639543180 277854085 PILOT NOTICED RIGHT BRAKE GRABING WHILE TAXIING OUT FOR DEPARTURE. AFTER STOPPING TO INVESTIGATE, NOTICED A BULGE ON THE INSIDE RIGHT WHEEL HALF. WHILE TAXIING BACK TO THE HANGER, THE BEAD AREA LET GO AND THE TIRE DEFLATED. AN 8 INCH PIECE BROKE OFF AT THE BEAD. THE PILOT STATED THAT A RATHER HARD LANDING HAD OCCURED JUST BEFOR THIS FLIGHT BUT DID NOT CAUSE ANY OTHER DAMAGE. 1L72 3O3 O 1A10 1E4 20010409003452001040900345CE 2001 4 9 20010403CW014 120010220G533010704 SKIN RKWELLNA265 NA26565 7630107CE FUSELAGE CRACKED B UVVRK NONE O OTHER ININSP/MAINT 1 CE0374VC 1500 46517 UPON REMOVAL OF INOPERABLE GPS ANTENNA FROM AIRCRAFT, THE UPPER COVER SEPARATED FROM THE BASE OF ANTENNA, EXPOSING THE INSIDE. THE INSIDE OF THE ANTENNA WAS FULL OF RUST FROM BASE. THE MOUNTING SURFACE OF THE ANTENNA WAS ALSO RUSTED, CAUSING THE AIRCRAFT UPPER SOCK SKIN TO CORRODE. SUSPECT OVER TORQUE OF MOUNTING SCREWS CAUSED THE COVER TO CRACK, ALLOWING MOISTURE TO ENTER AND RUST ANTENNA FROM INSIDE OUT. RECOMMEND INSPECTING OF THESE TYPE ANTENNAS UPON INSTALLATION, TO ASSURE THAT SCREWS ARE NOT OVER TORQUED AND HAD CRACKS. 2L72 4J A2WE 20010409003482001040900348CE 2001 4 9 20010403CW016 120010226G5711 SPAR CAP CESSNA150 150G 2071816CE CONT O200 O200* 17020SO RT WING CORRODED D K NONE O OTHER ININSP/MAINT 1 CE073232X10054 15064632 CORROSION FOUND EXFOLIATING SPAR CAP OR RIGHT WING HEAVY CORROSION ON UPPER CABIN CARRY THRU STRUCTURE. VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON CANTED BULKHEAD AT FUSLAGE STATION 20.5 BOTTOM FUSELAGE. AIRCRAFT IS BEYOND ECONOMICAL REPAIR. A SEARCH OF AIRCRAFT REGISTRY SHOWS IT SPENT 18 YEARS IN FLORIDA AND REMAINDER ON EAST COAST. CURRENT OWNER PURCHASED AIRCRAFT AFTER BEING TOLD THAT IT HAD NO CORRROSION BY THE SELLER. 1H71 3O3 O 3A19 E252 20010409003492001040900349CE 2001 4 9 20010403CW017 120010226G5711 SPAR CESSNA150 150G 2071816CE CONT O200 O200* 17020SO RT WING CORRODED D K NONE O OTHER ININSP/MAINT 1 CE073232X10054 15064632 CORROSION FOUND EXFOLIATING (1) SPAR CUP ON RIGHT WING HEAVY CORROSION ON UPPER CABIN (2) CARRY THRU STRUCTURE. (3) VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON (4)CANTED BULKHEAD AT FUSELAGE STATION 20.5 BOTTOM FUSELAGE. AIRCRAFT IS BEYOND ECONOMICAL REPAIR. A SEARCH OF AIRCRAFT REGISTRY SHOWS IT SPENT 18 YEARS IN FLORIDA AND REMAINDER ON EAST COAST. CURRENT OWNER PURCHASED AIRCRAFT AFTER BEING TOLD THAT IT HAD ON CORROSION, BY THE SELLERS. 1H71 3O3 O 3A19 E252 20010409003502001040900350CE 2001 4 9 20010403CW018 120010226G5532 SKIN CESSNA150 150G 2071816CE CONT O200 O200* 17020SO VERTICAL STAB DAMAGED D K NONE O OTHER ININSP/MAINT 1 CE073232X10054 15064632 CORROSION FOUND EXFOLIATING (1) SPAR CAP ON RIGHT WING HEAVY CORROSION ON (2) UPPER CABIN CARRY THRU STRUCTURE. (3) VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON (4)CANTED BULKHEAD AT FUSELAGE STATION 20.5 BOTTOM FUSELAGE. AIRCRAFT IS BEYOND ECONOMICAL REPAIR. A SEARCH OF AIRCRAFT REGISTRY SHOWS IT SPENT 18 YEARS IN FLORIDA AND REMAINDER ON EAST COAST. CURRENT OWNER PURCHASED AIRCRAFT AFTER BEING TOLD THAT IT HAD NO CORROSION BY THE SELLERS. 1H71 3O3 O 3A19 E252 20010409002032001040900203CE 2001 4 9 20010403CW019 120010226G5312 BULKHEAD CESSNA150 150G 2071816CE CONT O200 O200* 17020SO FUSELAGE DAMAGED D K NONE O OTHER ININSP/MAINT 1 CE073232X10054 15064632 CORROSION FOUND EXFOLIATING (1) SPAR CAP ON RIGHT WING HEAVY CORROSION ON (2) UPPER CABIN CARRY THRU STRUCTURE. (3) VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON (4)CANTED BULKHEAD AT FUSELAGE STATION 20.5 BOTTOM FUSELAGE. AIRCRAFT IS BEYOND ECONOMICAL REPAIR. A SEARCH OF AIRCRAFT REGISTRY SHOWS IT SPENT 18 YEARS IN FLORIDA AND REMAINDER ON EAST COAST. CURRENT OWNER PURCHASED AIRCRAFT AFTER BEING TOLD THAT IT HAD NO CORROSION BY THE SELLERS. 1H71 3O3 O 3A19 E252 20010409003582001040900358CE 2001 4 9 20010404CW001 120010206G27206565007188 CONTROL CABLE CESSNA500 550 2076604CE COCKPIT MISINSTALLED D K NONE W INADEQUATE Q C ININSP/MAINT 1 SW99829CB1108 5500829 DURING PHASE 5 INSPECTION, PILOTS RIGHT FORWARD RUDDER CABLE FOUND INCORRECTLY ROUTED THROUGH ACCESS HOLE IN WEB INSTEAD OF CABLE GUIDE BELOW HOLE. CABLE HAD CHAFED INTO LOWER EDGE OF HOLE IN WEB AND DOUBLER. DOUBLER REPLACED AND WEB REPAIRED, CABLE REPLACED. 1L72 4F A22CE 20010409003592001040900359SO 2001 4 9 20010404CW002 120010228G55215423224 SPAR PIPER PA31 PA31350 7103110SO ELEVATOR CRACKED B K NONE O OTHER ININSP/MAINT 1 SO05350MN3073 318152042 INSPECTION FOUND BOTH ELEVATOR SPARS CRACKED. INITIAL INSPECTION ADVISED AT 2500 HOURS TT. THIS WAS FIRST INSPECTION NOTE: TOTAL TIME 3073. 1L72 3O A20SO 20010409003282001040900328EA 2001 4 9 20010404CW003 220010219G8530AEL6510241 CYLINDER PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA ENGINE CRACKED B MW2RK NONE O OTHER ININSP/MAINT 1 GL174381L834 288516016 L1341139A CYLINDER CRACKED SAME AS PREVIOUS CYLINDERS, FROM TOP SPARK PLUG HOLE AROUND OUTSIDE EX SEAT TO BOTTOM SPARK PLUG HOLE. 1L71 3O3 O 2A13 E274 20010409003292001040900329EA 2001 4 9 20010404CW004 220010301G8530AEL6510241 CYLINDER PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA ENGINE CRACKED B MW2RK NONE O OTHER ININSP/MAINT 1 GL17800KA1013 288416019 L810539A CYLINDER CRACKED SAME AS PREVIOUS CYLINDERS FROM TOP SPARK PLUG HOLE AROUND OUTSIDE EX SEAT TO BOTTOM SPARK PLUG HOLE. 1L71 3O3 O 2A13 E274 20010409005772001040900577SO 2001 4 9 20010405CW001 220010405G8530646778 ROD CAP BEECH 58 58 1152740CE CONT O520 IO520C 17032SO CYLINDER 2 FAILED B CGHRK NONE O OTHER ININSP/MAINT 1 GL03827TS2206 895 TH836 267167R DURING CRUISE FLT RT ENG NR 2 CYL PISTON CONN ROD BROKE LOOSE FROM CRANKSHAFT, PENETRATED UPPER CRANKCASE. NR2 CYL SEP FROM ENGINE, RESTED IN COWLING. THE FORCE OF CONNECTING ROD COMING THROUGH THE CASE BROKE LEFT MAGNETO OFF ITS BASE AND PUNCHED A HOLE IN THE UPPER COWL. PILOT SECURED ENGINE AND FLEW TO A MAINTENANCE BASE. UPON REMOVING PIECES AND LAYING THEM OUT ON TABLE IT WAS NOTICED ONE OF THE CONNECTING ROD CAP BOLTS DID NOT HAVE THE REMAINS OF A COTTER PIN IN EITHER OF THE SAFETING HOLES. BOLT HEAD HAD BEEN BROKEN OFF(SUSPECTED FROM THE HAMMERING WHEN THE NUT WAS LOOSE). IT WAS ALSO NOTED THAT THREADS OF SAME BOLT, NOT AS DAMAGED AS BOLT ON OTHER SIDE , INDICATING IT UNSCREWED ITSELF. 1L72 3O3 O 3A16 E5CE 20010409004512001040900451NM 2001 4 9 20010406AP001 120010328G2510600N6525501 SEAT BELT DOUG 600N 600N 3027377NM COCKPIT BROKEN D K NONE O OTHER ININSP/MAINT 1 SW99957SD RN011 THE SEAT RESTRAINT SYSTEM ROTARY BUCKLE ASSEMBLY FAILED WHEN THE SCREWS PULLED THROUGH THE BACK PLATE. OTHER SAME TYPE ASSEMBLIES INSPECTED FOUND CRACKED BACK PLATES IN 5 OF THE 6 INSPECTED. 1G71 3U NCH3WE 20010409001702001040900170NE 2001 4 9 20010406CW001 220010201G73143031632B PUMP CESSNA500 550 2076604CE PWA JT8 JT8D15 52051NE RT ENGINE LEAKING B K NONE K FLUID LOSS ININSP/MAINT 1 GL152GG 1848 5500286 PCE70020 METAL FOUND IN FUEL PUMP FILTER. UPON DISASSEMBLY OF FUEL CONTROL / FUEL PUMP FOR REPLACEMENT OF FUEL PUMP FOUND BLUE DYE BETWEEN FUEL PUMP AND FUEL CONTROL INDICATING FUEL CONTROL BEARING WASHOUT DUE TO FUEL PUMP SHAFT SEAL LEAKAGE. THIS REQUIRED SENDING FUEL CONTROL OUT FOR REPAIR. 1L72 4F4 F A22CE E2EA 20010409000922001040900092NE 2001 4 9 20010409AP001 120010205G282026700115 ADAPTER CONAERLA4 LA4200 5110310NE FUEL SYSTEM CRACKED D K NONE KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO159WA 1455 0 520 FUEL SMELL IN CABIN, FUEL STAIN LEFT SIDE OF INTERNAL FUSELAGE AT AND BELOW ADAPTER. VISUALLY INSPECTED PART AND FOUND CRACK AT SUMP DRAIN VALVE FITTING. FUEL LEAKED INTO AND WAS STANDING IN THE HULL. LEAK DETECTED DURING REPAIR OF STRUCTURE IN THAT AREA. 1H71 3O 1A13 20010409003862001040900386GL 2001 4 9 20010409AP003 320010131G6114HCC2YR2CLEUF HUB HARTZL PIPER PA44 PA44180 7104402SO HARTZLHCC2Y HCC2YR2 GL PROPELLER ASSY CRACKED B O OTHER K FLUID LOSS ININSP/MAINT 1 SW99 3592 579 AU6092 AU6092 DURING PREFIGHT PILOT NOTICED GREASE ON BLADE. MECHANIC REMOVED SPINNER AND FOUND CRACK ON RADIUS OF THE HUB. 1L72 3O A19S0 5 CP920 20010409003872001040900387GL 2001 4 9 20010409AP004 320010131G6114HCC2YR2 HUB HARTZL PIPER PA44 PA44180 7104402SO HARTZLHCC2Y HCC2YR2 GL PROPELLER ASSY CRACKED B K NONE O OTHER ININSP/MAINT 1 SW99 3592 579 AU6092 AU6092 DURING PREFIGHT PILOT NOTICED GREASE ON BLADE. MECHANIC REMOVED SPINNER AND FOUND CRACK ON RADIUS OF THE HUB. 1L72 3O A19S0 5 CP920 20010409001682001040900168CE 2001 4 9 20010409CW001 120010226G532005132826 WEB CESSNA172 172N 2072434CE LYC O320 O320* 41508EA FUSELAGE CORRODED D K NONE O OTHER ININSP/MAINT 1 CE07733JC 17268322 CORROSION WAS FOUND ON RIGHT WEB AND STRINGER. REPLACED THESE PARTS LAST YEAR FOR SAME REASON. THE REPLACED HAD BEEN PAINTED WITH EXPOXY PRIMER PRIOR TO INSTALLATION. IT HAS BEEN NOTED THAT ALL PLACES THAT CORRODED BOTH TIME HAD BEEN IN DIRECT CONTACT WITH UPHOLSTERY THAT WAS INSTALLED 2.5 YEARS AGO. SUSPECT FABRIC WAS SPRAYED WITH SOME FORM OF FIRE RETARDENT THAT IS CORROSIVE. 1H71 3O3 ONT3A12 E274 20010409001692001040900169CE 2001 4 9 20010409CW002 120010226G531305120376 STRINGER CESSNA172 172N 2072434CE LYC O320 O320* 41508EA FUSELAGE CORRODED D K NONE O OTHER ININSP/MAINT 1 CE07733JC 17268322 CORROSION WAS FOUND ON RIGHT WEB AND STRINGERS. REPLACED THESE PARTS LAST YEAR FOR SAME REASON. THE REPLACED PARTS HAD BEEN PAINTED WITH EPOXY PRIMER PRIOR TO INSTALLATION. IT HAS BEEN NOTED THAT ALL PLACES THAT CORRODED BOTH TIMES HAD BEEN IN DIRECT CONTACT WITH UPHOLSTERY THAT WAS INSTALLED 2.5 YEARS AGO. SUSPECTS FABRIC WAS SPRAYED WITH SOME FORM OF FIRE RETARDENT THAT IS CORROSIVE. 1H71 3O3 ONT3A12 E274 20010409001712001040900171CE 2001 4 9 20010409CW003 120010226G531305120374 STRINGER CESSNA172 172N 2072434CE LYC O320 O320* 41508EA FUSELAGE CORRODED D K NONE O OTHER ININSP/MAINT 1 CE07733JC 17268322 CORROSION WAS FOUND ON RIGHT WEB AND STRINGERS. REPLACED THESE PARTS LAST YEAR FOR SAME REASON. THE REPLACED PARTS HAD BEEN PAINTED WITH EPOXY PRIMER PRIOR TO INSTALLATION. IT HAS BEEN NOTED THAT ALL PLACES THAT CORRODED BOTH TIMES HAD BEEN IN DIRECT CONTACT WITH UPHOLSTERY THAT WAS INSTALLED 2.5 YEARS AGO. SUSPECT FABRIC WAS SPRAYED WITH SOME FORM OF FIRE RETARDANT THAT IS CORROSIVE. 1H71 3O3 ONT3A12 E274 20010409003242001040900324WP 2001 4 9 20010409CW010 220010228G725030606901 BLADE GARRTTTFE731TFE7315R 01518WP LP TURBINE DAMAGED D K NONE O OTHER ININSP/MAINT 1 GL19 6823 4994 91174 3RD LPT BLADE SEPARATED AT MIDSPAN CAUSING DAMAGE BEYOND LIMITS TO ALL 3RD LPT BLADES. ALSO DAMAGED THE EXHAUST NOZZLE AND 3RD LPT NOZZLE BEYOND LIMITS. 4 F E6WE 20010409003302001040900330SO 2001 4 9 20010409CW011 220010409G8530A20TK99 VALVE GUIDE CONT O520 IO520F 17032SO CYLINDER STUCK D K NONE O OTHER ININSP/MAINT 1 AL03 500 RECEIVED 2 EA CYLINDERS FOR OVERHAUL UPON DISMANTLING WE FOUND BOTH EXHAUST VALVES STUCK . WE HAD TO DRIVE THEM OUT WITH A DRIFT. SN NR 15130 EXHAUST GUIDE SIZE BOTTOM .433 TOP .4365 SN NR 15131 EXHAUST GUIDE SIZE BOTTOM .433 TOP .437 3 O E5CE 20010409004942001040900494SO 2001 4 9 20010409CW012 220010409G8530A22EK99 VALVE GUIDE CONT O520 IO520F 17032SO CYLINDER STUCK D K NONE O OTHER ININSP/MAINT 1 AL03 500 RECEIVED 2 EA CYLINDERS FOR OVERHAUL. UPON DISMANTLING, WE FOUND BOTH EXHAUST VALVES STUCK. WE HAD TO DRIVE THEM OUT WITH A DRIFT. SN 15130 EXHAUST GUIDE SIZE BOTTOM .433 TOP .4365 SN 15131 EXHAUST GUIDE SIZE BOTTOM . 433 TOP .437 3 O E5CE 20010410002752001041000275EA 2001 4 10 20010409CW016 220010306G8530L2744051A CYLINDER CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA ENGINE CRACKED D A UNSCHED LANDING R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 CE07441CA2010 17280441 L2744051 AIRCRAFT WAS 4 MILES FROM AIRPORT WHEN A LOUD BANG WAS HEARD AND THE ENGINE STARTED VIBRATING AND MISSING. PILOT PULLED POWER BACK TO IDLE AND LANDED SAFELY AT AIRPORT. INSPECTED ENGINE AND FOUND NR 3 ENGINE CYLINDER WITH A CRACK, HALF AROUND CYLINDER. THIS CRACK STARTED AT THE 4TH FIN BACK FROM THE TOP SPARK PLUG HOLE AND PARRELLED THE FIN. DUE TO FREQUENT USE ENGINE TBO IS 2200 HOURS. 1H71 3O3 ONT3A12 1E10 20010502000402001050200040CE 2001 5 2 20010410AP001 120010216G282043362 NEEDLE VALVE PREAIR MA45 CESSNA182 182K 2072724CE CONT O470 O470R 17026SO CARBURETOR SEPARATED D O OTHER R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW993087Q52 52 7509409 18258087 815939R OWNER REPORTED ROUGH IDLE AFTER LANDING, ASSUMED THE PROBLEM WAS RELATED TO CARB ICE ON THE GROUND. AIRCRAFT WAS BROUGHT IN FOR ANNUAL INSPECTION AND DURING PRE INSPECTION RUN UP CONFIRMED ROUGH IDLE, BUT SMOOTHED OUT WHEN CARB HEAT WAS APPLIED. DURING INSPECTION FOUND THE CARBURATOR IDLE MIXTURE SCREW, SPRING, AND WASHER HAD FALLEN OUT. THE AIRCRAFT IS BASED AT A HIGH ALTITUDE (5883 FT) AIRPORT AND TO OBTAIN CORRECT IDLE MIXTURE SETTING THE IDLE MIXTURE SCREW HAS LIGHT CONTACT WITH SETTING SPRING. CARBURETOR WAS SUPPLIED WITH FACTORY REMANUFACTURED ENGINE 52.04 HOURS AGO. 1H71 3O3 ONT3A13 E273 20010502000422001050200042CE 2001 5 2 20010410AP002 120010221G531512134083 FLOORBEAM CESSNA210 2105 2073404CE FUSELAGE CORRODED D K NONE O OTHER ININSP/MAINT 1 SW991825Z3783 2050025 DURING ANNUAL INSPECTION DISCOVERED SEVERE INTERGRANULAR CORROSION ON LEFT 4 INCHES OF ANGLE. CORROSION OCCURED PRIMARILY WHERE .25 IN. HI-SHEAR RIVITS ATTACH ANGLE TO BULKHEAD AND WING LIFT STRUT ATTACH FITTING. ANGLE WAS LESS THAN HALF ORIGINAL THICKNESS WHEN REMOVED. LIGHT SURFACE CORROSION NOTED IN ENTIRE AREA. THIS AREA IS VERY CRITICAL AND SHOULD BE INSPECTED VERY THOROUGHLY DURING ALL INPECTIONS.FLOORBOARDS REMOVED AND NEW PART INSTALLED. 1H71 3O 3A21 20010502000432001050200043CE 2001 5 2 20010410AP003 120010222G3010 BOOT CESSNA441 441 2076020CE RT WING LEAKING B K NONE O OTHER ININSP/MAINT 1 SW99835MA 4410343 NOTED FUEL LEAK FROM BEHIND RT WING DE-ICE BOOT. AFTER PEELING BOOT BACK TO RESEARCH LEAK, NOTED NUMEROUS AREAS OF HEAVY CORROSION. AIRCRAFT WAS FERRIED TO FACILITY FOR REPLACEMENT OF LEADING EDGE ASSEMBLY. 1L72 3T RTA28CE 20010417001482001041700148CE 2001 4 17 20010410AP004 120010222G5511073261110 RIB CESSNA182 R182 2072734CE HORIZONTAL STAB CRACKED B K NONE O OTHER ININSP/MAINT 1 SW993621C2249 0280 DURING AN ANNUAL INSPECTION FOUND THE RT HORIZONTAL STABILIZER INBOARD LEADING EDGE RIB CRACKED. DETECTED CRACK DUE TO EXCESSIVE SKIN PLAY AT RIB AND A WORKING FASTNER. CONFIRMED CRACK USING A BORESCOPE. DISASSEMBLED THE EMPENNAGE ENOUGH TO FACILITATE RIB REPLACEMENT. 1H71 3O RT3A13 20010502000442001050200044CE 2001 5 2 20010410AP005 120010222G5730 SKIN CESSNA441 441 2076020CE RT WING CORRODED B K NONE O OTHER ININSP/MAINT 1 SW99835MA3320 3320 4410343 FOUND FUEL LEAK COMING FROM BEHIND THE RT WING DE-ICE BOOT. AFTER PEELING BACK BOOT TO LOCATE LEAK, NOTED SEVERAL AREAS OF HEAVY CORROSION ON LEADING EDGE. FERRIED AIRCRAFT TO FACILITY FOR LEADING EDGE REPLACEMENT. SUSPECT DE-ICE BOOT WAS INSTALLED USING IMPROPER PRACTICES ALLOWING MOISTURE TO GET IN BEHIND BOOT AND BECOME TRAPPED. 1L72 3T RTA28CE 20010502000452001050200045GL 2001 5 2 20010410AP006 120010223G5720 CUFF HOWARDDGA15 DGA15P 4690506GL RT WING STRUT CORRODED D K NONE O OTHER ININSP/MAINT 1 SW9936259 1770 THE STAINLESS STEEL CUFFS ARE ONLY ON THE RT WING STUTS AND THEY PROVIDE PROTECTION FOR THE STRUT WHEN OPENING/CLOSING THE CABIN DOOR. THESE CUFFS ARE NOT BONDED TO THE WING STRUT BUT ARE WRAPPED AROUND THE STRUT AND CRIMPED IN PLACE. WHEN THE CUFFS WERE REMOVED FOR NON-ROUTINE INSPECTION IT WAS FOUND THAT THE WING STRUT WAS SEVERLY RUSTED AND PITTED IN THE AREA UNDER THE CUFFS. 1H71 3R A717 20010419000012001041900001NE 2001 4 19 20010410AP007 120010221G32465003929 WHEEL SKRSKYS70 S70 8143001NE MLG CRACKED C K NONE O OTHER ININSP/MAINT 1 sw99 WHEEL ASSY SENT TO A CERTIFICATED REPAIR STATION FOR EDDY CURRENT INSPECTION. AFTER BUILD-UP, WHEEL AND TIRE ASSY WAS INFLATED TO 140 PSI AND LEFT FOR 12-24 HOUR LEAK CHECK. AFTER 36 HOURS TIRE PRESSURE WAS FOUND TO BE 30-40 PSI, AND A DAMAGED O-RING WAS SUSPECTED. UPON APPLYING 125 PSI, NITROGEN WAS HEARD ESCAPING. APPLYING LEAK DETECTOR REVEALED A CRACK AT LOWER PORTION OF INBOARD WHEEL HALF RETAINING BOLT HOLE. 2G72 4U H2NE 20010502000462001050200046EA 2001 5 2 20010410AP008 220010302G8530 STUD CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA NR 3 CYLINDER BROKEN D O OTHER E VIBRATION/BUFFET DEDESCENT 1 SW991558E 1349 17271046 L109476 PILOT REPORTED BAD VIBRATION ON FINAL APPROACH. UPON INSPECTION IT WAS DISCOVERED THAT THREE OF FOUR OF THE TOP CYLINDER HOLD DOWN STUDS ON THE NR 3 CYLINDER HAD BROKEN OFF AT THE ENGINE CASE. NO INTERNAL DAMAGE WAS FOUND. CAUSE UNKNOWN. 1H71 3O3 ONT3A12 E274 20010502000472001050200047CE 2001 5 2 20010410AP009 120010305G275045A620911 BELLCRANK BEECH MU300 400BEECH CE TE FLAPS CORRODED F K NONE O OTHER ININSP/MAINT 1 SW99406TS3661 RJ6 DURING ''A'' & ''B'' INSPECTION FOUND THAT BOTH INBOARD AND OUTBOARD FLAP BELL CRANKS ON BOTH WINGS HAD EXCCESSIVE PLAY. THIS CONDITION COULD BE OBSERVED WITH FULL CABLE TENSION WITH FLAPS IN FULL DOWN POSITION. WHEN EACH BELLCRANK WAS DISSASSEMBLED FOUND BOTH BEARINGS, BOLT, STEEL INSERT AND ALUMINUM BELL CRANK TO HAVE HEAVY CORROSION. BOTH OUTBOARD BELL CRANKS HAD TO BE REPLACED. 2H72 4F RTA16SW 20010502000482001050200048SO 2001 5 2 20010410AP010 220010308G8530 PISTON CONT O550 TSIOL550B SO NR 4 CYLINDER BROKEN D K NONE O OTHER ININSP/MAINT 1 SW99972 544 544 8020350 ON A FLIGHT FROM EL PASO TO 5T6 THE OIL PRESSURE STARTED TO FLUCTUATE , ON INSPECTION THE OIL FILTER WAS FULL OF ALUM. WHEN THE ENGINE WAS REMOVED & DISMANTLED NR 4 CYLINDER PISTON SKIRT WAS BROKEN OFF THERE WERE NO SIGHS OF ANY PARTS OUT OF ALLIGIMENT OR STUCK PISTON PIN THE CON. ROD NOT BENT THE CYL NO SIGNS OF OVER HEAT OR SUPPER COOLED THE RINGS NORMAL WEAR. 3 O E4SO 20010502000492001050200049CE 2001 5 2 20010410AP011 120010309G323320152 ACTUATOR CESSNA172 172RG 2072438CE MLG CRACKED B K NONE O OTHER ININSP/MAINT 1 SW995169V7298 172RG0458 DURING ACCOMPLISHMENT OF CESSNA SEB 01-2, THE RT MAIN GEAR ACTUATOR WAS FOUND TO BE CRACKED IN THE SADDLE AREA AS OUTLINED IN THE SEB. REMOVED THE ACTUATOR FROM SERVICE AND INSTALLED A NEW ASSEMBLY. 1H71 3O 3A17 20010502000562001050200056CE 2001 5 2 20010410AP012 120010316G2510051421515 SEAT BACK CESSNA172 172S 2072439CE COPILOTS SEAT BENT C K NONE O OTHER ININSP/MAINT 1 SW99789EP1007 172S8135 DURING PHASE 1 MAINTENANCE INSPECTION, CO-PILOTS SEAT BACK WAS RECLINED APPROXIMATELY 4 INCHES FROM FULL UPRIGHT POSITION. FOUND SEAT BACK FRAME P/N 0514215-15 WAS BENT AT THE TOP OF THE RIGHT ATTACH FORGING. 1H71 3O NT3A12 20010502000572001050200057EA 2001 5 2 20010410AP013 220010316G7322 SERVO CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA FUEL FLOW MALFUNCTIONED H K NONE O OTHER ININSP/MAINT 1 SW99949SP 172S8145 L2812051A ENGINE RSA-5AD1 FUEL SERVO WILL NOT MEET SPECIFICATIONS. FUEL FLOW BELOW 1700 RPM IS TOO HIGH. IDLE SPEED AND MIXTURE CAN NOT BE SET TO MFG SPECIFICATIONS WITH SATISFACTORY ENGINE OPERATION. FUEL SERVO REMOVED, SENT FOR REPAIRS. MAJOR REPAIRS ACCOMPLISHED AND SERVO REFLOWED TO PRECISION FLOW SHEET 30075-02 DATED 5 JAN 00. REINSTALLED FUEL SERVO, ADJUSTED IAW MFG SPECIFICATIONS, OPERATIONAL AND FLIGHT CHECKED SATISFACTORY. 1H71 3O3 ONT3A12 1E10 20010502000582001050200058EA 2001 5 2 20010410AP014 220010316G732225765362 FUEL CONTROL CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA ENGINE MALFUNCTIONED H K NONE O OTHER ININSP/MAINT 1 SW99567JW610 172S8187 L2822651A ENGINE RSA-5AD1 FUEL SERVO WILL NOT MEET SPECIFICATIONS. FUEL FLOW BELOW 1700 RPM IS TOO HIGH. IDLE SPEED AND MIXTURE CAN NOT BE SET TO MFG SPECIFICATIONS WITH SATISFACTORY ENGINE OPERATION. FUEL SERVO REMOVED, SENT FOR REPAIRS. MAJOR REPAIRS ACCOMPLISHED AND SERVO REFLOWED TO PRECISION FLOW SHEET 30075-02 DATED 5 JAN 00. REINSTALLED FUEL SERVO, ADJUSTED IAW MFG SPECIFICATIONS, OPERATIONAL AND FLIGHT CHECKED SATISFACTORY. 1H71 3O3 ONT3A12 1E10 20010502000592001050200059EA 2001 5 2 20010410AP015 220010316G732225765361 FUEL CONTROL CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA ENGINE MALFUNCTIONED H O OTHER O OTHER ININSP/MAINT 1 SW99494SP841 172S8035 L2790951A ENGINE RSA-5AD1 FUEL SERVO WILL NOT MEET SPECIFICATIONS. FUEL FLOW BELOW 1700 RPM IS TOO HIGH. IDLE SPEED AND MIXTURE CAN NOT BE SET TO MFG SPECIFICATIONS WITH SATISFACTORY ENGINE OPERATION. FUEL SERVO REMOVED, SENT FOR REPAIRS. MAJOR REPAIRS ACCOMPLISHED AND SERVO REFLOWED TO PRECISION FLOW SHEET 30075-02 DATED 5 JAN 00. REINSTALLED FUEL SERVO, ADJUSTED IAW MFG SPECIFICATIONS, OPERATIONAL AND FLIGHT CHECKED SATISFACTORY. RECOMMEND ALL RSA-5AD1 FUEL SERVO''S BE REFLOWED TO PRECISION FLOW SHEET 30075-02 IMMEDATELY. 1H71 3O3 ONT3A12 1E10 20010502000652001050200065CE 2001 5 2 20010410AP016 120010326G2510161102105 CONTROL HOUSING CESSNA172 172S 2072439CE COCKPIT SEAT BROKEN D K NONE O OTHER ININSP/MAINT 1 SW99948SP1008 172S8144 DURING PHASE 3 INSPECTION FOUND PILOTS SEAT LOCK CONTROL ASSEMBLY P/N 1611021-05 BROKEN. ONE SEAT LOCK PIN WAS ENGAGED AND WOULD NOT RELEASE DUE TO THE ACTUATOR CABLE BROKEN. THIS IS THE 5TH SEAT CONTROL ASSEMBLY THAT HAS FAILED WITH A BROKEN CABLE FOR THIS ORGANIZATION. REPLACED CONTROL ASSEMBLY. 1H71 3O NT3A12 20010502000662001050200066EA 2001 5 2 20010410AP017 220010328G8530CCST041CA CYLINDER LYC O320 O320D2J 41508EA ENGINE CRACKED F A UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW99 1310 CRACK IN CYLIDER EXTENDED FROM BOTH SPARK PLUG BOSSES TO THE EXHAUST SEAT. 3 O E274 20010502000682001050200068SO 2001 5 2 20010410AP019 120010315G7921AE7010201K0240 HOSE PIPER PA31T PA31T2 7103127SO PWA PT6 PT6A135 52043NE LT ENGINE CRACKED C A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW99410CA112 31T8166005 DURING CRUSE FLIGHT THE LT ENGINE LOW OIL PRESSURE WARNING SOUNDED ALERTING THE PILOT TO DROPPING OIL PRESURE. PILOT PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN AND MADE A UNEVENTFUL LANDING. TECHNICICAN INSTALLED A NEW REPLACEMENT INLET OIL COOLER HOSE AND RETURNED AIRCRAFT TO SERVICE. 1L72 3T4 TRTA8EA E4EA 20010502000692001050200069SO 2001 5 2 20010410AP021 220010403G8520655004 CONNECTING ROD CONT O520 IO520D 17032SO ENGINE GOUGED B K NONE O OTHER ININSP/MAINT 1 SW99 0 575948 FACTORY NEW ENGINE WITH 0 HRS TTIS WAS BEING DISASSEMBLED FOR CRANKSHAFT REPLACEMENT UNDER MSB 00-5. THE MAJORITY OF CONNECTING ROD BOLTS COULD NOT BE REMOVED WITH REASONABLE PRESSURE AND HAD TO BE DRIVEN OUT OF THE CAP. INSPECTION REVEALED THAT THE ROD BOLTS EXHIBITED A BURR AND EVIDENCE OF GALLING ON THE SHANK AT THE POINT WHERE THE ROD AND CAP PARTING SURFACE WOULD BE. INSPECTION OF THE CAPS SHOWED DAMAGE EVIDENCED BY SIGNIFICANT GOUGING WHERE THE BOLTS HAD BEEN REMOVED, RENDERING THEM UNSERVICEABLE. 3 O E5CE 20010502000702001050200070EA 2001 5 2 20010410AP022 220010326G7321 DRIVE SHAFT BENDIX DPF2 PIPER PA31T PA31T 7103124SO PWA PT6 PT6A28 EA FUEL CONTROL SHEARED G E ENGINE SHUTDOWN F FLT CONT AFFECTED CLCLIMB 1 GL11484SC A59060 31T7820022 PCE51554 ON CLIMBOUT FROM EANSVILLE, IN AT 12,500 THE PILOT NOTICED HE COULD NOT CONTROL THE RIGHT ENGINE WITH THE POWER LEVER. THE ENGINE WAS SHUT DOWN IN FLIGHT. THE TORQUE WAS REPORTED TO BE 1600 FT LBS AND THE PROPELLER SPEED WAS REPORTED TO BE 2200 RPM. NO OTHER ENGINE INDICATIONS WERE REPORTED. THE OUTSIDE AIR TEMPERATURE WAS -12 DEGREES C AND THE BAROMETRIC PRESSURE WAS 30.27. SHEARED FUEL CONTROL DRIVE SHAFT. 1L72 3T4 T A8EA E4EA 20010502000712001050200071SO 2001 5 2 20010410AP023 120010327G32226528000 STRUT PIPER PA28 PA28140 7102802SO NOSE GEAR CRACKED G K NONE O OTHER LDLANDING 1 GL117373J5518 2824728 THE STUDENT WAS ON HIS FINAL CROSS COUNTRY FLIGHT TO BLOOMINGTON, IN. THE TRAFFIC PATTERN AND FINAL APPROACH WAS NORMAL. THE PILOT FLARED AND TOUCHED THE MAIN GEAR FIRST ON RUNWAY 35 AT BMG. THE NOSE GEAR SETTLED ONTO THE RUNWAY, THE PILOT REACHED FOR THE BRAKE HANDLE WHEN THE NOSE SETTLED LOWER THAN NORMAL AND THE PROPELLER STRUCK THE GROUND. THE PILOT STATED ALL FLIGHT CONTROLS, AND ENGINE CONTROLS WERE NORMAL. THE APPROACH AND LANDING, AS DESCRIBED BY THE PILOT WAS CONFIRMED BY THE TOWER CONTROLLER ON DUTY AT THE TIME OF THE INCIDENT. THE NOSE GEAR INNER LOWER TUBE BROKE. INVESTIGATION REVEALED A POSSIBLE PRE-EXISTING CRACK RESULTING IN NOSE GEAR COLLAPSE. 1L71 3O 2A13 20010502000722001050200072CE 2001 5 2 20010410AP024 120010405G28101009200673 FLOAT VALVE BEECH 200 B200 1152922CE RT NACELLE TANK BENT D K NONE O OTHER ININSP/MAINT 1 SW99773TP295 BB1722 THE FUEL VENT FLOAT VALVE IN THE TOP OF THE RT NACELLE TANK WAS IMPROPERLY INSTALLED. THE FLOAT PIVOT BRACKET WAS BENT. THIS WOULD PREVENT THE VALVE FROM SEATING PROPERLY. THIS WAS ALLOWING FUEL TO TRANSFER INTO THE AUX TANK WHEN EVER THE MAIN TANK WAS FULL. 1L72 4T A24CE 20010417000962001041700096SO 2001 4 17 20010411CW001 220010319G8530530851 LIFTER CESSNA170 170A 2072304CE CONT C145 C145* 17012SO NR 5 CYLINDER BROKEN G K NONE O OTHER ININSP/MAINT 1 SW991228D 19782 AIRCRAFT SUFFERED A LOSS OF OIL PRESSURE. TEARDOWN OF THE ENGINE REVEALED THE HYDRAULIC LIFTER BODY ON THE NR 5 CYLINDER HAD BROKEN. 1H71 3O3 O A799 E253 20010417000132001041700013SO 2001 4 17 20010411CW012 220010206G732225765405 SERVO PIPER PA34 PA34220T 7103420SO CONT O360 LTSIO360RB SO ENGINE CARB INOPERATIVE B O OTHER O OTHER NRNOT REPORTED 1 EA074175D69 3449191 322088 COULD NOT ADJUST OVERLY RIGHT MIXTURE. SENT FOR FACTORY SERVICE. INSTALLED ON AIRCRAFT STILL COULD NOT ADJUST. SENT BACK TO FACTORY FOR REPAIRS. NOTE THESE UNITS ARE INSTALLED ON NEW AIRCRAFT, THIS IS 3RD SET OF SERVOS ON THIS AIRCRAFT. 1L72 3O3 O A7SO E9CE 20010417000142001041700014SW 2001 4 17 20010411CW013 120010227G2450727425 CIRCUIT BREAKER MOONEYM20 M20J 5870219SW LYC O360 IO360A3B6 41514EA MCAULY2D34C B2D34C214 GL ELECTRICAL INOPERATIVE D O OTHER J WARNING INDICATION LDLANDING 1 SO093758H 240930 L2556551A 993197 AIRCRAFT LANDING GEAR FAILED TO EXTEND AND AIRCRAFT LANDED GEAR UP. DURING REMOVAL OF AIRCRAFT FROM RUNWAY, IT WAS NOTED, LANDING GEAR CONTROL CIRCUIT BREAKER WAS OUT. DURING OPERATION OF LANDING GEAR ON JACKS, SYSTEM OPERATED NORMALLY. NOT KNOWN IF CIRCUIT BREAKER WAS PULLED OR TRIPPED. NEW CIRCUIT BREAKER WAS INSTALLED AS PRECAUTIONARY MEASURE. 1L71 3O3 O 2A3 1E10 5 CP7EA 20010417000702001041700070EA 2001 4 17 20010412CW002 220010307G7322105009 CARBURETOR CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA ENGINE DEFECTIVE B AMYRA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 CE0512182159 17261866 L3457327A DURING FLIGHT, AIRCRAFT WAS DOING TOUCH AND GO LANDINGS. PILOT PULLED BACK ON THROTTLE FOR MORE POWER BUT COULD NOT MOVE THROTTLE. LANDED SHORT OF RUNWAY, IN A FIELD. INVESTIGATION OF THROTTLE , FOUND CARBURETOR STUCK IN IDLE POSITION. REMOVED CARBURETOR AND FOUND COPPER BUTTERFLY RUBBING UP AGAINST INTERIOR OF THROTTLE ASSEMBLY. 1H71 3O3 ONT3A12 E274 20010417000752001041700075SO 2001 4 17 20010412CW005 120010111G571166762 SPAR PIPER PA28 PA28235 7102810SO LYC O540 O540* 41532EA WING CENTER BOX CORRODED B MI3RK NONE O OTHER ININSP/MAINT 1 NM0932138 287510014 INSPECTION REVEALED MISSING RIVET HEADS, RUST. CORROSSION ON REAR SPAR AT CENTER SECTION JUNCTION. 1L71 3O3 O 2A13 E295 20010417000772001041700077SO 2001 4 17 20010412CW007 120010111G5310 SPAR PIPER PA28 PA28235 7102810SO LYC O540 O540* 41532EA FUSELAGE CORRODED B MI3RK NONE O OTHER ININSP/MAINT 1 NM0932138 287510014 AFT CARRY THROUGH SPAR AND BAGGAGE DOOR FRAME AND OPPOSITE SIDE ARE RUSTING AND CORRODING AND STEEL FITTINGS UNDER BAGGAGE COMPARTMENT FLOOR. PN 62448-00 PN 62448-01 PN 62618-00 PN 62619-00 PN 62529-00 65383-00 . 1L71 3O3 O 2A13 E295 20010417000782001041700078SO 2001 4 17 20010412CW008 120010111G5310 DOOR FRAME PIPER PA28 PA28235 7102810SO LYC O540 O540* 41532EA FUSELAGE CORRODED B MI3RK NONE O OTHER ININSP/MAINT 1 NM0932138 287510014 AFT CARRY THROUGH SPAR AND BAGGAGE DOOR FRAME AND OPPOSITE SIDE ARE RUSTING AND CORRODING AND STEEL FITTINGS UNDER BAGGAGE COMPARTMENT FLOOR. PN 62488-00 PN 62448-01 PN 62618-00 PN 62619-00 PN 62529-00 PN 65383-00. 1L71 3O3 O 2A13 E295 20010417000802001041700080SO 2001 4 17 20010412CW009 220010301G8530 CYLINDER CESSNA310 310J 2074226CE CONT O470 IO470U 17026SO LT ENGINE LEAKING B K NONE K FLUID LOSS ININSP/MAINT 1 EA23515HW 310J0102 AIRCRAFT LANDED. OIL LEAKING FROM LEFT ENGINE. INSPECTION REVEALED NR 4 CYLINDER VALVE COVER BROKEN DUE TO VALVE ROCKER ASSEMBLY BROKEN FROM CYLINDER BOSS. PROBABLE CAUSE STUCK VALVE OR METAL FATIGUE AT BOSS. 1L72 3O3 O 3A10 3E1 20010417000812001041700081EA 2001 4 17 20010412CW010 220010301G8500 ENGINE PIPER PA31 PA31350 7103110SO LYC O540 IO540* 41532EA RIGHT MAKING METAL B K NONE O OTHER ININSP/MAINT 1 EA23283GT 317952139 AIRCRAFT LANDED. RIGHT ENGINE SHUTDOWN IN FLIGHT, DUE TO LOSS OF OIL PRESSURE. INSPECTION REVEALED METAL CONTAMINATION. 1L72 3O3 O A20SO 1E4 20010417000842001041700084EA 2001 4 17 20010413CW002 120010302G2752SC14000062 BEARING EATON CNDAIRCL600 CL6002B19 EA FLAP ACTUATOR FAILED B VK6RO OTHER O OTHER NRNOT REPORTED 1 GL09 1102 THRUST BEARING FAILURE DUE TO LACK OF LUBRICATION AND POSSIBLE PRELOAD CONDITION. 2L72 4F RTA21EA 20010417000852001041700085CE 2001 4 17 20010413CW003 120010220G32320842102 BELLCRANK CESSNA320 320F 2074516CE CONT O520 IO520* 17032SO NLG BROKEN B OF1RK NONE O OTHER ININSP/MAINT 1 EA173452Q3643 0052 LEFT NOSE GEAR DOOR ROD ATTACH CLEVIS PIN FELL OUT. UPON RETRACTION OF GEAR, LEFT NOSE DOOR FOULED THE RETRACTORY NOSE GEAR AND JAMMED. GEARBOX CONTINUED PULLING UNTIL 0842102 BELLCRANK BROKE. WHEN GEAR WAS EXTENDED NOSE GEAR WOULD NOT EXTEND. DOOR CLEVIS PINS WERE INSTALLED WITH AN 416 PINS INSTEAD OF COTTER PINS AS CALLED OUT BY IFC. 1L72 3O3 O 3A25 E5CE 20010417000862001041700086EA 2001 4 17 20010413CW004 220010305G852069796 DOWEL PIN LYC IO360 IO360L2A EA NR 1 BEARING MISINSTALLED B NX42K NONE W INADEQUATE Q C ININSP/MAINT 1 SO15 2173 L2776751A DURING ENGINE INSPECTION, IT WAS NOTED THAT THE NUMBER ONE MAIN BEARING DOWEL WAS INSTALLED BACKWARDS WITH IN THE CRANKCASE BEARING DOWEL BORE. THE IMPROPERLY INSTALLED DOWEL PREVENTED THE NEW BEARING FROM FULLY SEATING WITHIN THE CRANKCASE BORE. 3 O 1E10 20010417000872001041700087CE 2001 4 17 20010413CW005 120010321G531208130005 BULKHEAD CESSNA310 310K 2074228CE CONT O470 IO470* 17026SO FUSELAGE CRACKED B K NONE O OTHER ININSP/MAINT 1 WP23101JB5921 310K0110 DURING REPLACEMENT OF AIRCRAFT HEATER DUCTING, MECHANIC NOTICED THE RIGHT BULKHEAD AT STA 29.93 UNDER HEATER WAS CRACKED. ALSO CHECKED LEFT SIDE BULKHEAD AT STA 29.93 AND FOUND THAT BULKHEAD CRACKED IN THE SAME LOCATION. NOTE THAT SUPPORT FOR NOSE WHEEL STEERING PULLEY IS ATTACHED TO BULKHEAD NEAR CRACK. MOVEMENT OF PULLEY AND CABLE TENSION MAY CAUSE BULKHEAD TO FLEX. RECOMMEND CHECKING CABLE TENSION DURING INSPECTION OF NOSE WHEEL STEERING SYSTEM. 1L72 3O3 O 3A10 E1CE 20010417000882001041700088CE 2001 4 17 20010413CW006 120010321G531208130004 BULKHEAD CESSNA310 310K 2074228CE CONT O470 IO470* 17026SO FUSELAGE CRACKED B K NONE O OTHER ININSP/MAINT 1 WP23101JB5921 310K0110 DURING REPLACEMENT OF AIRCRAFT HEATER, DUCTING MECHANIC NOTICED THE RIGHT BULKHEAD AT STA 29.93 UNDER HEATER WAS CRACKED. REMOVED HEATER TO GAIN ACCESS TO BULKHEAD. NOTE THAT SUPPORT FOR NOSE WHEEL STEERING PULLEY IS ATTACHED TO BULKHEAD NEAR CRACK. MOVEMENT OF PULLEY AND CABLE TENSION MAY CAUSE BULKHEAD TO FLEX. RECOMMEND CHECKING CABLE TENSION DURING INSPECTION OF NOSE WHEEL STEERING SYSTEM. 1L72 3O3 O 3A10 E1CE 20010417000892001041700089SW 2001 4 17 20010413CW007 120010319G673041001554 HOUSING TEXTRON BELL 214 214B 1182100SW SERVO ACTUATOR CRACKED B K NONE O OTHER ININSP/MAINT 1 NM07 1109B CRACKS DETECTED ON FLANGE MOUNTS. REPLACED SERVO UNIT FROM SURPLUS. 2G71 4U H6SW 20010417001022001041700102EU 2001 4 17 20010413CW010 120010129G243220VR4D BATTERY AMD FALC50FALCON900 2700160EU CELL BLOCK UNAPPROVED PART B JGVRK NONE W INADEQUATE Q C ININSP/MAINT 1 CE09 131 TWO UNAUTHORIZED CELLS INSTALLED IN BATTERY BLOCK. UNAUTHORIZED CELLS REPLACEMENTS PERFORMED USING UNACCEPTABLE PRACTICES. RECOMMEND REPLACEMENT OF ENTIRE CELL BLOCK. 2L73 4F RTA46EU 20010417001032001041700103EA 2001 4 17 20010413CW011 220010327G741410682016 GEAR LYC O540 O540* 41532EA MAGNETO BROKEN D K NONE O OTHER ININSP/MAINT 1 GL23 HAVE FOUND 3 GEARS WITH 1 TOOTH BROKEN. WERE FOUND A 500 HOUR MAG INSPECTION AFTER ENGINE QUIT ON LANDING. FOUND 2 MORE GEARS WITH SEVERAL TEETH MISSING. MAGNETO JUMPED INTERNAL TIME. 3 O E295 20010417001042001041700104CE 2001 4 17 20010413CW013 120010308G3233 ACTUATOR CESSNA172 172R 2072401CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL MLG DISTORTED D K NONE O OTHER ININSP/MAINT 1 SW156189R8567 172RG0109 L2760936A 951813 FOUND CRACKS ON BOTH SIDES OF SADDLE SHAPED HOLE OF ACTUATOR BODY . 1H71 3O3 ONT3A12 E286 5 CP7EA 20010417001122001041700112CE 2001 4 17 20010416CW002 120010416G5540 STRUCTURE CESSNA206 TU206G 2073357CE CONT O520 TSIO520* 17040SO RUDDER DAMAGED D K NONE O OTHER ININSP/MAINT 1 GL1512TL U20606464 THE 206 SEAPLANE RUDDER ASSEMBLY IS PRONE TO DAMAGE AFT OF PN 12310661, DOUBLER AT THE BOTTOM OF THE RUDDER. DAMAGE OF THIS NATURE IS EVIDENT BY A KINK AT THE BOTTOM OF THE RUDDER ON BOTH SIDES. THIS DAMAGE IS CAUSED BY THE WIND WHEN A RUDDER LOCK IS NOT USED. IF RUDDER IS INSTALLED, A RUDDER LOCK SHOULD BE USED WHENEVER AIRCRAFT IS STORED OUTSIDE. ALSO, THIS AREA SHOULD BE CHECKED DURING PREFLIGHT. 1H71 3O3 O A4CE E8CE 20010417001142001041700114SO 2001 4 17 20010416CW006 120010108G5740 ATTACH FITTING PIPER PA32 PA32RT300 7103215SO LYC O540 IO540* 41532EA LT WING CRACKED D K NONE O OTHER ININSP/MAINT 1 EA256873C2451 32R7885034 INSPECTED AIRFRAME, FOUND THREE SEPARATE CRACKS IN THE LEFT WING FORWARD ATTACH FITTING AREA. 1L71 3O3 O A3SO 1E4 20010417001152001041700115CE 2001 4 17 20010416CW007 120010119G554007126161 BULKHEAD CESSNA182 182E 2072712CE CONT O470 O470* 17026SO RUDDER CRACKED D K NONE O OTHER ININSP/MAINT 1 NM039298X4103 18253698 WHILE PERFORMING A PRE PURCHASE LOOKOVER, FOUND A STOP DRILLED CRACK IN THE UPPER RADIUS ABOVE THE LEFT RUDDER STOP BOLT. FURTHER INSPECTION FOUND ANOTHER CRACK RADIATING OUTWARD FROM THE UPPER OUTBOARD EDGE OF THE UPPER RIGHT LIGHTENING HOLE. 1H71 3O3 ONT3A13 E273 20010417001162001041700116NE 2001 4 17 20010416CW009 220010110G7321324476810 FUEL CONTROL BEECH 200 B200 1152922CE PWA PT6 PT6A42 52043NE LT ENGINE INOPERATIVE D A UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 NM0963791 1769 BB1100 93649 DURING TRAINING FLIGHT IN AN EMERGENCY DECENT SIMILATION, THE LEFT ENGINE FLAMED OUT AND COULD NOT BE RESTARTED. REPLACED THE FUEL CONTROL AND OPERATION IS NORMAL. 1L72 4T4 T A24CE E4EA 20010417001172001041700117CE 2001 4 17 20010416CW010 120010313G2750500000863 CONTROL CABLE CESSNA414 414A 2075907CE CONT O520 TSIO520* 17040SO TE FLAPS BROKEN D K NONE O OTHER ININSP/MAINT 1 CE09414JK6160 414A0626 CABLE SNAPPED BY FIRST PULLEY OUTBOARD OF FLAP MOTOR, RIGHT SIDE. NO EVIDENCE OF WEAR OR CORROSION. PULLEY WAS TURNING FREE. FAILURE CAUSED SPLIT FLAPS ON LANDING. 1L72 3O3 O A7CE E8CE 20010417001182001041700118EA 2001 4 17 20010416CW011 220010223G7421RHB37E SPARK PLUG CESSNA206 T206H CE LYC O540 TIO540* 41532EA ENGINE INOPERATIVE D K NONE O OTHER ININSP/MAINT 1 GL13929MA211 T20608107 L1031161A UPON ANNUAL INSPECTION, FOUND 2 SPARK PLUGS NOT WORKING. CERAMIC ON TERMINAL END WAS LOOSE INSIDE THE PLUG. REMOVED AND REPLACED. 1H71 3O3 O A4CE E14EA 20010417001192001041700119GL 2001 4 17 20010416CW012 220010325G732323057869 GOVERNOR HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL ENGINE FAILED D K NONE O OTHER ININSP/MAINT 1 WP095187S C10968DV GOVERNOR FAILURES RANGE FROM 72 HOURS TO 1750 HOURS. 1G71 3U3 U H3WE E4CE 20010417001202001041700120GL 2001 4 17 20010416CW013 220010325G732323057869 GOVERNOR HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL ENGINE FAILED D K NONE O OTHER ININSP/MAINT 1 WP099106Z 800776D GOVERNOR FAILURES RANGE FROM 72 HOURS TO 1750 HOURS. 1G71 3U3 U H3WE E4CE 20010417001212001041700121GL 2001 4 17 20010416CW014 220010325G732323057869 GOVERNOR HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL ENGINE FAILED D K NONE O OTHER ININSP/MAINT 1 WP095200Y 1198D GOVERNOR FAILURES RANGE FROM 72 HOURS TO 1750 HOURS. 1G71 3U3 U H3WE E4CE 20010417002222001041700222GL 2001 4 17 20010416CW015 220010325G732323057869 GOVERNOR HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL ENGINE FAILED D K NONE O OTHER ININSP/MAINT 1 WP094575Z 370094D GOVERNOR FAILURES RANGE FROM 72 HOURS TO 1750 HOURS. 1G71 3U3 U H3WE E4CE 20010417002262001041700226GL 2001 4 17 20010416CW016 220010325G7323230578 GOVERNOR HUGHES369 369D 4470706WP ALLSN 250C 250C20 03013GL ENGINE FAILED D K NONE O OTHER ININSP/MAINT 1 WP095108E 811075D GOVERNOR FAILURE RANGES FROM 72 HOURS TO 1750 HOURS. 1G71 3U3 U H3WE E4CE 20010417002272001041700227CE 2001 4 17 20010416CW017 120010305G2450VR515GA VOLT REGULATOR CESSNA182 182Q 2072732CE CONT O470 O470* 17026SO ELECTRICAL FAILED D K NONE O OTHER ININSP/MAINT 1 WP234603N36 18267280 VOLTAGE REGULATOR WAS INSTALLED, AIRCREW SQUAWKED LOW VOLTAGE WARNNG LIGHT REMAINED ON AT ALL POWER SETTINGS. TROUBLESHOOTING DETERMINED OUTPUT VOLTAGE WAS BELOW MINIMUM OUTPUT AND ERRATIC. VISUAL INSPECTION OF THE REGULATOR INDICATED NO SIGNS OF EXTERIOR DEFECTOR DAMANAGE. NO DISASSEMBLY WAS ATTEMPTED. 1H71 3O3 ONT3A13 E273 20010417002352001041700235EA 2001 4 17 20010416CW018 220010315G7322MA3PA FLOAT CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA CARBURETOR CRACKED D VCTAK NONE O OTHER ININSP/MAINT 1 EA1789061442 442 15282616 1082315 DURING A 50 HOUR INSPECTION, PM CHECK ON AIRCRAFT RUN UP FOUND AIRCRAFT NOT SMOOTH RUN. AFTER CHECKING THE CARB, FOUND CRACKED FLOAT. MADE AIRCRAFT RUN RICH. THIS COULD TURN INTO A DANGER IN THE AIR. THIS REPLACEMENT OF THE OLDER, BETTER BRASS FLOAT WAS NOT GOOD. 1H71 3O3 ONT3A19 E223 20010417000932001041700093CE 2001 4 17 20010417AP002 120010125G5711 SPAR BBAVIA7 7KCAB 21101P3CE WINGS DAMAGED P K NONE O OTHER ININSP/MAINT 1 SW996369N2881 44 WOOD SPARS; NAILS OUT OF LEADING EDGE RIBS; WOODEN SPACERS WERE LEFTOUT OF FIRST FOUR IN-BOARD LEADINGEDGE RIBS; LEADING EDGE LOOSE; NAILSLOOSE; SOMEBODY HAD PATCHED UP BEFORE AND PUT SCREWS INSTEAD OF NAILS ON LEADING EDGE SPARS AND RIBS; SOME RIBS CRACKED; INNER RIB LACING CORDS BROKE; HAVE JUNKED WINGS AND REPLACING WITH NEW METAL SPAR WINGS LATER THIS YEAR. 1H71 3O A759 20010417001462001041700146GL 2001 4 17 20010417AP003 120010411G5610 CANOPY AMTR LONGEZLONGEZ 05690Z8GL LYC O540 IO540* 41532EA CANOPY LATCH FAILED G A UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW995439N240 240 CANOPY SHATTERED IN FLIGHT, DEPARTED AIRCRAFT AND HIT PROP, DESTROYING PROP. PILOT MADE EMERGENCY LANDING. IT APPEARS THE LONG-EZ CANOPY FRAME LATCH PASSED THROUGH THE FRAME AND RESTED ON THE GLASS. THE GLASS SHATTERED. 1M71 3O3 ORTEXPA1M711E4 20010502000772001050200077CE 2001 5 2 20010417AP004 120010412G5210 ROD BEECH MU300 400A 1155402CE PAX DOOR MISSING B O OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 GL15695TA RK310 CABIN DOOR WILL NOT OPEN FROM INSIDE OR OURSIDE. AFT PINS DO NOT RELEASE WHEN HANDLE IS MOVED. FOUND THE ACTUATING ROD MISSING THE ROD END COTTER PIN. REINSTALLED THE PIN AND COTTER PINNED. OPERATION CHECK NORMAL. 2H72 4F RTA16SW 20010417001132001041700113SO 2001 4 17 20010417AP005 120010416G32137873804 STRUT PIPER PA32 PA32301 7103207SO LT MLG CRACKED B K NONE O OTHER ININSP/MAINT 1 CE014291Y3639 328306016 DURING ANNUAL INSPECTION FOUND LEFT LOWER MAIN GEAR STRUT CRACKED AT THE ATTACHMENT OF THE STRUT TO THE AXLE SHAFT. THE STRUT CASTING WAS CRACKED IN TWO DIFFERENT PLACES WITH ONE CRACK MEASURING OVER 1 INCH IN LENGTH. EXAMINATION OF THE RIGHT STRUT FOUND NO DAMAGE. REVIEW OF THE AIRCRAFT MAINTENANCE RECORDS REVEALED A LANDING ACCIDENT SEVERAL YEARS AGO. TECHNICIAN RECOMMENDS DURING INSPECTIONS TO PLAY CLOSE ATTENTION TO MAIN GEAR CASTING. 1L71 3O A3SO 20010423003372001042300337 2001 4 23 20010418CW001 420010418G3422 GYRO CESSNA182 182 2072702CE CONT O470 O470* 17026SO COCKPIT INOPERATIVE D K NONE O OTHER ININSP/MAINT 1 SW016312A 33112 DURING ROUTINE ANNUAL INSPECTION THE ELEVATOR WAS FOUND TO TRAVEL ONLY 19 DEGREE UP. THE TYPE CERTIFICATE CALLS FOR 25 DEGREE. INVESTIGATION FOUND THE D. G. MOUNTED DIRECTLY ABOVE THE CONTROL WHEEL TUBE. AS THE WHEEL WAS PULLED AFT THE AN3-10A BOLT CONTACTED THE D.G. STOPPING THE TRAVEL. 1H71 3O3 ONT3A13 E273 20010424002332001042400233CE 2001 4 24 20010418CW002 120010418G5412 FASTENER CESSNA182 182 2072702CE FIREWALL LOOSE D K NONE O OTHER ININSP/MAINT 1 SW015590B 33590 OWNER REPORTED 2 LOOSE RIVETS AT THE FIREWALL ATTACH POINT STA. 5. INVESTIGATION REVEALED 2 MISSING RIVET HEADS AN426AD4 AND A FURTHER 25 RIVET HEADS HELD ON BY PAINT ALONE. 1 OTHER RIVET HEAD HAD A STRANGE APPEARANCE, SCRAPING THE PAINT OFF REVEALED A BONDO MATERIAL FILLING THE HOLE. THE AIRPLANE HAD BEEN REPAINTED IN ABOUT 1988 BY PERSONS UNKNOWN. 1H71 3O NT3A13 20010424002342001042400234CE 2001 4 24 20010418CW003 120010418G7120 HEAT SHIELD CESSNA182 182 2072702CE ENGINE MOUNT MISSING D K NONE O OTHER ININSP/MAINT 1 SW015590B 33590 THE ENGINE MOUNT HEAT SHIELDS HAD BEEN REMOVED AT SOME POINT ALLOWING HEAT DAMAGE REQUIRING 3 WELD REPAIRS. 1H71 3O NT3A13 20010424002352001042400235CE 2001 4 24 20010418CW004 120010418G2432 WIRE CESSNA182 182 2072702CE CONT O470 O470* 17026SO BATTERY DAMAGED D K NONE O OTHER ININSP/MAINT 1 SW015590B 33590 THE BATTERY CABLE WAS BARE IN MANY PLACES INCLUDING THE PENETRATION OF THE FIREWALL. IT HAD ALSO BEEN PENETRATED BY A SCREW THROUGH THE BELLY OF AIRCRAFT, JUST FORWARD OF THE BATTERY BOX. 1H71 3O3 ONT3A13 E273 20010424002572001042400257 2001 4 24 20010418CW005 420010418G3422 GYRO CESSNA182 182 2072702CE COCKPIT MISINSTALLED D K NONE W INADEQUATE Q C ININSP/MAINT 1 SW015590B 33590 THE DIRECTIONAL GYRO WAS POWERED BY A WIRE OF THREE SIZES NR 12, NR 16 AND NR 18, SPLICED TOGETHER OVER A LENGTH OF 20 INCHES, THE LARGE END WAS BENT INTO A HOOK, TINNED WITH SOLDER AND CONNECTED TO THE AMMETER. 1H71 3O NT3A13 20010424002592001042400259CE 2001 4 24 20010418CW007 120010402G272012606421 SPROCKET CESSNA CESSNA206 206H 2073301CE LYC O540 IO540* 41532EA IDLER MALADJUSTMENT B YFRSK NONE O OTHER ININSP/MAINT 1 SO072446X 08097 EXCESSIVE LEFT RUDDER PETAL PRESSURE REQUIRED TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. FOUND TRIM CHAIN TENSION ADJUSTMENT IDLER SPROCKET SLIPPED IN ADJUSTMENT SLOT. TRIM CHAIN JUMPED POSITION ON STEERING BUNGEE GEAR, CAMPING LIMITED LEFT RUDDER TRIM. RUDDER TRIM RIGGING RESET, AIRCRAFT FLIGHT CHECKED, RUDDER CONTROL SYSTEM AND RUDDER TRIM OPERATION NORMAL. 1H71 3O3 ORTA4CE 1E4 20010424002602001042400260CE 2001 4 24 20010418CW008 120010307G2497 WIRE CESSNA150 150L 2071826CE CONT O200 O200* 17020SO INSTRUMENT PANELCHAFED D K NONE O OTHER ININSP/MAINT 1 WP115427Q 15073327 WIRE SHIELDING CHAFED OTHER WIRES IN SAME BUNDLE CAUSING MULTIPLE SHORTS. OCCURRED IN FORMAL OPERATION. PROBABLE CAUSE WAS SHIELDING ON PB 10 TOUGHER THAN INSOLATION IN OTHER WIRES CAUSING SEVERE WEAR. TO PREVENT RECURRENCE PB 10 NEEDS A SLEEVE OR COVER OVER SHIELDING OR ISOLATE PB 10 FROM THE REST OF THE WIRE BUNDLE. 1H71 3O3 O 3A19 E252 20010424002612001042400261CE 2001 4 24 20010418CW009 120010308G2432S337711 SWITCH CESSNA172 172S 2072439CE COCKPIT INOPERATIVE D K NONE O OTHER ININSP/MAINT 1 NM03789EP1003 1003 172S8135 PILOT REPORTED AVIONICS MASTER SWITCH INOPERATIVE, WHEN BATTERY SWITCH IS TURNED ON, ALL AVIONICS LEFT IN ON POSITION POWER UP REGARDLESS OF AVIONICS MASTER SWITCH POSITION. MAINTENANCE FOUND ONE SIDE OF AVIONICS MASTER SWITCH INOPERATIVE. REPLACED AVIONICS MASTER SWITCH. OPERATIONAL CHECKED SATISFACTORY. 1H71 3O NT3A12 20010424002622001042400262CE 2001 4 24 20010418CW010 120010312G2510051421224 SEAT BACK CESSNA172 172S 2072439CE COCKPIT BENT D K NONE O OTHER ININSP/MAINT 1 NM03789EP1003 1003 172S8135 MAINTENANCE FOUND RIGHT FROMT SEAT BACK RECLINED APPROXIMATELY 4 INCHES FROM NORMAL UPRIGHT POSITION. THE SEAT WAS REMOVED AND INSPECTED, FINDING THE SEAT BACK FRAME BENT. THE FRAME WAS BENT ON THE LEFT SIDE JUST ABOVE THE ATTACH FORGING PN 05142158. REPLACED SEAT BACK FRAME. 1H71 3O NT3A12 20010424002632001042400263CE 2001 4 24 20010419CW001 120010314G270105600145 YOKE CESSNA172 172P 2072436CE LYC O320 O320D2J 41508EA CONTROL COLUMN CORRODED D K NONE O OTHER ININSP/MAINT 1 SO099766212525 17276219 MAINTENANCE TECH FOUND AREA BELOW PIVET BOLT EXCESSIVELY COVERED TO THE POINT OF EXFOLIATION. WHEN DRILLING THE INSPECTION HOLE CALLED FOR, THE DRILL BIT ACTUALLY FELL THROUGH AFTER APPROXIMATELY 2 TURNS OF THE BIT. CENTRAL YOKE WAS REPLACED AT THIS TIME. TECH STRONGLY RECOMMENDS THIS PROCEDURE SHOULD BECOME AN AIRWORTHINESS DIRECTIVE. 1H71 3O3 ONT3A12 E274 20010424002642001042400264SW 2001 4 24 20010419CW005 120010220G3210110538 NUT BBAVIA7 7GCBC 1220601SW LYC O320 O320* 41508EA MLG AXLE MISMANUFACTURED D K NONE W INADEQUATE Q C ININSP/MAINT 1 EA25613PC 125598 FOUND NEW AXLE NUTS TO HAVE CHAMFER CUT ON INSIDE DIAMETER, WHERE NUT CONTACTS BEARING. CONTACTED MFG., CONFIRMED THAT NO CHAMFER SHOULD BE PRESENT ON INSIDE DIAMETER. 1H71 3O3 ONCA759 E274 20010420000762001042000076EA 2001 4 20 20010419CW006 220010319G741410157120Y PINION GEAR BENDIX ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA ENG LT MAGNETO MALFUNCTIONED D K NONE O OTHER ININSP/MAINT 1 AL0171330 C049605 0542 ENGINE QUIT WHEN LEFT MAG WAS SELECTED DURING MAG CHECK AFTER START. RESTART WAS UNEVENTFUL. WITH MAG SWITCH IN BOTH, ENG WOULD NOT DEVELOP POWER, BEGAN BACKFIRING AND AFTERFIRING. ATTEMPT TO CHECK MAG TIMING, FOUND THE ENG LT MAG WOULD ONLY TURN INTERMITTENT WITH ENG. MAG AND ALL SPARK PLUGS WERE REPLACED DUE TO HEAVY LEAD AND CARBON FOULING. LOWER PLUGS HAD LEAD BRIDGING GAP. ENG OPS CHECKED GOOD. PILOT REPORTED HISTORY OF DIFFICULT STARTING. LEFT MAG CONTAINS RETARD POINTS. TEARDOWN FOUND WOODRUFF KEY SLOT IN PINION GEAR WORN TO A WIDTH OF 90 DEGREES ROTATION WITH OVER HALF OF MATERIAL BETWEEN THE GEAR ID AND TEETH GROOVES WORN AWAY. TIMING GEAR TEETH WERE MISSING AND MAG CASE FILLED WITH DEBRIS.1G71 3O3 O H11NM E295 20010424002652001042400265EU 2001 4 24 20010419CW007 120010306G2420P610151 ROTOR AUXILEC AEROSPATR72 ATR72202 8680940EU GENERATOR SHORTED B XC4RK NONE O OTHER ININSP/MAINT 1 SO19 1227 MAIN STATOR WINDINGS ON ROTOR ASSEMBLY SHORTED OUT AFTER 41.8 FLIGHT HOURS, SINCE OVERHAUL. THIS WAS A NEWLY MODIFIED ROTOR. THIS IS A POORLY DESIGNED ROTOR, PREVIOUS PN WAS P603744A, WHICH ALSO HAD A PROBLEM AND CAME APART WHILE IN OPERATION. 2H72 4T RTA53EU 20010420002292001042000229SW 2001 4 20 20010419CW008 120010319G673041002437 LEVER TEXTRON BELL 214 214B 1182100SW SERVO ACTUATOR CRACKED B K NONE O OTHER ININSP/MAINT 1 NM07 1228B CRACKING DETECTED ON TANG EDGE OF LEVER ASSEMBLY. 2G71 4U H6SW 20010424002732001042400273SW 2001 4 24 20010419CW012 120010402G5711 SPAR BBAVIA7 7ECA 21101NNSW LYC O235 O235* 41505EA RT WING CRACKED D K NONE O OTHER ININSP/MAINT 1 SW996309N 233 A LONGITUDINAL CRACK IN THE RIGHT FORWARD WOODEN WING SPAR, APPROXIMATELY 30 INCHES LONG. 1H71 3O3 O A759 E223 20010420002822001042000282WP 2001 4 20 20010419CW013 120010316G6322369A56553 BEARING HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL BLOWER ASSY DAMAGED D O OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 NM02622PB 880318D 831268 DURING SHUTDOWN, A LOUD GRINDING AND POPPING WAS HEARD COMING FROM THE TRANSMISSION AREA. OIL COOLER BLOWER ASSY PN 369025630-101 WAS REMOVED AND DISSASSEMBLED FOR INSPECTION. THE LOWER BLOWER BEARING PN 369A5655-3 HAD FAILED. IT IS SUSPECTED THAT THE BEARING CAGE FAILED AS NUMEROUS PIECES OF CAGE MATERIAL WAS RECOVERED. THIS BEARING HAS A RL OF 1200 HOURS. PART TT AT FAILURE WAS 515.4 BEARING RETAINED FOR 90 DAYS AS EXHIBIT. 1G71 3U3 U H3WE E4CE 20010424002782001042400278NE 2001 4 24 20010420CW001 220010221G7230 COMPRESSOR PWA JT8 JT8D9A 52048NE ENGINE DAMAGED D K NONE O OTHER ININSP/MAINT 1 SO19 48961 P667085 ENGINE WAS RECEIVED AT ENGINE SHOP FOR REPAIR DUE TO SUSPECTED OIL LEAK AS REPORTED BY THE CUSTOMER. DURING THE DISASSEMBLY OF THE HIGH COMPRESSOR MODULE, IT WAS DISCOVERED THAT THE COMPRESSOR DISKS STAGES NUMBER 8 AND 9 EXHIBITED A MELTING CONDITION DUE TO AN EXTREMELY HIGH HEAT EXPOSURE. THE C9 STAGE DISK BORE WAS MELTED COMPLETELY AND ROLLED OUT OF POSITION. 4 F E2EA 20010424002802001042400280SO 2001 4 24 20010420CW003 120010315G33406446 FLUX DETECTOR STEC PIPER PA28 PA28181 7102807SO LYC O360 O360A1D 41514EA LT WING TIP MALFUNCTIONED B PIQRK NONE L NO TEST ININSP/MAINT 1 EA21181LS354 FV5842 2843227 FOUND LONGLIGHT AND STROBES PULLING HSI OFF HEADING IN EXCESS OF 10 DEGREES. NO PLACARDS INSTALLED OR REQUIRED TO NOTIFY PILOT OF THIS CONDITION. 1L71 3O3 O 2A13 E286 20010424002852001042400285CE 2001 4 24 20010420CW007 120010402G7170AV171C47 O-RING CESSNA182 182 2072702CE QUICKDRAIN LEAKING G K NONE O OTHER ININSP/MAINT 1 NM07 200 THE QUICK DRAIN ORING THAT CAME WITH THE NEW QUICK DRAIN, SWELLED UP SO THAT IT IS PUSHED OUT OF THE GROOVE. OIL LEAKS PASSED IT EASILY. 1H71 3O NT3A13 20010424002862001042400286GL 2001 4 24 20010420CW008 120010402G5210 LATCH AMTR LONGEZLONGEZ 05690Z8GL LYC O540 IO540* 41532EA CANOPY FAILED H K NONE O OTHER ININSP/MAINT 1 GL235439N 98110139 CANOPY DEPARTED THE AIRCRAFT WHILE IN FLIGHT. CANOPY LATCH FAILED. 1M71 3O3 ORTEXPA1M711E4 20010423003462001042300346EA 2001 4 23 20010420CW009 220010316G8520LW11021 BEARING SCWZER269 269D 8059501EA LYC O360 HIO360D1A 41514EA NR 2 DAMAGED D K NONE O OTHER ININSP/MAINT 1 WP157430F187 150 1150452 RL2096751A AT 25 HOUR OIL CHANGE, FOUND METAL PARTICLES IN SUCTION SCREEN AND FILTER. ON INSPECTION, FOUND NR 2 MAIN BEARING HAD SPUN NEARLY CAUSING ENGINE FAILURE. CHECK SCREENS. 1G71 3U3 O0 4H12 1E10 20010424002892001042400289CE 2001 4 24 20010420CW011 120010309G2910S217840105 HYDRAULIC LINE CESSNA172 172RG 2072438CE LYC O360 IO360A1A 41514EA NOSE ACTUATOR BROKEN D K NONE O OTHER ININSP/MAINT 1 GL199864B 34151 172RG1060 NOSE GEAR UP HOSE PNS217840105 CAME OUT OF SWEDGE FITTING. 1H71 3O3 O 3A17 1E10 20010424003082001042400308CE 2001 4 24 20010423CW004 120010330G7110J744436 MOUNT CESSNA172 172R 2072401CE ENGINE COWLING TORN D CMXSK NONE O OTHER ININSP/MAINT 1 CE05453CM350 17280845 RUBBER TORN FROM MOUNTING PLATE. 1H71 3O NT3A12 20010424003092001042400309CE 2001 4 24 20010423CW005 120010402G27010411257 UNIVERSAL JOINT CESSNA172 172R 2072401CE CONTROL WHEEL CORRODED D CMXSK NONE O OTHER ININSP/MAINT 1 CE05455CM399 17280847 PIVOTS RUSTY, WOULD NOT SWIVAL, U JOINT COVERED BY RUBBER BOOT. PILOT REPORTED AILERONS HARD TO MOVE. 1H71 3O NT3A12 20010424003102001042400310EA 2001 4 24 20010423CW006 220010330G8520LN18840 CAMSHAFT CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA LOBES WORN D CMXSK NONE O OTHER ININSP/MAINT 1 CE05467CM590 17280859 LZ871551A CAMSHAFT WORN ON NR 5 LOBE. CYLINDERS NR 3 AND NR 4 INTAKE VALVE NOT OPENING FULLY. PILOT REPORTED ENGINE RUNNING ROUGH. 1H71 3O3 ONT3A12 1E10 20010424003172001042400317EA 2001 4 24 20010423CW013 220010326G7414M3548 ROTOR SLICK PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA MAGNETO BROKEN B UC2RK NONE O OTHER ININSP/MAINT 1 GL194148V1653 98040879 2843178 L3625536A PILOT REPORTED EXCESSIVE MAG DROP. FOUND RIGHT MAGNETO ROTOR ASSEMBLY CAM SLOT TO BE BROKEN. 1L71 3O3 O 2A13 E286 20010424003182001042400318SO 2001 4 24 20010423CW014 120010403G2421ALE1003K PLATE ELECTROSYS PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA ALTERNATOR BROKEN B UC2RK NONE O OTHER ININSP/MAINT 1 GL194146T1709 8053286 2843168 L3620536A DURING ROUTINE MAINTENANCE THE ALTERNATOR END PLATE WAS FOUND WITH THE FORWARD ATTACH EAR BROKEN OFF. 1L71 3O3 O 2A13 E286 20010502002802001050200280CE 2001 5 2 20010424CW001 120010131G2750169524074 CONTROL CABLE BEECH 23 B24R 1151253CE TE FLAPS FRAYED B K NONE O OTHER ININSP/MAINT 1 GL179321S MC341 DURING ANNUAL INSPECTION, CABLE WAS INSPECTED AND FOUND TO HAVE SEVERAL BROKEN STRANDS. AFTER FURTHER INSPECTION, FOUND THAT FLAP CABLE 169-524074 WAS CONTACTING A SCREW HEAD WHEN THE FLAPS ARE IN THE UP POSITION. RECOMMEND THAT PROTECTIVE TAPE BE PUT OVER THE SCREW AND TO MONITER FLAP CABLE EVERY 1000 HOURS. 1L71 3O A1CE 20010503001072001050300107WP 2001 5 3 20010424CW008 220010406G720030756392 SEAL GARRTTTFE731TFE7315R 01518WP NR 4 FAILED D K NONE O OTHER ININSP/MAINT 1 GL19 6972 P91222 NR 4 RUNNER FAILED CAUSING DAMAGE TO NEARBY COMPONENTS. 4 F E6WE 20010502002942001050200294CE 2001 5 2 20010425CW007 120010323G27101260141 TUBE CESSNA182 R182 2072734CE LYC O540 O540* 41532EA AILERON CONTROL LOOSE B GSZRK NONE O OTHER ININSP/MAINT 1 SW196161S6001 R18201633 DURING ANNUAL INSPECTION THE TWO ALUMINUM RIVETS SECURING THE FORWARD END OF SHAFT WERE FOUND LOOSE AND THE BUCK TAILS MISSING . THE SQUARK TUBE PORTION OF ASSEMBLY APPEARS TO BE ALUMINUM. THE FORWARD THREADED END IS STEEL. THE FIT OF THE TWO PARTS IS NOT VERY CLOSE. FOUND SHAFT ON FORWARD END OF TUBE WORN WERE IT IS INSTALLED IN BEARING BLOCK. IF THE TWO RIVETS HAD FALLEN OUT, IT COULD HAVE RESULTED IN TOTAL LOSS OF AILERON CONTROL.(PHOTOS) 1H71 3O3 ORT3A13 E295 20010503003962001050300396CE 2001 5 3 20010425CW009 120010402G291024411003 PIVOT CESSNA172 172RG 2072438CE LYC O360 O360* 41514EA MLG CRACKED B WIWRK NONE O OTHER ININSP/MAINT 1 WP076623Z 172RG0240 BOTH PIVOTS WERE FOUND CRACKED. THE RIGHT PIVOT WAS NOT ONLY CRACKED BUT SHOWED SIGNS THAT THE SPLINNED END WAS STARTING TO TWIST OFF. BOTH PIVOTS CRACKS WERE VISABLE WITH THE NAKED EYE, AND NEITHER LEAKED BRAKE FLUID THROUGH THE CRACKS AND INTO THE ACTUATOR. BOTH PIVOTS WERE ALSO THE OLDER ORIGINAL STYLE. 1H71 3O3 O 3A17 E286 20010503001582001050300158SO 2001 5 3 20010426CW010 220010123G8530 CYLINDER HEAD CONT O520 IO520F 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1697 286416R CYLINDERS CRACKED ON THE INTAKE SEAT TO NOZZLE AND OR INJECTOR HOLE. CYLINDER SERIAL NUMBERS: (52L962936), 52L962937, 52L962938, 52L962799. 3 O E5CE 20010503001592001050300159SO 2001 5 3 20010426CW011 220010123G8530 CYLINDER HEAD CONT O520 IO520F 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1697 286416R CYLINDER HEADS CRACKED ON THE INTAKE SEAT TO NOZZLE AND OR INJECTOR HOLE. CYLINDER HEAD SERIAL NUMBERS: 52L962936, (52L962937), 52L962938, 52L962799. 3 O E5CE 20010503001602001050300160SO 2001 5 3 20010426CW012 220010123G8530 CYLINDER HEAD CONT O520 IO520F 17032SO ENGINE CRACKED C CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1697 286416R CYLINDER HEADS CRACKED ON THE INTAKE SEAT TO NOZZLE AND OR INJECTOR HOLE. CYLINDER HEAD SERIAL NUMBERS: 52L962936, 52L962937, (52L962938), 52L962799. 3 O E5CE 20010503001612001050300161SO 2001 5 3 20010426CW013 220010123G8530 CYLINDER HEAD CONT O520 IO520F 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1697 286416R CYLINDER HEADS CRACKED ON THE INTAKE SEAT TO NOZZLE AND OR INJECTOR HOLE. CYLINDER HEAD SERIAL NUMBERS: 52L962936, 52L962937, 52L962938, (52L962799). 3 O E5CE 20010503002292001050300229SO 2001 5 3 20010426CW015 220010213G8530SA52000A20P CYLINDER HEAD CONT O520 IO520* 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1342 CYLINDERS HAVE CRACKS ADJACENT TO EXHAUST SEAT AND INTAKE SEATS BETWEEN FINS 14 AND 20. CYLINDER SERIAL NUMBERS: (52J976779), 52J976780, 52J976781, 52J976782, 52J976787, 52J976788. 3 O E5CE 20010509000032001050900003SO 2001 5 9 20010426CW016 220010213G8530SA52000A20P CYLINDER HEAD CONT O520 IO520* 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1342 CYLINDER CRACKS ADJACENT TO EXHAUST SEAT AND INTAKE SEAT BETWEEN FINS 14 AND 20. CYLINDER SERIAL NUMBERS: 52J976779, (52J976780), 52J976781, 52J976782, 52J976787, 52J976788. 3 O E5CE 20010503003292001050300329SO 2001 5 3 20010426CW017 220010213G8530SA52000A20P CYLINDER HEAD CONT O520 IO520* 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1342 CYLINDER CRACKS ADJACENT TO EXHAUST SEAT AND INTAKE SEATS BETWEEN FINS 14 AND 20. CYLINDER SERIAL NUMBERS: 352J976779, 52J976780, (52J976781), 52J976782, 52J976787, 52J976788. 3 O E5CE 20010503003302001050300330SO 2001 5 3 20010426CW018 220010213G8530SA52000A20P CYLINDER HEAD CONT O520 IO520* 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1342 CYLINDER CRACKS ADJACENT TO EXHAUST SEAT AND INTAKE SEATS BETWEEN FINS 14 AND 20. CYLINDER SERIAL NUMBERS: 52J976779, 52J976780, 52J976781, (52J976782), 52J976787, 52J976788. 3 O E5CE 20010503003312001050300331SO 2001 5 3 20010426CW019 220010213G8530SA52000A20P CYLINDER HEAD CONT O520 IO520* 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1342 CYLINDER CRACKS ADJACENT TO EXHAUST SEAT AND INTAKE SEATS BETWEEN FINS 14 AND 20. CYLINDER SERIAL NUMBERS: 52J976779, 52J976780, 52J976781, 52J976782, (52J976787), 52J976788. 3 O E5CE 20010509000042001050900004SO 2001 5 9 20010426CW020 220010213G8530SA52000A20P CYLINDER HEAD CONT O520 IO520* 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1342 CYLINDER CRACKS ADJACENT TO EXHAUST SEAT AND INTAKE SEATS BETWEEN FINS 14 AND 20. CYLINDER SERIAL NUMBERS: 52J976779, 52J976780, 52J976781, 52J976782, 52J976787, (52J976788). 3 O E5CE 20010503003322001050300332SO 2001 5 3 20010426CW021 220010205G8530SA52000A20P CYLINDER HEAD CONT O520 IO520* 17032SO ENGINE CRACKED B CY2RK NONE O OTHER ININSP/MAINT 1 AL03901931801 1801 CYLINDER HEADS CRACKED ON INTAKE SIDE ON EXTERIOR ADJACENT TO INTAKE SEAT. UNLIKE MANY OTHER CRACKED MILLINEUM CYLINDERS THESE WERE ALSO CRACKED ON THE EXHAUST SIDE , VISIBLE FROM OUTSIDE BETWEEN FINS 18 TO 20. SERIAL NUMBERS: (52L976947), 52L976948, 52L976949, 52L976950, 52L976957, 52L976958. 3 O E5CE 20010503003332001050300333SO 2001 5 3 20010426CW022 220010205G8530SA52000A20P CYLINDER HEAD CONT O520 IO520* 17032SO ENGINE CRACKED B CY2RK NONE O OTHER ININSP/MAINT 1 AL03901931801 1801 CYLINDER HEADS CRACKED ON INTAKE SIDE ON EXTERIOR ADJACENT TO INTAKE SEAT. UNLIKE MANY OTHER CRACKED MILLINEUM CYLINDERS THSES WERE ALSO CRACKED ON THE EXHAUST SIDE VISIBLE FROM OUTSIDE BETWEEN FINS 18 TO 20. SERIAL NUMBERS: 52L976947, (52L976948), 52L976949, 52L976950, 52L976957, 52L976958. 3 O E5CE 20010503003392001050300339SO 2001 5 3 20010426CW023 220010205G8530SA52000A20P CYLINDER HEAD CONT O520 IO520F 17032SO ENGINE CRACKED B CY2RK NONE O OTHER ININSP/MAINT 1 AL03901931801 1801 240934R CYLINDER HEADS CRACKED ON INTAKE SIDE ON EXTERIOR OR ADJACENT INTAKE SEAT. UNLIKE MANY OTHER CRACKED MILLINEUM CYLINDERS THESE WERE ALSO CRACKED ON THE EXHAUST SIDE VISIBLE FROM OUTSIDE BETWEEN FINS 18 TO 20. SERIAL NUMBERS: 52L976947, 52L976948, (52L976949), 52L976950, 52L976957, 52L976958. 3 O E5CE 20010503003402001050300340SO 2001 5 3 20010426CW024 220010205G8530SA52000A20P CYLINDER HEAD CONT O520 IO520F 17032SO ENGINE CRACKED B CY2RK NONE O OTHER ININSP/MAINT 1 AL03901931801 1801 240934R CYLINDER HEADS CRACKED ON INTAKE SIDE ON EXTERIOR ADJACENT TO INTAKE SEAT. UNLIKE MANY OTHER CRACKED MILLINEUM CYLINDER, THESE WERE ALSO CRACKED ON THE EXHAUST SIDE VISIBLE FROM OUTSIDE BETWEEN FINS 18 TO 20. CYLINDER SERIAL NUMBERS: 52L976947, 52L976948, 52L976949, (52L976950), 52L976957, 52L976958. 3 O E5CE 20010503003352001050300335SO 2001 5 3 20010426CW025 220010205G8530SA52000A20P CYLINDER HEAD CONT O520 IO520F 17032SO ENGINE CRACKED B CY2RK NONE O OTHER ININSP/MAINT 1 AL03901931801 1801 240934R CYLINDER HEADS CRACKED ON INTAKE SIDE ON EXTERIOR ADJACENT INTAKE SEAT. UNLIKE MANY OTHER CRACKED MILLINEUM CYLINDERS THESE WERE ALSO CRACKED ON THE EXHAUST SIDE VISIBLE FROM OUTSIDE BETWEEN FINS 18 TO 20. 3 O E5CE 20010503003362001050300336SO 2001 5 3 20010426CW026 220010205G8530SA52000A20P CYLINDER HEAD CONT O520 IO520F 17032SO ENGINE CRACKED B CY2RK NONE O OTHER ININSP/MAINT 1 AL03901931801 1801 240934R CYLINDER HEADS CRACKED ON INTAKE SIDE ON EXTERIOR ADJACENT TO INTAKE SEAT. UNLIKE MANY OTHER CRACKED MILLINEUM CYLINDERS THESE WERE ALSO CRACKED ON THE EXHAUST SIDE, VISIBLE FROM OUTSIDE BETWEEN FINS 18 TO 20. SERIAL NUMBERS: 52L976947, 52L976948, 52L976949, 52L976950, 52L976957, (52L976958). 3 O E5CE 20010503001412001050300141CE 2001 5 3 20010430CW001 120010327G27100400107159 CONTROL CABLE CESSNA150 152 2071835CE LYC O235 O235* 41505EA AILERONS BROKEN D K NONE O OTHER ININSP/MAINT 1 SO159308810573 15285398 DURING 100 HOUR INSPECTION, IT WAS DISCOVERED THAT THE LEFT AILERON CROSSOVER CABLE HAD A BROKEN STRAND AT A POINT 63.5 INCHES FROM THE TURNBUCKLE END. BROKEN STRAND WAS WHERE CABLE PARTED OVER A RUB BLOCK ATTACHED TO RIB AT WING STA. 56.875. 1H71 3O3 ONT3A19 E223 20010503001432001050300143CE 2001 5 3 20010430CW002 120010307G3230 LANDING GEAR BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MAINS MALFUNCTIONED D BSYAO OTHER J WARNING INDICATION DEDESCENT 1 GL0721ES TH1123 AIRCRAFT COMING INTO AIRPORT, COULD NOT GET (3) GEAR DOWN AND LOCK LIGHTS. FOUND GEAR INDICATOR LIGHT SWITCH IN DIM POSITION. PILOT COULD NOT SEE LIGHTS IN DAY FLIGHT. REPOSITIONED, CYCLED GEAR OPS CHECKS GOOD. 1L72 3O3 O 3A16 E5CE 20010503001442001050300144CE 2001 5 3 20010430CW003 120010307G323008421043 BELLCRANK CESSNA310 310R 2074245CE NOSE GEAR BROKEN D BSYAO OTHER O OTHER NRNOT REPORTED 1 GL076160X 310R1305 PILOT HEARD POPPING NOISE OUT OF GEAR, WHEN GEAR WAS RETRACTED. SELECTED GEAR DOWN AND DID A FLYBY. TOWER SAID NOSE GEAR HALF WAY DOWN, FLEW TO AIRPORT AND LANDED, NOSE GEAR COLLAPSED. LIFTED AIRCRAFT ON TO RUNWAY. NOSE GEAR SWUNG DOWN AND LOCKED, ZERO RESISTANCE, FOUND BELLCRANK BROKEN WHERE FORK BOLT GOES THROUGH. 1L72 3O 3A10 20010503001482001050300148SO 2001 5 3 20010430CW004 220010430G8550 ENGINE CESSNA210 T210M 2073451CE CONT O520 TSIO520* 17040SO NACELLE LACK OF LUBE D K NONE O OTHER ININSP/MAINT 1 GL15732UH 21061781 OWNER DISCOVERED A GREAT LOSS OF ENGINE OIL, FOLLOWING A COLD WEATHER FLIGHT. TEMPERATURE WAS 40 DEGREES C/F. AIR/OIL SEPARATOR INSTALLED PRIOR TO RECENT CYLINDER REPLACEMENT. 1H71 3O3 O 3A21 E8CE 20010503000012001050300001CE 2001 5 3 20010430CW005 120010329G80116462751 STARTER CESSNA310 310R 2074245CE CONT O520 IO520* 17032SO ENGINE FAILED D K NONE O OTHER ININSP/MAINT 1 GL1790FC 396 310R1838 THIS STARTER WAS SUPPLIED WITH A ZERO TIME OVERHAULED ENGINE. THE ENGINE WAS INSTALLED JULY 20, 2000. STARTER FAILED MARCH 23, 2001 AFTER ACCUMULATING ONLY 396.7 HOURS. DID NOT DISASSEMBLE STARTER DUE TO WARRANTY. 1L72 3O3 O 3A10 E5CE 20010503003282001050300328CE 2001 5 3 20010430CW008 120010402G2910244110010 PIVOT CESSNA172 172RG 2072438CE LYC O360 O360A1D 41514EA RT MLG BROKEN D WIWRK NONE O OTHER ININSP/MAINT 1 WP079516B2800 172RG0847 WHILE ON CHECK RIDE, THE RIGHT MAIN LANDING GEAR FAILED TO EXTEND. THE PILOT SUCCESSFULLY MANAGED TO LOCK THE GEAR IN PLACE BY LAYING ON THE FLOOR BEHIND THE PILOTS SEATS, USING HIS HEAD TO HOLD DOOR OPEN, REACHING OUT AND PULLED GEAR INTO POSITION. LANDED SAFELY. FOUND THE SPLINED PART OF THE PIVOT HAD COMPLETELY TWISTED OFF FROM THE REST OF THE PIVOT. NO HISTORY OF ANY BRAKE PROBLEMS, NOR REPORTS OF HARD LANDINGS WERE MADE. NO LEAKS WERE DETECTED WHILE PERFORMING THE ANNUAL INSPECTION. 1H71 3O3 O 3A17 E286 20010503002652001050300265CE 2001 5 3 20010430CW012 120010402G7603 HOUSING CESSNA172 172M 2072418CE LYC O320 O320D2G 41508EA THROTTLE CABLE CRACKED D K NONE O OTHER ININSP/MAINT 1 NM01703233857 17267200 L937739A THROTTLE CABLE OUTER HOUSING DETERIORATED AND SEPARATED FROM SWEDGED FITTING AT CLAMP LOCATION AFT OF ENGINE. THIS ALLOWED THE OUTER HOUSING TO MOVE INSTEAD OF THE CARBURETOR CONTROL ARM AS THE THROTTLE CONTROL WAS MOVED. RECOMMEND CABLE REPLACEMENT WHEN ANY INDICATION OF CRACKING IN THE OUTER HOUSING BECOMES VISIBLE. 1H71 3O3 ONT3A12 E274 20010501003632001050100363CE 2001 5 1 20010501AP004 120010424G783023220258511 LEVER ARONCA RKWELLNA265 NA26580 7630108CE THRUST REVERSER MISMANUFACTURED B JV2RK NONE O OTHER ININSP/MAINT 1 SW99316EC369 369 144 38038 ON 8/9/99 1EA. P/N232-20258-511 WAS INSTALLED ON L/H T/R. 2EA. P/N 232-20258-513 AND 2EA. 232-20258-514 LEVERS WERE INSTALLED ON R/H T/R DURING REPAIR OF THESE T/RS. IN JAN. 2001 THE CUSTOMER REPORTED PROBLEMS WITH THE LT T/R. INSPECTION OF BOTH T/RS REVEALED BROKEN DRIVE CABLES AND BENT LEVERS. IT WAS BELIEVED AT THIS TIME THAT THE LEVERS WERE NOT PER DRAWING AND REMAINING STOCK WAS RETURNED TO LEAR. LEAR RETURNED THE LEVERS AS BEING MANUFACTURED PER DRAWING. FURTHER INSPECTION AND DISCUSSION WITH LEAR ON 4/23/01 REVEALED THE PREVIOUSLY MENTIONED LEVERS INSTALLED NEW 8-20-99 WERE NOT MANUFACTURED IAW LEAR DRAWINGS. 2L72 4F A2WE 20010503000462001050300046CE 2001 5 3 20010501CW001 120010207G2140 FUEL CAP CESSNA421 421C 2076016CE CONT O520 GTSIO520F 17032SO HEATER CRACKED D K NONE O OTHER ININSP/MAINT 1 WP0912RJ 5280 421C0306 FUEL LEAK AT HEATER FUEL FILTER ASSEMBLY IN RIGHT WING. CAP ON TOP OF ASSEMBLY WAS FOUND TO HAVE CRACK IN THREADS. CAP IS MADE OF ALUMINUM. PART IS PRESUMED TO BE ORIGINAL EQUIPMENT. NO KNOW DISASSEMBLY IN SERVICE HISTORY. CAP WAS LOOSE IN SPITE OF LOCK TAB STILL BEING INTACT. 1L72 3O3 O A7CE E7CE 20010503001122001050300112NE 2001 5 3 20010501CW006 220010313G8530212359 CYLINDER SCWZERG164 G164A 3952704EA PWA R1340 R1340AN1 52016NE NR 2 ENGINE CRACKED G ZMIGK NONE O OTHER ININSP/MAINT 1 SO075076 1111 11091 NO RECORDS ON CYLINDERS. AIRCRAFT LOST POWER AFTER TAKE OFF AND LANDED LONG, RAN INTO WOODS (DESTROYED AIRCRAFT) PILOT UNHURT. INVESTIGATION REVEALED NR 2 ENGINE CYLINDER VAS CRACKED FROM THE INTAKE VALVE HOLE TO SPARK PLUG HOLE, ALMOST COMPLETELY AROUND THE CYLINDER. 1Q71 3R3 R 1A16 5E2 20010503001162001050300116SO 2001 5 3 20010501CW007 120010406G5210 LATCH PIPER PA23 PA23160 7102304SO LYC O320 O320* 41508EA PAX DOOR INOPERATIVE G K NONE O OTHER ININSP/MAINT 1 WP21333PE 232007 DOOR CAME OPEN IN FLIGHT CAUSING AIRCRAFT TO LOOSE DIRECTIONAL CONTROL. GROUND INVESTIGATION REVEALED THAT LATCH MECHANISM WAS NOT LOCKING PROPERLY AT THE JAMS. 1L72 3O3 O 1A10 E274 20010503002012001050300201CE 2001 5 3 20010501CW014 120010413G3000 SWITCH ASC BEECH 35 B35 1151506CE LT BRAKE INOPERATIVE B LX5RO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL19171CP 0854A FL244 LEFT BRAKE DEICE VALVE, SHOWING ITT RISE, LIGHT NOT ILLUMINATING. LIGHT SYSTEM CHECKS GOOD. BAD SWITCH ON VALVE. 1L71 3O A777 20010503002022001050300202CE 2001 5 3 20010501CW015 120010412G3000 SWITCH ASC BEECH B300 B300 1159232CE LT BRAKE INOPERATIVE B LX5RO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL19971LL 0831A FL267 LEFT BRAKE DEICE VALVE INDICATING LIGHT CIRCUIT OPEN IN VALVE. 2L72 4T RTA24CE 20010503002032001050300203CE 2001 5 3 20010501CW016 120010406G7160075014433 AIR BOX CESSNA182 182P 2075816CE CONT O470 O470S 17026SO ENGINE FAILED D K NONE O OTHER ININSP/MAINT 1 NE051408M113 18264319 226296R DURING ANNUAL INSPECTION, IT WAS NOTED THAT THE RIVETS THAT SECURE THE CARB HEAT VALVE PLATE TO THE CONTROL CROSS SHAFT WER COMING LOOSE. THIS APPEARS TO HAVE BEEN CAUSE BY SEALING MATERIAL ON THE VALVE PLATE WHICH WAS NOT CORRECTLY TRIMMED. AS A RESULT, THE MATERIAL WOULD BIND IN A CARB HEAT NEEDED POSITION, MAKING IT DIFFICULT TO RETURN THE VALVE TO A NO CARB HEAT POSITION. 1H71 3O3 ONTTA13 E273 20010503002042001050300204CE 2001 5 3 20010501CW017 120010501G272012604567 RUDDER BAR CESSNA206 U206G 2073356CE CONT O520 IO520* 17032SO RUDDER PEDALS DAMAGED B CL4RO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 AL039497R3102 U20606876 PILOT SIDE LEFT RUDDER PEDAL COLLAPSED IN FLIGHT. SAFECOM FILED. APPEARS THAT TORQUE TUBE MAY HAVE BEEN DAMAGED BY MAINTENANCE WHEN BUSHING WAS INSTALLED. 1H71 3O3 O A4CE E5CE 20010503002062001050300206SO 2001 5 3 20010501CW019 220010303G8530SA52000A1 CYLINDER CONT O520 IO520F 17032SO NR 3 DESTROYED B O3ORK NONE O OTHER ININSP/MAINT 1 AL03 96 96 563729 NR 3 CYLINDER AND PISTON ASSEMBLY. REMOVED DUE TO LOW COMPRESSION AND COMPLAINT FROM PILOT OF RUNNING ROUGH. PISTON APPEARS TO HAVE SEVERE PREIGNITION OR DETONATION. 3 O E5CE 20010503002072001050300207CE 2001 5 3 20010501CW020 120010412G2421635796 COUPLING ELECTROSYS CESSNA172 R172E 2072413CE CONT IO360 IO360* 17025CE ALTERNATOR DRIVESLIPPED D K NONE O OTHER ININSP/MAINT 1 SO157907N B022733 R1720298 239770R AT ENGINE CHANGE, FRESH OVERHAUL ALT INSTALLED AFTER 9.0 HOURS OF OPERATION NOTED ERATIC ALTERNATOR OUTPUT. INSPECTED ALTERNATOR AND DETERMINED ALTERNATOR DRIVE COUPLING SLIPPING. REPLACED ALTERNATOR DRIVE COUPLING WITH OVERHAULED LIKE ITEM AND REINSTALLED ALTERNATOR ON AIRCRAFT. 1H71 3O3 O 3A17 E1CE 20010503002092001050300209CE 2001 5 3 20010501CW022 120010412G3710632617D BEVEL GEAR CONT CESSNA337 337G 2075730CE CONT O360 IO360GB 17025SO VACUUM PUMP SHEARED D K NONE O OTHER ININSP/MAINT 1 SO15726AS725 7509 33701661 813014R A DETAILED INVESTIGATION OF THE STARTER DEIVE REVEALED THAT ALL TO THE GEAR TEETH WERE WORN EXCESSIVELY ON ONE OF THE BEVEL GEARS WHICH DRIVES THE VACUUM PUMP. THIS IS THE FIFTH FAILURE OF THIS GEAR THAT WE HAVE DETECTED. 1H72 3O3 O A6CE E1CE 20010503002102001050300210SW 2001 5 3 20010501CW023 120010128G3213530021000 DISK MOONEYM20 M20D 5870210SW LYC O360 O360* 41514EA MLG STRUT WORN D K NONE O OTHER ININSP/MAINT 1 NE031923Y 218 MAIN LANDING GEAR SHOCK DISCS WERE FOUND TO BE COMPRESSED BEYOND LIMITS. WHEN CHECKED PER THE MANUAL INSTEAD OF .1250 MAX CLEARANCE THER WAS .3750 INCH OF CLEARANCE. ALSO FOUND AN INCORRECT FITTING INSTALLED ON LEFT BRAKE THAT ALLOWED THE BRAKE HOSE TO INTERFEAR WITH THE INNER GEAR DOOR. 1L71 3O3 O 2A3 E286 20010503002362001050300236SO 2001 5 3 20010502CW001 120010305G52804752932 HINGE PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA MLG INNER DOOR CRACKED D K NONE O OTHER ININSP/MAINT 1 AL05555FS5393 317952046 INSPECTED HINGES, ONLY FORWARD HINGES ON BOTH DOORS HAD CRACKS ON INNER RADIUS APPROX .1250 TO .1875 INCH DEEP. REAR HINGES WERE NOT CRACKED, REPLACED ALL FOUR HINGES. SUSPECT CRACKS ARE CAUSED DUE TO LOCATION OF HYD ACTUATOR FORWARD OF FORWARD HINGE, CAUSING MORE STRESS ON FORWARD HINGE THAN ON REAR HINGE. 1L72 3O3 O A20SO E14EA 20010503002472001050300247SW 2001 5 3 20010502CW005 120010402G6210204011250113 BLADE BELL 204 UH1H 1181407SW LYC T53 T53* 41549NE MAIN ROTOR CRACKED D K NONE O OTHER ININSP/MAINT 1 NM01340WN2500 1648 6510081 LE17065BA A CRACK WAS NOTICED INSIDE DENT AFT OF THE SPAR ON THE TOP OF THE MAIN ROTOR BLADE. REMOVAL OF PAINT DETERMINED THE CRACK TO BE IN EXCESS OF 6 INCHES LONG. THE ROTOR BLADE WAS DETERMINED TO BE UNSERVICEABLE AND REMOVED FROM SERVICE. 1G71 4U4 U EXPA1G71E1EA 20010503000232001050300023EU 2001 5 3 20010502CW009 120010106G6220117775P BALL JOINT SNIAS 350 AS350B3 8680954EU STARFLEX WORN B R7MAK NONE O OTHER ININSP/MAINT 1 NM0752285505 3251 WORN BEYOND SERVICEABLE LIMITS. REMOVED AND REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 20010503003892001050300389NE 2001 5 3 20010502CW010 120010320G7810 EXHAUST PIPE SKRSKYS76 S76A 8143006NE RIGHT MISALIGNED B HEEAK NONE O OTHER ININSP/MAINT 1 WP095444X 760174 THE EXHAUST ASSEMBLY WAS SENT TO A REPAIR STATION FOR OVERHAUL. UPON REINSTALLATION IT WAS FOUND THAT THE RIGHT HAND EXHAUST PIPE CONTACTED THE NR 5 CYLINDER INTAKE PIPE. 1G72 3U H1NE 20010503002112001050300211CE 2001 5 3 20010503CW004 120010404G531005110006 DOOR FRAME CESSNA172 172E 2072412CE CONT O300 O300D 17022SO FUSELAGE MISINSTALLED H K NONE W INADEQUATE Q C ININSP/MAINT 1 NM083658S3222 17250858 24144DOD FUEL LINES RUBBING AND STRESSED DUE TO UPPER OUTBOARD DOOR FRAME PARTIALLY COVERING HOLE AND NOT ALLOWING CLEARANCE FOR FUEL LINE. CAUSE BY HOLE IN UPPER OB DOOR FRAMES NOT BEING CUT OUT TO ORIGINAL SIZE FOR CLEARANCE BY MFG. RECOMMENDATION IS TO ROUND OUT HOLE TO ORIGINAL OPENING TO ACCOMMODATE FUEL LINE. 1H71 3O3 ONT3A12 E253 20010503002132001050300213CE 2001 5 3 20010503CW005 120010404G531005110007 DOOR FRAME CESSNA172 172E 2072412CE CONT O300 O300D 17022SO FUSELAGE MISINSTALLED H K NONE W INADEQUATE Q C ININSP/MAINT 1 NM083658S3222 17250858 24144DOD FUEL LINES RUBBING AND STRESSED DUE TO UPPER OUTBOARD DOOR FRAME PARTIALLY COVERING HOLE AND NOT ALLOWING CLEARANCE FOR FUEL LINE. CAUSED BY THE HOLE IN DOOR FRAMES NOT BEING CUT OUT TO ORIGINAL SIZE FOR CLEARANCE BY MFG. RECOMMENDATION IS TO ROUND OUT HOLES TO ORIGINAL OPENING TO ACCOMMODATE FUEL LINE. 1H71 3O3 ONT3A12 E253 20010515000612001051500061EA 2001 5 15 20010503CW013 220010503G74144381 MAGNETO CESSNA172 172M 2072418CE LYC O320 O320* 41508EA LEFT INOPERATIVE D K NONE O OTHER ININSP/MAINT 1 GL0920421 17261276 PLASTIC SUPPORT FOR POINTS BROKEN, AND POINTS FAILED, FACTORY SEAL STILL ON MAGNETO. PILOT REPORTED ENGINE RUNNING ROUGH. MADE SAFE LANDING, CHECKED GOOD WITH REPLACEMENT MAGNETO. 1H71 3O3 ONT3A12 E274 20010515000802001051500080NE 2001 5 15 20010504CW002 220010227G7200P2A0851 SEAL IAE V2500 V2500A1 NE NR 4 BEARING CRACKED B KB1RK NONE O OTHER ININSP/MAINT 1 NE03 PART REJECTED AT PENETRANT INSPECTION FOR INDICATIONS AS MARKED ON BOTTOM OF PART (SIDE OF BOSS). 4 F E311NE 20010515000822001051500082NE 2001 5 15 20010504CW003 220010329G72002A0851 SEAL IAE V2500 V2500A1 NE NR 4 BEARING CRACKED B KB1RK NONE O OTHER ININSP/MAINT 1 NE03 PART REJECTED AT PENETRANT INSPECTION FOR INDICATIONS AS MARKED ON AREA ADJACENT TO BOSS. 4 F E311NE 20010515000882001051500088NE 2001 5 15 20010504CW006 220010216G7230787008 COMPRESSOR WHEEL PWA JT8 JT8D9A 52048NE 8TH STAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 SW99 26811 666322 AFTER ENGINE DISASSEMBLE, DURING INSPECTION ON EIGHTH STAGE DISK, A CRACK WAS DETECTED IN ONE OF THE TIE ROD HOLES. CRACK EXTENDED RADIALLY OUTBOARD FROM THE HOLE TO DEPTH OF 0.35 IN., DUE TO OXIDATION AND HEAVY CORROSION. IN ORDER TO HAVE MORE INFORMATION, PART WAS SENT TO OEM FOR EVALUATION. PART WILL BE LOCALLY SCRAPPED. 4 F E2EA 20010515000912001051500091EA 2001 5 15 20010504CW008 220010330G7200LW14820 SNAP RING PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA COUNTERWEIGHT DEFECTIVE D K NONE O OTHER ININSP/MAINT 1 NM0778GH 317852121 L247368A THIS ENGINE WAS RECEIVED ON 2/21/01 DUE TO A HOLE IN TOP OF ENGINE. DURING DISASSEMBLY IT WAS NOTED THAT THE CRANKSHAFT WAS BROKEN AT THE NR 1 ROD JOURNAL. THE SNAP RING AND PIN WERE MISSING FROM ONE OF THE COUNTERWEIGHTS. THE PIN UPON COMING OUT WAS PINCHED BETWEEN THE NR 2 CONNECTING ROD AND CONNECTING ROD HAD THE CAP PULLED OFF FROM DEBREE FLYING AROUND IN THE ENGINE. THE SNAP RING DID NOT HAVE ENOUGH TENTION TO KEEP IT EXPANDED IN PLACE ALLOWING IT TO COME OUT AND CAUSE CATASTROPHIC ENGINE FAILURE. 1L72 3O3 O A20SO E14EA 20010515000922001051500092SW 2001 5 15 20010504CW009 120010320G3260880013507 SWITCH MOONEYM20 M20J 5870219SW LYC O360 IO360A3D6D 41514EA AIRSPEED SEPARATED D K NONE O OTHER ININSP/MAINT 1 NM01923DH819 819 243368 L2671551A A/S SWITCH FAILED F/T 32-30-01, SWITCH WAS REMOVED AND SENT TO OEM VENDOR. SWITCH WAS PARTED FROM MOUNT. SWITCH WAS EXPOXED TO MOUNT AND RECALIBRATED. THE SWITCH WAS REINSTALLED AND PASSED. 1L71 3O3 O 2A3 1E10 20010515001182001051500118SO 2001 5 15 20010507CW001 220010405G8550C1650010102 SEPARATOR CESSNA182 182H 2072718CE CONT O470 O470* 17026SO AIR/OIL CONTAMINATED B ZM3RK NONE O OTHER ININSP/MAINT 1 WP073495S5686 18255895 OIL FILTER INSPECTION REVEALED EXCESSIVE AMOUNT OF CONTAMINATION. INVESTIGATION REVEALED AIR/OIL SEPERATOR INTERNAL SCREEN COMING APART. YEARS OF VIBRATION MAY HAVE CAUSED SCREEN SEPARATION. FACTORY RECOMMENDS 100 HOURS CLEANING. THERE IS NO WAY TO INSPECT UNIT WITHOUT CUTTING IT OPEN. 1H71 3O3 ONT3A13 E273 20010515001192001051500119CE 2001 5 15 20010507CW003 120010418G242199105921 ALTERNATOR CESSNA210 P210N 2073454CE CONT O520 TSIO520* 17040SO ENGINE MALFUNCTIONED C K NONE O OTHER ININSP/MAINT 1 NM10456BR15 P21000717 AIRCRAFT UNDER IMC WHEN LOW VOLT LIGHT CAME ON AND VOLTAGE DROP TO 23.0 VOLTS. PILOT SHUT EVERYTHING OFF AND DECLARED AN EMERGENCY WITH CASCADE APPROACH. LANDED WITHOUT INCIDENT. PART WAS UNDER WARRANTY SO COULD NOT DISASSEMBLE TO FIND OUT CAUSE OF FAILURE, PART IS PROPRIETARY FOR MFG. 1H71 3O3 O 3A21 E8CE 20010515001202001051500120SO 2001 5 15 20010507CW004 220010413G73226397172 FUEL CONTROL CESSNA185 A185F 2072821CE CONT O550 IO550D 17042SO CONTROL ARM DEFECTIVE B T9ZRK NONE O OTHER ININSP/MAINT 1 NM09 280 AIRCRAFT WAS INSPECTED FOR FUEL SYSTEM PROBLEMS. IT WAS DISCOVERED THAT THE CONTROL ARM ON THE THROTTLE BODY WAS SHIPPING ON THROUGH SHAFT. THIS CONDITION DID CAUSE THE AIRCRAFT TO ENCOUNTER A STOCK THROTTLE CONDITION, IN THE FULL THROTTLE POSITION. 1H71 3O3 O 3A24 E3SO 20010515001282001051500128CE 2001 5 15 20010507CW010 120010423G5521 SPAR CESSNA188 A188B 2073005CE CONT O520 IO520* 17032SO RT ELEVATOR CRACKED B K NONE O OTHER ININSP/MAINT 1 NM09731CS 18802796T FOUND RIGHT ELEVATOR SPAR CRACKED AT OUTBOARD ATTACH POINT. HORIZONTAL STABILIZER HAD PREVIOUS REPAIRS WERE LOCATED DIRECTLY FORWARD OF CRACK IN ELEVATOR SPAR. 1L71 3O3 O A9CE E5CE 20010515001442001051500144CE 2001 5 15 20010507CW020 120010329G575305239016 SKIN CESSNA172 172S 2072439CE LYC O360 IO360A1A 41514EA LEFT TE FLAP CRACKED D K NONE O OTHER ININSP/MAINT 1 NM07476SP1168 M2S8022 DURING A PHASE 2 INSPECTION PERFORMED, SEVERAL CRACKS WERE NOTICED ON THE TRAILING EDGE RIVETS ON THE LOWER LEFT FLAP SKIN, AT APPROX 2-3 FEET FROM THE INBOARD EDGE. 6 RIVETS HAD CRACKS STARTING TO FORM FROM THEM. THE CRACKS ARE ABOUT .1250 TO .2500 OF AN INCH LONG. 1H71 3O3 ONT3A12 1E10 20010516004082001051600408CE 2001 5 16 20010508CW002 120010508G275026111447 BRACKET CESSNA208 208B 2073701CE FLAP BROKEN D K NONE O OTHER ININSP/MAINT 1 SW0164BP 3789 0604 PRIMARY FLAP MOTOR DRIVE COUPLER FAILED. STAND BY SYSTEM USED TO EXTEND FLAPS. FLAP LIMIT SWITCHES NOT INCORPORATED IN STAND BY SYSTEM. OPERATIONAL SWITCH OF STAD BY SYSTEM HELD TOO LONG AND FLAP MOTOR CONTINUED TO RUN PAST LIMIT SWITCH LOCATION AND TWISTED FLAP DRIVE ASSEMBLY OUT OF MOUNTING BRACKET. RECOMMENDATION, PILOT BE MORE AWARE OF SYSTEM OPERATION OR INCORPORATE SWITCHES INTO STAND-BY SYSTEM. 1H71 3T A37CE 20010516004092001051600409EU 2001 5 16 20010508CW003 120010412G2121M3348A MOTOR DYNAIR SAAB SF340 SF340A 7850100EU FAN INOPERATIVE B O OTHER O OTHER NRNOT REPORTED 1 WP05 162 ARMATURE ASSEMBLY SHOWS SIGNS OF AN INTERFERENCE FIT. RECOMMEND OVERHAUL ONLY TO APPROVED OVERHAUL MANUAL USING ONLY APPROVED PARTS. 2L72 4T RTA52EU 20010516005472001051600547EU 2001 5 16 20010508CW004 120010412G2121M3348A MOTOR DYNAIR SAAB SF340 SF340A 7850100EU FAN WRONG PART B K NONE O OTHER ININSP/MAINT 1 WP05 170 FAN RETURNED TO MFG FOR UPGRADE TO C209-6901 CONFIGURATION, THE FAN WAS TESTED AND FOUND TO EXHIBIT EXCESSIVE VIBRATION. WHEN THE FAN WAS DISASSEMBLED, IT WAS DISCOVERED THAT THIS OVERHAULED UNIT HAS NOT BEEN OVERHAULED PER MFG OVERHAUL MANUAL. THE ARMATURE AND STATOR FIELD WINDINGS ARE NOT OF MFG DESIGN. MFG OVERHAUL MANUAL DOES NOT ALLOW FOR REWINDING OF THE ARMATURE OR FIELD WINDINGS. THE ARMATURE ASSY HAS NUMBERS STAMPED INTO IT, WHICH CAUSES AN OUT OF ROUND CONDITION. ARMATURE HAS A COMMUTATOR THAT IS NOT MFG PART INSTALLED ON IT. THE IMPELLER IS AT THE WRONG LOCATION, CAUSING IT TO RUB AGAINST THE FRONT END BELL. THE FIELD WINDINGS HAVE A THERMAL SWITCH ADDED THAT IS NOT PER OVERHAUL MANUAL. 2L72 4T RTA52EU 20010516005482001051600548EU 2001 5 16 20010508CW005 120010412G2121 MOTOR DYNAIR SAAB SF340 SF340A 7850100EU FAN UNAPPROVED PART B K NONE O OTHER ININSP/MAINT 1 WP05 174 MOTOR ASSEMBLY IS NOT A DYNAMIC AIR ENGINEERING PART. MOTOR ASSEMBLY DOES NOT MEET DAE DRAWING AND OVERHAUL MANUAL REQUIREMENTS. 2L72 4T RTA52EU 20010516005522001051600552EU 2001 5 16 20010508CW006 120010412G2121M3348A MOTOR DYNAIR SAAB SF340 SF340A 7850100EU FAN UNAPPROVED PART B K NONE O OTHER ININSP/MAINT 1 WP05 225 FAN RETURNED TO DAE FOR UPGRADE TO C209-690D CONFIGURATION. THE FAN WAS TESTED AND FOUND TO EXHIBIT EXCESSIVE VIBRATION. WHEN THE FAN WAS DISASSEMBLED, IT WAS DISCOVERED THAT THIS OVERHAULED UNIT HAS NOT BEEN OVERHAULED PER THE DAE OVERHAUL MANUAL. THE ARMATURE AND STATOR FIELD WINDING ARE NOT OF DAE DESIGN. DAE OVERHAUL MANUAL DOES NOT ALLOW FOR THE REWINDING OF THE ARMATURE OR FIELD WINDINGS. THE ARMATURE ASSY HAS AN OVERSIZE COMMUTATOR INSTALLED WHICH MAKES THE BRUSHES EXTEND PAST THE DESIGNED LIMIT, THE IMPELLER IS AT THE WRONG LOCATION, AND ARMATURE IS NOT BALANCED. THE FIELD WINDINGS ARE REWOUND AND HAVE UNACCEPTABLE AIR GAP. 2L72 4T RTA52EU 20010516005532001051600553SO 2001 5 16 20010508CW008 220010402G7414M1176 FRAME SLICK CESSNA206 TU206G 2073357CE CONT O520 TSIO520M 17040SO MOUNTING FLANGE CRACKED B QY5RK NONE K FLUID LOSS ININSP/MAINT 1 NE01232MT 1010441 U20606200 520356 OBSERVED AN OIL LEAK FROM MAG BASE. FOUND MOUNTING FLANGE CRACKED AROUND LOWER CLAMPING WASHER. REMOVED MAG AND FOUND APPROX 2 INCH PIECE OF MOUNTING FLANGE BROKEN OFF. 1H71 3O3 O A4CE E8CE 20010516004212001051600421SO 2001 5 16 20010508CW009 220010402G7414M3975 COIL SLICK CESSNA206 TU206G 2073357CE CONT O520 TSIO520* 17040SO MAGNETO INOPERATIVE B QY5RK NONE O OTHER ININSP/MAINT 1 NE01232MT 89070161 U20606200 MAGNETO INOPERATIVE BELOW 1,000 RPMS. OK AT 1,700 RPMS PER THE P.O.M. PILOTS HAD DONE A MAG CHECK AT IDLE WHICH LEAD TO THE DISCOVERY. OPENED MAGNETO FOR INSPECTION. TESTED COIL AND FOUND SECONDARY WINDING. RESISTANCE TOO HIGH BY FACTOR OF 10. 1H71 3O3 O A4CE E8CE 20010515001712001051500171SW 2001 5 15 20010508CW013 120010416G673041001554 HOUSING BELL 214 214B 1182100SW SERVO ACTUATOR GOUGED B QH5RK NONE O OTHER ININSP/MAINT 1 NM07 GOUGE PLUS LINER IND. BELOW GOUGE. 2G71 4U H6SW 20010523000192001052300019CE 2001 5 23 20010508CW016 120010413G323398820041 PISTON CESSNA172 172RG 2072438CE MLG ACTUATOR BROKEN D K NONE O OTHER NRNOT REPORTED 1 SO139985B10388 172RG1107 PISTON IN MAIN GEAR ACTUATOR BROKEN AT SECOND TOOTH FROM END. THIS LEFT GEAR TO SWING FREELY, NOT LOCKING DOWN. 1H71 3O 3A17 20010523000232001052300023SO 2001 5 23 20010508CW019 220010413G73226397172 THROTTLE BODY CESSNA188 188B 2073007CE CONT O520 IO520* 17032SO ENGINE OUT OF ADJ B T9ZRK NONE O OTHER ININSP/MAINT 1 SW99731CS280 280 18802796T THROTTLE BODY AND METERING UNIT WAS FOUND TO BE OUT OF ADJUSTMENT, DURING INSPECTION THE CONTROL ARM AT THROTTLE BODY WAS FOUND LOOSE AND ROTATING ON SHAFT. NO ADJUSTMENT OF IDLE MIXTURE OR IDLE COULD BE PERFORMED DUE TO CHANGING CONDITION BETWEEN THROTTLE BODY AND METERING UNIT. 1L71 3O3 O A9CE E5CE 20010524001312001052400131SO 2001 5 24 20010509CW002 120010326G27406270147 CONTROL CABLE PIPER PA28 PA28R201 7102816SO STABILIZER OUT OF RIG B H1ESO OTHER F FLT CONT AFFECTED DEDESCENT 1 NE012145M460 290 28R7837069 TRIM CABLE JACKSCREW STOP PIN NOT CONTACTING TRIM DRUM BEFORE TURNBUCKLE FERRULE REACHING AFT PULLEY AND CABLE GUARD, PREVENTING CABLE FROM MOVING. AC WAS IN FULL NOSE TRIM CONDITION, AC LANDED WITHOUT INCIDENT. TRIM CABLES WERE RE-RIGGED. 1L71 3O 2A13 20010524000042001052400004SW 2001 5 24 20010509CW009 120010413G5711 SPAR BBAVIA7 7EC 2110120SW CONT C90 C9012F 17009SO RT WING CRACKED D K NONE O OTHER ININSP/MAINT 1 GL0362667 7FC326 46889912 IN RECOVERING AIRFRAME, FOUND CRACK IN RIGHT WING REAR SPAR. AIRCRAFT WRECKED IN A NOSE OVER. NO LOG RECORD OF REPAIR TO REAR SPAR. 1H71 3O3 O A759 E252 20010510000012001051000001CE 2001 5 10 20010510AP001 120010424G783023220258511 LEVER ARONCA RKWELLNA265 NA26580 7630108CE THRUST REVERSER MISMANUFACTURED B JV2RK NONE W INADEQUATE Q C ININSP/MAINT 1 SW99316EC369 369 144 38038 ON 8/9/99 1EA. P/N232-20258-511 WAS INSTALLED ON LT T/R. 2EA. P/N 232-20258-513 AND 2EA. 232-20258-514 LEVERS WERE INSTALLED ON RT T/R DURING REPAIR OF THESE T/R''''S. IN JAN. 2001 THE CUSTOMER REPORTED PROBLEMS WITH THE LT T/R. INSPECTION OF BOTH T/RS REVEALED BROKEN DRIVE CABLES AND BENT LEVERS. IT WAS BELIEVED AT THIS TIME THAT THE LEVERS WERE NOT PER DRAWING AND REMAINING STOCK WAS RETURNED. 2L72 4F A2WE 20010510000022001051000002CE 2001 5 10 20010510AP002 120010309G3240ACM22740 VALVE RAYTHNDH125 HAWKER800 7450004CE GARRTTTFE731TFE7315BR WP MLG CONTAMINATED C D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO111650 526 NR 1 TIRE FLAT SPOTTED, NR 2 TIRE FLAT SPOTTED AND DEFLATED, NR 3 TIRE FLAT SPOTTED. VISUAL INSPECTION FOUND NR 1 MODULATOR VALVE CONTAMINATED WITH PAINT CHIPS AND SHAVINGS OF PLASTIC. FOUND NR 2 MODULATOR VALVE PISTON O-RING DECOMPOSED/CONTAMINATED. REPLACED NR 1 AND 2 MODULATOR VALVE, BRAKE CONTROL VALVE, FLUSHED ENTIRE BRAKE SYSTEM HYDRAULIC LINES AND FUNCTIONALLY TESTED BRAKE CONTROL SYSTEM. 2L72 4F4 FRTA3EU E6WE 20010510000032001051000003NM 2001 5 10 20010510AP003 120010425G3240 LINE AMD FALC50FALCON2000 2730170NM BRAKE SYSTEM LEAKING D K NONE K FLUID LOSS ININSP/MAINT 1 SO11120HG15 200055 RIGHT MLG BRAKE LINE WAS FOUND LEAKING FROM THE B NUT THAT CONNECTS THE LINE TO THE BRAKE CALIPER FITTING. THE BRAKE LINE IS MADE OF CLEAR PLASTIC TUBING AND THE B NUT IS BRASS AND UTILIZES A BRASS COMPRESSION FITTING TO FORM THE SEAL AT THE CALIPER FITTING. SUSPECT THE LEAK IS DUE TO THERMAL EXPANSION OF PLASTIC AND BRASS CAUSED BY ELEVATED BRAKE TEMPERATURES DURING SHORT FIELD BRAKING. SUGGEST THAT PLASTIC TUBING AND BRASS FITTINGS BE REMOVED AND REPLACED WITH AN STANDARD FITTINGS AND MEDIUM PRESSURE HOSE THAT MEETS THE APPROPRIATE MIL SPEC. 2K73 4F RTA50NM 20010510000042001051000004NM 2001 5 10 20010510AP004 120010425G5210 DOOR AMD FALC50FALCON2000 2730170NM PAX LEAKING D K NONE O OTHER ININSP/MAINT 1 SO11120HG15 200055 FOUND INSTRUMENTS AND RADIO DISPLAYS FOGGED OVER DUE TO CABIN WATER-LEAKS. LEAKS FOUND AROUND CABIN DOOR. SUSPECT LEAKAGE DUE IMPROPER DOOR ALIGNMENT AND/OR SEALING DURING MAUFACTURING. THIS CONDITION IF NOT CORRECTED WILL CAUSE PREMATURE CORROSION OF THE AIRCRAFT AND ELECTRICAL MALFUNCTION OF THE AVIONICS AND INSTRUMENTATION AS WELL AS DETERIORATION OF THE CABIN INTERIOR. SUBMITTER HAS OBSERVED THIS DISCREPANCY ON OTHER LIKE MODELS OF THIS AIRCRAFT. 2K73 4F RTA50NM 20010510000052001051000005CE 2001 5 10 20010510AP005 120010104G3242AC65218 MAXARET RAYTHNDH125 HAWKER800 7450004CE GARRTTTFE731TFE7315BR WP WHEEL AXLE INOPERATIVE C K NONE O OTHER ININSP/MAINT 1 SO111640 788 258376 NR 1 AND 2 TIRES FOUND FLAT SPOTTED DURING POST-FLIGHT INSPECTION. NR 1 MAXARET UNIT DID NOT PASS ANTI-SKID FUNCTIONAL TEST. REPLACED NR 1 MAXARET UNIT WITH OVERHAULD UNIT. 2L72 4F4 FRTA3EU E6WE 20010510000062001051000006CE 2001 5 10 20010510AP006 120010426G78101099500001 EXHAUST PIPE PWC BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA LT ENGINE BROKEN D K NONE O OTHER ININSP/MAINT 1 NM072354Y546 LJ1532 PE0179 THE LEFT ENGINE LEFT TAIL PIPE BROKE AT THE LIP HEAT INLET TUBE. 1L72 3T4 TRT3A20 E4EA 20010510000072001051000007GL 2001 5 10 20010510AP007 120010327G3213 ATTACH FITTING AVIAT A1 A1B GL LYC O360 O360* 41514EA LT MLG STRUT SHEARED G O OTHER O OTHER LDLANDING 1 NE03484C 2114 TACH 80.2 HOURS LEFT MAIN GEAR ATTACHMENT(FORWARD STRUT) SHEARED OFF AT FUSELAGE ATTACHMENT POINT DURING NORMAL LANDING OF AIRCRAFT. THE WELDED AREA THAT THE LH FORWARD STRUT ATTACHES TO THE FRAME LOOKS TO HAVE POSSIBLE INADEQUATE PENETRATION, POROUS AND CONSIDERED A COLD WELD. 1H71 3O3 ONCA22NM E286 20010510000082001051000008EA 2001 5 10 20010510AP008 120010427G3040F307 RESISTOR DHAV DHC6 DHC6300 2802606EA WINDSHIELD WIPERBURNED M H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW99 680 WINDSHIELD WIPER DROPPING RESISTOR SHORTED TO GROUND THROUGH DEACTIVATED WINDSHIELD WASHER RESISTOR MOUNT. THE WIPER DROPPING RESISTOR LEAD CHAFFED ON THE WINDSHIELD WASHER RESISTOR MOUNTING BRACKET. THIS RESULTED IN SMOKE IN THE COCKPIT DURING DESCENT WHILE USING WINDSHIELD WIPERS IN THE SLOW MODE. DEHAVILLAND MODIFICATION (MOD 6/1827)DEACTIVATED THE WINDSHIELD WASHER OPTION BY REMOVING THE WASHER SWITCH FROM THE OVERHEAD PANEL AND STOWING OR CAPPING THE POWER WIRE TO THE WASHER RESISTOR. 1H72 3T RTA9EA 20010529000012001052900001SO 2001 5 29 20010510CW001 120010308G274069623004 TUBE PIPER PA28 PA28140 7102802SO LYC O320 O320* 41508EA STABILIZER DEFECTIVE D K NONE W INADEQUATE Q C ININSP/MAINT 1 SW09567OU 2826467 ON THE TUBE, WHERE BOLT HOLE IS DRILLED THAT MOUNTS TO THE FRONT BRACKET ON STABILATOR, A HOLE IS IN TUBE, (90 DEGREE ANGLE TO THE BOLT HOLE). IT APPEARS THIS HOLE HAS SLAG IN IT AND SLAG EXIST ON INTERIOR OF THE TUBE THAT HAS BEEN THERE WHEN THE PART WAS FABRICATED. THIS EXTRANEOUS HOLE IS AT THE HIGH STRESS POINT IN THE TUBE AND HAS NOT BEEN ON ANY OF THE TUBES THAT HAVE BEEN INSPECTED FOR THE AD ON THE TUBES. HOLE WAS FOUND WHEN REMOVING THE THICK LAYER OF BLACK PAINT DOWN TO THE ZINC CHROMATE IN AREA THAT FITS INTO THE STABILATOR BRACKETS. THE AREA FIRST APPEARED AS A BLACK DOT OF PAINT AND CLOSER EXAMINATION REVEALED A HOLE HAD BEEN DRILLED AND FILLED WITH SOME TYPE OF MATERIAL AND PAINTED TO COVER. 1L71 3O3 O 2A13 E274 20010524000772001052400077SO 2001 5 24 20010511CW002 120010417G32226528000 FORK PIPER PA28 PA28181 7102807SO NLG STRUT SHEARED D EEJAO OTHER O OTHER LDLANDING 1 NM078285Y 288190023 THE AIRCRAFT WAS DOING A TOUCH AND GO, WHEN THE NOSE WHEEL STARTED TO SHIMMY. THE NOSE WHEEL FORK SHEARED OFF FROM THE LOWER STRUT TUBE. COULD NOT TELL IF THERE WAS A PREVIOUS CRACK IN THE TUBE. 1L71 3O 2A13 20010524000782001052400078NE 2001 5 24 20010511CW003 220010425G72502A0847 SEAL IAE V2500 V2500A1 NE NR 4 BEARING CRACKED B KB1RK NONE O OTHER ININSP/MAINT 1 NE01 PART RECEIVED FOR PENETRANT INSPECTION. PART REJECTED AT PENETRANT INSPECTION FOR INDICATION IN COUNTERBORE. 4 F E311NE 20010524001332001052400133EA 2001 5 24 20010511CW005 220010501G8520 CRANKCASE PIPER PA32 PA32R301T 7103220SO LYC O540 TIO540S1AD 41532EA HARTZLHCC3Y HCC3YR GL ENGINE CRACKED B BONRK NONE K FLUID LOSS ININSP/MAINT 1 GL198314B2077 32R8129021 L748061A FM183 DURING ANNUAL INSPECTION, NOTICED OIL ON LEFT FORWARD SECTION OF ENGINE. REMOVED PROP GOVERNOR AND ENGINE BAFFLING. FOUND SMALL CRACK IN CRANKCASE, FORWARD OF NR 2 CYLINDER UPPER FORWARD HOLD DOWN NUT. CONDITION PROBABLY CAUSED BY AGE, ENGINE HAS NEVER BEEN OVERHAULED. 1L71 3O3 O A3SO E14EA 5 CP25EA 20010515003322001051500332EU 2001 5 15 20010511CW007 120010419G6520369025400 GEARBOX HUGHES369 369FF EU ALLSN 250C 250C30 03013GL TAIL ROTOR FAILED B E6HRO OTHER O OTHER TXTAXI/GRND HDL 1 NM01530HL100031666 0066FF UPON SHUT DOWN, THE PILOT AND MECH NOTICE AN ODD NOISE COMING FROM THE TAIR ROTOR ACCOMPANIED BY A SLIGHT VIBRATION. AIRCRAFT WAS DUE FOR A 100 HR INSPECTION, SO T/R OIL WAS DRAINED AGAIN. THE CHIP PLUG HAD NO CHIPS BUT DID HAVE A BLACK PASTE. PASTE WAS EXAMINED AND HAD EXTREMELY SMALL METALLIC PARTICLES IN IT. NOT ENOUGH TO ILLUMINATE CHIP LIGHT. GEARBOX WAS DISASSEMBLED FOR INSPECTION. INPUT GEAR SHAFT WAS FOUND TO BE SHEARED IN TWO PIECES. IT IS NO UNDERSTOOD WHY THE GEARBOX DID NOT COMPLETELY FAIL BECOMING CATASTROPHIC. AIRCRAFT FLEW 3.5 HRS THIS DAY WITH NO EVIDENCE OF A PROBLEM. GEARSHAFT HAS BEEN SENT TO A LAB FOR TESTING AND MDHC HAS BEEN INFORMED. 1G71 3U3 U H3WE E1GL 20010524001432001052400143CE 2001 5 24 20010511CW008 120010423G531207126161 BULKHEAD CESSNA182 182L 2072726CE FUSELAGE CRACKED D K NONE O OTHER ININSP/MAINT 1 NM01423974787 18259003 FAILED INSPECTION DUE TO CRACKS IN CRITICAL AREAS, REPLACED. 1H71 3O NT3A13 20010524000132001052400013EA 2001 5 24 20010511CW014 220010419G732230802 FLOAT PRECISION PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA CARBURETOR DAMAGED B UC2RK NONE O OTHER ININSP/MAINT 1 GL1941460 75072523 2843153 L3611936A DURING OVERHAUL THE CARBURETOR FLOAT WAS FOUND WITH ONE OF THE CHAMBERS HALF FULL OF 100 LOW LEAD. 1L71 3O3 O 2A13 E286 20010524000292001052400029SW 2001 5 24 20010514CW003 120010507G322248838503 CYLINDER GULSTM112 114ARKWELL 7630315SW LYC O540 TIO540* 41532EA NLG FAILED H K NONE O OTHER NRNOT REPORTED 1 SW9957BH 3800 14001 NOSE GEAR ACTUATING CYLINDER, PN 48838503, FAILED INTERNALLY, CAUSING NOSE GEAR COLLAPSE, RESULTING IN MINOR DAMAGE TO AIRCRAFT 1L71 3O3 O A12SO E14EA 20010524000302001052400030CE 2001 5 24 20010514CW004 120010418G551095620010634 STABILIZER BEECH 95 95B55 1152729CE CONT O470 IO470* 17026SO RIGHT BENT D K NONE O OTHER ININSP/MAINT 1 SW091848W4195 TC1534 DURING INSTALLATION OF RIGHT HAND ELEVATOR, IT WAS DISCOVERED THAT WHEN THE ELEVATOR WAS MOVED FROM FULL DOWN TO FULL UP, THE STABILIZER WOULD FLEX UPWARD .4375. INVESTIGATION DISCLOSED THAT THE STABILIZER WAS BENT DOWN 2 DEGREES AT THE CENTER HINGE( BOTH SPARS) A TRIPLE PATCH WAS FOUND ON THE LOWER REAR SKIN, STARTING 12 INCHES FROM THE TIP. NO RECORD OF THIS REPAIR CAN BE FOUND IN THE AIRCRAFT RECORDS. CORRECTIVE ACTION: REMOVED AND REPLACED STABILIZER. 1L72 3O3 ORT3A16 E1CE 20010515005062001051500506CE 2001 5 15 20010515AP002 120010514G571257222061 RIB CESSNA441 441 2076020CE LEFT CENTER WINGCRACKED B K NONE O OTHER ININSP/MAINT 1 SW9912DT 8620 4410040 DURING A SCHEDULED INSPECTION, THE LEFT WING CENTER SECTION CANTED RIB CAP (CWS 26.85 INCHES) WAS FOUND CRACKED. THE CANTED RIB UPPER CAP (P/N: 5722206-1) WAS CRACKED AFT OF THE AFT MAIN SPAR AT FS 177.45, IN THE BEND RADIUS, AND RAN AFT APPROXIMATELY 1.375 INCH. THE CRACK WAS FIRST NOTED USING VISUAL INSPECTION THEN VERIFIED WITH DYE PENETRANT. AFTER REMOVING THE RIB CAP, CLOSE EXAMINATION OF THE PART REVEALED THAT THE CAP WAS MANUFACTURED SO THAT THE BEND WAS PARALLEL WITH GRAIN OF THE METAL INSTEAD OF PERPENDICULAR WHICH COULD RESULT IN THIS TYPE OF FAILURE. CESSNA CURRENTLY DOES NOT HAVE ANY SPECIFIC INSPECTIONS RELATING TO THIS MATTER, THEREFORE,THIS AREA SHOULD BE CLOSELY CHECKED DURING INSPECTIONS. 1L72 3T RTA28CE 20010515000812001051500081EU 2001 5 15 20010515AP004 120010504G3233AC11184 ACTUATOR FOKKERF27 F27MK400 4990626EU MLG BINDING M O OTHER J WARNING INDICATION CLCLIMB 1 SW99 8843 10652 LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER SELECTION OF LANDING GEAR TO THE UP POSITION. MAIN LANDING GEAR UPLOCK ACTUATOR WAS SLOW TO RETRACT TO LOCK THE GEAR IN THE UP POSITION AND TO EXTINQUISH THE UNSAFE LIGHT. THE ACTUATOR IS SPRING-LOADED TO THE RETRACT POSITION. 2H72 4T A817 20010515000832001051500083CE 2001 5 15 20010515AP005 120010504G7810829415 EXHAUST HEADER CESSNA421 421C 2076016CE CONT O520 GTSIO520N 17032SO WASTEGATE FLANGEDEFECTIVE B K NONE O OTHER ININSP/MAINT 1 SW996867D31 421C1084 THIS UNIT IS MANUFACTURED IN TWO HALVES, WHERE THE UPPER & LOWER HALVES WELDED TOGETHER (AT THE WASTE GATE FLANGE) THERE IS A HOLE AT THE WELD AREA ON EACH SIDE. THE REPLACMENT PART HAS AN ADDITIONAL WELD IN THESE AREAS THAT ARE NOT PRESENT ON THE DEFECTIVE PART. IT APPEARS THAT THE MANUFACTURING PROCESSES (WELDING)WERE NOT COMPLETED BEFORE THIS PART LEFT THE MANUFACTURE. THIS DEFECT WAS FOUND WHILE C\W THE EXHAUST PRESSURE TEST REQUIRMENTS OF AD 2000-01-16. 1L72 3O3 O A7CE E7CE 20010515000932001051500093 2001 5 15 20010515AP007 420010404G34217000466906 INDICATOR ATTITUDE FAILED D O OTHER W INADEQUATE Q C CRCRUISE 1 EA031NA 25 AFTER A FEW FLIGHTS WITH THE RECENTLY INSTALLED ADI IN THE PILOTS POSITION, THE GLIDESLOPE INDICATOR FAILED IN THE CENTER POSITION (INDICATING ON GLIDE PATH). INDICATOR REMAINED PARKED IN THIS POSITION FOR THE DURATION OF THE FLIGHT. REMOVED AND REPLACED UNIT. UNIT WAS OVERHAULED BY METRO AIRCRAFT INSTRUMENTS 20010524000662001052400066EA 2001 5 24 20010516CW001 220010511G852076220 STUD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA NR 3 CLYINDER FRACTURED G A UNSCHED LANDING DA INFLIGHT SEPARATION FLAME/FIRE CRCRUISE 1 AL0145008 1097 318052167 L691661A AT CRUISE FLIGHT, THE NR 3 CYLINDER SEPARATED FROM THE ENGINE CASE, WHICH RESULTED IN AN INFLIGHT FIRE. THE ENGINE CASE, CYLINDER HOLD DOWN STUDS THROUGH BOLT STUDS AND NR 3 CONNECTING ROD WERE SENT FOR LAB INVESTIGATION. INVESTIGATION RESULTS: THE PRIMARY CAUSE WHICH LED TO THE SEPARATION OF THE NR 3 CYLINDER WAS THAT THE THROUGH BOLT STUDS WERE MOST LIKELY NOT PROPERLY TORQUED. 1L72 3O3 O A20SO E14EA 20010524000032001052400003CE 2001 5 24 20010517CW009 120010427G2410DOFF10300J ALTERNATOR CESSNA177 177 2073704CE LYC O360 O360* 41514EA ENGINE SEIZED B R7LRK NONE O OTHER ININSP/MAINT 1 WP25412WS 126 17701475 ALTERNATOR OVERHAULED, INSTALLED ON AC. FRONT BEARING BALL CAGE BROKE APART AND ALLOWED BALLS TO COLLECT ON ONE SIDE OF BEARING, LOCKING THE ALTERNATOR SHAFT. FAILURE OCCURRED ON 2/10/2001 AFTER 126 HOURS TSOH. 1H71 3O3 ONTA13CE E286 20010529000372001052900037 2001 5 29 20010518CW001 420010430G3421 GYRO MOONEYM20 M20F 5870214SW COCKPIT CONTAMINATED B K NONE O OTHER ININSP/MAINT 1 WP279514M4315 2383 670091 DURING ANNUAL INSPECTION, FOUND LIQUID IN WINDOW OF GYRO, DISCONNECTED LINE TO HAVE WATER FLOW OUT, REMOVED INSTRUMENT. OPENDED CASE AND FOUND LONG-TERM CORROSION ON ALL INTERNAL PARTS. REPLACED WITH OVERHAULED INSTRUMENT. NO OTHER INSTRUMENTS CONTAINED WATER MAY HAVE GOTTEN WATER THROUGH A LEAKING EXTERIOR COWL DECK. 1L71 3O 2A3 20010529002692001052900269CE 2001 5 29 20010523CW001 120010501G2710051178217 YOKE CESSNA172 172L 2072432CE COCKPIT CORRODED D K NONE O OTHER APAPPROACH 1 SO193802Q3057 17259902 AIRCRAFT ON FINAL APPROACH, CONTROL YOKE FAILED AT APPROX 30 FT AGL. CONTROL YOKE FAILED JUST ABOVE PIVOT POINT BEHIND INSTRUMENT PANEL. CONTROL YOKE WAS EXTREMELY CORRODED AT FRACTURE POINT. 1H71 3O NT3A12 20010529002712001052900271EU 2001 5 29 20010523CW002 120010407G651083A851BC3 BEARING SNIAS 350 AS350B2 8680813EU T/R DRIVE SHAFT ROTATED C AALAK NONE O OTHER ININSP/MAINT 1 SW014035W2671 2912 AT A SCHEDULED INSPECTION THE BEARING PN 83A851BC3 HAD ROTATED IN THE RUBBER BUSHING PN FA3819 APPROX .3750. WE HAVE BEEN COMPLYING WITH SB REGARDING THE GREASING AND INSPECTION OF THESE BEARINGS AND STILL HAD A BEARING TURN. THIS IS AN AREA THAT CALLS FOR SPECIAL ATTENTION DURING INSPECTIONS AND DAILY PRE FLIGHTS. AT THIS TIME WE ARE INSTALLING THE NEWER TYPE BEARINGS THAT THIS SB DOES NOT APPLY TO. 1G71 3U H9EU 20010529002722001052900272EU 2001 5 29 20010523CW003 120010410G6510350A23106320 SEAL SNIAS 350 AS350B2 8680813EU T/R DRIVE SHAFT MISSING C K NONE O OTHER ININSP/MAINT 1 SW014035W2671 2912 2912 AT A SCHEDULED INSPECTION THE SELF ADHESIVE SEAL PN 350A-1063-20 WAS FOUND NOT TO BE INSTALLED. THIS IS A SEAL THAT IS INSTALLED FOR DISSIMILAR METAL CORROSION ON THE TAIL ROTOR DRIVE SHAFT HANGAR SUPPORT AND THE HANGAR BEARINGS. 1G71 3U H9EU 20010529002802001052900280CE 2001 5 29 20010523CW005 120010206G27803910104044 BEARING HELIO H295 H295 4300802CE TORQUE TUBE CRACKED D K NONE O OTHER ININSP/MAINT 1 NM095479G3782 1261 TORQUE TUBE BEARING MADE FROM NYLON MATERIAL HARDENS WITH AGE AND DURING OPERATION OF SLAT TORQUE TUBE. THE BEARING STARTS TO CRACK AT RIVET HOLES THAT ATTACHES IT TO WING RIB. REPLACED WITH NEW PORTS. 1H71 3O 1A8 20010529002812001052900281CE 2001 5 29 20010523CW006 120010206G27803910104046 BEARING HELIO H295 H295 4300802CE TORQUE TUBE CRACKED D K NONE O OTHER ININSP/MAINT 1 NM095479G3782 1261 TORQUE TUBE BEARING MADE FROM NYLON MATERIAL HARDENS WITH AGE AND DURING OPERATION OF SLAT TORQUE TUBE THE BEARING STARTS TO CRACK AT RIVET HOLES THAT ATTACHES IT TO WING RIB. REPLACED WITH NEW PARTS. 1H71 3O 1A8 20010529002822001052900282SW 2001 5 29 20010524CW001 120010427G760363255555 THROTTLE ARM MOONEYM20 M20R 5870225SW CONT O550 IO550* SO ENGINE WORN D K NONE O OTHER ININSP/MAINT 1 GL25143TM55 290242 684902 WHILE WARMING THE ENGINE FOR OIL CHANGE, NOTED THAT THERE WAS AN EXCESSIVE AMOUNT OF FREE PLAY IN THE THROTTLE LINKAGE. AFTER RUNNING THE ENGINE UP TO 1500 RPM, PULLED THROTTLE BACK TO IDLE, BUT THE ENGINE RPM DID NOT DECREASE. HAD TO USE THE MIXTURE CONTROL TO STOP ENGINE. INSPECTED THROTTLE LINKAGE AND FOUNDTHE THROTTLE ARM WAS LOOSE ON THE SHAFT. TORQUE SEAL ON THE ATTACHING NUT WAS NOT BROKEN AND NUT DID NOT APPEAR TO HAVE MOVED SINCE INSTALLATION. REMOVED THE THROTTLE ARM AND FOUND THE SERRATIONS ON THE ARM WHERE THE ARM MEETS THE THROTTLE SHAFT WERE WORN AWAY. ATTACHING NUT WAS NOT TIGHTENED PROPERLY AT INSTALLATION. MFG SUPPLIED NEW THROTTLE ARM , INSTALLED IT USING PROPER TORQUE PER SB. 1L71 3O3 ORT2A3 E3SO 20010529002832001052900283NE 2001 5 29 20010524CW002 120010427G6520643566409043 HOUSING SKRSKYS64 S64E 8142604NE T/R GEARBOX CRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09194AC6386 64017 DURING TEARDOWN FOR OVERHAUL, A CRACK WAS VISUALLY NOTICED AT APPROX THE 2 OCLOCK POSITION(AS INSTALLED ON AIRCRAFT) IN THE STRADDLE MOUNT OF THE IDLER GEAR ALIGNMENT BEARING PN SB2154-1 OF CENTER HOUSING PN 6435-66409-043. FURTHER INSPECTION AFTER REMOVAL OF BEARING RETAINER PN 6435-66427-103 REVEALED THE STRADDLE MOUNT WAS CRACKED IN HALF, PASSING THROUGH THE .275 IN DIAMETER HOLE FOR ROSAN STUD PN SF101-125A-6A. NO SECONDARY DAMAGE DUE TO THIS FAILURE WAS NOTED. 2G72 4U H4EA 20010529002902001052900290SO 2001 5 29 20010525CW001 120010226G55402344715 RUDDER HORN PIPER PA30 PA30 7103002SO LYC O320 IO320B1A 41508EA RUDDER CRACKED G K NONE O OTHER ININSP/MAINT 1 WP257129Y4374 30151 REMOVED HORN DUE TO WEAR BETWEEN HORN AND RUDDER. FOUND CRACKS FROM MOUNT HOLES TO TOP OF RUDDER HORNS OF SAME PART NUMBER TO BE CRACKED IN A SIMILAR FASHION . 1L72 3O3 O A1EA 1E12 20010529003362001052900336SW 2001 5 29 20010525CW005 120010525G2710145520101 CONTROL CABLE NAVIONNAVIONL17B 6150108SW AILERON FRAYED D K NONE O OTHER ININSP/MAINT 1 SO115335K NAV42235B UPON REMOVAL OF CABLES, FOUND FRAYED SECTION LOCATED JUST OUTBOARD OF THE AILERON ROLLERS (MID-WING ABOVE THE MAIN LANDING GEAR TRUNION). PROBABLE CAUSES INCLUDE ENVIRONMENTAL DAMAGE, TIME, AND INADEQUATE MAINTENCE OF ROLLERS. ROLLERS IN THIS AREA OF THIS AIRCRAFT WERE FROZEN. CABLES HAD BEEN COATED WITH GREASE IN THIS AREA OVER THE YEARS AND FORMED A SEMI-HARD SHELL WHICH COULD HAVE TRAPPED MOISTURE LEADING TO THE DAMAGE. RECOMMENDATIONS ARE TO MAINTAIN CABLES AND ROLLERS PROPERLY ESPECIALLY IN HARD TO REACH AREAS, AND THAT CABLES HAVE A FINITE LIFETIME. 1L71 3O A782 20010529003372001052900337SW 2001 5 29 20010525CW006 120010525G27301455201029 CONTROL CABLE NAVIONNAVIONL17A 6150106SW ELEVATOR FRAYED D K NONE O OTHER ININSP/MAINT 1 SO115335K NAV42235 UPON REMOVAL OF CABLE, FOUND FRAYED SECTION LOCATED AT THE LOWERMOST POINT EXITING THE PULLEY. PROBABLE CAUSES INCLUDE ENVIRONMENTAL DAMAGE (WHEEL WELL AREA) AND TIME. AS PART OF ANNUAL, ALL CABLES IN THIS AIRCRAFT WERE BEING REPLACED DUE TO OVERALL AGE AND CONDITION WHEN THIS PROBLEM WAS FOUND. 1L71 3O A782 20010529003382001052900338CE 2001 5 29 20010525CW007 120010327G7602C29950J0101 CONTROL CABLE CESSNA210 210L 2073448CE ENGINE BROKEN G A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 SO051759X367 210L60780 ENGINE STARTED TO SPAR DOWN IN FLIGHT. PILOT ATTEMPTED TO ADJUST MIXTURE, AFTER TURNING ON THE BOOST PUMPS. PILOT STATED, THE MIXTURE CABLE WAS LOOSE IN HIS HAND. ENGINE SHUT DOWN AND AIRCRAFT WAS LANDED , GEAR UP IN A FIELD. UPON EXAMINATION, THE MIXTURE CABLE WAS FOUND BROKEN AT THE POINT IT ENTERED THE PROTECTIVE BARREL OF THE ROD END. CORROSION WAS EVIDENT. 1H71 3O 3A21 20010529003402001052900340SO 2001 5 29 20010529CW001 120010502G274062701113 CONTROL CABLE PIPER PA28 PA28161 7102803SO STABILATOR FRAYED D K NONE O OTHER ININSP/MAINT 1 EA259182W6559 2841130 LEFT FORWARD STABILATOR CABLE WORN AND FRAYING AT SPAR FAIRLEAD AND REAR SPAR PULLEY. DIFFICULT TO DETECT WITHOUT REMOVING CABLE. 1L71 3O 2A13 20010529003412001052900341SO 2001 5 29 20010529CW003 120010508G2820STCSA1480WE FUEL TANK PIPER PA23 PA23250 7102308SO WING TIP BROKEN D K NONE O OTHER ININSP/MAINT 1 SO1521551 274714 FIBERGLASS WINGTIP FUEL TANK STC SA1480WE HAS AN EDGE DISTANCE OF .2500 INCH SCREW HOLES WHICH BROKE FIBERGLASS OUT CAUSING THE WINGTIP TO FALL OFF, WHILE AIRCRAFT WAS ON GROUND. FIBERGLASS TIP DOES NOT HAVE SUFFICIENT STRENGTH DUE TO FIBERGLASS THICKNESS AND EDGE DISTANCE. 1L72 3O 1A10 20010607000442001060700044CE 2001 6 7 20010529CW007 120010423G3710632617D GEAR CONT CESSNA337 337H 2075732CE VACUUM PUMP WORN D K NONE O OTHER ININSP/MAINT 1 SO15729AS725 33701938 A DETAINLED INVESTIGATION OF THE STARTER DRIVE REVEALED THAT ALL OF THE GEAR TEETH WERE WORN EXCESSIVELY ON ONE OF THE BEVEL GEARS WHICH DRIVES THE VACUUM PUMP. 1H72 3O A6CE 20010607000482001060700048CE 2001 6 7 20010529CW010 120010420G323008411132 SCREW CESSNA414 414 2075908CE MLG DAMAGED B AK6RK NONE O OTHER ININSP/MAINT 1 SW19922AS4803 4140033 UPON ANNUAL INSPECTION, FOUND ADJUSTING SCREW PN 084113-2, THREADS AT THE POINT OF PULLING OUT OF EYE BOLT END FITTINGS, PN 0841111-3. THIS IS THE 4TH DISCOVERY OF ADJUSTING SCREW AT THE POINT OF FAILURE WHICH, IF NOT HAD BEEN CORRECTED, WOULD BE IMMINENT GEAR FAILURE, SINCE THIS IS THE ONLY ITEM LOCKING THE MAIN GEAR INTO POSITION AFTER EXTENSION. 1L72 3O RTA7CE 20010607000492001060700049CE 2001 6 7 20010529CW011 120010405G323008411113 SCREW CESSNA414 414 2075908CE MLG DAMAGED B AK6RK NONE O OTHER ININSP/MAINT 1 SW19922AS4803 4140033 UPON ANNUAL INSPECTION, FOUND ADJUSTING SCREW, PN 084113-2, THREADS AT THE POINT OF PULLING OUT OF EYE BOLT END FITTINGS, PN 0841111-3,. THIS IS THE 4TH DISCOVERY OF ADJUSTING SCREW AT THE POINT OF FAILURE WHICH, IF NOT HAD BEEN SINCE THIS IS THE ONLY ITEM LOCKING THE MAIN GEAR INTO POSITION AFTER EXTENSION. 1L72 3O RTA7CE 20010710000592001071000059SW 2001 7 10 20010529CW014 120010313G7160600382305 LATCH MOONEYM20 M20S 5870226SW ALT AIR DOOR WORN B DY1RK NONE O OTHER ININSP/MAINT 1 EA132192N250 300041 DURING ROUTINE OIL CHANGE, FOUND MAGNETIC LATCH FOR ALTERNATE AIR DOOR BOX VERY WORN AND AREA AROUND IT COVERED IN ALUMINUM DUST. THE LATCH HOLDS THE DOOR IN THE CLOSED POSITION UNTIL THE AIR FILTER BECOMES CLOGGED WITH WATER/ICE (WHEN IN SUCH CONDITIONS) FORCING THE ALTERNATE AIR DOOR TO OPEN AUTOMATICALLY. WE ROUTINELY FIND THESE LATCHES VERY WORN AND ON THE VERGE OF COMING APART. THIS AIR BOX/LATCH SETUP IS USED ON SEVERAL MODELS, WHICH ALL HAVE THE SAME RECURRING WEAR PROBLEM. 1L71 3O RT2A3 20010710000602001071000060CE 2001 7 10 20010530CW001 120010530G3220NAS4645A15 BOLT CESSNA177 177RG 2073709CE NLG MISSING D K NONE O OTHER LDLANDING 1 SO137537V5311 0834 NOSE GEAR COLLAPSED ON LANDING ROLL OUT, DOWN LOCK LINK BOLT(LOWER) WAS FOUND MISSING PN NAS4645A15, NO MEANS OF SAFETY MAY BE USED WITH THIS DESIGN, ONLY LOCTITE CV SEALANT AS STATED IN SERVICE MANUAL. PART HAD 5311 HOURS. 1H71 3O A20CE 20010620000532001062000053WP 2001 6 20 20010531CW001 120010507G62105320003 BLADE HILLERUH12 UH12E 4360122WP MAIN ROTOR DELAMINATED B KQTRK NONE O OTHER ININSP/MAINT 1 SW11144HA538 HA3044 DOUBLER DELAMINATION NO SIGNS OF CORROSION OR IMPACT WHICH MIGHT CAUSE DELAMINATION. CAUSE UNKNOWN 1G71 3O 4H11 20010620000542001062000054 2001 6 20 20010531CW002 420010410G6122D4718 DRIVE GEAR HARTZL PIPER PA44 PA44180 7104402SO PROP GOVERNOR CRACKED B WIWRK NONE O OTHER ININSP/MAINT 1 WP074144C1034 227YS 4496020 GOVERNOR WAS SUBMITTED FOR INSPECTION DUE TO AN ENGINE FIRE ON THE GROUND. DURING INSPECTION, THE DRIVE GEAR PN D 4718 WAS FOUND CRACKED IN THE DRIVE GEAR SPLINES THAT ENGAGE THE GOVERNOR DRIVE ON THE ENGINE. THE GEAR CONTAINS TWO CRACKS, ALMOST 180 DEGREES APART AND OVER .5000 INCH LONG. HAD THE ENGINE NOT CAUGHT FIRE, THIS GEAR MOST LIKELY WOULD HAVE FAILED IN SERVICE. 1L72 3O A19S0 20010620000552001062000055CE 2001 6 20 20010531CW003 120010425G273115703072 CIRCUIT BOARD CESSNA206 TU206F 2073353CE ELEV TRIM SYSTEMSHORTED D K NONE O OTHER NRNOT REPORTED 1 NM088033Q704 420603088 SHORT CIRCUIT RESULTED IN BURNED SPOT ON BOARD AND OPEN CIRCUIT. CAUSE APPEARS TO HAVE RESULTED FROM ELECTRICAL OVERLOAD TO CONNECTION. CAUSE FOR OVERLOAD-UNKNOWN. 1H71 3O A4CE 20010620000612001062000061SW 2001 6 20 20010601CW004 120010509G6510407340339103 BEARING BELL 407 407 SW TAIL ROTOR SEIZED D YADAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 EA1970AP 786 53409 PILOT FELT EXCESSIVE VIBRATION AND HEADED BACK TO BASE, AFTER SHORT PERIOD VIBRATION INCREASED, PILOT LANDED IN FIELD. FOUND TAIL ROTOR HANGER BEARING SEIZED AND SPUN IN BEARING HOUSING. THE BEARING THAT FAILED IS THE FIRST BEARING AFT LOCATED JUST FORWARD OF OIL COOLER BLOWER. 1G71 3U O H2SW 20010620000662001062000066CE 2001 6 20 20010601CW009 120010511G3240 LINE BEECH 23 C23 1151242CE BRAKE SYS LEAKING B K NONE K FLUID LOSS ININSP/MAINT 1 GL139743L M1371 MOST OF THE FLEXIBLE FLUID LINES IN THIS AIRCRAFT WERE FOUND TO BE STIFF. TWO OF THE BRAKE LINES WERE FOUND TO BE CHAFFING ON THE FORWARD FIREWALL AREA AND WERE WORN SMOOTH ON THE OUTSIDE. BOTH OF THESE WERE LEAKING THROUGH THE HOSE. ALL OF THE FLEXIBLE FLUID LINES IN THE BRAKE SYSTEM WERE REPLACED. THE FLEXIBLE FLUID LINES BETWEEN THE FUEL TANKS AND SELECTOR VALVE WERE ALSO REPLACED. MOST OF THESE APPEARED TO BE ORIGINAL AND WERE ABOUT 30 YEARS OLD. THE FLEXIBLE LINES IN THE ENGINE COMPARTMENT ARE BEING REPLACED ALONG WITH ENGINE MAINTENANCE AT ANOTHER LOCATION. 1L71 3O A1CE 20010620000722001062000072CE 2001 6 20 20010604CW001 120010509G5712 RIB CESSNA177 177RG 2073709CE LT WING CRACKED B T9ZRK NONE O OTHER ININSP/MAINT 1 NM0952472 177RG1196 DURING THE INSTALLATION OF SHOULDER HARNESS KITS, THE HEADLINER WAS REMOVED. CORROSION ON CARRY THRU SPAR FORE AND AFT TOP SPAR CAPS AND SKIN WAS NOTICED. CORROSION WAS ALSO PRESENT AT LEFT AND RIGHT ROOT RIBS. LEFT ROOT RIB HAD SMALL CRACK. NO FURTHER ACTION TAKEN. 1H71 3O A20CE 20010620000732001062000073CE 2001 6 20 20010604CW002 120010405G781017540071 RISER CESSNA172 172Q 2072437CE LYC O360 O360* 41514EA EXHAUST SYS CRACKED D K NONE O OTHER ININSP/MAINT 1 CE09469NE 17275952 NR 3 EXHAUST RISER CRACKED AT FLANGE. NOTED: COMMON FAILURE, PER EXHAUST REPAIR STATION. 1H71 3O3 ONT3A12 E286 20010620000742001062000074EU 2001 6 20 20010604CW003 120010410G612021014 COLLAR SOCATAMS894 MS894A 8402842EU FRNKLN6AV3506A350C1 27043EA PROPELLER LOOSE D K NONE O OTHER ININSP/MAINT 1 CE0943BF 11931 528663 PROBLEM REPORTED: PROP WOULD NOT CYCLE W/WARM ENGINE OIL. DISASSEMBLED ENGINE AND FOUND ONE SOCKET HAS SCREW .1562 THAT HOLDS THE TRANSFER COLLAR TOGETHER BROKEN ALLOWING THE COLLAR AND SEALS TO BECOME LOOSE ON CRANKSHAFT OIL TO ESCAPE AND NOT ALL TO THE PROPELLER. NO IMPROPER REPAIR, PREVIOUS ACTIONS. 1L71 3O3 O 7A14 E9EA 20010625001672001062500167NE 2001 6 25 20010604CW005 120010426G5610S16206510421 TRACK SKRSKYS58T S58JT 8141807NE PILOT WNDOW DEFECTIVE A O OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 GL23902CH65 581539 TRACK ASSEMBLY ON PILOTS SLIDING WINDOW CAME APART ALLOWING WINDOW TO DEPART THE AIRCRAFT. WINDOW FRAME AND TRACK ASSEMBLY HAD ONLY 65 HOURS TT APPARENT DEFECTIVE TRACK ASSEMBLY. 2G72 4U 1H11 20010625001682001062500168CE 2001 6 25 20010604CW006 120010514G32200542106 SPRING CESSNA170 170B 2072306CE TAIL WHEEL BROKEN D O OTHER O OTHER NRNOT REPORTED 1 AL013143A300 25787 TAILWHEEL SPRING BROKE AT AN EXISTING CRACK. TAILWHEEL THEN DAMAGED THE LOWER SKINS OF THE RUDDER. 1H71 3O A799 20010625001722001062500172SW 2001 6 25 20010604CW012 120010522G2810 FUEL CELL MOONEYM20 M20F 5870214SW FUEL SYSTEM CONTAMINATED G A UNSCHED LANDING RY PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CLCLIMB 1 GL15301LM 670323 ENGINE LOST POWER, THEN QUIT, DURING TAKEOFF CLIMB. AIRCRAFT MADE OFF AIRPORT LANDING. INVESTIGATION FOUND WATER IN THE RIGHT HAND FUEL SUMP. AIRCRAFT HAD BEEN PARKED OUTSIDE THROUGH HEAVY RAIN. 1L71 3O 2A3 20010625001742001062500174GL 2001 6 25 20010604CW015 320010319G6110HCB37N5 CLAMP GULSTM690TP 690A 0141722SW HARTZLHCB3T HCB3TN5 GL PROPELLER CORRODED B K NONE O OTHER ININSP/MAINT 1 SW15246T 560 373 11254 BV3280 CORROSION IN CLAMPS AND BEARING RACES, REJECTED ALL 3 CLAMPS AND 1 RACE. 1H72 3T 2A4 6 CP15EA 20010625001762001062500176GL 2001 6 25 20010604CW016 120010511G7160191965910 HINGE BLANCA17 1731A 1220435GL LYC O540 IO540* 41532EA HARTZLHCC3Y HCC3YR GL ALT AIR DOOR FAILED D K NONE O OTHER ININSP/MAINT 1 EA059505E 7532159 L1270848A DY270 PILOT DID NOT REPORT ANY ABNORMAL OPERATION. AIR BOX WAS REMOVED AT ANNUAL INSPECTION FOR SERVICING AND ALTERNATE AIR DOOR FELL ON FLOOR. ALL HINGE PIN SEGMENTS HAD FAILED. 1L71 3O3 O A18CE 1E4 5 CP25EA 20010626000172001062600017NE 2001 6 26 20010605CW014 220010515G7314640197 SHAFT NASH GE CFM56 CFM56* 13802NE FUEL PUMP BROKEN B K NONE O OTHER ININSP/MAINT 1 SO17 FB78955 UPON DISASSEMBLY I FOUND THE SHAFT IN TWO PIECES. THE STANDARD 64-0197 SHAFT IS A SOLID ONE PIECE SHAFT. THE SHAFT THAT WAS REMOVED FROM THIS UNIT WAS MACHINED INTO TWO DIFFERENT PIECES, AND WAS HELD TOGETHER BY TWO PINS. THIS IS NOT A STANDARD REPAIR. ONE OF THE FINS FAILED AND SHAFT SEPARATED. 4 F E2GL 20010626000182001062600018CE 2001 6 26 20010605CW015 120010502G5540S100442A BUSHING CESSNA172 172 2072402CE RUDDER HINGE DAMAGED D K NONE O OTHER ININSP/MAINT 1 WP25 NEW RUDDER HINGE HOT BUSHING, MISSING LARGE CHUNK OUT OF BOTTOM END OF BUSHING. 1H71 3O NT3A12 20010626000192001062600019CE 2001 6 26 20010605CW016 120010426G7714S33291 TACHOMETER CESSNA172 172R 2072401CE COCKPIT OUT OF TOLERANCED K NONE O OTHER ININSP/MAINT 1 NM01 NEW TACHOMETERS OUT OF MFG 50 RPM TOLERANCES. DIGITAL CHECKS OF FINE ADDITIONAL 172R AND 172S AIRCRAFT SHOWED TACH TO READ WITHIN PLUS OR MINUS 50 RPM. DISCOVERED WHEN DOING AD. 1H71 3O NT3A12 20010626000202001062600020CE 2001 6 26 20010605CW017 120010516G2434DOFF10300E ALTERNATOR CESSNA337 337G 2075730CE CONT O360 IO360G 17025SO FWD ENGINE FAILED B N9VRO OTHER H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 SO03297DC 31 01697 352438 OWNER OF THIS AIRCRAFT EXPERIENCED FWD ENGINE ALTERNATOR FAILURE (AS INDICATOR BY FAILURE LIGHT) DURING FLIGHT. TECHNICIAN AND OWNER REMOVED ALTERNATOR FROM ENGINE AND DISCOVERED THE DRIVE SHAFT SHEARED. THE GEAR RETAINING BOLT HAD RUBBED INTERNALLY AND BUSTED A PIECE OF THE COTTER PIN OFF, WHICH WAS FOUND ON THE MAGNETIC OIL DRAIN PLUG. THE DRIVE GEAR ALSO DISPLAYED SIGNS OF WEAR. THE ALTERNATOR SHAFT FAILURE APPEARS TO BE A MATERIAL DEFECT. 1H72 3O3 O A6CE E1CE 20010628000122001062800012 2001 6 28 20010605CW018 420010504G2562AK450 TRANSMITTER MOONEYM20 M20R 5870225SW CONT O550 IO550* SO ELT FAILED B DY1RK NONE L NO TEST ININSP/MAINT 1 EA13121RP393 290141 DURING ANNUAL INSPECTION, PERFORMED ELT INSPECTION IAW FAR 91.207D, AND FOUND THAT ELT DOES NOT TRANSMIT A SIGNAL EVEN THOUGH RED TRANSMIT LIGHT ON UNIT LIGHTS UP. UNIT TESTED USING 3 DIFFERENT ANTENNA SOURCES AND VERIFIED THAT ELT BATTERY IS GOOD. TRANSMIT LIGHT WORKS IN THE ON POSITION AND ARM POSITION WHEN THE G SWITCH IS ACTIVATED BUT STILL NO AUDIBLE SIGNAL HEARD FROM AIRCRAFT RADIOS OR A PORTABLE AM RADIO. 1L71 3O3 ORT2A3 E3SO 20010716000012001071600001SO 2001 7 16 20010605CW019 120010511G3260 SWITCH SWFTMSGC1B GC1B 9230104SO CONT O360 IO360C 17025SO COCKPIT DEFECTIVE G O OTHER N FALSE WARNING LDLANDING 1 GL252429B 3729 060654R INVESTIGATION SUBSEQUENT GEAR UP LANDING, FINDS WIRES TO THROTTLE MICRO SWITCH FOR GEAR WARNING SYSTEM INCORRECTLY CONNECTED. SWITCH FUNCTION INOPERATIVE. WHEN WIRES CORRECTLY CONNECTED TO SWITCH, FUNCTION RESTARTED. FLAG/SPADE CONNECTING EXTREMELY LOOSE, FELL OFF AT SLIGHTEST FORCE. WHEN CONNECTED, SWITCH DOES NOT ACTIVATED GEAR WARNING LIGHT UNTIL THROTTLE IS PULLED HARD TO POST IDLE. (POOR WIRE CONNECTING, MISWIRED, AND MISRIGGED SWITCH. 1L71 3O3 ONCA766 E1CE 20010628000132001062800013CE 2001 6 28 20010606CW001 120010517G270105600145 YOKE CESSNA172 172P 2072436CE COCKPIT CORRODED B R2JRK NONE O OTHER ININSP/MAINT 1 EA21622588300 17275236 WHILE PERFORMING ANNUAL INSPECTION AND SB, FOUND ELEVATOR CONTROL YOKE CONTAINED RUSTY WATER, CAUSING EXCESSIVE CORROSION. IF THIS PART FAILS COMPLETE LOSS OF ELEVATOR CONTROL RESULTS. SB PERMITS DRILLING HOLE FOR RECURRING INSPECTION. SUGGEST SB SEB-01-3 BE MADE AN AD NOTE. 1H71 3O NT3A12 20010628000142001062800014EA 2001 6 28 20010606CW002 220010515G8530AL75089 PISTON RING CESSNA172 172RG 2072438CE LYC O360 O360* 41514EA NR 3 CYLINDER BROKEN D K NONE O OTHER ININSP/MAINT 1 EA259746B1110 172RG1009 AIRCRAFT WAS CONSUMING A LARGE QUANTITY OF OIL. UPON INSPECTION FOUND THE NR 3 CYLINDER OIL CONTROL RING LAND ELONGATED DUE TO A SMALL PIECE OF RING WHICH HAD BROKEN OFF AND BEGAN TO FLUTTER. PROBABLE CAUSE OF SHOCK COOLING. 1H71 3O3 O 3A17 E286 20010628000152001062800015SO 2001 6 28 20010606CW003 120010412G57116405506 SPAR PIPER PA25 PA25235 7102504SO LT WING CORRODED D K NONE O OTHER ININSP/MAINT 1 CE097031Z 252791 WING WAS BEING DISASSEMBLED FOR RIB REPLACEMENT. REINFORCEMENT PLATE WAS DRILLED OFF AND CORROSION FOUND ON AFT FACE OF SPAR WEB AND FACE OF REINFORCEMENT PLATE. CAUSE: MOISTURE WICKING BETWEEN PLATES AND LACK OF CORROSION PROTECTION. 1L71 3O 2A10 20010628000162001062800016SO 2001 6 28 20010606CW004 120010412G57206418800 DOUBLER PIPER PA25 PA25235 7102504SO LT WING CORRODED D K NONE O OTHER ININSP/MAINT 1 CE097031Z 252791 WING WAS BEING DISASSEMBLED FOR RIB REPLACEMENT. REINFORCEMENT PLATE WAS DRILLED OFF AND CORROSION FOUND ON AFT FACE OF SPAR WEB AND FACE OF REINFORCEMENT PLATE. CAUSE: MOISTURE WICKING BETWEEN PLATES AND LACK OF CORROSION PROTECTION. 1L71 3O 2A10 20010716000072001071600007 2001 7 16 20010608CW004 420010430G2210AC66375 HOUSING SERVO CRACKED H QH5RK NONE O OTHER ININSP/MAINT 1 NM07 CRACKS IN SERVO BODY. 20010716000082001071600008 2001 7 16 20010608CW005 420010430G2210AS67244 HOUSING SERVO CRACKED H QH5RK NONE O OTHER ININSP/MAINT 1 NM07 CRACKS IN SERVO BODY. 20010716000092001071600009 2001 7 16 20010608CW006 420010425G2210AS66375 HOUSING SERVO CRACKED H QH5RK NONE O OTHER ININSP/MAINT 1 NM07 CRACK IN SERVO BODY. 20010716000102001071600010CE 2001 7 16 20010612CW001 120010403G7603 THROTTLE CABLE CESSNA172 172M 2072418CE ENGINE FAILED D TG3RK NONE O OTHER ININSP/MAINT 1 NM017603 3857 17267200 AFTER REMOVING ENGINE COWLING, INSP ENG CONTROLS, DISCOVERED THROTTLE CABLE HAD FAILED, DUE TO AGE. DESIGN IS SUCH THAT OUTER HOUSING, WHICH IS CONSTRUCTED OF PLASTIC, HAD DEVELOPED SMALL CRACKS. CRACKS WERE VISIBLE IN AREAS AFT OF POINT OF FAILURE IN SECTION OF CABLE FORWARD OF THE FIREWALL. AT THE POINT IN THE CABLE THAT HAS A SWEDGED FITTING OVER THE OUTER HOUSING INTENDED TO SECURE CABLE TO THE BRACKET THAT MOUNTS TO ENGINE, THE OUTER HOUSING PLASTIC HAD CRACKED TO THE POINT THAT PIECES FELL OUT OF THE SWEDGED FITTING. CLAMP HAD LOST ITS TENSION ON OUTER HOUSING AND ANY MOVEMENT OF THE THROTTLE CONTROL WOULD CAUSE THE OUTER HOUSING TO MOVE INSTEAD OF CARBURETOR CONTROL ARM. 1H71 3O NT3A12 20010716000112001071600011NE 2001 7 16 20010612CW002 220010508G72502A0851 SEAL IAE V2500 V2500A1 NE NR4 BEARING CRACKED B KB1RK NONE O OTHER ININSP/MAINT 1 NE03 PART REJECTED A F.P. I. FOR LINEAR INDICATIONS ON BOSSES. 4 F E311NE 20010716000132001071600013 2001 7 16 20010612CW004 420010507G2561AV2A LIFE VEST CABIN FAILED B KQ1RK NONE O OTHER ININSP/MAINT 1 EA07 LIFE VEST FAILED. 20010716000142001071600014 2001 7 16 20010612CW005 420010507G2561KSE35L8 LIFE VEST CABIN FAILED B KQ1RK NONE L NO TEST ININSP/MAINT 1 EA07 LIFE VEST FAILED. 20010716000222001071600022CE 2001 7 16 20010612CW013 120010524G760312B57 THROTTLE ARM CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA COCKPIT CRACKED D K NONE O OTHER ININSP/MAINT 1 SW075302E410 17271828 L812076T THROTTLE ARM FOUND CRACKED DURING 100 HOUR INSPECTION, FIRST APPEARED TO BE CASTING FLASH. PART REMOVED, DYE CHECKED AND VERIFIED CRACKED. 1H71 3O3 ONT3A12 E274 20010716000232001071600023CE 2001 7 16 20010612CW014 120010501G323212810013 ACTUATOR CESSNA172 172RG 2072438CE MLG CRACKED D K NONE O OTHER ININSP/MAINT 1 WP096291R8861 172RG0151 DURING INSPECTION, FOUND THE NECK OF ACTUATOR HOUSING BODY CRACKED .7500 WAY AROUND. ROLLER FOR INTERNAL PISTON ARM AND GEAR WAS SLIDING OUT. GEAR WAS PERFORMING NORMAL AT TIME FOUND(100 HOUR INSPECTION). 1H71 3O 3A17 20010716000242001071600024EA 2001 7 16 20010612CW015 220010515G8530AL75089 RING CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA NR 3 CYLINDER WORN D K NONE O OTHER ININSP/MAINT 1 EA259746B1110 172RG1009 L2988836A AIRCRAFT WAS CONSUMING A LARGE QUANTITY OF OIL. UPON INSPECTION, FOUND THE NR 3 CYL OIL CONTROL RING LAND ELONGATED DUE TO A SMALL PIECE OF RING WHICH HAD PIECE OF RING WHICH HAD BROKEN OFF AND BEGAN TO FLUTTER. PROBABLE CAUSE: SHOCK COOLING. 1H71 3O3 O 3A17 E286 20010716000262001071600026CE 2001 7 16 20010612CW017 120010511G32400411549 BRACKET CESSNA206 TU206G 2073357CE LT MLG BROKEN D O OTHER O OTHER TXTAXI/GRND HDL 1 SO01206TT3359 020605283 PILOT LOST LEFT BRAKE DURING TAXI. INSPECTION REVEALED MASTER CYLINDER LOWER ATTACH BRACKETS BROKEN. 1H71 3O A4CE 20010716000272001071600027CE 2001 7 16 20010612CW018 120010511G32400411550 BRACKET CESSNA206 TU206G 2073357CE LT MLG BROKEN D O OTHER O OTHER TXTAXI/GRND HDL 1 SO01206TT U20605283 PILOT LOST LEFT BRAKE DURING TAXI. INSPECTION REVEALED MASTER CYLINDER LOWER ATTACH BRACKETS BROKEN. INSPECTION OF OTHER AIRCRAFT FOUND SAME PARTS BENT. 1H71 3O A4CE 20010716000292001071600029CE 2001 7 16 20010613CW002 120010526G275098600581 CONTROL CABLE CESSNA210 T210L 2073449CE T/E FLAP SLIPPED D K NONE F FLT CONT AFFECTED ININSP/MAINT 1 CE0593344 21060371 DURING 100 HR INSPECTION, FOUND FLAPS NOT WORKING PROPERLY, FOUND CONTROL PUSH/PULL CABLE OUTER HOUSING WHERE HOUSING IS CLAMPED, SLIPPING IN CLAMP BUSHING. ORDER NEW CABLE FROM CESSNA, IT WAS TOO SHORT, CALLED CESSNA AND FOUND THEIR STOCK WAS MANUFACTURED WRONG. CESSNA HAD A NEW CABLE MADE. INSTALLED NEW CABLE. OPS CHECKED. NEW CABLE WAS BINDING, CAUSING WING RIB TO FLEX AND STRETCHED CABLE HOUSING. 1H71 3O 3A21 20010717000352001071700035SW 2001 7 17 20010613CW006 120010526G3020189502 ARM BBAVIA7 7GCBC 1220601SW CARBURETOR HEAT WORN G K NONE O OTHER ININSP/MAINT 1 CE057650S652 92876 AN4 BOLT ACTS AS TERMINAL END OF CARBURETOR HEAT CABLE AND IS FREE TO ROTATE IN HOLE DRILLED NEAR END OF SHAFT ASSY ARM OF CARB HEAT BUTTERFLY VALVE IN CARB AIR INTAKE BOX. FORE AND AFT MOVEMENT, RESULTING FROM CARB HEAT APP. HAS ELONGATED HOLE IN ARM AND CUT BOLT APPROX .7500 THRU ITS DIAMETER, ALLOWING APPROX .3125 FREE TRAVEL OF ARM AND FREE VERT DISPLACEMENT OF CARB HEAT BUTTERFLY VALVE FROM FULLY CLOSED TO APPROX .5000 OPEN. REPAIR ACCOMPLISHED BY REAMING OUT HOLE ON ARM TO ACCEPT BUSHING TO RETAIN AN4 BOLT OR TO ACCEPT AN5 BOLT. THEREBY EXPANDING SURFACE BRG CONTACT BETWEEN ARM AND BOLT. FUTURE WEAR CAN BE MINIMIZED BY CONTINUED ATTENTION TO LUBRICATION OF BOLT. 1H71 3O NCA759 20010716000322001071600032CE 2001 7 16 20010613CW008 120010525G323312810003 ACTUATOR CESSNA172 172RG 2072438CE MLG CRACKED B K NONE O OTHER ININSP/MAINT 1 SO13646B 172RG1116 FOUND ONE ACTUATOR CRACKED. 1H71 3O 3A17 20010716000332001071600033CE 2001 7 16 20010613CW009 120010525G323312810003 ACTUATOR CESSNA172 172RG 2072438CE MLG CRACKED B K NONE O OTHER ININSP/MAINT 1 SO139654B 172RG0947 FOUND ONE ACTUATOR CRACKED. 1H71 3O 3A17 20010725000702001072500070NE 2001 7 25 20010613CW010 220010601G7261AS3209013 O-RING PWA PT6 PT6A67D NE ENGINE BROKEN F MASRK NONE O OTHER ININSP/MAINT 1 SW01 PART WAS REMOVED NEW FROM FLOOR STOCK. WHEN O-RING WAS REMOVED FROM SEALED PACKAGE IT WAS FOUND TO BE BRITTLE AND BROKEN INTO 4 PIECES. SEVERAL OTHER O-RINGS WERE CHECKED AND ALL WERE FOUND TO BE SERVICEABLE. 4 T E26NE 20010716000342001071600034NE 2001 7 16 20010613CW011 220010530G72503028601 BLADE PWA JT15 JT15D4 52112NE ENGINE SEPARATED B O OTHER O OTHER NRNOT REPORTED 1 SW1561MA PCE70547 BACKGROUND: PCE 70547 SUSTAINED TYPICAL BLADE SEPARATION AND RESULTED DOWN STREAM DAMAGE. THE 3028601 BLADE HAS A 3500 HOUR TIME LIMIT ON THE JT15D-4 ENGINE. THE SEPARATION OCCURS APPROX 1800 HOURS OF OPERATION DEPENDING ON ENGINE OPERATION. INSP OF BLADES REVEALED AN AVERAGE GROWTH OF.007. 4 F E1NE 20010716000352001071600035NE 2001 7 16 20010613CW012 220010530G72503028601 BLADE PWA JD15 JT15D1A NE ENGINE SEPARATED B IY2RO OTHER O OTHER NRNOT REPORTED 1 SW15511AT2717 PCE76579 BACKGROUND: THE 3028601 TURBINE BLADE INSTALLED ON THE JT15D-1A ENGINE HAVE A 3500 HOUR LIFE LIMIT. THIS TURBINE BLADE TENDS TO CRACK AT THE AIRFOIL AND BREAK CAUSING EXTENSIVE DOWNSTREAM FAILURE/DAMAGE. THE BLADE WILL TYPICALLY GROW IN EXCESS OF .007 INCH AND BREAK. THIS USUALLY HAPPENS BETWEEN THE 1800-3000 HOUR MARK, DEPENDING ON ENGINE OPERATION. 4 F E25EA 20010716000462001071600046CE 2001 7 16 20010613CW023 120010509G5711 SPAR CESSNA177 177RG 2073709CE WING CORRODED B T9ZRK NONE O OTHER ININSP/MAINT 1 NM0952472 177R61196 DURING THE INSTALLATION OF SHOULDER HARNESS KITS THE HEAD LINER WAS REMOVED. CORROSION WAS PRESENT AT FORE AND AFT UPPER, SPAR CAPS AND SKINS. OWNER WAS ADVISED. FURTHER INSPECTION FOUND CORROSION PRESENT UNDER LEAD SHEETS IN THE SAME AREA. LEFT AND RIGHT ROOT RIB ASSEMBLIES ALSO HAD CORROSION PRESENT AS WELL AS A CRACK IN THE LEFT HAND ROOT RIB. PROPER INSPECTION PROCEDURE SHOULD HAVE CAUGHT THIS PRIOR TO REACHING THIS STAGE OF CORROSION. 1H71 3O A20CE 20010424002872001042400287CE 2001 4 24 2001085 120010419G2720 CONTROL UNIT BEECH 1900 1900D 1154162CE RUDDER MALFUNCTIONED A GLBAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CE01257GL UE257 UNCOMMANDED RUDDER BOOST IN FLIGHT, PENDING CORRECTIVE ACTION 2L72 4T RTA24CE 20020124000992002012400099CE 2002 1 24 2001112329 120011126G2910465588001045 LINE RKWELLNA265 NA26565 7630107CE HYD SYSTEM CRACKED B K NONE K FLUID LOSS ININSP/MAINT 1 CE016NR 4655 46529 MAINTENANCE PERSONNEL NOTICED FLUID LEAKAGE FROM BELLY PANEL AFT OF LANDING GEAR FOLLOWING PILOT'S COMPLETION OF "SPOILER AUTO EXTEND" PREFLIGHT CHECK BY FLIGHT CREW. VISUAL INSPECTION DETERMINED SPOILER AUTO EXTEND LINE ASSEMBLY TO BE LEAKING PAST B-NUT AND SLEEVE WHERE IT CONNECTS TO SPOILER CONTROL DUMP VALVE. DEFECT WAS CRACK AT LIP OF DOUBLE FLARE. MOST PROBABLE CAUSE IS SUDDEN SHOCK FROM AUTO EXTEND ACTIONS AT LANDING AND DURING PREFLIGHT CHECKS. 2L72 4J A2WE 20010730003032001073000303EU 2001 7 30 2001F00015 220010605G73101159P20106 FUEL LINE GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY5118 54523EU RT ENGINE RUPTURED C O OTHER R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA0980AG 164 RIGHT MAIN FUEL LINE RUPTURED ON TAKEOFF WHICH CAUSED ENGINE TO SPOOL DOWN TO FLIGHT IDLE. REPLACED FUEL LINE ON ENGINE. HP FUEL PUMP WAS ALSO DAMAGED AND REPLACED. ENGINE WAS BORESCOPED AND RETURNED TO SERVICE. 2L72 4F4 FRTA12EA E2EU 20010717000362001071700036SO 2001 7 17 2001F00037 220010505G8520 SNAP RING CONT CESSNA185 A185F 2072821CE CONT O550 IO550* SO CRANKSHAFT MISSING D E ENGINE SHUTDOWN O OTHER ININSP/MAINT 1 AL0518118850 284276R 18503328 3-26-01 REMOVED NO. 1 AND 3 CYLINDERS TO COMPLY WITH CRANKSHAFT COUNTER WEIGHT AD. FACTORY TECH REP REMOVED AND INSPECTED COUNTER WEIGHT AMOUNTING FLANGES (4), REPLACED COUNTER WEIGHTS AND ASSOCIATED PARTS, AND CYLINDERS AND ASSOCIATED PARTS, 50 ENGINE HOURS LATER AFT COUNTER WEIGHT PIN FELL OUT DURING START UP. ENGINE DAMAGED SUBSTANTIAL. ENGINE REMOVED AND REPLACED. 1H71 3O3 O 3A24 E3SO 20010718001282001071800128CE 2001 7 18 2001F00046 120010430G575165241263 SKIN CESSNA500 550 2076604CE AILERON CRACKED B K NONE O OTHER ININSP/MAINT 1 SW01266217855 5500593 DURING A SCHEDULED PHASE INSPECTION THE LEFT AILERON WAS REMOVED. UPON REMOVAL THE LEADING EDGE SKIN AT THE WEIGHT ATTACHMENT SCREWS WAS FOUND CRACKED. THIS HAD ALLOWED THE SKIN TO CRACK ABOVE AND BELOW A SCREW APPROX. .5000. THE RIGHT AILERON WAS ALSO REMOVED AND TWO OF THESE LEADING EDGE WEIGHT SCREWS WERE ALSO FOUND LOOSE. 1L72 4F A22CE 20010802002612001080200261SO 2001 8 2 2001F00048 120010106G71208401002 MOUNT PIPER PA46 PA46310P 7104605SO ENGINE DAMAGED C K NONE O OTHER ININSP/MAINT 1 GL19251203890 468508097 FOUND ENGINE CONTROL CABLES CHAFFING ON THE ENGINE MOUNT DURING ENGINE CHANGE. DAMAGE WAS FOUND TO BE BEYOND LIMITS. SENT MOUNT FOR REPAIR. ENGINE MOUNT WAS FOUND TO HAVE 6 CRACKS AND CORROSION BEYOND LIMITS . 1L71 3O RTA25SO 20010730003042001073000304SO 2001 7 30 2001F00062 220010202G8520 DRIVE GEAR BEECH 36 A36 1151604CE CONT O520 IO520BA 17032SO ENGINE FAILED A O OTHER O OTHER NRNOT REPORTED 1 CE074456W300 300 E537 122716R ENG HAD STARTER DRIVE FAILURE. INVESTIGATION, STARTER DRIVE HAD BEEN SWITCHED 5 TIMES IN 300 HRS. FOUND OIL GALLEY TO STARTER DRIVE PLUGGED. SPLIT CRANKCASE, FOUND OIL GALLEY FROM REAR CAMSHAFT BRG SURFACE TO STARTER DRIVE BRG PLUGGED. THE PLUG WAS NOT IN PIECES BUT 1 SOLID PIECE OF SILICONE FROM JOURNAL TO STARTER DRIVE BRG. NO OTHER SILICONE WAS FOUND IN ENGINE. SILICONE APPEARS TO HAVE BEEN ACTUALLY INJECTED INTO OIL GALLEY, PRIOR TO ENGINE ASSEMBLY. PREVIOUS OVERHAUL: ENG O/H 8 YEARS(300 HRS) AGO BY LOG BOOK AND STICKER. ALL BEARING SURFACES IN ENG DESTROYED, INCLUDING CRANKCASE AND OIL PUMP. ENG OIL FILTER, SMALL AMT OF ALUMINUM. FOUND LG AMTS OF STEEL IN OIL SUMP FROM FAILED STARTER DRIVE. 1L71 3O3 O 3A15 E5CE 20010716000572001071600057CE 2001 7 16 2001F00063 120010319G331076080241 OVERLAY LEAR 35 31A 5170531CE COCKPIT CRACKED C A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA0370AE 707 188 DURING FLIGHT, PILOT OBSERVED SMOKE COMING FROM THE ENGINE INSTRUMENT PANEL LEFT ITT INDICATOR. PILOT DECLARED EMERGENCY AND LANDED. INVESTIGATION REVEALED THAT THE LIGHTING OVERLAY HAD CRACKED AND WAS ARCING AT THE CRACK. NO ARCING TO THE LOCAL STRUCTURE WAS FOUND. IT WAS DETERMINED THAT THE ENGINE INSTRUMENTS WERE NOT FLUSH WITH THE INSTRUMENT PANEL. ALLOWING A DEFLECTION IN THE OVERLAY. FURTHER INSPECTION FOUND MOST ALL OF THE ENGINE INSTRUMENT MOUNTING BRACKETS TO BE BENT AND BROKEN, POSSIBLY FROM OVER TIGHTENING. 2L72 4F RTA10CE 20010716000582001071600058 2001 7 16 2001F00067 420010419G2562AK450 ELT CESSNA206 U206G 2073356CE TAIL DEFECTIVE C K NONE O OTHER ININSP/MAINT 1 WP072PS 86 U20606916 ELT UNIT WEAK UPON TEST. REMOVED AND REPLACED BATTERIES (OLD WERE MISMATCHED) W/NEW, NO IMPROVEMENT. OUR GOVERNMENT RADIO SHOP CHECKED UNIT. 1) FOUND DISSIMILAR METALS ON SOLDERING JOINTS(IE STEEL/SOLDER) 2) UNIT WAY OFF FREQUENCY. 1H71 3O A4CE 20010717000372001071700037 2001 7 17 2001F00068 420010427G3418SL29849147173 VANE LEAR 25 25B 5170511CE STALL WARNING MALFUNCTIONED D K NONE O OTHER NRNOT REPORTED 1 GL25731CW 117 DOC HOWARD MACH II STC SYSTEM. AFTER A SCHEDULED 300 HOUR INSPECTION, AIRCRAFT WAS TEST FLOWN, FINDING AOA SYSTEM INOPERATIVE. SYSTEM WAS TROUBLESHOT, FOUND TO BE SATISFACTORY ON GROUND. IN FLIGHT AOA REMAIN STEADY, NO STALL WARNING, PUSH/PULLER FUNCTIONING WHILE EXPERIENCING WING AND TAIL BUFFET. SAFETY RECOMMENDATION INITIATED. 2L72 4J A10CE 20010716000602001071600060CE 2001 7 16 2001F00070 120010516G5310241127657 DOOR FRAME LEAR 35 35A 5170602CE FUSELAGE CRACKED D K NONE O OTHER ININSP/MAINT 1 EA17701DA 35A180 DURING ROUTINE INSPECTION FORWARD DOOR JAMB WAS FOUND CRACKS THE WIDTH OF THE DOOR JAMB IN LINE WITH THE HINGE SEAM. FURTHER DISASSEMBLY FOUND ADDITIONAL CRACKS ON THE FORMED STEP RISER, DIRECTLY BELOW THE DOOR JAMB BETWEEN THE JAMB AND THE DOOR SKIN. 2L72 4F A10CE 20010717000392001071700039EU 2001 7 17 2001F00071 120010524G32405713001501 CONTROL HANDLE ISRAEL1124 1124 4500102EU COCKPIT BROKEN D K NONE O OTHER NRNOT REPORTED 1 EA03351C 3000 264 PARKING BRAKE LEVER FELL OFF OF THE BRAKE CONTROL VALVE CAUSING THE PARKING BRAKE PORTION OF THE BRAKE CONTROL VALVE TO SPRING TO THE PARKING BRAKE POSITION LOCKING THE BRAKES. MAKING THE AIRCRAFT UNABLE TO MOVE. 2M72 4F A2SW 20010725006182001072500618EU 2001 7 25 2001F00091 120010601G2930EVP310 VALVE UROCOPEC120 EC120B 8680987EU HYD SERVO DEFECTIVE H O OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP25255SD395 1102 DURING NORMAL RUNUP PROCEDURES, THE HYDRAULICS ARE SWITCHED OFF AS PART OF THE SYSTEM CHECK. UPON ACTIVATING THE HYDRAULIC SWITCH ON THE COLLECTOR THE HYDRAULIC LIGHT ILLUMINATES BUT THE CONTROLS STILL HAD HYDRAULIC BOOST SUPPLIED BY THE ACCUMULATOR. THIS SHOULD NOT HAPPEN. ALL 3 SERVO ELECTROVALVES WERE REPLACED WHICH FIXED THE PROBLEM FOR 5 HOURS, THEN IT MALFUNCTIONED AGAIN. THE HYD POWER PACK WAS REPLACED FOR ANOTHER MAINTENANCE PROBLEM AND THAT ALSO RESOLVED THIS MALFUNCTIONED. 1G72 3U NCR0001RD 20010725006202001072500620EU 2001 7 25 2001F00092 120010601G2930EVP310 VALVE UROCOPEC120 EC120B 8680987EU HYDRAULIC SERVO DEFECTIVE H O OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP25255SD395 1102 DURING NORMAL RUNUP PROCEDURES, THE HYDRAULICS ARE SWITCHED OFF AS PART OF THE SYSTEM CHECK. UPON ACTIVATING THE HYDRAULIC SWITCH ON THE COLLECTOR THE HYD LIGHT ILLUMINATES BUT THE CONTROLS STILL HAD HYDRAULIC BOOST SUPPLIED BY THE ACCUMULATOR. THIS SHOULD NOT HAPPEN. ALL 3 SERVO ELECTROVALVES WERE REPLACED WHICH FIXED THE PROBLEM FOR 5 HOURS, THEN IT MALFUNCTIONED AGAIN THE HYDRAULIC POWER PACK WAS REPLACED FOR ANOTHER MAINTENANCE PROBLEM AND THAT ALSO RESOLVED THIS MALFUNCTION. 1G72 3U NCR0001RD 20010717000402001071700040EU 2001 7 17 2001F00093 120010601G2913EVP310 POWERPACK UROCOPEC120 EC120B 8680987EU HYDRAULIC SYS MALFUNCTIONED C K NONE J WARNING INDICATION TXTAXI/GRND HDL 1 WP25255SD395 1102 DURING NORMAL RUNUP PROCEDURES, THE HYDRAULICS ARE SWITCHED OFF AS PART OF THE SYSTEM CHECK. UPON ACTIVATING THE HYDRAULIC SWITCH ON THE COLLECTOR THE HYDRAULIC LIGHT ILLUMINATES BUT THE CONTROLS STILL HAD HYDRAULIC BOOST SUPPLIED BY THE ACCUMULATOR. THIS SHOULD NOT HAPPEN. ALL 3 SERVO ELECTROVALVES WERE REPLACED WHICH FIXED THE PROBLEM FOR 5 HOURS, THEN IT MALFUNCTIONED AGAIN. THE HYDRAULIC POWER PACK WAS REPLACED FOR ANOTHER MAINTENANCE PROBLEM AND THAT ALSO RESOLVED THIS MALFUNCTION. 1G72 3U NCR0001RD 20010725006222001072500622EU 2001 7 25 2001F00094 120010601G2930GHC1004 POWERPACK UROCOPEC120 EC120B 8680987EU HYD SYSTEM DEFECTIVE H O OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP25255SD400 1102 AFTER STARTING THE HELICOPTER THE CYELIC STICK FELT STIFF AND SLUGGISH WHEN MOVED IN ANY DIRECTION. AFTER RUNNING FOR SEVERAL MINUTES THE CONTROLS FELT BETTER BUT NOT NORMAL AFTER REPLACING THE HYDRAULIC POWER PACK THE PROBLEM WEN AWAY. THE FILTER WAS REMOVED AND WHAT APPEARED TO BE VERY FINE METALLIC PARTICLES WERE PRESENT IN THE HYDRAULIC FLUID. 1G72 3U NCR0001RD 20010802002622001080200262SO 2001 8 2 2001F00097 120010627G32224533307 STRUT PIPER PIPER PA31T PA31T1 7103126SO NLG LOOSE B K NONE O OTHER ININSP/MAINT 1 GL19819SW 31T8104059 INCIDENT HAPPENED DUE TO NOSE GEAR STEERING ARM PN 4438600 ON TOP OF NOSE STRUT HOUSING, BECOMING LOOSE DUE TO ATTACHMENT BOLTS FOR ARM BECOME LOOSE AND SHEARED OFF. AS A RESULT STEERING WAS MINIMAL AND UNCONTROLLABLE ON LANDING. 1L72 3T A8EA 20010727000032001072700003EA 2001 7 27 2001F00104 120010710G6310NAS12254N BOLT SCWZER269 269D 8059501EA DRIVESHAFT LOOSE D R AUTOROTATION IFJFLT. ATTITUDE INST. FLT CONT AFFECTED WARNING INDICATION HOHOVERING 1 SW17296RL 0020 DURING PRACTICE AUTOROTATION, ENGINE POWERSHAFT TO KFLEX POWERTRAIN ADAPTER CAME LOOSE BY BACKING OUT, DURING OPERATION MAIN ROTOR WAS NO LONGER POWERED BY ENGINE. BOLT PIN NAS1225-4N IS A BOLT WITH A SMALL CIRCLE OF PLASTIC ON THREADS FOR LOCKING. EMERGENCY LANDING, NO DAMAGE. 1G71 3U 0 4H12 20010717000412001071700041NE 2001 7 17 2001F00108 220010612G8530116734 CYLINDER DOUG DC3 DC3ASC3G 3021436WP PWA R1830 R1830* 52020NE ENGINE CRACKED G K NONE O OTHER ININSP/MAINT 1 SW1712BA 79 10035 NR 13 CYLINDER BARREL CRACKED ALL THE WAY AROUND WHERE HEAD IS THREADED ONTO BARREL. CRACK BROKE COMPRESSION RINGS RESULTING IN LOSS OF COMPRESSION. 2L72 4R4 R A669 5E4 20010717000422001071700042CE 2001 7 17 2001F00109 120010620G574451155496 BRACKET CESSNA CESSNA402 402C 207590RCE AILERON CRACKED D K NONE O OTHER ININSP/MAINT 1 SW0157PB 402C0300 CRACKED AT AILERON YOLK ATTACH POINTS. 1L72 3O A7CE 20010717000442001071700044CE 2001 7 17 2001F00111 120010625G2510 SPRING AMSAFTYEQUIP CESSNA182 182Q 2072732CE HARNESS BROKEN C K NONE O OTHER NRNOT REPORTED 1 WP234603N2 6262 18267280 AIRCREW SQUAWKED COPILOT INERTIA REEL HARNESS LOCKED UP AND WOULD NOT RELEASE. AMT DETERMINED COIL SPRING WITHIN INERTIA REEL HOUSING HAD BROKEN LOOSE FROM ITS INSTALLED POSITION AND JAMMED THE ROLLER. DATE STAMP FOR THE INERTIA REEL ASSEMBLY WAS 0401(APR 01). BOTH PILOT AND COPILOT INERTIA REELS WERE INSTALLED ON THIS AIRCRAFT 1 JUNE 01. COPILOT HARNESS LOCKED UP ON 7 JUNE O1. ASSEMBLY WAS RETURNED TO MFG FOR REWORK, 21 JUNE 01. 1H71 3O NT3A13 20010801001462001080100146EA 2001 8 1 2001F00113 220010605G852076148 CAMSHAFT PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA ENGINE CHIPPED C K NONE O OTHER ININSP/MAINT 1 AL05555FS1627 317952046 L861561A WHEN REMOVING NR 3 CYLINDER DUE TO LOW COMPRESSION, IT WAS NOTICED THAT THE LOBE ON THE CAMSHAFT FOR THE NR 3 INTAKE WAS CHIPPED. PEELING THE FACE OF THE INTAKE BODY WHICH RIDES ON THE LOBE REVEALED THAT IT ALSO WAS CHIPPED. BOTH OIL AND FILTER WERE CHANGED REGULARLY AT 50 HOURS. OBVIOUSLY ONE OF THE PARTS WAS OR BECAME CHIPPED AND CAUSED THE OTHER TO FAIL. 1L72 3O3 O A20SO E14EA 20010717000462001071700046EA 2001 7 17 2001F00114 220010605G852072877 CAMSHAFT PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA ENGINE CHIPPED C K NONE O OTHER ININSP/MAINT 1 AL05555FS1627 317952046 L861561A WHEN REMOVING NR 3 CYLINDER DUE TO LOW COMPRESSION, IT WAS NOTICED THAT THE LOBE ON THE CAMSHAFT FOR THE NR 3 INTAKE WAS CHIPPED. PEELING THE FACE OF THE INTAKE BODY WHICH RIDES ON THE LOBE REVEALED THAT IT ALSO WAS CHIPPED. BOTH OIL AND FILTER WERE CHANGED REGULARLY AT 50 HOURS. OBVIOUSLY ONE OF THE PARTS WAS OR BECAME CHIPPED AND CAUSED THE OTHER TO FAIL. 1L72 3O3 O A20SO E14EA 20010801001482001080100148NE 2001 8 1 2001F00118 320010702G6110E3932 HUB BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA HARTZLHCE4A HCE4A3I NE BRG RETENTION SCORED B K NONE O OTHER ININSP/MAINT 1 SO1749543104653463 UE181 HJ440 PROPELLER WAS RECEIVED FOR O/H WITH EXCESSIVE GREASE LEAKAGE FROM ALL BLADES. PROP WAS DISASSEMBLED TO START O/H PROCESS. WHEN HUB UNIT WAS SPLIT, THERE WAS EXCESSIVE AMOUNTS OF GREASE INSIDE. UPON FURTHER INSPECTION, THE BEARING RACE HAD SHATTERED INTO SEVERAL PIECES, SCORING THE INSIDE RETENTION AREA. REWORK WAS BEYOND ALLOWABLE LIMITS. HUB WAS RETIRED FROM SERVICE. 2L72 4T3 TRTA24CE E2NE 5 CP10NE 20010808003172001080800317CE 2001 8 8 2001F00164 120010622G2120973800011 DUCT BEECH 100 B100 1152919CE GARRTTTPE331TPE331* 01514WP CABIN PRESSURE FAILED G K NONE O OTHER ININSP/MAINT 1 EA2178DA BE11 WHILE TROUBLESHOOTING POOR CABIN PRESSURIZATION, FOUND FAILED HOSE IN LEFT ENGINE AIR SUPPLY LINE TO CABIN. THIS CAUSED PRESSURIZATION TO WORK POORLY, BECAUSE THERE WAS NO INPUT TO CABIN FROM LEFT FLOW PACK. SUSPECT DUCT FAILED DUE TO AGE. 1L72 4T3 T A14CE E2WE 20010810001542001081000154CE 2001 8 10 2001F00165 120010627G322235825174 ARM BEECH 95 95 1153402CE NLG CRACKED G O OTHER O OTHER TXTAXI/GRND HDL 1 SO09 DURING A RECENT INVESTIGATION OF AN INCIDENT OF A BEECH 95 THAT THE NOSE GEAR COLLAPSED ON ROLL OUT AFTER LANDING. IT WAS DISCOVERED THAT THE LANDING GEAR CRANK ARM PART NUMBER 35-825174 THAT ATTACHES TO THE LANDING GEAR TRANSMISSION BOX HAD CRACKED. THE CRACKED ARM ALLOWED THE ARM TO FLEX ADN ROTATE ON THE SPLINES OF THE TRANSMISSION SHAFT WHICH KEEPS THE PUSH PULL TUBE TO THE NOSE GEAR IN THE FORWARD POSITION. THIS ARM IS ALSO INSTALLED ON SEVERAL MODELS. PROBABLE CAUSE IS FATIGUE. RECOMMEND THAT ARM BE REMOVED AT THE NEXT INSPECTION AND INSPECTED WITH 10X MAGNIFIER. (ATTACHED PHOTOS) 1L72 3O 3A16 20010822002692001082200269SW 2001 8 22 2001F00205 120010712G5711 SPAR BBAVIA7 7AC 2110102SW CONT A65 A65* 17003SO WING CRACKED D K NONE O OTHER ININSP/MAINT 1 NM0183233 7AC1897 SPAR CRACKED 1H71 3O3 O A759 E205 20010905000472001090500047 2001 9 5 2001F00248 420010716G3418S16729 DETECTOR CESSNA182 182R 2072731CE CONT O470 O470* 17026SO WING INOPERATIVE D O OTHER O OTHER NRNOT REPORTED 1 EA2135VA 18268129 UPON INSTALLING NEW LIFT DETECTION NOTED THAT WHEN WIRED AS ORIGINALLY REMOVED FROM AIRCRAFT, WITH HEAT TURNED ON, DETECTION WAS INOPERATIVE. GROUND FOR HEATER WAS INSTALLED ON COMMON FOR DETECTION; CAUSING A NO POTENTIAL WHEN HEATER TURNED ON. 1L71 3O3 ONT3A13 E273 20010801001492001080100149WP 2001 8 1 2001FA0000001 220010515G85208976021 CAM CESSNA441 441 2076020CE GARRTTTPE331TPE331* 01514WP ENGINE MISMANUFACTURED B WTXRK NONE O OTHER ININSP/MAINT 1 NM074441T 4410133 AFTER INSTALLING NEWLY OVERHAULED ENGINE ON AIRCRAFT, FOUND THAT THE -30 P.P.C. COULD NOT BE RIGGED. REMOVED P.O.C. AND FOUND THAT THE CAM INSIDE, ALTHOUGH MARKED CORRECTLY (P/N 897602-1), THE CAM WAS MANUFACTURED WRONG. IT HAS THE WRONG CAM PROFILE. REF: SB TPE331-72-0904. 1L72 3T3 TRTA28CE E2WE 20010801001502001080100150WP 2001 8 1 2001FA0000002 220010514G85208976021 CAM CESSNA441 441 2076020CE GARRTTTPE331TPE331* 01514WP ENGINE MISMANUFACTURED B WTXRK NONE O OTHER ININSP/MAINT 1 NM074441T 4410133 P77443C AFTER INSTALLING NEWLY OVERHAULED ENGINE ON AIRCRAFT, FOUND THAT THE -30 P.P.C. COULD NOT BE RIGGED. REMOVED THE P.P.C. AND FOUND THAT THE CAM INSIDE, ALTHOUGH MARKED WITH THE CORRECT P/N (8976021) WAS MANUFACTURED WRONG. IT HAS THE WRONG CAM PROFILE. REF: SB TPE331-72-0904. 1L72 3T3 TRTA28CE E2WE 20010718000062001071800006NM 2001 7 18 2001FA0000003 120010501G324426107012 TIRE DORNERDO32 DO328100 2996000NM RT MLG DEFLATED C K NONE O OTHER ININSP/MAINT 1 SO11404SS 40 3090 DURING WALKAROUND INSPECTION AFTER LANDING IN KBHM, CREW DISCOVERED ROB MAIN LANDING GEAR TIRE WAS FLAT. THE WHEEL O-RING WAS FOUND PROTRUDING TOWARDS THE CENTER OF THE WHEEL. EIGHT OF THE TEN WHEEL THROUGH BOLTS WERE LOOSE. THE WHEEL WAS RETURNED TO THE OVERHAULER FOR EVALUATION AND OVERHAUL. 2H72 4T RTA45NM 20010724000032001072400003EU 2001 7 24 2001FA0000008 120010521G5540 RIVET ISRAEL1124 1124 4500102EU RUDDER CRACKED D K NONE O OTHER ININSP/MAINT 1 SW99980S 1 401 CRACKS IN DIMPLES OF RIVETS ON SKIN OF RUDDER, LOOKS LIKE THEY HAVE BEEN THERE SINCE MANUFACTURE. FABRICATING NEW RIBS PER GALAXY AEROSPACE DRAWINGS AND DOING A SPAR SPLICE PER GALAXY. SUSPECT ALL RUDDERS THAT ARE MANUFACTURED THE SAME AS THIS ONE ARE ALSO CRACKED. 2M72 4F A2SW 20010718000072001071800007EU 2001 7 18 2001FA0000009 120010518G5330 SKIN AMD FALC50FALCON50MYST2730106EU FUSELAGE CORRODED G BQVAK NONE O OTHER ININSP/MAINT 1 EA0150TG 6133 117 CORROSION IN AREA OF AFT FUSELAGE SKINS AT ACU EXHAUST OUTLETS. WATER ENTRAPMENT. REPAIRED UNDER BOMBARDIER REO NR 601-53-30-278. 2L73 4F A46EU 20010801001512001080100151NM 2001 8 1 2001FA0000012 120010521G3230108510 HOUSING BOEING727 727 UTILSYSNM AFT MOUNT BROKEN B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 HOUSING HAS A BROKEN AFT MOUNT. PROBABLE CAUSE: MISHANDLED 2L73 4J RTA3WE 20010801001522001080100152NM 2001 8 1 2001FA0000013 120010521G2730401606223 HOUSING MOOG BOEING727 727* NM SEAL PLATE SURFCCRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 1601D HOUSING ASSEMBLY IS CRACKED ON THE SEAL PLATE SURFACE. PROBABLE CAUSE: HOUSING ASSEMBLY IS MADE FROM MAGNESIUM ALLOY AND IS EXTREMELY SUSCEPTIBLE TO DISSIMILAR METAL CORROSION AND CRACKS. 2L73 4F RTA3WE 20010801001532001080100153NM 2001 8 1 2001FA0000014 120010518G2730401611572 BARREL MOOG BOEING727 727* NM BARRELL BORE CORRODED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 1098 BARREL ASSEMBLY HAS PITTING AND EROSION IN MAIN BORE. PROBABLE CAUSE: DISSIMILAR CORROSION. 2L73 4F RTA3WE 20010801001542001080100154NM 2001 8 1 2001FA0000015 120010518G2730401644557 HOUSING MOOG BOEING727 727* NM SEAL SURF, HOLESCORRODED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 1098 HOUSING ASSEMBLY HAS PITTING AND CORROSION IN BOLT HOLES, CAP ASSEMBLIES, PORTS AND SEALING SURFACES. PROBABLE CAUSE: DISSIMILAR CORROSION. RECOMMENDATIONS: REPLACE MAGNESIUM HOUSING ASSEMBLIES WITH ALUMINUM ALLOY. 2L73 4F RTA3WE 20010801001552001080100155NM 2001 8 1 2001FA0000016 120010518G2730401611572 HOUSING MOOG BOEING727 727 UTILSYSNM CK VLV PORT, LANCORRODED B IU6RK NONE O OTHER ININSP/MAINT 1 NM07 1098 ELBOW HOUSING HAS SEVERE CORROSION IN BOLT HOLES, CHEDK VALVE PORT, PACKING LANDS AND ON SEALING SURFACE FACE. PROBABLE CAUSE: DISSIMILAR CORROSION. RECOMMENDATIONS: REPLACE MAGNESIUM ELBOW WITH ALUMINUM ALLOY. 2L73 4J RTA3WE 20010801001562001080100156EA 2001 8 1 2001FA0000017 220010516G8520LW19332 CONNECTING ROD PIPER PA32 PA32300 7103212SO LYC O540 IO540K1A5 41532EA NR 2 CYLINDER FAILED D K NONE O OTHER ININSP/MAINT 1 NM025640M 3240295 L1774848A NR 2 PISTON WAS REMOVED, CONNECTING ROD BUSHING WAS FOUND TO HAVE MOVED TO THE POSITION AS SHOWN IN PHOTO AND ONLY STOPPED BY CONTACTING THE INSIDE OF PISTON PIN BOSS OF THE PISTON. BUSHING SHOWED EVIDENCE OF MOVING TORSIONALLY FROM PROPER POSITION IN REF. TO SPLIT LINE BUT DID NOT SHOW AMOUNT OF WEAR ON OD, NOT TURNING IN THE ROD AS CONTINUOUS CONDITION. SLIGHT DISCOLORATION OF PORTION OF BUSHING EXTENDING BEYOND ROD BOSS INDICATING IT HAD BEEN IN THIS POSITION FOR SOME HOURS. NO EVIDENCE OF DAMAGE TO PISTON BOSS OR PISTON PIN OD AND BUSHING ID. WHEN BUSHING WAS REMOVED FROM ROD, IT FRACTURED AS IN PHOTO. CORRESPONDING FRET LINE ON ROD BOSS ID AT POINT OF BUSHING FRACTURE. (ATTACHED PHOTO) 1L71 3O3 O A3SO 1E4 20010725006252001072500625NM 2001 7 25 2001FA0000018 120010518G6310A1902 BELT ROBSINR22 R22BETAII 7640110NM ROTOR DRIVE MALFUNCTIONED D O OTHER O OTHER NRNOT REPORTED 1 SW177087X488 2829 V-BELT, (PN A190-2) OF THE R22 DRIVE SYSTEM, MALFUNCTIONED BY COMING APART AND JUMPED OFF DRIVE PULLEYS, CAUSING LOSS OF DRIVE TO ROTOR DRIVE SYSTEM. 1G71 3O H10WE 20010801001572001080100157SW 2001 8 1 2001FA0000019 120010601G5711 SPAR BBAVIA7 7CCM 21101MWSW WING SPAR CRACKED D K NONE O OTHER ININSP/MAINT 1 GL152762E 7AC6345 CRACK ON BOTTOM SURFACE OF SPAR, LEFT SIDE REAR. (BUTT) FOUND PRIOR TO CRACK INSPECTION AS PER AD OWNER DISCONTINUED ANNUAL INSPECTION PRIOR TO FULL INSPECTION. 1H71 3O A759 20010801001582001080100158SW 2001 8 1 2001FA0000020 120010607G5720 STRUT BBAVIA7 7CCM 21101MWSW WING STRUT DEFECTIVE D K NONE O OTHER ININSP/MAINT 1 GL152762E 7AC6345 WING STRUTS HAD FILLED WITH WATER FROM SITTING OUTSIDE. RUST STAINS VISIBLE FROM OUTSIDE OF STUT. WHEN POKED WITH AIR AWL IT PUSHED A HOLE INTO STRUT AND DRAINED WATER. DRILLED A .0312 HOLE IN BOTTOM OF OTHER 3 STRUTS AND WATER CAME OUT IN EXCESS OF 1 CUP EACH. OWNER NOTIFIED OF UNAIRWORTHY CONDITION. 1H71 3O A759 20010801001592001080100159EA 2001 8 1 2001FA0000021 220010524G8530AEL6510212 CYLINDER PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA CYLINDER HEAD CRACKED B MW2RK NONE O OTHER ININSP/MAINT 1 GL174350G1379 288490058 CRACKED FROM SPARK PLUG HOLE TO EX SEAT. 1L71 3O3 O 2A13 E286 20010801001602001080100160EA 2001 8 1 2001FA0000022 220010524G8530AEL6510241 CYLINDER PIPER PA28 PA28161 7102803SO LYC O360 O360A4M 41514EA ENGINE CRACKED B MW2RK NONE O OTHER ININSP/MAINT 1 GL172366W823 288516046 CRACKED FROM TOP OF SPARK PLUG HOLE, AROUND OUTSIDE OF EX SEAT TO BOTTOM OF SPARK PLUG HOLE. 1L71 3O3 O 2A13 E286 20010801001612001080100161CE 2001 8 1 2001FA0000023 120010530G3213S3461111 BOLT CESSNA172 172S 2072439CE LEFT STRUT MISINSTALLED B K NONE O OTHER ININSP/MAINT 1 CE07784SP 172S8711 BOLTS ARE INSTALLED BACKWARDS, POINTING FORWARD. 1H71 3O NT3A12 20010801001622001080100162CE 2001 8 1 2001FA0000024 120010530G3213S3461116 BOLT CESSNA172 172S 2072439CE RIGHT STRUT MISINSTALLED B K NONE O OTHER ININSP/MAINT 1 CE07784SP 172S8711 BOLTS ARE INSTALLED BACKWARDS, POINTING FORWARD. 1H71 3O NT3A12 20010801001632001080100163CE 2001 8 1 2001FA0000025 120010530G5753AN311A BOLT CESSNA172 172S 2072439CE RT FLAP MISINSTALLED B K NONE O OTHER ININSP/MAINT 1 CE07784SP 172S8711 BOLTS ARE INSTALLED BACKWARDS, POINTING OUTBOARD. 1H71 3O NT3A12 20010801001642001080100164EA 2001 8 1 2001FA0000027 220010429G8500AN657A BOLT LYC O320 O320E2A 41508EA PROPELLER LOOSE C O OTHER O OTHER NRNOT REPORTED 1 GL1526RK 124 L2383927A PROPELLER BOLTS (AN6-57A) BROKE IN FLIGHT AT CRUISE POWER (2500 RPM) AT 7500 FT. MSL. NOTICED THAT ONE BOLT WAS MISSING AND THE NUT ON ANOTHER COULD BE REMOVED BY HAND. POSSIBLE THAT TWO NUTS, (MS 20365-624) LOOSENED CAUSING VIBRATION IN PROPELLER WHICH CAUSED BOLT FAILURE . NOTE: THAT ONLY THE TWO NUTS THAT SEEMED TO BE LOOSE, WERE REPLACED 124 HOURS BEFORE FAILURE. ALL OTHER NUTS WERE STILL INTACT. PROPELLER SEPARATED FROM ENGINE IN FLIGHT. 3 O E274 20010801001652001080100165CE 2001 8 1 2001FA0000028 120010601G5320365550483 GUARD BEECH 36 A36 1151604CE PULLEY CRACKED C WC7RK NONE O OTHER ININSP/MAINT 1 GL153243B100 E3243 THIS IS THE SECOND OCCURENCE OF THE PULLEY GUARD CRACKING. THE AIRCRAFT TOTAL TIME 703.1. ON THE FIRST OCCURENCE THE GUARD HAD A LARGE CRACK AND A PIECE MISSING. THIS OCCURENCE THE ENTIRE GUARD WAS FOUND MISSING. 1L71 3O 3A15 20010801001662001080100166EA 2001 8 1 2001FA0000030 220010524G8550LW1568B TUBE CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA OIL SUMP LOOSE B K NONE O OTHER ININSP/MAINT 1 SO134596P2000 15284776 INDUCTION TUBE ATTACHED TO OIL SUMP BECAME LOOSE CAUSING ROUGH RUNNING ENGINE. ENGINE OIL SUMP REPLACED TO CORRECT PROBLEM. 1H71 3O3 ONT3A19 E223 20010801001672001080100167EA 2001 8 1 2001FA0000031 220010605G8530AEL74230P010 GUIDE LYC O360 O360F1A6 41514EA EXHAUST OUT OF TOLERANCEH K NONE O OTHER ININSP/MAINT 1 EA17 L2915236A CYLINDER HAD LOW COMPRESSION READINGS, 20/80. CYLINDER WAS REMOVED FROM ENGINE AND INSPECTED. EX. GUIDE WAS INSPECTED AND FOUND TO BE OUT OF SERVICE LIMITS. EX GUIDE ID WAS MEASURED, AND A READING OF .5325 WAS TAKEN. MAX SERVICE DIMENSION FOR A 300 HR CYLINDER EX GUIDE ID IS .5015/.5025 PER LYCOMING O/H MANUAL 60294-7-8. THIS CYLINDER HAD 236 HOURS SINCE OVERHAUL. 3 O E286 20010718000082001071800008SO 2001 7 18 2001FA0000035 120010620G57121159WM4007415G RIB GIV GULSTMG1159 GIV 3980115SO LT WING CRACKED B K NONE O OTHER ININSP/MAINT 1 SO11460QS2298 2298 1360 1360 WHILE DOING A SCHEDULE VISUAL INSPECTION OF THE WING IT WAS NOTED A CRACK WAS IN RIB WEB. THE RIB IS LOCATED NEXT TO THE LAST OUTBOARD LEFT WING. CRACK IS 7 INCH LONG ALONG THE THE BOTTOM SIDE THEN TURNS UP AT BOTH ENDS FOR 1 INCH. REMOVED AND REPLACED WITH NEW RIB. 2L72 4F RTA12EA 20010801001692001080100169EA 2001 8 1 2001FA0000041 220010524G8550LW15688 SUMP CESSNA150 152 2071835CE LYC O235 O235* 41505EA SUMP ASSY, OIL FAILED B K NONE O OTHER ININSP/MAINT 1 SO134596P 15284776 INDUCTION TUBE ATTACHED TO OIL SUMP BECAME LOOSE CAUSING ROUGH RUNNING ENGINE. ENGINE OIL SUMP REPLACED TO CORRECT PROBLEM. 1H71 3O3 ONT3A19 E223 20010801001702001080100170CE 2001 8 1 2001FA0000042 120010601G575312210107 FLAP TRACK CESSNA206 TU206G 2073357CE WING LOOSE B K NONE O OTHER ININSP/MAINT 1 GL159851Z U20606701 THE LEFT HAND INBOARD FLAP TRACK IS WORKING LOOSE. THIS WAS INDICATED BY CRACKED COVE SKIN ATTACH BRACKETS. 1H71 3O A4CE 20010801001712001080100171SO 2001 8 1 2001FA0000043 120010525G711123810000 ALT AIR DOOR PIPER PA30 PA30 7103002SO RIGHT ENGINE LOOSE D C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL038379Y 301534 ON TAKEOFF ROLL, THE RIGHT ENGINE WOULD NOT DEVELOP FULL POWER. UPON FUTURE INVESTIGATION FOUND THE ALT AIR DOOR CAME LOOSE AND WAS BLOCKING THE EJECTOR INTAKE. UPON FINDING THIS WE INSPECTED THE LEFT ALT AIR BOX AND FOUND THE ALT AIR DOOR LAYING IN THE COWLING. 1L72 3O A1EA 20010801001732001080100173GL 2001 8 1 2001FA0000044 120010424G32305533525 PIN NAMER T6 SNJ4 6400414GL MLG WORN G K NONE O OTHER ININSP/MAINT 1 GL157083C2290 881447 BINDING OF PIN WOULD NOT ALLOW LEFT MAIN GEAR TO LOCK DOWN, CAUSING GEAR TO COLLAPSE ON LANDING. UPON INSPECTION, PIN DOES NOT APPEAR WORN. MANUAL DOES NOT CALL OUT FOR LUBING PIN. A SLIGHT OIL FILM ON PIN MAKES IT LOCK NORMAL. 1L71 3R A2575 20010801001742001080100174SO 2001 8 1 2001FA0000045 120010606G55406342004 RUDDER BAR PIPER PA32 PA32260 7103206SO RUDDER CRACKED D K NONE O OTHER ININSP/MAINT 1 AL014803S11045 321188 DURING 100 HOUR INSPECTION, FOUND LEFT RUDDER BAR CRACKED AT WELD WHERE STRAIGHT TUBE CONNECTS TO CARRY OVER TUBE. SPECULATE AGE AND USAGE CAUSED CRACK.. THIS COMPONENT HAS BEEN FOUND CRACKED SEVERAL TIMES IN THE PAST ON OTHER SIMILAR AIRCRAFT. LATER MODEL AIRCRAFT HAVE A REINFORCEMENT PLATE WELDED ON THIS AREA BY THE FACTORY. 1L71 3O A3SO 20010802002642001080200264CE 2001 8 2 2001FA0000046 120010615G61208976021 CAM CESSNA441 441 2076020CE GARRTTTPE331TPE331* 01514WP PITCH CONTROL MISMANUFACTURED B WTXRK NONE O OTHER ININSP/MAINT 1 NM07 P143091 RECEIVED A NEWLY OVERHAULED P.P.C. FROM MANUFACTURER, WAS UNABLE TO RIG. FOUND P.P.C. CAM HAD THE RIGHT PN BUT THE WRONG CAM PROFILE MANUFACTURE IN IT. REF: SB TPE331-72-0904. 1L72 3T3 TRTA28CE E2WE 20010801001762001080100176SO 2001 8 1 2001FA0000047 120010505G7810 EXHAUST PIPE PIPER PA18 PA18150 7101828SO ENGINE CRACKED D K NONE O OTHER ININSP/MAINT 1 GL034136E538 187809082 FOUND WELD ON WYE PIPE CRACKED AT ANNUAL INSPECTION. (NO PARTS AVAILABLE AT THIS TIME) ALSO FOUND INNER BAFFLE ON SAME PIPE CRACKED. 1H71 3O 1A2 20010801001772001080100177 2001 8 1 2001FA0000048 420010519G2320CI248 ANTENNA CESSNA182 T182 2072736CE VHF ANTENNA BROKEN D K NONE O OTHER ININSP/MAINT 1 GL193525R 18280977 AIRCRAFT FLEW IN WITH BOTH VHF COMM ANTENNA BROKEN. AIRCRAFT TOTAL TIME WAS 5 HOURS. PROBABLE CAUSE NOT KNOWN. 1L71 3O 3A13 20010801001782001080100178 2001 8 1 2001FA0000049 420010519G2320CI248 ANTENNA CESSNA182 T182 2072736CE VHF ANTENNA BROKEN D K NONE O OTHER ININSP/MAINT 1 GL193525R5 18280977 AIRCRAFT FLEW IN WITH BOTH ANTENNA BROKEN. AIRCRAFT TOTAL TIME WAS 5 HOURS. PROBABLE CAUSE NOT KNOWN. 1L71 3O 3A13 20010801001792001080100179CE 2001 8 1 2001FA0000052 120010606G55109664000093 PLATE BEECH 80 65B80 1152812CE RUDDER CORRODED C K NONE O OTHER ININSP/MAINT 1 EA2119CR 3278 LD372 DURING ANNUAL INSPECTION, UPPER AND MID RUDDER ATTACH FITTING PLATES (THESE CONTAIN THE BEARINGS) WERE FOUND TO BE SEVERELY EXFOLIATED. THE UPPER RUDDER ATTACH PLATE EXFOLIATED TO THE POINT THAT THE ATTACH POINT HAD FAILED. THE RUDDER COULD BE MOVED APPROXIMATELY SIX INCHES OUT OF ITS PLANE OF ROTATION DUE TO THE UPPER ATTACH POINT FAILURE. SUSPECT THAT INSUFFICIENT OR INFREQUENT INSPECTION OF THE AERA ALLOWED THE CORROSION TO PROGRESS TO THE EXTENT OF ATTACH POINT FAILURE. 1L72 3O 3A20 20010718000092001071800009SO 2001 7 18 2001FA0000053 120010622G325074381 SWIVEL GULSTMGV GULFSTREAMGV3980116SO NLG RUPTURED B O OTHER K FLUID LOSS APAPPROACH 1 WP051540 520 580 NOSE WHEEL STEERING SWIVEL, (AT NOSE LANDING GEAR ASSY) RUPTURED, DEPLETING THE LEFT HYDRAULIC RESERVOIR. NOTE: THIS RESERVOIR PROVIDES HYDRAULIC POWER TO THE FLAPS, LEFT THRUST REVERSER AND THE BRAKES. 2L72 4F RTA12EA 20010802002662001080200266SO 2001 8 2 2001FA0000055 120010605G273042901002 TUBE PIPER PA31 PA31350 7103110SO ELEVATOR CONTROLELONGATED B R2JRK NONE O OTHER ININSP/MAINT 1 EA2113FS 3692 318352024 WHILE C/W UNDER PANEL ITEMS ON ANNUAL CHECKLIST, FOUND ARM ON THE ELEVATOR CONTROL TUBE VERY LOOSE. DISASSEMBLY SHOWED HOLE WHERE ARM MOUNTS TO TUBE VERY ELONGATED. PART REPLACED WITH NEW PART. SUGGEST PHYSICALLY CHECKING EACH ARM FOR UNWANTED MOVEMENT WHEN DOING INSPECTION, NOT JUST VISUAL INSPECTION. 1L72 3O A20SO 20010802002672001080200267CE 2001 8 2 2001FA0000056 120010613G323312815041 ACTUATOR CESSNA177 177RG 2073709CE MLG FAILED D A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW9934072 177RG0960 DURING CRUISE FLIGHT PILOT REPORTED BUFFET AND LOSS OF GEAR UP INDICATION. PILOT SLOWED TO GEAR SPEED AND DESENDED TO VFR CONDITIONS AND RETURNED TO DEPARTURE AIRPORT. SELECTED GEAR DOWN AND COULD NOT GET GEAR DOWN INDICATION. EMERGENCY EXTENDED GEAR AND OBTAINED A GEAR DOWN INDICATION. UNEVENTFUL LANDING. ON INSPECTION FOUND THE LEFT MAIN GEAR DOWN LOCK ACTUATOR #1281504-1 HAD RUPTURED END SHAFT SEAL AND MOST OF HYDRAULIC FLUID HAD LEAKED FROM SYSTEM. DISSASEMBELED AND FOUND NO DEFECTS EXCEPT FAILED SEAL.REPLACED SEAL AND FUNTION TEST OK. 1H71 3O A20CE 20010801001802001080100180CE 2001 8 1 2001FA0000057 120010606G53209542001549 CHANNEL BEECH 35 V35A 1151544CE FUSELAGE CORRODED B K NONE O OTHER ININSP/MAINT 1 NE058359N D8753 UPON REMOVAL OF THE LARGE FLOORBOARD AFT OF THE SPAR, IT WAS NOTED THAT THE TEW MIDDLE/CENTER CHANNEL ASSEMBLIES WERE CORRODED. THE CORROSION WAS SO BAD THAT A TWO INCH AREA AND ONE INCH AREA ON THE OTHER THAT PROVIDES THE MOUNTING FOR THE SEAT RAILS WAS MISSING. THE CAUSE OF THE CORROSION BELIEVED TO BE DISIMILAR METAL CORRIOSION FROM THE SCREWS. LOOKED AT ALL THE OTHER SCREWS THAT SECURE THE CHANNELS AND STIFFENERS AND THEY WERE JUST STARTING TO CORRODE, SO THEY ALL GOT REPLACED. 1L71 3O 3A15 20010801001822001080100182GL 2001 8 1 2001FA0000058 120010327G321335017502 STRUT AVIAT A1 A1B GL MLG FAILED D K NONE O OTHER ININSP/MAINT 1 NE05484C 2114 LANDING GEAR STRUT FAILED AT WELD DUE TO COMPLETE LACK OF WELD PENETRATION. LANDING GEAR SEPARATED FROM AIRCRAFT AT LANDING. DUE TO WELD FAILURE. 1H71 3O NCA22NM 20010801001832001080100183SO 2001 8 1 2001FA0000059 120010616G32132468105 STRUT PIPER PA30 PA30 7103002SO RT MLG CRACKED D K NONE O OTHER ININSP/MAINT 1 SO088418Y7891 301570 RIGHT SIDE MAIN LANDING GEAR UPPER HOUSING CRACKED FROM BOLT HOLE WHERE BROKE LINE ATTACHES INTO THE INNER MOST AREA OF THE STRUT 1 INCH LONG ON EACH SIDE. LEAKING FLUID. POTENTIAL COMPLETE SEPARATION OF GEAR LEG. 1L72 3O A1EA 20010801001862001080100186SW 2001 8 1 2001FA0000060 120010611G2460 HARNESS MOONEYM20 M20K 5870220SW FUSELAGE CHAFED B K NONE O OTHER ININSP/MAINT 1 EA23252YC 251074 WHEN REPAIRING AVIONICS POWER SYSTEM, CB PANEL PULLED LOOSE AND OUT FOR MAINTENANCE. DISCREPANCY NOTED: FUSELAGE UNDER WINDSHIELD CHAFING POWER CABLES TO CB S AND RELAYS. NO CHAFE STRIP NOTED IN THIS AREA BEHIND CB PANEL AND CHAFING EVIDENCE ON LARGE POWER WIRES. GLARESHIELD REMOVAL TO INSPECT. PROBLEM NOT RELATED TO AVIONICS PROBLEM THAT WAS REPAIRED. 1L71 3O 2A3 20010801001872001080100187CE 2001 8 1 2001FA0000061 120010611G3210084212219 LINK CESSNA404 404 2075901CE LINK ASSY DRAG BENT D K NONE O OTHER ININSP/MAINT 1 SW01165SA 4040622 LINK ASSEMBLY DRAG. PN 0842122-19 1L72 3O RTA25CE 20010801001882001080100188CE 2001 8 1 2001FA0000062 120010611G2710581510326CR CONTROL CABLE CESSNA404 404 2075901CE LT AFT AILERON INOPERATIVE D K NONE O OTHER ININSP/MAINT 1 SW01165SA 4040622 LEFT HAND AFT AILERON CABLE. PN 5815103-26CR ( BLENDED ) 1L72 3O RTA25CE 20010801002012001080100201EA 2001 8 1 2001FA0000063 220010516G855006B23072 GASKET CESSNA172 172N 2072434CE LYC O320 O320* 41508EA OIL FILTER FAILED D K NONE O OTHER ININSP/MAINT 1 WP19737TC 17269654 AD2000-18-23 WAS C/W BY INSTALLING NEW GASKET PT NR 06B23072 UNDER 34 HOURS, GASKET BLEW OUT AND ALL THE OIL WAS BLOWN OUT. AIRCRAFT RETURNED TO AIRPORT SAFELY. INSPECTION OF GASKET REVELED THAT THE RUBBER GASKET HAD DESOLVED AND BECAME VERY SOFT. A NEW GASKET WAS INSTALLED AS PER INSTRUCTIONS IN THE SB. NO FURTHER PROBLEMS HAVE BEEN ENCOUNTERED WITH THIS AIRCRAFT. 1H71 3O3 ONT3A12 E274 20010801002022001080100202CE 2001 8 1 2001FA0000064 120010614G2730123460020 ELEVATOR CESSNA182 182S 2072701CE RT SIDE ELEVATORWEAK D K NONE O OTHER ININSP/MAINT 1 EA25132ME276 18280690 WHILE PERFORMING AN ANNUAL INSPECTION ON THIS AIRCRAFT, SEVERAL WRINKLES AND LOOSE RIVETS WERE DISCOVERED ON BOTH ELEVATORS ALONG WHERE THE BALANCE TAB ATTACHES TO THE ELEVATOR SPAR. THE STRUCTURE AROUND THIS AREA APPEARED VERY WEAK AND FLEXIBLE. CESSNA WAS CONTACTED FOR TECHNICAL ASSISTANCE. AT CESSNAS REQUEST, NEW REPLACEMENT ELEVATORS WERE INSTALLED, AND THE OLD ONES WERE RETURNED FOR AN ENGINEERING EVALUATION. ALL INSPECTORS ARE URGED TO VIGILANT FOR SUCH CONDITION ON OTHER AIRCRAFT OF THIS TYPE. 1H71 3O NT3A13 20010801002032001080100203NE 2001 8 1 2001FA0000066 120010515G554027103 PUSHROD CONAERLA4 LA4200 5110310NE AFT FUSELAGE CORRODED B K NONE O OTHER ININSP/MAINT 1 EA23911CY2194 532 REMOVED FORWARD LOWER ROD END FROM RUDDER PUSHROD ASSEMBLY, DUE TO VISIBLE CORROSION. FOUND EXTENSIVE CORROSION INTERNALLY ON ARM AND ROD ASSEMBLY. 1H71 3O 1A13 20010801002042001080100204CE 2001 8 1 2001FA0000067 120010503G322235825174 ARM BEECH 95 95 1153402CE NLG CRACKED G K NONE O OTHER ININSP/MAINT 1 SO092765Y TD136 UPON LANDING ROLL-OUT THE NOSE GEAR COLLAPSED. THE CRACK ON THE SPLINE PORTION OF ARM CAUSED THE ARM TO FLEX AND OPEN CAUSING MATING GEARS TO SEPARATE AND THE NOSE GEAR TO COLLAPSE. PROBABLE CAUSE IS FATIGUE. REOCCURRING INSPECTIONS ARE RECOMMENDED. 1L72 3O 3A16 20010718000102001071800010CE 2001 7 18 2001FA0000068 120010702G793030702464 INDICATOR RKWELLNA265 NA26565 7630107CE GARRTTTFE731TFE7313R1D 01518WP RT ENGINE DEFECTIVE B K NONE N FALSE WARNING ININSP/MAINT 1 CE0182CR 4950 46549 P83263 IN PROCESS OF PRE-FLIGHT INSPECTION NOTICED RIGHT ENGINE OIL FILTER BY-PASS INDICATOR PIN HAD POPPED. INSPECTED OIL FILTER AND TOOK SOAP SAMPLE (NEW OIL FILTER INSTALLED). AFTER TEST RUN AND LEAK CHECK, NOTICED PIN PARTIALLY POPPED AGAIN. REMOVED BY-PASS INDICATOR ASSEMBLY AND NOTICED MINIMAL RESISTANCE FOR PIN EXTENSION. REPLACED ASSEMBLY WITH NEW UNIT. DEFECTIVE UNIT HAS ASSEMBLY DATE OF 3Q/87. ADDITIONALLY THE FOLLOWING NUMBERS APPEAR ON ASSEMBLY:99193SOCN307246-4 N AND MFR 05228-7579668. 2L72 4J4 F A2WE E6WE 20010801002052001080100205CE 2001 8 1 2001FA0000069 120010614G273012346001 ELEVATOR CESSNA182 182S 2072701CE LT SIDE ELEVATORWEAK D K NONE O OTHER ININSP/MAINT 1 EA25132ME 18280690 WHILE PERFORMING AN ANNUAL INSPECTION ON THIS AIRCRAFT, SEVERAL WRINKLES AND LOOSE RIVETS WERE DISCOVERED ON BOTH ELEVATORS ALONG WHERE THE BALANCE TAB ATTACHES TO THE ELEVATOR SPAR. THE STRUCTURE AROUND THIS AREA APPEARED VERY WEAK AND FLEXIBLE. CESSNA WAS CONTACTED FOR TECHNICAL ASSISTANCE. AT CESSNAS REQUEST, NEW REPLACEMENT ELEVATORS WERE INSTALLED, AND THE OLD ONES WERE RETURNED FOR AN ENGINEERING EVALUATION. ALL INSPECTORS ARE URGED TO BE VIGILANT FOR SUCH CONDITION ON OTHER AIRCRAFT OF THIS TYPE. 1H71 3O NT3A13 20010801002072001080100207GL 2001 8 1 2001FA0000072 320010703G6110 SHAFT CESSNA421 421C 2076016CE CONT O520 GTSIO520H 17032SO MCAULY3AF34C3AF34C92 GL PROPELLER SHAFT SHEARED D K NONE O OTHER ININSP/MAINT 1 CE07421LF 421C0059 234899R 742786 AIRCRAFT PROPELLOR WENT INTO FEATHER ON APPROACH. AFTER LANDING, RESTARTED ENGINE AND PROPELLOR FELL OFF. PROP SHAFT SHEARED IN HALF. ENGINE HAD A PROP STRIKE 400 HOURS PREVIOUS. 1L72 3O3 O A7CE E7CE 5 CP22EA 20010801002092001080100209CE 2001 8 1 2001FA0000074 120010531G71129691910016 AIR BOX BEECH 95 95B55 1152729CE RT ENGINE CRACKED G K NONE O OTHER ININSP/MAINT 1 SO17380882356 69 TC2366 RIGHT ENGINE AIRBOX DISPLAYS MORE THAN NORMAL WEAR DUE TO VIBRATION INDUCED CRACKING OF AIRBOX COMPONENTS. 1L72 3O RT3A16 20010801002102001080100210SO 2001 8 1 2001FA0000075 120010509G2700KSC270720V BEARING EMB 145 EMB145 SO HINGE BEARING FAILED G K NONE O OTHER ININSP/MAINT 1 SW13 DURING RECEIVING INSPECTION FLAT NUT IS TESTED ON HOUSING. WILL SPIN FREELY ON BUT THEN LOCKS UP 50 TO 80 PER CENT FAIL RATE. 2L72 4F RTT00011AT 20010713000152001071300015CE 2001 7 13 2001FA0000076 120010625G2434DOFF10300J BRUSHES CESSNA172 172M 2072418CE ALTERNATOR WORN D O OTHER O OTHER NRNOT REPORTED 1 SW019627Q 600 17265711 BRUSHES WORN TOTALLY OUT, ALLOWING SPRINGS AND WIRES TO DAMAGE ROTOR SLIP RINGS. POOR QUALITY BRUSHES NOT TO LAST LONGER. 1H71 3O NT3A12 20010801002112001080100211CE 2001 8 1 2001FA0000077 120010627G7603359440465 THROTTLE BEECH 33 E33A 1151424CE COCKPIT MISALIGNED G K NONE O OTHER ININSP/MAINT 1 WP23464SR CE275 THE THROTTLE CONTROL KNOB BUTTON RETAINING SCREW LOOSENED ALLOWING THE THROTTLE CONTROL KNOB BUTTON TO MISALIGN AND JAM DURING THROTTLE APPLICATION. THE THROTTLE CONTROL KNOB BUTTON RETAINING SCREW WAS FOUND APPROX 8 TURNS LOOSE. 1L71 3O 3A15 20010801002122001080100212CE 2001 8 1 2001FA0000078 120010710G531207126161 BULKHEAD CESSNA182 182L 2072726CE FUSELAGE CRACKED B QRQRK NONE O OTHER ININSP/MAINT 1 SW053301R4504 18258601 CRACKS IN THE UPPER OUTBOARD CORNERS OF THE RUDDER CABLE CUT-OUTS ON THE 0712616-1 BULKHEAD ASSEMBLY. AREA IN WHICH CRACK OCCURS IS RELATIVELY THIN GAUGE MATERIAL THAT APPARENTLY PROVIDES LITTLE STRUCTURAL STRENGTH. THE FLANGES IN THIS AREA DO LITTLE MORE THAN SERVE AS A FASTENING POINT FOR AN AERODYNAMIC FAIRING. IT IS DOUBTFUL IF THIS DEFECT IMPAIRS THE STRUCTURAL STRENGTH OF THE BULKHEAD ASSEMBLY AS THE 0712616-4 STIFFENER THAT ATTACHES TO THE -1 BULKHEAD IS MUCH HEAVIER GAUGE MATERIAL. 1H71 3O NT3A13 20010801002132001080100213SW 2001 8 1 2001FA0000080 120010710G5711 SPAR BBAVIA7 7AC 2110102SW LT WING CRACKED C K NONE O OTHER ININSP/MAINT 1 GL1583280 1947 DURING INSPECTION, FOUND LT WING FORWARD SPAR CRACKED AT UNDERSIDE OF SPAR OUT BOUND OF LIFT STRUT ATTACH POINT. THIS WING WILL BE REPAIRED WITH NEW SPAR INSTALLED. 1H71 3O A759 20010801002142001080100214SW 2001 8 1 2001FA0000081 120010625G5711 SPAR BBAVIA7 7FC 2110124SW WING CRACKED D K NONE O OTHER ININSP/MAINT 1 WP279052B 7FC140 BOTH FRONT SPARS HAD SEVERE CRACKS AT ATTACH POINTS INTO BUSHINGS. 1H71 3O A759 20010802002682001080200268NE 2001 8 2 2001FA0000082 120010405G572021610075 ANGLE CONAERLA4 LA4250 5110320NE WING CRACKED D K NONE O OTHER ININSP/MAINT 1 SO14 1574 31 WHILE PREPARING PRE-PURCHASE CONDITION REPORT ON ABOVE AIRCRAFT. THE LEFT LOWER SPAR DOUBLER WAS FOUND CRACKED. VISUAL INSPECTION SHOWED LOWER SPAR ANGLE CRACKED. 1H71 3O 1A13 20010801002152001080100215NE 2001 8 1 2001FA0000083 120010405G573021610063 DOUBLER LAKEACLAKE 250LAKE 5110322NE WING CRACKED D K NONE O OTHER ININSP/MAINT 1 SO149224D1574 31 WHILE PREPARING PRE-PURCHASE CONDITION REPORT ON ABOVE AIRCRAFT, THE LEFT LOWER SPAR DOUBLER WAS FOUND CRACKED. VISUAL INSPECTION SHOWED LOWER SPAR ANGLE CRACKED. 1H71 3O NC1A13 20010801002242001080100224GL 2001 8 1 2001FA0000085 320010601G6110C5046 PLATE CESSNA182 R182 2072734CE MCAULY2D34C B2D34C218 GL AFT BLKHD ATTACHCRACKED C K NONE O OTHER ININSP/MAINT 1 EA21 THIS PROPELLER INSTALLATION UTILIZES 2 SPINNER AFT BULKHEAD ATTACH PLATES, PN A1639-9. BOTH PLATES WERE FOUND TO BE CRACKED WITHIN 50 HR OF INSTALLATION OF PROP AFTER OVERHAUL. BECAUSE BULKHEAD ATTACHMENT PLATES ARE INSTALLED UNDER ATTACHMENT NUTS, PN A1639-9, THAT HOLDS THE PROP TO THE ENGINE IS SUBJECTED TO VERY HIGH CONTACT FORCES DUE TO THE SMALL SHOULDER ON THE NUT(A1639-9). THE LIKELIHOOD OF THIS FAILURE WILL INCREASE WITH THE NUMBER OF TIMES THESE FASTENERS ARE TORQUED. IPC CALLS FOR THE INSTALLATION OF A WASHER BETWEEN ATTACHMENT PLATE AND NUT, EXCEPT THERE IS NOT SUFFICIENT CLEARANCE TO ALLOW THE INSTALLATION OF THE WASHER. 1H71 3O RT3A13 5 CP7EA 20010801002252001080100225NE 2001 8 1 2001FA0000086 120010424G2752MS28775115010 O-RING GERDES LAKEACLAKE 250LAKE 5110321NE SHAFT DETERIORATED G K NONE O OTHER ININSP/MAINT 1 SO17CGPXH1868 741 DURING LOCAL FLIGHT, PILOT NOTICED HYDRAULIC PUMP CYCLING CONSTANTLY. PILOT ELECTED TO LAND AND CHECK. LANDING GEAR WOULD NOT FULLY EXTEND. PILOT COULD NOT GET LANDING GEAR FULLY UP OR DOWN. EMERGENCY LANDING MADE WITH PARTIAL GEAR ON GRASS STRIP WITH MINIMAL DAMAGE. FOUND T/E FLAP ACTUATOR SHAFT SEALS (3 ORINGS) LEAKING FLUID CAUSING LACK OF SUFFICIENT PRESSURE TO OPERATE GEAR AND FLAPS. 1H71 3O NC1A13 20010801002272001080100227GL 2001 8 1 2001FA0000087 320010228G6110C5152 COUNTERWEIGHT MCAULY CESSNA208 208 2073702CE MCAULY3AF34C3AF34C* GL ARM CRACKED G K NONE O OTHER ININSP/MAINT 1 SO23LVWYZ1720 952445 0522 DURING MAGNETIC PARTICLE INSPECTION, AN INDICATION WAS FOUND IN THE TRANSITION BETWEEN THE COUNTERWEIGHT ARM AND THE ATTACHMENT AREA, WHERE IT JOINS THE BLADE ROOT. THE CRACK APPEARS LIKE A HAIR LINE BUT STRONG INDICATION, ONCE IT WAS GROUND TO MAXIMUM DEPTH ALLOWABLE THE CRACK STARTED TO GROW IN WIDTH AS WELL AS CHANGED ITS DIRECTION BY 90 DEGREE, SO THE CRACK DEVELOPED A PATTERN TYPICAL FROM A FORGING FOLD. A PERIODICAL INSPECTION COULD BE A GOOD PREVENTATIVE TECHNIQUE. 1H71 3T NTA37CE 5 CP22EA 20010802002692001080200269CE 2001 8 2 2001FA0000091 120010525G553004310093 FITTING CESSNA150 152 2071835CE VERTICAL STAB CRACKED D K NONE O OTHER ININSP/MAINT 1 NM01714TD 15279413 DURING ROUTINE 100 HR INSPECTION, MINOR CORROSION WS FOUND ON BOTH LEFT AND RIGHT VERTICAL STABILIZER ATTACH FITTINGS, APPROX BS 200.4. UPON REMOVAL OF CORROSION, A CRACK WS FOUND IN THE RADIUS OF THE RIGHT FITTING APPROXIMENTLY .7500 OF THE WAY ACROSS AND APPROX .50 PERCENT OF THE THICKNESS DEEP. PROBABLE CAUSE: ROUTINE STRESS SOLUTION: TIME LIFE REPLACEMENT OF ATTACH FITTINGS. 1H71 3O NT3A19 20010801002292001080100229EA 2001 8 1 2001FA0000092 220010612G8530O5K21114 CYLINDER CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA INTAKE ARM CRACKED D K NONE O OTHER ININSP/MAINT 1 SO1366934347 15281670 L2129415 DURING ROUTINE INSPECTION, FOUND NR 1 CYLINDER TO BE CRACKED ABOVE THE INTAKE VALVE GUARD AREA. WHEN PRESSURIZED, THE ENTIRE LENGTH OF THE CRACK PRODUCED BUBBLES. 1H71 3O3 ONT3A19 E223 20010801002302001080100230CE 2001 8 1 2001FA0000093 120010607G323298820152 ACTUATOR CESSNA172 172RG 2072438CE MLG CRACKED D K NONE O OTHER ININSP/MAINT 1 SW179515B4503 172RG0846 DEFECT WAS DISCOVERED WHILE PERFORMING SB MAIN LANDING GEAR ACTUATOR INSPECTION. PART HAD CRACKED IN THE SUSPECTED AREA, THE SADDLE SHAPED HOLE AND CIRCUMFERENCE OF THE 2.28 INCH DIA. BORE AND STEP, NEAR THE ROLLER BEARING ASSEMBLY. THERE WAS NO EVIDENCE OF PILOT ERROR OR ABUSE. PART OTHERWISE INDICATED NORMAL WEAR. PROBABLE CAUSE: STRESS RISER INHERENT TO DESIGN, OR PART NOT DESIGNED TO BE STRONG ENOUGH. RECOMMENDATION: REDESIGN PART. 1H71 3O 3A17 20010801002312001080100231CE 2001 8 1 2001FA0000094 120010607G323298820152 ACTUATOR CESSNA172 172RG 2072438CE MLG CRACKED B K NONE O OTHER ININSP/MAINT 1 GL179515B4503 172RG0846 DEFECT WAS DISCOVERED WHILE PERFORMING SB MAIN LANDING GEAR ACTUATOR INSPECTION. PART HAD CRACKED IN THE SUSPECTED AREA, THE SADDLE-SHAPED HOLE AND CIRCUMFERENCE OF THE 2.28 INCH DIA BORE AND STEP, NEAR THE ROLLER BEARING ASSY. THERE WAS NO EVIDENCE OF PILOT ERROR OR ABUSE. PART OTHERWISE INDICATED NORMAL WEAR. PROBABLE CAUSE: STRESS-RISER INHERNTTO DESIGN, OR PART NOT DESIGNED TO BE STRONG ENOUGH. RECOMMENDATION: REDESIGN PART. 1H71 3O 3A17 20010801002322001080100232CE 2001 8 1 2001FA0000095 120010102G2822476411 PUMP CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO AFT OB WING TIP INTERMITTENT C K NONE O OTHER ININSP/MAINT 1 GL175336C167 310R1542 ON THE LEFT SIDE OF AC, WE HAVE REPLACED THE CIRCULATING PUMP NUMEROUS TIMES WHILE RIGHT SIDE HAS BEEN FINE. MOST RECENT DATES OF REPLACEMENT AS FOLLOWS: 12-9-99 TACH 3443.5, 9-18-2000 3715.3, 12-29-2000 3882.4. AS STATED EARLIER ALL 3 OF THESE WERE ON THE LEFT SIDE. ON 12-29-2000, WE INSPECTED THE WIRING AND BOTH INLET AND OUTLET HOSES/LINES FOR OBSTRUCTIONS. EACH PUMP WHEN REMOVED WAS VERY INTERMITTEN AND WOULD WORK WHEN THE CASING WAS TAPPED ON. PUMP NEEDS IMPROVEMENT. 1L72 3O3 O 3A10 E5CE 20010801002332001080100233EU 2001 8 1 2001FA0000097 320010524G61116607132886 BLADE ROTOL ROTOL R4204 R130420412 EU OUTER SLEEVE CRACKED C MS1RK NONE O OTHER ININSP/MAINT 1 EA27 265105020 DR6869386 DR6869386 PROPELLER RECEIVED FOR OVERHAUL. BLADE SN 616 WAS FOUND TO HAVE A CRACKED OUTER SLEEVE AT ROOT END OF BLADE. BLADE REJECTED FROM FURTHER SERVICE. 6 CP890 20010801002352001080100235CE 2001 8 1 2001FA0000098 120010606G5530 RIB CESSNA172 172 2072402CE RUDDER BROKEN D K NONE O OTHER ININSP/MAINT 1 NE015838A419 28438 UPPER RUDDER RIB WAS FOUND BROKEN AT THE OPENING FOR UPPER HINGE BOLT INSTALLATION ACCESS. THIS TYPE OF DAMAGE IS A REOCCURRING PROBLEM DUE TO A LACK OF PROPER GUST LOCKS FOR THE RUDDERS, WIND SLAPPING OF THE RUDDER WITH THE ARM OF THE BALANCE WEIGHT CAUSING CRACKS IN THE RIB WEAK POINT EVEN WITH THE ADDED DOUBLER. PROPER SECURING THE RUDDER WHEN OUTSIDE, MAY PREVENT FURTHER DAMAGE. 1H71 3O NT3A12 20010801002362001080100236SO 2001 8 1 2001FA0000099 120010608G78208523304 MUFFLER PIPER PA32 PA32R301 7103218SO LYC 0540 IO540K1G5D 41532SO ENGINE CRACKED B EWGRK NONE O OTHER ININSP/MAINT 1 SO059265B757 3246029 UPON REMOVAL OF HEATING SHROUDS FOR INSPECTION, FOUND SIDNIFICANT DISTORTION OF MUFFLER WAS CRACKED AT UPPER LEADING EDGE WELD. 1L71 3O3 O A3SO 1E4 20010801002422001080100242CE 2001 8 1 2001FA0000100 120010618G27300411258 BELLCRANK CESSNA150 150G 2071816CE CONT O200 O200* 17020SO ELEVATOR BLCRK ELONGATED D K NONE O OTHER ININSP/MAINT 1 WP283343J3456 15066043 FOUND ELEVATOR BELLCRANKS CABLE ATTACH POINTS ELONGATED. RIGHT ATTACH WAS ELONGATED BY .215, LEFT ATTACH WAS ELONGATED BY .248, THE AN23-11 ATTACH BOLT IS .184. DRILLED OVERSIZE AND PUT NAS 75-3-004 STEEL BUSHING PRESSED IN, TO BRING BACK CORRECT TOLERANCE. 1H71 3O3 O 3A19 E252 20010801002432001080100243SO 2001 8 1 2001FA0000101 120010628G78208523310 MUFFLER PIPER PA32 PA32R301 7103218SO LYC 0540 IO540K1G5D 41532SO RIGHT CRACKED B K NONE O OTHER ININSP/MAINT 1 SO059265B757 3246029 UPON REMOVAL OF HEATING SHROUDS FOR INSPECTION, FOUND SIGNIFICANT DISTORTION OF MUFFLER CAN. THE MUFFLER WAS CRACKED AT UPPER LEADING EDGE WELD. 1L71 3O3 O A3SO 1E4 20010801002442001080100244 2001 8 1 2001FA0000102 420010604G3421101490159 GYRO CESSNA172 172R 2072401CE LYC O360 IO360A1C 41514EA ATTITUDE FAILED B OF1RK NONE O OTHER ININSP/MAINT 1 EA179453Z294 17280193 GYRO TUMBLED IN FLIGHT AND WOULD NOT RE-ERECT. MAINTENANCE TROUBLESHOOTING REVEALED NO DEFECTS WITH INSTRUMENT AIR SYSTEM. GYRO WAS REPLACED WITH A SERVICEABLE OVERHAULED UNIT. SYSTEM RETESTED AND REPLACEMENT GYRO FUNCTIONS NORMALLY. AIRCRAFT AND SYSTEM HAVE BEEN MAINTAINED AS PER MANUFACTURERS RECOMMENDATIONS SINCE NEW. 1H71 3O3 ONT3A12 1E10 20010801002452001080100245GL 2001 8 1 2001FA0000103 320010320G6110 SNAP RING MCAULY CESSNA182 182P 2075816CE CONT O470 O470R 17026SO MCAULY2A34C 2A34C203 GL NR 1& 2 BLDE RETFAILED D IT6RK NONE O OTHER ININSP/MAINT 1 NM015612J 74517 18263467 459837 EXTERNAL SNAP RING ON PROPELLER BLADE CAME OFF AFTER PREFLIGHT ENGINE HAD STOPPED ON INITIAL START, THEN WAS RESTARTED. SNAP RING CAME OFF BLADE SHANK BUT WAS RETAINED BY SPINNER. THEN AIRPLANE WAS FLOWN FOR 2 HOURS WITH FIVE TOUCH AND GO LANDINGS, WITHOUT FAILURE OF PROPELLER. PROPELLER WAS THEN REMOVED AND TAKEN BACK TO OVERHAUL SHOP WHERE TEAR-DOWN WAS COMPLETED. FINDING WAS SNAP-RING WAS NOT SEATED PROPERLY. THE BLADE TO PISTON LINK WAS DAMAGED AND REPLACED. THE PROPELLER BLADE WAS DRESSED AT SHANK. 1H71 3O3 ONTTA13 E273 5 CP3EA 20010801002462001080100246SO 2001 8 1 2001FA0000104 120010621G57116207006 SPAR PIPER PA32 PA32300 7103212SO LYC O540 TIO540* 41532EA OB OF MAIN GEAR CORRODED D K NONE O OTHER ININSP/MAINT 1 WP0786CA 3194 3240957 WHILE RE-SKINNING THE LEFT UPPER INBOARD WING SKIN, WE FOUND CORROSION IMMEDIATELY OUT BOARD OF THE LEFT MAIN LANDING GEAR CASTING ON THE LOWER AFT SIDE OF THE MAIN SPAR INSIDE THE WING. THE CORROSION SEEING TO BE CENTRALIZED AROUND ONE RIVET AND RADIATING OUTWARD FROM THAT RIVET. THERE IS NO OTHER CORROSION IN THAT AREA OF THE WING. 1L71 3O3 O A3SO E14EA 20010801002472001080100247SW 2001 8 1 2001FA0000106 120010702G5711 SPAR BBAVIA7 7AC 2110102SW CONT O200 O200A 17020SO LIFT STRUT ATTCHCRACKED D K NONE O OTHER ININSP/MAINT 1 SW071703E 7AC5268 690748A FOUND A SMALL LONGITUDINAL CRACK BETWEEN THE PLYWOOD DOUBLER PLATE AT THE FORWARD LIFT STRUT ATTACH FITTING AND THE NEXT OUTBOARD RIB ALONG THE REAR FACE OF THE SPAR. WITH A MIRROR IN THE NEXT OUTBOARD RIB BAY, THE CRACK PROTRUDED ABOUT THREE INCHES. WHEN THE FABRIC WAS REMOVED THE CRACK RAN FROM THREE INCHES INBOARD OF THE PLYWOOD DOUBLER AT THE LIFT STRUT ATTACH FITTING TO ABOUT THREE INCHES OUTBOARD OF THE SAME DOUBLER. THE CRACK WAS ONLY VISIBLE ON THE AFT FACE OF THE SPAR. 1H71 3O3 O A759 E252 20010801002482001080100248EA 2001 8 1 2001FA0000107 220010626G8520 CRANKSHAFT PIPER PA60 PA60601P 7106012NM LYC O540 TIO540* 41532EA ENGINE BROKEN B GSZRC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW19377RC 140 61P057579632L570161A ENGINE FAILED ON TAKE OFF. FACTORY REP. REPORTED BY PHONE THAT CRANKSHAFT HAD BROKEN. 1M72 3O3 ORTA17WE E14EA 20010801002492001080100249CE 2001 8 1 2001FA0000108 120010627G37100701030807 HOSE CESSNA182 182R 2072731CE CONT O470 O470* 17026SO VACUUM SYSTEM DISINTEGRATED B HX1RK NONE O OTHER ININSP/MAINT 1 EA259953H 18268139 CUSTOMER REPORTED LOW VACUUM INDICATION BUT GYROS RUNNING OK. INITIAL INVESTIGATION ALL HOSES LOOKED OK, HOWEVER WHEN HOSES WERE TOUCHED, FELL APART. THE ABOVE REFERENCED PN IS FOR ONE OF THE VACUUM GAUGE HOSES, HOWEVER ALL INSTRUMENT HOSE WERE OF THE SAME TYPE AND ALL FELL APART WHEN TOUCHED. BOTH GYROS WERE REMOVED FROM INLET FITTINGS (SCREENS ON INLET PORTS STOPPED MATERIAL FROM GETTING IN INSTRUMENTS). A TEMPORARY IN LINE FILTER WAS INSTALLED ON THE INLET SIDE OF VACUUM PUMP TO PREVENT MATERIAL FROM GOING INTO THE PUMP AND THE AIRCRAFT WAS GROUND RUN. NO DATES WERE FOUND ON THE HOSES. THE NUMBER 04A WAS ON SEVERAL HOSES EVERY 6 INCHES. THEY APPEAR TO BE ORIGINAL HOSES. 1L71 3O3 ONT3A13 E273 20010801002502001080100250SO 2001 8 1 2001FA0000112 120010627G3210AN310A BOLT PIPER PA30 PA30 7103002SO LYC O320 IO320* 41508EA MLG BROKEN B K NONE O OTHER ININSP/MAINT 1 SO137993Y 301098 THE AN3-10A BOLT, HOLDING THE MAIN GEAR SPRING ATTACH BRACKET ON TO THE STRUT HOUSING, BROKE. IT CAUSED THE BRACKET TO JAM AGAINST THE GEAR FORWARD ATTACH FITTING AND WOULD NOT LET THE GEAR GO DOWN. AIRCRAFT LANDED WITH THE GEAR UNSAFE. 1L72 3O3 O A1EA 1E12 20010801002512001080100251EA 2001 8 1 2001FA0000113 220010704G8530AEL6510241 CYLINDER PIPER PA28 PA28161 7102803SO LYC O320 O320* 41508EA HEAD CRACKED B MW2RK NONE O OTHER ININSP/MAINT 1 GL174381L306 288516016 L1341139A CYLINDER CRACKED FROM TOP SPARK PLUG HOLE AROUND OUTSIDE EXSEAT TO BOTTOM SPARK PLUG HOLE. 1L71 3O3 O 2A13 E274 20010801002532001080100253EA 2001 8 1 2001FA0000114 220010709G8530AEL6510241 CYLINDER PIPER PA28 PA28161 7102803SO LYC O360 O360* 41514EA CYLINDER HEAD CRACKED B MW2RK NONE O OTHER ININSP/MAINT 1 GL174328D1293 288416019 CYLINDER CRACKED FROM TOP SPARK PLUG HOLE AROUND OUTSIDE EXSEAT TO BOTTOM SPARK PLUG HOLE. 1L71 3O3 O 2A13 E286 20010725006152001072500615SW 2001 7 25 2001FA0000115 120010608G2810206362002103 CAP BELL 407 407 SW FUEL CELL BINDING C K NONE K FLUID LOSS ININSP/MAINT 1 EA01 35 53444 FUEL FILLER CAP DOES NOT SEAT PROPERLY DUE TO CLOSE TOLERANCE BETWEEN AIRFRAME SPACERS AND CAP. THIS OCCURS 8 OR 9 TIMES OUT OF TEN CLOSURES. THE FUEL LEAKS DOWN THE SIDE OF THE AIRFRAME AND GETS SUCKED INTO AIR CONDITIONING FAN THRU CONDENSER. FUEL SPRAY BECOMES PRESSURIZED SPRAYING UP INTO AFT COMPARTMENTS BELOW BAGGAGE COMPARTMENT. AIRCRAFT INVERTERS ALSO WET WITH FUEL SPRAY, COULD BE SOURCE OF IGNITION AND POSSIBLE IN FLIGHT FIRE. RECOMMENDATION, OPEN UP CLEARANCE BETWEEN CAP DIAMETER AND AIRFRAME SPACERS. THIS AIRCRAFT HAS HAD PART 1 OF ASB 407-01-41 INCORPORATED. 1G71 3U O H2SW 20010727002602001072700260NE 2001 7 27 2001FA0000117 120010727G63217636309103102 DISK SKRSKY SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL2B NE ROTOR BRAKE CRACKED C K NONE E VIBRATION/BUFFET ININSP/MAINT 1 EA17317MX930 C207002824 760499 20523 DURING A SCHEDULED MAINTENANCE EVENT THE MAIN ROTOR BRAKE DISC WAS FOUND TO BE FRACTURED, COMPLETELY THROUGH, FROM THE OUTER TO THE INNER CIRCUMFERENCE, AND THERE WERE SOME VISUAL CRACKS EMANATING FROM AROUND THE MOUNTING HOLES. THE CREW HAD MENTIONED, THAT DURING ROTOR BRAKING, HAD FELT SOMETHING AND NOTICED AN INCREASE IN VIBRATION. THIS COMPONENT IS MOUNTED BETWEEN THE ENGINE INLETS, SURROUNDED BY NUMEROUS FUEL AND HYDRAULIC LINES, AND SHARES THE SAME DRIVE AS THE TAIL ROTOR. IF THIS WERE TO SEPARATE DURING GROUND OR FLIGHT OPERATIONS THE RESULT WOULD BE CATASTROPHIC. SIKORSKY AIRCRAFT (610-954-9613) WILL RECEIVE THE ASSEMBLY ON 7-29-01, AND FOWARD IT TO SIKORSKY ENGINEERING. 1G72 3U3 UNCH1NE E00054EN 20010801002542001080100254GL 2001 8 1 2001FA0000118 120010706G2820 CHECK VALVE CIRRUSSR SR20 05628AJGL CONT O550 IO550* SO RT HEADER TANK MISINSTALLED B NF2RK NONE O OTHER ININSP/MAINT 1 GL11960CM31 0041 685781 RIGHT FUEL QUANTITY GAUGE FALLS TO ZERO WHEN RIGHT TANK WAS SELECTED. FOUND FUEL QUANTITY TRANSMITTER WAS CORRECT, INBOARD TRANSMITTER MOUNTED IN THE HEADER TANK WAS GOING TO ZERO WHEN FUEL WAS BEING USED FROM THE RIGHT TANK. CAUSE: THE FUEL INLET CHECK VALVE WAS GLUED CLOSED DURING ASSEMBLY OF THE AIRCRAFT. THE ENG WOULD USE MORE FUEL THAN THE RATE THE HEADER TANK COULD FILL, THIS CONDITION COULD CAUSE ENGINE STOPPAGE.DURING REPAIRS IT WAS FOUND THE NORMAL OPERATING SYSTEM CAN NOT KEEP EITHER HEADER TANK FULL. FUEL QUANTITY INDICATION IS NOT ACCURATE WHEN ENGINE IS USING FUEL FROM THAT TANK. 1H71 3O3 ONCA00009CHE3SO 20010801002552001080100255EA 2001 8 1 2001FA0000119 220010718G8500RJ0506041 DOOR RAJAYXXXXXXX MOONEYM20 M20D 5870210SW LYC O360 O360* 41514EA TURBO DOOR LOOSE D K NONE O OTHER ININSP/MAINT 1 SO09191PA500 248 DURING ANNUAL INSPECTION, PART WAS OBSERVED TO BE EXTREMELY LOOSE. REMOVED PART FROM ASSEMBLY. FOUND PORTION OF HINGE MISSING, HINGE PIN 95 PER CENT WORN THROUGH AND SIDE BRACKETS WORN 90 PER CENT THROUGH. REMOVED ASSEMBLY AND REPLACED DOOR AND FRAME WITH SERVICEABLE PART. FOUND BYPASS FLUTTER VALVE FOR CARB HEAT MISSING. INSTALLED NEW PART AND SECURED. 1L71 3O3 O 2A3 E286 20010801002562001080100256CE 2001 8 1 2001FA0000120 220010712G7320S29991 SWIVEL CESSNA337 T337G 2075726CE CONT IO360 IO360* 17025CE MIXTURE CONTROL SEPARATED D K NONE O OTHER ININSP/MAINT 1 WP23265 6 6 P3370232 INSTALLED BALL JOINT OR SWIVEL PN S2999-1 ON MIXTURE CONTROL CABLE FRONT AND REAR ENGINES AT TIME OF ENGINE INSTALLATION. A/C WAS TEST FLOWN AND FERRIED TO PAINT SHOP AND RETURNED. PREVIOUS TO ANY ADDITIONAL ADJUSTMENT AND WHILE IN THE COCKPIT PERFORMING A MAINTENANCE CHECK AND OPERATING THE MIXTURE CONTROL, THE SWIVEL SEPARATED ON THE REAR ENGINE CABLE. FURTHER OPERATION, IT WAS NOTED THE FRONT ENGINE MIXTURE CONTROL BALL JOINT SWIVEL CAME APART. MFG WAS NOTIFIED. 1H72 3O3 O A6CE E1CE 20010801002582001080100258CE 2001 8 1 2001FA0000121 120010711G2497 WIRE CESSNA175 175 2072502CE CONT O300 GO300* 17022SO INST PANEL DEFECTIVE B K NONE O OTHER ININSP/MAINT 1 NM096651E1904 56151 AIRCRAFT BROUGHT TO BE CLEAN-UP WIRING BEHIND INSTRUMENT PANEL. UPON FURTHER INSPECTION I IMMEDIATELY DISCONNECTED THE SHIPS BATTERY DUE TO THE FACT THE WIRING WAS IN SUCH A DISARRAY I COULD NOT BELIEVE IT WORKED AND IF SO WHY IT HAD NOT CAUSED A FIRE. IE: EXPOSED SOLDER SPLICES THAT WERE IN POWER FEED LINES. 4 DIFFERENT SPLICES PLUS 1 FUSE IN LESS THAN 16 INCHES IN THE AME 18AWG WIRE. FUSES IN LINE WITH FUSES, WIRE STRANDS TWISTED, POORLY SOLDERED AND HOOKED TO THE LINE SIDE OF MASTER SWITCH. ALL DEFECTS WERE CORRECTED AND AC APPROVED FOR RETURN TO SERVICE. 1H71 3O3 ONT3A17 E298 20010801002592001080100259CE 2001 8 1 2001FA0000122 120010621G2140C3A051 HEATER BEECH 60 A60 1153604CE LYC O541 TIO541* 41536EA CABIN LEAKING D K NONE K FLUID LOSS ININSP/MAINT 1 NM0881AG 323 323 P219 DURING PRESSURE DECAY TEST FOUND GASKETS. CANASTER A09077 AND NOZZLE 29D-28 LEAKING. REPLACED AND HEATER PASSED PRESSURE DECAY TEST. 1L72 3O3 O A12CE E10EA 20010801002602001080100260CE 2001 8 1 2001FA0000123 120010629G57115262 SPAR BBAVIA7 7KCAB 21101P3CE LYC O320 IO320* 41508EA WING CRACKED G K NONE O OTHER ININSP/MAINT 1 GL1386960 44674 DURING INSPECTION OF RIGHT WING, A CRACK WAS FOUND ON THE AFT SIDE OF THE FORWARD WOOD SPAR, 79 INCHES OUTBOARD FROM THE BUTT RIB. THE 5 INCH LONG, HORIZONTAL CRACK WAS LOCATED AT THE COMPRESSION MEMBER AND RAN THROUGH THE HOLES FOR THE DRAG WIRES. UNDETERMINED CAUSE. 1H71 3O3 O A759 1E12 20010802000012001080200001SO 2001 8 2 2001FA0000128 120010711G27308283302 ROD PIPER PA46 PA46310P 7104605SO ELEVATOR CONTROLCORRODED B K NONE O OTHER ININSP/MAINT 1 GL19248SP2321 468608024 ELEVATOR PUSH PULL CONTROL ROD VERY RUSTY AND PITTED. LOCATED IN TAIL SECTION WHERE MOISTURE AND CONTAMINATION ACCUMULATE. 1L71 3O RTA25SO 20010802001382001080200138EA 2001 8 2 2001FA0000129 220010629G7310 SERVO PREAIR RSA5AD1 CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA MCAULY1A170 1A170E GL FUEL INJECTION MALFUNCTIONED C C ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW99948SP1119 70168504 172S8144 L2812651A SL029 RPM SET TO 1500 FOR PURGING FUEL VAPORS PRIOR TO TAXI, TAXI AND RUN UP WERE NORMAL. WHEN FULL THROTTLE WAS APPLIED FOR TAKE OFF THE ENGINE WOULD NOT DEVELOP FULL POWER. IT WOULD ONLY DEVELOP 2000 RPM. MAINTENANCE INSTALLED CLEAR FUEL LINE ON OUTLET LINE FROM FUEL INJECTION SERVO IAW PRECISION AIRMOTIVE TROUBLESHOOTING TECHNIQUES. THE THROTTLE AND MIXTURE WERE OPENED TO SIMULATE ENGINE OPERATION, VAPOR BUBBLES WERE OBSERVED FOR APPROXIMATELY 10 MINUTES FLOWING FROM THE FUEL SERVO. AFTER 10 MINUTES, THE LINE FILLED WITH FUEL AND THE ENGINE HAD COOLED. THE ENGINE WAS STARTED AND ALL OPERATION NORMAL WITH FULL POWER BEING DEVELOPED. AIRCRAFT RELEASED FOR TEST FLIGHT. TEST FLOWN SATISFACTORY. 1H71 3O3 ONT3A12 1E10 5 NP857 20010802001392001080200139CE 2001 8 2 2001FA0000130 120010629G7100LW12427 CYLINDER CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA MCAULY1A170 1A170E GL ENGINE OVERHEATED D A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 SW99494SP1116 172S8035 L2790951A SD013 PILOT REPORTED ENGINE STARTED RUNNING ROUGH IN FLIGHT AND LOOSING ALTITUDE. MADE EMERGANCY LANDING, WENT OFF END OF RUNWAY AND WENT UPSIDE DOWN. AIRCRAFT RIGHTED AND MOVED TO HANGER. MAINTENANCE FOUND #2 CYLINDER EXHAUST PUSHROD BENT IN HALF & BROKEN, THE PUSHROD HOUSING BENT AND PULLED LOOSE FROM CASE WITH SUBSIQUENT OIL LOSS. THE INTAKE PUSHROD & HOUSING WAS BENT. WHEN THE VALVE COVER WAS REMOVED BOTH VALVES WERE CLOSED AND NOT STUCK. THE VALVES WERE REMOVED FROM THE CYLINDER AND FELL OUT OF THE GUIDES FREELY, THEY WERE FREE OF CARBON DEPOSITES AROUND STEMS. BOTH VALVE SEATS WERE BURNED & THE INTAKE VALVE WAS ALSO BURNED AROUND THE SEATING AREA. 1H71 3O3 ONT3A12 1E10 5 NP857 20010802001492001080200149CE 2001 8 2 2001FA0000131 120010703G5711 SPAR BBAVIA7 7KCAB 21101P3CE UNSECURE D K NONE O OTHER ININSP/MAINT 1 SW998680V775 AIRCRAFT REGISTERED AS BELLANCA. MODEL IS 7KCAB. DESIGN NOW OWNED BY AMERICAN CHAMPION. WOOD SPAR WING INSPECTED IN ACCORDANCE WITH AD 2000-25-02. SEVERAL RIB/SPAR ATTACHMENT NAILS MISSING. PER SERVICE LETTER SL-417 THE SPAR "DAMAGE" CAUSED BY THE MISSING NAILS WAS NOT SIGNIFICANT ENOUGH TO REQUIRE REPAIR. NEW NAILS INSTALLED IN ACCORDANCE WITH INSTRUCTIONS FROM AMERICAN CHAMPION. 1H71 3O A759 20010802001502001080200150CE 2001 8 2 2001FA0000133 120010430G311004110591 SHOCK MOUNT CESSNA210 210D 2073414CE INSTR PANEL BROKEN C B EMER. DESCENT O OTHER DEDESCENT 1 SW993738Y3304 21058238 AFTER FLYING THROUGH TURBULANCE THE PILOT COULD NOT LEVEL OFF ATER A DECENT DUE TO LIMITED ELVEATOR CONTROL. A NOSE FIRST LANDING WAS ACCOMPLISHED WITH THE AIRCRAFT/ENGINE RECEVING SUBSTANTIAL DAMAGE. INITIAL OBSERVATIONS REVEALED THE ELVEATORS ONLY GOING TO NEAR LEVEL FLIGHT POSITION. INVESTIGATION FOUND THAT THE HEADING SITUATION INDICATOR WAS MOUNTED DIRECTLY ABOVE THE CONTROL COLUMN WHICH WAS BEING HIT BY THE CONTROL COLUMN STOP. THE INSTRUMENT PANEL WAS RECONFIGURED TO ITS PRESENT LAYOUT IN 1994. THE INSTRUMENT PANEL SHOCK MOUNTS INTHE LOWER RIGHT AND LOWER CENTER WERE BROKEN. THE DATES ON THE PANEL SHOCK MOUNTS WERE ALL PREVIOUS TO 1963, THE DATE THE AIRCRAFT WAS MANUFACTURED. 1H71 3O 3A21 20010802001722001080200172CE 2001 8 2 2001FA0000135 120010705G2421DOFF10300FR ALTERNATOR CESSNA172 R172G 2072421CE CONT O360 IO360DB 17025SO MISOVERHAULED C K NONE O OTHER ININSP/MAINT 1 SW997753L 170 R1720429 239773R DURING MAINTENANCE 100 HOUR INSPECTION, FOUND ALTERNATOR INTERNAL FAN SHIELD SEPERATED FROM FAN DUE TO SHEARED RIVITS AND THE DRIVE SHAFT OIL SEAL WAS LEAKING. REPLACED ALTERNATOR WITH UNIT OVERHAULED BY DIFFERENT MANUFACTURER, OPERATIONAL CHECKED SATISFACTORY. 1H71 3O3 O 3A17 E1CE 20010802001822001080200182CE 2001 8 2 2001FA0000136 120010705G3710P10UCB86 FITTING CESSNA182 182S 2072701CE VACUUM SYSTEM BROKEN B D RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP077260Q16 18280957 THE PILOT REPORTED THAT THERE WAS ZERO VACUUM INDICATED ON THE GAUGE AND THAT THE HSI GYRO WOULD NOT ERECT. A VISUAL INSPECTION BY A MAINTENANCE TECHNICIAN REVEALED THAT THE VACUUM SUPPLY LINE REDUCER FITTING WAS BROKEN IN TWO. 1H71 3O NT3A13 20010802001842001080200184SO 2001 8 2 2001FA0000137 120010702G32608929103 DOWNLOCK SWITCH PIPER PA44 PA44180 7104402SO MLG INOPERATIVE D K NONE O OTHER ININSP/MAINT 1 SW99 2490 4496013 WHILE CONDUCTING A SCHEDULED INSPECTION,THE TECHNICIAN DISCOVERED SEVERAL WIRES WERE BROKEN OF THE DOWN LIMIT SWITCH.THERE WERE NO PROBLEMS REPORTED BY THE PILOT AT THIS TIME.ALSO WHEN PLACING THE AIRCRAFT ON JACKS AND PERFORMING A LANDING GEAR TEST THERE WERE NO PROBLEMS FOUND.EVERYTHING SEEMED NORMAL. WHEN THE LANDING GEAR WAS RETRACTED SEVERE TENSION OCCURED ON THE WIRES AND WERE THEREFORE PULLED FROM THE SWITCH ASSY.A PROBLEM COULD HAVE OCCURED IF ALL THE WIRES HAD BROKEN. BOTH THE LT AND RT DOWN LIMIT SWITCHES WERE REPLACED AND THE WIRES REROUTED. ATTENTION SHOULD BE PAID TO THE ROUTING OF THE WIRES,WHEN THE LANDING GEAR RETRACTS. 1L72 3O A19S0 20010802001872001080200187CE 2001 8 2 2001FA0000138 120010709G3242 BRAKE CESSNA172 172M 2072418CE MLG INOPERATIVE P D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW9912790 17262262 PRIOR TO TAXI THE PARKING BRAKE WAS FOUND INOP; HOWEVER, THE BRAKES OPERATED NORMALLY. THE AIRCRAFT WAS TAXIIED TO THE RUNUP AREA AND CONDUCTING THE RUNUP USING THE STANDARD BRAKES. AFTER RUNUP, THE PILOT WAS INSTRUCTED TO TAXI INTO POSITION AND HOLD. WHILE TAXIING INTO POSITION THE LEFT BRAKE FAILED. THE PILOT HAD THE COPILOT HID THE BRAKES ON THE RIGHT SEAT. THE LEFT BRAKE WAS INOP ALSO. THE AIRCRAFT VERRED RIGHT OFF THE APPROACH END OF THE RUNWAY STRIKING A RUNWAY LIGHT. AFTER SECURING THE ENGINE, THE PROPELLER WAS EXAMINED FOR STRIKES. ONE BLADE HAD SURFACE DAMAGE TO THE PAINT ON THE TIP. THE OTHER BLADE HAD A 3/16 INCH NICK ON THE LEADING EDGE ABOUT 2 INCHES FROM THE TIP AND THE TIP WAS BENT AFT ABOUT 1/21H71 3O NT3A12 20010802001892001080200189CE 2001 8 2 2001FA0000139 120010709G3213SA530348 PISTON CESSNA172 172D 2072410CE CONT O300 O300D 17022SO STRUT CRACKED D K NONE O OTHER ININSP/MAINT 1 EA012051Y840 17249551 24597R DURING REPAIRS TO CYCL NR 4 FOR LOW COMPRESSION FOUND 1INCH CRACK IN PISTON SKIRT STARTING AT BOTTOM OF PISTON. 1H71 3O3 ONT3A12 E253 20010802001942001080200194SW 2001 8 2 2001FA0000140 120010712G2810 SUMP GULSTM680 680E 0141604SW FUEL TANK CORRODED D K NONE O OTHER ININSP/MAINT 1 SW99692784800 680E78150 MAIN FUEL SUMP REMOVED FROM ACFT. TO FACILITATE MAIN TANK REMOVAL FROM ACFT. VISUAL INSPECTION OF INSIDE OF PART REVEALED CONSIDERABLE CORROSION ON BOTTOM INSIDE SUMP. AFTER CLEANING, OBSERVED ONE AREA WHERE CORROSION THROUGH WALL TO OUTERSKIN ON CASTING HAD ALMOST COMPLETE PENETRATION. UNABLE TO DETERMINE INTERNAL CORRODED CONDITION OF PART WHILE PART WASINSTALLED ON ACFT. 1H72 3O 2A4 20010802001962001080200196SO 2001 8 2 2001FA0000141 220010426G741410682016 GEAR CONT D6LN3000 PIPER PA32 PA32RT300 7103215SO LYC 0540 IO540K1G5D 41532SO DISTRIBUTOR BROKEN G A UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 EA0139503 32R7885224 L1795748A ON TAKE OFF AT APPROXIMATLEY 500 FEET THE ENGINE FAILED. THE AIRCRAFT LANDED IN GRASS AT END OF RUNWAY WITHOUT INCIDENT. INSPECTION SHOWED THAT BOTH DISTRIBUTOR GEARS HAD FAILED, TEETH MISSING. 1L71 3O3 O A3SO 1E4 20010802001982001080200198EA 2001 8 2 2001FA0000142 220010512G8530FRST14 CYLINDER LYC O720 IO720A1B 41546EA ENGINE BROKEN B A UNSCHED LANDING D INFLIGHT SEPARATION NRNOT REPORTED 1 SW99 278 BARREL TO HEAD SEPERATION DURING FLIGHT. 3 O 1E15 20010802002022001080200202GL 2001 8 2 2001FA0000143 120010713G3221 BUSHING CIRRUS CIRRUSSR SR20 05628AJGL CONT O550 IO550* SO MLG LOOSE H O OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 EA21 27 27 0021 0012 685745 ON LANDING, NOSE WHEEL HAD SEVERE OSCILLATION/SHIMMY. INSPECTION AFTER TAXI FOUND NOSE WHEEL FAIRING CRACKED AND TIRE DAMAGED AROUND CIRCUMFERENCE. FURTHER INSPECTION FOUND THAT THE BUSHING ON THE RIGHT BOTTOM NLG MOUNT TO THE ENGINE MOUNT SHIFTED OUT OF ITS SEAT IN THE NLG WISHBONE MOUNT CAUSING THE BOLT TO RIDE ON THE HOLE IN THE NLG WISHBONE MOUNT. WE BELIEVE THAT THE PROBLEM IS A RESULT OF POSTION/TYPE OF BUSHINGS ON ASSEMBLY. 1H71 3O3 ONCA00009CHE3SO 20010802002042001080200204EA 2001 8 2 2001FA0000145 220010718G731325765362 SERVO CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA FUEL INJECTOR FROZEN D C ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW99949SP1053 543 172S8145 L2812051A SECOND FLIGHT OF THE DAY, TEMP 89F, DA 9444. ENGINE START WAS DIFFICULT, TAXI AND ENGINE RUN UP NORMAL. AIRCRAFT TOOK THE RUN WAY FOR TAKE OFF. WHEN THROTTLE WAS OPENED TO FULL POWER, ENGINE HAD POPPING NOISE AND WOULD ONLY DEVELOP 2000 RPM. TAKE OFF WAS ABORTED FOR LOW POWER. A CLEAR LINE WAS INSTALLED FROM THE FUEL INJECTION SERVO TO THE FLOW DIVIDER IAW PRECISION AIRMOTIVE TROUBLE SHOOTING MANUAL AND EXCESSIVE VAPOR IN THE LINE WAS DISPLACING THE FUEL WHEN THE ENGINE WAS RUN. THE ENGINE WAS ALLOWED TO COOL COMPLETELY AND RESTARTED, NO VAPOR WAS DETECTED AND ALL OPERATION WAS NORMAL INCLUDING FUEL FLOW WITH THE ENGINE DEVELOPING FULL POWER. AIRCRAFT TEST FLOWN AND RELEASED. 1H71 3O3 ONT3A12 1E10 20010802002062001080200206SO 2001 8 2 2001FA0000146 220010724G8520646778 CONNECTING ROD CONT O520 IO520C 17032SO ENGINE GOUGED B K NONE O OTHER ININSP/MAINT 1 SW99 3 816945R FACTORY REBUILT ENGINE WITH 3.3 TTIS WAS BEING DISASSEMBLED FOR INSPECTION DUE TO A PROPELLER STRIKE. ONE OF THE #6 CONNECTING ROD BOLTS COULD NOT BE REMOVED WITH REASONABLE PRESSURE AND HAD TO BE DRIVEN OUT OF THE CAP. INSPECTION OF THE BOLT REVEALED THAT A BURR AND EVIDENCE OF GALLING HAD OCCURRED ON THE SHANK AT THE POINT WHERE ROD AND CAP PARTING SURFACES MEET. THE CAP WAS DAMAGED WITH SIGNIFICANT GOUGING WHERE THE BOLT HAD TO BE DRIVEN OUT LEAVING IT UNSERVICEABLE. 3 O E5CE 20010802002082001080200208SW 2001 8 2 2001FA0000149 120010728G324640041 WHEEL AIRTRCAT300 AT301 0390103SW MLG FATIGUED G C ABORTED TAKEOFF D INFLIGHT SEPARATION TOTAKEOFF 1 GL214361S5100 3010041 DURING TAKEOFF, RIGHT MAIN WHEEL HALF (OUTBOARD) SEPARATED. PILOT UNABLE TO REGAIN CONTROL AND WENT IN ROAD DITCH AND LANDED INVERTED. MINOR INJURY TO PILOT. WHEEL NUT, BEARING AND SPACER WERE STILL ON AXLE UPON ARRIVAL AT ACCIDENT SCENE. OUTER BEARING RACE HAD PULLED THROUGH WHEEL HALF RACE SHOULDER AND ALL 9 WHEEL BOLTS WERE EITHER BROKE UNDER TENSION OR HAD NUTS PULLED OFF BOLTS LEAVING BOLTS INTACT WITH NUT THREADS STILL EMBEDDED IN BOLT THREADS. CAUSE OF WHEEL FAILURE UNKNOWN AT THIS TIME. IMPROPER WHEEL ASSEMBLY OR INSTALLATION OF OVERSIZE TIRES AND TOO MUCH AIR PRESSURE ARE POSSIBILITIES OF FAILURE. 1L71 3R A9SW 20010802002102001080200210CE 2001 8 2 2001FA0000150 120010731G571257222062 RIB CESSNA441 441 2076020CE RT CENTER WING CRACKED B K NONE O OTHER ININSP/MAINT 1 SW992624D4196 4410122 DURING A SCHEDULED INSPECTION, IT WAS NOTED THAT THE RH CENTER WING CANTED RIB CAP P/N: 5722206-2 (RH CWS26.85) HAD A VISUALLY SUSPECT AREA ALONG THE BEND RADIUS BETWEEN THE CENTER WING MAIN SPAR (FS177.45) AND FS188.95". FURTHER INSPECTION USING FLUORESCENT PENETRANT REVEALED (2) CRACKS IN THE RADIUS, THE ORIGINAL SUSPECT AREA (FS185.35) AND ONE STARTING AT THE MAIN SPAR (FS177.45) PROTRUDING AFT. BOTH CRACKS ARE APPROXIMATELY .75" LONG. AFTER REMOVAL OF THE RIB CAP, CLOSE EXAMINATION OF THE PART REVEALED THAT THE CAP WAS MANUFACTURED SO THAT THE BEND WAS PARALLEL WITH THE GRAIN OF THE METAL INSTEAD OF PERPENDICULAR WHICH COULD RESULT IN THIS TYPE OF FAILURE. CESSNA CURRENTLY DOES NOT HAVE ANY SPECIFIC INSPECT1L72 3T RTA28CE 20010802002132001080200213CE 2001 8 2 2001FA0000151 120010731G2800 FITTING LEAR 25 25B 5170511CE DEFUEL SYSTEM CLOGGED B K NONE O OTHER ININSP/MAINT 1 SW99751GA 122 WHILE DEFUELING THE AIRCRAFT PREPATORY TO PAINTING, IT WAS DISCOVERED THAT NO FLOW COULD BE ACHIEVED THROUGH THE RIGHT DEFUEL FITTING. THE DEFUEL WAS ACCOMPLISHED BY TRANSFERRING ALL OF THE FUEL TO THE LEFT TANK AND REMOVING IT THROUGH THAT VALVE. WHEN WE OPENED THE RIGHT TANK A SHOP RAG WAS FOUND PLUGGING THE DEFUEL PORT. IT HAD OBVIOUSLY BEEN LEFT IN THE TANK DURING PRIOR MAINTENANCE. 2L72 4J A10CE 20010802002292001080200229SO 2001 8 2 2001FA0000154 220010426G741410682016 GEAR CONT D6LN3000 PIPER PA32 PA32RT300 7103215SO LYC 0540 IO540K1G5D 41532SO HARTZLHCC2Y HCC2YK1 GL DISTRIBUTOR BROKEN G A UNSCHED LANDING YG ENGINE STOPPAGE MULTIPLE FAILURE TOTAKEOFF 1 EA0139503 D040001GR 32R7885224 L1795748A CH32104A AFTER TAKE OFF AT APPROX 500FT AGL, THE ENGINE STOPPED RUNNING. AIRCRAFT MADE EMERGENCY LANDING IN A FIELD WITH NO DAMAGE OR INJURIES. INSPECTION OF MAGNETO REVEALED THAT BOTH DISTRIBUTOR GEARS HAD FAILED. MAGNETO WAS REBUILT BY TCM 04/07/2000 AND INSTALLED ON 5/12/2000. 1L71 3O3 O A3SO 1E4 5 CP920 20010802002312001080200231EA 2001 8 2 2001FA0000155 220010516G8520SL13S19646 GEAR PIPER PA30 PA39 7103902SO LYC O320 IO320B1A 41508EA CRANKSHAFT DAMAGED B K NONE O OTHER ININSP/MAINT 1 GL21 DURING COMPLICANCE WITH AD 96-09-10 - COMPLIED ALSO WITH AD 91-14-22 CRANKSHAFT GEAR RETAINING BOLT. ORDERED NEW CRANKSHAFT GEARS PN SL13S19464 FOR LH AND RH ENGINES. WHEN INSTALLING NEW GEARS IT WAS DISCOVERED ONE HAD THE TIMING MARK ON THE CORRECT TOOTH AND THE OTHER GEAR HAD THE TIMING MARK INSTALLED ONE TOOTH OFF. THESE ARE THE FIRST OF THESE GEARS WE HAVE PURCHACED. NOTIFIED SUPERIOR AIR PARTS 5-15-2001. SUGGEST ALL OPERATORS USING THIS GEAR LOOK FOR PROPER TIMING MARKS ON THE GEAR BEFORE INSTALLATION- IMPROPERLY TIMED GEARS TRAINS COULD RESULT IN ENGINE DAMAGE AND STOPPAGE. 1L72 3O3 O A1EA 1E12 20010802002362001080200236EA 2001 8 2 2001FA0000156 220010514G7314RG9570R1 PUMP PWA PT6 PT6A6 52043EA ENGINE LEAKING B D RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SW99451DM164 PCEPRO212 PILOT REPORTED FUEL SMELL IN CABIN, LATER NOTIFIED FUEL LEAKING FROM ENGINE COMPARTMENT. TECHNICIAN FOUND LOW PRESSURE FUEL PUMP LEAKING AT RELIEF AND SCREWS LOOSE. PUMP REMOVED AND REPLACED WITH NEW UNIT. (REFERENCE TEXTRON LYCOMING AD 98-18-12 AND TEXTRON LYCOMING SERVICE BULLETIN 529 DEALS WITH SAME PROBLEM FOUND WITH THIS PUMP OF SAME CRANE/LEARROMEC "AN" ROTARY FUEL PUMP MODEL SERIES.) 3 T E4EA 20010802002392001080200239GL 2001 8 2 2001FA0000157 320010517G6110 SNAP RING BEECH 58 58 1152740CE CONT O550 IO550C SO MCAULY3AF32C3AF32C512 GL BLADE TO HUB DAMAGED B K NONE P NO WARNING INDICATION ININSP/MAINT 1 SO11818JC59 59 TH1620 L676535 L901873 THE AFOREMENTIONED AIRCRAFT ARRIVED FOR ENGINE OIL & FILTER CHANGE. UPON COMPLETION OF SERVICE, A PRE-ENGINE RUN / WALK AROUND INSPECTION WAS PERFORMED. DURING THIS WALK AROUND INSPECTION THERE WAS A CONSIDERABLE AMOUNT OF EXCESSIVE PLAY NOTED IN ONE OF THE RT PROPELLER BLADES. REMOVED THE RT PROPELLER SPINNER ASSEMBLY FOR FURTHER INVESTIGATIONS AND NOTED THE SNAP RING THAT SECURES THE BLADE INTO THE PROPELLER HUB ASSEMBLY TO BE PARTIALLY INTACT WITH A SMALL PORTION ACTUALLY SECURING BLADE IN THE HUB ASSEMBLY. THE PROPELLER WAS IMMEDIATELY REMOVED AND ROUTED TO THE PREVIOUS OVERHAUL FACILITY FOR INSPECTION AND REPAIR. PROPELLER TSO: 51.9.PROBABLE CAUSE: IT APPEARS THAT THE SECURING SNAP RING WAS NOT CORRECTLY 1L72 3O3 O 3A16 E3SO 5 CP22EA 20010802002422001080200242CE 2001 8 2 2001FA0000158 120010522G30102H598 VALVE CESSNA310 T310R 2074246CE DEICE SYSTEM INOPERATIVE D K NONE O OTHER ININSP/MAINT 1 SW99310KH 310R1507 DURING INSTALLATION OF AIRCRAFT SURFACE KNOWN ICE KIT FOUND SURFACE DEICE FLOW VALVE #2H59-8 (MFG. BY PARKER HANNIFIN, AIRBORNE) S/N 9AT-83 TO CAUSE UNCOMMANDED DEICE BOOT INFLATIONS. INSTALLED SECOND NEW VALVE S/N 9AT-91 OBTAINED FROM A DIFFERENT DISTRIBUTOR WITH SAME RESULTS. SPOKE WITH AIRBORNE TECH SUPPORT AND WAS GIVEN A MANUFACTURES POST ASSEMBLY INSPECTION TEST PROCEDURE. TESTED THREE MORE VALVES FROM VARIOUS DISTRIBUTORS S/N 9AT-85, 6AT-48, 6AT-55 AND VARIFIED BOTH VISUALLY AND OPERATIONALLY THAT ALL WERE DEFECTIVE. DEFECT CAN BE SEEN AT TOP OF VALVE WHERE SOLENOID PLATE IS RIVETED TO BODY. A LARGE GAP EXISTS ALLOWING PRESSURE AIR ESCAPE CAUSING VALVE ACTUATION. NO ADDITIONAL SUPPLY OF VALVES AVAIL1L72 3O 3A10 20010802002442001080200244CE 2001 8 2 2001FA0000159 120010501G81204709089011 WASTEGATE VALVE CESSNA206 TU206G 2073357CE CONT O520 TSIO520M 17040SO ENGINE EXHAUST UNDERTORQUED D K NONE O OTHER ININSP/MAINT 1 SW99 FOUND THE 7 ACTUATOR TO BYPASS VALVE MOUNTING BOLTS (REF. GARRETT MANUAL TP30-4001-1 PG. 10-11 ITMES NR 7 AND 10) WITH LITTLE TO NIL MEASURABLE TORQUE. THIS IS THE SECOND ACTUATOR ON WHICH WE HAVE DISCOVERED THIS PROBLEM. DURING INSTALLATION INSPECTION, A WRENCH JUST HAPPENED TO BE PLACED ON THESE BOLTS WHICH WERE THEN OBSERVED TO BE LOOSE. 1H71 3O3 O A4CE E8CE 20010802002452001080200245EA 2001 8 2 2001FA0000160 220010604G8530RL499751A CYLINDER LYC O360 IO360B1E 41514EA ENGINE SEPARATED G O OTHER Y ENGINE STOPPAGE CLCLIMB 1 SW013708T3500 THE NUMBER ONE CYLINDER HEAD SEPERATED FROM THE CYLINDER RESULTING IN AN ACCIDENT DESTROYING THE AIRCRAFT AND INJURING THE PILOT. NOTE: THE ENGINE EXCEEDED THE MANUFACTURERS CALENDER TBO OF 12 YEARS AND 2000 HOURS. 3 O 1E10 20010802002462001080200246EU 2001 8 2 2001FA0000161 120010608G7100UAE651 SEAL AMD FALCONFALCON20 2730103EU LEFT ENG PYLON BROKEN C E ENGINE SHUTDOWN L NO TEST ININSP/MAINT 1 EA01 9728 325 WHILE PERFORMING POST MAINTENANCE ENGINE RUN FOR AN UNRELATED ACTION, THE LEFT ENGINE FAILED TO RESPOND TO THROTTLE MOVEMENT. UPON FURTHER INVESTIGATION THE LEFT ENGINE TORSION TUBE ASSY (P/N MY20571-53810) WAS FOUND BROKEN APPART INSIDE THE ENGINE PYLON BETWEEN FUSELAGE STATION FR31 AND FR32. THE BREAK WAS LOCATED AT THE INBOARD SECTION OF THE TORSION TUBE IDENTIFIED AS A "SEAL" AS SHOWN IN FALCON 20 IPC CHAP, 76-10-20, PAGE 50-0, ITEM 50, P/N UAE651. INTEGRATED INTO THIS PART IS A METAL "UNIVERSAL-JOINT TYPE CONFIGURATION WHICH HAD CRACKED COMPLETELY THROUGH. 2L72 4F RTA7EU 20010808003182001080800318SW 2001 8 8 2001FA0000163 220010803G85204109 STUD WACO YMF YMF 9600412EA JACOBPR755 R755* 35006SW NR 4 CYLINDER BROKEN D K NONE O OTHER ININSP/MAINT 1 WP0753WC 252 FSC062 FOUND BROKEN CYLINDER BASE STUD ON NR 4 CYLINDER. AFTER REMOVING BROKEN STUD, FOUND TWO OTHERS BENT, SENT STUDS FOR EVALUATION TO SEE IF THEY MET DESIGN INTENT. THE STUDS DID NOT MEET SPECIFICATIONS. 1Q71 3R3 R ATC542 TC237 20010807000042001080700004 2001 8 7 2001FA0000164 420010425G6113055032110 BULKHEAD CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA MCAULY1A170 1A170E GL PROP SPINNER CRACKED D K NONE O OTHER ININSP/MAINT 1 AL03430CP42 172S8692 L2938051A UPON A POSTFLIGHT INSPECTION, THE PROPELLER SPINNER BULKHEAD ASSEMBLY WAS DISCOVERED CRACKED. THE CORNER PORTION OF THE BULKHEAD WAS COMPLETELY RIPPED AWAY AND THE EDGE OF THE SPINNER WAS PEELING UP. PROBABLE CAUSE: MANUFACTURING DEFECT SUSPECTED. 1H71 3O3 ONT3A12 1E10 5 NP857 20010807000032001080700003CE 2001 8 7 2001FA0000165 120010804G2460727725 CIRCUIT BREAKER BEECH 1900 1900D 1154162CE COCKPIT FAILED B A UNSCHED LANDING BG SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE CRCRUISE 1 SW9984802 UE53 DURING FLIGHT, SMOKE WAS OBSERVED COMING FROM THE REAR OF A CB PANEL. CB'S PULLED PROGRESSIVELY TO IDENTIFY ONE CAUSING SMOKE. OTHERS RESET AFTER ISOLATING FAULTY ONE. AIRCRAFT LANDED. ON GROUND, FAILED CB REPLACED. FURTHER TROUBLE SHOOTING REVEALED. POWER WIRE TO WING ICE INSPECTION LIGHT CHAFFED AGAINST STRUCTURE NEAR LIGHT ASSY. WIRE REPAIRED. 2L72 4T RTA24CE 20010808003192001080800319GL 2001 8 8 2001FA0000166 220010531G73232526146 BEARING HONEYWELL SKRSKYS76 S76 8143010NE ALLSN 250C 250C20B 03013GL PT GOVERNOR DISINTEGRATED Z K NONE O OTHER ININSP/MAINT 1 WP23PTYDC 652 BR31687 760220 SPOOL BEARING ASSEMBLY DISINTEGRATED. INNER AND OUTER RACES ARE ALL THAT REMAINS. NEARLY ALL EVIDENCE OF BALLS FROM BEARING MISSING. REASON FOR FAILURE POSSIBLY DUE TO BEARING BALL RETAINER FAILURE. 1G72 3U3 U H1NE E4CE 20010808003212001080800321EA 2001 8 8 2001FA0000167 220010201G8520SL13885 MAIN BEARING CESSNA185 A185E 2072818CE LYC O540 TIO540* 41532EA ENGINE DELAMINATED D K NONE O OTHER ININSP/MAINT 1 WP19694BK54 1851582 L474361A DURING SCHEDULED OIL AND FILTER CHANGE ON ENGINE REFERENCED, FOUND BEARING PARTICLES WITHIN OIL FILTER. DISASSEMBLED ENGINE TO FIND FRONT MAIN BEARING EXHIBITING DELAMINATION OF THE LINER SURFACE. FAULTY MANUFACTURING OF BEARING IS SUSPECT. 1H71 3O3 O 3A24 E14EA 20010816000962001081600096CE 2001 8 16 2001FA0000168 120010803G3230358250944 PLUNGER BEECH 56 56TC 1152736CE LYC O541 TIO541E1B4 41536EA NLG FAILED G A UNSCHED LANDING O OTHER TOTAKEOFF 1 SW015455U TG22 PILOT DEPARTED SANTA FE, NM AND RETRACTED GEAR. THE TOWER NOTICED THE NOSE GEAR STILL HANGING DOWN. PILOT LOWERED GEAR, THE MAINS LOCKED DOWN BUT THE NOSE DID NOT LOCK DOWN. PILOT LANDED AND THE NOSE GEAR COLLAPSED. THE AFT END ATTACH FITTING OF THE PLUNGER ASSEMBLY (P/N 35-825094-4) FAILED. TOTAL TIME AND CYCLES ON THE NOSE GEAR IS UNKNOWN. 1L72 3O3 O 3A16 E10EA 20010808003262001080800326 2001 8 8 2001FA0000169 420010710G2561KS9P0Z01 LIFE VEST CABIN FAILED B KQ1RK NONE O OTHER ININSP/MAINT 1 EA07 LIFE VEST FAILED MFG RECOMMENDED 2 PSI INFLATION TEST I/A/W MANUAL 25-60-1 DOM: NOVEMBER 1982 20010808003292001080800329SO 2001 8 8 2001FA0000170 120010706G7722481389 PROBE PIPER PA46 PA46350P SO LYC O540 TIO540AE2A 41532EA TIT SYSTEM FAILED D O OTHER O OTHER NRNOT REPORTED 1 WP15135CC49 4636192 L1012361A PART FAILED IN 49 HOURS. THIS PART IS REPLACED DURING AN AD REQUIREMENT EVERY 250 HOURS BUT ONLY LASTED 49 HOURS. 1L71 3O3 ORTA25SO E14EA 20010808003332001080800333CE 2001 8 8 2001FA0000171 120010706G2810S23591 CHECK VALVE CESSNA172 172R 2072401CE LT FUEL TANK MISINSTALLED C O OTHER K FLUID LOSS NRNOT REPORTED 1 WP09361ES1731 17280011 WHEN FUEL TANKS WERE FILLED TO ABOVE 35 GALLONS, HIGH AMBIENT TEMPERATURE CAUSED FUEL TO LEAK FROM VENT TUBE. REMOVED LEFT FUEL BAY INSPECTION PLATE AND FOUND THAT THE FUEL VENT TUBE INVERTED CHECK VALVE S2359-1 ALSO INVERTED FROM FACTORY. ROTATED 180 DEGREES TO CURRENT POSITION. INSPECTION PLATE SHOWED NO SIGN OF EVER BEEN REMOVED. 1H71 3O NT3A12 20010808003362001080800336CE 2001 8 8 2001FA0000172 120010615G5210051701912 HINGE PIN CESSNA172 172R 2072401CE CABIN DOOR BROKEN B K NONE O OTHER ININSP/MAINT 1 EA07172WY1722 17280334 DURING A PHASE II INSPECTION, FOUND LEFT AND RIGHT LOWER CABIN DOOR HINGE PINS, BROKEN. IT APPEARS THAT THE CABIN DOOR WAS NOT INSTALLED PROPERLY FROM THE FACTORY, CAUSING UNDUE STRAIN ON LOWER HINGES. 1H71 3O NT3A12 20010808003392001080800339WP 2001 8 8 2001FA0000173 120010607G6510 DRIVE SHAFT ROBSINR22 R22 7640102WP TAIL ROTOR FAILED F YV3RK NONE O OTHER TXTAXI/GRND HDL 1 WP05 DURING RUN-UP PRIOR TO TAKE-OFF, AN R22 TAIL ROTOR DRIVE CUT LOOSE AND SEVERED THE TAIL BOOM. HELICOPTER WAS ABOUT TO FLY TO A MAINTENANCE FACILITY FOR 100 HOUR INSPECTION. PRELIMINARY SURVEY INDICATES THAT THE INCIDENT WAS INITIATED BY THE TAIL ROTOR DRIVE SHAFT DAMPER BREAKING OFF INSIDE THE TAIL BOOM. THIS ALLOWED THE DRIVE SHAFT TO WHIP, FRACTURE, AND CUT OFF THE TAIL BOOM. 1G71 3O H10WE 20010808003402001080800340EA 2001 8 8 2001FA0000174 120010601G492032020725 CHECK VALVE CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF341A NE APU DAMAGED D K NONE O OTHER ININSP/MAINT 1 SW05604MU 5406 DURING REPLACEMENT OF THE CHECK VALVE, FOUND PIECES OF CHECK VALVE FLAPPERS, REPLACED WITH PN 320-2832-1-1 SN 635 OPERATIONAL CHECKED SATISFACTORY. NOTE: ALL PIECES REMOVED. 2L72 4F4 FRTA21EA E15NE 20010808003412001080800341CE 2001 8 8 2001FA0000175 120010530G7120241302411 BRACKET CESSNA172 172RG 2072438CE LYC O360 VO360* 41514EA ENGINE MOUNT CRACKED D K NONE O OTHER ININSP/MAINT 1 GL119578B6324 172RG0895 DURING ENGINE CHANGE, THE ENGINE MOUNT WAS REMOVED FOR INSPECTION. MOUNT WAS REMOVED FOR INSPECTION. THE FIREWALL ATTACH POINTS FOR THE ENGINE MOUNT WERE THEN INSPECTED. THE UPPER LEFT BRACKET WAS FOUND CRACKED AT THE ENGINE MOUNT BOLT HOLE. THE BRACKET INBOARD 2 RIVETS THAT ATTACH IT TO THE LONGERON HOT SECTION WERE MISSING. SUSPECT THIS CAUSED THE CRACK. 1H71 3O3 O 3A17 1E1 20010808003422001080800342SO 2001 8 8 2001FA0000176 120010627G3233SFA2325 ACTUATOR PIPER PA32 PA32RT300T 7103216SO LYC O540 TIO540* 41532EA MLG LEAKING D K NONE K FLUID LOSS NRNOT REPORTED 1 WP233620255 32R7887028 L5351UA ACTUATOR LEAKS FLUID FROM SHAFT SEAL. SEAL PN 762-084 WAS FOUND SPLIT ON I.D. 1L71 3O3 O A3SO E14EA 20010810001552001081000155EA 2001 8 10 2001FA0000177 220010713G8540LW10284 GEAR PIPER PA31 PA31350 7103110SO LYC O540 LTIO540* 41533EA ENGINE BROKEN B DECRO OTHER O OTHER NRNOT REPORTED 1 GL193556F883 318052066 ONE TOOTH ON GEAR SEPARATED AND LODGED BETWEEN CRANKSHAFT GEAR AND OIL PUMP HOUSING. THIS CAUSED THE REMAINING TEETH OF THE CRANKSHAFT GEAR TO ROUND OFF AND DISENGAGE FROM THE OTHER GEARS. THIS ALSO CAUSED 2 IDLER GEARS AND THE OIL PUMP DRIVE GEAR TO SHEAR SEVERAL TEETH AS WELL. 1L72 3O3 O A20SO E14EA 20010810001562001081000156SW 2001 8 10 2001FA0000178 120010611G32331020004 ACTUATOR MOONEYM20 M20M 5870222SW LANDING GEAR FAILED D O OTHER J WARNING INDICATION NRNOT REPORTED 1 GL09321JL741 270162 ACTUATOR FAILED BOTH MANUALLY AND ELECTRICALLY RESULTING IN A GEAR UP LANDING. 1L71 3O RT2A3 20010810001582001081000158CE 2001 8 10 2001FA0000179 120010808G716005521644 AIR BOX CESSNA172 172N 2072434CE LYC O320 O320* 41508EA ENGINE DAMAGED B EL6RK NONE O OTHER ININSP/MAINT 1 EA23737MP 17269524 NOTED: DURING ANNUAL INSPECTION, CARBURETOR AIR BOX OUTLET/INLET FOR CARBURETOR HEAT SWEDGED ONTO AIR BOX. ROUND METAL FLANGE VIBRATING AND CHAFING WHERE SWEDGING DONE. GETS LOOSE AND CHAFES ITSELF TO PIECES. COULD EVENTUALLY BREAK, ALLOWING HOSE TO FALL OFF AND CARBURETOR TO INGEST THIN PIECES OF METAL. 1H71 3O3 ONT3A12 E274 20010810001592001081000159NE 2001 8 10 2001FA0000180 220010709G7321 FUEL CONTROL CESSNA500 500CESSNA 2076602CE PWA JD15 JT15D1A NE RT ENGINE MALFUNCTIONED D A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 EA0788GJ 5000155 PCE76335 DURING A CLIMB THROUGH FL 290, THE RIGHT ENGINE FAN SPEED DECREASED TO 82 PERCENT. ENGINE IGNITION WAS SELECTED ON TO NO EFFECT. AN EMERGENCY WAS DECLARED AND A SAFE LANDING WAS MADE. SUSPECT THAT THE FUEL CONTROL UNIT MALFUNCTIONED. 1L72 4F4 F A22CE E25EA 20010810001612001081000161EA 2001 8 10 2001FA0000181 220010516G855006B23072 GASKET CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA ENGINE DEFECTIVE D O OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP19737TC 17269654 L446076 AD 200-18-23 WAS C/W BY INSTALLING NEW GASKET PT 06B23072 UNDER OIL FILTER ADAPTER PLATE. WITHIN 34 HOURS, GASKET BLEW OUT AND ALL THE OIL WAS BLOWN OUT. AIRCRAFT RETURNED TO AIRPORT SAFELY. INSPECTION OF GASKET REVELED THAT THE RUBBER GASKET HAD DISSOLVED AND BECAME VERY SOFT. A NEW GASKET WAS INSTALLED AS PER INSTRUCTIONS IN THE SB 543A, NO FURTHER PROBLEMS HAVE BEEN ENCOUNTERED WITH THIS AIRCRAFT. 1H71 3O3 ONT3A12 E274 20010810001672001081000167CE 2001 8 10 2001FA0000182 120010614G3710653487 GASKET CESSNA182 182S 2072701CE LYC O540 IO540AB1A5 EA VACCUUM PUMP MISSING D K NONE K FLUID LOSS ININSP/MAINT 1 EA25132ME276 18280690 L2728048A WHILE PERFORMING AN ANNUAL INSPECTION ON THIS AIRCRAFT, AND OIL LEAK WAS NOTICED COMING FROM THE LOWER VACUUM PUMP DRIVE PAD. FURTHER INSPECTION REVEALED THAT THE GASKET FOR THE PUMP WAS MISSING. A NEW GASKET WAS INSTALLED AND A LEAK CHECK WAS PERFORMED. 1H71 3O3 ONT3A13 1E4 20010810001872001081000187EA 2001 8 10 2001FA0000185 120010423G2750 FLAP BLANCA1413 14132 1201004EA FRNKLN6A41506A4150B3 27024EA LT WING DEPARTED C O OTHER D INFLIGHT SEPARATION APAPPROACH 1 WP0774285 1398 13505 LT FLAP SEPARATED FROM A/C AT ABOUT 500 FT WHILE TURNING DOWNWIND TO AIRPORT. A/C WAS BEING CONFIGURED FOR LANDING AT THE TIME OF SEPARATION. 80 MPH GEAR DOWN AND THE FLAP HANDLE WAS PULLED FOR FULL FLAP. AN IMPULSE WAS FELT IN THE HANDLE WHICH I FIRST THOUGHT WAS A BROKEN FLAP CABLE AND IMMEDIATELY RETRACTED THE FLAPS OR IN THIS CASE THE FLAP. THE A/C WAS STABLE AND CONTROLLABLE SO MORE POWER WAS ADDED AND LANDED FASTER THAN NORMAL. MOISTURE HAD COLLECTED IN THIS AREA AND COMPROMISED THE WOOD AND GLUE CAUSING THE FAILURE OF THE OUTBOARD HINGE RIB, INSPECTION AT THIS AREA IS ONLY POSSIBLE BY CUTTING A HOLE. THE INBOARD RIB OF THE FLAP FAILED, THIS WAS SECONDARY AFTER THE OUTBOARD HINGE SEPARATED FROM THE WING.1L71 3O3 O A773 E238 20010816000982001081600098CE 2001 8 16 2001FA0000186 120010809G571257222062 RIB CESSNA441 441 2076020CE RT WING CRACKED B K NONE O OTHER ININSP/MAINT 1 AL05441DB 4410300 DURING A SCHEDULED INSPECTION THE LEFT AND RIGHT CANTED RIB CAPS P/N 5722206-1 AND 5722206-2 WERE FOUND CRACKED APPROXIMATELY 1 INCH BEHIND THE FORWARD SPAR. WHILE ACCOMPLISHING THE REPAIR TO THIS AREA, ANOTHER CRACK WAS FOUND IN THE LEFT WING/FUSELAGE CLOSEOUT P/N 6720001-3. THE CLOSEOUT CANNOT BE SEEN UNTIL THE WING FAIRINGS ARE REMOVED, THUS IT CANNOT BE SEEN DURING NORMAL INSPECTION. 1L72 3T RTA28CE 20010816000992001081600099CE 2001 8 16 2001FA0000187 120010810G5720 ANGLE CESSNA441 441 2076020CE WING CRACKED C K NONE O OTHER ININSP/MAINT 1 AL05441JC 4410156 DURING A SCHEDULED INSPECTION, THE LEFT CANTED RIB CAP P/N 5722206-1 WAS FOUND CRACKED APPROXIMATELY 1 INCH AFT OF THE FORWARD WING SPAR. WHILE REPAIRING THIS CRACK THE UPPER WING TO FUSELAGE CLOSEOUT ANGLE P/N 5720001-3 WAS FOUND CRACKED. THESE CLOSEOUT ANGLES CANNOT BE SEEN UNLESS THE WING TO FUSELAGE FAIRINGS ARE REMOVED AND THUS ARE NEVER INSPECTED DURING NORMAL MAINTENANCE. 1L72 3T RTA28CE 20010816001002001081600100SO 2001 8 16 2001FA0000188 120010810G7430103572101 IGNITION SWITCH PIPER PA28 PA28180 7102808SO LYC O360 O360A4A 41514EA INSTRUMENT PANELFAILED D K NONE O OTHER TXTAXI/GRND HDL 1 SO06 A NEW SWITCH WAS INSTALLED TO COMPLY WITH AD 76-07-12. THE NEW SWITCH WOULD NOT ENERGIZE THE STARTER CONTACTOR. A SECOND SWITCH WAS ORDERED. 1L71 3O3 O 2A13 E286 20010820000312001082000031EA 2001 8 20 2001FA0000189 220010720G852072877 LIFTER PIPER PA28 PA28140 7102802SO LYC O320 O320E3D 41508EA ENGINE BROKEN D K NONE O OTHER ININSP/MAINT 1 NM078715E2600 287625149 L4434627A DURING TEAR DOWN FOR OVERHAUL A PIECE OF METAL WAS FOUND IN OIL SUMP. FURTHER INSPECTION FOUND THAT THE HEAD OF LIFTER BODY FOR NR 1 CYLINDER EXHAUST VALVE WAS HALF GONE. (PIECE IN OIL SUMP) FROM WEAR ON REMAINING PART, APPEARS THAT IT HAD BEEN THAT WAY FOR SEVERAL HOURS. PART HAD AT LEAST 2600 HOURS SINCE OVERHAUL. 1L71 3O3 O 2A13 E274 20010820000322001082000032EA 2001 8 20 2001FA0000190 220010720G8530SL17540 EXHAUST VALVE PIPER PA28 PA28140 7102802SO LYC O320 O320E3D 41508EA ENGINE BROKEN D A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 NM078715E2600 2600 287625149 L4434627A AIRCRAFT WAS ON A TRAINING FLIGHT, STEM BROKE AT VALVE HEAD. ENGINE LOST POWER BUT WAS ABLE TO LAND. ENGINE CHANGED. PROBABLE CAUSE OF BREAKAGE: OLD AGE. 1L71 3O3 O 2A13 E274 20010820000332001082000033CE 2001 8 20 2001FA0000191 120010817G711217500117 SHROUD CESSNA172 172N 2072434CE LYC O320 O320* 41508EA ENGINE CHAFED B EL6RK NONE O OTHER ININSP/MAINT 1 EA23737MP 17269524 NOTED: DURING ANNUAL INSPECTION ON NUMEROUS AIRCRAFT, SCREEN INSIDE OF CARB HEAT SHROUD VIBRATING AND CHAFING ITSELF TO PIECES BE ALLOWED TO BE SUCK INTO THE CARB INLET. (SHROUD LOCATED ON CYLINDER STACK ASSEMBLY WITH CLAMPS). 1H71 3O3 ONT3A12 E274 20010821000252001082100025 2001 8 21 2001FA0000192 420010820G2561P0723105 LIFE VEST CABIN FAILED B KQ1RK NONE O OTHER ININSP/MAINT 1 EA07 LIFE VEST FAILED, MANUFACTURE RECOMMENDED 2 PSI CELL TEST IAW 21-60-7. DATE OF MFG. SEPT 1986. 20010821000262001082100026EA 2001 8 21 2001FA0000193 220010730G8520LW13818 CRANKCASE PIPER PA28 PA28R201 7102816SO LYC O360 IO360C1C 41514EA ENGINE CRACKED D K NONE K FLUID LOSS ININSP/MAINT 1 WP279235G 2837055 L2545951A AT INSPECTION AN AREA OF OIL IS NOTICED BEHIND PROP- IT APPEARS TO LOOK LIKE THE SPLIT CASE SEAM IS LEAKING. CLEAN AREA AND USE NDT DEVELOPER. RUN-UP PLANE AND CRACK APPEARS. THERE ARE SEVERAL STYLES OF CASE FOR THIS ENGINE. BUT ON A CERTAIN STYLE SEEMS TO CRACK. 1L71 3O3 O 2A13 1E10 20010821000272001082100027SW 2001 8 21 2001FA0000194 120010806G302019940 CONTROL ARM BBAVIA8 8GCBC 1220803SW LYC O360 VO360* 41514EA ENGINE FAULTY B RJWRO OTHER O OTHER NRNOT REPORTED 1 GL15437AC182 39398 WHEN MOVING CARBURETOR HEAT CONTROL, CARB HEAT CONTROL ARM (PN 1-9940) CONTACTS JAM NUT ON THE THROTTLE CONTROL ROD CLEVIS (PN A31800), MOVING THE THROTTLE OUT OF POSITION. 1H71 3O3 O A21CE 1E1 20010823000152001082300015NE 2001 8 23 2001FA0000195 220010703G8530366249 CYLINDER AIRTRCAT300 AT301 0390103SW PWA R1340 R1340* 52016NE ENGINE CRACKED D K NONE O OTHER ININSP/MAINT 1 CE073164H6375 3010539 THE NR 3 CYLINDER HEAD CRACKED AT THE ROCKER BOSS, ENGINE LOST POWER, AIRCRAFT EMERGENCY LANDED IN A FIELD. 2ND OCCURANCE. 1L71 3R3 R A9SW 5E2 20010823000222001082300022SO 2001 8 23 2001FA0000196 220010724G8500 ENGINE BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO ENGINE BAY FAILED B CGORK NONE O OTHER ININSP/MAINT 1 GL035688K 200 TC765 1921768LR PILOT REPORTED SEVERE ENGINE VIBRATION FOLLOWING POWER REDUCTION ON INITIAL CLIMB-OUT AFTER DEPARTURE FROM AIRPORT. ENGINE SHUTDOWN AND FEATHERED. NOTED CATASTROPHIC LEFT ENGINE FAILURE UPON INITIAL INSPECTION. NR 5 CONNECTING ROD OBSERVED WITH CLEAN BREAK THROUGH LARGE HOLE IN CRANKCASE; NR 6 CONNECTING ROD SEVERELY BENT. NR 5, NR 6 PISTONS DAMAGED SEVERELY AND SEIZED IN CYLINDERS. OBSERVED CAMSHAFT BROKEN; FOUND PISTON PIN LOOSE WITH OTHER CRANKCASE AND CYLINDER BROKEN PARTS. EXACT FAIL MODE UNDETERMINED. ENGINE RECORDS NOT SUPPLIED. 1L72 3O3 ORT3A16 3E1 20010823000242001082300024EU 2001 8 23 2001FA0000197 220010616G8550956470 LINE DIAMONDA20 DA20A1 GL ROTAX 912 ROTAX912 55555EU OIL SUCTION BROKEN G K NONE O OTHER ININSP/MAINT 1 SO15442PC 10042 4412740 OIL SUCTION LINE/ NR 3 CONNECTING ROD BROKE AT CRANKSHAFT. ROD PROTRUDED THROUGH ENGINE CASING. SB ADDRESSES SUBJECT OIL LINES TO BE INSPECTED FOR KINKS AND SHARP BENDS. ALSO, NONCOMPLIANCE COULD RESULT IN ENGINE DAMAGE. SUSPECT THAT OIL MAY HAVE BEEN RESTRICTED FROM ENTERING INTO ENGINE CASING DUE TO DEFECTIVE OIL LINES. DEFECTIVE OIL LINES. RECOMMEND AD AT 100 HR INTERVALS. 1L71 3O3 INTTA4CH EXPE3I 20010823000262001082300026EU 2001 8 23 2001FA0000198 220010616G8550956476 LINE DIAMONDA20 DA20A1 GL ROTAX 912 ROTAX912 55555EU OIL PRESS DEFECTIVE G K NONE O OTHER ININSP/MAINT 1 SO15442PC 10042 4412740 OIL PRESSURE LINE-NR 3 CONNECTING ROD BROKE AT CRANKSHAFT. ROD PROTRUDED THROUGH ENGINE CASING. SERVICE INSTRUCTION ADDRESSES SUBJECT OIL LINES TO BE INSPECTED FOR KINKS AND SHARP BENDS. ALSO, NONCOMPLIANCE COULD RESULT IN ENGINE DAMAGE. SUSPECT OIL MAY HAVE BEEN RESTRICTED FROM ENTERING INTO ENGINE CASING DUE TO DEFECTIVE OIL LINES. RECOMMEND AD AT 100 HR INTERVALS. 1L71 3O3 INTTA4CH EXPE3I 20010823000272001082300027CE 2001 8 23 2001FA0000199 120010711G323398820152 ACTUATOR CESSNA172 172RG 2072438CE MLG CRACKED B LW5TK NONE O OTHER ININSP/MAINT 1 GL179515B4503 172RG0846 BOTH ACTUATORS WERE INSPECTED IAW SB, CRACKS WERE FOUND IN THE AREA THAT ACCOMPLISHMENT INSTRUCTIONS INDICATED. PARTS WERE REMOVED FROM SERVICE. 1H71 3O 3A17 20010830010692001083001069SW 2001 8 30 2001FA0000200 120010712G2842206379006101 TOTALIZER BELL 206 206L1 1182107SW ALLSN 250B 250B* GL FUEL SYS INTERMITTENT D A UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL21656NA 45391 TOT INDICATOR RED LIGHT FLASHED ON INTERMITTENTLY CAUSING PILOT TO MAKE PRECAUTIONARY LANDING. 1G71 3U3 T H2SW E10CE 20010823000742001082300074CE 2001 8 23 2001FA0000202 120010627G32305081032019 SOCKET BEECH 1900 1900D 1154162CE TORQUE ARM CRACKED B K NONE O OTHER ININSP/MAINT 1 SO19 9947 DURING LIQUID PENETRANT INSPECTION IAW MM NDT WE HAVE FOUND CRACKS ON THE LOWER LUGS WERE THE TORQUE ARM ATTACHED, DEPTH OF CRACKS ARE UNKNOWN, BUT VISUAL INSPECTION WILL REVEAL CRACKS WITH ANY USE OF MAGNIFICATION DEVICES OR PENETRANT DYE. WHEN WE RECEIVED UNITS, THEY NEVER HAVE THE DASH NUMBER JUST THE SERIES 50-810320. ALL SOCKETS SHOULD BE CONSIDERED. CAUSE IS UNKNOWN. 2L72 4T RTA24CE 20010823000752001082300075SO 2001 8 23 2001FA0000206 220010815G74141051324 SPRING CONT CESSNA206 TU206G 2073357CE CONT O520 TSIO520M 17040SO IMPULSE COUPLINGBROKEN D K NONE O OTHER ININSP/MAINT 1 SW99PK-MP11 E189909FR U20605864 818029R THE MAGNETO IMPULSE COUPLING SPRING BROKE ABOUT 6 INCHES FROM THE OUTER END OF THE SPRING. THE FAILURE WAS DISCOVERED BECAUSE THE IMPULSE COUPLING WOULD NOT ENGAGE DURING THE ENGINE STARTING PROCESS. 1H71 3O3 O A4CE E8CE 20010823000812001082300081CE 2001 8 23 2001FA0000207 120010815G3397LF11 WIRE CESSNA208 208 2073702CE BEACON CHAFED D K NONE L NO TEST ININSP/MAINT 1 SW999Q-CA9647 20800010 WIRES LF11 AND LF12 ARE ROUTED THROUGH THE VERTICAL STABILIZER WITHOUT PROTECTION OR SUPPORT. THESE WIRES POWER THE FLASHING RED BEACON MOUNTED ON THE TOP OF THE FIN. BOTH WIRES CHAFED AGAINST THE EDGE OF THE HOLE IN THE STABILIZER RIB THROUGH WHICH THEY WERE ROUTED AND WORE THROUGH THE INSULATION CAUSING A SHORT CIRCUIT AND THE BREAKER TO OPEN. 1H71 3T NTA37CE 20010823000822001082300082GL 2001 8 23 2001FA0000208 120010810G320112446105 FAIRING CIRRUSSR SR20 05628AJGL NLG LOOSE B ESMRK NONE O OTHER ININSP/MAINT 1 SO11747CD69 0047 BRACKETS THAT HOLD THE NOSE WHEEL FAIRING TO THE NOSE GEAR FORK PART NUMBER 1799-001, ARE HELD TO THE FORK BY BOLTS THAT ARE NOT DRILLED FOR SAFETY WIRE, THEY DO NOT THREAD INTO SELF LOCKING NUTS PLATES, NOR DO THEY CALL OUT FOR LOCK WASHERS. THE BOLTS LOOSEN UP, THE FAIRING MOVES AROUND, AND LEAVES THE AIRPLANE. EXAMINED OTHER SAME MODEL AIRCRAFT, AND FOUND LOOSE FAIRINGS. BROUGHT THIS CONDITION TO THE OPERATORS ATTENTION. CONDITION NOTED BY: JACK D. TOBIN A&P 2250313. 1H71 3O NCA00009CH 20010823000832001082300083NE 2001 8 23 2001FA0000209 220010822G853011874 PUSHROD PWA R1340 R1340AN1 52016NE EXHAUST FAILED G ISSGA UNSCHED LANDING Y ENGINE STOPPAGE NRNOT REPORTED 1 GL27 21730 ENGINE FAILED DUE TO FAILURE OF NR 1 EXHAUST PUSHROD. UNEVENTFUL LANDING MADE. 3 R 5E2 20010831000052001083100005GL 2001 8 31 2001FA0000210 320010717G6111FC8477A4 BLADE HARTZLHCC2Y HCC2YK2 GL PROPELLER CRACKED B ME4RAE UNSCHED LANDING ENGINE SHUTDOWN RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CLCLIMB 1 SO19 835 AU3069E PILOT REPORTED ON TAKE OFF THAT THE PROPELLER WOULD NOT MAKE FULL POWER. PILOT RETURNED TO THE FIELD. PRIOR TO TOUCHDOWN, PILOT EXPERIENCED A VIBRATION. IMMEDIATELY AFTER TOUCHDOWN, THE VIBRATION INCREASED SIGNIFICANTLY, AND THE ENGINE SHUT DOWN. A FIELD INSPECTION REVEALED THE PROPELLER TO BE OUT OF TRACK OVER ONE INCH (1 IN). THE PROPELLER WAS REMOVED AND SENT FOR INSPECTION/ EVALUATION. UPON DISASSEMBLY OF THIS PROPELLER A VISUAL INSPECTION REVEALED A LARGE CRACK APPROXIMATELY 270 DEGREES AROUND THE NR 2 BLADE SHANK. THE HUB APPEARS TO BE CRACKED IN THE NR 2 BLADE ARM AS WELL. 5 CP920 20010905000482001090500048CE 2001 9 5 2001FA0000211 120010808G1100 PLACARD CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA CARBURETOR FOD C O OTHER CR F.O.D. PARTIAL RPM/PWR LOSS LDLANDING 1 GL096746442 42 15281850 L1402115 DURING TOUCH AND GO LANDING AS CARB HEAT WAS APPLIED, ENGINE LOST POWER. REMOVING CARB HEAT DID NOT IMPROVE PERFORMANCE. DURING INVESTIGATION AND CARB REMOVAL, FOUND STARTER LUBRICATION DECAL LODGED IN VENTURI. AFTER REMOVAL AND REINSTALLATION OF CARB. ENGINE POWER RETURNED TO NORMAL. RECOMMEND THESE DECALS BE REMOVED PRIOR TO STARTER AND CARBURETOR INSTALLATION ON ENGINE. ( FOUND WARRANTY WARNING DECAL ON OVERHAULED CARB) 1H71 3O3 ONT3A19 E223 20010831001672001083100167EA 2001 8 31 2001FA0000212 220010813G8520LW17162 CRANKSHAFT PIPER PA28 PA28180 7102808SO LYC O360 O360A3A 41514EA ENGINE BROKEN G O OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 GL038424W 1564 282651 L741036A CRANKSHAFT FRONT MAIN JOURNAL, FRACTURED AT THE REAR RADIUS OF THE CRANKSHAFT FLANGE. PROPELLER SEPARATED FROM THE AIRCRAFT. LOSS OF OIL AND OIL PRESSURE, ENGINE SEIZED UP AND QUIT. THIS CRANKSHAFT WAS PURCHASED BY THE AIRPLANES INSURANCE COMPANY AT THE LAST OVERHAUL, (6-4-99), HISTORY AND TOTAL TIME OF CRANKSHAFT IS UNKNOWN. CRANKSHAFT MAY HAVE BEEN SUBJECT TO A PRIOR PROPELLER STRIKE DAMAGE ACCIDENT, AS NOTED BY THE SPIRAL TYPE FRACTURE OF THE FRONT CRANKSHAFT JOURNAL. 1L71 3O3 O 2A13 E286 20010831001682001083100168SO 2001 8 31 2001FA0000213 120010810G2752452860 BEARING PIPER PA23 PA23250 7102308SO LYC O540 TIO540* 41532EA FLAP ACTUATOR BROKEN B O OTHER F FLT CONT AFFECTED APAPPROACH 1 SO0154828 277554125 FLAP ACTUATOR ROD END BEARING, BROKEN ON SHORT FINAL. REPLACED BEARING PN 452860. 1L72 3O3 O 1A10 E14EA 20010905000492001090500049 2001 9 5 2001FA0000214 420010606G2340600591463 INTERPHONE CNDAIRCL604 CL604 EA EQUIP BAY UNSERVICEABLE D O OTHER O OTHER TXTAXI/GRND HDL 1 GL0915SP 570 5402 ON TAXI IN, CREW EXPERIENCED A LOUD CONTINUOUS SQUEAL IN THEIR HEADSETS AND ALSO OVER THE COCKPIT SPEAKERS. COMMUNICATION WAS IMPOSSIBLE WITH THE TOWER. OUR CUSTOMER SERVICE REP HAD US DISCONNECT THE HEADPHONE/MIC JACK ASSEMBLY IN THE AFT EQUIPMENT BAY. THE SQUEAL WENT AWAY. A NEW UNIT WAS ORDERED AND INSTALLED. A NEW UNIT WAS ORDERED AND INSTALLED. THE SYSTEM IS ONLY ACTIVE WITH WEIGHT ON WHEELS , BUT IT COULD STILL POSE A SERIOUS COMMUNICATION PROBLEM ON THE GROUND AT A BUSY AIRPORT. 2L72 4F RTA21EA 20010905000502001090500050SO 2001 9 5 2001FA0000216 120010727G792063201000 LINE PIPER PA28 PA28180 7102808SO LYC O360 O360* 41514EA OIL SYSTEM CORRODED D O OTHER K FLUID LOSS NRNOT REPORTED 1 EA137299W1830 281121 ON THE THIRD FLIGHT AFTER UPDATING THE OIL PUMP IN THE ENGINE PER AD, AN OIL FILM WAS NOTED AT THE FIREWALL ADJACENT TO THE SPOT WHERE THE OIL PRESSURE LINE PASSES THROUGH A GROMMET (DISC, FIREWALL PN 63915-003). OIL WAS ALSO PRESENT ON THE FIREWALL BLANKET ON THE INSIDE OF THE COCKPIT. AFTER DISASSEMBLING THE DISC A RETAINERS FROM THE FIREWALL, ABOUT 10-15 LBS PRESSURE WAS EXERTED ON THE ALUMINUM OIL LINE ASSEMBLY. IT SEPARATED INTO TWO PIECES DUE TO CORROSION OF THE METAL, INSIDE THE AREA WHERE IT PASSES THROUGH THE DISC/RETAINER ASSEMBLY. THIS PART HAS A TOTAL TIME OF ONLY 1830 HOURS IT IS A 1963 AIRCRAFT. 1L71 3O3 O 2A13 E286 20010831001692001083100169EA 2001 8 31 2001FA0000217 220010720G853072057 VALVE SEAT PIPER PA18 PA18150 7101828SO LYC O360 O360* 41514EA INTAKE PORT LEAKING D K NONE O OTHER ININSP/MAINT 1 AL05272CC 9925CC L37352736A DURING COMPRESSION CHECK, LOW CYLINDER PRESSURE WAS DISCOVERED. LEAKAGE WAS DETERMINED TO BE BETWEEN NUMBER FOUR CYLINDER INTAKE VALVE AND VALVE SEAT. AFTER REMOVING INTAKE VALVE, FURTHER INSPECTION REVEALED POOR CONDITION OF VALVE SEAT IN REGARDS TO A LACK OF A DISTINCT CONTACT WEAR PATTERN WITH VALVE. APPROXIMATELY ONLY ONE QUARTER OF THE DIAMETER OF THE VALVE SEAT SHOWED CLEAN CONTACT WITH THE VALVE WHILE THE OTHER THREE QUARTERS APPEARED ROUGH WITH EVIDENCE OF COMPRESSION BLOWBY. LEAKAGE CAUSED BY POOR SEAL BETWEEN VALVE AND SEAT DUE TO POSSIBLE IMPROPER VALVE SEAT INSTALLATION, VALVE LAPPING OR VALVE GUIDE BOSS NOT TRUE WITH VALVE SEAT FACE. 1H71 3O3 O 1A2 E286 20010831001702001083100170CE 2001 8 31 2001FA0000218 120010718G5730052301158 SKIN CESSNA172 172N 2072434CE LYC O320 O320* 41508EA RT WING CORRODED B A5ORK NONE O OTHER ININSP/MAINT 1 SO092168E7177 17271177 ON INSPECTION OF RIGHT WING ASSEMBLY, MECH NOTICED THAT A LOT OF RIVETS HAD POPPED FROM CORROSION UNDER THE LEADING EDGE SKIN AT THE FORWARD SPAR. THE WING WAS REMOVED FROM THE AIRCRAFT, BROUGHT TO THIS FACILITY FOR REPAIR. WING WAS DISASSEMBLED FOR REPAIR AND CORROSION REMOVAL. THE WING WAS FOUND TO HAVE MORE THAN AVERAGE AMOUNT OF HEAVY CORROSION TO SKINS, RIBS, SPARS AND STRINGERS. FOUR NOSE RIBS WHERE CORRODED THOUGH REQUIRING REPLACEMENTS. ALSO ALL SKINS WERE REPLACED. THE REMAINDER OF THE PARTS REQUIRED REMOVAL OF CORROSION, CLEANING AND TREATING OF PARTS. OWNER STATED THAT THE WING WAS NOT THAT BAD A YEAR AGO. 1H71 3O3 ONT3A12 E274 20010831001712001083100171CE 2001 8 31 2001FA0000219 120010621G570012NB108 NUT BEECH 95 95B55 1152729CE CONT O470 IO470* 17026SO WING CRACKED D K NONE O OTHER ININSP/MAINT 1 SO1370CL TC2263 DURING INSPECTION FOR ANNUAL, CRITERION AND FREQUENCY FOR WING BOLT INSPECTION. RECEIVED NEW HARDWARE. SENT OUT HARDWARE FOR MAGNETIC PARTICLE PROCESS PER MM. NDT PERSONAL INFORMED OF CONDITION OF NEW NUTS, STATING ROUGH INSIDE SURFACE AND LINEAR INDICATION ON INSIDE APPEARING AS CRACK INDICATIONS. BOTH NUTS WERE RED TAGGED AND BOTH PARTS RETURNED WITH 8130S FOR FURTHER INSPECTION. 1L72 3O3 ORT3A16 E1CE 20010831001722001083100172SO 2001 8 31 2001FA0000220 120010806G78206751700 MUFFLER PIPER PA32 PA32RT300 7103215SO LYC 0540 IO540K1G5D 41532SO ENGINE SPLIT D K NONE O OTHER NRNOT REPORTED 1 SW073516M2049 32R7885009 L1753348A THE CENTER MUFFLER HOUSING SPLIT OPEN AT THE UPPER WELD SEAM ALLOWING EXHAUST TO DAMAGE THE UPPER ALUMINUM MUFFLER ASSEMBLY SHROUD AND THE ENGINE INDUCTION COVER. SUGGEST THAT A VERY CLOSE INSPECTION BE DONE BY BOTH VISUAL AND PRESSURE CHECK METHODS OF ALL MUFFLER AND EXHAUST STACK WELD SEAMS. 1L71 3O3 O A3SO 1E4 20010831001732001083100173GL 2001 8 31 2001FA0000221 320010726G61102202 BEARING PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2A GL PROPELLER CRACKED B LU4RK NONE O OTHER ININSP/MAINT 1 SO1735272 317952142 DJ8665A RELEVANT INDICATION 1L72 3O3 O A20SO E14EA 5 CP33EA 20010831001742001083100174GL 2001 8 31 2001FA0000222 320010726G61103252L FORK PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2A GL PROPELLER CRACKED B LU4RK NONE O OTHER ININSP/MAINT 1 SO1735272 317952142 DJ8665A RELEVANT INDICATION 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000512001090500051EU 2001 9 5 2001FA0000223 120010712G6320C632A2115101 HOUSING UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE MAIN ROTOR CORRODED D K NONE O OTHER ININSP/MAINT 1 SW09120GB597 597 1063 34076 MFG CONCESSION APPLIED TO MGB- INSTALLATION OF BEVEL GEAR AND BEVEL PINION GEAR. DISASSEMBLY OF MGB FOR MODIFICATION, CORROSION WAS ON SUPPORT STUDS OF THE LOWER HOUSING AND THE BORES OF MAIN MODULE OF THE AFFECTED STUDS, INSP REVEALED CORROSION IN THE BORES. CLEANED AND TREATED THE BORES AND STUDS TO ACCEPTABLE STANDARDS, RECORDS OF THE MGB WERE REVIEWED, INDICATING THE COMPONENT WAS MANUFACTURED 8/98, WITH TOTAL TIME SINCE NEW-597.3 HOURS. THE OVERHAUL INTERVAL OF THE MGB IS 2000 HRS. THE MM WAS FOLLOWED FOR THE PROCEDURES OF DISASSEMBLY, ASSEMBLY AND COMPLETION OF THIS MODIFICATION, AND NO MENTION OF CORROSION IN THIS AREA OF THE MGB. FOLLOWED THE SPM FOR CORROSION CONTROL TO MAGNESIUM. PROBABLE CAUSE OF TH1G72 3U3 UNCR0001RD E34NE 20010917001362001091700136EU 2001 9 17 2001FA0000224 120010808G7600C761A1014101 LEVER UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE ANTICIPATR LEVERMISINSTALLED D K NONE O OTHER ININSP/MAINT 1 SW09162TA1225 1001 AFTER INSTALLATION OF THE NEW ANTICIPATOR COMPONENTS UNDER THE CARGO COMPARTMENT FLOOR ON THE LEFT SIDE . WE COULD NOT ACHIEVE THE CRITERIA MENTIONED WITH ADJUSTMENTS AND TESTS. UPON FURTHER INSPECTION, WE DISCOVERED THE ANTICIPATOR LEVER SECURED TO THE COLLECTIVE SHAFT FORWARD OF THE INSTALLED SB WAS INSTALLED FROM FACTORY 180 FROM A NORMAL POSITION. WHICH WHT NEW MODIFICATION WE INSTALLED, CAUSING THE ADJUSTMENTS FOR THE ANTICIPATOR AT THE FUEL CONTROL TO BE INCORRECT. ONCE THE ANTICIPATOR LEVER WAS REMOVED, AND INSTALLED CORRECTLY, WE WERE ABLE TO ACHIEVE CORRECT ADJUSTMENTS WITH THE ANTICIPATOR SIDE OF THE FUEL CONTROL UNIT. 1G72 3U3 UNCR0001RD E34NE 20010831001752001083100175 2001 8 31 2001FA0000225 420010717G6113055032110 BULKHEAD CESSNA172 172S 2072439CE LYC O320 IO320* 41508EA MCAULY1A170 1A170E GL SPINNER CRACKED C K NONE O OTHER ININSP/MAINT 1 AL03430CP 172S8692 L2938051A UC057 UPON A POSTFLIGHT INSPECTION, THE PROPELLER SPINNER BULKHEAD AND SPINNER ASSEMBLY WERE DISCOVERED CRACKED. THE CORNER PORTION OF THE BULKHEAD WAS COMPLETELY RIPPED AWAY AND THE EDGE OF THE SPINNER WAS PEELING UP AND TORN. PROBABLE CAUSE: MANUFACTURING DEFECT SUSPECTED. 1H71 3O3 ONT3A12 1E12 5 NP857 20010831001762001083100176CE 2001 8 31 2001FA0000226 120010728G5711 SPAR BEECH 55 95C55 1152708CE CONT O520 IO520* 17032SO LT WING CRACKED D K NONE O OTHER ININSP/MAINT 1 SW152764T TE372 CRACK DEVELOPED ON TOP OF LEFT WING. INVESTIGATION REVEALED LOWER FORWARD WING SPAR HINGES AND PINS WORN OUT RESULTING IN EXCESS OF MOVEMENT IN THE LEADING EDGE OF WINGS. NEW WING SPARS 1L72 3O3 O 3A16 E5CE 20010831001772001083100177EA 2001 8 31 2001FA0000227 220010730G7200PT6A41 ENGINE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA LEFT FAILED G E ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 EA032025M102061596 BB384 PCE80823 LEFT ENGINE SHUT DOWN DUE TO CHIP DETECTOR LIGHT ON ENGINE SURGING AND OIL PRESSURE FALLING OFF. ON INITIAL INSPECTION SUSPECTS COMPRESSOR, NR1 OR NR 2 MAIN LINE BEARING FAILURE. 1L72 4T4 T A24CE E4EA 20010831001782001083100178SO 2001 8 31 2001FA0000228 120010622G274062701114 CONTROL CABLE PIPER PA28 PA28161 7102803SO STABILIZER FRAYED H CDHSK NONE O OTHER ININSP/MAINT 1 EA059182W7000 2841130 RIGHT FORWARD STABILATOR CABLE- THIS LOCATION HAS SEVERAL PULLIES THAT DO NOT HAVE BEARINGS, WHEN THEY GET STUCK (NOT MUCH CABLE DEFLECTION AND THEREFORE NOT MUCH PRESSURE TO TURN THE PULLEY) THE CABLE WEARS THIN AND EVENTUALLY FRAYS. DIFFICULT TO DETECT WITHOUT CLEANING CABLE AND CHECKING WITH FINGERNAIL OR RAG. THIS CABLE LOOKED FINE BUT HAD 50 PERCENT BROKEN STRANDS WHEN IT WAS REMOVED AND BIRDGAGED. 1L71 3O 2A13 20010905000522001090500052 2001 9 5 2001FA0000229 420010716G3418S16729 DETECTOR CESSNA182 182R 2072731CE CONT O470 O470* 17026SO LT WING INOPERATIVE D O OTHER O OTHER NRNOT REPORTED 1 EA2135VA 18268129 UPON INSTALLING NEW LIFT DETECTION, NOTED THAT WHEN WIRED AS ORIGINALLY REMOVED FROM AIRCRAFT, WITH HEAT TURNED ON, DETECTION WAS INOPERATIVE. GROUND FOR HEATER WAS INSTALLED ON COMMON FOR DETECTION; CAUSING A NO POTENTIAL WHEN HEATER TURNED ON. 1L71 3O3 ONT3A13 E273 20010831001792001083100179SO 2001 8 31 2001FA0000230 220010829G8540632617 BEVEL GEAR CESSNA337 337D 2075717CE CONT O360 IO360CB 17025SO ACCESSORY DRIVE FAILED D O OTHER O OTHER NRNOT REPORTED 1 WP0751WM 3371140 236532R TROUBLESHOT LOSS OF VACUUM ON REAR ENGINE AND DETERMINE ACCESSORY DRIVE ASSEMBLY GEAR BOX FOR VACUUM PUMP AND HYDRAULIC PUMP INOPERABLE. REMOVE AND DISASSEMBLED GEAR BOX AND FOUND BEVEL GEAR PN 632617 STRIPPED OF ALL GEAR TEETH. ENGINE HAD BEEN RECENTLY OVERHAULED. OIL LEVEL AT CORRECT CAPACITY. POSSIBLE CAUSE OF FAILURE MAY BE DUE TO IMPROPER GEAR MESH OF BEVEL GEARS FROM WORN OR INCORRECT SHOULDER THICKNESS ON BUSHING. MFG IS NOW AWARE OF THE GEAR MESH PROBLEM AND HAS CORRECTED IT VIA A SB AND ISSUED THE MODIFIED ADAPTER ACCESSORY DRIVE FOR REPLACEMENT. 1H72 3O3 O A6CE E1CE 20010831001802001083100180SO 2001 8 31 2001FA0000231 220010816G72306375506 VALVE SEAT CESSNA185 A185E 2072818CE CONT O520 IO520* 17032SO CYLINDER CRACKED D K NONE O OTHER ININSP/MAINT 1 SO0070083 18501950 282858 DURING A ROUTINE COMPRESSION CHECK, A LEAK WAS FOUND IN THIS CYLINDER (AIR WAS ESCAPING FROM IN BETWEEN COOLING FINS). UPON REMOVAL OF CYLINDER, 2 CRACKS APPROX. 1 INCH AND .7500 INCH LONG, WERE FOUND TO BE EMANATING FROM THE EXHAUST VALVE SEAT. 1H71 3O3 O 3A24 E5CE 20010831001812001083100181SO 2001 8 31 2001FA0000232 120010816G243478483000 STRUT PIPER PA28 PA28R200 7102811SO ALTERNATOR CRACKED D O OTHER O OTHER NRNOT REPORTED 1 SO17318MC926 28R35155 ALTERNATOR FRONT ATTACHMENT STRUT FOUND CRACKED. 1L71 3O 2A13 20010831001822001083100182CE 2001 8 31 2001FA0000233 120010717G32465010720 BOLT BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE MLG WHEEL BROKEN C WXHMO OTHER O OTHER NRNOT REPORTED 1 NM01440DS1000 RK8 1 MAIN WHEEL TIE BOLT BROKE AND DEPARTED AIRCRAFT, RESULTING IN UNSEATING OF WHEEL HALF SEALING O-RING AND SUBSEQUENT LOSS OF AIR PRESSURE. BOLT WAS MAGNAFLUXED 14 HOURS PREVIOUS WITH NO DEFECTS NOTED. 2H72 4F4 FRTA16SW E25EA 20010831001832001083100183EU 2001 8 31 2001FA0000234 120010702G6210355A11002009 BLADE AEROSPAS355 AS355F2 8680812EU ALLSN 250C 250C20 03013GL MAIN ROTOR CRACKED E K NONE O OTHER ININSP/MAINT 1 SO1742AT 2220 5462 FOUND CRACK ON PREFLIGHT. NO SURE CAUSE FOR CRACK. CRACK BEYOND LIMITS. 1G72 3U3 U H11EU E4CE 20010831001842001083100184EA 2001 8 31 2001FA0000235 120010806G32226A0720401 LINK DHAV DHC2 DHC2MK3 2800107EA NLG BROKEN D O OTHER E VIBRATION/BUFFET LDLANDING 1 NM01227N 1686TB UPON LANDING AT BFI, BOTH NOSE WHEEL BEGAN TO SHIMMY, PILOT PULLED NOSE WHEELS OFF OF RUNWAY UPON TOUCHDOWN AGAIN, SEVERE SHIMMY OCCURRED. RIGHT NOSE GEAR LINK RAM END BROKE ALLOWING GEAR TO DEPART FROM AIRCRAFT. 1H71 3T A806 20010910002102001091000210CE 2001 9 10 2001FA0000238 120010831G32332653361203 CLEVIS PIN RKWELLNA265 NA26565 7630107CE GARRTTTFE731TFE7313R1D 01518WP MLG ACTUATOR CRACKED B K NONE O OTHER ININSP/MAINT 1 CE0182CR 8760 600 46549 CRACKED PIN FOUND AS A RESULT OF CONDUCTING MAGNETIC PARTICLE INSPECTION OF MAIN LANDING GEAR ACTUATOR ROD CLEVIS PIN AND ATTACHING HARDWARE IN ACCORDANCE WITH SMIP ATA CODE 323076. CRACK IS LOCATED IN RELIEF AREA RADIUS DIRECTLY UNDER CLEVIS PIN HEAD. 2L72 4J4 F A2WE E6WE 20010905000532001090500053SO 2001 9 5 2001FA0000239 120010720G2842 O-RING PIPER PA31T PA31T 7103124SO PWA PT6 PT6* 52043EA FUEL PROBE LEAKING D O OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09700LT 2260 31T7920046 AFTER FUELING AIRCRAFT, FUEL STARTED LEAKING FROM RIGHT NACELLE FUEL PROBE COVER. FOUND O-RING BETWEEN MOUNT PLATE AND TOP OF PROBE EXTRUDED IN 2 AREAS. FUEL WAS RUNNING OUT OF THOSE AREAS. DEFUELED AND REPLACED PROBE WITH SERVICEABLE UNIT. 1L72 3T3 T A8EA E2NE 20010910003072001091000307SO 2001 9 10 2001FA0000240 120010801G2460688498 RELAY PIPER PA46 PA46500TP SO PWA PT6 PT6* 52043EA COCKPIT DAMAGED B NM4RH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO157156217 PILOT REPORTED SMOKE IN COCKPIT AND THEN CABIN FAN CIRCUIT BREAKER POPPED. FOUND LOAD BUS RELAY PN 688498 LOCATED BELOW RIGHT CIRCUIT BREAKER PANEL, WITH A HOLE BURNED IN IT. WITH CIRCUIT BREAKER PULLED, THE SMOKE WENT AWAY. PILOT RETURNED AIRCRAFT TO FACTORY FOR REPAIR. 1L71 3O3 TRTA25SO E2NE 20010905001102001090500110SW 2001 9 5 2001FA0000241 120010522G7160646207 TUBE MOONEYM20 M20R 5870225SW CONT O550 IO550G 17042SO NR 6 CYLINDER CRACKED B EA6RK NONE O OTHER ININSP/MAINT 1 NE0146WB 68 290226 679484 INDUCTION TUBE AT NR 6 CYLINDER IS COMPLETELY CRACKED AT FLANGED END. 1L71 3O3 ORT2A3 E3SO 20010905001112001090500111SO 2001 9 5 2001FA0000243 120010827G32303807802 DOWNLOCK BRACKET PIPER PA32 PA32R300 7103213SO LYC O540 TIO540* 41532EA NLG BROKEN G O OTHER J WARNING INDICATION CRCRUISE 1 AL01200HM351 32R7680025 NOSE GEAR DROPPED OUT OF WHEEL WELL IN FLIGHT. FOUND DOWNLOCK BROKEN WHERE NOSE ACTUATOR ROD ATTACHES. THIS HAS HAPPENED ON MORE THAN ONE OCCASION WITH SAME TYPE OF AIRCRAFT IN THE PAST. 1L71 3O3 O A3SO E14EA 20010905001122001090500112CE 2001 9 5 2001FA0000244 120010824G57530523920 BEARING CESSNA206 U206G 2073356CE CONT C85 C85* 17008SO FLAP TRACK WORN B DVPRK NONE O OTHER ININSP/MAINT 1 SO039489Z473 U20606525 INNER BEARING WAS PUSHED OUT TO ONE SIDE SHOWING EXCESSIVE WEAR. 1H71 3O3 O A4CE E233 20010910003082001091000308CE 2001 9 10 2001FA0000245 120010906G5210169420036147 STRUCTURE BEECH 23 C23 1151242CE LYC O360 VO360* 41514EA LT DOOR BROKEN D O OTHER EF VIBRATION/BUFFET FLT CONT AFFECTED APAPPROACH 1 EA21200878100 M2063 PILOTS REPORTED SEVERE BUFFET DURING SLOW FLIGHT, APPROACH TO LANDING, ROUND-OUT, AND FLARE. BUFFET WAS AGGRAVATED BY LEFT SLIP. FOUND BOTTOM DOOR GASKET MISSING AND FIBERGLASS DOOR STRUCTURE BROKEN AT LAST RIVET ON DIAGONAL GUSSET. THIS ALLOWED AIR ESCAPING FROM CABIN TO DISRUPT AIRFLOW OVER THE WING AND STABILATOR. FABRICATED HAT SECTION CHANNEL FROM 0.032 2024-T3, BONDED TO FIBERGLASS CHANNEL WITH HYSOL EA9309, AND RIVETED THROUGH OUTSIDE SKIN. INSTALLED NEW DOOR GASKET. FOUND RIGHT CABIN DOOR BROKEN ALSO. SUSPECT CAUSE IS DUE TO PILOTS LEAVING DOORS OPEN AND UNATTENDED TO COOL CABIN AND WIND OPENING DOOR HARD AGAINST THE STOP. 1L71 3O3 O A1CE 1E1 20010910003092001091000309CE 2001 9 10 2001FA0000246 120010906G712010598000021 CHANNEL BEECH 76 76 1153005CE LYC O360 VO360* 41514EA ENGINE MOUNT BROKEN B G2ARK NONE O OTHER ININSP/MAINT 1 NE056714R ME320 BOTH UPPER OUTBOARD ENGINE MOUNT CHANNELS BROKEN THROUGH JUST ABOVE NUT PLATE HOLE. MAY HAVE BEEN CAUSED BY STRESSES IMPOSED BY THE COUNTER ROTATING ENGINES AND/OR UNREPORTED HARD LANDINGS. 1L72 3O3 O A29CE 1E1 20010913001852001091300185SO 2001 9 13 2001FA0000247 120010706G214023D04 VALVE PIPER PA23 PA23250 7102308SO LYC O540 TIO540* 41532EA HEATER DEFECTIVE D K NONE K FLUID LOSS ININSP/MAINT 1 EA2168SE 273780 AFTER COMPLYING WITH AD AND SB, VALVE WAS DEEMED AIRWORTHY AND REINSTALLED IN AIRCRAFT. CONNECTED A PRESSURE GAUGE TO VERIFY THAT SETTING WAS CORRECT BECAUSE OF THE QUANTITY OF SOOT IN THE EXHAUST PIPE AND STREAM. WHILE REMOVING TEE FITTING AND GAUGE,THE FUEL DID NOT STOP DRIPPING FROM THE VALVE OUTLET. ENERGIZED THE FUEL PUMP BRIEFLY TO PRESSURIZE THE VALVE AND THE FUEL DID NOT STOP, PN OF VALVE IS NOT READABLE. IT APPEARS TO HAVE BEEN SALVAGED FROM ANOTHER AIRCRAFT BECAUSE THE PAINT ON IT DOES NOT MATCH THIS AIRCRAFT. NEW VALVE IN ORDER. 1L72 3O3 O 1A10 E14EA 20010910003112001091000311NE 2001 9 10 2001FA0000248 220010708G7321 FUEL CONTROL CESSNA500 500CESSNA 2076602CE PWA JD15 JT15D1A NE RT ENGINE MALFUNCTIONED D O OTHER R PARTIAL RPM/PWR LOSS CLCLIMB 1 EA0788GJ 5000155 PCE76335 DURING A CLIMB THROUGH FL 290, THE RIGHT ENGINE FAN SPEED DECREASED TO 82 PERCENT. ENGINE IGNITION WAS SELECTED ON TO NO EFFECT. AND EMERGENCY WAS DECLARED AND A SAFE LANDING WAS MADE. SUSPECT THAT THE FUEL CONTROL UNIT MALFUNCTIONED. 1L72 4F4 F A22CE E25EA 20010910003142001091000314EA 2001 9 10 2001FA0000250 220010814G7414AB3571651 COIL MOONEYM20 M20E 5870212SW LYC O360 IO360A1A 41514EA MAGNETO CRACKED D K NONE O OTHER ININSP/MAINT 1 SW099240M478 1193 L252751A WHILE REPAIRING LEFT BENDIX S20 SERIES MAGNETO, FOUND MAGNETO COIL CRACKED. REPLACED COIL WITH A NEW TCM COIL PN 10-357165 COIL. ALSO FOUND CRACK IN DISTRIBUTOR BLOCK, REPLACED. 1L71 3O3 O 2A3 1E10 20010913001862001091300186EA 2001 9 13 2001FA0000251 220010814G8550 IMPELLER MOONEYM20 M20E 5870212SW LYC O360 IO360A1A 41514EA OIL PUMP DAMAGED D K NONE O OTHER ININSP/MAINT 1 SW099240M478 1193 L252751A OIL PUMP IMPELLERS S1B 524, FOUND OIL PUMP GEARS TO BE STEEL TYPE BUT NO DOCUMENTATION AS TO WHAT PN THE GEARS WERE. FOUND GEARS HAD FOREIGN MATERIAL HAD PASSED THROUGH THE OIL PUMP. OIL PUMP GEARS WERE NOT AIRWORTHY REGARDLESS OF PART NUMBERS. INSTALLED IMPELLER KIT PN 05K19423S. (ATTACHED PHOTOS) 1L71 3O3 O 2A3 1E10 20010913001882001091300188EA 2001 9 13 2001FA0000252 220010814G855078531 HOUSING MOONEYM20 M20E 5870212SW LYC O360 IO360A1A 41514EA OIL PUMP GALLED D K NONE O OTHER ININSP/MAINT 1 SW099240M478 1193 L252751A WHEN COMPLYING WITH AD, OIL PUMP IMPELLERS, S1B524, FOUND OIL PUMP BODY GALLED DUE TO FOREIGN MATERIAL PASSING THROUGH OIL PUMP ASSEMBLY. REPLACED OIL PUMP BODY WITH NEW PART. (PHOTOS ATTACHED) 1L71 3O3 O 2A3 1E10 20010910004262001091000426 2001 9 10 2001FA0000253 420010822G2561AC2D21344101 LIFE VEST CABIN FAILED B KQ1RK NONE L NO TEST ININSP/MAINT 1 EA07 LIFE VEST FAILED MFG RECOMMENDED TWO(2) PSI INFLATION TEST IAW MM. DATE OF MFG: JAN 1988 20010913001892001091300189GL 2001 9 13 2001FA0000254 220010716G72612060405441 TUBE BELL 206 206L1 1182107SW ALLSN 250B 250B* GL ENGINE CORRODED D K NONE K FLUID LOSS ININSP/MAINT 1 EA1798KR 5885 45683 MAIN GEARBOX TO OIL COOLER TRANSFER TUBE LEAKING DUE TO CORROSION PITTING. AREA WHERE TUBE RUNS THRU AREA IS FILLED WITH LOOSE FIBERGLASS SOUND PROOFING WHICH HOLDS MOISTURE AND CAUSES CORROSION. RECOMMEND REMOVING INSULATION FROM THESE AREAS. 1G71 3U3 T H2SW E10CE 20010910004272001091000427NE 2001 9 10 2001FA0000255 220010725G853028160 VALVE SPRING WTHRLY620 620B 9630605CE PWA R985 R985AN1 52008NE NR 1 CYLINDER BROKEN D A UNSCHED LANDING R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 NM052035N6170 1591 15642 ENGINE BEGAN BACKFIRING AND POWER DECREASED, AIRCRAFT LANDED AS A RESULT OF RUNNING THROUGH A FENCE. FOUND NR 1 CYLINDER INTAKE VALVE SPRINGS BROKEN. REPLACED SPRINGS, OPERATION NORMAL. APPEARED TO BE SMALL RUST PITS IN BREAK AREAS. 1L71 3R3 RNCA26WE 5E1 20010913001902001091300190EA 2001 9 13 2001FA0000256 220010724G7310601800 GASKET PIPER PA46 PA46500TP SO PWA PT6 PT6* 52043EA ENGINE LEAKING D O OTHER K FLUID LOSS CRCRUISE 1 EA25310JM47 4697069 FUEL WAS LEAKING IN FLIGHT AND ON GROUND. GASKET ON FILTER ASSY. E6 BYPASS GASKET LEAKING. 1L71 3O3 TRTA25SO E2NE 20010913001912001091300191CE 2001 9 13 2001FA0000257 120010802G53410512122 BLOCK CESSNA175 175A 2072504CE CONT O300 GO300* 17022SO WING ATTACH CORRODED B K NONE O OTHER ININSP/MAINT 1 GL097912T 56612 DISSIMILAR METAL CORROSION ON WING ATTACH POINTS. BLOCK ARE ATTACHED TO FUSELAGE SPAR ASSEMBLY PN 05121246 WITH (4) AW320A BOLTS. REMOVE FOR INSPECTION. 1H71 3O3 O 3A17 E298 20010913002192001091300219CE 2001 9 13 2001FA0000258 120010802G53410411129 BLOCK CESSNA175 175A 2072504CE CONT O300 GO300* 17022SO WING ATTACH CORRODED B K NONE O OTHER ININSP/MAINT 1 GL097912T2142 56612 DISSIMILAR METAL CORROSION ON WING ATTACH POINTS. BLOCKS ARE ATTACHED TO FUSELAGE SPAR ASSEMBLY. PN 0511162-S WITH (4) AN3-21A BOLTS. REMOVE FOR INSPECTION. 1H71 3O3 O 3A17 E298 20010913002222001091300222CE 2001 9 13 2001FA0000259 120010703G5712 RIB BBAVIA8 8KCAB 2110612CE LYC O360 AEIO360H1A 41514EA LT&RT WING DAMAGED D K NONE O OTHER ININSP/MAINT 1 NE0580TA 1511 63280 L2167853A FOUND LOOSE AND/OR MISSING NAILS AT RIB/FRONT SPAR CONNECTION. 2 RIBS ON RT WING AND 2 RIBS ON LT WING FOUND DAMAGED WHILE INSPECTING PER REGMENTS OF AD. 1H71 3O3 O A21CE 1E10 20010913002252001091300225SO 2001 9 13 2001FA0000260 120010721G2434LAY6421 BRUSHES PIPER PA32 PA32301 7103207SO ALTERNATOR WORN G O OTHER O OTHER NRNOT REPORTED 1 NE0342993 328306025 ALTERNATOR BRUSHES WORN, BATTERY WEAK. 1L71 3O A3SO 20010913002262001091300226EA 2001 9 13 2001FA0000261 220010613G855070484 SCREEN CESSNA172 172L 2072432CE LYC O360 O360* 41514EA OIL FILTER CRUSHED D K NONE O OTHER ININSP/MAINT 1 NM094250Q120 17260150 L3603436A METAL IN FILTER. FOUND SCREEN CRUSHED (FROM FACTORY BUILDUP) ALLOWED METAL TO CONTAMINATE ENGINE. 1H71 3O3 ONT3A12 E286 20010913002282001091300228EA 2001 9 13 2001FA0000262 220010613G8520 CRANKCASE CESSNA172 172L 2072432CE LYC O360 O360* 41514EA ENGINE MISMANUFACTURED D K NONE W INADEQUATE Q C ININSP/MAINT 1 NM094250Q 17260150 L3603436A TOOLING-MACHINE CHATTER LEFT ROUGH, UNFINISHED AREA FOR CYL BASE O-RING TO SEAT AGAINST ALL FOUR CASE CYLINDER HOLES. 1H71 3O3 ONT3A12 E286 20010913002292001091300229EA 2001 9 13 2001FA0000263 220010613G8530LW11775 PISTON PIN CESSNA172 172L 2072432CE LYC O360 O360* 41514EA ENGINE WORN D K NONE O OTHER ININSP/MAINT 1 NM094250Q120 17260150 L3603436A METAL IN FILTER. PISTON PIN PLUG- EXCESSIVE WEAR. ONE PIN WORN DOWN .500 INCH. ALL PLUGS WORN. 1H71 3O3 ONT3A12 E286 20010913002302001091300230SO 2001 9 13 2001FA0000264 120010807G3080A110240 PROBE PIPER PA28 PA28161 7102803SO LYC O320 O320* 41508EA CARB ICE DETECT DEFECTIVE D HE8MO OTHER N FALSE WARNING NRNOT REPORTED 1 CE0983416658 288116160 L1082939A ICEMAN CARBURETOR, ICEMAN DETECTOR ALERTS EVEN WHEN THERE IS NO ICE. THERE APPEARS TO BE A MALFUNCTION OF THE PROBE. 1L71 3O3 O 2A13 E274 20010913002312001091300231CE 2001 9 13 2001FA0000265 120010801G5753052390 ROLLER CESSNA172 172N 2072434CE LYC O320 O320* 41508EA T/R FLAP CRACKED D K NONE O OTHER ININSP/MAINT 1 CE09738DB5300 17269886 FLAP ROLLER FOUND NOT TURNING. REMOVED AND FOUND CRACKS. THIS IS NOT THE FIRST TIME THIS CONDITION WAS FOUND. LACK OF PROPER MAINTENANCE. DIRTY AND DRY ROLLER BEARINGS. 1H71 3O3 ONT3A12 E274 20010913002322001091300232SO 2001 9 13 2001FA0000266 120010807G3080A110240 PROBE PIPER PA28 PA28161 7102803SO LYC O320 O320* 41508EA CARB ICE DETECT DEFECTIVE D HE8MO OTHER O OTHER NRNOT REPORTED 1 CE0947979318 287816175 L779939A CARBURETOR ICE DETECTOR ALERTS EVEN WHEN THERE IS NO ICE. THERE APPEARS TO BE A MALFUNCTION OF THE PROBE. 1L71 3O3 O 2A13 E274 20010913002342001091300234SW 2001 9 13 2001FA0000267 120010618G2710730048503 TUBE MOONEYM20 M20K 5870220SW CONT O520 TSIO520* 17040SO AILERON CORRODED B EA6RK NONE O OTHER ININSP/MAINT 1 NE01389CS880 250860 FATAL INTERNAL CORROSION, CAUSED BY TRAPPED MOISTURE INSIDE PUSH PULL CONTROL TUBE FOR AILERON. CORROSION WAS FOUND DURING ANNUAL INSPECTION. 1L71 3O3 O 2A3 E8CE 20010913002362001091300236SW 2001 9 13 2001FA0000268 120010820G7603TCM646224A THROTTLE ARM MOONEYM20 M20R 5870225SW CONT O550 IO550* SO COCKPIT WORN B EA6RK NONE O OTHER ININSP/MAINT 1 NE0153WM 322 290191 679406 THE PRESSED IN BUSHING AT THE END OF THE THROTTLE ARM WAS WORN THRU. THE BRONZE SECTION. (ATTACHED PHOTO) 1L71 3O3 ORT2A3 E3SO 20010914000612001091400061CE 2001 9 14 2001FA0000269 120010912G33404502131REVR1 LANDING LIGHT CESSNA650 650 2076802CE EXTERIOR DEFECTIVE D K NONE L NO TEST ININSP/MAINT 1 SO01733H 6500210 BOUGHT OVERHAULED LIGHT FROM CESSNA, (OVERHAULED BY GRIMES). RETRACTABLE LIGHT RETRACTS, EXTENDS, AND LIGHTS UP BUT WILL NOT ADJUST TO ALLOW FOR PROPER ALIGNMENT OF THE BEAM OF LIGHT. THE BEAM OF LIGHT POINTS AT THE GROUND RATHER THAN OUT IN FRONT OF THE AIRPLANE. MAINTENANCE MANUAL INSTRUCTIONS WERE FOLLOWED BUT ADJUSTMENT PROCEDURES HAD NO EFFECT. THE OVERHAUL COULD NOT HAVE BEEN COMPLETED IN A CORRECT MANNER, THIS PART HAS ZERO TIME IN SERVICE. 2L72 4F A9NM 20010914000732001091400073CE 2001 9 14 2001FA0000270 120010912G33404502131 MOTOR CESSNA650 650 2076802CE LANDING LIGHT FAILED C K NONE O OTHER DEDESCENT 1 GL10733K 6500222 UNIT RECEIVED AND INSTALLED. OPERATED UNIT 3 CYCLES AND ON 4 EXTENSION UNIT WOULD NOT EXTEND AND MOTOR SEIZED AND SMELLED OF BURNING ELECTRICAL WIRING. UNIT WAS PURCHASED THRU CESSNA AS AN OVERHAULED PART BY AN OUTSIDE VENDOR. THE UNIT HAS A HISTORY OF EARLY FAILURE AFTER OVERHAUL. THIS COMPANY HAS HAD FIVE WARRANTY ACTIONS CLAIMED ON THIS PART NUMBER. 2L72 4F A9NM 20010914000742001091400074CE 2001 9 14 2001FA0000271 120010912G33404502131 MOTOR CESSNA650 650 2076802CE LANDING LIGHT DEFECTIVE C K NONE O OTHER DEDESCENT 1 GL10733K 6500222 UNIT RECEIVED AND INSTALLED. WHEN LIGHT IS RETRACTED, UNIT CONTINUES TO RUN WITH A GRINDING NOISE AND MOTOR WILL NOT SHUT OFF. UNIT WAS NOT ADJUSTED ON INSTALLATION. UNIT WAS PURCHASED THRU CESSNA AS AN OVERHAULED PART BY AN OUTSIDE VENDOR. THE UNIT HAS A HISTORY OF EARLY FAILURE AFTER OVERHAUL. THIS COMPANY HAS HAD FIVE WARRANTY ACTIONS CLAIMED ON THIS PART NUMBER. 2L72 4F A9NM 20010914000762001091400076CE 2001 9 14 2001FA0000272 120010912G33404502131 LANDING LIGHT CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP EXTERIOR DAMAGED D K NONE W INADEQUATE Q C ININSP/MAINT 1 SO01733H 6500210 RECEIVED THIS PART FROM CESSNA WITH UNDAMAGED PACKING. THE GROUND LUG WAS BENT, LOOSE AND HAD DAMAGED THREADS. THIS PART WAS PROPERLY PACKED WITH SPRAYED IN FOAM. THIS PART WAS DAMAGED PRIOR TO BEING PLACED IN THE BOX. 2L72 4F4 F A9NM E6WE 20010914000782001091400078CE 2001 9 14 2001FA0000273 120010912G33404502131 MOTOR CESSNA650 650 2076802CE LANDING LIGHT FAILED D K NONE L NO TEST ININSP/MAINT 1 SO01733H 113 113 6500210 RETRACTABLE LIGHT WOULD NOT EXTEND. IT SEEMS TO ME THAT AN AIRCRAFT PART SHOULD BE CAPABLE OF STAYING IN SERVICE FOR MORE THAN 113.7 HOURS. 2L72 4F A9NM 20010917001392001091700139NM 2001 9 17 2001FA0000274 120010808G2760654494715 HOUSING BOEING BOEING737 737* NM SPOILER ACTUATORCRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 10268 HOUSING IS CRACKED ON THE OPPOSITE SIDE OF THE PORTS. INSTALL HOUSING PN 65-44947-15. NOTE: HOUSING IS PN 65-44947-15 AND IS THE REPLACEMENT TO SOLVE PROBLEMS OF CRACKS NOTED ON PREVIOUS HOUSING DASH NUMBERS PER SL. 2L72 4F RTA16WE 20010917001402001091700140NM 2001 9 17 2001FA0000275 120010808G2760654494710 HOUSING BOEING737 737* NM ACTUATOR CRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 15735 HOUSING IS CRACKED ON THE LOWER SHOULDER NEAR BEARING MOUNT LUG. INSTALL HOUSING PN 65-44947-15. 2L72 4F RTA16WE 20010917001422001091700142NM 2001 9 17 2001FA0000276 120010808G276065C268636 HOUSING BOEING BOEING737 737* NM ACTUATOR CRACKED B IU6DK NONE O OTHER ININSP/MAINT 1 NM01 30072 WN0009 HOUSING IS CRACKED AND BROKEN AT THREADED AREA. FATIGUE/OVERSTRESSED. 2L72 4F RTA16WE 20010917001482001091700148NM 2001 9 17 2001FA0000277 120010723G2730401606223 HOUSING BOEING727 727 UTILSYSNM SEAL PLATE CORRODED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 HOUSING ASSEMBLY IS CORRODED ON THE SEAL PLATE SURFACE, IN THE CHECK VALVE PORTS AND BOLT HOLES. HOUSING ASSEMBLY IS MADE FROM MAGNESIUM ALLOY AND IS EXTREMELY SUSCEPTIBLE TO DISSIMILAR METAL CORROSION AND CRACKS. 2L73 4J RTA3WE 20010917001492001091700149NM 2001 9 17 2001FA0000278 120010716G2730401606223 HOUSING MOOG BOEING727 727* NM SEAL PLATE CORRODED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 1433D HOUSING ASSEMBLY IS CORRODED ON THE SEAL PLATE SURFACE, IN THE CHECK VALVE PORTS AND BOLT HOLES. HOUSING ASSEMBLY IS MADE FROM MAGNESIUM ALLOY AND IS EXTREMELY SUSCEPTIBLE TO DISSIMILAR METAL CORROSION AND CRACKS. 2L73 4F RTA3WE 20010917001502001091700150NM 2001 9 17 2001FA0000279 120010716G2760654494710 HOUSING BOEING BOEING727 727 UTILSYSNM ACTUATOR CRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 41454 0970 HOUSING IS CRACKED ON THE OPPOSITE SIDE OF THE PORTS. INSTALL HOUSING PN 65-44947-15. 2L73 4J RTA3WE 20010917001522001091700152NM 2001 9 17 2001FA0000280 120010716G2760654494710 HOUSING BOEING BOEING737 737 UTILSYSNM ACTUATOR CRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 50886 0893 HOUSING IS CRACKED ON THE OPPOSITE SIDE OF THE PORTS. INSTALL HOUSING PN 65-44947-15. 2L72 4F RTA16WE 20010917001532001091700153NM 2001 9 17 2001FA0000281 120010717G323065179547 HOUSING BOEING BOEING727 727 UTILSYSNM ACTUATOR CRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 RC707 THE HOUSING HAD A CRACK IN THE CENTER OF THE BARREL. 2L73 4J RTA3WE 20010917001542001091700154CE 2001 9 17 2001FA0000282 120010811G323312416195F ACTUATOR CESSNA210 210L 2073448CE CONT O520 IO520* 17032SO MLG CRACKED G K NONE O OTHER ININSP/MAINT 1 SW118137L 21060624 LEFT MAIN GEAR ACTUATOR CRACKED, RESULTING IN THE LOSS OF HYDRAULIC FLUID. AIRCRAFT MADE A GEAR UP LANDING, AIRCRAFT HAS SUBSTANTIAL DAMAGE TO HORIZONTAL STABILIZER AND ELEVATOR. 1H71 3O3 O 3A21 E5CE 20010917001102001091700110SO 2001 9 17 2001FA0000286 220010825G74144301 MAGNETO CESSNA150 150G 2071816CE CONT O200 O200A 17020SO ENGINE INOPERATIVE C A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SW992750S 15066650 54877A INSTALLED NEW LEFT AND RIGHT SIDE SLICK (UNISON) MAGNETOS AND IGNITION HARNESS. TEST RUN OK. ON FIRST FLIGHT AFTER 15 MIN. ENGINE POWER LOSS OCCURED. AFTER LANDING FOUND LEFT MAG INOP. REMOVED MAG AND FOUND THAT COIL INSULATION HAD BURNED THROUGH AND HIGH VOLTAGE WAS ARCING TO CASE OF MAG THROUGH COIL INSULATION. 1H71 3O3 O 3A19 E252 20010917001122001091700112NE 2001 9 17 2001FA0000287 220010807G8500 ENGINE WSK M18 M18DROMADER 9810102EU WSK PZL PZLM18 67203NE WSK US132 US132000A NE NACELLE MALFUNCTIONED G K NONE O OTHER AGAGRICULTURE 1 SW114206B 1Z00507 FLYING IN CRUISE WHEN BUTTERFLY ON INTAKE STARTED FLUCUATING. PULLED UP AND REDUCED POWER. APPROXIMATELY 10 SECONDS LATER LOST POWER. ACFT. HIT LOW LEVEE SKIDDED ACROSS FIELD AND HIT SECOND LEVEE. UPON STRIKING SECOND LEVEE ACFT. ROLLED OVER ON ITS NOSE AND SKIDDED TO A REST UPSIDE DOWN IN A RICE FIELD. 1L71 3O4 R A47EU E10NE 5 CP4NE 20010917001202001091700120SO 2001 9 17 2001FA0000292 120010905G3220AN3105MS24665 COTTER PIN PIPER PA28 PA28R201 7102816SO NLG MISSING B A UNSCHED LANDING DJ INFLIGHT SEPARATION WARNING INDICATION LDLANDING 1 GL21279ND599 2844034 DURING A TRAINING FLIGHT, UPON GEAR RETRACTION THE CFI HEARD A THUMP FROM THE NOSE AREA.THE GEAR UNSAFE LIGHT DIDNT EXTINGUISH. MLG EXTEND WAS ATTEMPTED , DIDNT RECEIVE A NLG DOWN AND LOCKED INDICATION. RETRACTION AND EMERGENCY EXTEND WAS ATTEMPTED. PERFORMED A FLYBY AND WERE INFORMED THE NLG WAS TRAILING. UPON LANDING THE NLG COLAPSED UPON INSPECT BY MAINT, IT WAS FOUND COTTERPINS WERE MISSING FROM THE NLG SPRING ARM ASSY PIVOT BOLT. ALLOWED THE BOLT TO BACK OUT OF POSITION ALLOW RELEIVING THE TENSION ON THE ARM NOT ALLOWING TO TRAVEL TO FULL DOWN AND LOCK. INSPECTION OF THE BOLT SHOWED NO EVIDENCE OF A BROKEN COTTER PIN OR DAMAGE TO THE THREADS OF THE BOLT. 3 WASHERS REMAINED ON THE THREAD SIDE OF THE BOLT. 1L71 3O 2A13 20010917001332001091700133NM 2001 9 17 2001FA0000294 120010907G6700500N711311 CONTROL ROD DOUG 600N 600N 3027377NM NOTAR FAN DAMAGED D K NONE O OTHER ININSP/MAINT 1 SW99957SD RNO11 DURING REMOVAL OF THE AFT FAN (NOTAR) CONTROL ROD P/N 500N7113-11 WE FOUND SOME CONTACT DAMAGE. IT APPEARS THIS ROD IS MAKING CONTACT WITH THE FAN GEARBOX OUTPUT GEARSHAFT I.D. 1G71 3U NCH3WE 20010917001552001091700155GL 2001 9 17 2001FA0000295 120010726G7100 PISTON AMTR MONG MONG 0565379GL ENGINE BURNED C K NONE O OTHER ININSP/MAINT 1 GL23426RT60 214 NR 1 PISTON ON 2 CYCLE EXPERIMENTAL POWER PLANT BURNED THRU RESULTING IN LOSS OF POWER, RESULTING IN CRASH. DTW 2001 056- C-NR 1 01LA0155. 1Q71 3O NCEXPA1Q71 20010917001352001091700135NM 2001 9 17 2001FA0000296 120010907G6700500N711311 CONTROL ROD DOUG 600N 600N 3027377NM NOTAR FAN DAMAGED D K NONE O OTHER ININSP/MAINT 1 SW99958SD RNO18 DURING REMOVAL OF THE AFT FAN (NOTOR) CONTROL ROD P/N 500N7113-11 WE FOUND SOME CONTACT DAMAGE. IT APPEARS THIS ROD IS MAKING LIGHT CONTACT WITH THE FAN GEARBOX OUTPUT GEARSHAFT I.D. AND THE FAN SUPPORT SHAFT I.D. 1G71 3U NCH3WE 20010917001562001091700156NM 2001 9 17 2001FA0000297 120010829G6230A4801 BOOT ROBSIN ROBSINR22 R22BETAII 7640110NM LYC O360 VO360* 41514EA SWASHPLATE SPLIT D K NONE O OTHER ININSP/MAINT 1 NM022223P153 3573 2962 FOUND SWASHPLATE BOOT SPLIT OPEN AT THE CENTER FOLD. SPLIT WAS APPROX 4 TO 6 INCHES IN LENGTH. 1G71 3O3 O H10WE 1E1 20010918000012001091800001SO 2001 9 18 2001FA0000298 120010626G272062701008 CONTROL CABLE PIPER PA32 PA32301T 7103209SO RUDDER BROKEN G K NONE O OTHER ININSP/MAINT 1 EA118108W 328024002 DURING ANNUAL INSPECTION, FOUND LEFT AFT RUDDER CABLE TURNBUCKLE THREADED SWAGED END BROKEN AT THREADED END THAT SCREWS INTO TURNBUCKLE BARREL. SAFETY WIRE WAS ONLY THING THAT PREVENTED COMPLETE LOSS OF RUDDER CONTROL. 1L71 3O A3SO 20010919002512001091900251GL 2001 9 19 2001FA0000300 220010623G7200 ENGINE BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL NACELLE MALFUNCTIONED C A UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW9934698 4324 DEPARTING THE AIRPORT, THE ENGINE FLAMED OUT OR SURGED. THE ENGINE WAS RUN ON A TEST CELL. TEST CELL SHOWED: 1)A CYCLING ANTI-ICE VALVE SOLENOID. 2) A RICH FUEL FLOW. 3) A WARPED OUTER COMBUSTION CHAMBER. THIS TOGETHER, COULD CAUSE A SURGE. 1G71 3U3 U H2SW E4CE 20010919002532001091900253GL 2001 9 19 2001FA0000301 220010727G7320 SPRING BENDIX BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL CONTROL ARM DEFECTIVE C K NONE O OTHER ININSP/MAINT 1 SW993209G 1694 330958 51567 895634 THE FUEL CONTROL OVERCENTER SPRING IS SO STRONG THAT IS WILL RUN THE RPM AND TOUQUE UP UNCOMMANDED. THIS TIME IT CAUSED AN OVER TORQUE OF 115 PERCENT FOR 1 SECOND. 1G71 3U3 U H2SW E1GL 20010919000032001091900003SO 2001 9 19 2001FA0000302 120010702G716071713 TUBE PIPER PA44 PA44180 7104402SO LYC O360 LO360E1A6 41514EA NR 3 CYLINDER CRACKED C K NONE O OTHER ININSP/MAINT 1 SW159290P1508 99 4496019 RL48371A FOUND NR 3 INTAKE TUBE LEAKING AT 100 HOUR INSPECTION. REMOVED TUBE AND FOUND A CRACK AT FLANGE CRACK APPEARS TO HAVE BEEN REPAIRED BUT WELD DOESNT COVER THE WHOLE CRACK. 1L72 3O3 O A19S0 E286 20010919000012001091900001EA 2001 9 19 2001FA0000305 220010918G8510LW13792 SEAL PIPER PA30 PA30 7103002SO LYC O320 IO320B1A 41508EA HARTZLHCE2Y HCE2YL2 GL ENGINE FAILED C A UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW997331Y 80 30292 L76455 DURING A CROSS-COUNTRY FLIGHT BETWEEN CNO AND SPF (31 AUG 01 THRU 3 SEP 01), OIL STREAKS FROM THE NOSE BOWLS OF BOTH ENGINES INCREASED WITH EACH LEG. UPON RETURN TO CNO, COWLS AND PROPELLERS HAVE BEEN REMOVED. DURING INSPECTION OF ENGINE NOSE SEALS, BOTH SEALS HAVE BEEN "BLOWN OUT" OF THE CASE, AND ARE HANGING FROM THE CRANKSHAFT BETWEEN THE CASE AND PROP FLANGE. BOTH ENGINES HAVE 80 HOURS SINCE OVERHAUL BY LYCOMING. ENGINE OIL ANALYSIS WILL BE PERFORMED AND FILTERS CUT OPEN FOR INSPECTION. 1L72 3O3 O A1EA 1E12 5 CP9EA 20010919000022001091900002CE 2001 9 19 2001FA0000307 120010918G5280 BRACKET BEECH 36 A36 1151604CE MLG DOOR CRACKED A K NONE O OTHER ININSP/MAINT 1 SO15373DR E3373 WHILE PERFORMING ANNUAL INSPECTION A CRACKED BRACKET WAS FOUND AT THE REAR RIGHT INBOARD GEAR DOOR HINGE. UPON REMOVING THE WING-TO-FUSELAGE CLOSEOUT PANEL IT WAS DISCOVERED THAT THE FORWARD TWO INBOARD GEAR DOOR HINGE BRACKETS WERE ALSO CRACKED. CAUSE UNKNOWN. 1L71 3O 3A15 20010920000032001092000003EA 2001 9 20 2001FA0000309 220010821G7313 INJECTOR CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA ENGINE MALFUNCTIONED C O OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SW17172RC 17280204 ENGINE FAILED TO DEVELOP FULL POWER AFTER LONG POWER OFF DECENT AT HIGH DENSITY ALTITUDE CONDITIONS. CORRECTIVE ACTIONS TAKEN: FUEL INJECTOR SERVO REPAIRED BY CRS/NE2R WO R01-042240. FLOW DIVIDER MODIFIED IAW SI. C/W SI AND SB. 1H71 3O3 ONT3A12 1E10 20010920000062001092000006SO 2001 9 20 2001FA0000310 120010904G292253E19600 VALVE PIPER PA32 PA32300 7103212SO LYC O540 TIO540* 41532EA THERMAL BYPASS MISMANUFACTURED D K NONE O OTHER ININSP/MAINT 1 SW994087R1087 3240405 NUT CAME OFF THE THERMOSTATIC BYPASS VALVE AND FELL INTO THE OIL SUMP. CUSTOMER COMPLAINT, HIGH OIL TEMPERATURE. 1L71 3O3 O A3SO E14EA 20010920000072001092000007CE 2001 9 20 2001FA0000311 120010822G8011S1577A1 CONTACTOR CESSNA182 R182 2072734CE LYC O540 O540* 41532EA STARTER FAILED D K NONE O OTHER ININSP/MAINT 1 NE034373R138 R18200595 CONTACTOR FAILED/ CLOSED CAUSING STARTER TO BURN OUT. THIS IS SECOND FAILURE OF A NEW CONTACTOR IN LESS THAN 140 HOURS. (ONE STARTER CONTACTOR, ONE MASTER CONTACTOR) 1H71 3O3 ORT3A13 E295 20010920000122001092000012EU 2001 9 20 2001FA0000312 120010919G7160430110217 MODULATOR BOLKMS117 BK117B2 5626013EU LYC LTS101LTS101600A 41560NE AIRFLOW LOOSE D K NONE O OTHER ININSP/MAINT 1 NM077059N 7154 WHILE TROUBLESHOOTING ENGINE FOR SURGING PROBLEM. AIRFLOW MODULATOR WAS CHANGED. FILTER ELBOW HAS TO BE TRANSFERED TO NEW MODULATOR. FOUND FILTER SCREEN TO BE LOOSE INSIDE ELBOW AT THIS TIME. BROKEN FILTER HAD NO EFFECT ON THIS SURGING PROBLEM. MUST INSPECT FILTER ELBOW WHEN CHANGING AIRFLOW MODULATOR. 1G72 3U3 UNCH13EU E5NE 20010924000072001092400007EU 2001 9 24 2001FA0000313 120010530G3510A1B0BR14 PRESSURE SWITCH STBROSSD3 SD330 8100602EU OXYGEN SYSTEM LEAKING C U4FMK NONE O OTHER ININSP/MAINT 1 NM05173Z 1 SH3116 WHILE SERVICING THE OXYGEN SYSTEM, THE HIGH PRESSURE TRANSDUCER SHAFT SEAL BLEW OUT. THIS PRESSURE SWITCH IS PART OF AN STC MODIFICATION TO CERTIFY THE AIRCRAFT AS A SD3-30, . THIS IS SECOND OCCURANCE OF THIS FAILURE. THE FIRST FAILURE WAS ASSUMED TO BE THAT THE WRONG PN, LOW PRESSURE TRANSDUCER HAD BEEN INSTALLED. UPON REPLACEMENT OF THE SECOND UNIT TAE MAXIMUM PRESSURE OF 750 PSIG IS FAR BELOW THE 1800 PSIG SYSTEM PRESSURE. 2H72 4T A41EU 20010921000022001092100002GL 2001 9 21 2001FA0000314 320010805G6110HCE5N3 PROPELLER PIAGIOP180 P180 6960204EU PWA PT6 PT6* 52043EA HARTZLHCE5N HCE5N3 GL NR 2 DAMAGED C O OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 WP11705PA347 127 1014 HF42 AIRCRAFT LANDED RENO, PILOTS NOTICED DIFFICULTY GETTING PROP INTO BETA AND SLIGHT VIBRATION DURING ROLLOUT. AT HANGER, PILOTS NOTICED LOWER NG ON NR 1 ENGINE ADN ON SHUTDOWN. NR 1 PROP STAYED IN A FLIGHT PITCH ANGLE WHILE NR 2 PROP WENT TO FEATHER PER NORMAL OPS. ON TEARDOWN AT PROP SHOP, NR 1 PROP WAS FOUND TO HAVE INTERNAL DAMAGE. 1H72 3O3 TRTA59EU E2NE 5 CPZONE 20010920000272001092000027GL 2001 9 20 2001FA0000315 220010801G72306890550 SCROLL BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL COMPRESSOR CRACKED B K NONE O OTHER ININSP/MAINT 1 SW09108FH4205 2770 CAE831748 WHILE TROUBLESHOOTING CAUSE OF HIGH TOT, AIR LEAK WAS DISCOVERED AROUND UPPER PORTION OF COMPRESSOR. FURTHER INVESTIGATION REVEALED A CRACK APPROXIMATELY 3.810 INCHES LONG IN AREA BETWEEN CUSTOMER BLEED AIR PORT AND FORWARD OF DIFFUSER. CRACK DID NOT ORIGINATE AROUND WELD. APPLYING HAND PRESSURE UPON BLEED AIR PORT, THE SCROLL MATERIAL CAN BE SEEN LIFTING UP. A COMBINATION OF VIBRATORY STRESS AND METAL FATIGUE ARE FACTORS. 1G71 3U3 U H2SW E4CE 20010920000022001092000002CE 2001 9 20 2001FA0000316 120010919G7120045100336 MOUNT CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA MCAULY1A103 1A103TCM GL ENGINE GROOVED D K NONE O OTHER ININSP/MAINT 1 SW995362M3357 1003 15284562 L2084215 R776391 1. DURING A ROUTINE INSPECTION, TWO ENGINE MOUNT DIAGONALS WERE FOUND TO HAVE WORN AREAS ON THEM CAUSED BY THE BATTERY TRAY FLEXING DOWN AGAINST THE MOUNT AND FROM A STAINLESS STEEL TAG ON THE OIL PRESSURE LINE.2. THE CLAMP THAT SUPPORTS THE BATTERY TRAY ON THE MOUNT SHOULD BE CHECKED ON A REGULAR BASIS TO MAKE SURE IT IS TIGHT AND WILL NOT ALLOW ANY CONTACT WITH THE MOUNT.3. ALL LINES ADJECENT TO THE MOUNT SHOULD BE CHECKED TO ENSURE THAT NO TAGS WILL CAUSE ANY CONTACT WITH THE MOUNT. 1H71 3O3 ONT3A19 E223 5 NP50GL 20010921000032001092100003GL 2001 9 21 2001FA0000317 320010814G6110B4459 PIN MCAULY CESSNA402 402B 207590PCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C87 GL PROPELLER CRACKED C LU4RK NONE O OTHER ININSP/MAINT 1 SO17403GC 733162 402B0305 733162 PROPELLER SHOWS RELEVENT INDICATION. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010921000042001092100004EU 2001 9 21 2001FA0000318 120010830G5753T700A5755060000 CARRIAGE SOCATATBM TBM700 8682000EU PWA PT6 PT6* 52043EA LEFT FLAB IB WORN C VY2RK NONE O OTHER ININSP/MAINT 1 EA235HT 1950 9 AFTER REMOVAL OF LEFT FLAP, DISCOVERED LEFT INBOARD CARRIAGE, PART LISTED ABOVE AND ACTUATOR NUT COVER, PN T700A2750029000, WORN FROM CONTACT WITH ACTUATOR NUT. WEAR APPEARS TO BE FROM WORN BUSHINGS IN CARRIAGE AND ACTUATOR NUT COVER AS WELL AS WEAR IN LOCATOR PINS IN ACTUATOR NUT. FOUND SAME WEAR IN RIGHT INBOARD FLAP CARRIAGE, PN T700A5755060001 AND ACTUATOR NUT COVER COVER PN T700A2755063000 AND ACTUATOR NUT COVER PN T700A2750029000. 1L71 3T3 TRTA60EU E2NE 20010921000052001092100005SO 2001 9 21 2001FA0000319 220010904G7414 GEAR CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO MAGNETO DAMAGED C K NONE O OTHER ININSP/MAINT 1 AL0554GV 427 20700447 818885R DURING ENGINE RUN UP TO ANALYZE A FUEL FLOW PROBLEM, IT WAS DISCOVERED THAT THE RIGHT MAGNETO WAS DEAD. SUBSEQUENT INVESTIGATION REVEALED THAT THE RIGHT MAGNETO WAS INTERNALLY LOCKED AND FOUND THAT THE MAGNETO DRIVE GEAR AND THE ACCESSORY DRIVE GEAR WAS UNSERVICEABLE. MAGNETO BEING SENT TO MFG FOR EVALUATION. 1H71 3O3 O A16CE E5CE 20010921000062001092100006CE 2001 9 21 2001FA0000320 120010820G3510510010951 LINE CESSNA425 425 2076018CE PWA PT6 PT6* 52043EA OXYGEN SYSTEM DETERIORATED C K NONE O OTHER ININSP/MAINT 1 CE07900MS5390 4250079 LEFT SIDE WALL WAS REMOVED TO INSTALL RADIO EQUIPMENT. THE VERTICAL DUCT FOR AIR TO OVERHEAD WEMAC SHOWED DEFINITE SIGNS OF BURNING AND SEVERE DETERIORATION. UPON FURTHER EXAMINATION, THE OXYGEN LINE CROSSING DUCT HAD SEVERE CORROSION WHERE CONTACT BETWEEN THE LINE AND DUCT HAD OCCURRED, AND HAD 2 HOLES IN THE LINE. WHEN THE OXYGEN WAS TURNED ON, OXYGEN WAS SPRAYED ON DUCT AND BEHIND SIDEWALL OF AIRCRAFT. MANUFACTURED NEW LINE TO REPLACE CORRODED LINE. INSTALLED NEW DUCT. SPIRAL WRAPPED OXYGEN LINE WHERE CONTACT WITH DUCT OCCURS. 1L72 3T3 TRTA7CE E2NE 20010924000082001092400008CE 2001 9 24 2001FA0000322 120010605G242199105921 ALTERNATOR CESSNA206 U206G 2073356CE ENGINE MALFUNCTIONED C O OTHER O OTHER NRNOT REPORTED 1 NE029933Z187 U20606754 OPERATOR REPORTED EXCESSIVE NOISE IN HEADSET FROM RADIOS. TROUBLESHOOTING FOUND NOISE DISAPPEARED WITH ALTERNATOR OFF LINE. FURTHER INVESTIGATION FOUND MAGNETIC COMPASS DEVIATION OF 20 DEGREES WITH ALTERNATOR ON LINE. ELECTRICAL SYSTEM WIRING GROUNDS, BONDING AND SHIELDING CHECKED. IN LINE NOISE FILTERS HAD NO AFFECT ON NOISE EMISSION. INSTALLED THREE ALTERNATORS, SN: A-160134, A-160136, AND A-160130 WITH NO CHANGES IN NOISE OR COMPASS DEVIATION. INSTALLED ALTERNATIVE MFG/ELECTRO SYSTEMS ALTERNATOR, PART NUMBER E3FF10300AA, WHICH ELIMINATED RADIO NOISE AND MAGNETIC COMPASS DEVIATION. 1H71 3O A4CE 20010924000092001092400009CE 2001 9 24 2001FA0000323 120010918G2752505211516 PISTON BEECH BEECH B300 B300 1159232CE FLAP ACTUATOR CRACKED C K NONE K FLUID LOSS ININSP/MAINT 1 SW99988ME4611 935A91 FL77 RIGHT OUTBOARD FLAP ACTUATOR CRACKED AT BASE OF PISTON WHERE THE END PLUG IS ATTACHED. THE CRACK WAS 1.5 INCHES LONG AND RESULTED IN THE LOSS OF THE LUBRICATING OIL FROM OUT OF THE PISTON AND SCREW ASSEMBLY. THE LOSS OF OIL WAS THE FIRST INDICATION OF A PROBLEM, AND IT WAS WHILE INVESTIGATING THE OIL LEAK THAT THE CRACK WAS DISCOVERED.THIS CRACK COULD RESULT IN A SIGNIFICANT LOSS OF STRUCTURAL STRENGTH OF THE ACTUATOR WHICH COULD RESULT IN THE STRUCTURAL FAILURE OF THE ACTUATOR ASSEMBLY. 2L72 4T RTA24CE 20010924000022001092400002SW 2001 9 24 2001FA0000324 120010827G531317031725 STRINGER GULSTM690TP 690D 3970405SW LT WING INBD CORRODED B K NONE O OTHER ININSP/MAINT 1 SW99120EK5552 15026 WHILE REPLACING FUEL BAG, STRINGER 6A, LEFT WING INBOARD WAS FOUND TO BE AFFECTED BY GENERAL SURFACE AND PITTING CORROSION. THE CORROSION ON THE STRINGER WAS LOCATED BETWEEN WING STATION 24 AND 39, AND AFFECTED THE STRINGER UP TO AN APPROXIMATE DEPTH OF .08 INCHES. THE CORROSION WAS POSSIBLY CAUSED BY WATER BEING TRAPPED BETWEEN THE STRINGER AND THE FUEL BAGS. WATER MAY HAVE ENTERED THROUGH WING ACCESS PANELS LOCATED ABOVE FUEL BAGS. THE ADDITION OF DRAIN HOLES IN THIS AREA, AND A POSITIVE SEAL ON UPPER WING INSPECTION PANELS MIGHT PREVENT THIS CORROSION FROM OCCURING. (M) 1H72 3T 2A4 20010924000032001092400003 2001 9 24 2001FA0000325 420010824G6113055032110 SPINNER CESSNA172 172S 2072439CE MCAULY1A170 1A170E GL PROPELLER DAMAGED A K NONE O OTHER ININSP/MAINT 1 SW99435ER 172S8652 NUTPLATE BROKEN OFF. CHANGED NUMEROUS SPINNERS AND BACK PLATES BECAUSE THE PRE-DRILLED HOLES DO NOT LINE UP WITH THE NUTPLATES ON THE SPINNER BACK PLATE. THIS IS A COMMON PROBLEM WITH THIS A/C MODEL R/S. (M) 1H71 3O NT3A12 5 NP857 20010924000042001092400004CE 2001 9 24 2001FA0000326 120010811G5610303 WINDSHIELD CESSNA150 152 2071835CE COCKPIT CRACKED B O OTHER O OTHER NRNOT REPORTED 1 SW99714TW 15279429 WINDSHIELD CRACKED DIRECTLY ABOVE COMPASS BLOCK AND SMALL SECTION 12 INCHES BY 6 INCHES WITH COMPASS ATTACHED. SUSPECT CRACK DEVELOPED ABOVE COMPASS BLOCK, PERHAPS BY FUELER LEANING ON WINDSHIELD, AND THEN CONTINUED TO DEVELOP CRACK UNTIL SECTION LOST INTERGRITY AND FELL INWARD INTO CABIN. (M) 1H71 3O NT3A19 20010924000052001092400005GL 2001 9 24 2001FA0000327 120010829G7120 MOUNT CIRRUSSR SR20 05628AJGL ENGINE DAMAGED D O OTHER O OTHER LDLANDING 1 SW99168CD144 1079 MADE A HARD LANDING, THE AIRCRAFT HAD PORPOISED HITTING HARD ON 2ND OSC. UPON INSPECTION IT WAS FOUND THAT THE LDG SHOCK PUCKS WERE DEFORMED AND THE REBOUND PUCKS, ONE OF WHICH WAS MISSING, WITH THE MOUNT WASHERS BENT. ALSO, THE SHOCK PUCK MOUNT PLATE STUD'S WERE BENT, CLOSER INSPECTION REVEALED LIND SEED OIL AT THE WEB CLUSTER ADJACENT TO THE SHOCK MOUNT PLATE OF THE DIAGONAL SUPPORT TUBE, SHOCK MT SUPPORT TUBE AND A STIFFENER TUBE A DYE-PIN INSPECTION REVEALED A .5 INCH CRACK THROUGH THE WELD AT THE CLUSTER. (M) 1H71 3O NCA00009CH 20010924000062001092400006EA 2001 9 24 2001FA0000328 220010715G8500 BLOCK BEECH 23 B23 1151240CE LYC O360 O360* 41514EA ENGINE CRACKED G O OTHER YJ ENGINE STOPPAGE WARNING INDICATION APAPPROACH 1 SW999815S M1799 2100436A AIRCRAFT WS ON FINAL APPROACH TO OCF, ENGINE WAS NOISY AND QUIT. AIRCRAFT MADE EMERGENCY LANDING ON HORSE RACE TRACK. OPENED COWLING, FOUND 3 INCH CRACK AFT, LEFT, TOPSIDE OF ENGINE BLOCK. ENGINE HAS 2776 HOURS SINCE OVERHAUL. 15 DAYS OUT OF ANNUAL INSPECTION. (M) 1L71 3O3 ORTA1CE E286 20010925000022001092500002CE 2001 9 25 2001FA0000329 120010801G7603AN54A BOLT BEECH 200 B200 1152922CE PWA PT6 PT6A42 52043NE ENGINE CONTROL BACKED OUT C K NONE O OTHER ININSP/MAINT 1 NM07424RA2393 BB1583 AN5-4A BOLT IN BOTTOM PIVOT POINT ROD ATTACHMENT BACKED OUT CAUSING LOSS OF ENGINE CONTROL. AN936B516 LOCK WASHER WAS PRESENT. 1L72 4T4 T A24CE E4EA 20010925000032001092500003GL 2001 9 25 2001FA0000330 220010817G7230230397911 SPLINE ADAPTER AGUSTAA109 A109A2 0260120EU ALLSN 250C 250C20B 03013GL COMPRESSOR ASSY FAILED C LN3RO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 NM0155NW 153481814 7267 CAE834892 ENGINE SHUTDOWN DURING FLIGHT DUE TO FLAMEOUT. CAUSE: FAILURE OF SPLINED ADAPTER IN COMPRESSOR ASSEMBLY. 1G72 3U3 U H7EU E4CE 20010925000042001092500004SO 2001 9 25 2001FA0000331 120010806G3230PA402427 BOLT PIPER PA23 PA23250 7102308SO LYC O540 IO540* 41532EA DRAGLINK BROKEN G K NONE O OTHER ININSP/MAINT 1 SO15638879000 277854032 BOLT SHEARED IN HALF, ALLOWING RIGHT MAIN LANDING GEAR TO COLLAPSE ON LANDING ROLL. BOLT SUSPECTED TO BE ORIGINAL. 1L72 3O3 O 1A10 1E4 20010925001092001092500109 2001 9 25 2001FA0000332 420010924G25651061323418 SLIDE BOEING737 737 UTILSYSNM SERVICE DOOR FAILED B K NONE O OTHER ININSP/MAINT 1 SW15 23812 LT AFT SERVICE DOOR SLIDE FAILED TO FULLY INFLATE, WHILE COMPLYING WITH BOEING TASK CARD B25-61-35-C, OPERATIONAL CHECK OF ESCAPE SLIDE SYSTEMS. BOTTLE PSI WAS IN RED RANGE PRIOR TO TEST. 2L72 4F RTA16WE 20010925000012001092500001CE 2001 9 25 2001FA0000333 120010902G3244505C66 TIRE BEECH 58 58P 1152744CE MLG FAILED G O OTHER O OTHER TOTAKEOFF 1 SW15582TA1208 905 TJ191 NOSE TIRE FAILED AND NOSE GEAR COLLAPSED. 1L72 3O A23CE 20011001000152001100100015CE 2001 10 1 2001FA0000337 120010813G321124900022 BUSHING CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA GEAR ACTUATOR FAILED B K NONE O OTHER ININSP/MAINT 1 SO135199U137 172RG0279 L1358536A BUSHING , INSTALLED ON MAIN GEAR ACTUATOR AS PART OF AD, HAS WORKED ITS WAY OUT OF HOUSING. PART HAS 137 HOURS SINCE INSTALLED. THIS IS SECOND BUSHING FOUND BAD WITH FEW HOURS. 1H71 3O3 O 3A17 E286 20011001000162001100100016CE 2001 10 1 2001FA0000338 120010730G3230244110010 PIVOT CESSNA172 172RG 2072438CE LYC O360 VO360* 41514EA RT MLG BROKEN B K NONE O OTHER ININSP/MAINT 1 SO139656B921 172RG0949 RIGHT MAIN LANDING GEAR PIVOT PN 24411001-10 BROKEN, SHEARING OFF GEAR FROM PIVOT. THIS PART WAS INSTALLED ON 01/20/2000, BEING THE NEW IMPROVED PIVOT. ON 05/28/2001 PIVOT WAS INSPECTED AND DYE PENTRANT FOR CRACKS PER AD AND SB. SERVICE KIT 172-151 INSTALLED. 113 HOURS LATER ON 07/27/2001 PIVOT BROKE. AIRCRAFT LANDED WITH NO DAMAGE. 1H71 3O3 O 3A17 1E1 20011002000072001100200007 2001 10 2 2001FA0000339 420010712G2562 LEAD BBAVIA7 7EC 2110120SW CONT C90 C90* 17009SO ELT BATTERY SEVERED D K NONE L NO TEST ININSP/MAINT 1 AL014392C 7EC421 NEGATIVE LEAD FROM LOWER BATTERY COMPARTMENT TO TRANSMITTER WAS SEVERED DUE TO CORROSION. LOWER AND UPPER BATTERY. CONTACTS WERE CORRODED AND PLATING HAD FLAKED OFF. ONE OF THE EIGHT DURACELL BATTERIES WAS DEAD BUT NO CORROSION ON IT AND HAD NO BATTERY LEAKAGE. THIS FINDING WAS MADE DURING THE ANNUAL INSPECTION ON THIS AIRCRAFT. THE BATTERIES WERE ALL WITHIN THEIR DUE DATES. 1H71 3O3 O A759 E252 20011001000172001100100017CE 2001 10 1 2001FA0000340 120010801G2752505212224 ACTUATOR BEECH 200 B200 1152922CE PWA PT6 PT6* 52043EA RT TE FLAPS CRACKED D K NONE O OTHER ININSP/MAINT 1 SW01711HA1818 BB1417 NORMAL FLIGHT OPERATION THE CENTER SHAFT OF THE ACTUATOR CRACKED THE ENTIRE LENGTH CAUSING FLAP BOUNCING SIMILAR TO BAD ROLLERS. RECOMMEND INSPECTING TOP AND BOTTOM OF ACTUATOR CENTER SHAFT DURING REGULAR PHASE INSPECTIONS. 1L72 4T3 T A24CE E2NE 20011001000182001100100018CE 2001 10 1 2001FA0000341 120010822G7921537312 PLATE CESSNA310 310L 2074230CE CONT O470 IO470D 17026SO OIL COOLER WRONG PART G O OTHER WJ INADEQUATE Q C WARNING INDICATION NRNOT REPORTED 1 NM092209F 310L0009 ENGINE HAD LOST OIL PRESSURE DURING FLIGHT. AFTER A SAFE LANDING IT WAS DETERMINED THAT THE OIL HAD LEAKED OUT FROM THE BETWEEN THE OIL COOLER PLATE AND THE ENGINE. THE OIL COOLER PLATE ATTACHMENT NUTS WERE FOUND TO BE LOOSE. THE GASKET BETWEEN THE PLATE AND THE ENGINE WAS THE INCORRECT ONE. CONSULT THE APPROPRIATE PARTS BOOK AND INSTALL THE CORRECT PART. PROPERLY TORQUE ALL FASTENERS TO THE CORRECT SPECIFICATIONS. 1L72 3O3 O 3A10 3E1 20011001000192001100100019CE 2001 10 1 2001FA0000342 120010806G215073838430 ACM CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL CABIN COOLING SEIZED G O OTHER J WARNING INDICATION NRNOT REPORTED 1 SW11750EC1113 7500007 FORWARD AIR CYCLE MACHINE SEIZED DURING ROUTINE USAGE. PROBABLE CAUSE IS BEARING FAILURE. UNIT WAS OPERATED NORMALLY, AND WAS SERVICED AS SCHEDULED. 2L72 4J4 FRTT00007WITE6CH 20011001000202001100100020CE 2001 10 1 2001FA0000343 120010927G29106000100369 LINE LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE HYD SYSTEM FAILED G O OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP01991DB661 177 LEFT HYDRAULIC PRESSURE LINE FROM ENGINE TO HYDRAULIC MANIFOLD BROKE AT FLARE. 3 MILE FINAL EMPTIED HYDRAULIC RES INTO EQUIPMENT BAY/BAGGAGE COMPT. LINE REMOVED AND SENT TO MFG FOR EVALUATION. NOTE: RIGHT HYDRAULIC PRESSURE LINE REMOVED AND REPLACED AS WELL AND SENT IN FOR EVALUATION. 2L72 4F4 FRTA10CE E35NE 20011002000082001100200008SO 2001 10 2 2001FA0000344 120010815G2121313B57 ARMATURE DYNAMICAIR PIPER PA31 PA31P350 7103111SO FAN WRONG PART G K NONE W INADEQUATE Q C ININSP/MAINT 1 WP23CFZIC 702 FAN RETURNED TO MFG FOR OVERHAUL, THE FAN WAS DISASSEMBLED AND FOUND TO HAVE AN ARMATURE OF NOT MFG DESIGN. INSTALLED THE ARMATURE LAMINATIONS ARE NOT COATED, ALLOWING THE ARMATURE TO RUST. THE WINDINGS HAVE EXCESSIVE COATING WHICH CAUSED THE ARMATURE TO RUB THE BRUSH HOLDER. THIS WAS COMPENSATED BY SOMEONE REPOSITIONING THE BRUSH HOLDER FURTHER AWAY FROM THE COMMUTATOR WHICH CAUSED AN IN ACCURATE BRUSH LOAD. 1L72 3O RTA8EA 20011001000362001100100036GL 2001 10 1 2001FA0000345 220010304G8510 BEARING AMTR LANCARLANCAIRES GL AMTR CHEVY8CHEVYV8 GL BELT DRIVE FAILED C O OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP07350N ES0261 1C947072 FLYING AT 5000 FEET, SAW SMOKE COME OUT OF FRONT OF COWL. PULLED POWER BACK. SMOKE QUIT. INCREASED POWER TO TRY TO MAKE AIRPORT. PROPELLER QUIT TURNING. AFTER CRASH, BELT MOSTLY GONE. LOOKS LIKE LOWER FRONT BEARING ON DRIVE SEIZED OR OVER HEATED AND CAUSED THE BELT TO FAIL. 1L71 3 V EXPA1L71EXPE3V 20011001000382001100100038SO 2001 10 1 2001FA0000346 120010726G32136531904 CYLINDER PIPER PA28 PA28180 7102808SO LYC O360 VO360* 41514EA LANDING GEAR CRACKED C K NONE O OTHER ININSP/MAINT 1 GL13152997733 287305051 CYLINDER, LANDING GEAR STUB AXLE AND OLEO PISTON ASSY 1L71 3O3 O 2A13 1E1 20011001000392001100100039SO 2001 10 1 2001FA0000347 120010725G32137873805 AXLE PIPER PA28 PA28180 7102808SO LYC O360 VO360* 41514EA PISTON ASSY CRACKED C K NONE O OTHER ININSP/MAINT 1 GL13152997733 287305051 CYLINDER, LANDING GEAR STUB, AXLE AND OLEO PISTON ASSY 1L71 3O3 O 2A13 1E1 20011001000542001100100054CE 2001 10 1 2001FA0000348 120010727G2435 BEARING LUCAS LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP STARTER GEN FAILED C O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION NRNOT REPORTED 1 GL13100KK679 97514 065 AIRCRAFT EXPERIENCED RIGHT GENERATOR FAILURE. GENERATOR LINE CONTACTOR FAILED TO OPEN AUTOMATICLY AND CREW WAS UNABLE TO SELECT GENERATOR OFF. RIGHT AIRCRAFT MAIN POWER BUSS EXPERIENCED SPIKING WHICH RESULTED IN DAMAGING 3 OR THE MAIN POWER DISTRIBUTION PANELS ALONG WITH MELTING THE SOLDER OUT OF THE STARTER/GENERATOR SPEED PICKUP CONNECTOR. CREW ENDED UP HAVING COMPLETE LOSS OF RIGHT MAIN BUSS AND ASSOCIATED SYSTEMS. 2L72 4F4 FRTT00008WIE6WE 20011001000552001100100055EA 2001 10 1 2001FA0000349 220010723G8530 CYLINDER PIPER PA31 PA31P350 7103111SO LYC O540 TIO540V2AD 41532EA NR 5 DAMAGED C A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 EA09184JB2307 31P8414049 L856061A WHILE IN CRUISE CONFIGURATION AT 16500 FEET, 32 INCH HG/2200 RPM THE PILOT NOTED A SHUTTER FOLLOWED BY A DROP IN MANIFOLD PRESSURE RESULTED. WITHIN 60 SECONDS THE MANIFOLD PRESSURE FLUCTUATED RAPIDLY, FOLLOWED BY A LOUD BANG. THE ENGINE WAS SECURED AND AN UNEVENTFUL LANDING FOLLOWED. INSPECTION OF THE ENGINE REVEALED THE NR 5 CYLINDER ASSEMBLY HAD SEPARATED FROM THE ENGINE. THE PISTON AND CONNECTING ROD WERE ATTACHED AND IN THE CYLINDER, THE ROD CAP HAD SEPARATED AND WAS FOUND IN THE CRANKCASE. 1L72 3O3 ORTA8EA E14EA 20011001000562001100100056CE 2001 10 1 2001FA0000350 120010710G771347083621 CONTROLLER CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO INTERNAL FAILED D K NONE O OTHER ININSP/MAINT 1 SW01525RH 358 402C0525 823318R UNABLE TO CONTROL MANIFOLD PRESSURE 1L72 3O3 O A7CE E8CE 20011001000572001100100057CE 2001 10 1 2001FA0000351 120010907G49903862332113 COVER GARRTT RAYTHNDH125 HAWKER800XP CE GARRTTTFE731TFE7315BR WP APU OIL FILTER BROKEN C K NONE O OTHER ININSP/MAINT 1 SW09811TA T601 258516 T601 WHEN REMOVING THE APU OIL FILTER COVER, THE RETAINING EARS THAT HOLD THE END OF THE COVER, THE RETAINING EARS THAT HOLD THE COVER IN PLACE BREAKS OFF. RECOMMEND MANUFACTURING A FILTER COVER WITH A HEX FITTING ON THE END OF THE COVER, IT WOULD MAKE IT EASIER TO TWIST OFF THE COVER. 2L72 4F4 FRTA3EU E6WE 20011002000092001100200009CE 2001 10 2 2001FA0000352 120010924G2460 BUSS CESSNA172 172R 2072401CE ELECTRICAL DAMAGED C A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW992458G870 17280893 PILOT REPORTED LOSS OF HALF OF AVIONICS BUSS, INCLUDING ONE NAV/COM AND GPS AND SMOKE AND A BAD ODOR IN THE COCKPIT. WIRE NR 2H1002 (22 GAUGE) BURNED FROM THE NAV. LIGHT C/B SWITCH TO PIN 11 OF THE JC001 CONNECTOR AND FROM PC001, PIN 11 TO JV001, PIN 1. THE RED LEAD FROM THE TAIL NAV LIGHT ASSEMBLY SHORTED OUT TO A NUT-PLATE ON THE RUDDER THAT HOLDS THE RUDDER TIP ON, BUT DOES NOT DISPLAY EVIDENCE OF OVERHEATING, OTHER THAT THE PINHEAD SIZED BURN MARK. 1H71 3O NT3A12 20011002000102001100200010EU 2001 10 2 2001FA0000353 120010928G2720PC43301A1 CONTROL CABLE RHNFLUEXT300EA300L 70218DGEU RUDDER LOOSE D K NONE O OTHER ININSP/MAINT 1 SW9925AP 66 66 094 ROUTINE ANNUAL INSPECTION REVEALED AFT RUDDER CABLE THIMBLE EYES WERE LOOSE IN THE LOOP AT THE ATTACHMENT TO THE RUDDER. THE THIMBLE COULD BE REMOVED FROM THE LOOP. THE NICROPRESS CRIMP WAS MADE TOO FAR FROM THE THIMBLE. REPLACED THE RUDDER CABLES WITH NEW ONES. 1M71 3O NCEA67U 20011002000122001100200012CE 2001 10 2 2001FA0000354 120010806G57530523921 ROLLER CESSNA172 172N 2072434CE TE FLAPS DAMAGED B A UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 SW99737ME 17269516 AIRCRAFT RETURNED FROM FLIGHT WITH RIGHT FLAP DAMAGED. FLAP WAS STUCK AT ABOUT 20 DEGREES AND WAS TWISTED AND JAMMED IN TRACKS. FOUND INBOARD AFT. ROLLER WORN AND SPLITTING. INBOARD FLAP TRACK ALSO DAMAGED. SUSPECT WORN OUT FLAP ROLLER OR EXCESSIVE AIRCRAFT SPEED WHEN LOWERING FLAPS. RECOMMENDED YEARLY OR 500 HOURS FLAP ROLLER INSPECTION AND LUBE. (M) 1H71 3O NT3A12 20011002000132001100200013SO 2001 10 2 2001FA0000355 120010817G28233138400 CONTROL CABLE PIPER PA23 PA23250 7102308SO LYC O540 IO540* 41532EA TANK SELECTOR BROKEN D K NONE O OTHER ININSP/MAINT 1 NE0323TA 277854114 CABLE BROKE JUST BELOW SWIVEL FITTING OR THE RIGHT WING FUEL TANK SELECTOR HANDLE. RECOMMEND THAT THE AD INCLUDE THE FUEL SELECTOR CABLE ALSO BE INSPECTED. 1L72 3O3 O 1A10 1E4 20011002000212001100200021EA 2001 10 2 2001FA0000356 220010829G8530AEL6510241 CYLINDER HEAD PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA ENGINE CRACKED B MW2RK NONE O OTHER ININSP/MAINT 1 GL172366W953 288516046 R917539A CYLINDER CRACKED FROM TOP SPARK PLUG AROUND OUT SIDE OF EX SEAT TO BOTTOM SPARK PLUG HOLE. SAME AS ALL THE REST. 1L71 3O3 O 2A13 E274 20011002000222001100200022SO 2001 10 2 2001FA0000357 120010830G7170S6250 VALVE PIPER PA34 PA34200T 7103406SO CONT O360 LTSIO360E 17025SO OIL DRAIN MISINSTALLED D K NONE W INADEQUATE Q C ININSP/MAINT 1 EA1344RK 347770296 THE OIL SUMP DRAIN PANEL (ON THE LOWER COWL) WAS INSTALLED BACKWARDS. THIS ALLOWED THE OIL DRAIN VALVE TO CONTACT THE PANEL AND DEPRESS THE VALVE. CONTACT ONLY OCCURS WHEN THE ENGINE IS RUNNING. 1L72 3O3 O A7SO E9CE 20011002000232001100200023EA 2001 10 2 2001FA0000358 220010912G8500LW16819 CRANKCASE CESSNA172 172N 2072434CE LYC O320 O320* 41508EA ENGINE CRACKED B NDDGK NONE O OTHER ININSP/MAINT 1 EA07739LK 17270626 R839376T ENGINE FOUND TO BE CRACKED. THE FRACTURE OCCURRED ON THE LEFT HAND CASE HALF RUNNING FROM THE 9 OCLOCK POSSITION OF THE NR 2 CYLINDER PAD TO THE MAIN BEARING BOSS AREA. THIS CRACK WAS CAUSED BY POOR SCAVENGING OF AIR DURING THE CASTING PROCESS. 1H71 3O3 ONT3A12 E274 20011002000242001100200024EA 2001 10 2 2001FA0000360 220010713G7414 MAGNETO PIPER PA28 PA28R201 7102816SO LYC O360 IO360A1A 41514EA ENGINE SEPARATED B MGFRA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 EA2347337 28R7737159 TRANSIENT PILOT LANDED WITH LOSS OF OIL PRESSURE. OIL WAS OVER AIRCRAFT BELLY AND ENGINE COMPARTMENT. INVESTIGATION FOUND RIGHT MAGNETO HANGING BY DISTRIBUTOR WIRES AND LEFT MAGNETO VERY LOOSE. AIRCRAFT ANNUAL APPROXIMATELY 20 HOURS PRIOR. CONCLUSION: MAGNETOS MAY NOT HAVE BEEN RETIGHTENED DURING ANNUAL-IF THEY WERE RETIMED. 1L71 3O3 O 2A13 1E10 20011002000252001100200025CE 2001 10 2 2001FA0000361 120010920G5712 RIB CESSNA210 T210L 2073449CE CONT O520 TSIO520* 17040SO LEFT WING CRACKED B BIORK NONE O OTHER ININSP/MAINT 1 EA23375AB3505 21061352 LEFT WING RIB CRACKED WHERE LEFT FLAP BELLCRACK SUPPORT BRACKETS ARE MOUNTED, CRACK RUNS FROM INBOARD LOWER SUPPORT BRACKET RIVET HOLE APPROX. ONE(1) INCH IN LENGTH DOWN AND TO THE LEFT. PROBABLE CAUSE: FLAPS EXTENDED AT TOO HIGH OF AN AIRSPEED. 1H71 3O3 O 3A21 E8CE 20011002000272001100200027CE 2001 10 2 2001FA0000362 120010920G32463190 TUBE CESSNA185 A185F 2072821CE LYC O540 TIO540* 41532EA FLOAT PUMP DISCONNECTED D O OTHER P NO WARNING INDICATION NRNOT REPORTED 1 AL05185JS 18503095 ONE AFT COMPARTMENT PUMP OUT TUBE WAS DISCONNECTED NOT ALLOWING THE WATER TO BE PUMP FROM FLOAT. AIRCRAFT SWAMPED RIGHT FLOAT ON TURN AND STARTED TO SINK. 1H71 3O3 O 3A24 E14EA 20011002000282001100200028EA 2001 10 2 2001FA0000363 220010829G7414 SHAFT CESSNA172 172K 2072430CE LYC O320 O320* 41508EA MAGNETO SHEARED D O OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 GL137071G521 17258771 PILOT REPORTED 700 RPM DROP ON LEFT MAGNETO. MAGNETO REMOVED AND INSPECTED. FOUND DRIVE SHAFT/ MAGNETO/ ROTOR SHEARED IN HALF. MAGNETO REPLACED. 1H71 3O3 ONT3A12 E274 20011002000012001100200001CE 2001 10 2 2001FA0000364 120010928G28106207010144 LINE CESSNA650 650 2076802CE HYD SYSTEM CHAFED B K NONE WK INADEQUATE Q C FLUID LOSS ININSP/MAINT 1 GL1572ST 5921 6500072 THE AIRCRAFT WAS MANUFACTURED WITH THE HYDRAULIC PRESSURE AND RETURN LINES CONTACTING EACH OTHER. THE RETURN LINE EVENTUALLY WORE THROUGH AND STARTED TO LEAK, THE PRESSURE LINE WAS ALSO SEVERLY WORN AND REQUIRED REPLACEMENT. THE REPAIR IS EXTENSIVE BECAUSE THE LINES ARE SWAGED REQUIREING THE REPLACEMENT OF MANY LINES AND FITTINGS. NOT ALL OF THESE LINES ARE AVAILABLE FROM CESSNA. THE AREA WHERE THE LINES ARE IN CONTACT CAN BE VERY DIFFICULT TO INSPECT. IN MOST CASES THE AREA IS ONLY VISIBLE WITH A MIRROR. THEY CHECKED ANOTHER CESSNA 650 THAT WAS IN THE SHOP AND IT HAD ONLY .010 BETWEEN THE LINES. IT WOULD BE ADVISABLE FOR OTHER OPERATORS OF THIS MODEL AIRCRAFT TO HAVE THESE LINES INSPECTED AT THE EARLIEST POSSI2L72 4F A9NM 20011002000022001100200002CE 2001 10 2 2001FA0000365 120010813G2730 SCREW CESSNA441 441 2076020CE ELEVATOR CONTROLLOOSE B O OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 SW99181MD10133 4410295 EXCESS FRICTION IN PITCH, (ELEVATOR) CONTROL. DISASSEMBLY OF CONTROL, REVEALED RETAINING SCREW HAD BACKED OUT OF NYLON SLIDE. UNCONTAINED PARTS OCCASSIONALLY POSITIONED THEMSELVES THROUGH OUT NORMAL MOTION OF THE CONTROL SO AS TO CREATE EXCESS FRICTION. (M) 1L72 3T RTA28CE 20011002000032001100200003SO 2001 10 2 2001FA0000366 120010820G1400 TAPE PIPER PA28 PA28140 7102802SO CARB SHROUD LOOSE B O OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SW999831W 2823335 PILOT COMPLAINED OF ROUGH RUNNING ENGINE LOW STATIC RPM ONLY OBTAINABLE BY LEANING MIXTURE, FOUND APPROX 1 SQUARE INCH OF TIN FOIL LODGED IN CARB VENTURI, EXAMINATION OF HEAT SHROUD ON EXHAUST PIPE RUB AREA WAS WRAPPED WITH ALUMINUM FOIL TAPE TO TAKE UP PLAY, MORE LOOSE FOIL READY TO DISLODGE AND MAKE ITS WAY TO SNUFF AIR IN CARB. (M) 1L71 3O 2A13 20011002000042001100200004 2001 10 2 2001FA0000367 420010816G2312VP10 ANTENNA BEECH 33 35C33 1151408CE VHF SYSTEM CRACKED B O OTHER O OTHER APAPPROACH 1 SW996124V CD856 A/C ARRIVED WITH AN ANTENNA 'FLUTTERS' SQUAK. UPON INSPECTION OF VHF COMM ANTENNA, IT WAS NOTED THAT THE ANTENNA WAS INSTALLED WITH NO SUPPORTING DOUBLER. UPON ANTENNA REMOVE, A 5.5 INCH RADIAL CRACK WAS DISCOVERED AROUND THE ANTENNA BASE. THE ADJOINING STRINGER IS ALSO CRACKED. THE SKIN UNDER THE ANTENNA AS CORRODED DUE TO NO SEALANT BEING APPLIED TO THE ANTENNA BASE AFTER INSTALLATION. (M) 1L71 3O 3A15 20011002000052001100200005EA 2001 10 2 2001FA0000368 220010625G8530 EXHAUST VALVE PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA ENGINE FAILED D A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW99477021147 287890120 THE AIRCRAFT WAS AT NORMAL CRUISE, THE PILOT STATED THAT IT STARTED TO LOSS POWER AND RAN ROUGH. AFTER LANDING AT A ALTERNATE AIRPORT THE AIRCRAFT STOPPED RUNNING. AFTER PULLING THE CYLINDER, THE TOP OF THE EXHAUST VALVE WAS MISSING. THE STEM AND RETAINING CLIPS WHERE STILL IN PLACE. THE TOP OF THE VALVE HAD BEEN FOUND IN THE INTAKES. CAUSE OF THE MALFUNCTION UNKNOWN. TOTAL TIME ON THE VALVE IS 1146.8 HOURS. (M) 1L71 3O3 O 2A13 E286 20011003000032001100300003GL 2001 10 3 2001FA0000370 120010829G551081611 TERMINAL AVIAT A1 A1B GL LYC O360 O360A1D 41514EA HORIZONTAL STAB BROKEN B V2ARK NONE O OTHER ININSP/MAINT 1 AL03711HY 2025 FORWARD HORIZONTAL STABILIZER STRUT UPPER TERMINAL WAS FOUND BROKEN ON PREFLIGHT. BREAK OCCURED ON .3125 (5/16) THREADED PORTION AT UPPER END OF THREADS. 1H71 3O3 ONCA22NM E286 20011003000042001100300004CE 2001 10 3 2001FA0000371 120011002G3230 LANDING GEAR CESSNA177 177RG 2073709CE LYC O360 IO360A1A 41514EA MAINS FROZEN B BLBRK NONE O OTHER ININSP/MAINT 1 GL178253G 177RG0153 NOSE GEAR IN UP POSITION HAD HYDRAULIC LOCK. KEEPING THE NOSE GEAR IN THE UP POSITION EXTENDED GEAR, MAIN GEAR LOCKED DOWN, NOSE GEAR DID NOT FULLY EXTEND DUE TO HYDRAULIC LOCK IN THE RETURN LINE. 1H71 3O3 O A20CE 1E10 20011003000052001100300005CE 2001 10 3 2001FA0000372 120010824G531224120043 BULKHEAD CESSNA172 172RG 2072438CE LYC O360 VO360* 41514EA FUSELAGE CRACKED G K NONE O OTHER ININSP/MAINT 1 WP156190R 172RG0110 FOUND CRACKS ON RIGHT AND LEFT HAND SIDES OF BULKHEAD JUST FORWARD OF BATTERY. 1H71 3O3 O 3A17 1E1 20011003000062001100300006CE 2001 10 3 2001FA0000373 120010829G272098820104 ROD CESSNA172 172P 2072436CE LYC O320 O320* 41508EA PILOTS LT PEDAL FAILED B FFGRK NONE O OTHER ININSP/MAINT 1 SO33514035726 17274308 ACTUATION ROD TO RUDDER PEDAL BROKE AT BASE OF THREADS AT FORK. THERE WAS NO DAMAGE TO RUDDER PEDAL OR BRAKE MOUNT FOUND. 1H71 3O3 ONT3A12 E274 20011003000082001100300008 2001 10 3 2001FA0000374 420010212G6122MS914401 GASKET MCAULY AMTR VANS RV8 GL LYC O360 IO360A1B6 41514EA GOVERNOR LEAKING D K NONE K FLUID LOSS ININSP/MAINT 1 WP2788PV 010038 80024 GASKET PN MS914401 THAT IS SUPLIED WITH THE NEW GOVERNOR DOES NOT COVER THE FULL FACE MATING SURFACE OF THE GOVERNOR EXPOSING APPROX. .0625 INCH OF THE LOWER SCREW HOLE. THE LOWER SCREW HOLE INTERSECTS AN OIL PRESSURE CAVITY ON THE ENGINE MATING SERVICE. THE SHORT GASKET LEAKS OIL FROM LOW RPM. DURING AN INITIAL FLIGHT OVER 4 QUARTS OF OIL LEAKED IN LESS THAN 15 MINUTES OF FLIGHT. 1L71 3O3 ONTEXPA1L711E10 20011003000012001100300001CE 2001 10 3 2001FA0000375 120011002G5753 FLAP CESSNA172 172N 2072434CE WING MISINSTALLED C K NONE W INADEQUATE Q C ININSP/MAINT 1 SW9938PA 17270182 PROBLEMS FOUND AFTER RECENT PAINT AND INTERIOR:SEAT BELTS INSTALLED BACKWARDS,RIGHT FLAP INSTALLED WITHOUT ALL SPACERS RESULTING IN DAMAGE TO FLAP,AILERON HINGE PINS NOT SECURED,NOSE TIRE INSTALLED BACKWARDS,FRONT COWLING SCREWS MISSING. 1H71 3O NT3A12 20011003000022001100300002SO 2001 10 3 2001FA0000376 120011002G2400467067 ISOLATOR PIPER PA28 PA28R201T 7102813SO CONT O360 TSIO360FB 17025SO HARTZLHCC2Y HCC2YF1 GL ELECTRICAL BURNED OUT D H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL273543M3150 28R7803176 299526R AM1855 IN CRUISE FLIGHT NOTICED THE AMP GAUGE WAS SHOWING THE ALTERNATOR PUTTING OUT OVER 45 TO 50 AMPS. DME DROPPED OF LINE, LOST THE TRANSPONDER SIGNAL. VFR CONDITIONS AND CANCLED FLIGHT. LANDED AT THE CLOSEST AIRPORT. STARTED AIRCRAFT. RADIOS WORKING. 30 TO 45 MIN INTO THE FLIGHT, AVIONICS STARTED TO DROP OFF LINE. MAINT. TECH FOUND BATTERY WAS DEAD. BATTERY WAS CHARGED AND REINSTALLED. RUN UP OF THE AIRCRAFT SHOWED NO ALT PROBLEM AT ALL AND BUSS VOLTAGE WAS 13.75 BUT STILL HAD 35AMP DRAW. ONE OF FOUR PLASTIC INSULATOR THAT INSULATES THE DIODE & COOLER ASSEMBLY FROM THE HOLD DOWN SCREWS HAD POSSABLY BEEN TIGHTENED TO TIGHT. METAL DIODE ASSY WAS SHORTED TO GROUND. REPLACED THE SCREW AND INSULATOR. 1L71 3O3 O 2A13 E9CE 5 CP920 20011004000012001100400001EU 2001 10 4 2001FA0000377 120010903G5751212111407 LINK CASA C212 C212200 2410304EU GARRTTTPE331TPE331* 01514WP ATTACH BOLT CRACKED C K NONE O OTHER ININSP/MAINT 1 SO15316ST 289 DURING ROUTINE INSPECTION FOUND RIGHT AILERON OUTBOARD HINGE LOOSE. THE OUTBOARD LINK WAS CRACKED AT THE WING ATTACH BOLT LOWER LUG. NO DAMAGE TO THE WING OR AILERON WAS FOUND. 2H72 4T3 TRTA43EU E2WE 20011004000022001100400002 2001 10 4 2001FA0000378 420010927G34972H1002 WIRE CESSNA172 172R 2072401CE NAVIGATION LIGHTBURNED C XVESK NONE L NO TEST ININSP/MAINT 1 SO192458G874 17280893 PILOT REPORTED LOSS OF HALF AVIONICS BUSS, SMOKE AND BAD ODOR IN COCKPIT. T/S, FOUND WIRE BURNT FROM NAV LIGHT C/B SWITCH TO PIN 11 OF THE JC001 CONNECTOR AND FROM PC001, PIN 11 TO JV001, PIN 1. RED LEAD FROM TAIL NAV LIGHT HOUSING SHORTED OUT TO NUT-PLATE ON RUDDER THAT HOLDS RUDDER TIP ON, BUT DOES NOT DISPLAY EVIDENCE OF OVERHEATING, OTHER THAN PINHEAD SIZED BURN MARK. SEVERAL OTHER WIRES WERE DAMAGED WHEN WIRE NR 2H1002 MELTED. NOTE: ALL THREE NAV-LAMPS FEED INTO A SINGLE TWO FOOT LENGTH OF 22 GAUGE WIRE BEFORE CONNECTING THE 5 AMP BREAKER. MOST OF LENGTH OF WIRE TO TAIL IS DAMAGED, LAST SECTION TO BREAKER IS BURNED BARE. THIS SECTION THAT MELTED INTO ADJACENT WIRES IN BUNDLE. ONCE WIRE BURNED TH1H71 3O NT3A12 20011004000032001100400003CE 2001 10 4 2001FA0000379 120010909G5320 PANEL CESSNA177 177B 2073708CE LYC O360 O360* 41514EA TRANSPONDER LOOSE C K NONE O OTHER ININSP/MAINT 1 SW0913519 17702432 OWNER/OPERATOR REPORTED THAT CONTROL YOKE WOULD NOT PULL BACK TO RAISE THE ELEVATOR. ON INSPECTION IT WAS FOUND THAT THE PANEL MOUNT TRAY FOR THE TRANSPONDER ON THE RIGHT SIDE OF THE PANEL HAD DROPPED .2500 OF INCH AND WAS CONTAINING AND RESTRICTING AFT MOVEMENT OF THE CONTROL YOKE. THE AIRCRAFT COULD NOT ROTATE ON TAKEOFF AND IT WAS A CLOSE CALL. AN ADDITIONAL SUPPORT WAS INSTALLED ON THE BACK OF THE TRAY. AVIONICS INSTALLER OVER-LOOKED THE POSSIBILITY OF THE TRAY DROPPING DOWN. UNDER PANEL AREA SHOULD BE INSPECTED AT EACH ANNUAL, 100 HOUR AND AFTER NEW AVIONICS INSTALLATION. 1H71 3O3 O A13CE E286 20011009000252001100900025CE 2001 10 9 2001FA0000380 120010911G32405100106159 LINE CESSNA414 414A 2075907CE CONT O520 TSIO520* 17040SO BRAKE ASSY CHAFED G K NONE K FLUID LOSS ININSP/MAINT 1 CE05414AN4224 414A0819 BRAKE LINE ROUTED UNDER THE CO-PILOTS SEAT PEDESTAL AREA IS CHAFFING ON HEAT DUCT TUBING. SLIDING A 193-6 LOW PRESSURE HOSE OVER THE BRAKE LINE WILL KEEP THE BRAKE LINE FROM DEVELOPING A HOLE. 1L72 3O3 O A7CE E8CE 20011009000262001100900026CE 2001 10 9 2001FA0000381 120010911G32405100106159 LINE CESSNA414 414A 2075907CE BRAKE ASSY CHAFED G K NONE O OTHER ININSP/MAINT 1 CE052702L4375 414A0608 RIGHT BRAKE LINE ROUTED UNDER CO-PILOT SEAT PEDISTAL AREA IS CHAFFING ON HEAT DUCT TUBING. SLIDING A 193-6 LOW PRESSURE HOSE OVER THE BRAKE LINE WILL KEEP THE BRAKE LINE FROM DEVELOPING A HOLE. 1L72 3O A7CE 20011009000272001100900027CE 2001 10 9 2001FA0000382 120010906G3240 BOLT CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA BRAKE CYLINDER MISSING D K NONE O OTHER ININSP/MAINT 1 SW0781JD 4577 172RG1184 L3108636A LEFT LANDING GEAR WOULD NOT EXTEND IN FLIGHT. AIRCRAFT WAS HOISTED UP AND THE GEAR EXTENDED AND LOCKED. FOUND A BOLT MISSING FROM THE LEFT BRAKE CYLINDER. PERFORMED SEVERAL GEAR RETRACTIONS AND OPS CHECKED OK. 1H71 3O3 O 3A17 E286 20011009000232001100900023CE 2001 10 9 2001FA0000383 120010929G2410646655A1 DRIVE GEAR TELEDYNECRIT CESSNA421 421C 2076016CE CONT O520 GTSIO520L 17032SO ALTERNATOR DAMAGED B A UNSCHED LANDING EH VIBRATION/BUFFET ELECT. POWER LOSS-50 PC CRCRUISE 1 SW99112MJ 421C0907 292300R L. ALTERNATOR FAILED DURING FLIGHT AND A VIBRATION WAS NOTED ABOUT 20 MINUTES LATER. THE ENGINE OIL PRESSURE DROPPED ABOUT 25 PSI AND A PRECAUTIONARY LANDING WAS MADE. UPON REMOVAL OF THE ALTERNATOR IT WAS DISCOVERED THE DRIVE HUB WAS NEARLY DESTROYED AND THE DRIVE GEAR BOLTS WERE MISSING AND THE GEAR WAS LOOSE ON THE BULLGEAR SHAFT. THE REMNANTS OF THE DRIVE GEAR WERE LOCATED IN THE OIL PAN ALONG WITH THE CASTLE NUT AND COTTER PIN. (SEE PHOTO)THIS IS THE SECOND OCCURRENCE OF THIS TYPE FAILURE IN THE PAST 2 WEEKS, THE OTHER WAS ON THE I. ENGINE OF A 421C WITH ABOUT 1400 HOURS ON THE ENGINE AND LESS THAN 100 HOURS ON THE ALTERNATOR SMOH. NEITHER ALTERNATOR EXHIBITED ANY BEARING PROBLEMS. WE HAVE BEEN UNABL 1L72 3O3 O A7CE E7CE 20011219001212001121900121GL 2001 12 19 2001FA0000384 220011005G7230230397911 ADAPTER ALLSN AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20F 03013GL COMP COUPLING CORRODED B K NONE O OTHER ININSP/MAINT 1 SW99 2450 CAC30224P 5030 CAE840216 COUPLING HAS EXCESSIVE FRETTING WEAR ON OD SURFACE. CONTINUED OPERATION MAY HAVE CAUSED FAILURE. SAME CONDITION NOTED ON OTHER COUPLINGS OF THE SAME PART NUMBER. THIS PART NUMBER IS CURRENTLY UNDER INVESTIGATION BY ROLLS-ROYCE (ALLISON ENGINE COMPANY)DUE TO FAILURES OF LIKE PARTS. 1G72 3U3 U H11EU E4CE 20011009000242001100900024SO 2001 10 9 2001FA0000385 220011003G8530646279 PISTON CESSNA175 175A 2072504CE CONT O300 GO300C 17022SO MCAULY1B175 1B175MFC GL ENGINE CRACKED D K NONE O OTHER ININSP/MAINT 1 SW99 56291 12558OC 8464 WHILE PREPARING TO INSTALL A NEW STEEL CYLINDER AND PISTON, NOTICED THAT THE NEW PISTON WAS CRACKED ALL THE WAY THROUGH THE FOURTH RING GROOVE. THE PISTON SKIRT WAS ALSO BULGED IN THE AREA OF THE CRACK. 1H71 3O3 O 3A17 E298 5 NP857 20011015000772001101500077 2001 10 15 2001FA0000386 420010918G2300S2870 SWITCH CESSNA182 182S 2072701CE LYC O540 IO540* 41532EA PILOT PTT INOPERATIVE B LC1RO OTHER O OTHER NRNOT REPORTED 1 EA073261M548 18280347 THE PILOTS SIDE PUSH TO TALK SWITCH WENT BAD WITH ONLY 548.0 TACH TIME. REPLACE THE BAD SWITCH WITH A NEW ONE. THE NEW SWITCH WAS BAD ALSO, THEN REPLACED THE NEW SWITCH THE SECOND NEW SWITCH TESTED OK. WHEN INSTALLING SWITCHES, WAS CAREFUL NOT TO OVERHEAT SWITCH. 1H71 3O3 ONT3A13 1E4 20011015000792001101500079SW 2001 10 15 2001FA0000387 120010709G5711 SPAR BBAVIA7 7CCM 21101MWSW CONT C90 C90* 17009SO WING CRACKED D K NONE O OTHER ININSP/MAINT 1 NM012959E 7AC6545 DURING INSPECTION TO COMPLY WITH AD, CRACKS WERE FOUND INBOARD AND LEFT FRONT SPAR, INBOARD END RIGHT REAR SPAR. .001 FEELER GAGE COULD BE INSERTED .1250 OR MORE INTO CRACKS. 1H71 3O3 O A759 E252 20011015000872001101500087 2001 10 15 2001FA0000388 420010711G6113055032110 BULKHEAD CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA MCAULY1A170 1A170* GL SPINNER CRACKED D K NONE O OTHER ININSP/MAINT 1 NM013526J72 172S8829 THE AREA AROUND THE NUTPLATE NEAREST TO THE PROPELLER ON THE AFT SPINNER BULKHEAD HAD CRACKED AND BROKEN FREE OF THE BULKHEAD IN FLIGHT. THE SECTION OF THE SPINNER ATTACHED TO THE BROKEN PIECE WAS PULLED AWAY FROM THE BULKHEAD. THE SPINNER HAD STARTED TO DEVELOPE CRACKES ALONG THE BEND RADIUS. BOTH THE SPINNER AND AFT SPINNER BULKHEAD WERE REPLACE WITH FACTORY NEW. 1H71 3O3 ONT3A12 1E10 5 NP857 20011015000902001101500090SO 2001 10 15 2001FA0000389 120010418G71201020691 SUPPORT AMRGENAA1 AA1 0630610SO LYC O320 O320E2G 41508EA MOUNT CORRODED D K NONE O OTHER ININSP/MAINT 1 NM015985L2229 AA10285 CORROSION DISCOVERED IN UPPER SURFACES OF BOTH LEFT AND RIGHT SUPPORTS. DETECTED BY PREPING THE SUPPORTS FOR PAINT WITH A STAINLESS STEEL WIRE BRUSH AND SLIGHT RAISED LINE WAS NOTICED. PICKING REVEALED A LARGE AREA OF POWDER CORROSION AND EXFOLIATION BELOW THE SURFACE. THE OTHER SUPPORT WAS PICKED AT, THOUGHT THE SURFACE LOOKED OK AND IT WAS ALSO CORRODED AS MUCH AS THE FIRST ONE. THE SUPPORTS MUST BE REPLACED WHICH IS WELL COVERED IN THE AIRCRAFT MM. INNERGRANULAR CORROSION IS USUALLY THE RESULT OF DEFECTIVE HEAT TREATING DURING MANUFACTURING AND THIS PART IS USED ON ALL MODELS OF THIS PRODUCT LINE. 1L71 3O3 O A11EA E274 20011015000912001101500091SO 2001 10 15 2001FA0000390 220010922G7322NA53B CARBURETOR BBAVIA7 7AC 2110102SW CONT A65 A65* 17003SO ENGINE INOPERATIVE G K NONE O OTHER ININSP/MAINT 1 EA1385122 7AC3855 ENGINE FAILURE, BELIEVE DUE TO FUEL STARVATION. GOOD FUEL FLOW UP TO CARBURETOR. NO CONTAMINATION FOUND WITH GASCOLATOR. UPON CARBURETOR DISASSEMBLY FOUND VERY FINE DIRT IN CARBURETOR FUEL STRANER AND FLOAT CHAMBER. ALSO, FOUND MAIN AIR BLEED JET NEARLY TOTALLY OBSTRUCTED WITH GUMMY LIKE FOREIGN MATTER. PROBABLE CAUSE: FUEL FLOW IMBALANCE. ONE EITHER OBSTRUCTION OF AIR JET OR FUEL JET. 1H71 3O3 O A759 E205 20011015000932001101500093CE 2001 10 15 2001FA0000391 120010903G531207126167 BULKHEAD CESSNA182 182N 2072730CE CONT O470 O470R 17026SO REAR FUSELAGE CRACKED G K NONE O OTHER ININSP/MAINT 1 WP199024G6880 18260564 451652 IN COMPLYING WITH AD, (CRACKS AND LOOSE BOLTS IN FIN AND RUDDER) CRACKS WERE FOUND IN THE AREA IN THE AFT BULKHEAD BETWEEN THE RUDDER CABLE CUTOUT AND THE BULKHEAD FLANGE. 1 CRACK EACH SIDE, BULKHEAD WAS REPLACED. 1H71 3O3 ONT3A13 E273 20011015000942001101500094CE 2001 10 15 2001FA0000392 120010816G8011 BEARING ELECTROSYS BEECH 76 76 1153005CE LYC O360 O360A1G6D EA FWD BUSHING DEPARTED B HUNRK NONE O OTHER ININSP/MAINT 1 NM016013M A040394 ME102 L2555136A IN STARTER DRIVE END CASTING, THE (FORWARD) BUSHING DEPARTED FROM THE CASTING THIS IS THE FORWARD PIVOT BUSHING/BEARING FOR THE BENDIX DRIVE SHAFT. 432.24 HOURS OF FLIGHT TRAINING, OVERHAULED BY MFG. 1L72 3O3 O A29CE E286 20011015000232001101500023CE 2001 10 15 2001FA0000393 120010927G2730380210417005 SUPPORT RKWELLNA265 NA26580 7630108CE FUSELAGE BROKEN B K NONE O OTHER ININSP/MAINT 1 SW99380GK 38044 DURING SCHEDULED INSPCTION FOUND SMALL PIECE OF A BEARING BOSS IN HELL HOLE. UPON INVESTIGATION FOUND ELEVATOR TORQUE TUBE SUPPORT MISSING PIECE. ALSO FOUND RT SUPPORT CRACKED IN THE SAME POSITION. REPLACED BOTH RT AND LT ELEVATOR SUPPORT BRACKETS. 2L72 4F A2WE 20011015000262001101500026EU 2001 10 15 2001FA0000394 120011010G2510350A77125807 SEAT SNIAS 350 AS350B2 8680813EU COCKPIT CRACKED B O OTHER O OTHER NRNOT REPORTED 1 CA 6098U 2718 COCKPIT SEAT CRACKED 1G71 3U H9EU 20011015000652001101500065EA 2001 10 15 2001FA0000395 220011008G7313LW18265 INJECTOR CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA MCAULY1A170 1A170E GL ENGINE CLOGGED B A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 WP07428SA597 27 172S8547 L2914851A UC063 PILOT REPORTED THAT DURING CLIMBOUT THE ENGINE BEGAN RUNNING ROUGH, AT WHICH TIME HE RETURNED TO THE AIRPORT (PHX). TECHNICIAN COULD NOT DUPLICATE THE MALFUNCTION ON A GROUND RUN UP. THE FUEL INJECTOR NOZZLES WERE REMOVED & INSPECTED AND THE NR 2 INJECTOR WAS FOUND TO BE PLUGGED. THE INJECTOR NOZZLES WERE CLEANED & REINSTALLED. THE ENGINE RUNUP WAS NORMAL AND SMOOTH, AND THE AIRCRAFT WAS FLOWN BACK TO PHOENIX. 1H71 3O3 ONT3A12 1E10 5 NP857 20011015000682001101500068GL 2001 10 15 2001FA0000396 120011010G7160 DUCT CIRRUSSR SR22 GL AIR BOX LOOSE D K NONE O OTHER ININSP/MAINT 1 NE012345B27 0077 ALTERNATE ENGINE AIR BOX ATTACHED TO ENGINE THROTTLE BODY WITH ONE HOSE CLAMP AND CUSHION CLAMP AT FACTORY. MAINTENANCE MANUAL FIG 71-601 CORRECTLY SHOWS TWO HOSE CLAMPS AND ONE CUSHION CLAMP WHICH ACTS AS SUPPORT FOR ALTERNATE AIR CONTROL CABLE. LACK OF SECOND HOSE CLAMP ALLOWS ALTERNATE AIR BOX TO ROTATE CAUSING DUCT DAMAGE. 1H71 3O NCA00009CH 20011015000692001101500069CE 2001 10 15 2001FA0000397 120011011G5313CM32091 STRINGER CESSNA500 550 2076604CE FUSELAGE DAMAGED B K NONE O OTHER ININSP/MAINT 1 GL07205SC9156 9156 5500156 DURING AN AVIONICS INSTALLATION EVENT WITH THE AIRCRAFTS' INTERIOR REMOVED IT WAS NOTED THAT THE FUSELAGES' UPPER CROWN SKIN, ABOUT THE CENTERLINE HAD BEEN PREVIOUSLY MODIFIED AT ONE TIME TO "BLANK OUT" A ANTENNA INSTALLATION NO LONGER IN USE. EXTREMELY POOR WORKMANSHIP AND NON STANDARD PRACTICES WERE EXHIBITED IN THE INSTALLATION OF TWO INTERNAL DOUBLERS, THAT INCLUDED LARGE HOLES CUT IN THE UPPER CENTERLINE STRINGER ABOUT BL 0.00 AT APPROX. FUSELAGE STATION 240.00. THE TWO HOLES CREATED SIGNIFICANT VOIDS IN THE "T"S' FLANGE, IN CONTACT WITH THE FUSELAGE SKIN, WHICH WERE UNREINFORCED. 1L72 4F A22CE 20011031001042001103100104CE 2001 10 31 2001FA0000398 120010928G76031023890091 THROTTLE CABLE BEECH 58 58P 1152744CE CONT O520 TSIO520* 17040SO RT THROTTLE CHAFED C O OTHER O OTHER NRNOT REPORTED 1 SW99145Z 242 TJ289 PILOT COMPLAINED, RIGHT THROTTLE VERY STIFF, THROTTLE HAD BEEN REPLACED FOUR MONTHS EARLIER FOR SAME REASON. UPON REMOVAL IT WAS DISCOVERED THAT THE CABLE, WHICH WAS COVERED WITH FIRE SLEEVE, HAD BEEN CHAFFING ON THE LOWER PART OF THE TURBOCHARGER COMPRESSOR HOUSING CLAMP, WHERE IT HAD CHAFFED THE CABLE HAD INDICATIONS OF BEING OVERHEATED. CABLE SHOULD HAVE BEEN ROUTED ABOVE THE EXHAUST WHERE IT WOULD HAVE BEEN PROTECTED BY THE EXHAUST HEAT SHIELD. WHEN REPLACING PARTS WITH NO CLEAR GUIDANCE ON ROUTING, NEED TO MAKE SURE TO FOLLOW INSTALLATION GUIDE. 1L72 3O3 O A23CE E8CE 20011031001052001103100105CE 2001 10 31 2001FA0000399 120010901G2710 BRACKET CESSNA206 P206D 2073338CE CONT O520 IO520* 17032SO AILERON PULLEY MISMANUFACTURED C K NONE W INADEQUATE Q C ININSP/MAINT 1 WP258734Z P2060534 DURING ANNUAL INSPECTION, THE ABSENCE OF THE SAFETY COTTER PIN (-23) WAS NOTED (PORT SIDE) (AILERON PULLEY BRACKET) CONSTRUCTION OF THE BRACKET WAS SUCH THAT A COTTER PIN COULD NOT HAVE BEEN INSERTED AT THE FACTORY. (SEE DIAGRAM) 1H71 3O3 O A4CE E5CE 20011031001072001103100107CE 2001 10 31 2001FA0000400 120010828G32421138932 STATOR CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE RT MLF BRAKE BROKEN C O OTHER O OTHER TXTAXI/GRND HDL 1 WP1926496 5500607 FOLLOWING A NORMAL LANDING AND ROLL OUT FOR A RIGHT TURN ON TO THE TAXI WAY THE RIGHT MAIN WHEEL LOCKED UP. AFTER JACKING THE MAIN WHEEL AND PULLING THE TIRE, A PIECE OF STATOR WAS FOUND COMPLETE BROKEN OUT OF THE STATOR CAUSING THE WHEEL TO LOCK. THIS BRAKE ASSY AND THE LEFT HAD BOTH BEEN CHANGED AT THE SAME TIME. SB AND MFG WERE DONE ELIMINATING THE NEED TO SEPARATE THE BRAKE ASSYS FOR INSPECTION. AS CAN BE SEEN BOTH STATORS WERE CLOSE TO FAILURE. THE LEFT ASSY WAS OPENED UP AND STATORS WERE CRACKED TO POINT WHERE FAILURE WAS MATTER OF TIME. BOTH BRAKES HAD 585 LANDINGS. 1L72 4F4 F A22CE E1NE 20011101000562001110100056SO 2001 11 1 2001FA0000401 120010618G371072979 GEAR AMRGENAA1 AA1B 0631206SO LYC O235 O235C2C 41505EA VACUUM PUMP WORN G O OTHER K FLUID LOSS NRNOT REPORTED 1 EA071409R3165 AA1B0509 L1197115 REMOVE VACUUM PUMP DRIVE SHAFT GEAR, OIL LEAKING INTO VACUUM PUMP, WORN SPOT ON SHAFT DAMAGED OIL SEAL CAUSING OIL LEAK. 1L71 3O3 O A11EA E223 20011128000652001112800065SO 2001 11 28 2001FA0000402 220011002G8550 OIL FILTER EXTRA EA400 EA400 EU CONT O550 TSIOL550C SO ENGINE CHAFED G O OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP0714EX 15 AIRCRAFT EXPERIENCED AT TOTAL ENGINE FAILURE DUE TO LOSS OF OIL PRESSURE. THE CAUSE WAS TO A B-NUT ON A T-FITTING LOCATED ON THE METERED PRESSURE TEST PORT FOR THE THROTTLE BODY HAD WORN A HOLE THRU THE OIL FILTER HOUSING. THE THROTTLE HOUSING IS MOUNTED ON RUBBER TUBING AND MOVES THRU VIBRATION AND MAKING CONTACT. THERE NEEDS TO BE MORE CLEARANCE BETWEEN THE FITTING AND OIL FILTER. 1H71 3O3 ORTA43CE E4SO 20011031001092001103100109EA 2001 10 31 2001FA0000403 220010731G8530 EXHAUST VALVE MOONEYM20 M20J 5870219SW LYC O360 IO360A1A 41514EA NR 1 CYLINDER BROKEN C O OTHER O OTHER NRNOT REPORTED 1 WP191084Z1964 241132 NR 1 CYLINDER BROKEN, AN EXHAUST VALVE WHICH DESTROYED THE PISTON AND CYLINDER HEAD. ALSO, FOUND NR 1 INTAKE TUBE SEAL PN 77569, TORN AND TWISTED WHICH COULD HAVE CAUSED A LEAN MIXTURE ON THAT CYLINDER. 1L71 3O3 O 2A3 1E10 20011031001102001103100110CE 2001 10 31 2001FA0000404 120011001G7120265102215 MOUNT CESSNA208 208B 2073701CE PWA PT6 PT6A11 52043NE ENGINE CRACKED D K NONE O OTHER ININSP/MAINT 1 WP119750B 208B0100 DURING NON ROUTINE INSPECTION OF ENGINE MOUNT, A CRACK WAS FOUND IN THE WELD OF THE LOWER RIGHT ATTACH POINT (RING TO AIRCRAFT SUPPORT) SHIMMY DAMPENER WAS IN GOOD CONDITION WITH NO LEAKS DETECTED. NOSE GEAR BUSHINGS WERE ALSO SATISFACTORY. 1H71 3T3 T A37CE E4EA 20011031001112001103100111SO 2001 10 31 2001FA0000405 220010926G74146310 MAGNETO BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO ENGINE FAILED G K NONE O OTHER ININSP/MAINT 1 WP075519A497 CE1337 820453R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IN ACCORDANCE WITH THE MM. REMOVED THE REAR COVER OF MAGNETO AND FOUND A GRAY COLOR POWDER ON THE CAP AND AROUND THE COIL. THIS WAS FOUND ON THE MAGNETOS THAT HAD FAILED IN FLIGHT WITH ABOUT THE SAME FLIGHT TIME ON THEM. MFG WAS INFORMED OF FAILURES. 1L71 3O3 O 3A15 E5CE 20011031001122001103100112NM 2001 10 31 2001FA0000406 120010829G3250 ROD UNIVAR415 415C 0420302NM CONT C75 C75* 17005SO NLG STEERING BROKEN D K NONE O OTHER TXTAXI/GRND HDL 1 GL1994157 1480 STEERING ROD KNUCKLE BROKE AS AIRCRAFT WAS BEING REPOSITIONED AFTER LOG. THIS ROD HAS BROKEN NUMEROUS TIMES IN THE PAST, KNOW OF 3 RODS BREAKING IN THE PAST. 1L71 3O3 O A718 E233 20011031001132001103100113EU 2001 10 31 2001FA0000407 220010904G7421NCKB8ES SPARK PLUG AMTR AVID AVIDFLYERHH 95708FUGL ROTAX 532 ROTAX532 55555EU ENGINE BROKEN G A UNSCHED LANDING O OTHER NRNOT REPORTED 1 AL0347065 063 THE CERAMIC PORTION OF THE SPARK PLUG BROKE COMPLETELY AROUND AND ALLOWED THE SPARK PLUG WIRE TO FALL OFF WITH THE PIECE OF CERAMIC INSIDE THE WIRE AND CAP. ENGINE WOULD NOT MAINTAIN POWER ON 1 CYLINDER CAUSING FORCED LANDING AND DAMAGE TO AIRCRAFT. 1H71 3O3 INCEXPA1H71EXPE3I 20011031001142001103100114GL 2001 10 31 2001FA0000408 120010119G3244 TIRE AMTR EAGLE CHRISEAGLE2 GL LYC O360 IO360A1C 41514EA LANDING GEAR FAILED C O OTHER O OTHER NRNOT REPORTED 1 SW09316 419 TIRE FAILURE, STRIPPED RIB. CAUSE: UNDETERMINED, PENDING EVALUATION BY MFG. 1Q71 3O3 O EXPA1Q711E10 20011031001152001103100115SO 2001 10 31 2001FA0000409 120010904G78200990D113 MUFFLER AMRGENAA1 AA1 0630610SO LYC O235 O235C 41505EA ENGINE CRACKED D K NONE O OTHER ININSP/MAINT 1 SO135903L2330 AA10203 DURING ANNUAL INSPECTION, MUFFLER WAS FOUND CRACKED IN THE AREA WHERE TAIL PIPE IS WELDED TO CAN. 742 HOURS SINCE LAST INSPECTION. (ATTACHED PHOTOS) 1L71 3O3 O A11EA E223 20011101000572001110100057EA 2001 11 1 2001FA0000410 220010223G8520 SEAL AMTR LONGEZLONGEZ 05690Z8GL LYC O235 O235L2C 41505EA ENGINE BLEW OUT G A UNSCHED LANDING K FLUID LOSS NRNOT REPORTED 1 GL0393RF 675 1787L ENGINE CRANKCASE BREATHER HOSE MAY HAVE ICED UP CAUSING CRANKCASE PRESSURE TO BUILDUP, BLOWING CRANKSHAFT SEAL OUT OF CRANKCASE. ALL ENGINE SEIZED UP AND QUIT. PILOT MADE AND EMERGENCY LANDING, NO DAMAGE TO AIRCRAFT. 1M71 3O3 ORTEXPA1M71E223 20011031001162001103100116 2001 10 31 2001FA0000411 420011004G2300S28701 SWITCH CESSNA182 182S 2072701CE LYC O540 IO540* 41532EA COCKPIT FAILED C K NONE O OTHER NRNOT REPORTED 1 EA073261M 18280347 PUSH TO TALK SWITCH FAILED AFTER 1 HOUR OF OPERATION. HAS HAPPENED FOUR TIMES IN A ROW. 1H71 3O3 ONT3A13 1E4 20011128000662001112800066SW 2001 11 28 2001FA0000412 120010830G78106422209052 TAB MOONEYM20 M20K 5870220SW CONT O360 TSIO360LB 17025SO ENGINE BROKEN B TZ3RO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 WP01231EC65 250167 247414R SECURING/ATTACHING TAB WELDED TO EXHAUST RISER ASSEMBLY FOR CYLINDER NR 4 BROKE OFF CAUSING SUDDEN LOSS OF ENGINE MANIFOLD PRESSURE AND POWER RESULTING IN IMMEDIATE LANDING OF AIRCRAFT. (NR 4 CYLINDER RISER SEPARATED FROM NR 6 RISER WHEN TAB BROKE. 1L71 3O3 O 2A3 E9CE 20011101000602001110100060GL 2001 11 1 2001FA0000413 120010829G5730 STRUCTURE BLANCA1419 14193A 1220408GL CONT O470 IO470* 17026SO WING DETERIORATED D K NONE W INADEQUATE Q C ININSP/MAINT 1 SO098507R2619 4269 DURING ANNUAL INSPECTION, IN THE AREA OF THE WING WALK, WOOD DETERIORATION WAS FOUND AT THE AFT, IB UPPER SKIN SEPARATED FROM THE FORWARD EDGE, OB EDGE AND AFT TRAILING EDGE, THE ENTIRE WING WALK AREA FABRIC WAS LOOSE FROM THE STRESSED SKIN PANELS THE OWNER THEN, NOT BELIEVING SB REQUIRED AND NOT WILLING TO PROPERLY REMOVE THE EFFECTED SKIN, A CABINET MAKER AND HIMSELF SLIP IN ON AN OFF DAY. THE DAMAGE THAT WAS DONE TO THE SPAR THREE DIFFERENT SPOTS AT WS 6 TO WS 10.5 SEVERELY DAMAGED THE SPAR DUE TO COMPRESSION CAUSED BY THE CHISEL. WHAT WAS TO BE SKIN CHANGE, NOW INCLUDES SPAR CHANGE/SPLICE. SENT PICTURES TO MFG WAS INFORMED DAMAGE WAS SEVERE. 1L71 3O3 O 1A3 E1CE 20011101000582001110100058CE 2001 11 1 2001FA0000414 120010921G282107560058 FUEL STRAINER CESSNA182 R182 2072734CE LYC O540 O540* 41532EA FUEL SYSTEM BACKED OUT D K NONE O OTHER ININSP/MAINT 1 NM034447R5648 R18200601 DURING ANNUAL INSPECTION NOTICED FUEL STRAINER STANDPIPE HAD BACKED OUT AND WAS ABLE TO PULL IT OUT OF TOP ASSEMBLY WITH FINGERS. 1H71 3O3 ORT3A13 E295 20011031001172001103100117SW 2001 10 31 2001FA0000415 120011004G5711 SPAR BBAVIA7 7GCBC 1220601SW LYC O320 O320* 41508EA RT WING CRACKED D K NONE O OTHER ININSP/MAINT 1 NM035074X2714 40 WHILE INSPECTING WING SPARS IN COMPLIANCE WITH AD, THE FRONT SPAR IN THE RIGHT WING WAS FOUND TO HAVE A COMPRESSION CRACK AT THE BUTT END AND THE REAR SPAR IN THE LEFT WING WAS FOUND TO HAVE A LONGITUDINAL CRACK APPROXIMATELY 14 INCHES INBOARD FROM THE TIP. 1H71 3O3 ONCA759 E274 20011101000592001110100059CE 2001 11 1 2001FA0000416 120011011G322022430151 CLAMP CESSNA182 R182 2072734CE LYC O540 O540* 41532EA NLG BENT D O OTHER O OTHER UKUNKNOWN 1 GL252063S2954 R18201292 NOSE GEAR FAILED TO EXTEND, BUT FELL OUT WHEN AIRCRAFT WAS LIFTED FROM RUNWAY. ON JACKS, GEAR OPS WAS NORMAL. THIS CLAMP WAS BENT WHICH MAY HAVE ALLOWED SHIMMY DAMPENER TO JAM THE GEAR. MAY HAVE BEEN DAMAGED FROM TUG OVER TURNING THE GEAR. 1H71 3O3 ORT3A13 E295 20011101000612001110100061CE 2001 11 1 2001FA0000417 120010830G3213AN310S NUT CESSNA421 421B 2076014CE CONT O520 GTSIO520F 17032SO RT MLG FAILED D K NONE O OTHER TXTAXI/GRND HDL 1 SO09781SL149 421B0343 AIRCRAFT WAS TAXING FROM THE MAIN RUNWAY TO THE GATE, PILOT FELT AND HEARD BUMPING NOISE UPON MAKING A RIGHT TURN. AS HE WAS MAKING RIGHT TURN ONTO RAMP TORQUE LINKS SEPARATED CAUSING THE RIGHT WHEEL AND PISTON ASSEMBLY TO ROTATE ABOUT 135 DEGREES, CAUSING DAMAGE TO THE TO THE OB GEAR DOOR. THE NUT STRIPPED ITS THREADS, SHEARED THE COTTER KEY AND DEPARTED THE AIRCRAFT. BOLT REMAINED IN UPPER TORQUE LINK. NEW MLG SCISSORS WASHER REPLACEMENT KIT WAS INSTALLED, KIT DOES NOT INCLUDE A NEW NUT AND SUGGEST USING OLD NUT. NEW NUT WAS USED. THE LEFT GEAR BOLT WAS INSPECTED AND FOUND NUT WAS WOBBLY ON BOLT THREADS. NEW KITS AND NUT WERE INSTALLED ON BOTH SIDES. 1L72 3O3 O A7CE E7CE 20011030001092001103000109NM 2001 10 30 2001FA0000419 120010820G3240511531 HOUSING PNEUDRAULICS BOEING737 737 UTILSYSNM SHUTTLE VALVE CRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 3488 HOUSING IS CRACKED INSIDE THE MOUNTING BOLT HOLE. FATIGUE, DEFECT IN THE CASTING OF THE HOUSING AND/OR OVER TORQUE OF BOLT ON INSTALLATION. 2L72 4F RTA16WE 20011030001102001103000110NM 2001 10 30 2001FA0000420 120010821G3240511531 HOUSING PNEUDRAULICS BOEING737 737 UTILSYSNM SHUTTLE VALVE CRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 339 HOUSING IS CRACKED ALONG THE TOP CASTING SEAM. FATIGUE, DEFECT IN THE CASTING OF THE HOUSING AND/OR OVER TORQUE OF BOLT ON INSTALLATION. 2L72 4F RTA16WE 20011030001112001103000111NM 2001 10 30 2001FA0000421 120010821G3240511531 HOUSING PNEUDRAULICS BOEING737 737 UTILSYSNM SHUTTLE VALVE CRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 788 HOUSING IS CRACKED INSIDE THE MOUNTING BOLT HOLE. FATIGUE, DEFECT IN THE CASTING OF THE HOUSING AND/OR OVER TORQUE OF BOLT ON INSTALLATION. 2L72 4F RTA16WE 20011030001122001103000112NM 2001 10 30 2001FA0000422 120010821G2761654494713 HOUSING BOEING BOEING737 737 UTILSYSNM SPOILER ACTUATORBROKEN B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 9858 HOUSING BEARING LUG IS BROKEN ON BOTH SIDES OF BEARING. 2L72 4F RTA16WE 20011030001132001103000113NM 2001 10 30 2001FA0000423 120010821G2761654494715 HOUSING BOEING727 727 UTILSYSNM SPOILER ACTUATORCRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 4621 HOUSING IS CRACKED ALONG FIRST SHOULDER ON SAME SIDE AS PORTS. 2L73 4J RTA3WE 20011030001142001103000114NM 2001 10 30 2001FA0000424 120010821G2761654494713 HOUSING BOEING BOEING737 737 UTILSYSNM SPOILER ACTUATORCRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 4468 HOUSING IS CRACKED ALONG FIRST SHOULDER ON SAME SIDE AS PORTS. 2L72 4F RTA16WE 20011030001152001103000115NM 2001 10 30 2001FA0000425 120010821G2761654494710 HOUSING BOEING BOEING737 737 UTILSYSNM SPOILER ACTUATORCRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 43737 0785 HOUSING IS CRACK ON ID OF PORT. 2L72 4F RTA16WE 20011030001162001103000116NM 2001 10 30 2001FA0000426 120010821G2761654494713 HOUSING BOEING BOEING737 737 UTILSYSNM SPOILER ACTUATORCRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 8143 HOUSING IS CRACKED ALONG THE SECOND SHOULDER OPPOSITE THE PORTS. 2L72 4F RTA16WE 20011030001172001103000117NM 2001 10 30 2001FA0000427 120010821G2761654494710 HOUSING BOEING BOEING737 737 UTILSYSNM SPOILER ACTUATORCRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 4592215683 4348 HOUSING IS CRACKED UNDER THE RETRACT PORT. 2L72 4F RTA16WE 20011101000622001110100062NE 2001 11 1 2001FA0000429 220010926G7250769104 TURBINE PWA JT8 JT8D15 52051NE ENGINE CRACKED B W9DRK NONE O OTHER ININSP/MAINT 1 NE03 7914 THE 4TH STAGE TURBINE DISK BALANCE WEIGHT FLANGE HAS MULTIPLE CRACKS (APPROX. 80) INITIATING FROM THE SCALLOP AND BALANCE WEIGHT HOLES. CRACK LENGTH VARIES FROM .001 TO .5 INCH. IT WAS NOTED THAT ONE CRACK IS PROGRESSING PAST ONE OF THE TWO OIL DRAIN HOLES AND INTO THE RADIUS OF THE DISK OUTER RIM. 4 F E2EA 20011031001192001103100119 2001 10 31 2001FA0000430 420011008G2561PO723E105P LIFE VEST CABIN FAILED B KQ1RK NONE O OTHER ININSP/MAINT 1 EA07 LIFE VEST FAILED, MFG RECOMMENDED 2 PSI CELL TEST IAW MANUAL. 20011031001202001103100120GL 2001 10 31 2001FA0000431 320010828G61101851 BEARING HARTZL PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL PROPELLER ASSY CRACKED B LU4RK NONE O OTHER ININSP/MAINT 1 SO17 BU16907 BU16907 RELEVANT INDICATION. 4 T E4EA 6 CP15EA 20011031001212001103100121 2001 10 31 2001FA0000432 420010809G2564R0097104 LIFE RAFT CABIN POROUS B ALGRK NONE O OTHER ININSP/MAINT 1 SW03 LIFE RAFT TOO POROUS. 20011101000702001110100070SW 2001 11 1 2001FA0000433 120010831G291041002418 CYLINDER TEXTRON BELL 214 214B1 1182105SW SERVO ACTUATOR CRACKED B B80RO OTHER O OTHER NRNOT REPORTED 1 NM07 7513 1371 1885B SURFACE MATERIAL DEFECT/CRACK. 2G71 4U H6SW 20011101000632001110100063GL 2001 11 1 2001FA0000434 320010905G6110C4503 FORK HARTZLHCC4Y HCC4YR2 GL PROPELLER CRACKED B ME4RK NONE O OTHER ININSP/MAINT 1 SO19 1113 FH596 PROPELLER WAS RECEIVED FOR STANDARD 60 MONTH OVERHAUL IAW MFG SL. CURRENT PROPELLER TIMES ARE: TTSN1113.80 TSO N/A. THIS IS THE PROPELLERS FIRST OVERHAUL. DURING THE INSPECTION OF THE PROPELLER COMPONENTS, FOR PART NUMBER C-4503, SERIAL NUMBER N0901 WAS FOUND CRACKED IN THE FORWARD INBOARD EAR. ALSO, THE CORRESPONDING BLADE, PART NUMBER FC7663D6Q WITH SERIAL NUMBER H37377 HAS A BENT BLADE PIN AND BEARING RACE PART NUMBER A-2202 WAS FRETTED. HARTZELL PROPELLER WAS NOTIFIED VIA PHONE. ALL CONDEMNED PARTS WERE RED TAGGED AND ENTERED ON MFG FORM 101DA BEFORE RETURNING TO CUSTOMER. THE REMAINING PARTS CHECK GOOD. PROPELLER WAS REASSEMBLED WITH REPLACEMENT PARTS AND RETURNED TO SERVICE. 5 CP52GL 20011101000692001110100069SW 2001 11 1 2001FA0000437 120010831G291041002418 CYLINDER TEXTRON BELL 214 214B1 1182105SW SERVO ACTUATOR CRACKED B B80RO OTHER O OTHER NRNOT REPORTED 1 NM07 7513 1371 1885B SURFACE MATERIAL DEFECT/CRACKED. 2G71 4U H6SW 20011101000682001110100068 2001 11 1 2001FA0000441 420010814G34215546257001 CONNECTOR COLLINS VERTICAL GYRO CORRODED B M71RO OTHER N FALSE WARNING NRNOT REPORTED 1 SW15 6055 EXCESSIVE CORROSION ON CONNECTOR BETWEEN PINS N,P, AND M. THIS RESULTED IN ATTITUDE INDICATOR FLAGGING AND SHOWING IMPROPER ATTITUDES. 20011101000672001110100067 2001 11 1 2001FA0000442 420010914G2561S5600AV2A LIFE VEST CABIN FAILED B KQ1RK NONE O OTHER ININSP/MAINT 1 EA07 LIFE VEST TYPE AV-2(A) MFG MARCH 1983 FAILED. MFG RECOMMENDED 2 PSI CELL TEST I/A/W 25-60-55. 20011101000712001110100071GL 2001 11 1 2001FA0000443 320010913G6111S90AT2 BLADE MCAULY2A34C 2A34C66 GL PROPELLER CRACKED B ME4RK NONE O OTHER ININSP/MAINT 1 SO19 MCAULEY BLADE PART S90AT-2 WITH SERIAL NUMBER OD044YSC WAS RECEIVED FOR OVERHAUL. BLADE TIMES ARE UNKNOWN. BLADE RECEIVED AS A SINGLE BLADE WITH FERRULE INSTALLED. AFTER FERRULE REMOVAL, DURING BLADE BUTT, FLORESCENT PENETRATE INSPECTION, BLADE WAS DISCOVERED CRACKED IN THE LAST THREAD, FORWARD SIDE, FROM 1:00 TO 5:00 O'CLOCK POSITION. BLADE WAS RED TAGGED. 5 CP3EA 20011105000352001110500035 2001 11 5 2001FA0000444 420010727G34215546257001 CONNECTOR COLLINS VERTICAL GYRO CORRODED B M71RO OTHER N FALSE WARNING NRNOT REPORTED 1 SW15 6224 EXCESSIVE CORROSION ON CONNECTOR BETWEEN PINS N AND P. CORROSION CAUSED BY INTERNAL CONDENSATION. THIS IS RESULTED IN ATTITUDE INDICATOR FLAGGING AND SHOWING IMPROPER ATTITUDES. 20011101001112001110100111 2001 11 1 2001FA0000445 420010921G2561KS9P0101 LIFE VEST CABIN FAILED B KQ1RK NONE O OTHER ININSP/MAINT 1 EA07 LIFE VEST FAILED. THE MFG RECOMMEDNDED CELL PRESSURE TEST IAW 25-60-01. DOM: JUNE 1980 20011101001122001110100112GL 2001 11 1 2001FA0000446 320010925G61141A103TCM6958 HUB MCAULY1A103 1A103TCM GL PROPELLER CRACKED B ME4RK NONE O OTHER ININSP/MAINT 1 SO19 DURING INSPECTION, PROPELLER HUB WAS FOUND TO HAVE FORGING LAP IN HUB AREA. 5 NP50GL 20011101001132001110100113 2001 11 1 2001FA0000448 420010926G2561KS9P0101 LIFE VEST CABIN FAILED B KQ1RK NONE O OTHER ININSP/MAINT 1 EA07 LIFE VEST FAILED. THE MFG RECOMMENDED TWO PSI TEST IAW MANUAL. DOM FEB 1982 20011101001142001110100114 2001 11 1 2001FA0000449 420010922G2561KS9P0101H02 LIFE VEST CABIN FAILED B KQ1RK NONE O OTHER ININSP/MAINT 1 EA07 LIFE VEST FAILED. THE MFG RECOMMENDED 2 PSI CELL TEST IAW MANUAL. DOM JAN 1981 20011101001152001110100115SW 2001 11 1 2001FA0000450 120010925G6410406016100119 BLADE BELL 407 407 1182206SW ALLSN 250C 250C47B GL TAIL ROTOR DEBONDED B IIFRK NONE O OTHER ININSP/MAINT 1 SW03407AK 53269 FOUND OVAL SHAPED AREA ON OUTSIDE OF TAIL ROTOR BLADE DEBONDED. 11 INCHES FROM BLADE ROOT TO 17 INCHES FROM BLADE ROOT. 1 INCH FROM TRAILING EDGE TO 3 INCHES FROM TRAILING EDGE OF BLADE. 1G71 3U3 UO H2SW E1GL 20011105000492001110500049EU 2001 11 5 2001FA0000451 120010925G6210117150041 BLADE BOLKMS117 BK117A1 5626010EU MAIN ROTOR DELAMINATED B YIVRK NONE O OTHER ININSP/MAINT 1 SW19 6969 M/R BLADE WAS RECEIVED FOR INSP AND EVAL. ABRASION STRIP CRACK WAS IDENTIFIED AT BLADE STATION 2305. PORTION OF ABRASION STRIP WAS REMOVED TO ALLOW EVALUATION OF UNDERLYING SURFACE. SKIN WAS ALSO CRACKED WITH DELAMINATION SURROUNDING AREA. REVIEW OF BLADE RECORDS INDICATE THAT MFG PERFORMED REPAIR ON INNER WEIGHT 1 AND 2, CRACK IN ABRASION STRIP FROM A DRILL MARK ON INSIDE OF ABRASION STRIP IN AREA OF THIS REFERENCED REPAIR. REPAIR PERFORMED BY MFG IS FOR INSTALLATION OF PINS THROUGH INNER WEIGHTS 1 AND 2. THREE DRILL MARKS ON INSIDE SURFACE OF ABRASION STRIP THAT LINE UP WITH PINS INSTALLED FROM UPPER SURFACE. 1G72 3U H13EU 20011101001162001110100116GL 2001 11 1 2001FA0000453 320010911G6110840118 TUBE HARTZLHCB5M HCB5MP3 GL PROPELLER CRACKED B ME4RK NONE O OTHER ININSP/MAINT 1 SO19 445 EVA2042 PROPELLER WAS FOR RECEIVED FOR STANDARD 60 MONTH OVERHAUL. CURRENT PROPELLER TIMES ARE TTSN 445.0 AND TSO N/A. THIS IS THE PROPELLER`S FIRST OVERHAUL. DURING THE INSPECTION OF THE PROPELLER COMPONENTS, HUB PART NUMBER 840-118, SERIAL NUMBER EVA2042 WITH PILOT TUBE PART NUMBER B-4020 WAS FOUND CRACKED IN NR 1 BLADE POSITION, 1.00 INCH FROM THE HUB SHOULDER FROM 11:00 TO 1:00 POSITION. THE CRACKED PILOT TUBE WAS REMOVED AND REPLACED AND THE HUB CHECKED SERVICEABLE, AFTER REPAIR. THE CORRESPONDING BLADE, NR 1 CHECK SERVICEABLE WITH NO DEFECTS NOTED. PROPELLER WAS REASSEMBLED AFTER OVERHAUL AND RETURNED TO SERVICE. 6 CP44GL 20011105000362001110500036EA 2001 11 5 2001FA0000454 220011004G7322 CARBURETOR CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA ENGINE DEFECTIVE D A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SW0349445 15283460 RL1860315 PILOT TOOK OFF IN AIRCRAFT, TURNED DOWNWIND AND ENGINE STARTED RUNNING ROUGH AND LOSING POWER. PILOT LANDED AC AND ENGINE QUIT AS HE PULLED OFF RUNWAY. ALL SYSTEMS CHECKED POINTED TO INSTALLED NEW REBUILT CARBURETOR AND ENGINE FUNCTIONED NORMALLY. PROBABLE CAUSE FLOAT STICKING IN CARBURETOR. RECOMMENDATIONS TO PREVENT RECURRENCE. CARBURETOR RETURNED TO MFG FOR EVALUATION. 1H71 3O3 ONT3A19 E223 20011101001172001110100117NE 2001 11 1 2001FA0000455 220011009G8530 CYLINDER MAULE MT7235MT7235 5470209SO LYC O540 IO540W1A5 41532NE ENGINE SEPARATED D O OTHER O OTHER CRCRUISE 1 WP11390AT 18028C L2559148A CRUISE FLIGHT. SUSPECT MFG DEFECTIVE CYLINDER WALL. NITRIDE CYLINDER. CYLINDER SEPARATION. 1H71 3O3 ONC3A23 1E4 20011101001182001110100118CE 2001 11 1 2001FA0000456 120010815G32405100106159 LINE CESSNA414 414A 2075907CE CONT O520 TSIO520* 17040SO BRAKE SYS CHAFED C O OTHER K FLUID LOSS NRNOT REPORTED 1 CE05368874094 414A0835 RIGHT BRAKE LINE HAD A HOLE CHAFFED IN IT FROM BEING IN CONTACT WITH THE LINE HEATER DUCT LINE UNDER THE CO-PILOTS SEAT. THE BRAKE LINE RUNS UNDER THE HEAT DUCT AND IS VERY DIFFICULT TO SEE. THIS IS AN ORIGINAL PART. 1L72 3O3 O A7CE E8CE 20011101001192001110100119EA 2001 11 1 2001FA0000457 220011016G8520 CRANKSHAFT UNIVAR108 1083 9230408NM FRNKLN6A41656A4165* 27025EA ENGINE BROKEN D MS2RO OTHER R PARTIAL RPM/PWR LOSS CRCRUISE 1 CE09833C 378 1083833 911174017 CRANKSHAFT BROKEN IN FLIGHT, LANDED WITHOUT INCIDENT. CRANKSHAFT BROKEN ON THE FORWARD SIDE OF JOURNAL NR 1 CYLINDER. 1H71 3O3 O A767 E238 20011101001202001110100120SO 2001 11 1 2001FA0000458 220010928G8520SA628488 LIFTER CESSNA206 TU206G 2073357CE CONT O520 TSIO520* 17040SO ENGINE SPALLED D K NONE O OTHER ININSP/MAINT 1 WP015424Y326 U20605287 512594 DURING ROUTINE OIL CHANGE, METAL WAS FOUND IN FILTER. ENGINE WAS REMOVED AND DISASSEMBLED. CAUSE WAS FOUND TO BE LIFTER FACE AND CAM LOBE SPALLING ON CYLINDER CAM LOBES NR5 AND NR6 INTAKE. NO CORROSION NOTED. TWO OTHER INTAKE LIFTERS EXHIBIT PREMATURE WEAR, REMAINING CAM LOBES CHECK. OKAY FOR WEAR. CAMSHAFT WAS INSTALLED. 1H71 3O3 O A4CE E8CE 20011105000372001110500037SO 2001 11 5 2001FA0000459 220010928G8530SA643766 CYLINDER CESSNA210 T210M 2073451CE CONT O520 TSIO520* 17040SO ENGINE OUT OF TOLERANCED O OTHER W INADEQUATE Q C NRNOT REPORTED 1 WP01761RD336 21062450 269614R CUSTOMER COMPLAINED OF INTERMITTENT ROUGHNESS. REMOVAL OF CYLINDERS REVEALED STICKING INTAKE VALVES. GUIDE TO VALVE TOLERANCE TOO TIGHT, BELOW MFG MINIMUM LIMITS. MFG CLAIMS TOLERANCE TOO TIGHT FROM NORMAL OPERATION. NO BUILD UP NOTED OF ANY KIND ON VALVE STEM OR INSIDE DIAMETER OF VALVE GUIDE. TOLERANCE WAS INCORRECTLY MACHINED AT PART/CYLINDER MANUFACTURE OR ASSEMBLY. RECOMMEND DISASSEMBLY AND INSPECTION OF NEW CYLINDER ASSEMBLIES TO CHECK TOLERANCES. 1H71 3O3 O 3A21 E8CE 20011105000382001110500038WP 2001 11 5 2001FA0000460 220011022G726030702123 GEARSHAFT HONEYWELL GARRTTTFE731TFE7313 01518WP ENGINE SEPARATED B IY2RE ENGINE SHUTDOWN O OTHER CLCLIMB 1 SW15 7629 P2528 P83190 83190 WAS REMOVED FROM SABRE 65 DUE TO AN IN-FLIGHT SHUTDOWN DURING CLIMB. TRANSFER HORIZONTAL BEVEL GEARSHAFT EXHIBITED SEPARATED GEAR TEETH, THUS CAUSING IFSD DUE TO NO AGB ROTATION. 4 F E6WE 20011211000102001121100010SO 2001 12 11 2001FA0000461 120011021G510245 FITTING BALWKSFIRE FIREFLY715 1050518SO FUEL SYSTEM LEAKING B F65RK NONE O OTHER ININSP/MAINT 1 SW153214V104 THIS SET OF FUEL HOSES WERE OBTAINED FROM THE HOLDER OF A PMA. THEY WERE INSTALLED IN MAY OF 1998. THE HOSE WAS FOUND TO BE LEAKING AT THE CONNECTION WHERE THE RUBBER HOSE MEETS THE FITTING. THE LEAK DOES NOT APPEAR TO BE CAUSED BY MISHANDLING BUT BY A POOR FITTING. 1B00 A14SO 20011105000392001110500039SO 2001 11 5 2001FA0000462 220011017G8530 CYLINDER CESSNA421 421B 2076014CE CONT O520 GTSIO520C 17032SO ENGINE MALFUNCTIONED G A UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 GL17421CR 421B0224 LEFT ENGINE EXPERIENCED A VIBRATION. PILOT ELECTED TO LAND . REPLACED NR 2 CYLINDER. CLEANED VALVE GUIDES ON REMAINING CYLINDERS. REPLACED SPARK PLUG ON NR 1 CYLINDER. FLIGHT CHECK GOOD. 1L72 3O3 O A7CE E7CE 20011105000402001110500040EU 2001 11 5 2001FA0000463 120010924G2730 ELEVATOR GROB ASTIR G102IIIB 1660106EU TAIL FLUTTER C O OTHER F FLT CONT AFFECTED CRCRUISE 1 WP1149JJ 5606CB WHILE CRUISING IN LEVEL FLIGHT AT 100 KTS, INDICATED, 5000 MSL, THE PILOT INITIATED A CLIMB ESTIMATED BETWEEN 2.0-2.5 G`S. AS SOON AS THE CLIMB WAS INITIATED FLUTTER WAS NOTED IN THE PITCH MOTION OF THE STICK (ELEVATOR FLUTTER). BACK PRESSURE WAS RELAXED AND THE FLUTTER STOPPED. THE GLIDER LANDED WITHOUT FURTHER INCIDENT. GLIDER IS CURRENTLY BEING EXAMINED AT MFG. 1K00 RCG33EU 20011105000412001110500041WP 2001 11 5 2001FA0000465 120011012G3246152058 WHEEL BENDIX DOUG DC8 DC8* WP LANDING GEAR CRACKED B INWRK NONE O OTHER ININSP/MAINT 1 SO19 H3501OB NON DESTRUCTIVE TESTING INSPECTION SHOWED CRACK INDICATION AT BASE OF THE VALVE. 2L74 4J F 4A25 20011128000682001112800068 2001 11 28 2001FA0000466 420011004G25627A1169SHARC7 SWITCH ELT INOPERATIVE D K NONE L NO TEST ININSP/MAINT 1 GL15 1385 WOULD NOT ACTIVATE - G SWITCH DEFECTIVE. WILL ACTIVATE IF TURNED ON, USING MECHANICAL SWITCH. 20011128000692001112800069 2001 11 28 2001FA0000467 420010824G3422060001701 GYRO COCKPIT DEFECTIVE B M2QAK NONE O OTHER ININSP/MAINT 1 SO09 OUT OF BOX FAILURE, SLOW TO ERECT. AFTER AIR IS DISCONNECTED GYRO ROLLS OVER 120 DEGREES. 20011128000702001112800070CE 2001 11 28 2001FA0000468 120010329G275251152401 GEAR CESSNA421 421B 2076014CE CONT O520 GTSIO520K 17032SO FLAP ACTUATOR DAMAGED G K NONE O OTHER APAPPROACH 1 SW11421HM3100 421B0029 ON FINAL, THE FLAPS MADE A LOUD POPPING SOUND. REMOVE FLAP ACTUATOR AND FOUND THAT THE GEAR BOX HAD ONE GEAR WITH THE TEETH MISSING. 1L72 3O3 O A7CE E7CE 20011128000712001112800071EA 2001 11 28 2001FA0000469 220011003G741410068 GEAR AMTR HDWINDHEADWIND GL FRNKLN4AC1764AC176B* 27006EA MAGNETO BROKEN G A UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 NM093948 2000 AB7 FOLLOWING TAKEOFF, AT ABOUT 200 FT, ENGINE FAILED. AIRCRAFT LANDED IN FIELD WITHOUT FURTHER INCIDENT. SUBSEQUENT INSPECTION REVEALED CAM GEAR, WHICH DRIVE BOTH MAGNETO GEARS, HAD SHATTERED. CAM GEAR IS MADE OF MICARTA (FIBER) MATERIAL. 1H71 3O3 O EXPA1H71TC221 20011128000742001112800074EA 2001 11 28 2001FA0000472 220010912G8520SL13212M03 BEARING LYC O360 HIO360D1A 41514EA ENGINE FAILED B K NONE O OTHER ININSP/MAINT 1 GL03 331 L1195451A ENGINE WAS REMOVED DUE TO METAL CONTAMINATION. FOUND NR 3 CONNECTING ROD BEARING FAILED. THE ENGINE DID NOT EXHIBIT SIGNS OF OIL STARVATION. CAUSE FOR THIS FAILURE COULD BE DELAMINATION OF THE ROD BEARING. 3 O 1E10 20011203000562001120300056SO 2001 12 3 2001FA0000477 120011015G2121313B57 ARMATURE PIPER PA31 PA31P350 7103111SO FAN IMPROPER D K NONE L NO TEST ININSP/MAINT 1 WP23 347 FAN WAS TESTED AND FOUND NOT TO RUN, FAN WAS DISASSEMBLED AND FOUND TO HAVE A BRUSH LEAD WIRE CUT. THIS CAUSED THE FAN TO FAIL. THE FAN HAS AN ARMATURE IN IT THAT IS NOT OF MFG DESIGN AND DOES NOT MEET MFG SPECIFICATIONS. THE ARMATURE LAMINATIONS ARE NOT PROTECTED AND THE WIRE IS NOT WOUND PER MFG SPECIFICATIONS. 1L72 3O RTA8EA 20011203000572001120300057EA 2001 12 3 2001FA0000478 220010623G7322IO323 ACCELL PUMP CESSNA182 R182 2072734CE LYC O540 IGO540* 41532EA CARBURETOR STIFF D O OTHER O OTHER NRNOT REPORTED 1 SW035284T R18201848 L2201140 THE CARB HAD TO BE CHANGED BECAUSE OF STIFF THROTTLE. THE CAUSE BEING THE ACCELERTOR PUMP, LINKAGE RODS. PRECISION SIL-MS-1CW. HAD NO EFFECT ON THE PUMP RODS. 1H71 3O3 ORT3A13 1E11 20011203000582001120300058EA 2001 12 3 2001FA0000479 220011024G7322103235 ACCELL PUMP CESSNA182 R182 2072734CE LYC O540 O540J3C5 41532EA CARBURETOR STIFF D O OTHER O OTHER NRNOT REPORTED 1 SW036485T R18202039 CARBURETOR CHANGED BECAUSE OF ACCELERATOR PUMP STIFFNESS. PRECISION SIL CW AND HAD NO EFFECT ON EITHER CARBURETOR. 1H71 3O3 ORT3A13 E295 20011203000592001120300059NM 2001 12 3 2001FA0000480 120010717G56105717623097 WINDOW BOEING737 737317 138447PNM GE CFM56 CFM56* 13802NE COCKPIT CRACKED G K NONE O OTHER ININSP/MAINT 1 SO15253DV 23800 AIRCRAFT PARKED ON HOT RAMP WITH INTERIOR REFLECTIVE SHADES INSTALLED IN THE COCKPIT. PRIOR TO PREFLIGHT, CREW STARTED APU FOR AIR CYCLE MACHINE(AIR CONDITIONING), UPON REMOVAL OF SUN SHADES IN THE COCKPIT, THE NR 2 PILOT WINDOW INNER PANE SHATTERED. 2L72 4F4 FRTA16WE E2GL 20011203000602001120300060WP 2001 12 3 2001FA0000481 220010810G732189711012 FCU CESSNA441 441 2076020CE GARRTTTPE331TPE33110 01514WP LT ENGINE FAULTY G O OTHER O OTHER NRNOT REPORTED 1 WP07687AE 1313 4410087 P77369 ENGINE WOULD NOT REDUCE FUEL FLOW IN EITHER COMPUTER MODE OR MANUAL MODE TO ALLOW A NORMAL LANDING. THE AIRCRAFT HAD TO BE LANDED SINGLE ENGINE INSTALLING A REPAIRED FUEL CONTROL UNIT CURED THE FAULT. 1L72 3T4 TRTA28CE E4WE 20011203000612001120300061WP 2001 12 3 2001FA0000482 220010810G732189711019 FCU CESSNA441 441 2076020CE GARRTTTPE331TPE33110 01514WP LT ENGINE MISREPAIRED D K NONE WJ INADEQUATE Q C WARNING INDICATION ININSP/MAINT 1 WP07687AE 990 4410087 P77369 UNIT WAS INSTALLED AFTER REPAIR BY MFG. UPON APPLYING POWER TO THE FUEL CONTROL AIRCRAFT HAD THE LEFT MONOPOLE FAIL LIGHT ILLUMINATED. FOUND THE WIRING AT THE FUEL CONTROL ELECTRICAL CONNECTOR MISSOLDERED, RESOLDERED WIRING AT THE CONNECTOR UNIT OPERATIONALLY CHECKED GOOD. 1L72 3T4 TRTA28CE E4WE 20011203000622001120300062WP 2001 12 3 2001FA0000483 220010810G732189711012 FCU CESSNA441 441 2076020CE GARRTTTPE331TPE33110 01514WP LT ENGINE FAULTY D O OTHER O OTHER NRNOT REPORTED 1 WP07689AE 4798 4410281 ENGINE WOULD NOT OPERATE NORMALLY IN COMPUTER MODE. ENGINE SPEED WAS NOT BEING REGULATED PROPERLY BY FUEL CONTROL TORQUE MOTOR ENGINE OPERATED NORMALLY IN MANUAL MODE. OVERHAULED FUEL CONTROL WAS INSTALLED AND ENGINE OPERATED NORMALLY IN BOTH COMPUTER AND MANUAL MODES. 1L72 3T4 TRTA28CE E4WE 20011203000632001120300063SO 2001 12 3 2001FA0000484 120010906G2612512T130B150001 THERMOSWITCH GULSTMGV GV 3980116SO RROYCEBR700 BR700710A110 NE FIRE DETECTION WRONG PART G O OTHER WN INADEQUATE Q C FALSE WARNING NRNOT REPORTED 1 SO0315UC 263 589 FOUND THERMAL SWITCH PN 512T130B150001 INSTALLED. REMOVED SWITCH AND INSTALLED PN GAS850DF512-250 REV B. THIS SWITCH CORRECTED PROBLEM. THE REMOVED SWITCH CAUSED (FIRE WARNING LIGHT FOR THE LEFT AFT DUCT) TO COME ON. NO LEAKS NOTED. THE SWITCH REMOVED WAS NOT CORRECT PART NUMBER. 2L72 4F4 FRTA12EA E00057EN 20011120000912001112000091NE 2001 11 20 2001FA0000485 120011101G242128B135145AM GENERATOR SKRSKYS61 S61N 8142104NE NR 2 ENGINE FAILED C K NONE BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SW9991158 363 61424 A BURNING SMELL WAS DETECTED IN FLIGHT. FOLLOWED BY THE NR 2 AC GEN DROPPING OFF-LINE. THE REST OF THE FLIGHT CONTINUED NORMALLY. 2G72 4U 1H15 20011203000642001120300064EA 2001 12 3 2001FA0000487 220011009G7322229164 TUBE PRECISION CESSNA172 172L 2072432CE LYC O320 O320E2D 41508EA CARBURETOR SEPARATED C O OTHER O OTHER DEDESCENT 1 AL057564G 1618 CK49483 17259264 R4279327A DURING DECENT, THE PILOT WAS UNABLE TO REDUCE POWER. USING THE MIXTURE CONTROL, THE PILOT MADE AN UNEVENTFUL LANDING. MAINTENANCE PERSONNEL FOUND THE ACCELERATOR DISCHARGE TUBE LAYING ON THE BOTTOM OF THE INTAKE AIRBOX. IT WAS DETERMINED THAT THE ACCELERATOR DISCHARGE TUBE SEALANT (LOCKTITE) HAD FAILED, CAUSING IT TO SEPARATE FROM THE ACCELERATOR DISCHARGE PORT. THIS CAUSED THE DISCHARGE TUBE TO LIFT UP THROUGH THE BOOST VENTURI BLOCKING ANY MOVEMENT OF THE THROTTLE VALVE. 1H71 3O3 ONT3A12 E274 20011203000652001120300065NM 2001 12 3 2001FA0000488 120011023G5302HS54825H18 BOLT DOUG 600N 600N 3027377NM ALLSN 250C 250C47B GL TAILBOOM BROKEN C K NONE O OTHER ININSP/MAINT 1 WP05959SD RN019 DURING PREFLIGHT PILOT FOUND TAILBOOM BOLT MOVED. MAINTENANCE REMOVED COVER FOUND BOLT SAFETIED, BUT BROKEN 2.5 THREADS FROM SHANK BOLT REMOVED AND REINSTALLED 265.2 HOURS BEFORE. 1G71 3U3 UNCH3WE E1GL 20011203000662001120300066EA 2001 12 3 2001FA0000489 220011101G8520LW13884 MAIN BEARING CESSNA182 182S 2072701CE LYC O540 IO540AB1A5 EA ENGINE DELAMINATED E K NONE O OTHER ININSP/MAINT 1 GL0361US 60 18280935 L2783748C FRONT MAIN BEARING DELAMINATION. DEFECT AREA WAS ABOUT THE SIZE OF A DIME. THERE WAS EVIDENCE OF SUBSURFACE FLAWS IN THE SURROUNDING AREA. THE CAUSE WOULD BE IMPROPER MANUFACTURING. 1H71 3O3 ONT3A13 1E4 20011129000652001112900065GL 2001 11 29 2001FA0000490 320011025G6110C4503 FORK BEECH 55 E55 1152732CE CONT O550 IO550C SO HARTZLHCC4Y HCC4YF2 GL PROPELLER CRACKED B LU4RK NONE O OTHER ININSP/MAINT 1 SO177226R211 TE1013 GL87 RELEVANT INDICATION(CRACK) FOUND BY NON DESTRUCTIVE TEST INSPECTION. 1L72 3O3 O 3A16 E3SO 5 CP52GL 20011129000672001112900067GL 2001 11 29 2001FA0000491 320011025G6110C4503 FORK BEECH 55 E55 1152732CE CONT O550 IO550C SO HARTZLHCC4Y HCC4YF2 GL PROPELLER CRACKED B LU4RK NONE O OTHER ININSP/MAINT 1 SO177226R211 TE1013 RELEVANT INDICATION (CRACK) FOUND BY NON DESTRUCTIVE TEST INSPECTION. 1L72 3O3 O 3A16 E3SO 5 CP52GL 20011129000682001112900068GL 2001 11 29 2001FA0000492 320011022G6111V8433N10 BLADE PIPER PA23 PA23250 7102308SO LYC O540 O540* 41532EA HARTZLHCA2 HCA2MVK2 GL PROPELLER CRACKED B LU4RK NONE O OTHER ININSP/MAINT 1 SO1763ZZ 272421 JH652 CRACK FOUND IN BLADE SHANK BETWEEN TWO SHOULDERS APPROX 2 INCHES IN LENGTH. THREE HUNDRED HOURS EST SINCE LAST INSPECTION. 1L72 3O3 O 1A10 E295 5 CP24EA 20011203000672001120300067CE 2001 12 3 2001FA0000493 120011023G531205121411 BULKHEAD CESSNA170 170B 2072306CE CONT O300 O300* 17022SO FUSELAGE CRACKED B K NONE O OTHER ININSP/MAINT 1 EA053511C2246 26554 BULKHEAD CRACKED AT LOWER RIGHT CORNER WHERE STEERING CABLE PULLEY BRACKET ATTACHES. 1H71 3O3 O A799 E253 20011203000682001120300068 2001 12 3 2001FA0000494 420011023G2300TED93010 CONNECTOR CESSNA172 172R 2072401CE LYC O360 IO360B1E 41514EA COMM SYSTEM LOOSE B I97RO OTHER O OTHER NRNOT REPORTED 1 CE0735331 17281037 COM 1 AND COM 2 INTERMITTENTLY INOPERATIVE. UPON INSPECTION FOUND SMALL COLLARS THAT COME WITH 90 DEGREE CONNECTOR LOOSE IN THE REAR OF BOTH COM 1 AND COM 2 COAX CONNECTORS. 1H71 3O3 ONT3A12 1E10 20011203000692001120300069EA 2001 12 3 2001FA0000497 220011022G8520 CRANKCASE GULSTM500 500B 0141106SW LYC O540 IO540E1A5 41532EA ENGINE CRACKED E O OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW15127KH 672 500B102738 CRANKCASE WAS CRACKED AT NR 2 UPPER CYLINDER STUD AND LEAD INTO OIL PRESSURE GALLEY. ENGINE LOST OIL PRESSURE AND WAS FEATHERED. 1H72 3O3 O 6A1 1E4 20011203000702001120300070CE 2001 12 3 2001FA0000498 120011025G5330 PANEL CESSNA210 210A 2073408CE CONT O470 IO470* 17026SO FUSELAGE CRACKED D K NONE O OTHER ININSP/MAINT 1 SO139419X3395 21057719 WHILE AC WAS IN SHOP FOR PROP/ENGINE BALANCING, CRACK APPROX 4.5 INCHES LONG WAS FOUND ON REAR PANEL OF LOWER FORWARD FUSELAGE STRUCTURE. PANEL PN 12530181. PANEL WAS REPAIRED BY ADDITION OF DOUBLER AS SHOWN ON 377. CRACK WAS LOCATED ON SHEET METAL ABOVE WHEEL WELL. 1H71 3O3 ORT3A21 E1CE 20011120000922001112000092CE 2001 11 20 2001FA0000499 120011108G28222017002 PUMP RKWELLNA265 NA26565 7630107CE FUEL SYS FAILED B K NONE J WARNING INDICATION CRCRUISE 1 CE0182CR 1407 1407 46549 PILOTS REPORTED THAT IN CRUISE FLIGHT LEFT LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED AND LEFT FUEL PUMP CIRCUIT BREAKER POPPED A FEW SECONDS LATER. AFTER LANDING, MAINTENANCE CREW REENGAGED CIRCUIT BREAKER, AND PUMP RAN, BUT WAS EXTREMELY NOISY. THERE WERE NO PREVIOUS INDICATIONS SUGGESTING IMMINENT PUMP FAILURE. MANDATORY OVERHAUL FREQUENCY OF PUMP IS 2000 HOURS, THIS PUMP HAD 1,407 HOURS TOTAL TIME AND SINCE INSTALLATION APRIL 99. SPECULATE THAT AN INTERNAL BEARING FAILED BASED ON THE NOISE PUMP MADE AND THE FACT THAT THERE WAS NO METAL PARTICLE CONTAMINATION IN THE OUTPUT LINE OR IN LINE FILTER. PUMP SENT TO OVERHAUL FACILITY TO DETERMINE ACTUAL FAILURE. 2L72 4J A2WE 20011203000712001120300071SW 2001 12 3 2001FA0000500 120011028G5711 SPAR CAP MOONEYM20 M20C 5870208SW LYC O360 O360* 41514EA WING CORRODED D K NONE O OTHER ININSP/MAINT 1 SO139671M3514 670007 DURING ANNUAL INSPECTION, WING CARRY THROUGH SPAR WAS FOUND TO HAVE EXFOLIATION CORROSION ON TOP SPAR CAP. 1L71 3O3 O 2A3 E286 20011203000722001120300072EU 2001 12 3 2001FA0000501 120011101G3242AH52430 BRAKE ASSY HWKSLYDH125 DH1253ARA 423013PEU RROYCEVIPER VIPER522 54552EU MLG FAILED D O OTHER O OTHER LDLANDING 1 CE03230TS NA700 REPLACE BRAKE ASSEMBLIES UPON 3RD LANDING (TAXING THE NEXT DAY) BRAKES FAILED. 2L72 4J4 J A3EU E3EU 20011203000732001120300073CE 2001 12 3 2001FA0000503 120011106G531331120111 STRINGER LEAR 35 31A 5170531CE GARRTTTFE731TFE731* 01518WP FUSELAGE CRACKED D K NONE O OTHER ININSP/MAINT 1 SW11370SC4814 070 THE RIB IS CRACKED IN 3 EACH PLACES WERE IT ATTACHES TO SKIN CRACKS ORIGINATE FROM RIVETS AND CRACKING TOWARDS OTHER RIVETS. 2L72 4F4 FRTA10CE E6WE 20011203000742001120300074SO 2001 12 3 2001FA0000505 220011029G73246314272A20 FLOW DIVIDER BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO ENGINE DEFECTIVE C VJ3RO OTHER O OTHER NRNOT REPORTED 1 WP075582X887 CE1353 820397R ENGINE RUN ROUGH AND SOMETIME WOULD NOT SHUT DOWN. THE FUEL FLOW DIVIDER WOULD STICK OPEN, LETTING CONTINUOUS FUEL FLOW TO THE ENGINE. THE FLOW DIVIDER WAS REMOVED AND REPLACED WITH A NEW ONE, OPERATION OF ENGINE CHECKED OUT NORMAL. 1L71 3O3 O 3A15 E5CE 20011203000752001120300075SO 2001 12 3 2001FA0000506 220011029G7414M3004 BRUSHES SLICK BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO MAGNETO WORN C VJ3RK NONE O OTHER ININSP/MAINT 1 WP078268T998 00051554 CE1547 820321 MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. THE WEAR ON THIS BRUSH IS ABOVE NORMAL FOR 500 HOURS. (PN M3004 BRUSH). 1L71 3O3 O 3A15 E5CE 20011203000762001120300076SO 2001 12 3 2001FA0000507 220011029G7414M3004 BRUSHES BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO MAGNETO WORN C VJ3RK NONE O OTHER ININSP/MAINT 1 WP0738071504 CE935 820386R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. THE WEAR ON THIS BRUSH IS ABOVE NORMAL FOR 500 HOURS. (PN M3004 BRUSH) 1L71 3O3 O 3A15 E5CE 20011203000772001120300077SO 2001 12 3 2001FA0000508 220011029G7414 BRUSHES SLICK BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO MAGNETO WORN C VJ3RK NONE O OTHER ININSP/MAINT 1 WP0738071504 K3823 CE935 820386R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. THE WEAR ON THIS BRUSH IS ABOVE NORMAL. 1L71 3O3 O 3A15 E5CE 20011203000782001120300078SO 2001 12 3 2001FA0000509 220011029G7414M3004M BRUSHES SLICK BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO MAGNETO WORN C VJ3RK NONE O OTHER ININSP/MAINT 1 WP078268T998 00051555 CE1547 820321 MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. THE WEAR ON THIS BRUSH IS ABOVE NORMAL FOR 500 HOURS. (PN M3004M BRUSH) 1L71 3O3 O 3A15 E5CE 20011203000792001120300079SO 2001 12 3 2001FA0000510 220011029G7414M3004 BRUSHES SLICK BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO MAGNETO WORN C VJ3RK NONE O OTHER ININSP/MAINT 1 WP075521A455 01042023 CE1338 820460R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPARK LINE TO GROUND. THE WEAR ON THIS BRUSH IS ABOVE NORMAL FOR 500 HOURS. (PN M3004 BRUSH) 1L71 3O3 O 3A15 E5CE 20011203000802001120300080SO 2001 12 3 2001FA0000511 220011029G731464621216A PUMP BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO ENGINE LEAKING C VJ3RO OTHER K FLUID LOSS NRNOT REPORTED 1 WP075582X887 CE1353 820397R LEAKING FUEL FROM CASE DRAIN. 1L71 3O3 O 3A15 E5CE 20011203000812001120300081CE 2001 12 3 2001FA0000512 120011108G213113035616 CONTROLLER CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE CABIN PRESSURE MISREPAIRED C U1UMK NONE W INADEQUATE Q C ININSP/MAINT 1 SW015314J3685 5500663 UPON INSTALLATION OF A REPAIRED CABIN PRESSURE RATE CONTROLLER IT WAS FOUND THAT THE AC WOULD NOT TEST OR PRESSURIZE ON THE GROUND. AFTER CHECKING THE ATTACHING SYSTEMS THE CANNON PLUG ON THE CONTROLLER WAS DISCONNECTED AND INSPECTED. AT INSPECTION IT WAS FOUND THAT THE CANNON PLUG PINS WERE PUSHED BACK FAR ENOUGH AND ALSO BENT SO AS NO CONNECTION COULD BE MADE. IT WAS ALSO NOTED THAT ON THE INSIDE OF THE CANNON PLUG THE INSULATION ON THE WIRES HAD NOT BEEN STRIPPED BACK. THE WIRES WERE JUST CRIMPED TO THE PINS AND PUT IN TO THE CANON PLUG. 1L72 4F4 F A22CE E1NE 20011203000832001120300083GL 2001 12 3 2001FA0000514 120011030G2820 FUEL LINE BLANCA17 1731ATC 1220437GL LYC O540 TIO540* 41532EA FUEL SYSTEM CORRODED B FB6RA UNSCHED LANDING K FLUID LOSS NRNOT REPORTED 1 NM01398281678 7331044 AIRCRAFT EXPERIENCED A MASSIVE FUEL LEAK INSIDE OF CABIN AREA CAUSING AN INFLIGHT EMERGENCY. DETERMINED FUEL LEAK CAUSED BY CORROSION OF FUEL LINE FROM FIRE WALL TO FUEL PRESSURE INDICATOR. CORROSION CAUSED BY DISSIMILAR METAL OXIDATION WHERE FUEL LINE WAS ROUTED AGAINST STEEL RIBBED DEFROSTER HOSE. ALUMINUM FUEL LINE RUBBED THROUGH OUTER MATERIAL OF DEFROSTER HOSE RESULTING IN ALUMINUM TO STEEL CONTACT. SUSPECT CONDITION EXISTED SINCE MANUFACTURE OF AIRCRAFT. EXTREME HAZARD TO FLIGHT. 1L71 3O3 O A18CE E14EA 20011203001082001120300108CE 2001 12 3 2001FA0000518 120011031G5530 RIVET BEECH 58 58P 1152744CE CONT O520 TSIO520* 17040SO VERTICAL STAB BROKEN B FE6RK NONE O OTHER ININSP/MAINT 1 NM11145Z TJ289 RIVET HEAD MISSING ON EXTENSION FITTING OF VERTICAL STABILIZER FORWARD SPAR JUST ABOVE AREA WHERE SPAR IS BOLTED TO FUSELAGE BULKHEAD. THERE IS NO EVIDENCE OF CORROSION OR CRACKING OF STRUCTURE IMMEDIATELY SURROUNDING RIVET LOCATION. RIVET APPEARS TO HAVE FAILED IN TENSION. ADJACENT RIVETS APPEAR SOUND. 1L72 3O3 O A23CE E8CE 20011203001092001120300109CE 2001 12 3 2001FA0000519 120011031G53301024400291 SKIN BEECH 58 58P 1152744CE CONT O520 TSIO520* 17040SO FUSELAGE CRACKED B FE6RK NONE O OTHER ININSP/MAINT 1 NM11145Z 7165 TJ289 FOUND ONE INCH LONG CRACK IN AFT UPPER FUSELAGE SKIN AT BASE OF VERTICAL FIN. CRACK STARTS AT LEFT FORWARD STABILIZER SPAR EXTENSION CUTOUT AND EXTENDS UPWARD. SUSPECT LACK OF PROPER RADIUS IN CORNER OF CUTOUT CREATED A STRESS RISER WHICH CAUSED THE SKIN TO CRACK DURING NORMAL FLEXING OF AFT FUSELAGE. 1L72 3O3 O A23CE E8CE 20011203001102001120300110CE 2001 12 3 2001FA0000520 120011031G57301021000115 SKIN BEECH 58 58P 1152744CE CONT O520 TSIO520* 17040SO WING CRACKED B FE6RK NONE O OTHER ININSP/MAINT 1 NM11145Z 7165 TJ289 LOWER INBOARD LEADING EDGE SKIN CRACKED BETWEEN FUEL TANK DRAIN FITTING HOLE AND REAR EDGE OF SKIN. CRACK IS THROUGH AND AREA APPROXIMATELY 2 INCHES WIDE THAT HAS NO RIVET CONNECTING SKIN TO FRONT SPAR STRUCTURE. NORMAL FLEXING OF WING APPEARS TO BE STRESSING THE SKIN IN THIS AREA. THIS IS THE THIRD BARON FOUND WITH THIS PROBLEM. 1L72 3O3 O A23CE E8CE 20020124001012002012400101SO 2002 1 24 2001FA0000521 120011030G27106270102TO13 CONTROL CABLE PIPER PA28 PA28140 7102802SO AILERON & RUDDERCORRODED D K NONE O OTHER ININSP/MAINT 1 EA23 2471 2821855 CONTROL CABLES FOUND TO HAVE CORRODED END FITTINGS AS DESCRIBED IN NTSB LETTER OF APRIL 16, 2001 TO FAA. AILERON, RUDDER,AND STABILATOR CABLES ALL REPLACED WITH NEW. MECHANIC NEEDS TO USE A LOW POWER(5X OR 10X) MAGNIFING GLASS TO SEE PITTING CLEARLY. 1L71 3O 2A13 20011120000932001112000093EA 2001 11 20 2001FA0000522 120011030G3230 DRAG BRACE FRCHLD22 22C7A 3370104EA LANDING GEAR FAILED C O OTHER O OTHER UKUNKNOWN 1 SW99 DRAG BRACE FAILURE. 1H71 3I ATC438 20020124001022002012400102CE 2002 1 24 2001FA0000524 120011105G5511123262224 SPAR CESSNA CESSNA210 T210N 2073456CE ELEVATOR CRACKED G K NONE O OTHER ININSP/MAINT 1 NM04843YT4546 100 21063334 THE FRONT SPAR,ATTACHMENT BRACKET,UPPER AND LOWER SPARS, AND DOUBLERS OF THE HORIZONAL STABILIZER WAS CRACKED. 1H71 3O 3A21 20020124001032002012400103CE 2002 1 24 2001FA0000525 120011105G5521123262226 SPAR CESSNA CESSNA210 T210N 2073456CE ELEVATOR CRACKED G K NONE O OTHER ININSP/MAINT 1 NM04843YT4546 100 21063334 ELEVATOR SPAR CRACKED,ATTACHMENT BRACKET, AND DOUBLERS ALSO CRACKED. 1H71 3O 3A21 20020124001042002012400104CE 2002 1 24 2001FA0000526 120011105G5521123262227 SPAR CESSNA CESSNA210 T210N 2073456CE ELEVATOR CRACKED G K NONE O OTHER ININSP/MAINT 1 NM04843YT4546 100 21063334 ELEVATOR FRONT SPAR, DOUBLERS, AND ATTACHMENT CRACKED.AIRCRAFT USED IN PIPELINE PATROL. 1H71 3O 3A21 20020125000032002012500003SO 2002 1 25 2001FA0000528 120011105G2140A23D04 VALVE PIPER PA23 PA23250 7102308SO HEATER LEAKING D K NONE K FLUID LOSS ININSP/MAINT 1 GL1317WE 3692 277854118 WHILE PERFORMING THE INSPECTION OF THE HEATER FUEL REGULATOR VALVE P/N A23D04 (PIPER P/N 461-731) AS REQUIRED BY AD 2001-17-13, THE VALVE WAS FOUND TO LEAK BY VISUAL INSPECTION. THE LEAKAGE WAS NOT EVIDENT UNTIL THE VALVE WAS REMOVED FROM THE SHROUD. THE VALVE WAS REPLACED WITH A NEW VALVE AS REQUIRED. 1L72 3O 1A10 20020125000042002012500004CE 2002 1 25 2001FA0000529 120011105G5753 ARM CESSNA172 172 2072402CE TE FLAPS WORN C K NONE O OTHER ININSP/MAINT 1 GL154124F3451 46024 DURING AN ANNUAL INSPECTION, ALL FOUR OF THE FLAP ARMS HAD WEAR FROM THE ROLLERS. THE DAMAGE ON 3 OF THE ARMS WAS ABLE TO BE BLENDED WITH LESS THAN .020 OF MATERIAL REMOVAL AND WERE SERVICEABLE AS PER SERVICE BULLETIN. THE DAMAGE TO THE RT INBOARD ARM WAS UNABLE TO BE BLENDED OUT WITHIN LIMITS. A NEW FLAP ARM KIT P/N SK180-44-1 WAS ORDERED. UPON RECEIPT THE NEW PARTS WERE INSPECTED AND IT WAS FOUND THAT ONE OF THE RIVETS HAD NOT BEEN BUCKED AT ALL AND 3 OTHERS HAD SHOP HEADS THAT WERE NOT BUCKED TO THE PROPER DIMENSIONS. THE RIVETS WERE SQUEEZED TO THE PROPER DIMENSIONS AND THE NEW ARM ASSEMBLY INSTALLED. 1H71 3O NT3A12 20020129000022002012900002GL 2002 1 29 2001FA0000530 120011104G5510 TIE BOLT AVIAT A1 A1B 2210406GL LYC O360 O360* 41514EA HARTZLHCC2Y HCC2YK1 GL HORIZONTAL STAB SHEARED C K NONE O OTHER ININSP/MAINT 1 GL15 500 5 L3732036A CH33963B AVIAT HUSKY A1B. BROKEN TIE-ROD BOLT DISCOVERED DURING A POST-FLIGHT PILOT'S INSPECTION. THIS PART ATTACHES THE STRUT (LEFT SIDE STRUT (1 OF 3) = LOWER, ANTERIOR)TO THE LEADING EDGE OF THE HORIZONTAL STABILIZER. UNABLE TO PROVIDE AVIAT PN AS THEIR PARTS CATALOG IS NOT REVISED FROM EARLIER HUSKY MODELS TO SHOW THIS PART AND/OR PROVIDE A NUMBER. 1H71 3O3 ONCA22NM E286 5 CP920 20020125000052002012500005CE 2002 1 25 2001FA0000531 120011108G323008411132 SCREW CESSNA340 340A 2076405CE CONT O520 TSIO520NB 17040SO MCAULY3AF32C3AF32C93 GL DOWNLOCK BROKEN B BIGRO OTHER O OTHER TXTAXI/GRND HDL 1 NM09115BH7169 340A1531 DOWNLOCK ADJUSTING SCREW BROKE FOR REASONS UNKNOWN.THIS ALLOWED LEFT MAIN GEAR TO LOSE DOWNLOCK TENSION. LEFT MAIN LANDING GEAR RETRACTED UNTIL IT STOPPED AGAINST INBOARD GEAR DOOR. THIS ALLOWED PROP TO HIT THE GROUND AND DAMAGE TO LEFT FLAPS OCCURED. 1L72 3O3 O 3A25 E8CE 5 CP22EA 20020125000062002012500006NE 2002 1 25 2001FA0000532 220011108G85503020907 DIPSTICK CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE ENGINE BROKEN B D RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SW1543SA 4951 1471 5500086 PCE71655 FAILURE OF OIL DIPSTICK AT ATTACHMENT LOCK NUT CAUSING LOSS OF OIL AND LOWER THAN NORMAL OIL PRESSURE. 1L72 4F4 F A22CE E1NE 20011205000732001120500073SW 2001 12 5 2001FA0000534 120011016G63103039080 GEARBOX BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MAKING METAL C EA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP19412DE2690 248 36033 APPORXIMATELY 45 MINUTES INTO CRUISE FLIGHT A NR 2 ENGINE CHIP LIGHT ILLUMINATED. THE NR 2 ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO BASE AND PERFORMED A RUN ON LANDING DUE TO INSUFFICIENT POWER FOR HOVERING. THE MAINTENANCE TECHNICIANS PULLED THE NR 2 ENGINE CHIP DETECTORS AND FOUND SIGNIFICANT METAL DEBRIS ON THE ENGINE/COMBINING GEARBOX CHIP DETECTOR AND IN THE OIL FILTER. THE ENGINE OIL WAS SUBSEQUENTLY DRAINED. THE OIL SYSTEM WAS FLUSHED AND THE FILTER REPLACED. THE CHIP DETECTOR WAS CLEANED OF ALL DEBRIS AND THE HELICOPTER WAS RUN FOR 5 MINUTES ON THE GROUND. THE HELICOPTER WAS SHUT DOWN AFTER 5 MINUTES AND AGAIN METAL DEBRIS WAS FOUND ON THE ENGINE/COMBINING GEARBOX CHIP DETECTOR AND IN THE OI1G72 4U4 U H4SW E22EA 20020125000212002012500021CE 2002 1 25 2001FA0000535 120011016G56201014400421 WINDOW BEECH 200 B200 1152922CE CARGO BAY CRACKED C O OTHER O OTHER CRCRUISE 1 WP19185XP3185 BB952 LEFT HAND BAGGAGE COMPARTMENT WINDOW OUTER PANE CRACKED WHILE IN CRUISE FLIGHT. INNER PLY REMAINED INTACT AND FLIGHT CONTINUED UNPRESSURIZED TO HOME BASE WITHOUT FURTHER INCIDENT. 1L72 4T A24CE 20011205000742001120500074GL 2001 12 5 2001FA0000536 220011003G741223064130 EXCITER BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED D C ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SW9917SP 245 53444 847487 ENGINE FAILED TO START. IGNITORS WERE NOT HEARD AS NORMALLY HEARD. IGNITOR WAS REPLACED WITH NEGATIVE RESULTS. IGNITION EXCITOR REPLACED WITH NEW, RESOLVING DESCREPANCY. 1G71 3U3 UO H2SW E1GL 20020125000232002012500023EA 2002 1 25 2001FA0000537 220011019G855078531 HOUSING LYC O320 O320E3D 41508EA OIL PUMP CRACKED B K NONE O OTHER ININSP/MAINT 1 WP07 2981 589 L3400727A UPON DIASSEMBLING THE OIL PUMP, A MINIMUM OF 4 CRACKS WERE FOUND EMANATING RADIALLY FROM THE IMPELLER SHAFT BORE EXTENDING THROUGH THE PUMP BODY. NO EVIDENCE OF FOREIGN OBJECTS PASSING THROUGH THE PUMP GEARS WAS FOUND. 3 O E274 20020125000262002012500026GL 2002 1 25 2001FA0000539 120011024G2821 FUEL FILTER AMTR KIS KISTR1 056201WGL AMTR SUBURUSUBURU GL FUEL SYSTEM CLOGGED G K NONE O OTHER ININSP/MAINT 1 GL09 6 INTREGAL FUEL TANK, FIBERGLASS DUSTY FIBERS CLOGGED FUEL FILTER ENOUGH TO DEGRADE POWER. FORCED LANDING DUE TO LACK OF POWER. AIRCRAFT HAD 6 HOURS SINCE INITAL FLIGHT. IT APPEARS THAT FIBERS FROM INSIDE THE FIBERGLASS FUEL TANK MIGRATED IN THE FIRST FEW HOURS OF OPERATION AND CLOGGED THE IN-LINE FUEL FILTER. 1L71 3O3 ONTEXPA1L71EXPE3O 20011205000752001120500075NM 2001 12 5 2001FA0000540 120011026G5302500N31296 ANGLE DOUG 600N 600N 3027377NM FUSELAGE CRACKED D K NONE O OTHER ININSP/MAINT 1 SW99957SD2125 RN011 INSPECTED RT UPPER TAILBOOM ATTACH FITTING ON FUSELAGE . WE FOUND A CRACK IN ANGLE P/N 500N3129-6. THIS ANGLE CAN ONLY BE SEEN BY REMOVAL OF THE RIVETED PANEL ON THE SIDE OF THE FUSELAGE. WE HAVE FOUND CRACKS ON ALL 3 OF OUR 600N MODELS . 1G71 3U NCH3WE 20011205000762001120500076NM 2001 12 5 2001FA0000541 120011026G5302500N31296 ANGLE DOUG 600N 600N 3027377NM TAIL BOOM CRACKED D K NONE O OTHER ININSP/MAINT 1 SW99958SD2219 RN018 DURING INSPECTION OF THE RT UPPER TAILBOOM MOUNT WE FOUND P/N 500N3129-6 ANGLE CRACKED. TO INSPECT, YOU MUST REMOVE THE RIVETED CLOSURE ,ON THE SIDE OF THE FUSELAGE. WE HAVE FOUND CRACKS ,ON ALL 3, OF OUR 600N MODELS. 1G71 3U NCH3WE 20011205000772001120500077NM 2001 12 5 2001FA0000542 120011026G5302500N3422 FITTING DOUG 600N 600N 3027377NM TAIL BOOM CRACKED D K NONE O OTHER ININSP/MAINT 1 SW99959SD1993 RN019 AFTER THE PILOT REPORTED UNUSUAL TAILBOOM MOVEMENT DURING HIS PREFLIGHT IHSPECTION , ONE OF OUR MECHANICS REMOVE THE TAILBOOM ATTACHMENT FAIRING. HE FOUND THE RT UPPER TAILBOOM ATTACH BOLT HAD FRACTURED , AND THE BOLT HEAD WAS HELD ONLY BY SAFETY WIRE.WE THEN REMOVED THE RIVETED CLOSURE COVERING THE NUTPLATE AND ATTACH FITTING. WE FOUND FITTING, P/N 500N3422,CRACKED AND ANGLE P/N 500N3129-6 ,ALSO CRACKED. WE HAVE GROUNDED ALL 3 OF OUR 600N MODELS , AND HAVE FOUND CRACKS ON ALL 3 ANGLES . 1G71 3U NCH3WE 20020125000292002012500029CE 2002 1 25 2001FA0000543 120011030G571257222061 RIB CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP LT CENTER WING CRACKED B K NONE P NO WARNING INDICATION ININSP/MAINT 1 SO1584LJ 5155 4410084 DURING A SCHEDULED INSPECTION, IT WAS NOTED THAT THE LEFT WING CENTER SECTION CANTED RIB CAP P/N: 5722206-1 (LCWS 26.85) HAD A VISUALLY SUSPECT AREA ALONG THE BEND RADIUS BETWEEN THE CENTER WING MAIN SPAR (FS 177.45) AND FS 188.95. FURTHER INSPECTION USING FLUORESCENT PENETRANT REVEALED (2) CRACKS IN THE RADIUS. BOTH CRACKS ARE APPROXIMATELY 1INCH LONG. AFTER REMOVAL OF THE RIB CAP, CLOSE EXAMINATION OF THE PART REVEALED THAT THE CAP WAS MANUFACTURED WITH THE BEND RADIUS PARALLEL TO THE GRAIN OF THE METAL RESULTING IN A GRAIN SEPARATION TYPE CRACK. 1L72 3T4 TRTA28CE E4WE 20020125000302002012500030CE 2002 1 25 2001FA0000544 120011030G571257222061 RIB CESSNA441 441 2076020CE LT CENTER WING CRACKED B K NONE O OTHER ININSP/MAINT 1 SO1584LJ 5155 4410084 DURING A SCHEDULED INSPECTION, IT WAS NOTED THAT THE RIGHT WING CENTER SECTION CANTED RIB CAP P/N: 5722206-2 (RCSW 26.85) HAD A VISUALLY SUSPECT AREA ALONG THE BEND RADIUS AFT OF THE CENTER WING MAIN SPAR (FS 177.45). FURTHER INSPECTION USING FLUORESCENT PENETRANT CONFIRMED A 1INCH CRACK. AFTER REMOVAL OF THE RIB CAP, CLOSE EXAMINATION OF THE PART REVEALED THAT THE CAP WAS MANUFACTURED WITH THE BEND RADIUS PARALLEL TO THE GRAIN OF THE METAL RESULTING IN A GRAIN SEPERATION TYPE CRACK. 1L72 3T RTA28CE 20011203001112001120300111SO 2001 12 3 2001FA0000545 220011025G74146320 MAGNETO CESSNA340 340A 2076405CE CONT O520 TSIO520NB 17040SO ENGINE CORRODED C O OTHER O OTHER NRNOT REPORTED 1 NE05340KG1200 340A1505 R278307R PILOT NOTED INTERMITTENT ROUGH ENGINE AND FLUCTUATING EGT. DURING SUBSEQUENT TROUBLE SHOOTING, NOTED ONLY ONE IMPULSE COUPLING SOUND. WHEN PULLING ENGINE THROUGH WITH SPARK PLUGS OUT AND TIMING WAS WAY OFF. UPON REMOVAL FOUND THAT COULD BARELY TURN THE MAGNETO BY HAND. WHEN MAGNETO WAS OPENED, THERE WAS RUST SHOWING ON ROTOR AND COIL WEDGE WAS LOOSE. 1L72 3O3 O 3A25 E8CE 20011203001122001120300112 2001 12 3 2001FA0000546 420011026G6113055032111 BULKHEAD CESSNA172 172S 2072439CE SPINNER BROKEN D K NONE O OTHER ININSP/MAINT 1 NM08753GW287 172S8753 REAR SPINNER BULKHEAD WAS FOUND BROKEN AT NUTPLATE NEAREST TO AFT SIDE OF NR 1 BLADE. MATERIAL HAD COMPLETELY SEPARATED FROM BULKHEAD AND ALLOWED THE SPINNER TO BEND OUTWARD FROM CENTRIFUGAL FORCE. SPINNER WAS NOT OBVIOUSLY DAMAGED. THIS BULKHEAD WAS INSTALLED ON THIS AIRCRAFT AT 153.3 HOURS ACTT. THE SPINNER WAS ALSO REPLACED AT THIS TIME DUE TO CRACKING, THE SPINNER WAS REPLACED A SECOND TIME AT 394.7 HOURS ACCT DUE TO CRACKS FROM THE BLADE CUTOUT. AT THIS TIME THE BULKHEAD WAS INSPECTED WITH NO SIGNS OF CRACKING. 1H71 3O NT3A12 20011203001132001120300113EA 2001 12 3 2001FA0000547 220010905G7310LW120980140 FUEL LINE MOONEYM20 M20J 5870219SW LYC O360 IO360A1A 41514EA ENGINE CRACKED D K NONE O OTHER NRNOT REPORTED 1 EA21107191068 243141 FOUND THREE CRACKED FUEL INJECTOR LINES. CRACKS ARE LOCATED AT THE SILVER SWEAT JOINT IN THE FILLET. IT IS AS THOUGH THE JOINT WAS NOT PROPERLY PREPARED OR THE FLUX WAS NOT EFFECTIVE. TWO OF THE TUBES HAD ONLY 1068.2 HOURS SINCE NEW. 1L71 3O3 O 2A3 1E10 20011203001142001120300114EA 2001 12 3 2001FA0000548 220010905G7310LW129980104 FUEL LINE BEECH 23 A2324 1151226CE LYC O360 IO360A1A 41514EA ENGINE CRACKED D K NONE O OTHER NRNOT REPORTED 1 EA213601Q1068 MA226 FOUND THREE CRACKED FUEL INJECTOR LINES. THE CRACKS ARE LOCATED AT THE SILVER SWEAT JOINT IN THE FILLET. IT IS AS THOUGH THE JOINT WAS NOT PROPERLY PREPARED OR THE FLUX WAS NOT EFFECTIVE. TWO OF THE TUBES HAD ONLY 1068.2 HOURS SINCE NEW. 1L71 3O3 O A1CE 1E10 20011203001152001120300115SO 2001 12 3 2001FA0000549 120010921G7810LW13027 ADAPTER PIPER PA31 PA31P 7103120SO LYC O541 TIGO541E1A 41539EA ENGINE BROKEN B EA ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 WP07651SC 31P7630006 L34362 FLANGE ON LEFT ENGINE OUTBOARD ADAPTER BROKE OFF OF ADAPTER. EXHAUST GASES LEAKED FROM SYSTEM CAUSING TURBOCHARGER OUTPUT TO DROP. PILOT SHUT DOWN ENGINE AND RETURNED TO AIRPORT. 1L72 3O3 O A8EA E19EA 20011203001162001120300116SW 2001 12 3 2001FA0000550 120011101G2730200190202 SWITCH MOONEYM20 M20K 5870220SW CONT O360 TSIO360* 17025SO ELEVATOR TRIM STUCK C O OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 WP215262M 251183 DURING TRIM ADJUSTMENT, PILOT EXPERIENCED AN UNCOMMANDED NOSE DOWN ATTITUDE. GROUND INVESTIGATION REVEALED THAT THE ELEVATOR TRIM SWITCH HAD STUCK IN THE NOSE DOWN POSITION. 1L71 3O3 O 2A3 E9CE 20011203001172001120300117SO 2001 12 3 2001FA0000551 220011114G8550 ADAPTER CESSNA182 182B 2072706CE CONT O470 O470L 17026SO ENGINE DEFECTIVE C K NONE J WARNING INDICATION ININSP/MAINT 1 NM087179E 52179 816510L4 NO OIL PRESSURE UPON ENGINE START UP. OIL PUMP, SUCTION TUBE, AND CONNECTIONS CHECKED OK. REMOVED FILTER ADAPTER, INSTALLED FILTER SCREEN ENGINE HAD PROPER OIL PRESSURE. NO APPARENT DAMAGE TO FILTER ADAPTER. 1H71 3O3 ONT3A13 E273 20011210001092001121000109CE 2001 12 10 2001FA0000552 120011108G2436S23731 CONNECTOR CESSNA210 T210N 2073456CE CONT O520 TSIO520* 17040SO VOLTAGE REG LOOSE B O OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL216410N 21062986 AIRCRAFT LOST ELECTRICAL POWER IN FLIGHT. PLUG THAT CONNECTED VOLTAGE REGULATOR/ WARNING INDICATOR TO ALTERNATOR DID NOT LOCK AND VIBRATED LOOSE. BECAUSE THE LOW VOLTAGE INDICATOR DIE NOT ILLUMINATE AND THE AMMETER IS ON THE FAR RIGHT SIDE OF CABIN, PILOT WAS UNAWARE OF PROBLEM UNTIL RADIO COMMUNICATION FAILED. 1H71 3O3 O 3A21 E8CE 20011205000782001120500078EU 2001 12 5 2001FA0000553 120010925G6210117150041 BLADE BOLKMS117 BK117A1 5626010EU MAIN ROTOR CRACKED B YIVRK NONE O OTHER ININSP/MAINT 1 SW19 6969 M/R BLADE WAS RECD AT MFG FOR INSP AND EVAL. ABR STRIP CRACK WAS ID AT BLADE STAT 2305. PORTION OF ABR STRIP WAS REMOVED TO ALLOW EVAL OF UNDERLYING SURFACE. SKIN WAS CRACKED WITH DELAM SURROUNDING AREA. REVIEW OF BLADE RECORDS INDICATE MFG REPAIR ON INNER WEIGHT 1 AND 2. CRACK IN ABR STRIP PROPAGATED FROM A DRILL MARK ON INSIDE OF ABR STRIP IN AREA OF THIS REF REPAIR. REPAIR PERFORMED FOR INSTALL OF PINS THROUGH INNER WEIGHTS 1 AND 2. THREE DRILL MARKS ON INSIDE SURFACE OF ABRASION STRIP THAT LINE UP PINS. PINS ARE INSTALLED FROM UPPER SURFACE, AND IS OBVIOUS THAT HOLES WERE DRILLED TOO DEEP ALLOWING DRILL TO MARK INSIDE OF LWR LEG OF ABR STRIP. CUST REPORTED HAVING OTHER BLADES THAT DEVELOPED ABRASIO1G72 3U H13EU 20011203001192001120300119SO 2001 12 3 2001FA0000554 120011105G2810 FUEL CAP PIPER PA22 PA22108 7102204SO LYC O235 O235* 41505EA RT WING IMPROPER PART D O OTHER W INADEQUATE Q C NRNOT REPORTED 1 EA094855Z 228430 (2) PILOTS HAD FUEL STARVATION. BOTH PILOTS, ON LANDING, CHECK RIGHT WING TANKS AND HEARD HISSING SOUND. EXAMINED CAPS AND FOUND NOW VENT HOLES. BOTH CAPS SEEMED NEW AND MADE OF ALUMINUM. CHANGED CAPS TO VENTED STYLE, HAD NO FURTHER TROUBLE. 1H71 3O3 O 1A6 E223 20011203001202001120300120EA 2001 12 3 2001FA0000555 220011107G8520LS13521 BEARING PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA ENGINE FAILED G K NONE O OTHER ININSP/MAINT 1 EA258458H450 288290053 L2777436A WHILE ACCOMPLISHING 50 HOUR INSPECTION, METAL WAS FOUND IN FILTER. TEAR DOWN OF ENGINE REVEALED THAT BEARING PART FAILED. BATCH NUMBER ON BEARING WAS 5-99. 1L71 3O3 O 2A13 E286 20011203001212001120300121SO 2001 12 3 2001FA0000557 220011115G8520 CRANKSHAFT CIRRUSSR SR20 05628AJGL CONT O360 IO360E 17025SO ENGINE FAILED C A UNSCHED LANDING O OTHER CRCRUISE 1 SO0576CP 410 1054 357182 IN FLIGHT ENGINE FAILURE, CRANKSHAFT COUNTERWEIGHT AND DOUBLE ROD FAILURE, BLEW TWO ROD THROUGH CASE.(K) 1L71 3O3 ONTA00009CHE1CE 20011203001222001120300122EA 2001 12 3 2001FA0000558 220011026G8520 STUD PIPER PA18 PA18 7101802SO LYC O235 O235C1 41505EA ENGINE BROKEN D O OTHER O OTHER NRNOT REPORTED 1 CE077278K 18185 611315 BROKEN CYLINDER BASE STUDS, 5 STUDS BROKEN ON NR 1 CYLINDER, FOUND MIS-TORQUED ON NR 2, NR 3, AND NR 4, ALSO.(K) 1H71 3O3 O 1A2 E223 20011203001232001120300123SO 2001 12 3 2001FA0000564 120010827G32303807802 DOWNLOCK PIPER PA32 PA32R300 7103213SO LYC O540 IO540* 41532EA NLG BROKEN D O OTHER O OTHER CRCRUISE 1 AL01200HM351 32R7680025 NOSE GEAR DROPPED OUT OF WHEEL WELL INFLIGHT. FOUND DOWNLOCK BROKEN WHERE NOSE ACTUATOR ROD ATTACHES. THIS HAS HAPPENED ON MORE THAN ONE OCCASION WITH SAME TYPE OF AIRCRAFT IN THE PAST. SUSPECT MFG. IS MAKING PART FROM SUBSTANDARD MATERIAL. THIS PROBLEM HAS JUST BEEN HAPPENING IN THE PREVIOUS YEAR. THIS PART WAS INSTALLED NEW ABOUT 350 HOUR PREVIOUSLY.(K) 1L71 3O3 O A3SO 1E4 20011203001252001120300125SO 2001 12 3 2001FA0000565 220011112G7414M3006 BEARING SLICK CESSNA182 182Q 2072732CE CONT O470 O470U 17026SO MAGNETO FAILED B CS3RK NONE O OTHER ININSP/MAINT 1 WP176204N 99082637 18267796 PILOT REPORTED RIGHT MAGNETO INOPERATIVE ON RUNUP. REMOVED RIGHT MAGNETO FOUND VERY HAD TO TURN. DISASSEMBLED MAGNETO AND FOUND DRIVE END BEARING FAILED. 1H71 3O3 ONT3A13 E273 20011203001262001120300126SO 2001 12 3 2001FA0000566 220011116G7414 DISTRIBUTOR BLK SLICK BEECH 33 F33A 1151425CE CONT O520 IO520B 17032SO MAGNETO INOPERATIVE B VJ3RK NONE O OTHER ININSP/MAINT 1 WP075585Y463 01042020 CE1389 820461R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW THE MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY SENT TO MFG. FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO.(K) 1L71 3O3 O 3A15 E5CE 20011206001392001120600139SO 2001 12 6 2001FA0000567 220011115G7414 DISTRIBUTOR BLK SLICK BEECH 33 F33A 1151425CE CONT O520 IO520B 17032SO MAGNETO INOPERATIVE B VJ3RK NONE O OTHER ININSP/MAINT 1 WP071569P522 01040901 CE1300 820454R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO.(K) 1L71 3O3 O 3A15 E5CE 20011206001402001120600140SO 2001 12 6 2001FA0000568 220011115G7414 DISTRIBUTOR BLK SLICK BEECH 33 F33A 1151425CE CONT O520 IO520B 17032SO MAGNETO INOPERATIVE B VJ3RK NONE O OTHER ININSP/MAINT 1 WP074609M504 00033035 CE772 820261R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY SENT TO MFG. FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO.(K) 1L71 3O3 O 3A15 E5CE 20011206001412001120600141SO 2001 12 6 2001FA0000569 220011115G7414 DISTRIBUTOR BLK SLICK BEECH 33 F33A 1151425CE CONT O520 IO520B 17032SO MAGNETO INOPERATIVE B VJ3RK NONE O OTHER ININSP/MAINT 1 WP071569P522 01040864 CE1300 820454R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO. 1L71 3O3 O 3A15 E5CE 20011206001422001120600142SO 2001 12 6 2001FA0000570 220011115G7414 DISTRIBUTOR BLK SLICK BEECH 33 F33A 1151425CE CONT O520 IO520B 17032SO MAGNETO INOPERATIVE B VJ3RK NONE O OTHER ININSP/MAINT 1 WP074609M504 00033043 CE772 820261R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY SENT TO MFG. FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO.(K) 1L71 3O3 O 3A15 E5CE 20011206001432001120600143CE 2001 12 6 2001FA0000571 120011116G5510MS210783 NUT PLATE CESSNA172 172R 2072401CE LYC O360 IO360A1A 41514EA HORZ STAB BROKEN D DF2SK NONE O OTHER ININSP/MAINT 1 SW15869CP2355 17280641 DURING 100 HOUR INSPECTION, TECHNICIAN FOUND LOWER ELEVATOR STOP NUTPLATE BROKEN AND FIBER LOCK PORTION OF PART SEPARATED FROM THE REST OF NUTPLATE DETAIL REPEATED ELEVATOR CONTACT WITH STOP BOLT WHEN AIRCRAFT IS PARKED AND CONTROL LOCK IS IN, SUCH AS IN WINDY CONDITIONS.(K) 1H71 3O3 ONT3A12 1E10 20011203001272001120300127EA 2001 12 3 2001FA0000572 220011106G852077672 LIFTER BEECH 60 60 1153602CE LYC O541 TIO541E1C4 41536EA ENGINE SPALLED D K NONE O OTHER ININSP/MAINT 1 WP0733LB 132 132 P74 L163859 UPON REMOVAL OF PUSH RODS AND PUSH ROD TUBES FOR RESEAL, THE LIFTERS WERE REMOVED FOR BLEEDING. THE LIFTERS WERE INSPECTED AND WERE FOUND TO HAVE SEVERE SPALLING. MFG WAS NOTIFIED AND ENGINES ARE TO BE REMOVED AND SENT BACK FOR REPAIR. ENGINES HAVE 132.4 HRS TT. CAMSHAFT IS ALSO WORN. 1L72 3O3 O A12CE E10EA 20011203001282001120300128EU 2001 12 3 2001FA0000573 220011023G8520996920 BEARING AMTR AVDFLYAVIDFLYER GL ROTAX 277 ROTAX277 55555EU ENGINE FAILED G O OTHER R PARTIAL RPM/PWR LOSS CRCRUISE 1 NM0894RS 260 260 3 6913440 ENGINE FAILED IN-FLIGHT DUE TO FAILURE OF CONNECTING ROD ROLLER BEARINGS ON CRANKSHAFT ASSEMBLY. CAUSE UNKNOWN. 1H71 3O3 X EXPA1H71EXPE3X 20011206001442001120600144EA 2001 12 6 2001FA0000576 220011126G8520 CRANKSHAFT CESSNA206 206CESSNA 2073302CE LYC O540 TIO540* 41532EA ENGINE FAILED C O OTHER O OTHER NRNOT REPORTED 1 SO11919LL T20608174 L1044761A CONFIRMED BY ENGINE MANUFACTURER-ENGINE CRANKSHAFT FAILED AT NR 5 CRANKPIN. 1H71 3O3 O A4CE E14EA 20011206001452001120600145EA 2001 12 6 2001FA0000577 220011114G7310LW120980210 FUEL LINE CESSNA182 182S 2072701CE LYC O540 IO540AB1A5 EA ENGINE CHAFED B VDNRK NONE K FLUID LOSS ININSP/MAINT 1 SW09931SJ316 18280931 L2781648A DURING 100 HOUR INSPECTION, DISCOVERED NR2 CYLINDER FUEL INJECTION LINE LEAKING WHILE ACCOMPLISHING MFG SB. FUEL LINE SUPPORT CLAMP HAD BECOME LOOSE AND CAUSED LINE TO CONTACT NR2 CYLINDER FINS, WHICH WORE 6 GROOVES IN LINE. 1H71 3O3 ONT3A13 1E4 20011206001462001120600146CE 2001 12 6 2001FA0000578 120011115G551212326003 SKIN CESSNA210 210D 2073414CE CONT O520 IO520A 17032SO HORIZ STAB DAMAGED D K NONE O OTHER ININSP/MAINT 1 EA13210KE1710 21058505 715920 DURING AN ANNUAL INSPECTION THE RIGHT INBOARD SKIN HAD EXCESSIVE OIL CANNING WHEN FLEXED. WHEN FAIRING, PN 12124265 AND 12124266 (RIGHT AND LEFT) WERE REMOVED, THE RIGHT UPPER SKIN SURFACE UNDER FAIRING WAS CHAFFED THROUGH 4 INCHES IN LENGTH THE LEFT SKIN IN SAME LOCATION WAS CHAFFED 50 PER CENT. .020 SKIN. REPLACED AFFECTED SKINS AND REMOVED SHARP EDGE ON FAIRING AND USED ANTI-CHAFE TAPE. 1H71 3O3 O 3A21 E5CE 20011206001472001120600147CE 2001 12 6 2001FA0000579 120011115G551212326004 SKIN CESSNA210 210D 2073414CE CONT O520 IO520A 17032SO HORIZ STAB DAMAGED D K NONE O OTHER ININSP/MAINT 1 EA13210KE1710 21058505 112413R DURING AN ANNUAL INSPECTION THE RIGHT INBOARD SKIN HAD EXCESSIVE OIL CANNING WHEN FLEXED. WHEN FAIRING, PN 12124265 AND PN 12124266 (RIGHT AND LEFT) WERE REMOVED, THE RIGHT UPPER SKIN SURFACE UNDER FAIRING WAS CHAFFED THROUGH 4 INCHES IN LENGTH THE LEFT SKIN IN SAME LOCATION WAS CHAFFED 50 PER CENT. REPLACED AFFECTED SKINS AND REMOVED SHARP EDGE ON FAIRING AND USED ANTI-CHAFE TAPE. 1H71 3O3 O 3A21 E5CE 20011210001102001121000110CE 2001 12 10 2001FA0000580 120011031G3411S10711 PITOT LINE CESSNA182 182S 2072701CE PITOT/STATIC SYSBURNED D K NONE O OTHER ININSP/MAINT 1 EA259472F296 18280201 PITOT HEAT INSULATION, BURN MARKS WERE FOUND ON PITOT PRESSURE LINE. CONDITION RESULTS FROM HAVING PLASTIC LINE CONNECTED TO HEATED PITOT MAST. THE SB CORRECTS THIS BY ADDING PLASTIC SPIRAL WRAP TO LINE AND POWER WIRES AT THE PITOT MAST. THIS PREVENTS PITOT LINE FROM DIRECTLY CONTACTING HOT PARTS OF PITOT MAST, BUT SPIRAL WRAP INSULATION IS MADE OF SAME MATERIAL AS ORIGINAL PITOT LINE AND SUBJECT TO SAME HEAT DAMAGE. 1H71 3O NT3A13 20011206001482001120600148CE 2001 12 6 2001FA0000581 120011103G81204664120004 BEARING CESSNA414 414A 2075907CE CONT O520 TSIO520* 17040SO TURBOCHARGER DRAGGING D E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 EA1784DA 2278 414A0519 AIRCRAFT LANDED WITH LEFT ENGINE FEATHER AND SECURED. PILOT REPORTED LOW MANIFOLD PRESSURE. INSPECTION REVEALED LEFT TURBOCHARGER BEARINGS DRAGGING. REPLACED TURBOCHARGER WITH OVERHAUL UNIT. ENGINE OPERATIONALLY CHECKED OK. COMPONENT AGE SUSPECTED AS CAUSE BUT LOGBOOKS WERE UNAVAILABLE . TT 2278 1L72 3O3 O A7CE E8CE 20011210001112001121000111SO 2001 12 10 2001FA0000582 120011114G2140A2300475 REGULATOR PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA CABIN HEATER LEAKING D K NONE K FLUID LOSS ININSP/MAINT 1 SO053581C142 318052091 THE HEATER FUEL REGULATOR, WAS INSTALLED NEW, IN OUR AIRCRAFT. AD`S HAVE BEEN COMPLIED WITH. DURING ROUTINE HEATER INSPECTION AND CHECK, FOUND NEW TYPE REGULATOR SEEPING FUEL AROUND HOUSING SEAL. 1L72 3O3 O A20SO E14EA 20011210001122001121000112WP 2001 12 10 2001FA0000583 120011005G2434 WIRE ELECTROSYS RYAN ST3 ST3KR 7830502WP CONT O360 TSIO360KB 17025SO ALTERNATOR MISSING B TZ3RK NONE WJ INADEQUATE Q C WARNING INDICATION ININSP/MAINT 1 WP012022 9032694 1054 NEW EXCHANGE ALTERNATOR SUPPLIED. ALTERNATOR OUTPUT OK. PANEL INOPERATIVE LIGHT STAYS ILLUMINATED. INSPECTION OF ALTERNATOR REVEALED MISSING LEAD WIRE FROM STATOR TO STATOR. ALT LIGHT TERMINAL ON ALTERNATOR. ALTERNATOR REQUIRES ADDITIONAL LEAD WIRE FOR AIRCRAFT WITH PANEL DOWN OPERATIVE LIGHT CONNECTED TO STATOR TERMINAL ON ALTERNATOR. 1L71 3R3 O A749 E9CE 20011210001132001121000113EA 2001 12 10 2001FA0000584 220011114G8530LW12429 CYLINDER PIPER PA25 PA25 7102502SO LYC O540 TIO540C1A 41532EA ENGINE DELAMINATED B YYBRK NONE O OTHER ININSP/MAINT 1 GL03 L529661A LYCOMING CYLINDER PN LW12429 WITH A CERMINILL COATING FROM ECI DELAMINATED. THE AREA WAS ABOUT 1.5 INCHES IN LENGTH AND ABOUT .250 WIDE AT THE TOP OF THE CYLINDER BORE, ABOVE THE PISTON RING TRAVEL. THE PROBABLE CAUSE WAS CORROSION UNDER THE CERMINILL COATING. THIS IS A PLATING DEFECT. THE ECI BATCH NUMBER ON THE CYLINDERS ARE 46463-3, 46463-10, 40739-3D, AND 40739-6D. 1L71 3O3 O 2A10 E14EA 20011210001142001121000114SO 2001 12 10 2001FA0000585 120011124G5102GL0115721688 FUEL LINE BALWKSFIRE FIREFLY715 1050518SO FUEL SYSTEM LEAKING B F65RO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW153214V110 F7912 THIS SET OF FUEL HOSES WERE OBTAINED FROM THE HOLDER OF A PMA. THEY WERE INSTALLED IN MAY. THE HOSE WAS FOUND TO BE LEAKING AT THE CRIMP CONNECTION AT THE END OF THE HOSE. THE LEAK DOES NOT APPEAR TO BE CAUSED BY MISHANDLING, BUT BY A POOR CRIMP JOB. THIS IS THE SECOND HOSE FROM THIS SET THAT HAVE STARTED LEAKING FROM THE SAME LOCATION. 1B00 A14SO 20011210001152001121000115CE 2001 12 10 2001FA0000586 120010430G272004115261 MOUNT CESSNA150 152 2071835CE LYC O235 O235* 41505EA RUDDER PEDAL CRACKED D O OTHER O OTHER NRNOT REPORTED 1 NM17497928393 15283517 PILOTS RIGHT HAND LOW RUDDER PEDAL ASSEMBLY MOUNT CRACKED AROUND WELD CAUSING ON GROUND LOSS OF DIRECTIONAL CONTROL AND MADE BRAKING DIFFICULT. 1H71 3O3 ONT3A19 E223 20011210001162001121000116EA 2001 12 10 2001FA0000587 220011102G852069373 BEARING CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA CONNECTING ROD DEBONDED D K NONE O OTHER ININSP/MAINT 1 NM07714VV1076 15279475 L1843715 PLATING ON BEARING UNBONDED FORM BACKING (ROD SIDE NOT THE CAP SIDE) DATE CODE ON BACK OF BEARING IS 200. 1H71 3O3 ONT3A19 E223 20011210001172001121000117SO 2001 12 10 2001FA0000588 120011120G271062701124 CONTROL CABLE PIPER PA28 PA28181 7102807SO AILERON WORN B UC2RK NONE O OTHER ININSP/MAINT 1 GL19414872125 2843179 DURING A ROUTINE INSPECTION, SUBSTANTIAL WEAR WAS FOUND WHERE THE AILERON BALANCE CABLE RUNS THROUGH THE RIGHT SIDE OF THE FUSELAGE. CABLE WEAR WAS PROBABLY CAUSED BY IMPROPER CABLE ALIGNMENT DURING ASSEMBLY BY MFG. THIS IS THE SECOND OCCURRENCE OF THIS TYPE OF DEFECT FOUND IN OUR FLEET.(K) 1L71 3O 2A13 20011210001182001121000118SO 2001 12 10 2001FA0000589 220011126G8520642396 CRANKSHAFT CESSNA414 414A 2075907CE CONT O520 TSIO520NB 17040SO ENGINE BROKEN B VA1RO OTHER O OTHER NRNOT REPORTED 1 SW19717BD2059 414A0337 521140 CRANKSHAFT BROKE IN 3 SECTIONS, HAD 595.9 SMOH. NO SIGNS OF OIL STARVATION. 1L72 3O3 O A7CE E8CE 20011210001192001121000119NE 2001 12 10 2001FA0000590 120011017G7922 NUT LAKEACLAKE 250LAKE 5110322NE LYC O540 TIO540* 41532EA VERNATHERM MISSING D K NONE O OTHER ININSP/MAINT 1 SO1559CA 616 129 L29861A REMOVED VERNATHERM TO COMPLY WITH MFG SB (CHECK NUT TIGHTNESS). WHEN VALVE REMOVED, THE NUT WAS MISSING. AFTER A THROUGH SEARCH THE NUT WAS FOUND IN THE INBOARD HOSE, OIL COOLER END OF THE COPILOT SIDE OF OIL COOLER (2 OIL COOLER ARE ON THIS INSTALLATION).(K) 1H71 3O3 ONC1A13 E14EA 20011211000112001121100011GL 2001 12 11 2001FA0000591 320010611G61118381010 CLAMP HARTZLHCA2 HCA2MVK2 GL PROPELLER CRACKED B ME4RK NONE O OTHER ININSP/MAINT 1 SO19 1928 H1766 PROPELLER RECEIVED FOR STANDARD OVERHAUL, DUE TO TIME IAW MFG SL. (TSO)1982.9. AFTER PROPELLER DISASSEMBLY, THE FOLLOWING COMPONENTS ARE CONDEMNED: BLADE (PN MV8433-4, SN 36637R) DAMAGED IN COLD ROLLED AREA DUE TO CLAMPS. BLADE (PN MV8433-4, SN C85096R) DAMAGED IN COLD ROLLED AREA DUE TO CLAMPS. CLAMP (PN 838-1010, SN 44) CRACKED THROUGH THE INNER CLAMP ATTACHMENT HOLE. CLAMP (PN 838-1010, SN 57) CRACKED THROUGH INNER CLAMP ATTACH. HOLE. PILOT INDICATED NO ABNORMAL OP. 5 CP24EA 20011211000122001121100012GL 2001 12 11 2001FA0000592 320010611G61118381010 CLAMP HARTZLHCA2 HCA2MVK2 GL PROPELLER CRACKED B ME4RK NONE O OTHER ININSP/MAINT 1 SO19 1928 H1766 PROPELLER RECEIVED FOR STANDARD OVERHAUL, DUE TO TIME. (TSO) 1982.9. AFTER PROPELLER DISASSEMBLY, THE FOLLOWING COMPONENTS ARE CONDEMNED: BLADE (PN MV8433-4, SN 36637R) DAMAGED IN COLD ROLLED AREA DUE TO CLAMPS. BLADE (PN MV8433-4, SN C85096R) DAMAGED IN COLD ROLLED AREA DUE TO CLAMPS. CLAMP (PN 838-1010, SN44) CRACKED THROUGH THE INNER CLAMP ATTACHMENT HOLE. CLAMP (PN 838-1010, SN57) CRACKED THROUGH INNER CLAMP ATTACHMENT HOLE. PILOT INDICATED NO ABNORMAL OP. 5 CP24EA 20011210001202001121000120CE 2001 12 10 2001FA0000593 120011121G3246 WHEEL CESSNA182 R182 2072734CE LYC O540 O540* 41532EA LANDING GEAR CRACKED B K NONE O OTHER ININSP/MAINT 1 EA079979C R18200495 CRACK, 1.25 INCHES IN LENGTH, EMANATING FROM BOLT HOLE. 1H71 3O3 ORT3A13 E295 20011210001212001121000121SO 2001 12 10 2001FA0000594 120010724G28201442800 GASCOLATOR PIPER PA28 PA28* SO LYC O360 O360* 41514EA ENGINE CRACKED G O OTHER A FLAME/FIRE TXTAXI/GRND HDL 1 WP07 DURING ENGINE START, AN INDUCTION FIRE STARTED WHEN THE CARBURETOR BACKFIRED. THE FIRE COULD NOT BE EXTINGUISHED AND DESTROYED THE AIRCRAFT. DURING AN INVESTIGATION THE GASCOLATOR COVER WAS FOUND CRACKED. IT APPEARS THE FUEL LEAKING FROM THE COVER APPEARS TO HAVE FED THE FIRE THAT DESTROYED THE AIRCRAFT. 1L71 3O3 O 2A13 E286 20011210001222001121000122CE 2001 12 10 2001FA0000595 120010710G3213 BUSHING CESSNA CESSNA310 310J 2074226CE CONT O470 O470M 17026SO TORQUE LINK SEPARATED D O OTHER O OTHER TOTAKEOFF 1 SW17 RIGHT MAIN LANDING GEAR UPPER AND LOWER TORQUE LINKS BECAME DISCONNECTED FROM EACH OTHER DURING TAKEOFF ROLL. IT APPEARS THAT A PRESSED IN BUSHING, SEPARATED FROM THE LOWER TORQUE LINK ALLOWING THE BOLT HEAD AND WASHER TO PASS THROUGH THE ENLARGED HOLE NORMALLY OCCUPIED BY THE BUSHING. CATALOG INDICATES THAT A SPECIAL WASHER IS REQUIRED UNDER THE BOLT HEAD. THE SPECIAL WASHER HAS A LARGER OUTSIDE DIAMETER THAN THE STANDARD AN WASHER WHICH WAS FOUND INSTALLED. MM INSTRUCTION DO NOT REQUIRE INSTALLATION OF SPECIAL WASHER. 1L72 3O3 O 3A10 E273 20011210001232001121000123EU 2001 12 10 2001FA0000597 120011120G32307733690395 RELAY SOCATATB20 TB20TRINIDAD8680695EU LYC O540 IO540* 41532EA LANDING GEAR FAILED G O OTHER O OTHER NRNOT REPORTED 1 WP251871S336 1871 LANDING GEAR FAILED TO EXTEND. CIRCUIT BREAKER FOUND OPEN. INVESTIGATION FOUND LANDING GEAR UP, RELAY POINTS WELDED CLOSED. 1L71 3O3 ORTA51EU 1E4 20011210001242001121000124CE 2001 12 10 2001FA0000598 120010817G3260 LENS BEECH 200 200BEECH 1152920CE PWA PT6 PT6A60A 52043NE INSTRUMENT PNL LOOSE D L ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL17339AJ BB339 PILOT REPORTED THAT UPON SETUP FOR APPROACH AND GEAR DOWN SELECTION WAS MADE WITH GEAR SWITCH. THAT AN INDICATION FOR BOTH MAIN GEAR WERE DOWN AND LOCKED, BUT NO INDICATION OF THE NOSE GEAR DOWN AND LOCKED. AIRCRAFT DIVERTED AND VERIFIED WITH ATC THAT NOSE GEAR WAS DOWN. CAUSE: NOSE GEAR GREEN LAMP SOCKET LENS CAME LOOSE. AIRCRAFT LANDED INCIDENT FREE. PLACED AIRCRAFT ON JACKS, RECHECKED EMERGENCY GEAR EXTENSION OPERATION AND RIGGING PER MM. PERFORMED NORMAL EXTENSION AND RETRACTION. TIGHTENED NOSE LAMP LENS FUNCTIONAL TEST OF ALL WORK PERFORMED CHECKS, OK. 1L72 4T4 T A24CE E4EA 20011210001252001121000125CE 2001 12 10 2001FA0000599 120011023G5521043200121 SPAR CESSNA150 152 2071835CE LYC O235 O235* 41505EA ELEVATOR CRACKED D K NONE O OTHER ININSP/MAINT 1 WP07945846515 15285738 REMOVED ELEVATOR TO REPAIR WORN OUTBOARD HINGE BUSHINGS, AFTER ELEVATOR WAS REMOVED FOUND THE ELEVATOR SPAR CRACKED UNDER THE OUTBOARD HINGE WHERE IT ATTACHES TO THE SPAR, REPLACED SPAR WITH NEW. 1H71 3O3 ONT3A19 E223 20011210001262001121000126SO 2001 12 10 2001FA0000600 120010817G324616106900 WHEEL PIPER PA23 PA23250 7102308SO LYC O540 TIO540* 41532EA LT MLG CRACKED D K NONE O OTHER ININSP/MAINT 1 EA2168SE 273780 DURING ANNUAL INSPECTION, FOUND LEFT INNER MAIN WHEEL HALF CRACKED IN THE BEAD AREA ORIGINATING FROM BRAKE ATTACHMENT PLATE RIVETS. 1L72 3O3 O 1A10 E14EA 20011210001342001121000134EA 2001 12 10 2001FA0000601 220011126G7414IO68256013 GEAR PIPER PA32 PA32R300 7103213SO LYC O540 IO540K1A5 41532EA MAGNETO BROKEN D K NONE O OTHER ININSP/MAINT 1 AL01200HM 481 32R7680025 DURING INSPECTION FOUND A DISTRIBUTOR GEAR TOOTH BROKEN AND LAYING IN MAG CAP. THIS IS AN ONGOING PROBLEM. THIS MAG HAS PLASTIC GEARS AND HAS BEEN FOUND IN THIS CONDITION ON NUMEROUS MAGNETOS OF THIS TYPE IN THE PAST. 1L71 3O3 O A3SO 1E4 20011210001352001121000135SO 2001 12 10 2001FA0000602 120011116G52803807601 BRACE PIPER PA32 PA32R300 7103213SO LYC O540 TIO540* 41532EA NLG DOOR BROKEN D K NONE O OTHER ININSP/MAINT 1 AL0140449473 32R7780519 INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE. 1L71 3O3 O A3SO E14EA 20011210001362001121000136SO 2001 12 10 2001FA0000603 120011126G52803807601 BRACE PIPER PA32 PA32R300 7103213SO LYC O540 IO540* 41532EA NLG DOOR BROKEN D K NONE O OTHER ININSP/MAINT 1 AL01200HM481 32R7680025 INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE CRACKED AT REAR ATTACH POINT. THIS IS A COMMON PROBLEM FOUND ON THIS MODEL AIRCRAFT. 1L71 3O3 O A3SO 1E4 20020125000392002012500039SO 2002 1 25 2001FA0000604 220011205G8530501867 WASHER MOONEYM20 M20K 5870220SW CONT O360 TSIO360GB 17025SO ENGINE CYLINDER MISSING D K NONE W INADEQUATE Q C ININSP/MAINT 1 SW09231ND 250207 309202 WHILE TROUBLESHOOTING A FUEL FLOW PROBLEM, AN OIL LEAK MANIFESTED AT NR 6 EXHAUST ROCKER COVER. WHEN COVER REMOVED, THE TAB WASHERS WERE FOUND MISSING FROM THE ROCKER SHAFT STUDS. ALL COVERS WERE REMOVED AND THE SAME CONDITION FOUND. A CHECK OF MAINTENANCE RECORDS REVALED A "TOP OVERHAUL" WAS ACCOMPLISHED 14.7 HOURS PREVIOUS. SUBMITTER SUSPECTS WASHERS WERE LEFT OFF DURING REASSEMBLY. THE TAB WASHERS SERVE TO SAFETY THE ROCKER SHAFT RETAINING NUTS. LOSS OF THE RETAINING NUTS COULD RESULT IN CATASTROPHIC ENGINE FAILURE AND UNPLANNED TERMINATION OF FLIGHT. SUBMITTER FAILS TO COMPREHEND OVERLOOKING THIS CRITICAL PART. INSTALLED 501867 WASHERS ON ALL ROCKER SHAFT STUDS AND SECURED. 1L71 3O3 O 2A3 E9CE 20020125000402002012500040SO 2002 1 25 2001FA0000605 120011205G71203872902 MOUNT PIPER PA32 PA32R301 7103218SO ENGINE CRACKED B K NONE O OTHER ININSP/MAINT 1 SO054369M1877 32R8413022 ENGINE TRUSS WELD ASSY FOUND CRACKED AT STEERING ARM ATTACH POINT 1L71 3O A3SO 20020125000412002012500041SO 2002 1 25 2001FA0000606 120011205G71203872919 MOUNT PIPER PA32 PA32R301 7103218SO ENGINE CRACKED B K NONE O OTHER ININSP/MAINT 1 SO05395HP873 3213085 ENGINE TRUSS WELD ASSEMBY FOUND CRACKED AT STEERING ARM ATTACH POINT. 1L71 3O A3SO 20020125000432002012500043SO 2002 1 25 2001FA0000607 220011114G74146310 MAGNETO CESSNA182 182E 2072712CE CONT O470 O470R 17026SO RT & LT FAILED C A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO113390Y231 18254390 ENGINE RAN A LITTLE ROUGH WHEN STARTED. RAN SMOOTHLY AFTER WARMING UP. A 45 MIN FLIGHT WAS MADE AND THEN ENGINE WAS SHUT DOWN. THE ENGINE STARTED AGAIN WITH NO PROBLEM. ABOUT 45 MINUTES INTO THE NEXT LEG, THE ENGINE BEGAN RUNNING ROUGH AND MISSING. INITIALLY, CARBURATOR ICE WAS SUSPECTED AND CARB HEAT WAS APPLIED. AFTER ABOUT 15 MIN OF FULL CARB HEAT, THE ENGINE APPEARED TO RUN SMOOTHLY. RETURNED TO HOME AIPORT (30 MIN) AND LANDED WITH NO PROBLEM. CARB ICE WAS NOT EXPECTED AS THE HUMIDITY WAS LOW (20 PERCENT). ANOTHER SOURCE FOR THE ENGINE ROUGHNESS WAS LOOKED FOR. IT WAS DISCOVERED THAT ENGINE WOULD NOT START. IGNITION WAS CHECKED AND IT WAS DISCOVERED THE BOTH MAGNETOS IMPULSE COUPLINGS HAD FAILED 1H71 3O3 ONT3A13 E273 20020125000462002012500046EU 2002 1 25 2001FA0000608 120011206G2820L24266701320000 SUPPORT ZLIN 242 Z242L 9970204EU LYC O360 AEIO360A1B6 41514EA FUEL SERVO BROKEN B A UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO15147FS1135 0735 L2842451A EYE SCREW, IS A SUPPORT STRUT WHICH ATTACHES TO THE EXHUST STACK AT ONE END AND THE FUEL SERVO TO ENGINE SUMP ATTACHMENT STUDS AT THE OTHER END. THE STRUT FELL BETWEEN THE THROTTLE ARM AND SUMP. THIS PREVENTED THE ENGINE FROM BEING ABLE TO REDUCE POWER BELOW 1500 RPM. CONDITION REPORTED BY PILOT AND FOUND BY MECHANIC. SUBMITTER REPLACED PART AND SECURED STRUT AT AN ADDITIONAL POINT IN CASE THE REPLACEMANT PART BREAKS AGAIN. THIS ADJUSTMENT WOULD PREVENT THE STRUT FROM FALLING INTO THE CONTROL LINKAGE IF THE PROBLEM REOCCURES. 1L71 3O3 O0 A76EU 1E10 20020125000472002012500047GL 2002 1 25 2001FA0000609 120011016G3201 BRACKET CIRRUSSR SR20 05628AJGL MLG FAIRING BROKEN B ESMRK NONE O OTHER ININSP/MAINT 1 SO11155CD264 1058 BOTH LEFT AND RIGHT MAIN LANDING GEAR INBOUARD FAIRING BRACKETS BROKEN, CAUSING FAIRING TO BE VERY LOOSE. GAUGE OF METAL IS TOO THIN FOR THIS HIGH VIBRATION APPLICATION. 1L71 3O NTA00009CH 20020125000492002012500049GL 2002 1 25 2001FA0000610 120011016G612050597001 BEARING CIRRUSSR SR20 05628AJGL HARTZLHCC3Y PHCC3YF1 GL PROP GOVERNOR BROKEN B ESMRK NONE O OTHER ININSP/MAINT 1 SO11155CD264 1058 PROPELLER GOVERNOR CABLE EXTREMELY STIFF WITH POSSIBLE BROKEN WIRE INSIDE OUTER SHROUD. THIS CAUSED THE THROTTLE LEVER BEARING, WHERE THE ROD END FOR THE PROP GOVERNOR CABLE ATTACHES TO THE THROTTLE LEVER, TO BREAK APART. THE STRENGTH OF THE BEARING FOR THIS APPLICATION IS QUESTIONABLE. THE THROTTLE LEVER PN 10007-001 ALSO HAD TO BE REPLACED. 1L71 3O NTA00009CH 5 CP25EA 20020125000512002012500051CE 2002 1 25 2001FA0000611 120011010G2400S2800275 CONNECTOR CESSNA172 172R 2072401CE J BOX INADEQUATE B ESMRK NONE O OTHER ININSP/MAINT 1 SO11109PH1411 17280802 CONNECTOR PB017, PN: S2800-275, WHICH ATTACHES SHIP WIRING TO J2 OF POWER JUCTION BOX MC01-2A, HAD INADEQUATE CRIMPS OF BOTH WIRE ENDS ATTACHING WIRES TO SOCKETS. SOCKET "A" HAD AN OPEN CIRCUIT WHICH CAUSED LOSS OF BUSS NR 2 H1014. WHEN PULLED ON, THE WIRES EASILY CAME OUT OF THE CONNECTOR. CORRECTIVE ACTION WAS TO CRIMP & SOLDER THE CONNECTOR. 1H71 3O NT3A12 20020125000562002012500056CE 2002 1 25 2001FA0000612 120011123G3240 BRAKE ASSY CESSNA188 A188B 2073005CE MLG MALFUNCTIONED G K NONE O OTHER TXTAXI/GRND HDL 1 SW019541J 18803819T THE PILOT STARTED THE AIRCRAFT ENGINE, THE AIRCRAFT STARTED TO ROLL, AT WHICH TIME THE PILOT APPLIED THE BRAKES. THE LEFT BRAKE WAS OPERATIONAL BUT THE RIGHT WAS FLAT. THIS CAUSED THE AIRCRAFT TO SWERVE TO THE LEFT HITTING A CESSNA CARAVAN DAMAGING BOTH AIRCRAFT. THE BRAKE SYSTEM WAS INSPECTED, RESERVOIR FOUND TO BE FULL, NO LEAKS FOUND. SUSPECT AIR IN THE BRAKE SYSTEM. 1L71 3O A9CE 20020125000642002012500064 2002 1 25 2001FA0000614 420011124G3120S17111 PRESSURE SWITCH CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA MCAULY1C160 1C160DTM GL FUEL SYSTEM LEAKING D K NONE K FLUID LOSS ININSP/MAINT 1 EA215444J5595 17273798 RL96576T 731908 ON ANNUAL INSPECTION FOUND OIL DRIPPING ON RIGHT SIDE OF AFT FIREWALL IN CABIN. TRACED TO LEAKING HOUR METER OIL PRESSURE SWITCH. SWITCH WAS LEAKING INTERNALLY. REPLACED SWITCH. 1H71 3O3 ONT3A12 E274 5 NP910 20020125000662002012500066SO 2002 1 25 2001FA0000615 120011127G57506270114 CONTROL CABLE PIPER PA28 PA28140 7102802SO TE FLAPS CORRODED D K NONE O OTHER ININSP/MAINT 1 EA23 2821855 NEW FLAP CABLE (62701-14) ORDERED TO REPLACE EXISTING FLAP CABLE THAT CORRODED ON MS21260 END FITTING WAS ALSO FOUND TO BE PITTED AND CORRODED. 1L71 3O 2A13 20020125000682002012500068SO 2002 1 25 2001FA0000616 120011129G5330 PANEL GULSTMG1159 GIV 3980115SO FUSELAGE CRACKED B K NONE O OTHER ININSP/MAINT 1 SO11464QS 1264 PANEL (107-CLB-5) LOCATED ON THE LOWER PORTION OF THE FUSELAGE PRESSURE VESSEL AFT OF THE MAIN WHEEL WELL CRACKING AROUND A VHF ANTENNA MOUNTING NUTPLATE ATTACHED TO THE PANEL. 2L72 4F RTA12EA 20020125000692002012500069CE 2002 1 25 2001FA0000617 120011130G212109040022 FAN CESSNA425 425 2076018CE COCKPIT FLOOR FAILED B O OTHER O OTHER CRCRUISE 1 GL095PP 30 0198 AIRCRAFT RETURNED FROM FLIGHT WITH CABIN BLOWER OPERATING BUT NOT MOVING ANY AIR. GAINED ACCESS TO BLOWER ASSEMBLY UNDER CO-PILOT FLOOR. FOUND ALL FAN BLADES TO BE BROKEN OFF. THIS IS THE SECOND TIME THIS HAS HAPPENED IN LESS THAN TWO MONTHS. CHECKED MOTOR FOR SECURITY AND LOOSENESS, CHECKED GOOD. CHECKED FAN HUB FOR SECURITY AND LOOSENESS ON MOTOR SHAFT AND FOUND THAT IT WAS TIGHT. INSTALLING TECHNICIAN SAID THAT HE SPECIFICALLY CHECKED FOR BLADE CLEARANCE AROUND HOUSING WHEN THIS FAN WAS INSTALLED AND IT WAS FINE. HIGHLY SUSPECT DEFECTIVE FAN BLADE AT MANUFACTURE. RECOVERED ALL BROKEN BLADES AND INSPECTED. FOUND ONE WITH WHAT APPEARED TO BE A CLEAN BREAK AT BASE. SUSPECT THAT ONE DEFECTIVE BLADE BRO1L72 3T RTA7CE 20020125000722002012500072CE 2002 1 25 2001FA0000618 120011130G551017052 BRACKET PIPER PA23 PA23150 7102303CE HORIZONTAL STAB CRACKED D K NONE O OTHER ININSP/MAINT 1 NM09 AFTER REMOVING THE PAINT FROM THE ELEVATOR HINGE BRACKETS, DISCOVERED THAT BOTH ELEVATOR HINGE BRACKETS ON THE RIGHT SIDE OF THE HORIZONTAL STABILIZER WERE CRACKED THROUGH THE BEARING BORE BOSS, BETWEEN THE BORE AND THE OUTER EDGE OF THE BRACKET. THE CAUSE OF THE CRACK IS UNKNOWN. 1L72 3O RT1A10 20020125000782002012500078SO 2002 1 25 2001FA0000620 120011203G3234 CONTROL HANDLE EMB 120 EMB120 3260201SO MLG FAILED C O OTHER O OTHER NRNOT REPORTED 1 SW99 LANDING GEAR CONTROL LEVER FAILURE. 2L72 4T RTA31SO 20020125000872002012500087 2002 1 25 2001FA0000621 420011203G2210065001790100 ROLL SERVO BEECH 58 58 1152740CE AUTO PILOT MALFUNCTIONED C O OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 SO05 378 378 TH1947 OPERATOR THAT ROLL CONTROL BECAME RESTRICTED AND DIFFICULT DURING FLIGHT. INVESTIGATION REVEALED THAT THE PRIMARY ROLL SERVO WAS FOUND TO BE CAUSING RESTRICTION TO CAPSTAN. THIS SERVO WAS REMOVED AND HAS AUDIBLE SOUND OF OBJECTS FLOATING LOOSE INTERNALLY. 1L72 3O 3A16 20020125000882002012500088SW 2002 1 25 2001FA0000622 120011204G2820 LINE MOONEYM20 M20J 5870219SW FUEL SYSTEM LEAKING C K NONE K FLUID LOSS ININSP/MAINT 1 EA21 MOONEY 201 M20J: OWNER REPORTED LOW FUEL PRESSURE. FOUND AEROQUIP LINE LEAKING THROUGH BODY OF INNER TUBE STOCK. THIS LINE HAS A STAINLESS STEEL BRAID COVERING FULL LENGTH. HOSE HAD A CURE DATE 3RD QUARTER 1995 WITH MANUFACTURED DATE JAN 1998. HOSE IS CONNECTED TO FUEL INJECTOR AND FUEL PRESSURE SENDER. HOSE WAS LEAKING SUBSTANCIAL AMOUNTS OF FUEL ABOVE EXHAUST SYSTEM AND ENGINE OPERATION WAS NOT AFFECTED. 1L71 3O 2A3 20020125000892002012500089 2002 1 25 2001FA0000623 420011203G2210065001790100 ROLL SERVO AMTR KITFOXKITFOXIV 05620EPGL AUTO PILOT MALFUNCTIONED C A UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 NM11316R 378 OPEREATOR ENCOUTERED RESTRICTED ROLL AUTHORITY. PRIMARY AP SERVO WAS FOUND TO BE CAUSING RESTICTED CAPSTAN MOVEMENT. SOUNDS LIKE LOOSE PARTS AR FLOATING AROUND INSIDE SERVO BODY 1H71 3I NCEXPA 20011210001372001121000137SO 2001 12 10 2001FA0000629 120011116G52803807601 BRACE PIPER PA32 PA32R300 7103213SO LYC O540 IO540* 41532EA NLG DOOR BROKEN D K NONE O OTHER ININSP/MAINT 1 AL01200HM 32R7680025 INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE. 1L71 3O3 O A3SO 1E4 20011210001382001121000138SO 2001 12 10 2001FA0000630 120011116G52803807601 BRACE PIPER PA32 PA32R300 7103213SO LYC O540 IO540* 41532EA NLG DOOR BROKEN D K NONE O OTHER ININSP/MAINT 1 AL0197CR 1075 32R7780078 INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE. 1L71 3O3 O A3SO 1E4 20011210001392001121000139SO 2001 12 10 2001FA0000631 120011116G52803807601 BRACE PIPER PA32 PA32R300 7103213SO LYC O540 TIO540* 41532EA NLG DOOR BROKEN D K NONE O OTHER ININSP/MAINT 1 AL018506F97 32R7780107 INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE. 1L71 3O3 O A3SO E14EA 20011210001402001121000140SO 2001 12 10 2001FA0000632 120011116G52803807601 BRACE PIPER PA32 PA32R300 7103213SO LYC O540 TIO540* 41532EA NLG DOOR BROKEN D K NONE O OTHER ININSP/MAINT 1 AL018506F297 32R7780107 INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE. 1L71 3O3 O A3SO E14EA 20011210001412001121000141SO 2001 12 10 2001FA0000633 120011116G52803807601 BRACE PIPER PA32 PA32R300 7103213SO LYC O540 TIO540* 41532EA NLG DOOR BROKEN D K NONE O OTHER ININSP/MAINT 1 AL018506F93 32R7780107 INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE. 1L71 3O3 O A3SO E14EA 20011210001422001121000142SO 2001 12 10 2001FA0000634 120011116G52803807601 BRACE PIPER PA32 PA32R300 7103213SO NLG DOOR BROKEN D K NONE O OTHER ININSP/MAINT 1 AL014352F369 32R7680441 INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE. 1L71 3O A3SO 20011210001432001121000143SO 2001 12 10 2001FA0000635 120011116G52803807601 BRACE PIPER PA32 PA32R300 7103213SO NLG DOOR BROKEN D K NONE O OTHER ININSP/MAINT 1 AL014352F103 32R7680441 INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE. 1L71 3O A3SO 20011210001442001121000144SO 2001 12 10 2001FA0000636 120011116G52803807601 BRACE PIPER PA32 PA32R300 7103213SO NLG DOOR BROKEN D K NONE O OTHER ININSP/MAINT 1 AL014352F321 32R7680441 INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE. 1L71 3O A3SO 20011210001452001121000145SO 2001 12 10 2001FA0000637 120011116G52803807601 BRACE PIPER PA32 PA32R300 7103213SO LYC O540 TIO540* 41532EA NLG DOOR BROKEN D K NONE O OTHER ININSP/MAINT 1 AL0140449153 32R7780519 INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE. 1L71 3O3 O A3SO E14EA 20011210001462001121000146SO 2001 12 10 2001FA0000638 120011116G52803807601 BRACE PIPER PA32 PA32R300 7103213SO LYC O540 TIO540* 41532EA NLG DOOR BROKEN D K NONE O OTHER ININSP/MAINT 1 AL014044953 32R7780519 INSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE. 1L71 3O3 O A3SO E14EA 20011211000132001121100013SO 2001 12 11 2001FA0000639 220011129G7414 DISTRIBUTOR BLK BEECH 33 F33A 1151425CE CONT O520 IO520B 17032SO MAGNETO FAILED B VJ3RK NONE O OTHER ININSP/MAINT 1 WP071556A449 01040866 CE1318 820455R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW THE MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY SENT TO MFG FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO. 1L71 3O3 O 3A15 E5CE 20011211000142001121100014SO 2001 12 11 2001FA0000640 220011128G7414 DISTRIBUTOR BLK BEECH 33 F33A 1151425CE CONT O520 IO520B 17032SO MAGNETO FAILED B VJ3RK NONE O OTHER ININSP/MAINT 1 WP075530A998 00050438 CE1342 813779R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW THE MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. NEW DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO. 1L71 3O3 O 3A15 E5CE 20011211000152001121100015SO 2001 12 11 2001FA0000641 220011128G7414 DISTRIBUTOR BLK SLICK BEECH 33 F33A 1151425CE CONT O520 IO520B 17032SO MAGNETO FAILED B VJ3RK NONE O OTHER ININSP/MAINT 1 WP075540P 01040863 CE1335 820456R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY SENT TO MFG FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO. 1L71 3O3 O 3A15 E5CE 20011211000162001121100016SO 2001 12 11 2001FA0000642 220011129G7414 DISTRIBUTOR BLK BEECH 33 F33A 1151425CE CONT O520 IO520B 17032SO MAGNETO FAILED B VJ3RK NONE O OTHER ININSP/MAINT 1 WP078240T695 00070052 CE1542 820387R MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW THE MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK ASSEMBLY FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY SENT TO MFG FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY, INSTALLED IN MAGNETO. 1L71 3O3 O 3A15 E5CE 20011211000172001121100017 2001 12 11 2001FA0000643 420011026G2561FV353500137 LIFE VEST CABIN FAILED B KQ1RK NONE O OTHER ININSP/MAINT 1 EA07 LIFE VEST, TYPE FV-35. MFG AVG 1986 FAILED THE MFG. RECOMMENDED 2 PSI CELL TEST IAW MM. 20011211001112001121100111CE 2001 12 11 2001FA0000644 120011130G6120 PIN CESSNA414 414A 2075907CE CONT O520 TSIO520* 17040SO MCAULY3AF32C3AF32C93 GL PROPELLER BROKEN B FG6REA ENGINE SHUTDOWN UNSCHED LANDING WE INADEQUATE Q C VIBRATION/BUFFET NRNOT REPORTED 1 NM1130EE 5064 1690 414A0443 746886 PILOT NOTICED SEVERE VIBRATION IN LEFT ENGINE, SHUTDOWN AND ATTEMPTED FEATHER, WOULD NOT FEATHER, LANDED. FOUND 1 BLADE IN FEATHER AND FREE TO ROTATE. INSPECTION REVEALED 1 ACTUATING PIN HAD FRACTURED IN THREADS. PIN HOLE IN FERRULE NOT DRILLED AND TAPPED DEEP ENOUGH TO ALLOW PIN TO TIGHTEN ON WASHER. FATIGUE TO THREADS LED TO FAILURE.(K) 1L72 3O3 O A7CE E8CE 5 CP22EA 20011211001122001121100112NE 2001 12 11 2001FA0000645 320011107G61116607132886 BLADE ROTOL R389 R3894123F25 NE PROPELLER CRACKED B MS1RK NONE O OTHER ININSP/MAINT 1 EA27 288576741 DR61587 PROPELLER RECEIVED FOR ROUTINE OVERHAUL. AT TEARDOWN, FOUND BLADE (PN 6607132886 SN 2) CRACKED IN OUTER SLEEVE APPROXIMATELY 2.5 INCHES LONG. BLADE REJECTED FROM FURTHER SERVICE. 6 CP30NE 20011211001132001121100113SO 2001 12 11 2001FA0000646 220011025G8530652956 VALVE CESSNA182 182 2072702CE CONT O470 O470L 17026SO ENGINE WORN B CY4RO OTHER O OTHER NRNOT REPORTED 1 AL035670B153 33670 069841R CYLINDER REMOVED DUE TO LOW COMPRESSION. VALVE STEM WORN TO 0.005. 1H71 3O3 ONT3A13 E273 20011211001152001121100115NE 2001 12 11 2001FA0000647 320011129G6114660714200 HUB ROTOL R389 R3894123F25 NE PROPELLER CRACKED B MS1RK NONE O OTHER ININSP/MAINT 1 EA27 7522 DR6178587 PROPELLER RECEIVED FOR OVERHAUL. AT TEAR DOWN, FOUND HUB ASSEMBLY CRACKED ON BLADE BEARING FACE AT HUB SPLIT LINE NR 4 BLADE PORT. HUB ASSEMBLY REJECTED FROM FURTHER SERVICE. 6 CP30NE 20011211001162001121100116NE 2001 12 11 2001FA0000648 320011129G61116607132886 BLADE ROTOL R389 R3894123F25 NE PROPELLER CRACKED B MS1RK NONE O OTHER ININSP/MAINT 1 EA27 25344833 DR694884 PROPELLER WAS REMOVED FROM AIRCRAFT TO CORRECT GREASE LEAK. AT DISASSEMBLY, BLADE (SN 279) WAS FOUND TO BE CRACKED ON OUTER SLEEVE AT ROOT END. BLADE REJECTED FROM FURTHER SERVICE. 6 CP30NE 20011212000912001121200091SO 2001 12 12 2001FA0000649 220010717G8530SA52000A20P CYLINDER CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1500 240860 CYLINDER CRACKED ON INTAKE AND EXHAUST SEATS. 1H71 3O3 O A16CE E5CE 20011212000922001121200092SO 2001 12 12 2001FA0000650 220010717G8530SA52000A20P CYLINDER CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1500 240860 CYLINDER CRACKED ON INTAKE AND EXHAUST SEATS. 1H71 3O3 O A16CE E5CE 20011212000932001121200093SO 2001 12 12 2001FA0000651 220010717G8530SA52000A20P CYLINDER CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1500 240860 CYLINDER CRACKED ON INTAKE AND EXHAUST SEATS. 1H71 3O3 O A16CE E5CE 20011212000942001121200094SO 2001 12 12 2001FA0000652 220010717G8530SA52000A20P CYLINDER CONT O520 IO520F 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1500 CRACKED ON INTAKE AND EXHAUST SEATS. 3 O E5CE 20011212000952001121200095SO 2001 12 12 2001FA0000653 220010717G8530SA52000A20P CYLINDER CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1500 CYLINDER CRACKED ON INTAKE AND EXHAUST SEAT. 1H71 3O3 O A16CE E5CE 20011212000962001121200096SO 2001 12 12 2001FA0000654 220010716G8530SA52000A20P CYLINDER CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 1648 240860 CYLINDER CRACKED ALL THE WAY AROUND AT THE VALVE SEAT LINE AND BURNED THROUGH THE EXHAUST PORT SIDE. 1H71 3O3 O A16CE E5CE 20011212000972001121200097EA 2001 12 12 2001FA0000655 220011106G852077672 LIFTER BEECH 60 60 1153602CE LYC O541 TIO541E1C4 41536EA ENGINE SPALLED B EKGRK NONE O OTHER ININSP/MAINT 1 WP0733LB 132 P74 L104559 UPON REMOVAL OF PUSH RODS AND PUSH ROD TUBES FOR RESEAL. THE LIFTERS WERE REMOVED FOR BLEEDING. THE LIFTERS WERE INSPECTED AND WERE FOUND TO HAVE SEVERE SPALLING. MFG WAS NOTIFIED AND ENGINES ARE TO BE REMOVED AND SENT BACK FOR REPAIR. ENGINES HAVE 132.4 HOURS TT. CAMSHAFT IS ALSO WORN. 1L72 3O3 O A12CE E10EA 20011212000982001121200098 2001 12 12 2001FA0000656 420011126G6122A21107 IDLER GEAR MCAULY CESSNA182 182K 2072724CE CONT O470 O470* 17026SO PROP GOVERNOR CRACKED B LU4RK NONE O OTHER ININSP/MAINT 1 SO172544R 70647 18258244 RELEVANT INDICATION. (CRACK) 1H71 3O3 ONT3A13 E273 20011213000842001121300084EA 2001 12 13 2001FA0000657 220011130G7414M3007 IMPULSE COUPLINGSLICK CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA LT & RT MAGNETOSWORN D UL9GO OTHER O OTHER NRNOT REPORTED 1 GL156436P 15285013 L2223415 INSTALLED NEW M3007 IMPULSE COUPLINGS ON BOTH MAGNETOS. BOTH COUPLINGS CAME OUT OF BOXES DATED 5/25/01. INITIAL OPERATION WAS FINE. IMPULSE COUPLINGS INTERMITTENT SNAPPING. REMOVED MAGNETOS, INSPECTED COUPLINGS PAWLS SHOWED NOTICEABLE WEAR AT CONTACT POINT WITH STRIKER PIN. ALSO LOOSENESS AT PIVOT PIN ATTACH. SUSPECT BAD BATCH OF METAL OR HEAT TREATMENT. INSTALLED NEW IMPULSE COUPLING ASSEMBLIES OPERATIONAL CHECK, FINE. DEFECTIVE IMPULSE COUPLINGS TIME IN SERVICE 93 HOURS/ 119 HOURS 1H71 3O3 ONT3A19 E223 20011214000572001121400057CE 2001 12 14 2001FA0000658 120011103G7160BA8110 GASKET CESSNA180 180K 2072624CE CONT O470 O470U 17026SO AIR FILTER LOOSE D K NONE O OTHER ININSP/MAINT 1 SW0920379450 18053185 THIS AIR FILTER ASSEMBLY HAS THE MANUFACTURING DEFECT DESCRIBED IN AD. WITH THE GASKET COMING LOOSE. FOUND IT DURING ANNUAL INSPECTION AND DISCOVERED THAT IT (BA 8110) IS NOT COVERED BY THE AD. 1H71 3O3 O 5A6 E273 20011214000582001121400058SO 2001 12 14 2001FA0000659 120011204G27209621200 TORQUE TUBE PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360* 17025SO RUDDER DAMAGED B R2JRK NONE O OTHER ININSP/MAINT 1 EA212190K4230 347970096 WHILE INSPECTING RUDDER ON ANNUAL INSPECTION THE INSPECTOR FOUND LOOSENESS AT THE RUDDER TORQUE TUBE ATTACH BOLTS. TEARDOWN INSPECTION SHOWED BOLT HOLES OVERSIZE AND ELONGATED. NEW PARTS INSTALLED BECAUSE (AN 174) BOLTS WERE LARGEST SIZE BOLTS PERMITTED. MFG SB REFERS TO THIS PROBLEM. 1L72 3O3 O A7SO E9CE 20011214000592001121400059SO 2001 12 14 2001FA0000660 120011204G521047958008 SNUBBER PIPER PA31T PA31T 7103124SO CABIN DOOR FAILED D K NONE W INADEQUATE Q C ININSP/MAINT 1 SO11311AC10 31T8120016 RECEIVED 2 DIFFERENT SNUBBERS AND INSTALLED. NEITHER HAD ANY SNUBBING ACTION. NEW PARTS FROM THE FACTORY. 1L72 3T A8EA 20011214000732001121400073CE 2001 12 14 2001FA0000661 120011120G3710CH442CW8 COUPLING CESSNA340 340A 2076405CE CONT O520 TSIO520NB 17040SO VACUUM PUMP SHEARED D O OTHER O OTHER NRNOT REPORTED 1 NM022741R230 340A0922 503320 PNEUMATIC PUMP COUPLING SHEARED AFTER 230.7 HOURS OF OPERATION. 1L72 3O3 O 3A25 E8CE 20011214000742001121400074CE 2001 12 14 2001FA0000662 120011011G3710CH442CW8 PUMP CESSNA340 340A 2076405CE CONT O520 TSIO520NB 17040SO PNEUMATIC SYS SHEARED D O OTHER O OTHER NRNOT REPORTED 1 NM022741R113 340A0922 519294 PNEUMATIC PUMP SHEARED AFTER 113 HOURS OF OPERATION. PUMP COULD BE ROTATED WHEN REMOVED. COUPLING SHOWED SIGNS OF HEAT (MELTED EDGES). 1L72 3O3 O 3A25 E8CE 20011217000782001121700078SO 2001 12 17 2001FA0000664 120011118G2720408424 RUDDER PEDAL PIPER PA18 PA18135 7101820SO COCKPIT WORN D K NONE O OTHER ININSP/MAINT 1 WP219952Q3700 183579 DURING DISASSEMBLY FOR REBUILD ALL AND RUDDER PEDALS WERE FOUND TO BE DAMAGED DUE TO THE RETURN SPRING(40494100) CUTTING THROUGH LOWER HINGE SHAFT, WALL. ALL HAD BEEN WELD REPAIRED BUT WERE AGAIN WORN THROUGH, ALL REPLACED NEW AND APPEAR TO HAVE SAME WALL THICKNESS. AS THE WEAR PROGRESSES THE POTENTIAL FOR BINDING EXISTS. 1H71 3O 1A2 20011217000792001121700079SO 2001 12 17 2001FA0000665 120011118G2720404825 RUDDER PEDAL PIPER PA18 PA18135 7101820SO COCKPIT WORN D K NONE O OTHER ININSP/MAINT 1 WP219952Q3700 183579 DURING DISASSEMBLY FOR REBUILD ALL 4 RUDDER PEDALS WERE FOUND TO BE DAMAGED DUE TO THE RETURN SPRING (40941-00) CUTTING THROUGH LOWER HINGE SHAFT WALL. ALL 4 HAD BEEN WELD REPAIRED BUT WERE AGAIN WORN THROUGH. ALL REPLACED NEW AND APPEAR TO HAVE SAME WALL THICKNESS. AS THE WEAR PROGRESSES THE POTENTIAL FOR BINDING EXISTS. 1H71 3O 1A2 20011217000802001121700080SO 2001 12 17 2001FA0000666 120011204G534395554000 BRACKET PIPER PA34 PA34200 7103405SO LYC O360 IO360A1A 41514EA FUSELAGE WORN D K NONE O OTHER ININSP/MAINT 1 SO1566BL 347250285 DURING PERFORMANCE OF 100 HOUR INSPECTION AND COMPLIANCE WITH AD. DURING GEAR RETRACTION NOTICED MOVEMENT OF NOSE GEAR SUPPORT CENTER ATTACH BOLT. AFTER INVESTIGATION AND INSTALLATION OF ACCESS PANEL ON BELLY OF AIRCRAFT FOUND BRACKET PART 95554-000 LOOSE AND WORN EXCESSIVELY INSTALLED NEW FACTORY PARTS. AIRCRAFT TOTAL TIME 9750.2 1L72 3O3 O A7SO 1E10 20011217000812001121700081SO 2001 12 17 2001FA0000667 120011204G534395554000 BRACKET PIPER PA34 PA34200 7103405SO LYC O360 IO360A1A 41514EA FUSELAGE CRACKED D K NONE O OTHER ININSP/MAINT 1 SO151056U 347250040 DURING PERFORMANCE OF 100 HOUR INSPECTION AND COMPLIANCE WITH AD. DURING GEAR, RETRACTION NOTICED MOVEMENT, OF NOSE GEAR SUPPORT CENTER ATTACH BOLT AFTER INVESTIGATION AND INSTALLATION OF ACCESS PANEL ON BELLY OF AIRCRAFT FOUND BRACKET PART 95554-000 CRACKED AND FITTING PART 95555-000 LOOSE AND WORN EXCESSIVELY. INSTALLED NEW FACTORY PARTS AIRCRAFT. TOTAL TIME 4793.9 1L72 3O3 O A7SO 1E10 20011217000822001121700082SO 2001 12 17 2001FA0000668 220011201G8530 EXHAUST VALVE CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE STUCK D O OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 AL0517GN 20700693 EXHAUST VALVE APPARENTLY STUCK OPEN, WAS STRUCK BY PISTON AND IN TURN SLIGHTLY BENT AT THE STEM. THIS INADVERTENTLY CAUSE THE VALVE TO STICK IN A CLOSED POSITION THERE BY BENDING THE EXHAUST PUSHROD SLIGHTLY. 1H71 3O3 O A16CE E5CE 20011217000832001121700083CE 2001 12 17 2001FA0000669 120011201G306026700696 RESISTOR CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA PROP ANTI-ICE FAILED D O OTHER O OTHER NRNOT REPORTED 1 AL05715HE 208B0603 PROPELLER ANTI-ICE VARISTOR MELTED PLUGS. PLUGS SEEM TO OPEN AND WEAR CAUSING INTERMITTENT POWER TO BRUSH BLOCK, DUE MOST LIKELY TO VIBRATION. CHANGING CONNECTORS WOULD FIX PROBLEM. 1H71 3T3 T A37CE E2NE 20011219000812001121900081CE 2001 12 19 2001FA0000670 120011120G3211 FRAME BEECH 76 76 1153005CE RT MLG CRACKED B ZM3RK NONE O OTHER ININSP/MAINT 1 WP07819ER4724 ME199 DURING ANNUAL INSPECTION, THE RIGHT MAIN LANDING GEAR A-FRAME WAS FOUND CRACKED HALF WAY AROUND THE CIRCUMFERENCE OF THE A FRAME TUBE IN THE AREA WHERE RECURRING INSPECTION WAS REQUIRED BY AD. THIS A-FRAME DID NOT REQUIRE RECURRING INSPECTION BECAUSE IT WAS (PN 105-810023-76) WHICH ELIMINATED THE RECURRING INSPECTION REQUIREMENT. THE A-FRAME HAD 4724.2 HRS 1L72 3O A29CE 20011219000822001121900082SO 2001 12 19 2001FA0000671 120011114G7820 MUFFLER MAULE MX7 MXT7180A 5460187SO LYC O340 O340* 41510EA ENGINE CRACKED G K NONE O OTHER ININSP/MAINT 1 SW1754CH 300 21028C 3562336A WELD SHOULD BE INSPECTED EACH 100 HOURS OR EVERY OIL CHANGE. CRACK COULD BRING EXHAUST GAS INTO CABIN. POOR DESIGN OF MUFFLER AND NOT SUPPORTED PROPERLY. 1H71 3O3 ONC3A23 E277 20020125000902002012500090CE 2002 1 25 2001FA0000672 120011129G5320 EYEBOLT CESSNA170 170B 2072306CE LYC O340 O340* 41510EA FUSELAGE MISINSTALLED D K NONE W INADEQUATE Q C ININSP/MAINT 1 AL014669C 25613 FLOAT EQUIPPED, LIFTING EYES WERE INSTALLED IN THE WRONG POSITION. RESULTING IN DRILLING THROUGH THE MAIN FORWARD WING SPAR AND LEAVING APPROXIMATELY EDGE DISTANCE. BETWEEN THE FORWARD SPAR ATTACH BOLT AND EDGE OF SPAR. (EYES SHOULD BE INSIDE CABIN TOP RIVET LINE) (K) 1H71 3O3 O A799 E277 20011219000832001121900083NM 2001 12 19 2001FA0000673 120011108G2730401611557 HOUSING MOOG BOEING727 727* NM FEEL CONTROL CORRODED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 335 HOUSING ASSEMBLY HAS HEAVY PITTING AND CORROSION IN THE BOLT HOLES, PORTS, CAP ASSEMBLIES AND ON THE SEALING SURFACES. DISSIMILAR METAL CORROSION. 2L73 4F RTA3WE 20011219000842001121900084NM 2001 12 19 2001FA0000674 120011112G2730401611565 HOUSING MOOG BOEING727 727* NM FEEL CONTROL CORRODED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 335 ELBOW HOUSING HAS SEVERE CORROSION IN THE BOLT HOLES, CHECK VALVE PORT, PACKING LANDS AND ON THE SEALING SURFACE. DISSIMILAR METAL CORROSION. 2L73 4F RTA3WE 20011219000852001121900085NM 2001 12 19 2001FA0000675 120011112G27304016146202 CAP MOOG BOEING727 727* NM FEEL CONTROL CORRODED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 335 CAP ASSEMBLY HAS SEVERE CORROSION IN THE PACKING GROOVE, THE INTERIOR AND EXTERIOR SURFACES. DISSIMILAR METAL CORROSION. 2L73 4F RTA3WE 20011219000862001121900086NM 2001 12 19 2001FA0000676 120011112G27304016146302 CAP MOOG BOEING727 727 UTILSYSNM FEEL CONTROL CORRODED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 335 CAP ASSEMBLY HAS SEVERE CORROSION IN THE PACKING GROOVE, THE INTERIOR AND EXTERIOR SURFACES. DISSIMILAR METAL CORROSION. 2L73 4J RTA3WE 20020125000912002012500091NM 2002 1 25 2001FA0000677 120011108G32204400612 COIL PLESSEY BOEING727 727* NM MOTOR BRAKE SHORTED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 901 21201 BRAKE COILS ARE SHORTED AND BURNED. UNDER NORMAL OPERATION THE VIBRATION INCURRED HAS BEEN FOUND TO CAUSE ABRADING BETWEEN THE BRAKE COILS AND STUDS WHICH RESULTS IN A SHORT AND ARCING OF THE BRAKE COILS. REDUCE THE SIZE OF THE COIL WINDINGS OR DIAMETER OF THE STUDS TO ALLOW FOR GREATER CLEARANCE BETWEEN THE TWO. (NOTE: THIS MALFUNCTION APPLIES TO BOTH NEW AND REWOUND COIL ASSEMBLIES. 2L73 4F RTA3WE 20020125000922002012500092NM 2002 1 25 2001FA0000678 120011108G32204400613 COIL PLESSEY BOEING727 727* NM MOTOR BRAKE SHORTED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 901 21201 BRAKE COILS ARE SHORTED AND BURNED. UNDER NORMAL OPERATION THE VIBRATION INCURRED HAS BEEN FOUND TO CAUSE ABRADING BETWEEN THE BRAKE COILS AND STUDS WHICH RESULTS IN A SHORT AND ARCING OF THE BRAKE COILS. REDUCE THE SIZE OF THE COIL WINDINGS OR DIAMETER OF THE STUDS TO ALLOW FOR GREATER CLEARANCE BETWEEN THE TWO. 2L73 4F RTA3WE 20011231001602001123100160NM 2001 12 31 2001FA0000679 120011120G3240511531 HOUSING BOEING737 737* NM SHUTTLE VALVE CRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 HOUSING IS CRACKED INSIDE ONE OF THE BOLT MOUNTING HOLES. FATIGUE, DEFECT IN THE IN THE CASTING OF THE HOUSING AND /OR OVERTORQUING OF BOLT ON INSTALLATION. 2L72 4F RTA16WE 20011231001612001123100161NM 2001 12 31 2001FA0000680 120011120G2923654468311 HOUSING BOEING737 737* NM HYDRAULIC SYS CRACKED B IU6RK NONE O OTHER ININSP/MAINT 1 NM01 HOUSING CRACKED IN PORT NR 1 WHILE APPLYING PRESSURE DURING TESTING. HOUSING HAD LIQUID PENETRANT INSPECTION ACCOMPLISHED PRIOR TO TESTING, WITH NO DEFECTS NOTED. MATERIAL THICKNESS OF PORT NR 1 IS THIN. FATIGUE AND POSSIBLY THE INSTALLATION AND TORQUING OF THE FITTING COULD CONTRIBUTE OVER A PERIOD OF TIME. 2L72 4F RTA16WE 20011231001622001123100162CE 2001 12 31 2001FA0000681 120011126G531204500391791 BULKHEAD CESSNA150 150F 2071814CE CONT O200 O200* 17020SO FUSELAGE CRACKED D K NONE O OTHER ININSP/MAINT 1 GL136937F350 15063537 SINCE MFG. WENT TO PLASTIC BULKHEAD, THEY CRACK ABOUT EVERY 200 HOURS. 1H71 3O3 O 3A19 E252 20020125000932002012500093SO 2002 1 25 2001FA0000682 220010614G8550640849 COVER SWFTMSGC1B GC1B 9230104SO CONT C125 C125 17011SO OIL FILTER FAILED D A UNSCHED LANDING KYJFLUID LOSS ENGINE STOPPAGE WARNING INDICATION NRNOT REPORTED 1 NM132432B 3732 62791R WHILE AIRCRAFT WAS IN FLIGHT ALL ENGINE OIL WAS PUMPED OVERBOARD CAUSING CATASTROPHIC ENGINE FAILURE. LOSS OF ENGINE OIL WAS DUE TO FAILURE OF THREADS ON MAGNESIUM CRANKCASE COVER ASSEMBLY. THE THREADS FAILED WHERE THE OIL FILTER ADAPTER THREADS INTO THE CRANKCASE COVER ASSEMBLY. TO PREVENT REOCCURRENCE, REMOVE THREADED TYPE CONTINENTAL OIL FILTER ASSEMBLY FROM SERVICE. 1L71 3O3 ONCA766 E236 20011231001632001123100163CE 2001 12 31 2001FA0000683 120011211G5610NH2401691 WINDOW RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE731* 01518WP COCKPIT DELAMINATED D K NONE O OTHER ININSP/MAINT 1 WP07910JD655 258420 WINDOW DELAMINATED AT THE CENTER HEATING ELEMENT. POSSIBLE SHORT AT INTERNAL WIRING TO HEATING ELEMENT. THE DELAMINATION AREA IS IN THE BOTTOM CENTER. THE UNIT IS BEING SENT TO MFG FOR FURTHER EVALUATION. 2L72 4F4 FRTA3EU E6WE 20011231001642001123100164SO 2001 12 31 2001FA0000684 220011204G741410357586 DISTRIBUTOR GEARCONT CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MAGNETO BROKEN D A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 NM05402NQ K099814ER 402C0093 AT FIRST POWER REDUCTION AFTER TAKE OFF RIGHT ENGINE STARTED RUNNING ROUGH. PILOT SUSPECTED A MAGNETO AND ISOLATED PROBLEM TO THE RIGHT MAGNETO. PILOT RETURNED TO THE AIRPORT WITH RIGHT ENGINE RUNNING ON JUST THE LEFT MAGNETO. UPON REMOVAL AND DISASSEMBLY OF MAGNETO, THE DISTRIBUTOR GEAR WAS FOUND WITH BROKEN TEETH AND NOT TURNING, RESULTING IN THE MAGNETO FAILING TO FUNCTION, NO OTHER DEFECTS FOUND. DISASSEMBLED LEFT MAGNETO AND NO FAULTS FOUND, POINTS CHECKED GOOD AND NO ADJUSTMENTS NEEDED. NO REASON FOUND FOR FAILURE OF DISTRIBUTOR GEAR IN RIGHT MAGNETO. 1L72 3O3 O A7CE E8CE 20011231001652001123100165EA 2001 12 31 2001FA0000685 220011211G8530 VALVE SEAT ENSTRMF28 280C 3300505GL LYC O360 HIO360E1AD 41514EA ENGINE LOOSE G O OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 EA17123MT 1063 NUMBER 4 CYLINDER HAD AN INTAKE VALVE SEAT COME LOOSE AND THE PISTON HAD BROKEN RINGS. SUBSEQUENT LOSS OF POWER. 1G71 3O3 O H1CE 1E10 20011231001662001123100166CE 2001 12 31 2001FA0000686 120011211G251005142132 CYLINDER CESSNA172 172R 2072401CE SEAT FAILED B WIWRO OTHER O OTHER NRNOT REPORTED 1 WP07181MW3500 17280181 SEAT LOCK CYLINDER FAILED TO LOCK IN POSITION WITH NORMAL SEATBACK PRESSURE. CABLE ADJUSTMENT WITHIN LIMITS. FAILURE OCCURRED DURING NORMAL USE. 1H71 3O NT3A12 20020125000952002012500095EU 2002 1 25 2001FA0000687 120010628G7830 BRACKET AMD FALC50FALCON50MYST2730106EU GARRTTTFE731TFE731* 01518WP T/R DOOR BROKEN D O OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO11500AF7225 170 AFTER LANDING, THE CREW TRIED TO STOW THE THRUST REVERSER HAD A TRANSIT LIGHT ON IN THE COCKPIT. A VISUAL INSPECTION REVELED THE RIGHT THRUST REVERSER DOOR (PN C41B30212-39 SN 2287) HINGE ARM HAD BROKE BETWEEN THE LOWER HINGE BEARING AND THE DOOR. ALSO DAMAGED WERE A SUPPORT BRACKET (PNF50B583001024) AND THE RIGHT UPPER BUSHING. A NEW BRACKET WAS INSTALLED AND THE BUSHING WAS REPLACED WITH AN OVERSIZED BUSHING. A ROD BEARING AND ALL HINGE BOLTS FOR BOTH LEFT AND RIGHT DOORS WERE REPLACED. 2 OTHER CASES OF CRACKS WERE FOUND IN THE AREA OF OUT THRUST REVERSER HINGE FAILURE. THE PROBABLE CAUSE FOR FAILURE WAS FATIGUE. 2L73 4F4 F A46EU E6WE 20011231001672001123100167CE 2001 12 31 2001FA0000688 220010316G7314LW15473 PUMP CONT IO360 IO360* 17025CE ENGINE FAILED C XBTRK NONE L NO TEST ININSP/MAINT 1 SW15 966336A ON 16 MAR O1 BPA RETURNED TO SERVICE (PN IO360, SN 966336A) AFTER SATISFACTORY TEST AFTER OVERHAUL. THE ENGINE WAS SUBSEQUENTLY INSTALLED AT ANOTHER FACILITY. THE MECHANIC NOTIFIED US BY PHONE THAT FUEL WOULD NOT FLOW THRU THE FUEL PUMP EVEN WITH THE USE OF THE WOBBLE PUMP, THAT FUEL PRESSURE FROM THE WOBBLE PUMP WAS AVAILABLE AT THE ENGINE NEW AT INSTALLATION IN FACILITY AND IS AFFECTED BY SB. THIS IS IN DIRECT CONFLICT WITH THE FIELD REPORTS OF FAILURE QUOTED ABOVE. THIS IS A DEFINITE SAFETY OF FLIGHT ITEM. COMPLETE STOPPAGE OF THE ENGINE CAN AND IS LIKELY TO OCCUR WITH NO REMEDIAL ACTION AVAILABLE TO THE PILOT. 3 O E1CE 20020117000382002011700038 2002 1 17 2001FA0000689 420011024G6122 LINE CESSNA208 208 2073702CE ENGINE CRACKED A HSYAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 NM05903FF B0003 AIRCRAFT WOULD NOT MAKE TAKEOFF POWER, RESULTED IN RTO. CRACKED PY LINE BETWEEN FUEL CONTROL AND PROP GOV. REMOVED AND REPLACED PY RIGHT LINE GOING TO PROP AND PERFORMED A SUCCESSFUL OPERATIONAL AND LEAK CHECK. (M) 1H71 3T NTA37CE 20020116001492002011600149SO 2002 1 16 2001FA0000690 120011113G2910 HYDRAULIC LINE EMB 120 EMB120ER 3260203SO HYDRAULIC SYS CHAFED A HSYAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM05223AS 120021 BLUE HYDRAULIC FLUID LOSS. BLUE SYSTEM HYDRAULIC LINE CHAFFED THROUGH. REPAIRED LINE WITH PERMISSIVE IAW EMB-120 MM 20-10-01 AND A SUCCESSFUL LEAK CHECK WAS PERFORMED. (M) 2L72 4T RTA31SO 20011231001682001123100168 2001 12 31 2001FA0000691 420011214G34226446 FLUX DETECTOR PIPER PA46 PA46500TP 7104622SO PWA PT6 PT6* 52043EA DIRECTIONAL SYS FAILED B O OTHER O OTHER NRNOT REPORTED 1 EA07164ST 4697064 AFTER 10-30 HOURS OF AIRCRAFT OPERATION FLUX VALVE IS FAILING. SUSPECT THE PROBLEM IS VIBRATION RELATED. NEED TO REPLACE HORIZONTAL STABILIZER IF PROBLEM CANNOT BE ISOLATED. 1L71 3O3 TRTA25SO E2NE 20020201000202002020100020EA 2002 2 1 2002F00003 120010911G5320858947 SUPPORT CNDAIRCL604 CL604 1900301EA WATER SEP CRACKED H K NONE O OTHER ININSP/MAINT 1 WP28TCDHE 5358 THE FLANGE OF THE WATER SEPARATOR SUPPORT ASSEMBLY WAS CRACKED IN TWO PLACES. 2L72 4F RTA21EA 20020201000212002020100021NE 2002 2 1 2002F00036 320011218G6111RFC11M1R6A BLADE HAMSTD14RF 14RF9 NE PROPELLER CRACKED B K NONE O OTHER ININSP/MAINT 1 NM01 3085 TWO CRACK INDICATIONS ON THE BLADE SHANK. ONE IN THE FILLET AREA AND THE OTHER IN THE BLADE BUTT AREA. INDICATIONS WERE PARALLEL AND 2 TO 3 INCHES IN LENGTH. 6 CP11NE 20020125001002002012500100GL 2002 1 25 2002FA0000000 320011212G6114D4883C55 HUB MCAULY2AF34C2AF34C55 GL PROPELLER CRACKED B ME4DK NONE O OTHER ININSP/MAINT 1 SO15 815861 DURING INSPECTION HUB WAS FOUND TO BE CRACKED IN THREADS. HUB HAS BEEN SCRAPPED. 5 CP5EA 20020125001022002012500102SO 2002 1 25 2002FA0000001 220011113G853035967 SEAT CONT O520 IO520* 17032SO ENG CYLINDER CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL03 116 818927R FOUND SEAT CRACKED DURING CLYINDER INSPECTION AT 116.7 HOURS SINCE FACTORY REMANUFACTURE. 3 O E5CE 20020125001032002012500103SO 2002 1 25 2002FA0000002 120011129G3411 PITOT LINE PIPER PA28 PA28181 7102807SO LEFT WING DETERIORATED B NS4RK NONE O OTHER ININSP/MAINT 1 SO359290N481 2843108 DURING 24 MONTH IFR RECERTIFCATION, STATIC SYSTEM HAD WIDE OPEN LEAK. DURING TROUBLESHOOTING, PITOT SYSTEM FOUND TO HAVE WIDE OPEN LEAK ALSO. FOUND BOTH HOLES SPLIT AND DETERIORATED AT JUNCTION FROM PITOT/STATIC PROBE TO METAL LINES IN LEFT WING. NOTE: THIS AIRCRAFT IS LOCATED IN HIGH CORROSION ENVIRONMENT (SALT AIR). SUGGEST USE OF FUEL LINE, INSTEAD OF VACCUM LINE. 1L71 3O 2A13 20020125001042002012500104CE 2002 1 25 2002FA0000003 120011127G7714S25502 CABLE CESSNA172 172S 2072439CE LYC O360 IO360A1A 41514EA TACHOMETER BROKEN G K NONE O OTHER ININSP/MAINT 1 GL11917MA1139 172S8270 TACHOMETER CABLE BROKE, JUST AFT OF ENGINE. 1H71 3O3 ONT3A12 1E10 20020125001052002012500105SW 2002 1 25 2002FA0000004 120011216G8011S8111 CONTACTOR BBAVIA402 402CHAMP 2110204SW CONT O200 O200A 17020SO FIELD COIL BROKEN C K NONE O OTHER ININSP/MAINT 1 EA259957Y32 40213 UNABLE TO OPERATE AIRCRAFT. STARTER CONTACTOR RELAY INOPERATIVE UPON DISASSEMBLY, FOUND FIELD COIL WIRE WHERE IT ATTACHES TO POSITIVE CONNECTOR BROKEN OFF. 1L72 3O3 O A3CE E252 20020125001062002012500106CE 2002 1 25 2002FA0000005 120011220G760263255536 ARM CESSNA337 337H 2075732CE CONT O360 IO360GB 17025SO MIXTURE CONTROL WORN D K NONE O OTHER ININSP/MAINT 1 NE021258S 33701894 352804 DURING ANNUAL INSPECTION FOUND MIXTURE ARM ROD END ATTACHING BOLT LOOSE. ATTEMPTED TO TIGHTEN BOLT BUT FOUND THERE WAS STILL PLAY. DISASSEMBLED ROD END ATTACHING BOLT AND A STEEL SERRATED BEARING INSERT FELL OUT OF THE BRONZE MIXTURE ARM. THIS WAS CAUSED BY THE ROD END ATTACHING BOLT BEING TOO LOOSE. SPHERICAL BALL ROD END ATTACHING BOLTS SHOULD BE TIGHT TO ALLOW THE ROD END TO ROTATE AROUND THE BALL. 1H72 3O3 O A6CE E1CE 20020125001072002012500107CE 2002 1 25 2002FA0000006 120011201G322022430151 CLAMP CESSNA182 TR182 2072735CE LYC O540 O540* 41532EA SHIMMY DAMPER BROKEN D K NONE O OTHER ININSP/MAINT 1 GL23737HU R18200832 THIS CLAMP HOLDS THE SHIMMY DAMPNER IN POSITION ON THE NOSE GEAR BARRELL WITH A PIN WELDED INSIDE THE CLAMP. PIN WAS FOUND BROKEN AND THIS ALLOWED THE CLAMP TO SHIFT WHICH CAUSED THE SHIMMY DAMPNER TO HIT THE GEAR WELL AND SOME TIMES LOCK THE GEAR IN THE UP POSITION. A SLIP MARK HELPS TO FIND THIS PROBLEM ON PREFLIGHT INSPECTION AND ANNUALS. I DO NOT THINK THIS PIN GETS BROKEN IN NORMAL USE BUT COULD VERY EASILY BE BROKEN BY USE OF A LARGE TUG. 1H71 3O3 O 3A13 E295 20020125001082002012500108EA 2002 1 25 2002FA0000007 220011215G732278A110 LOCK PRECISION CESSNA172 172M 2072418CE LYC O320 O320* 41508EA CARB BOWL INOPERATIVE D K NONE O OTHER ININSP/MAINT 1 SW01 20 CARBURETOR BOWL SCREWS LOOSE WITH TAB LOCKS IN PLACE. LOCKS DO NOT HELP SCREWS SECURELY LETTING SCREW LOOSEN SLIGHTLY CAUSING POOR RUNNING ENGINE AND FUEL LEAK, POTENTIAL FIRE HAZARD. IMPROVE FIT OF LOCK TO HOUSING. 1H71 3O3 ONT3A12 E274 20020125001092002012500109CE 2002 1 25 2002FA0000009 120011212G3230 GEARBOX CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MLG WORN D K NONE O OTHER ININSP/MAINT 1 WP135403M17891 402B0003 DURING GEAR EXTENSION, PILOT REPORTED A LOUD NOISE. REPORTED 3 GREEN LIGHTS FOR DOWN AND LOCK GEAR INDICATION, AND EMERGENCY LANDING ASSISTANCE WAS REQUESTED, AIRCRAFT LANDED SAFELY AND TAXIED TO THE MAINTENANCE FACILITY, UPON INSPECTION OF THE LANDING GEAR SYSTEM, THE REDUCTION GEAR UNIT WAS FOUND TO BE WORN AND THE CAUSE OF THE LOUD NOISE. TOOTHED PART OF THE UNIT WAS REPLACED GEAR UP AND DOWN. CHECKS WERE PERFORMED, IAW MM AND FOUND TO BE IN LIMITS. AIRCRAFT LOG BOOK ENTRY WAS MADE AND RELEASED TO SERVICE. 1L72 3O3 O A7CE E8CE 20020125001102002012500110SO 2002 1 25 2002FA0000010 220011210G8530534398 EXHAUST ROCKER CESSNA182 182L 2072726CE CONT O470 O470R 17026SO ENGINE MISMANUFACTURED D K NONE W INADEQUATE Q C ININSP/MAINT 1 NM0242862189 18259222 THE INSTALLED EXHAUST ROCKERS WERE PN 534398. THEY EXPLAINED THAT THOSE ROCKERS DID NOT HAVE THE HOLE DRILLED TO SQUIRT OIL ON THE EXHAUST VALVE STEM. THE NEW EXHAUST ROCKER HAS THAT SQUIRTER HOLE TO AID IN LUBRICATION. THIS WAS CAUSE OF FAILURE, PER MFG. NEW EXHAUST ROCKER IS PN 641682 (2 PIECE BUSHING) OR PN 652130 (1 PIECE BUSHING). SOME REPAIR SHOPS MODIFY OLD PART NUMBER ROCKER ARM BY DRILLING THE SQUIRTER HOLE. OLD ROCKER ARMS (PN 534398) WERE INSTALLED IN THE ENGINE FOR AT LEAST THE PREVIOUS 1400 HOURS PRIOR TO THE OVERHAUL AND DID NOT CAUSE PREMATURE VALVE OR GUIDE WEAR. 1H71 3O3 ONT3A13 E273 20020125001112002012500111SO 2002 1 25 2002FA0000011 220011210G8530643767 GUIDE CESSNA182 182L 2072726CE CONT O470 O470R 17026SO CYLINDER WORN D K NONE O OTHER ININSP/MAINT 1 NM0242862189 18259222 COMPRESSION TEST INDICATED NR 1 AND NR 2 CYLINDERS HAVE EXHAUST LEAKS. REMOVED CYLINDERS AND DIMENSIONALLY INSPECTING VALVES AND GUIDES. SEVERE WEAR OF BOTH GUIDE AND VALVE. 1H71 3O3 ONT3A13 E273 20020125001122002012500112SO 2002 1 25 2002FA0000012 220011210G8530652956 VALVE CONT CESSNA182 182L 2072726CE CONT O470 O470R 17026SO CYLINDER WORN D K NONE O OTHER ININSP/MAINT 1 NM0242862189 18259222 COMPRESSION TEST INDICATED NR 1 AND NR 2 CYLINDERS HAVE EXHAUST LEAKS. REMOVED CYLINDERS AND DIMENSIONALLY INSPECTING VALVES AND GUIDES. SEVERE WEAR OF BOTH GUIDE AND VALVE. 1H71 3O3 ONT3A13 E273 20020125001132002012500113CE 2002 1 25 2002FA0000013 120011112G712045A34361005 MOUNT BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE ENGINE CRACKED D K NONE O OTHER ININSP/MAINT 1 SO11712TA2799 RK186 WHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT TO BE CRACKED. 2H72 4F4 FRTA16SW E25EA 20020125001142002012500114EA 2002 1 25 2002FA0000015 220011024G852075089 PISTON LYC O320 O320D2G 41508EA ENGINE MISMANUFACTURED D K NONE O OTHER ININSP/MAINT 1 SO01 DURING INSTALLATION OF NEW PISTON AND RINGS. IT WAS NOTED THAT ONE OF THE PISTONS WOULD ONLY SLIDE INTO THE BARREL HALF WAY. PISTON SKIRT OD WERE CHECKED, OK AT 5.1175 OD. THE PROBLEM WAS FOUND TO BE THE OD OF THE PISTON JUST BELOW THE PISTON PIN WAS MEASURED TO BE 5.1255 ON THE PISTON THAT DID NOT FIT, THIS IS MUCH LARGER THAN THE SAME OD OF PISTONS THAT DID FIT WHICH WAS MEASURED TO BE 5.1025. 3 O E274 20020125001152002012500115EU 2002 1 25 2002FA0000016 120011211G2910 HOSE BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE731* 01518WP HYD SYSTEM CORRODED G K NONE O OTHER ININSP/MAINT 1 SO17731DL NA0234 HEAVY CORROSION BUILD UP UNDER OUTER PLASTIC SLEEVE ON EXTERIOR HYDRAULIC SYSTEM FLEX HOSES MOSTLY IN THE LANDING GEAR AREA DUE TO WATER OR DISSIMILAR METAL. THIS ONLY NOTED ON 700 SERIES AIRCRAFT. REC. SB OR SL TO LOOK FOR BULGING AT METAL BRAID HOSE WHERE HOSE MEETS THE (B) NUT FITTING. 2L72 4F4 F A3EU E6WE 20020125001182002012500118EU 2002 1 25 2002FA0000017 120011214G3230259UM95 TORQUE LINK BRAERO1000 HAWKER1000 7450005EU MLG CRACKED B RO3RK NONE O OTHER ININSP/MAINT 1 CE03 DURING OVERHAUL, INSPECTION PROCESSES ARE IDENTIFYING CRACKS IN THE FLANGE / WEBBING AREAS OF THE STEEL TORQUE LINKS (PN 25-9UM9-5) FOR THE MAIN LANDING GEAR. CRACKS HAVE BEEN FOUND ON FOUR(4) OF THE LINKS, WHICH HAVE BETWEEN 3967 AND 5603 CYCLES SINCE REPLACEMENT. 2L72 4F RTA3EU 20020125001192002012500119CE 2002 1 25 2002FA0000018 120011212G2421 BOLT PRESTOLITE CESSNA421 421B 2076014CE CONT O520 GTSIO520H 17032SO ALTERNATOR LOOSE D K NONE O OTHER ININSP/MAINT 1 GL07421PK44 A119964 421B0830 22441373H ALTERNATOR THRU BOLT CAME OUT AND ARCED ON STATOR TERMINAL. INSPECTED ALTERNATOR AND REINSTALLED ALTERNATOR BOLT. CHECKED TORQUE ON REMAINING BOLTS. SUGGEST BENDING LOCK TABS OVER PROPERLY AFTER TORQUING BOLTS. 1L72 3O3 O A7CE E7CE 20020125001202002012500120SO 2002 1 25 2002FA0000019 120011218G55301610303 BRACKET PIPER PA23 PA23250 7102308SO LYC O540 IO540* 41532EA VERTICAL STAB CRACKED B K NONE O OTHER ININSP/MAINT 1 WP176249Y3132 273487 L1981948 VERTICAL STAB BRACKET CRACKED, OCCURRED DURING NORMAL OPERATING CONDITIONS AND WAS DISCOVERED AT APPROX. 3130 ACTT. 1L72 3O3 O 1A10 1E4 20020125001212002012500121SO 2002 1 25 2002FA0000020 120011218G55301610302 BRACKET PIPER PA23 PA23250 7102308SO LYC O540 IO540* 41532EA VERTICAL STAB CRACKED D K NONE O OTHER ININSP/MAINT 1 WP176249Y3132 273487 VERICAL STAB BRACKET CRACKED, OCCURRED DURING NORMAL OPERATING CONDITIONS AND WAS DISCOVERED AT APPROX 3130 AC TT. 1L72 3O3 O 1A10 1E4 20020125001222002012500122SO 2002 1 25 2002FA0000021 220011126G8520 CONNECTING ROD CESSNA172 172H 2072424CE CONT O300 O300* 17022SO ENGINE FAILED D O OTHER R PARTIAL RPM/PWR LOSS DEDESCENT 1 EA233910R 17255410 NUMBER THREE CYLINDER CONNECTING ROD AND CAP FAILED AT CRANKSHAFT. THE CONNECTING ROD THEN FELL DOWN TO THE BOTTOM OF THE CYLINDER BORE AND WAS STRUCK REPEATEDLY BY THE CRANKSHAFT UNTIL ENGINE WAS SHUTDOWN. THE FAILURE OCCURRED AFTER FINAL POWER REDUCTION DURING A ROUTINE LANDING. THE PILOT DESCRIBED HEARING A LOUD BANG FOLLOWED BY A LOSS OF POWER. CAUSE OF FAILURE UNDETERMINABLE. 1H71 3O3 ONT3A12 E253 20020125001242002012500124EU 2002 1 25 2002FA0000022 120011012G6520350A33109100 GEAR AEROSPAS355 AS355* EU T/R GEARBOX MISALIGNED B FF6RK NONE O OTHER ININSP/MAINT 1 NM08 UNABLE TO ESTABLISH ACCEPTABLE GEAR PATTERN ON PINION. 1G72 3U H11EU 20020125001252002012500125SO 2002 1 25 2002FA0000023 220011113G8520 BEARING CESSNA402 402B 207590PCE CONT O520 TSIO520EB 17040SO LT ENGINE FAILED D EA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SO173748C1166 402B0606 815069R IN FLIGHT FAILURE OF LT ENGINE NR 2 ROD BEARING FAILED CAUSING CASE DAMAGE. ROUGH RUNNING AND OIL LOSS. PILOT SHUT DOWN ENGINE AND MADE A SUCCESSFUL LANDING TBO IS 1400 HR. ENGINE HAD 1166.9 SINCE FACTORY REMANUFACTURE. 1L72 3O3 O A7CE E8CE 20020125001262002012500126CE 2002 1 25 2002FA0000024 120011214G6120C2995060102 CONTROL CABLE CESSNA182 182M 2072728CE CONT O470 O470R 17026SO PROPELLER BROKEN G K NONE O OTHER ININSP/MAINT 1 CE01713983695 18259607 2000529R PILOT COMPLAINED THAT THE PROPELLER CONTROL WAS HARD TO MOVE. WHEN TECHNICIAN INVESTIGATED, THE CONTROL CABLE BROKE AND CAME OFF IN TECHNICIAN`S HAND. REMOVED AND REPLACED CONTROL WITH NEW PART. 1H71 3O3 ONT3A13 E273 20020125001312002012500131EU 2002 1 25 2002FA0000026 120011203G243523091004 STARTER GEN ISRAELGALAXYGALAXY 4500307EU ENGINE FAILED G O OTHER O OTHER NRNOT REPORTED 1 GL2535BP 016 STARTER GEN FAILED. 2L72 4F RTA53NM 20020125001322002012500132EU 2002 1 25 2002FA0000027 120011214G4930FB9682 FUEL BOWL HWKSLYDH125 HS125600A 4230158EU GARRTTTFE731TFE731* 01518WP APU CONTAMINATED D K NONE O OTHER ININSP/MAINT 1 NE05800NM 256027 DURING SCHEDULED INSPECTION AND FILTER CHANGE, EXCESSIVE CONTAMINATION FOUND IN FILTER BOWL ASSEMBLY. 2L72 4J4 F A3EU E6WE 20020125001332002012500133CE 2002 1 25 2002FA0000028 120010714G281041424 FUEL CELL CESSNA414 414 2075908CE CONT O520 TSIO520* 17040SO RT WING ROTTED D K NONE O OTHER ININSP/MAINT 1 SW17127BC 4140519 RIGHT OUTBOARD WING FUEL CELL (PN 4142-4) REPLACES (PN 5026102-4). FUEL CELL IS 11 YEARS OLD. MPG, DATE 2-90. FUEL CELL CAME APART (TOTALLY ROTTEN AND BRITTLE) AT TOP OF FILLER NECK. FUEL CELL WAS MADE OF DIFFERENT MATERIAL, NOT OF THE NORMAL RUBBER. BAD TANK FOUND. 1L72 3O3 ORTA7CE E8CE 20020118000312002011800031SW 2002 1 18 2002FA0000029 120010730G6220222012104101 PITCH HORN BELL 230 230 1182149SW ALLSN 250C 250C30 03013GL MAIN ROTOR CRACKED D K NONE O OTHER ININSP/MAINT 1 NM09230LF2714 23017 CRACK FOUND ON MAIN ROTOR GRIP AT BOLT HOLE WHERE GRIP ATTACHES TO PITCH HORN. CRACK EXTENDED FROM BOLT HOLE FOR 1.5 FEET TO OUTSIDE OF GRIP. 1G72 3U3 UNCH9SW E1GL 20020125001342002012500134EU 2002 1 25 2002FA0000030 120010101G53204A53360284001 FITTING ISRAELGALAXYGALAXY 4500307EU DOOR STRUT BROKEN D K NONE O OTHER ININSP/MAINT 1 GL2583EJ 1100 009 FITTING HOLDS CABIN ENTRANCE DOOR AIR SPRING. SPRING GIVES DOOR SUPPORT DURING OPENING. DOOR SUPPORT DURING OPENING, FITTING BROKE ALLOWING DOOR WEIGHT TO HAVE TO BE SUPPORTED BY CREW. PART TT 1100 HRS 2L72 4F RTA53NM 20020125001352002012500135EU 2002 1 25 2002FA0000031 120010101G801123091004 STARTER ISRAELGALAXYGALAXY 4500307EU ENGINE FAILED D K NONE O OTHER ININSP/MAINT 1 GL2583EJ 009 STARTERS ARE FAILING WITH ONLY 200 TO 300 HOURS. 2L72 4F RTA53NM 20020125001372002012500137CE 2002 1 25 2002FA0000032 120011228G3211513210P24 BUSHING CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MLG BRACE CORRODED D K NONE O OTHER ININSP/MAINT 1 WP1398692 402B1050 L275471R BEARING PART OF BUSHING, NOT TAKING GREASE. DISASSEMBLE AND PHYSICALLY INSPECT BOTH. FOUND CORRODED 1L72 3O3 O A7CE E8CE 20020125001382002012500138SO 2002 1 25 2002FA0000035 120011214G7714598881 PICKUP PIPER PA32 PA32R301T 7103220SO LYC O540 TIO540* 41532EA ENGINE TACH MISMANUFACTURED C K NONE O OTHER ININSP/MAINT 1 WP07298AT418 3257069 L1006661A REMOVED MAGS FOR 500 HR INSPECTION, NYLON GEARS IN LT MAG DETERORATING, FROSTED APPEARANCE ON BOTH DISTRIB AND CAM GEARS. MAG HAS ELECT TACH PICK UP IN PLACE OF NORMAL MAG VENT. 1L71 3O3 O A3SO E14EA 20020125001392002012500139CE 2002 1 25 2002FA0000036 120011228G33100713247200 RHEOSTAT CESSNA172 172H 2072424CE CONT O300 O300* 17022SO CABIN BURNED D K NONE L NO TEST ININSP/MAINT 1 GL193297L 17256197 SMOKE IN COCKPIT, COMING FROM OVERHEAD. TURNED OFF RADIO LIGHT RHEOSTAT AND INSTRUMENT LIGHT RHEOSTAT. SMOKE THEN QUIT. INVESTIGATION FOUND RADIO LIGHT RHEOSTAT WAS OVERHEATING AND SMOKING. RHEOSTAT WAS REMOVED. 1H71 3O3 ONT3A12 E253 20020128000012002012800001EU 2002 1 28 2002FA0000038 120010606G2121M3348A MOTOR DYNAMICAIR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE FAN MISREPAIRED D K NONE W INADEQUATE Q C ININSP/MAINT 1 WP1569LP 217 340AO69 FAN RETURNED TO MFG FOR UPGRADE TO C209-6901) CONFIGURATION. FAN WAS DISAS AND FOUND TO BE NOT OVERHAULED PER REQUIRED MM. ARMAT AND WINDINGS NOT OF MFG DESIGN. MM DOES NOT ALLOW FOR REWINDING OF ARMAT FIELD WINDINGS, OR REPLACEMENT OF PARTS OTHER THAN LISTED. ARMAT ASSY STACK LENGTH IS TOO SHORT, THE IMPELLER IS GLUED ON, COMMUTATOR IS UNDERSIZE AND AIR GAP BETWEEN IMPELLER AND WINDINGS IS TOO SMALL. VENT HOLES IN MTR ARE ENLARGED CAUSING REDUC AIR FLOW THROUGH MTR CAUSING BRUSH HOLDERS TO OVERHEAT. END BELL IS MODI NOT TO REQMT. THREADED BAR WAS USED TO HOLD MOTOR TO HOUSING INSTEAD OF REQUIRED BOLTS. FILTER IS REWORKED (UNSERVICABLE PART). POS STUD IS LOOSE AND NOT MAKING ELECTRIC CONTACT. 2L72 4T4 TRTA52EU E8NE 20020128000032002012800003CE 2002 1 28 2002FA0000040 120011206G3230 PIVOT ASSY CESSNA182 R182 2072734CE LT MLG CRACKED D K NONE K FLUID LOSS ININSP/MAINT 1 SW15757KP R18201242 FORWARD BEARING AREA OF LEFT MAIN GEAR PIVOT WAS DETERMINED TO BE CRACKED AND LEAKING BREAK FLUID. THE PIVOT ASSEMBLY WAS REPLACED WITH A USED SERVICEABLE PIVOT ASSEMBLY OF THE SAME PART NUMBER. 1H71 3O RT3A13 20020128000042002012800004SO 2002 1 28 2002FA0000041 120010821G322040336000 DRAG LINK PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA NLG BROKEN B BX4RK NONE O OTHER ININSP/MAINT 1 NM03114SA13729 318052053 RIGHT NOSE GEAR DRAB LINK FAILED JUST FORWARD OF WHERE GEAR ACTUATOR ATTACHES. 1L72 3O3 O A20SO E14EA 20020128000052002012800005GL 2002 1 28 2002FA0000042 120011113G52106E21 HOOK ZENITH AMTR CH601 ZODIAC GL CANOPY LOCK MALFUNCTIONED D O OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 GL17324DZ18 63682 NO FLAW FOUND ON LOCK HOOK. CANOPY SEPARATED FROM FUSELAGE IN STRAIGHT AND LEVEL FLIGHT. 1L71 3O NCEXPA1L71 20020128000062002012800006EA 2002 1 28 2002FA0000043 220010418G8500 ENGINE GIPPLDGA200 GA200 EU LYC O540 O540A1D5 41532EA NACELLE FAILED C E ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION LDLANDING 1 SW15280GA451 2009825F ENGINE ACTED AS THOUGH CARBURETOR ICE WAS BEING CLEARED WITH CARBURETOR HEAT ON. LANDED UNEVENTFULLY. AT TOUCHDOWN, COULD HEAR A LOUD SQUEAK. AT ENGINE SHUT DOWN, ENGINE STOPPED AS THOUGH A BRAKE WAS APPLIED. PROP WAS DIFFICULT TO TURN BY HAND. ALUMINUM AND FERROUS METAL WAS FOUND IN OIL SCREEN, FILTER AND OIL COOLER. 1L71 3O3 ONCA00001LAE295 20020116000012002011600001NE 2002 1 16 2002FA0000044 220010707G7200 TIE ROD PWA JT8 JT8D15A 52051NE SIXTH STAGE FAILED W K NONE O OTHER ININSP/MAINT 1 EA01GCEAF 686373 CREW REPORTED HIGH VIBRATION IN CRUISE AT FL 330. GROUND RUNS CARRIED OUT AND VIBRATION CONFIRMED. ENG HEARD TO BE MAKING A METALLIC SCRAPING SOUND WHEN TURNED BACKWARDS. SIG DAMAGE WAS FOUND WHILE BORESCOPING. INSP OF 6TH STAGE REVEALED THAT REAR TIEROD HAD FAILED AND WAS STUCK IN GASPATH BETWEEN C6 BALDES AND INTERMEDIATE CASE VANES. ONE TIE ROD FAILED IN 4TH STG LAND. FRNT REMAINED IN PLACE WHILE REAR PART MOVED AFT. REAR END OF TIEROD MANAGED TO COME OUT OF TIEROD HOLE. BROKEN OFF TIEROD PART CAME OUT OF TIEROD HOLE, THEN PUNCTURED INTERM CASE WHILE TIEROD HEAD STAYED IN CONTACT WITH C6 DISK OUTER RIM. EXTENSIVE SECONDARY DAM CAUSED TO AIRFOILS DOWN STREAM OF C6 BY BROKEN OFF FRAGMENTS OF BLD LOCKS 4 F E2EA 20020128000072002012800007CE 2002 1 28 2002FA0000045 120010403G32520842102 SHIMMY DAMPENER CESSNA310 310J 2074226CE NLG DAMAGED G O OTHER O OTHER TXTAXI/GRND HDL 1 SO1563GG 4878 310J0152 PILOT MADE A HARD LEFT TURN CAUSEING DAMAGE TO THE NOSE GEAR AREA. BENT ROD ON THE SHIMMY DAMPER CAUSING INTERNAL DAMAGE TO THE COMPONENT. 1L72 3O 3A10 20020118000322002011800032SW 2002 1 18 2002FA0000048 120010804G642047LM2505 UNIVERSAL JOINT BELL 47 47G5 1181032SW ALLSN 250C 250C* GL TAIL ROTOR FAILED C LPGGK NONE O OTHER ININSP/MAINT 1 GL212251W 559 7965 CAE801089B WAS INVOLVED IN AERIAL APPLICATION, ON A SPRAY RUN PILOT NOTICED THAT HE WAS PICKING UP VIBRATION IN TAIL ROTOR CONTROL PEDALS AND CEASED SPRAY OPERATIONS. CAME IN FOR LANDING AND AT HOVER IS WHEN THE U-JOINT FAILED. HELICOPTER TURNED 180 DEGREES BEFORE LANDING. NO DAMAGE TO AIRCRAFT. PART THAT FAILED INSPECTED DAILY. LUBRICATED EVERY 10-15 HOURS. AFTER EXAMINING FAILED U-JOINT, FOUND THAT ONLY HALF OF JOINT WAS RECEIVING ANY GREASE. DONT KNOW HOW LONG THIS CONDITION OF NO GREASE WAS HAPPENING. 1G71 3O3 U 2H3 E4CE 20020128000092002012800009NM 2002 1 28 2002FA0000049 120010705G3240 SHUTTLE VALVE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE MLG BRAKE MALFUNCTIONED D D RETURN TO BLOCK A FLAME/FIRE TXTAXI/GRND HDL 1 WP07347PH9490 65 480 RT OUTBOARD BRAKE LOCKED UP DURING TAXI AND CAUSED BRAKE FIRE. VALVE WAS PLACED ON TEST STAND AND REPEATEDLY TESTED VIGOROUSLY FOR 50 MINUTES PER OEMS ATP. NO PROBLEMS WERE NOTED. VALVE WAS THEN TORN DOWN AND INSPECTED. ONLY IRREGULARITY FOUND WAS LOOSE SCREEN IN FILTER FITTING ON INLET PORT. THIS COULD HAVE CAUSED PROBLEM ON OUTLET PORT. IT IS INCONCLUSIVE AS TO THIS VALVE CAUSING THE LOCKUP, BUT FILTER WAS REPLACED AND ONCE AGAIN VALVE TESTED GOOD. ALL FILTERS ON ALL VALVES NEED TO BE VERY THOROUGHLY INSPECTED. 2H72 4T4 TRTA13NM E20NE 20020128000102002012800010SO 2002 1 28 2002FA0000051 120011031G55205161802 BALANCE WEIGHT PIPER PA31T PA31T1 7103126SO ELEVATOR CRACKED D K NONE O OTHER ININSP/MAINT 1 NM09824VA4825 31T8104039 DURING INSPECTION, FOUND RIGHT ELEVATOR BALANCE WEIGHT HAD A CRACK IN TO LEAD WEIGHT BEHIND THE REAR MOUNTING BOLT. WITH WEIGHT REMOVED THE CRACK COULD BE EXPANDED BY HAND. (K) 1L72 3T A8EA 20020128000112002012800011EA 2002 1 28 2002FA0000052 220011230G7322CF30766 FLOAT MARVELSCHEBX CESSNA150 152 2071835CE LYC O235 O235* 41505EA CARBURETOR FAILED G O OTHER YJ ENGINE STOPPAGE WARNING INDICATION LDLANDING 1 NE0365463 CR15647 15281566 ON LANDING THE ENGINE QUIT. FUEL WAS OBSERVED LEAKING FROM THE AIRCRAFT. DURING DISASSEMBLY OF THE CARBURETOR IT WAS NOTED BOTH FLOATS WERE FILLED WITH FUEL CAUSING FUEL TO POUR THRU THE VENT. THE MANUFACTURE DATE OF THE FLOAT WAS 4/92. 1H71 3O3 ONT3A19 E223 20020128000122002012800012CE 2002 1 28 2002FA0000053 120010122G561010138402522 WINDSHIELD BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE COCKPIT CRACKED D K NONE O OTHER ININSP/MAINT 1 NM02200WB140 FA5 WINDSHIELD DEVELOPED CRACK IN OUTER PLY AT LOWER CENTER CORNER, CRACKING APPEARED CIRCUMFRONTIAL AT APPROXIMATELY 5 FEET 6 INCHES. WINDSHIELD WAS INSTALLED WITH MFG KIN NR 101-5041-1S. 2L72 4T4 T A24CE E4EA 20020128000152002012800015CE 2002 1 28 2002FA0000056 120010109G2750 PIN CESSNA501 501 2076603CE PWA JT15 JT15D1 52060NE TE FLAP GEARBOX SHEARED B BGSRK NONE O OTHER ININSP/MAINT 1 EA21597CS 5010293 THE SHEAR PIN CONNECTING THE FLAP DRIVE MOTOR TO THE FLAP GEARBOX SHEARED OFF AS THE CREW ATTEMPTED TO POSITION FLAPS TO 2ND POSITION. AFTER INVESTIGATION, THE FLAP GEAR BOX WAS DETERMNED TO BE DEFECTIVE. 1L72 4F4 F A27CE E1NE 20020118000192002011800019EU 2002 1 18 2002FA0000067 120011022G78100292808700 EXHAUST STACK SNIAS 350 AS350BA 8680817EU ENGINE CRACKED A O OTHER O OTHER NRNOT REPORTED 1 WP19270SH958 1864 ENGINE EXHAUST IS CRACKED. INSTALLED SERVICEABLE EXHAUST STACK. (M) 1G71 3U NCH9EU 20020118000202002011800020EU 2002 1 18 2002FA0000068 120011018G6410350A33215300 BEARING SNIAS 350 AS350* EU TAIL ROTOR CUT A O OTHER O OTHER NRNOT REPORTED 1 WP19115SH640 3141 BEARING HAS DEEP CUT, DELAMINATION. REPLACED WITH NEW BEARING. (M) 1G71 3U H9EU 20020118000212002011800021 2002 1 18 2002FA0000069 420011017G3422RCA15BR1 GYRO SNIAS 350 AS350BA 8680817EU COCKPIT INOPERATIVE A O OTHER O OTHER NRNOT REPORTED 1 WP19230SH11 2337 DIRECTIONAL GYRO INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. (M) 1G71 3U NCH9EU 20020118000222002011800022 2002 1 18 2002FA0000070 420011011G3422RCA15BK1 GYRO SNIAS 350 AS350BA 8680817EU COCKPIT PRECESSES A O OTHER O OTHER NRNOT REPORTED 1 WP19230SH319 2337 DIRECTIONAL GYRO PRECESSES CONTINUOUSLY. REPLACED WITH SERVICABLE UNIT. (M) 1G71 3U NCH9EU 20020118000232002011800023EU 2002 1 18 2002FA0000071 120011016G3110704A47270101 INDICATOR SNIAS 350 AS350BA 8680817EU COCKPIT INTERMITTENT A O OTHER O OTHER NRNOT REPORTED 1 WP1937SH 1221 2300 FUEL PSI READING INTERMITTENT. FURTHER TROUBLESHOOTING FOUND BAD GROUND WIRE, THIS UNIT IS TO BE RESTOCKED. INSTALLED SERVICEABLE INSTRUMENT CLUSTER. (M) 1G71 3U NCH9EU 20020118000242002011800024SW 2002 1 18 2002FA0000072 120010828G6510407340339101 BEARING BELL 407 407 1182206SW MAIN ROTOR WORN B O OTHER O OTHER NRNOT REPORTED 1 SW03404AL 53479 BEARING SHOWING SIGNS OF WEAR AND BEGINNING SIGNS OF OVERTEMP. SCRAPPED BEARING. (M) 1G71 3U O H2SW 20020118000252002011800025NE 2002 1 18 2002FA0000073 220010807G725023053299 TURBINE WHEEL SKRSKYS76 S76 8143010NE ALLSN 250C 250C40B 03032NE ENGINE CORRODED B O OTHER O OTHER NRNOT REPORTED 1 SW03707AL1110 760189 TURBINE CAME IN FOR SHOP VISIT FOR LOW POWER. BEGAN DISASSEMBLY OF TURBINE, REMOVED OUTER COMBUSTION CASE AND FOUND SULFIDATION ON 1ST STAGE WHEEL. HAD ONE BLADE MISSING AND SEVERAL BROKEN BLADES. THIS TURBINE HAD A ROLLS ROYCE LINER. HAVE WHEELS TESTED FOR PROPER COATING. (M) 1G72 3U3 U H1NE E1GL 20020118000262002011800026SW 2002 1 18 2002FA0000074 120011002G5330206010200133 SKIN BELL 206 206B 1181511SW FUSELAGE CORRODED B K NONE O OTHER ININSP/MAINT 1 SW035743B3310 3056 DISCOVERED DURING ROUTINE AIRFRAME INSPECTION, LOWER SKIN CORRODED AND SEPARATED BENEATH OUTBOARD GRIP FINGER DOUBLER. (M) 1G71 3U H2SW 20020118000272002011800027GL 2002 1 18 2002FA0000075 220010822G72506895801 TURBINE WHEEL BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL ENGINE CORRODED B O OTHER O OTHER NRNOT REPORTED 1 SW032025G987 45690 WHEN TURBINE CAME IN FOR NR 3 AND NR 4 WHEEL CHANGE AND VISUAL INSPECTION ON TURBINE HOT END. NR 1 WHEEL SHOWED EARLY ATTACH OF SULFIDATION. HAVE WHEEL TESTED FOR PROPER COATING. (M) 1G71 3U3 U H2SW E1GL 20020118000282002011800028EU 2002 1 18 2002FA0000076 120010808G63204649010006 CASE UROCOPEC135 EC135T1 5620026EU M/R GEARBOX DAMAGED A O OTHER O OTHER NRNOT REPORTED 1 EA03511ME547 0143 FOUND HOLE IN MAIN GEARBOX CASING. (M) 1G72 3U H88EU 20020128000172002012800017 2002 1 28 2002FA0000078 420010918G3197PQ876SW RING CESSNA172 172M 2072418CE LYC O320 O320* 41508EA WIRE BURNED D K NONE O OTHER ININSP/MAINT 1 GL131368U317 17267039 PART WAS INSTALLED AROUND TACH AND CONNECTED TO REOSTATE FOR THE INSTRUMENT LIGHTS. IT SHORTED OUT THE SYSTEM AND BURNED OUT REOSTATE-S2091-5 AND POWER TRANSISTER 2N3055. THIS CAUSED NO INSTRUMENT LIGHTS IN AIRCRAFT. OWNER NOTICED NO LIGHTS AND NOTIFIED TECHNICIAN. TROUBLESHOOTING THE SYSTEM TECH FOUND THAT WIRES ON TOP OF RING WAS TOUCHING ONE ANOTHER, CAUSING A DIRECT SHORT. 1H71 3O3 ONT3A12 E274 20020128000182002012800018EA 2002 1 28 2002FA0000079 220010930G7414M3635 IMPULSE COUPLINGSLICK PIPER PA25 PA25235 7102504SO LYC O540 O540B2C5 41532EA MAGNETO SEPARATED D E ENGINE SHUTDOWN DK INFLIGHT SEPARATION FLUID LOSS TXTAXI/GRND HDL 1 EA338903L230 255364 L121180 DURING GROUND RUN, OPERATOR NOTED A LOUD BANG AND SUDDEN OIL LEAKAGE. AFTER SHUT DOWN FOUND THAT LT MAGNETO CAME OFF THE ACCESSORY HOUSING, CAUSING OIL LEAK. BANG WAS CAUSED BY MAG HOUSING WHICH CAME APART AT UPPER ATTACHMENT AREA (ATACHMENT LUG). 1L71 3O3 O 2A10 E295 20020128000192002012800019WP 2002 1 28 2002FA0000083 120011016G792253E22144 VERNATHERM ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA OIL COOLER STUCK D O OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 NE058353K797 0348 L2507840A HIGH OIL TEMPERATURES, AT RED LINE 245 DEGREES, VERIFIED BY DECREASE IN OIL PRESSURE. FOUND VALVE STUCK, NOT EXTENDING. REMOVED AND REPLACED WITH NEW PART. OPS CHECKED GOOD. 1G71 3O3 O H11NM E295 20020128000222002012800022CE 2002 1 28 2002FA0000088 120011211G521007110271 HANDLE CESSNA182 182D 2072710CE CONT O470 O470* 17026SO CREW DOOR STRIPPED D K NONE O OTHER ININSP/MAINT 1 WP019109X 18253509 WHILE INVESTIGATING A COMPLAINT OF A DEFECTIVE DOOR LATCH IT WAS DISCOVERED THAT THE INTERNAL SPLINES OF THE DOOR HANDLE WERE STRIPPED. 1H71 3O3 ONT3A13 E273 20020128000232002012800023CE 2002 1 28 2002FA0000089 120011119G5260 STRUT CESSNA310 310Q 2074242CE CONT O470 IO470* 17026SO AIRSTAIR BROKEN D K NONE O OTHER ININSP/MAINT 1 NE028TC 310Q0264 MAINTENANCE PERSONNEL ATTEMPTED TO BOARD AIRCRAFT WHEN MOUNTING STEP STRUT ASSEMBLY BROKE AWAY. WELD ASSEMBLY (PN 0811946-23) FAILED COMPLETELY AT UPPER STEP. INDICATIONS OF A PRE EXISTING CRACK AROUND ONE THIRD OF THE CIRCUMFERENCE OF THE TUBE. NO SIGNS OF RUST BLEED THROUGH AT THE EXTERIOR PAINT. STEP MOUNTING SCREW SPACERS MISSING AT UPPER STEP. 1L72 3O3 O 3A10 E1CE 20020128000312002012800031NM 2002 1 28 2002FA0000091 120010627G2612088131007 SWITCH BOEING737 737* NM FIRE DETECTION SHORTED B O OTHER O OTHER NRNOT REPORTED 1 SW99XAAEX6 32774 SWITCHES SHORTED INTERNALLY. SHOULD RETURN TO N/O CONDITION. LOOKS LIKE MICROSWITCH FAILED INTERNALLY IN ASSY. REMOVED AND REPLACED SWITCHES, RETESTED NO MALFUNCTION OR DEFECTS NOTED. FIRE BELL CUTOUT SWITCHES AND SYSTEM OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 20020128000332002012800033CE 2002 1 28 2002FA0000092 120011219G2730676033215 TIE ROD CESSNA750 750 2076810CE RT ELEVATOR STIFF C K NONE O OTHER ININSP/MAINT 1 NM09551AM262 262 7500155 DURING INSPECTION AND PERFORMANCE, BEARING ROD END LUBRICATION, P/N 676033215 TIE ROD, INTERCONNECTING THE TWO OUTBOARD ELEVATOR BELLCRANKS, WAS FOUND TIGHT AND NOT ABLE TO ROTATE SLIGHTLY ABOUT ITS LONGITUDINAL AXIS. IT WAS DISCOVERED THAT THE ROD ENDS, WHICH ARE RIVETED TO THE MAIN TUBE AND NOT ADJUSTABLE, WERE MISALIGNED WITH EACH OTHER---NOT IN THE SAME PLANE. WHEN ATTACHED TO THE BELLCRANKS, THE ROD ENDS WERE PINCHED AGAINST THE BELLCRANK EARS INSTEAD OF JUST THE SPHERICAL BEARING. NO DAMAGE WAS NOTED ON THE BELLCRANK EARS, HOWEVER, FUTURE PROBLEMS MIGHT ARISE AS THE TIE ROD AND OTHER PUSHROD AND BUNGEE ROD ENDS IN THIS SYSTEM ARE SUBJECT TO ROD END BEARING CORROSION. TIE ROD WAS REPLACED WITH NEW PART W2L72 4J RTT00007WI 20020124000332002012400033GL 2002 1 24 2002FA0000095 120011210G32133525151004 FORK AMTR GLASARGLASAIRIISTD05602E5GL MLG BROKEN G O OTHER O OTHER LDLANDING 1 GL07225S 918 40 DURING LANDING THE AIRCRAFT VEERED OFF TO THE RIGHT SIDE OF THE RUNWAY. AN INSPECTION REVELED A RIGHT HALF FORK WAS BROKEN. THE WHEEL ATTACHES TO THIS HALF FORK WHICH ATTACHES TO THE MAIN STRUT. PER A GLASAIR REPRESENATIVE, MFG. OF THE GLASAIR KITS FOR AMATUERBUILDERS, THIS PART IS NOW MADE OF STEEL. THE CAST ALUMINUM HALF FORK, SUCH AS THE BROKEN PART, WAS REPLACED BY THE STEEL HALF FORK ABOUT 8-10 YEARS AGO. AN UPGRADE WAS MADE AVAILABLE TO ALL THE PREVIOUS KITS FROM GLASAIR. 1L71 3O RTEXPA1L71 20020128000372002012800037EA 2002 1 28 2002FA0000096 220011210G8550 ENGINE AMRGENAG5B AG5B 3990100SO LYC O360 O360A4K 41514EA SNSNCH76E 76EM8 EA NACELLE LEAKING F O OTHER K FLUID LOSS NRNOT REPORTED 1 EA09999TE68 10201 L3776336A ENGINE DEVELOPED OIL LEAK AT THE TOP OF THE CASE NEAR THE ACCESSORY CASE. LEAK BEGAN DURING INITIAL ENGINE RUN. LEAK IS APPX 1/8 QT PER 6 HRS. LEAK COULD NOT BE FIXED WITHOUT REMOVING ENGINE. 1L71 3O3 ONT1L71 E286 5 NP4EA 20020124000382002012400038SO 2002 1 24 2002FA0000100 220010921G7414K3823 DISTRIBUTOR SLICK 6310 CESSNA206 U206G 2073356CE CONT O550 IO550F 17042SO MAGNETO BURNED D D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW99PK-MP9 00111980 U20606987 MAGNETO FAILED - WOULD NOT RUN AT ALL. THE DISTRIBUTOR GEAR SUPPORT WAS FOUND TO BE BADLY BURNED FROM SPARKS GOING FROM THE THE SHAFT TO GROUND ON THE M3485 BEARING CAP BY ARCING ACROSS THE SUPPORT. SUPPORT IS BADLY MELTED. M3215 CARBON BRUSH IS BURNED ALSO. DISTRIBUTOR BLOCK AND GEAR ARE COATED WITH A WHITE DEPOSIT MATERIAL WHICH IS ALSO SEEN SPATTERED INSIDE THE MAGNETO HOUSING AND ON THE COIL. 1H71 3O3 O A4CE E3SO 20020124000392002012400039SO 2002 1 24 2002FA0000101 220010925G7414K3823 DISTRIBUTOR SLICK 6310 CESSNA206 U206G 2073356CE CONT O550 IO550F 17042SO MAGNETO BURNED D D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW99PKMPT12 00111983 U20606987 MAGNETO FAILED - WOULD NOT RUN AT ALL. THE DISTRIBUTOR GEAR SUPPORT WAS FOUND TO BE BADLY BURNED SHOWING DEEP TRACKING FROM SPARKS GOING FROM THE SHAFT TO GROUND ON THE M3485 BEARING CAP BY ARCING ACROSS THE SUPPORT. SUPPORT HAS A DEEP TRACK BURNED ACROSS IT. DISTRIBUTOR BLOCK AND GEAR ARE COATED WITH A WHITE DEPOSIT MATERIAL WHICH IS ALSO SEEN SPATTERED INSIDE THE MAGNETO HOUSING AND ON THE COIL. MAGNETO WAS SUPPLIED AS PART OF A FACTORY REBUILT ENGINE. 1H71 3O3 O A4CE E3SO 20020124000402002012400040 2002 1 24 2002FA0000103 420010809G2564R0097104 LIFE RAFT CABIN DAMAGED B O OTHER L NO TEST NRNOT REPORTED 1 SW03 DURING 1ST 8 MONTH INSPECTION, LIFE RAFT HAS TOO MUCH POROSITY. RECOMMENDATION BETTER COATING OF FABRIC AND MORE INTENSIVE INSPECTION AFTER MANUFACTURING OF RAFT. (M) 20020124000412002012400041SO 2002 1 24 2002FA0000105 220010810G85506420B5415R HOUSING CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO SCAV PUMP FRACTURED D E ENGINE SHUTDOWN K FLUID LOSS APAPPROACH 1 SW99121PB1482 402C0507 ON FINAL APPROACH, CREW NOTICED OIL LEAKING FROM LEFT ENGINE COWL. OIL PRESSURE AND TEMPERATURE WERE INDICATING NORMAL. CREW SHUT DOWN LEFT ENGINE AS A PRECAUTION AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SCAVENGE PUMP HOUSING FRACTURED AND LEAKING. TEAR DOWN REVEALED SCAVENGE PUMP DRIVEN GEAR FAILED, CAUSING THE HOUSING TO CRACK. MAINTENANCE REMOVED AND REPLACED STARTER ADAPER OIL FILER AND CHANGED OIL. AIRCRAFT RETURNED TO SERVICE. (M) 1L72 3O3 O A7CE E8CE 20020124000422002012400042EA 2002 1 24 2002FA0000106 220010801G7414 BEARING AMRGENAG5B AG5B 3990100SO LYC O360 VO360* 41514EA MAGNETO FAILED B O OTHER O OTHER NRNOT REPORTED 1 SW991194T 10083 MAGNETO FORWARD BEARING SEIZED BENDING SHAFT AND DRIVE GEAR ROAD OVER ENGINE ACCESSORY DRIVE GEAR CHIPPING DRIVE GEAR AND PUTTING ENGINE OUT OF TIME SHUTTING ENGINE DOWN WHEN TAXIING AND ENGINE WOULD NOT RESTART. (M) 1L71 3O3 ONT1L71 1E1 20020124000442002012400044CE 2002 1 24 2002FA0000107 120011212G3710H67402A3 SHUTTLE VALVE CESSNA401 401 207590CCE VACUUM SYSTEM FAILED B ED ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW993264Q1577 4010064 AFTER STARTING THE RT ENGINE & THE LT ENGINE IS OFF. THE RT VACUUM SYSTEM PULLED BOTH LT & RT ORANGE INDICATOR BULLETS ON THE VACUUM GAUGE INDICATING THAT THE LT VACUUM SYSTEM IS WORKING, BUT THE LT ENGINE IS SHUT DOWN. CAUSE: THE LT SHUTTLE/CHECK VALVE FOR THE WING DEICE BOOTS STUCK OPEN ALLOWING THE RT VACUUM PUMP TO SUCK DOWN THE LT SYSTEM THROUGH THE LT VACUUM PUMP GIVING A FALSE OPERATIONAL INDICATION. 1L72 3O A7CE 20020124000492002012400049SO 2002 1 24 2002FA0000109 220011207G7414K3823 DISTRIBUTOR SLICK 6310 CESSNA206 U206F 2073333CE CONT O550 IO550F 17042SO MAGNETO BURNED C D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW99PKMPR2 00111980 U20603398 284921 MAGNETO HAD FAILED 9.3 HOURS AFTER BEING SUPPLIED AS A PART OF A FACTORY REBUILT ENGINE. IT WAS DISASSEMBLED AND THE DISTRIBUTOR, COIL, CAPACITOR AND BREAKER WERE REPLACED. MAGNETO WAS CHECKED OK. 2.5 HOURS AFTER THIS REPAIR THE MAGNETO FAILED AGAIN. THE DISTRIBUTOR GEAR SUPPORT WAS FOUND TO BE BADLY BURNED SHOWING DEEP TRACKING FROM APARKS GOING FROM THE SHAFT TO GROUND ON THE M3485 BEARING CAP BY ARCING ACROSS THE SUPPORT. SUPPORT HAS A DEEP TRACK BURNED ACROSS IT AND IS PARTLY BURNED AWAY. 1H71 3O3 O A4CE E3SO 20020124000502002012400050SO 2002 1 24 2002FA0000110 220011207G7414K3823 DISTRIBUTOR SLICK 6230 CESSNA206 TU206G 2073357CE CONT O520 TSIO520M 17040SO MAGNETO BURNED D D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW99PKMPY449 00091743 U20606904 818183R MAGNETO WAS SUPPLIED AS PART OF A TCM FACTORY REBUILT ENGINE. IT FAILED AND UPON INSPECTION IT WAS DISCOVERED THAT THE DISTRIBUTOR GEAR SUPPORT WAS BADLY BURNED BY SPARKS GOING FROM THE COIL TERMINAL TO GROUND ON THE M3485 BEARING CAP BY ARCING ACROSS THE SHELF OF THE SUPPORT. SUPPORT HAS A DEEP TRACK BURNED ACROSS IT. 1H71 3O3 O A4CE E8CE 20020124000522002012400052SO 2002 1 24 2002FA0000111 120011221G32307954302 BOLT PIPER PA28 PA28151 7102805SO DRAG LINK FAILED D A UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SW99431254395 6 287415430 JUST AFTER TAKEOFF, THE GREASE BOLT (P/N 79543-02) FAILED AND ALLOWED THE UPPER AND LOWER TORQUE LINKS TO SEPARATE. THIS ALLOWED THE STUB AXLE, OLEO TUBE, AND RIGHT WHEEL AND BRAKE ASSEMBLY TO FALL OFF THE AIRCRAFT. THE BRAKE LINE BROKE ALLOWING EVERYTHING TO FALL FREE. THE ASSEMBLY WAS RECOVERED AND THE TORQUE LINKS FOUND TO BE INTACT. THE GREASE BOLT WAS NOT RECOVERED, SO THE EXACT LOCATION OF THE FAILURE IS UNKNOWN. THIS AIRCRAFT HAS BEEN USED FOR TRAINING EXTENSIVELY, SO STRESSES ON THE GEAR ARE HIGHER THAN IN NORMAL USE. ANY SIDE LOAD ON THE GEAR STRESSES THE GREASE BOLT, SO PERHAPS A LANDING WHILE YAWED CRACKED THE BOLT, CAUSING A FAILURE ON THE NEXT FLIGHT. 1L71 3O 2A13 20020124000622002012400062CE 2002 1 24 2002FA0000112 120011227G3340W31X100010 SWITCH CESSNA172 172S 2072439CE INSTRUMENT PANELFAILED D K NONE L NO TEST ININSP/MAINT 1 NM03 1429 172S8135 PRE-RUN FOR MAINTENANCE FOUND TAXI LIGHT ON WITH SWITCH IN THE OFF POSITION. MAINTENANCE FOUND TAXI LIGHT SWITCH FAILED IN THE ON POSITION. REPLACED SWITCH AND FUNCTIONAL CHECKED SAT. 1H71 3O NT3A12 20020124000632002012400063EU 2002 1 24 2002FA0000113 120011108G2613 OVERHEAT LOOP BRAERODH125 BAE125800A 1500285EU AFT E/E BAY FAILED D K NONE L NO TEST ININSP/MAINT 1 GL0712F 258182 DURING A 5 YEAR FUNCTIONAL TEST OF THE REAR EQUIPMENT BAY OVERHEAT DETECT SYSTEM, THE FUNCTIONAL TEST FAILED. FOUND FUSE F36(3AMP) ON THE ZK PANEL BLOWN. THE FLIGHT CREW HAS NO WAY OF KNOWING THEIR OVERHEAT DETECT SYSTEM IS INOP, BECAUSE THE COCKPIT TEST CIRCUIT, WHICH TESTED OK, IS NOT WIRED THROUGH THIS FUSE. THIS COULD BE A POTENTIALLY DANGEROUS SITUATION. 2L72 4F RTA3EU 20020124000822002012400082CE 2002 1 24 2002FA0000124 120011219G2120 ODOR RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP COCKPIT DETECTED B E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP07833QS 258433 107407 DURING CLIMB AT FL240, PILOTS NOTICED "BURNING" SMELL FOLLOWED BY A HUMMING SOUND FROM THE LEFT-HAND SIDE OF AIRCRAFT. PILOT ELECTED TO SHUTDOWN ENGINE. 2L72 4F4 FRTA3EU E6WE 20020128000462002012800046EU 2002 1 28 2002FA0000136 120010116G2435150SG10095 BRUSHES UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE STARTER GEN WORN C K NONE O OTHER ININSP/MAINT 1 WP25255SD200 1618 1102 34117 DEFECT FOUND DURING SCHEDULED MAINTENANCE, 100 HOUR INSPECTION. LARGE QUANTITY OF CARBON DUST NOTICED AROUND STARTER GENERATOR. FURTHER INSPECTION FOUND BRUSHES WORN BEYOND LIMITS. 1G72 3U3 UNCR0001RD E34NE 20020130000082002013000008SW 2002 1 30 2002FA0000143 120011231G5302206033004045 SUPPORT BELL 206 206L 1181522SW TAILBOOM MISMANUFACTURED B ALGRK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 TRIED TO PUT SUPPORT IN FIXTURE TO LOCATE TO TAILBOOM. RADIUS BEND IS TOO WIDE. BETTER QUALITY CONTROL AT MFG. 1G71 3U H2SW 20020130000092002013000009SW 2002 1 30 2002FA0000144 120011231G5302206033004045 SUPPORT BELL 206 206L 1181522SW TAILBOOM MISMANUFACTURED C ALGRK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 TRIED TO PUT SUPPORT IN FIXTURE TO LOCATE TO TAILBOOM. RADIUS BEND IS TOO WIDE. BETTER QUALITY CONTROL AT MFG. 1G71 3U H2SW 20020130000102002013000010SW 2002 1 30 2002FA0000145 120011231G5302206033004045 SUPPORT BELL 206 206L 1181522SW TAILBOOM MISMANUFACTURED C ALGRO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03 TRIED TO PUT SUPPORT IN FIXTURE TO LOCATE TO TAILBOOM. RADIUS BEND IS TOO WIDE. BETER QUALITY CONTROL AT MFG. 1G71 3U H2SW 20020130000932002013000093NM 2002 1 30 2002FA0000149 120011218G5346 SUPPORT PIPER PA60 PA60601 7106010NM MLG CRACKED D K NONE O OTHER ININSP/MAINT 1 WP01700US14000 610652796214 DURING ROUTINE MAINTENANCE TO REPLACE MAIN TIRES, THE AIRCRAFT WAS JACKED. THE NOSE LANDING GEAR HAD EXCESSIVE MOVEMENT. THE NOSE LANDING GEAR ACTUATOR SUPPORT STRUCTURE WAS FOUND CRACKED IN NUMEROUS MEMBERS OF THE SUPPORT STRUCTURE AND CRACKED THROUGH PREVIOUS REPAIRS. 1M72 3O RTA17WE 20020130000942002013000094NM 2002 1 30 2002FA0000150 120011218G553122000000 RIB PIPER PA60 PA60601 7106010NM VERTICAL STAB CRACKED D K NONE O OTHER ININSP/MAINT 1 WP01700US 610652796214 DURING ANNUAL INSPECTION THE VERTICAL STABILIZER LOWER FORWARD RIB WAS FOUND CRACKED AT THE 90 DEGREE BEND ADJACENT TO THE FORWARD SPAR. THIS AREA NEEDS CLOSE INSPECTION. 10X MAGNIFYING GLASS SHOULD HELP. 1M72 3O RTA17WE 20020205000432002020500043SO 2002 2 5 2002FA0000154 220011231G8530641320 CYLINDER HEAD PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360EB 17025SO LT ENGINE SEPARATED B DYTREA ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SO152931L105 347970387 DURING LEVEL FLIGHT THE LEFT ENGINE STARTED RUNNING VERY ROUGH. ENGINE FEATHERED AND AIRCRAFT RETURNED TO AIRPORT. ENGINE UNCOWLED AND NR 5 CYLINDER HEAD WAS FOUND SEPARATED FROM BARREL. 1L72 3O3 O A7SO E9CE 20020312000042002031200004SO 2002 3 12 2002FA0000160 120010116G271062701123 WIRE ROPE PIPER PA32 PA32300 7103212SO PWA PT6 PT6A67B 52043NE LT AILERON WORN B UC2RK NONE O OTHER ININSP/MAINT 1 GL194145R2227 3240495 LEFT AILERON BALANCE CABLE, DURING A ROUTINE INSPECTION, THE LEFT AILERON BALANCE CABLE WAS FOUND WORN WHERE THE CABLE PASSES OVER THE CENTER PULLEY IN THE MIDDLE OF THE FUSELAGE. 1L71 3O4 T A3SO E26NE 20020312000342002031200034GL 2002 3 12 2002FA0000210 320011201G6111R10115255 BLADE HARTZLHCB3R HCB3R304 GL PROPELLER BROKEN B F3PRO OTHER O OTHER NRNOT REPORTED 1 SW15 1015 EMA1094 BLADE LOST APPROXIMATELY 11 INCHES INBOARD FROM TIP. HAD PREVIOUS KNOWN GROUND STRIKE ALL BLADES. REMOVED SUBJECT BLADES AND HUB FROM SERVICE. REPLACED WITH NEW. 2 OTHER BLADES SHOW SIGNS OF STRAIGHTING 02-01-2002 5 CP28EA 20020312000362002031200036CE 2002 3 12 2002FA0000212 120011226G57510322709 BRACKET CESSNA195 195A 2073110CE JACOBSR755 L4* 35003EA AILERON HINGE CORRODED D K NONE O OTHER ININSP/MAINT 1 CE03195CN 16062 R7557 BOTH BRACKETS CRACKED ALL THE WAY ACROSS BEARING BOSS, SEVERELY CORRODED AND MOUNTING LEG OF ONE BRACKET BROKEN OFF. THE PROBLEM WITH THESE BRACKETS IS THE HIGHLY REAACTIVE MAGNESIUM WHICH THEY ARE MADE OF. THIS IS A HIGHLY CRITICAL COMPONENET AND SHOULD BE INSPECTED CLOSELY OR REPLACED. 1H71 3R3 R A790 TC121 20020312000372002031200037CE 2002 3 12 2002FA0000213 120011226G575103227091 BRACKET CESSNA195 195A 2073110CE JACOBSR755 L4* 35003EA AILERON HINGE CRACKED D K NONE O OTHER ININSP/MAINT 1 CE03195CN 16062 R7557 BOTH BRACKETS CRACKED ALL THE WAY ACROSS BEARING BOSS, SEVERLY CORRODED AND MOUNTING LEG OF ONE BRACKET BROKEN OFF. THE PROBLEM WITH THESE BRACKETS IS THE HIGHLY REACTIVE MAGNESIUM WHICH THEY ARE MADE OF. THIS IS A HIGHLY CRITICAL COMPONENT AND SHOULD BE INSPECTED CLOSELY OR REPLACED. 1H71 3R3 R A790 TC121 20020312000452002031200045EA 2002 3 12 2002FA0000221 220010125G8530LS32000WA21P CYLINDER PIPER PA18 PA18150 7101828SO LYC O320 O320* 41508EA ENGINE CRACKED B CY4RK NONE O OTHER ININSP/MAINT 1 AL037477L665 187509060 L4155427A ENGINE INSTALLED IN FEBRUARY 1997. AT APPROXIMATELY 665 HOURS, TWO CYLINDERS WERE CRACKED THROUGH THE FINS OUTSIDE THE EXHAUST PORT, ADJACENT TOTHE EXHAUSE SEAT. 1H71 3O3 O 1A2 E274 20020312000532002031200053CE 2002 3 12 2002FA0000229 120010401G322235825005 BOLT BEECH 35 N35 1151528CE CONT O470 IO470* 17026SO NLG BENT D K NONE O OTHER ININSP/MAINT 1 SW011228Z5040 D6688 DURING ANNUAL INSPECTION, CHECKING NOSE GEAR BOLT. BOLT WAS BENT. 1L71 3O3 O 3A15 E1CE 20020312000552002031200055CE 2002 3 12 2002FA0000231 120010530G5320 PLATE BBAVIA11 11AC 0191102CE CONT A65 A65* 17003SO RT SPAR DELAMINATED D K NONE O OTHER ININSP/MAINT 1 EA259540E1685 11AC1178 FWD REINFORCING PLATE ON RIGHT REAR SPAR AT STRUT ATTACH FITTING WAS FOUND DELAMINATING AND SEPARATING FROM SPAR AT BOND AREA. PROBABLE CAUSE IS ATTACK BY MOISTURE AND THIN OR POOR QUALITY WOOD SURFACE FINISH. RECOMMEND MORE PRECAUTION WHEN FINISHING WOOD STRUCTURES. PART TOTAL 1685 HOURS. 1H71 3O3 O A761 E205 20020312000562002031200056SW 2002 3 12 2002FA0000232 120010815G5720 FLANGE BBAVIA7 7ECA 21101NNSW LYC O290 O290* 41506EA WING RIB LOOSE D K NONE O OTHER ININSP/MAINT 1 SW07576791515 99974 FOUND LOOSE NAILS LESS THAN .1250 OUT ON SECOND RIB OUTBOARD OF STRUT AFT SPAR. FIRST AND SECOND RIB INBOARD OF STRUT AND FIRST RIB OUTBOARD OF STRUT AND FRONT SPAR ALL ON RIGHT WING. LEFT WING, FOUND LOOSE NAILS MORE THAN .1250 OR MISSING ON 1ST AND 2ND RIB OUTBOARD OF STRUT ON FRONT SPAR. ONE NAIL MISSING ON 1ST RIB INBOARD OF STRUT ON FRONT SPAR. ONE LOOSE LESS THAN .1250 ON SECOND RIB INBOARD OF STRUT ON FRONT SPAR. NO CRACKS FOUND IN EITHER WING. 1H71 3O3 O A759 E229 20020225000162002022500016CE 2002 2 25 2002FA0000233 120010828G2530 DRAIN VALVE RKWELLNA265 NA26565 7630107CE GARRTTTFE731TFE7313R1D 01518WP GALLEY CRACKED C O OTHER KF FLUID LOSS FLT CONT AFFECTED CRCRUISE 1 GL0745H 7367 4652 AIL TRIM LIGHT ILLUM DURING CRUISE FLIGHT. PILOT ATTEMPTED TO FREE FROZEN CONTROLS BY SLAMMING CONTROL WHEEL TO LEFT. CONTROLS WERE FREE BUT BINDING. CONTROLS FROZE WHEN PIC SLAMMED CONTROL WHEEL LEFT, CONTROL WHEEL STUCK IN LEFT POSITION. CAUSING AN CONTINUOUS TURN OF A/C. DIVERTED TO ENROUTE AIRPORT. AT LOW ALTITUDE CONTROLS WARMED UP AND AILERONS WERE RELEASED. MECHANIC LOOKED AT A/C AND NO PROBLEM NOTED WITH CONTROLS. TRIP WAS CONTINUED WITH NO PROBLEMS. UPON RETURN TO HOME BASE A/C WAS REINSPECTED. A CRACKED DRAIN FITTING IN THE GALLEY WAS ALLOWING WATER FROM ICE BIN DRAIN TO LEAK INTO AP SERVO AND FREEZE. FITTING WAS REPLACED. NO PROBLEMS NOTED SINCE FITTING REPLACED. 2L72 4J4 F A2WE E6WE 20020312000582002031200058CE 2002 3 12 2002FA0000235 120010925G57115271 SPAR BBAVIA7 7KCAB 21101P3CE LYC O320 IO320* 41508EA WING CRACKED D K NONE O OTHER ININSP/MAINT 1 SW098615V2230 50475 WING MAIN SPAR, TOP OF SPAR OUTBOARD OF STRUT FITTING. 1H71 3O3 O A759 1E12 20020312000592002031200059SW 2002 3 12 2002FA0000236 120011017G57115271 SPAR BBAVIA7 7GCBC 1220601SW LYC O320 O320* 41508EA WING CRACKED D K NONE O OTHER ININSP/MAINT 1 NM038807 1632 47373 FOUND A CRACK AT THE SPAR BUTT ON THE RIGHT FORWARD SPAR WHILE COMPLYING WITH AD. THE CRACK WAS CLOSE TO THE WING ATTACH FITTING WHICH LIMITED THE ABILITY TO FULLY INSPECT THE CRACK WITHOUT MAJOR DISASSEMBLY. A PIECE OF .020 INCH SAFETY WIRE WAS ABLE TO GO INTO THE CRACK .5000 INCH. ( A FEELER GUAGE COULD NOT BE USED DUE TO THE LOCATION IN REFERENCE TOTHE ATTACHMENT BARCKET). THE CRACK APPEARED TO START FROM JUST BELOW THE WING ATTACHMENT BOLT AND GO TOWARD THE LOWER ATTACHMENT BOLT. 1H71 3O3 ONCA759 E274 20020312000602002031200060SW 2002 3 12 2002FA0000237 120010813G1400 FASTENER BBAVIA7 7GCBC 1220601SW LYC O320 O320* 41508EA RT WING LOOSE D K NONE O OTHER ININSP/MAINT 1 EA2538WK 3617 113379 RIGHT WING: 16 LOOSE NAILS, 3 VERY LOOSE, 1 MISSING LEFT WING: 9 LOOSE NAILS, 0 VERY LOOSE, 0 MISSING. 1H71 3O3 ONCA759 E274 20020312000612002031200061SW 2002 3 12 2002FA0000238 120010507G57115263 SPAR BBAVIA7 7GCAA 21101N8SW LYC O320 O320A2D 41508EA WING CRACKED D VE6RK NONE O OTHER ININSP/MAINT 1 CE035038A 37679 L4862927A INSPECTED AIRCRAFT AS PER AD, FOUND LEFT AFT SPAR HAS COMPRESSION CRACK AT OUTBOARD END OF DOUBLER PLATES FOR STRUT ATTACH FITTING. 1H71 3O3 O A759 E274 20020312000622002031200062SW 2002 3 12 2002FA0000239 120010627G57115262 SPAR BBAVIA7 7ECA 21101NNSW LYC O235 O235* 41505EA WINGS CRACKED D K NONE O OTHER ININSP/MAINT 1 WP252763G1762 459 DURING ANNUAL INSPECTION, WING SPAR INSPECTION IAW AD., FOUND LONGITUDINAL CRACKS IN THE AREA OF WING STRUT ATTACH POINTS. RIGHT FORWARD SPAR LONGITUDINAL CRACK OBSERVED FROM MISSING CENTER RIB NAIL, INBOARD FROM THE STRUT ATTACH DOUBLER APPROXIMATELY 2 INCH LONG, ANOTHER OUTBOARD FROM STRUT ATTACH DOUBLER UPPER BOLT HOLE APPROXIMATELY 3 INCHES LONG. LEFT FORWARD SPAR, OUTBOARD RIB FROM STRUT ATTACH DOUBLER, A RIB NAIL WAS PREVIOUSLY REPLACED AND LONGITUDINAL CRACK IN BOTH DIRECTIONS FROM NAIL POSITION (CENTER NAIL) APPROXIMATELY 2 INCHES LONG. THIS IS WHERE THE INSPECTION WAS TERMINATED. DID NOT CUT ANY HOLES OR INSPECT THE REST OF THE SPAR DUE TO REJECTION OF THE WING SPARS. 1H71 3O3 O A759 E223 20020312000632002031200063SW 2002 3 12 2002FA0000240 120010103G5711 SPAR BBAVIA7 7AC 2110102SW CONT A65 A65* 17003SO RT WING CRACKED D K NONE O OTHER ININSP/MAINT 1 SO054221E 7AC7151 1) RIGHT WING FRONT SPAR BETWEEN 3RD AND 4TH RIB ON FORWARD FACE OF SPAR A CRACK CROSSING 3 ANNUAL RINGS APPROXIMATELY 4 INCHES IN LENGTH. 2) LEFT WING LOOSE OR MISSING NAILS IN FRONT SPAR AS 3RD AND 4TH RIBS LOOSE OR MISSING NAILS IN FRONT AND REAR SPARS ADJACENT TO STRUT ATTACH FITTING AND OUTBOARD OF SAME. 1H71 3O3 O A759 E205 20020312000642002031200064SW 2002 3 12 2002FA0000241 120010103G5711 SPAR BBAVIA7 7AC 2110102SW CONT A65 A65* 17003SO RT WING CRACKED D K NONE O OTHER ININSP/MAINT 1 SO0583946 7AC2628 1) RIGHT WING/ CRACKS PROPAGATING FROM BOLT HOLES ADJACENT TO FUSELAGE ATTACHMENT FROM AND REAR. 2) CRACK OUTBOARD OF REAR LIFT STRUT REAR SPAR (RIGHT WING) 3) LEFT WING REAR SPAR (ORIGINAL FACTORY SPAR) EDGE GLUED JOINT DELAMINATED FROM ATTACH FITTING OUT TO AILERON 1ST INBOARD RIB. 1H71 3O3 O A759 E205 20020312000652002031200065SW 2002 3 12 2002FA0000242 120010615G5711SAR5263L SPAR BBAVIA7 7GCAA 21101N8SW LYC O320 O320A2B 41508EA LT WING FAILED D K NONE O OTHER ININSP/MAINT 1 EA237591F5025 21070 L3018827A CRACK IN REAR SPAR OF LEFT WING OUTBOARD OF DOUBLER AT SPAR ATTACH FITTING. WING HAS HIT GROUND BEFORE WHEN INBOARD LANDING GEAR BOLT FAILED. TIP OF FORWARD SPAR HAS REPAIR AND DOUBLER. 1H71 3O3 O A759 E274 20020312000662002031200066SW 2002 3 12 2002FA0000243 120010517G1400 FASTENER BBAVIA7 7ECA 21101NNSW CONT O200 O200* 17020SO SPAR MISSING D K NONE O OTHER ININSP/MAINT 1 SW179510S2572 7ECA275 APPROXIMATELY 8 RIB ATTACH NAILS WERE FOUND MISSING ON EACH WING. (BOTH SPARS) SCRATCHES AND GOUGES WERE FOUND ON LEFT REAR SPAR MID AREA. THESE WERE APPARENTLY MADE BY REPAIRMAN SLIDING RIBS DOWN SPAR, DURING THE LAST REPAIR OF WING. BOTH WINGS WILL HAVE COVER REMOVED FOR FURTHER INSPECTION AND REPAIR. 1H71 3O3 O A759 E252 20020312000672002031200067CE 2002 3 12 2002FA0000244 120010517G1400 FASTENER BBAVIA8 8KCAB 2110612CE LYC O360 AEIO360* EA RIB MISSING D K NONE O OTHER ININSP/MAINT 1 SO092561Z1290 35377 APPROXIMATELY 10 RIB NAILS WERE MISSING ON EACH WING. NAIL HOLES WERE NOT ELONGATED. NO OTHER DAMAGE WAS FOUND. THE GENERAL LOCATION OF MISSING NAILS WERE AT STRUT ATTACH AREAS. 1H71 3O3 O A21CE 1E10 20020312000682002031200068CE 2002 3 12 2002FA0000245 120010630G5711SA5263R SPAR BBAVIA7 7KCAB 21101P3CE LYC O320 IO320* 41508EA RT WING CRACKED D K NONE O OTHER ININSP/MAINT 1 WP098643 3161 35473 L495755A AIRFRAME TOTAL TIME 3161 DURING THE ANNUAL INSPECTION AND WHILE COMPLYING WITH AD INSTRUCTIONS. IT WAS DISCOVERED THAT THE RIGHT WING REAR SPAR HAD AN 8 INCHES LONG LONGITUDINAL CRACK AT THE REAR STRUT ATTACH POINT. ITS SUSPECTED THAT THE AIRFRAME HIGH TIME COULD BE THE CAUSE. 1H71 3O3 O A759 1E12 20020312000692002031200069SW 2002 3 12 2002FA0000246 120010718G5711 SPAR BBAVIA7 7FC 2110124SW CONT C90 C90* 17009SO RT WING DEFECTIVE D FYUGK NONE O OTHER ININSP/MAINT 1 SO159898B 218 CRACK VISIBLE MIDWAY FROM TOP TO BOTTOM OF RIGHT WING FRONT SPAR FROM 44 INCHES INBOARD ALONG SPAR TO APPROXIMATELY 130 INCHES FROM INBOARD. WOOD APPEARS TO BE IN GOOD CONDITION OTHER WISE. DEFECT DISCOVERED DURING SPAR INSPECTION IN COMPLIANCE WITH AD. AIRCRAFT WAS NOT DAMAGED OR UNAIRWORTHY IN ANY OTHER WAY. 1H71 3O3 O A759 E252 20020312000702002031200070CE 2002 3 12 2002FA0000247 120011226G5751 BRACKET CESSNA195 195B 2073112CE JACOBSR755 R7557 35003EA IB AILERON CRACKED D K NONE O OTHER ININSP/MAINT 1 CE03195BA 16069 BOTH BRACKETS CRACKED COMPLETELY ACROSS BEARING BOSSES. THIS IS A RECURRING AND EXTENSIVE PROBLEM THAT IS POTENTIALLY VERY CRITICAL FOR CONTROLLABILITY OF THE AIRCRAFT. WE WERE ABLE TO BREAK THE INBOARD END OF AN AILERON LOOSE FROM THE AIRCRAFT WITH APPROXIMATELY 40 LBS OF FORCE EXERTED BY HAND ON THE AILERON WITH A BEARING BOSS CRACKED ON THE HINGE BRACKET. 1H71 3R3 R A790 5E11 20020312000712002031200071CE 2002 3 12 2002FA0000248 120011226G575103227091 BRACKET CESSNA195 195B 2073112CE JACOBSR755 R7557 35003EA AILERON HINGE CRACKED D K NONE O OTHER ININSP/MAINT 1 CE03195BA 16069 BOTH BRACKETS CRACKED COMPLETELY ACROSS BEARING BOSSES. THIS IS A RECURRING AND EXTENSIVE PROBLEM THAT IS POTENTIALLY VERY CRITICAL FOR CONTROLLABILITY OF THE AIRCRAFT. WE WERE ABLE TO BREAK THE INBOARD END OF AN AILERON LOOSE FROM THE AIRCRAFT WITH APPROXIMATELY 40 LBS OF FORCE EXERTED BY HAND ON THE AILERON WITH A BEARING BOSS CRACKED ON THE HINGE BRACKET. 1H71 3R3 R A790 5E11 20020312000732002031200073CE 2002 3 12 2002FA0000250 120010125G5711 SPAR BBAVIA7 7KCAB 21101P3CE LYC O320 IO320* 41508EA WING CRACKED D K NONE O OTHER ININSP/MAINT 1 SO116369N2881 44 WOODEN SPARS, NAILS OUT OF LEADING EDGE RIBS, WOODEN SPACERS WERE LEFT OUT OF FIRST FOUR INBOARD LEADING EDGE RIBS. LEADING EDGE LOOSE, NAILS LOOSE. HAD BEEN PATCHED BEFORE, HAD PUT SCREWS INSTEAD OF NAILS ON LEADING EDGE SPARS AND RIBS. SOME RIBS CRACKED, INNER RIB LACING CORDS BROKEN, HAVE SCRAPPED WINGS AND REPLACING WITH NEW METAL SPAR WINGS. 1H71 3O3 O A759 1E12 20020312000742002031200074SW 2002 3 12 2002FA0000251 120010717G57115270 SPAR BBAVIA7 7GCBC 1220601SW LYC O320 O320* 41508EA WING CRACKED D K NONE O OTHER ININSP/MAINT 1 CE092546Z979 99877 DETECTED COMPRESSION CRACK AT TOP OF AFT SPAR ON THE OUTBOARD END OF LIFT STRUT DOUBLER PLATE. CRACK PROGRESSED DOWN AFT SIDE ABOUT 1 INCH. LONGITUDINAL CRACK WAS ALSO FOUND IN AFT SPAR LAST 12 INCHES NEAR TIP. CRACK WAS IN CENTER OF SPAR. WHEN THE WING WAS DISASSEMBLED FOR SPAR REPLACEMENT, LONGITUDINAL CRACKS WERE FOUND ON FRONT SPAR UNDER THE DOUBLER PLATES FOR THE FUSELAGE TO WING ATTACH FITTINGS. THESE CRACKS WERE NOT DETECTED UNTIL THE PLATE WAS REMOVED. CRACKS WERE BETWEEN THE BOLT HOLES FOR THE DOUBLER PLATE. THIS WING SUSTAINED A TIP STRIKE, AND WAS REPAIRED. SUBMITTER SPECULATES THAT COMPRESSION CRACK AND OTHER DAMAGE OCCURRED AT THIS TIME. 1H71 3O3 ONCA759 E274 20020312000762002031200076SW 2002 3 12 2002FA0000253 120010403G5711 SPAR BBAVIA7 7ECA 21101NNSW LYC O235 O235* 41505EA RT WING CRACKED D TVMRK NONE O OTHER ININSP/MAINT 1 EA056309N2214 233 WHILE COMPLYING WITH AD, A LONGITUDINAL CRACK IN THE RIGHT FOREWARD WOODEN WING SPAR APPROXIMATELY 30 INCHES LONG. 1H71 3O3 O A759 E223 20020312000782002031200078SW 2002 3 12 2002FA0000255 120010801G1400 FASTENER BBAVIA7 7ECA 21101NNSW LYC O235 O235* 41505EA FWD & REAR SPARSMISSING D K NONE O OTHER ININSP/MAINT 1 CE09869833566 103174 NUMEROUS RIB NAILS MISSING OR BACKED OUT FARTHER THAN .1250 ON FORWARD AND AFT WING SPARS, LEFT AND RIGHT WINGS. INSPECTED SPARS AND REPLACED SUCH NAILS. 1H71 3O3 O A759 E223 20020312000792002031200079SW 2002 3 12 2002FA0000256 120010626G5711 SPAR BBAVIA7 7GCB 2110130SW LYC O320 O320* 41508EA RT WING CRACKED G K NONE O OTHER ININSP/MAINT 1 GL079866Y 64 LONGITUDINAL CRACK LOCATED AT ROOT END OF FRONT WING SPAR IN RIGHT WING. CRACK RUNS FROM BUTT END OF SPAR THROUGH THE TWO TOP BOLT HOLES OF THE SPAR TO FUSELAGE ATTACHMENT BRACKET. CRACK COULD BE SEEN IN THE BUTT END GRAIN AND BY REMOVING THE FUSELAGE ATTACHMENT BRACKET AND THE BUSHINGS FROM THE BOLT HOLES. 1H71 3O3 O A759 E274 20020312000822002031200082SW 2002 3 12 2002FA0000258 120010718G5711 SPAR BBAVIA7 7EC 2110120SW RT WING CRACKED C K NONE O OTHER ININSP/MAINT 1 SO159898B 218 WING SPAR, CRACK VISIBLE MIDWAY FROM TOP TO BOTTOM OF NIGHT WING FRONT SPAR FROM 44 INCHES INBOARD ALONG SPAR TO APPROXIMATELY 1130 INCHES FORM INBOARD. WOOD APPEARS TO BE IN GOOD CONDITION OTHERWISE. DEFECT DISCOVERED DURING SPAR INSPECTION IN COMPLIANCE WITH AD. AIRCRAFT WAS NOT DAMAGED OR UNAIRWORTHY IN ANY OTHER WAY. 1H71 3O A759 20020312000862002031200086SW 2002 3 12 2002FA0000263 120010129G5711 SPAR BBAVIA7 7GCAA 21101N8SW LT WING CRACKED D K NONE O OTHER ININSP/MAINT 1 CE07CGFJD 92 WINGS REMOVED FROM AC, THE REPAIR ON THE LT REAR SPAR STRUT ATTACH POINT. ALL FABRIC COVERING REMOVED, LT REAR SPAR HAD A 1 INCH X 16 INCHES LONG .1250 PLYWOOD STRIP GLUED TO THE TOP OF THE SPAR WHICH HID THE CRACK TO BUSHING HOLE. IT WOULD APPEAR THAT CRACK, 4 .7500 AND ADDING THE 1 INCH X 16 INCH STRIP ON TOP. GLUING WAS LESS THAN ACCEPTABLE. 2 INCH CRACK ON THE LT SPAR REMOVED FROM THE RIB FLANGE AND THE RIB MOVED, DETECTION OF THE CRACK IS NEXT TO IMPOSSIBLE. THE 1 INCH COMPRESSION FAILURE ON THE RIGHT SPAR IS BESIDE EDGE OF THE .1250 PLYWOOD REINFORCEMENT. CRACK IS VISIBLE WITH GOOD LIGHT, CRACK DOES NOT GO COMPLETELY ACROSS THE .7500 INCH THICKNESS AND NO LINE VISIBLE ON THE OPPOSITE SIDE. 1H71 3O A759 20020312000872002031200087CE 2002 3 12 2002FA0000264 120010313G276026270522 SOLENOID LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP SPOILER MANIFOLDINTERMITTENT B WIBRK NONE O OTHER ININSP/MAINT 1 SW1110AH 657 SPOILER OPERATION INTERMITTENT. MAINIFOLD ASSEMBLY HAS TWO SOLENOIDS, APPEARS THAT ONE MAY BE STICKING OR HAVE AN ELECTRICAL PROBLEM. 2L72 4F4 F A10CE E6WE 20020312000892002031200089SO 2002 3 12 2002FA0000267 220011201G8520SA640518 PISTON CESSNA182 182M 2072728CE CONT O470 O470R 17026SO NR 5 CYL FAILED G A UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 WP1971298280 18259567 CASTROSPHOIC ENGINE FAILURE AFTER TAKEOFF. EMERGENCY LANDING WAS EXECUTED WITHOUT INCIDENT. ENGINE WAS DISASSEMBLED, REVEALING NR 5 PISTON DISINTEGRATED. ENGINE HAD BEEN OVERHAULED APPROXIMATELY 280 HOURS AND 3.5 YEARS PRIOR TO FAILURE. ALL PISTONS HAD BEEN REPLACED WITH NEW AT OVERHAUL. PARTS WERE SUBMITTED TO THE MANUFACTURER FOR ANALYSIS. 1H71 3O3 ONT3A13 E273 20020313000092002031300009GL 2002 3 13 2002FA0000294 120010722G2821 FUEL FILTER AMTR GLASARGLASAIR 05618GTGL LYC O360 IO360A1A 41514EA ENGINE FUEL CLOGGED C K NONE O OTHER ININSP/MAINT 1 WP2314WQ 2172 IN LINE FUEL FILTER INSTALLED BETWEEN FUEL SELECTOR VALVE AND BOOST PUMP. CLOGGED WITH RUST DEBRIS, AND RESTRICTED FLOW TO ENGINES. 1L71 3O3 ORTEXPA1L711E10 20020313000142002031300014GL 2002 3 13 2002FA0000299 220011220G732323065125 GOVERNOR ALLSN 250C 250C30 03013GL ENGINE INOPERATIVE B AC2RK NONE O OTHER ININSP/MAINT 1 SW03 11056 890384 VERY SENSITIVE, COULD NOT MATCH TORQUES AND SHAFT IS RACHETY. REPLACED WITH SERVICEABLE PART. 3 U E1GL 20020313000172002031300017EA 2002 3 13 2002FA0000304 220011126G74141068256013 MAGNETO PIPER PA32 PA32R300 7103213SO LYC O540 IO540* 41532EA ENGINE BROKEN D K NONE O OTHER ININSP/MAINT 1 AL05200HM 32R7680025 DURING INSPECTION FOUND A DISTRIBUTOR GEAR TOOTH BROKEN AND LAYING IN MAGNETO CAP. THIS MAGNETO HAS PLASTIC GEARS AND HAS BEEN FOUND IN THIS CONDITION ON NUMEROUS MAGNETOS OF THIS TYPE. 1L71 3O3 O A3SO 1E4 20020313001212002031300121CE 2002 3 13 2002FA0000338 120010918G3310PQ876SW LIGHT CESSNA172 172M 2072418CE LYC O320 O320* 41508EA COCKPIT SHORTED D K NONE L NO TEST ININSP/MAINT 1 GL131368U 17267039 THE PART WAS INSTALLED AROUND THE TACH AND CONNECTED TO THE RHEOSTAT FOR THE INSTRUMENT LIGHTS. AFTER A COUPLE OF YEARS IT SHORTED OUT THE SYSTEM. IT BURNED OUT THE RHEOSTAT S2091-5 AND THE POWER TRANSISTOR 2N3055. THIS CAUSED NO INSTRUMENT LIGHT IN THE AIRCRAFT. THIS HAPPENED IN THE DAY TIME AND NOT AT NIGHT IFR. THE OWNER NOTICED NO LIGHTS AND NOTIFIED HIS TECHNICIAN. AFTER TROUBLESHOOTING THE SYSTEM HE FOUND THAT THE WIRES ON THE TOP OF THE LITE RING WERE TOUCHING ONE ANOTHER, CAUSING A DIRECT SHORT. CALLED MFG, THEY INQUIRED, WHEN THIS RING WAS INSTALLED. THEY SAID TO REMOVE IT FROM THE AIRCRAFT AND SEND IT BACK TO THEM, THEY WOULD REPLACE IT FREE OF CHARGE, BECAUSE THIS IS AN OLD STYLE RING. 1H71 3O3 ONT3A12 E274 20020327000762002032700076CE 2002 3 27 2002FA0000345 120010402G2810051600918 FUEL TANK CESSNA172 172S 2072439CE LYC O360 IO360A1A 41514EA FUSELAGE CRACKED D O OTHER K FLUID LOSS TXTAXI/GRND HDL 1 SO05272RP613 172S8405 DURING GROUND RUN, DETECTED FUEL SMELL IN COCKPIT. REMOVED FORWARD FLOOR PANS AND OBSERVED FUEL PUDDLE AND STAIN. INSPECTION REVEALED STAINING ON RESERVOIR TANK. DEFUELED AIRCRAFT AND REMOVED RESERVOIR TANK. STRIPPED PAINT FROM SUSPECTED CRACK AREA. DYE PEN INSPECTION REVEALED 1 INCH CRACK ON LOWER AFT WELD BEAD. REPLACED WITH NEW PART, SUSPECTED CAUSE: STRESS DUE TO UPPER MOUNT HOLE NOT ALIGNED WITH NUT PLATE. 1H71 3O3 ONT3A12 1E10 20020327000942002032700094SW 2002 3 27 2002FA0000347 120010625G5711 SPAR BBAVIA7 7ECA 21101NNSW CONT O200 O200* 17020SO RT WING CRACKED B K NONE O OTHER ININSP/MAINT 1 GL05CFQYQ1905 128 TROUBLE AREA IN THE REGION OF LIFT STRUT ATTACHMENT POINT, REMOVED VARNISH AND SMALL AMOUNT OF WOOD, COULD IDENTIFY SMALL CRACK IN THE GLUE JOINT ON REAR FACE OF RT REAR WING SPAR. ALSO DETECTED ON UPPER EDGE OF RT REAR SPAR A TOTAL OF 5 COMPRESSION TYPE CRACKS. TWO ACTUAL SPLITS WERE REVEALED STARTING AT THE REINFORCING PLYWOOD PLATE. FOLLOWED EDGE GRAIN OF WOOD FRO ABOUT 2 AND 3 INCHES. TWO OF THESE CRACKS EXTENDED DOWN THROUGH SPAR, AT PLYWOOD PLATE EDGE, A DISTANCE OF ABOUT 40-50 PER CENT OF THE WING SPAR. SUGGEST: ALL PLYWOOD REINFORCING PLATES HAVE THEIR VERTICAL EDGES CHAMFERED(TAPERED) AT LEAST .7500 INCH, HELP IN REDUCING STRESS RISER CRATED AT VERTICAL EDGE OF REINFORCING PLATE. 1H71 3O3 O A759 E252 20020405000072002040500007CE 2002 4 5 2002FA0000443 120011203G311004131267 RHEOSTAT CESSNA182 182 2072702CE CONT O470 O470* 17026SO INSTRUMENT PANELSHORTED D O OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM055379B3026 33379 FLYING LOW THRU MOUNTAIN PASS, TRIED TO TURN ON INSTRUMENT LIGHTS. MUCH SMOKE IN CABIN, TURNED OFF MASTER. FOUND RESISTOR WINDINGS FAILED, CONTACT ARM BURNED THRU TO CASE, ALSO CIRCUT BREAKER DID NOT OPEN. FOUND PLASTIC TRIM PANEL HOLE HAD EGG SHAPE, BUTTON COULD NOT POP OUT. REMOVE BACK OF SWITCH AND INSPECT. BETTER TO REPLACE WITH PUSH-PULL SWITCH AND CHECK CIRCUIT BREAKERS. 1H71 3O3 ONT3A13 E273 20020425000542002042500054GL 2002 4 25 2002FA0000524 120011119G7120 MOUNT CIRRUSSR SR22 2130001GL CONT O550 IO550* SO ENGINE CHAFED B MNGRK NONE O OTHER ININSP/MAINT 1 SW05730CD101 0053 DURING THE 100 HOUR INSPECTION, A FUEL LINE CLAMP WAS FOUND CHAFING ON THE ENGINE MOUNT. THE CLAMP HAD CHAFED APPROXIMATELY .006 INTO ONE OF THE ENGINE MOUNT TUBES. THE CLAMP FOR THIS LINE APPEARS TO BE TOO LONG, ALLOWING IT TO CONTACT THE MOUNT TUBE. THE ENGINE MOUNT WAS REPLACED AND THE CLAMP ATTACH BRACKET WAS SHORTENED SO AS TO PREVENT A REOCCURANCE OF THIS CONDITION. THIS AREA SHOULD BE GIVEN A CLOSE INSPECTION FOR CHAFING AND THE CLAMP REPOSITIONED OR THE BRACKET SHORTENED. 1L71 3O3 ONTA00009CHE3SO 20020506001342002050600134CE 2002 5 6 2002FA0000560 120010117G2140FR13E55IEL4500 COMBUST CHAMBER CESSNA421 421C 2076016CE CONT O520 GTSIO520* 17032SO HEATER CRACKED D K NONE L NO TEST ININSP/MAINT 1 GL136798V531 421C1254 OWNER REQUESTED PRESSURE DECAY TEST IAW AD. PRESSURE COULD NOT BE MAINTAINED. REMOVED HEATER, DISCOVERED LARGE CRACK AT AFT, LOWER WALL OF COMBUSTION CHAMBER, ALONG WELD LINE. THIS HEATER WAS INSTALLED 11/1/99 WITH ONLY 531.3 TT HEATER HOURS ON PART. FACTORY REBUILT UNIT INSTALLED WITH NEW CERAMIC COATED LINER TO PREVENT CRACKING. HEATER WAS REPLACED WITH FACTORY WARRANTY UNIT, AND SENT BACK TO FACTORY FOR EXCHANGE. 1L72 3O3 O A7CE E7CE 20020514000392002051400039WP 2002 5 14 2002FA0000582 120010420G6310369D25146 BEARING RACE HUGHES369 369D 4470706WP M/R TRANSMISSIONCRACKED B EOORK NONE O OTHER ININSP/MAINT 1 AL03C6PHC 180257D REMOVED MAIN ROTOR TRANSMISSION FOR AN OIL LEAK. FOUND FORWARD TAIN ROTOR O/P ASSEMBLY PINION BEARING INNER RACE. CRACKED. REPLACED BEARING ASSEMBLY. 1G71 3U H3WE 20020523001052002052300105CE 2002 5 23 2002FA0000665 120011120G5410 STRUCTURE CESSNA411 411A 2075904CE CONT O520 GTSIO520C 17032SO NACELLE CORRODED B A5ORK NONE O OTHER ININSP/MAINT 1 SO09333SF3788 4110260 DURING INSPECTION OF THE WING NACELLE BAGGAGE COMPARTMENT STRUCTURE CORROSION WAS DISCOVERED UNDER THE TRIM AND CARPETS. UPON REMOVAL OF THE NACELLE BAGGAGE COMPARTMENT TRIM AND CARPETS SEVER SURFACE CORROSION WAS DISCOVERED. MAJOR SECTION OF THE NACELLE STRUCTURE IN BOTH WINGS WAS DAMAGED BY CORROSION. THE PROBABLE CAUSE OF THIS CORROSION WAS THE USE OF TRIM ADHESIVE DIRECTLY ON THE AIRCRAFT STRUCTURE. THE TRIM ADHESIVE ACTED LIKE AN ACID ON THE SKINS, RIBS, ANGELS AND BULKHEADS OF THE NACELLE. RECOMMEND ONLY APPROVED ADHESIVES BE USED TO INSTALL TRIM AND CARPETS. 1L72 3O3 O A7CE E7CE 20020729000092002072900009EA 2002 7 29 2002FA0000860 220010925G7414BL68256013 MAGNETO PIPER PA32 PA32RT300T 7103216SO LYC O540 TIO540S1AD 41532EA ENGINE CRACKED G O OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL253994517 32R7887172 AIRCRAFT ON CLIMBOUT FROM AIRPORT, LOST ENGINE POWER AND CRASHED. INVESTIGATION CONCLUDED MAGNETO FAILED DUE TO FATIGUE CRACK IN HOUSING CAUSING MAGNETO HOUSING TO SEPARATE FROM ENGINE. 1L71 3O3 O A3SO E14EA 20020826000572002082600057CE 2002 8 26 2002FA0000987 120010801G32139530489 AXLE HELIO H295 H295 4300802CE LYC O480 GO480* 41527EA MLG BROKEN G O OTHER O OTHER LDLANDING 1 AL0150718 1268 RIGHT GEAR AXLE BROKE (MAIN) ON LANDING, CAUSING SUBSTANTIAL DAMAGE TO FUSELAGE GEAR ATTACH AREA. 1H71 3O3 O 1A8 E275 20020919000022002091900002CE 2002 9 19 2002FA0001052 120011203G311004131267 RHEOSTAT CESSNA182 182 2072702CE CONT O470 O470* 17026SO INTERNAL SHORTED D O OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM055379B3026 33379 FLYING LOW THROUGH A MOUNTAIN PASS TRIED TO TURN ON INSTRUMENTS LIGHTS. SMOKE IN CABIN. TURNED OFF MASTER. FOUND RESISTOR WINDINGS FAILED. CONTACT ARM BURNED THRU TO CASE. ALSO CIRCUIT BREAKER DID NOT OPEN. 1H71 3O3 ONT3A13 E273 20030106000122003010600012CE 2003 1 6 2002FA0001387 120010701G272012600211 BELLCRANK CESSNA180 180K 2072624CE CONT O470 O470J 17026SO RUDDER PEDALS BENT D O OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM02644262067 18052897 AIRCRAFT WAS INVOLVED IN AN ACCIDENT ON LANDING DUE TO LOSS OF CONTROL. CFI WAS FLYING FROM THE RT SEAT. AIRCRAFT LEFT THE RUNWAY TO THE RT EVEN THOUGH PILOT APPLIED FULL LT RUDDER. DURING INSPECTION. DISCOVERED THAT THE LT RUDDER PEDAL WOULD UNLOCK (STOWABLE PEDALS) WHEN FIRM PRESSURE WAS APPLIED, DUE TO BENT BELLCRANK. 1H71 3O3 O 5A6 E273 20030218000832003021800083 2003 2 18 2003FA0000125 420010711G6113055032111 BULKHEAD CESSNA172 172S 2072439CE SPINNER CRACKED B IBIRO OTHER O OTHER NRNOT REPORTED 1 EA27740SP126 172S8671 SPINNER AFT BULKHEAD, CRACKED. 1H71 3O NT3A12 20030312000482003031200048NM 2003 3 12 2003FA0000184 120010623G6320900D1400005101 TRANSMISSION DOUG MD900 MD900 3027375NM PWC PW207 PW207E NE MAIN ROTOR MAKING METAL D K NONE O OTHER ININSP/MAINT 1 EA113PD 56 90000085 MAIN TRANSMISSION PRODUCING METAL CHIPS. CHIP SIZE EXCEED MAINTENANCE MANUAL LIMITS. 1G72 3U3 UNCH19NM E42NE 20030313000012003031300001NM 2003 3 13 2003FA0000186 120010724G6220900C2010186101 DRIVE LINK DOUG MD900 MD900 3027375NM PWC PW207 PW207E NE MAIN ROTOR WORN D K NONE O OTHER ININSP/MAINT 1 EA113PD 107 90000085 MAIN ROTOR UPPER DRIVE LINK BEARING PLAY EXCEEDS MAINTENANCE MANUAL LIMITS. 1G72 3U3 UNCH19NM E42NE 20030313000022003031300002NM 2003 3 13 2003FA0000187 120010726G6220900C2010186101 DRIVE LINK DOUG MD900 MD900 3027375NM PWC PW207 PW207E NE MAIN ROTOR WORN D K NONE O OTHER ININSP/MAINT 1 EA11902PD 90000084 MAIN ROTOR UPPER DRIVE LINK BEARING PLAY EXCEEDS MAINTENANCE MANUAL LIMITS. 1G72 3U3 UNCH19NM E42NE 20030313000032003031300003NM 2003 3 13 2003FA0000188 120010906G2910071142258 INDICATOR DOUG MD900 MD900 3027375NM PWC PW207 PW207E NE FILTER BYPASS DEFECTIVE D K NONE O OTHER ININSP/MAINT 1 EA113PD 90000085 AFTER INSTALLING NEW HYDRAULIC FILTER, THE RETURN SIDE BYPASS INDICATOR POPPED WITH NO PRESSURE APPLIED. AFTER RESETTING THE INDICATOR, INDICATOR POPPED AGAIN. REPLACED IMPENDING BY-PASS INDICATOR PN 071142-258. OPS CHECK GOOD. 1G72 3U3 UNCH19NM E42NE 20030313000042003031300004NM 2003 3 13 2003FA0000190 120010917G2910AC3676F1 FILTER DOUG MD900 MD900 3027375NM PWC PW207 PW207E NE HYD SYSTEM CONTAMINATED D K NONE O OTHER ININSP/MAINT 1 EA11902PD 90000084 BYPASS PIN POPPED ON NR 1 HYDRAULIC RETURN FILTER. REMOVED FILTER AND INSPECTED FOR CONTAMINATION. REPLACED FILTER. OPS AND LEAK CHECK GOOD. 1G72 3U3 UNCH19NM E42NE 20030313000122003031300012GL 2003 3 13 2003FA0000218 120010905G4900427CK1 BATTERY BOMBDRBD700 BD7001A10 1390006GL RROYCEBR700 BR700710A22009500NE APU FAULTY C O OTHER O OTHER NRNOT REPORTED 1 SO11226HD168 9022 12201 AIRCRAFT WAS CONNECTED TO EXTERNAL AIRCRAFT POWER CART, AND POWERED UP. A LOUD POP WAS HEARD COMING FROM AFT EQUIPMENT BAY OF AIRCRAFT. DURING INVESTIGATION, ANOTHER POP WAS HEARD. ACCESSED APU BATTERY. FOUND IT TO BE DAMAGED AND SMOKING. FOUND SEVERAL CELLS BURNED AND HEAT BLANKET BURNED, ALSO. SUSPECT BATTERY CHARGER TO BE FAULTY. BOTH COMPONENTS REPLACED. REMOVED ITEMS, SENT FOR EVALUATION. NO DAMAGE TO AIRCRAFT. THE COCKPIT INDICATION AT TIME OF INCIDENT SHOWED (APU BATT FAIL) TEMPERATURE AND VOLTAGE WERE NORMAL. 2L72 4F4 FRTT00003NYE00061EN 20030409000632003040900063SO 2003 4 9 2003FA0000324 220011116G8520SA639193 BUSHING CONT A50 A502 17002SO CRANK C/WEIGHT MISMANUFACTURED B JZYRO OTHER W INADEQUATE Q C NRNOT REPORTED 1 NM09 WHILE CHECKING THE SIZE OF THE NEW MFG SA639193 BUSHINGS PRIOR TO INSTALLATION IN THE COUNTERWEIGHTS I FOUND TWO NEW STANDARD SIZE BUSHINGS THAT WERE APPROXIMATELY .002 SMALL IN THE OUTER DIAMETER. 3 O E190 20030507001582003050700158CE 2003 5 7 2003FA0000400 120010816G323012416308 BUMPER BLOCK CESSNA210 P210N 2073454CE CONT O520 TSIO520* 17040SO MLG DEBONDED B SMTRO OTHER O OTHER NRNOT REPORTED 1 EA175555S136 P21000417 LT AND RT MAIN LANDING GEAR SHELL BUMPER DEBONDS. THE BUMPER EDGES CURL OVER PREVENTING MAIN GEAR STRUT FROM MAKING FULL DOWN TRAVEL. THIS CONDITION PREVENTS MAIN GEAR STRUT FROM CONTACTING DOWNLOCKS AND PROPER DOWNLOCK SWITCH ACTUATION, THEREFORE, AN UNSAFE CONDITION IT APPEARS THAT MFG MAY HAVE CHANGED THE COMPOSITION OF THE SHELL BUMPER MATERIAL WHICH DOES NOT HAVE GOOD BONDING QUALITIES. (PHOTO) 1H71 3O3 O 3A21 E8CE 20030917000062003091700006CE 2003 9 17 2003FA0000755 120011229G270105117821 CONTROL COLUMN CESSNA185 A185F 2072821CE CONT O520 IO520* 17032SO COCKPIT CRACKED D O OTHER O OTHER NRNOT REPORTED 1 AL05185AF2126 18502236 A CRACK WAS FOUND ON THE AFT SIDE, ASCENDING UP FROM THE BASE OF THE CONTROL COLUMN (CONTROL U ASSY). THE CRACK MEASURED APPROXIMATELY 6 INCHES AND HAD SPREAD APART APPROXIMATELY .5000 INCH JUST ABOVE THE ELEVATOR PUSH-PULL TUBE BEARING AND EXTENDED UP THROUGH THE PIVOT BEARING. SIGNIFICANT AMOUNTS OF RUST WERE NOTED INSIDE THE COLUMN AT THE BASE OF THE CRACK. IT SHOULD BE NOTED THE AIRCRAFT IS INSTALLED ON AMPHIBIAN FLOATS. POSSIBLE CAUSE OF CRACK COULD BE CONTRIBUTED TO WATER COLLECTING IN THE BOTTOM OF THE COLUMN AND FREEZING. 1H71 3O3 O 3A24 E5CE 20031114000502003111400050EA 2003 11 14 2003FA0001091 220010601G8520 FLANGE PITTS S2B S2B 2210006SO LYC O540 AEIO540D4A5 41532EA HARTZLHCC2Y HCC2YR4 GL CRANKSHAFT CRACKED B R6ARO OTHER O OTHER NRNOT REPORTED 1 WP01260MM 5186 FOUND CRACKED CRANKSHAFT FLANGE. INSTALLED 3 BLADE PROP TO DECREASE STRESS ON CRANKSHAFT. 1Q71 3O3 ONCA8SO 1E4 5 CP920 20031114000452003111400045EA 2003 11 14 2003FA0001092 220010701G8520 FLANGE PITTS S2B S2B 2210006SO LYC O540 AEIO540D4A5 41532EA HARTZLHCC2Y HCC2YR4 GL CRANKSHAFT CRACKED B R6ARO OTHER O OTHER NRNOT REPORTED 1 WP01260GR 5059 FOUND CRACKED CRANKSHAFT FLANGE. INSTALLED 3 BLADE MT PROP TO DECREASE STRESS ON CRANKSHAFT.(K) 1Q71 3O3 ONCA8SO 1E4 5 CP920 20041004000962004100400096CE 2004 10 4 2004FA0000742 120010109G1430 NUT BEECH 35 V35B 1151548CE CONT O520 IO520BA 17032SO MCAULY3A32C 3A32C76 GL RUDDER CRACKED D O OTHER O OTHER NRNOT REPORTED 1 WP074572A3452 D9150 ON ANNUAL INSPECTION OF RUDDERS AT THE CENTER ATTACH FITTING AFT SPAR MOUNT, SLIGHT RUST WAS NOTED. FURTHER INSPECTION REVEALED 5 OUT OF THE 8 ATTACH NUTS ON THE SPAR ATTACH WERE CRACKED THROUGH TO THE BOLT THREADS. THESE NUTS ARE CRACKED ONLY O THE BOTTOM AREA OF NUT. LOOKING DOWN AT THE ATTACH NUTS WILL NOT SHOW CRACKS. TELL TALE RUST ON THE BOLT THREADS IS THE ONLY TOP SIDE INDICATOR. RECOMMEND THAT NAS679A NUT BE INSPECTED OR REPLACED WITH MS21042 OR MS21083N. THESE NUTS ARE USED IN OTHER LOCATIONS ON THE PLANE. EXPOSED NUTS ARE MORE SUSCEPTIBLE TO CRACKING. 1L71 3O3 O 3A15 E5CE 5 CP21EA 20020128000512002012800051 2002 1 28 223527605 420011203G2562BP1010 BATTERY NARCO 10 CESSNA150 150J 2071820CE CONT O200 O200A 17020SO MCAULY1A100 1A100* GL ELT LEAKING P K NONE O OTHER ININSP/MAINT 1 SO116083010 10 19503 15070606 250894 G1018 ON DOING A PRE FLIGHT INSPECTION I FOUND THAT ACID WAS LEAKING FROM THE ELT BATTERY. FURTHER INSPECTION SHOWS THAT ACID LEAKING FROM THE PACK HAD DESTROYED THE ELT ELECTRONICS MODULE, THE MOUNTING BASE WAS EATEN THROUGH AS WAS THE CARPET AND THE ACID WAS ATTACKING THE FLOOR OF THE BAGGAGE COMPARTMENT. 1H71 3O3 O 3A19 E252 5 NP918 20020128000542002012800054SO 2002 1 28 3372 120011203G5102 WEB BALWKS F11B BALWKSFIREFYFIREFLY11B 1050140SO UPPER ENVELOPE DAMAGED B O OTHER O OTHER NRNOT REPORTED 1 NM037244W171 30 003 F11B003 HOT AIR BALLOON ENVELOPE TOP GIRDLE 1INCH WEBBING STRETCHED. TOP ENVELOPE FABRIC PANELS DO NOT STRETCH, CAUSING SEVERE STITCH-HOLE ELONGATION DAMAGE TO FABRIC ALONG ALL TOP PANEL VERTICAL SEAMS, EXTENDING FROM TOP GIRDLE DOWNWARD 6-12 INCHES. 1B00 A14SO 20010502000672001050200067SO 2001 5 2 58392816R 120010319G5712 RIB PIPER PA28 PA28R200 7102811SO LT WING CRACKED P K NONE O OTHER ININSP/MAINT 1 SW992816R 28R35297 INSPECTION OF AIRCRAFT IN MAINT HANGAR REVEALED TWO INCH CRACK ON LT WING AT APPROX WS 49.25, AROUND SINGLE RIVET, SKIN HAD BULGED AROUND RIVET AND CRACKED FORE AND AFT. INSPECTION IN WHEEL WELL SHOWED THAT RIVETS ATTACHING FLANGE TO FALSE REAR SPAR AND RIB TO FALSE REAR SPAR HAD SHEARED, HEADS GONE, SOME PORTION OF RIVETS LEFT, LEAVING NO STRENGTH BELOW AREA OF SKIN. INSPECTION INSIDE INSPECTION PANEL IMMEDIATELY AFT OF THAT AREA REVEALED CRACKED RIB AT JOIN WITH FALSE REAR SPAR. CLOSE INSPECTION SHOWS EVIDENCE THAT THERE WAS DAMAGE SOME TIME AGO WHICH HAD BEEN WORKING ITSELF DURING FLIGHT OPS (ALUM. DUST AROUND FAILURE AND SEAMS, DIRT AND GREASE AT PLACES WHERE RIVET HEADS WERE GONE). 1L71 3O 2A13 20010503002372001050300237 2001 5 3 65BA046A 420010413G2300 RHEOSTAT PIPER PA32 PA32300 7103212SO LYC O540 IO540K1A5 41532EA RADIO FAILED H GSBAK NONE O OTHER ININSP/MAINT 1 AL0176RL 15481 327540024 L1737448A RETURNING FROM A FLIGHT, PILOT SHUT DOWN ENGINE, RADIO MASTER, THE A/C MASTER. WHEN MASTER WAS SHUT OFF, PILOT HEARD A POP FROM THE RIGHT SIDE OF PANEL. HE CHECKED BREAKERS, NOTICED NONE BLOWN, BUT SMELLED; NOTICE SMOKE COMING FROM BEHIND PANEL TO LEFT OF CIRCUIT BREAKERS. WHEN INVESTIGATED, FOUND RHEOSTAT ASSEMBLY WIRING AND COMPONENTS BURNT FOR CABIN LIGHT CONTROLS. PART WAS REPLACED WITH SERVICABLE ASSEMBLY. 1L71 3O3 O A3SO 1E4 20010502000552001050200055CE 2001 5 2 951141 120010314G2910124F0016CL0532 HOSE CESSNA500 550 2076604CE HYD PUMP BURST B R8RRA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP073262M2572 5500652 DURING FLIGHT BOTH THE HYDRAULIC FLOW LIGHTS AND THE HYDRAULIC RESERVEOIR LOW LEVEL LIGHT ILLUMNINATED. FOUND THE PRESSURE LINE FROM THE NR 1 HYDRAULIC PUMP BURST APPROX. 18 INCHES FROM THE PUMP. THERE WERE NO CHAFF MARKS ON THE HOSE, SUSPECT INTERNAL FAILURE OF THE HOSE. THE INCIDENT IS STILL UNDER INVESTIGATION. 1L72 4F A22CE 20010924000102001092400010NE 2001 9 24 A244583 220010826G7310430137601C TUBE BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE FUEL MANIFOLD CRACKED D O OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO15911WJ 7050 L45178 MINUTE CRACK DEVELOPED IN MANIFOLD RIGID TRANSFER TUBE, CAUSING INFLIGHT FUEL LEAK. ALLOW USE OF FLEXIBLE TRANSFER TUBE FUEL MANIFOLDS ON LTS101650B1. 1G72 3U3 U H13EU E5NE 20010507005722001050700572GL 2001 5 7 AC2A072773 220010110G72506898683 NOZZLE BELL 206 206L3 1182108SW ALLSN 250C 250C30S 03013GL 4TH STAGE DEBONDED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0117238 51492 MAIN ROTOR BLADES FAILED TO TURN BY SPECIFIED N1 SPEED UPON STARTING ENGINE. IT WAS DETERMINED THAT SOMETHING INSIDE OF TURBINE WAS RUBBING DUE TO SOUND COMING FROM TURBINE WHEN ROTOR WAS TURNED BACKWARDS. TURBINE WAS REMOVED AND DISASSEMBLED. IT WAS FOUND THAT THE 4TH STAGE NOZZLE #4 BLADE PATH HAD DISBONDED AND WAS RUBBING THE #4 TURBINE WHEEL OUTER DIAMETER KNIFE EDGES CREATING DRAG THAT WAS CAUSING PROBLEM WITH MAIN ROTOR NOT TURNING ON START. DISBONDING WAS IN APPROXIMATELY 25 SEPARATE SPOTS SPACED AROUND CIRCUMFRENCE OF BLADE PATH, WITH THE LARGEST SPOT BEING AROUND ONE QUARTER INCH IN DIAMETER, ROUGHLY ROUND IN SHAPE AND RAISED ENOUGH TO CONTACT THE WHEEL OUTER DIAMETER. THIS CONDITION WOULD APPEAR TO B1G71 3U3 U H2SW E1GL 20010507005732001050700573SW 2001 5 7 AC2A072774 120010110G2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED H AC2AK NONE L NO TEST ININSP/MAINT 1 FS017159H676 51397 PART IS WEAK. REPLACED BATTERY 1G71 3U H2SW 20010507005742001050700574SW 2001 5 7 AC2A072775 120010111G2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED H AC2AK NONE L NO TEST ININSP/MAINT 1 FS0117238807 51492 PART IS WEAK. REPLACED BATTERY 1G71 3U H2SW 20010507005752001050700575NE 2001 5 7 AC2A072776 120010112G2430A1077B RELAY SKRSKYS76 S76A 8143006NE BATTERY SHORTED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS017266K 760283 PART CIRCUIT-SHORTED. REPLACED RELAY 1G72 3U H1NE 20010507005762001050700576NE 2001 5 7 AC2A072777 120010122G63207635109082105 CHIP DETECTOR SKRSKYS76 S76A 8143006NE ENGINE LEAKING H AC2AK NONE K FLUID LOSS ININSP/MAINT 1 FS015403C 760141 PART LEAKS AT CONNECTOR. REPLACED CHIP DETECTOR 1G72 3U H1NE 20010507005772001050700577EU 2001 5 7 AC2A072778 120010125G2435230321825 STATOR BOLKMS105 BO105S 5626006EU STARTER GEN GROUNDED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS018775 8034 775 PART IS CIRCUIT-GROUNDED. REPLACED STATOR. 1G72 3U H3EU 20010507005782001050700578EU 2001 5 7 AC2A072779 120010125G2435230322111 ARMATURE BOLKMS105 BO105S 5626006EU STARTER GEN GROUNDED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS018776 776 PART IS CIRCUIT-GROUNDED. REPLACED ARMATURE 1G72 3U H3EU 20010507005792001050700579EU 2001 5 7 AC2A072780 120010125G2435230322111 ARMATURE BOLKMS105 BO105S 5626006EU STARTER GEN GROUNDED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS018775 775 PART IS CIRCUIT-GROUNDED. REPLACED ARMATURE. 1G72 3U H3EU 20010507005802001050700580GL 2001 5 7 AC2A072781 220010130G723023039791 SPLINE ADAPTER 6890550 BELL 206 206B3 1181506SW ALLSN 250C 250C* GL COMPRESSOR CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01214601562 41256 4075 COMPRESSOR WAS REMOVED TO FACILITATE GEARBOX MAINTENANCE. SPLINE ADAPTER WEAR WAS CHECKED WITH GO-NO-GO GAUGE AND WAS FOUND TO BE WORN. SPLINE ADAPTER WAS REMOVED AND WAS FOUND TO HAVE A RING OF CORROSION PITTING AROUND OUTSIDE CIRCUMFRENCE OF ADAPTER .650 INCH FORWARD OF AFT END OF ADAPTER. LOCATION OF CORROSION IS AT THE POINT WHERE THE ADAPTER SEATS INTO THE IMPELLER AT THE JUNCTION OF THE AFT END OF THE IMPELLER AND THE ADAPTER. CORROSION IS AT THE SAME LOCATION WHERE A PREVIOUS SPLINE ADAPTER FAILED HERE AT CHEVRON RESULTING IN AN IN FLIGHT ENGINE FAILURE AND UNSCHEDULED LANDING. SPLINE ADAPTER FIT AND INSTALLATION WAS IN ACCORDANCE WITH MAINTENANCE INSTRUCTIONS. SPLINE ADAPTER WAS REPLACED. COMPRESSOR I1G71 3U3 U H2SW E4CE 20010507005812001050700581GL 2001 5 7 AC2A072782 220010130G723023039791 SPLINE ADAPTER 6890550 BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL COMPRESSOR CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0159588756 41394 780 COMPRESSOR WAS REMOVED DUE TO F.O.D. SPLINE ADAPTER WAS REMOVED IN ORDER TO DISASSEMBLE COMPRESSOR ROTOR FOR REPAIR. SPLINE ADAPTER WAS FOUND TO HAVE A RING OF CORROSION AROUND OUTSIDE CIRCUMFRENCE OF ADAPTER .650 INCH FROM REAR END OF ADAPTER. CORROSION IS AT THE POINT WHERE THE ADAPTER SEATS INTO THE IMPELLER AT THE JUNCTION OF THE ADAPTER AND THE REAR END OF THE IMPELLER. CORROSION IS AT THE SAME LOCATION WHERE CHEVRON PREVIOUSLY HAD AN ADAPTER FAIL THAT RESULTED IN AN IN FLIGHT ENGINE FAILURE AND UNSCHEDULED LANDING. SPLINE ADAPTER FIT AND INSTALLATION WERE IN ACCORDANCE WITH MAINTENANCE INSTRUCTIONS. SPLINE ADAPTER WAS REPLACED. COMPRESSOR IS STILL IN SPARES AT THIS TIME AND HAS NOT BEEN RETURNED TO SERVIC1G72 3U3 U H3EU E4CE 20010507005822001050700582GL 2001 5 7 AC2A072783 220010213G721023063371 SEAL BELL 206 206L3 1182108SW ALLSN 250B 250B* GL GEARBOX LEAKING H AC2AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 FS017159J 51408 AIRCRAFT WAS GROUND RUN AND LEAK CHECKED FOLLOWING ENGINE CHANGE. NO LEAKS FOUND. AIRCRAFT RETURNED AFTER 20 MINUTE TEST FLIGHT. OIL WAS FOUND IN THE ENGINE PAN. OIL LEAKING FROM STARTER-GENERATOR SEAL ON ENGINE GEARBOX. REPLACED SEAL. UPON INSPECTION OF SEAL, IT WAS FOUND TO HAVE A TEAR OR CUT HALF WAY AROUND THE INSIDE CIRCUMFERENCE OF THE SEAL. 1G71 3U3 T H2SW E10CE 20010507005832001050700583NE 2001 5 7 AC2A072784 220010311G753223005366 BLEED VALVE BELL 430 430 1182150SW ALLSN 250C 250C40B 03032NE ENGINE LOOSE H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH46 49037 844154 BLEED VALVE HOUSING WAS LOOSE. REPLACED DIAPHRAGM. REASSAMBLED AND PERFORMED TEST. 1G72 3U3 URTH9SW E1GL 20010515001092001051500109CE 2001 5 15 AC2A072785 120010311G781012502642 EXHAUST PIPE CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01 5357 EXHAUST COLLECTOR FOUND CRACKED REPLACED WITH NEW COLLECTOR 1H71 3O3 O A4CE E5CE 20010507005842001050700584NE 2001 5 7 AC2A072786 220010327G7320AN8378J ELBOW BELL 430 430 1182150SW ALLSN 250C 250C40B 03032NE ENGINE LEAKING H AC2AK NONE K FLUID LOSS ININSP/MAINT 1 FS01430CV46 49072 844154 FUEL LEAK ON LINE FROM CEFA TO HMU. FOUND ELBOW ON CEFA HAD A MILLING MARK ON FACE OF FLANGE. REPLACED ELBOW. 1G72 3U3 URTH9SW E1GL 20010507005852001050700585NE 2001 5 7 AC2A072787 220010327G72616871937 LINE BELL 430 430 1182150SW ALLSN 250C 250C40B 03032NE ENGINE LEAKING H AC2AK NONE K FLUID LOSS ININSP/MAINT 1 FS01430CV46 49072 844154 OIL LEAK ON INBOARD SIDE OF NR 1 ENGINE. FOUND TUBE ASSY FROM CHECK VALVE TO GEAR BOX HOUSING WOULD NOT SEAT PROPERLY. REPLACED TUBE ASSY. 1G72 3U3 URTH9SW E1GL 20010507005862001050700586SW 2001 5 7 AC2A072788 120010331G2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN WEAK H AC2AK NONE O OTHER ININSP/MAINT 1 FS017159J319 51408 PART IS WEAK. REPLACED BATTERY WITH A NEW PART 1G71 3U H2SW 20010507005872001050700587 2001 5 7 AC2A072789 420010402G34161042011968E ALTIMETER SKRSKYS76 S76A 8143006NE COCKPIT OUT OF TOLERANCEH AC2AK NONE L NO TEST ININSP/MAINT 1 FS015403C 760141 VIBRATOR INOP,AUTOPILOT CORRECTION POTENTIOMETER OUT OF TOLERANCE AND OFF FLAG STICKS. REPLACED INST. 1G72 3U H1NE 20010507005882001050700588NE 2001 5 7 AC2A072790 120010405G243503600923 BEARING 23081018 SKRSKYS76 S76A 8143006NE DRIVE END DETERIORATED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS015401G907 3361 760137 PART IS DETERIORATED. BEARING CAGE FAILED ALLOWING ALL BALLS TO GROUP TOGETHER. NO BALLS WERE LOST OR DETERIORATED OVERHAULED STARTER - GENERATOR AND REPLACED BEARINGS. 1G72 3U H1NE 20010507005892001050700589 2001 5 7 AC2A072791 420010416G2210065001580211 COMPUTER BELL 430 430 1182150SW COCKPIT FAILED H AC2AK NONE L NO TEST ININSP/MAINT 1 FS01430CV105 49072 AFCS PIT CAUTION LIGHT DURING AP2 TEST. AP2 & SAS2 CAUTION LIGHT REMAINS ON AFTER COMPLETION OF TEST. AFCS PIT CAUTION LIGHT ILLUMINATES WHEN IN AP2. REPLACED WITH NEW PART. 1G72 3U RTH9SW 20010510001392001051000139SW 2001 5 10 AC2A072803 120010101G6220430010101101 YOKE BELL 430 430 1182150SW ROTOR HEAD CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH2862 49037 SPAN-WISE CRACK ON TOP APPROX 12 INCHES FROM CENTER. REPLACED. 1G72 3U RTH9SW 20010510001402001051000140SW 2001 5 10 AC2A072804 120010101G6220430010101101 YOKE BELL 430 430 1182150SW MAIN ROTOR CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH2862 49037 SPAN-WISE CRACK 12 INCHES FROM CENTER. REPLACED. 1G72 3U RTH9SW 20010510001412001051000141SW 2001 5 10 AC2A072805 120010101G6410222016001131 BLADE BELL 430 430 1182150SW TAIL ROTOR CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH1742 49037 FEATHERING BEARINGS CRACKED. FEATHERING BEARINGS WERE REPLACED BEFORE THIS AT TIME 589.4. THE BLADE HAS 1152.8 SINCE REPLACEMENT OF BEARINGS. REPLACED BLADE 1G72 3U RTH9SW 20010510001422001051000142SW 2001 5 10 AC2A072806 120010101G6510430044100101 DRIVE SHAFT BELL 430 430 1182150SW TAIL ROTOR CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH2862 49037 CORROSION AROUND FLANGE AREA. DRIVE SHAFTS WERE NR 2 & 3 AND AREA OF CORROSION WAS NEAR WHERE OILCOOLER COWLING AND TAIL DRIVE SHAFT COWLING MEET. REPLACED DRIVE SHAFTS. 1G72 3U RTH9SW 20010510001432001051000143SW 2001 5 10 AC2A072807 120010101G6220430310101105 SHEAR RESTRAINT BELL 430 430 1182150SW MAIN ROTOR DELAMINATED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH2862 49037 DELAMINATING FROM SHAFT REPLACED SHEAR RESTRAINT. 1G72 3U RTH9SW 20010510001442001051000144SW 2001 5 10 AC2A072808 120010101G6300430010212101 RESTRAINT BELL 430 430 1182150SW MAIN ROTOR DRIVEDEBONDED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH2862 49037 ELASTOMERIC DEBONDING REPLACED RESTRAINT 1G72 3U RTH9SW 20010510001452001051000145SW 2001 5 10 AC2A072809 120010101G6710222382001107 ACTUATOR BELL 430 430 1182150SW FLIGHT CONTROL LEAKING H AC2AK NONE K FLUID LOSS ININSP/MAINT 1 FS01430CH2862 49037 LEAKING, REPLACED ACTUATOR. 1G72 3U RTH9SW 20010510001462001051000146SW 2001 5 10 AC2A072810 120010101G7120430360051101 MOUNT BELL 430 430 1182150SW ENGINE WORN H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH2862 49037 REAR ENGINE MOUNT BEARING AT DECK WORN. BALL (P/N 230-360-101-103) NOT WORN. ROD END BODY (P/N 230-360-101-105) WAS WORN. REPLACED MOUNT 1G72 3U RTH9SW 20010510001472001051000147SW 2001 5 10 AC2A072811 120010101G6210430015001123 BLADE BELL 430 430 1182150SW MAIN ROTOR CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH1370 49037 CRACKED INBOARD TRIM TAB REPLACED TRIM TAB 1G72 3U RTH9SW 20010510001482001051000148SW 2001 5 10 AC2A072812 120010129G7921230365001101 BLOWER BELL 430 430 1182150SW ALLSN 250C 250C40B 03032NE OIL COOLER DEFECTIVE H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH693 49037 BEARING MAKES CLICKING SOUND AND CORROSION NEAR REAR NUT. PART WAS NEVER INSTALLED ON AIRCRAFT DUE TO THIS. 1G72 3U3 URTH9SW E1GL 20010510001492001051000149SW 2001 5 10 AC2A072813 120010202G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0131079296 51526 CRACKED. 1G71 3U H2SW 20010510001502001051000150SW 2001 5 10 AC2A072814 120010205G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS015370290 51249 CRACKED. 1G71 3U H2SW 20010510001512001051000151SW 2001 5 10 AC2A072815 120010220G291070053H000A100A HOSE BELL 206 206L3 1182108SW HYD SYSTEM LEAKING H AC2ABA EMER. DESCENT UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 FS0117592 51535 AT CRUISE TO LEEVILLE (LA) HELIPORT, THE PILOT HEARD A LOUD GRINDING NOISE FOLLOWED BY COMPLETE HYDRAULIC FAILURE. THE PILOT PERFORMED THE EMERGENCY PROCEDURE THEN CONFIRMED IT WITH THE BOOK WITH NO CORRECTION TO THE EMERGENCY. PILOT PERFORMED A SHALLOW APPROACH WITH A SLIGHT RUN ON LANDING, AND SHUT DOWN THE AIRCRAFT. REPLACED HYDRAULIC LINE P/N 70-053H000A100A. 1G71 3U H2SW 20010510001522001051000152SW 2001 5 10 AC2A072817 120010223G3340AN33201 RELAY BELL 206 206B3 1181506SW LANDING LIGHT FAILED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS017131U9 4111 RELAY FAILED AFTER 41 DAYS ON THE AIRCRAFT. THE LANDING LIGHT WAS INOPERABLE. 1G71 3U H2SW 20010510001532001051000153SW 2001 5 10 AC2A072818 120010306G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS017159H441 51397 CRACKED. REPLACED PART. 1G71 3U H2SW 20010510001542001051000154SW 2001 5 10 AC2A072819 120010311G62104300150037101 EROSION SHIELD 430015001123BELL 430 430 1182150SW MAIN ROTOR BLADEDAMAGED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV A1118 49072 EROSION TAPE FOR MAIN ROTOR BLADE WAS FOUND BUBBLED. FUTHER INSPECTION FOUND BUBBLE WAS FULL OF WATER. THERE WAS NO SIGN OF AREA OF ENTRY. REPLACED EROSION TAPE. 1G72 3U RTH9SW 20010515001102001051500110SW 2001 5 15 AC2A072820 120010311G6230430010105105 PLATE 430010100113BELL 430 430 1182150SW MAIN ROTOR LOOSE H AC2AK NONE O OTHER ININSP/MAINT 1 FS01 46 A166 CLAMP PLATE WAS NOT SHIMED PROPERLY ON SHEAR RESTRAINT. RESHIMED CLAMP PLATE. 1G72 3U RTH9SW 20010510001552001051000155SW 2001 5 10 AC2A072821 120010311G5210 LATCH BELL 430 430 1182150SW CREW DOOR OUT OF ADJ H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV46 49072 CABIN DOOR WAS EXTREMELY HARD TO OPEN AND WOULD NOT CLOSE PROPERLY. AJUSTED DOOR LATCHES. 1G72 3U RTH9SW 20010510001562001051000156SW 2001 5 10 AC2A072822 120010311G7500230025203101 TUBE BELL 430 430 1182150SW ENGINE BLEED AIRCHAFED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV46 49072 CUSTOMER BLEED AIR TUBE HAD A WORN SPOT FROM THE UPPER ENGINE COWLING(PN 230-061-803-104). REPLACED TUBE ASSY AND REPAIRED COWLING. 1G72 3U RTH9SW 20010510001572001051000157SW 2001 5 10 AC2A072823 120010311G5320222035165164 CLIP BELL 430 430 1182150SW FUSELAGE MISINSTALLED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV46 49072 TAIL ROTOR DRIVE SHAFT COVER (PN 222-035-165-179) WAS RUBBING TAIL ROTOR DRIVE SHAFT SUPPORT BEARING SUPPORT (PN 430-035-164-105). CAUSE OF RUBBING WAS FORWARD TAIL ROTOR DRIVE SHAFT COWLING CLIP (PN 222-025-165-164) WAS INSTALLED TO CLOSE TOGETHER AND DID NOT GIVE SUFFICIENT CLEARENCE FOR SUPPORT. ADDED SPACER PAD BETWEEN DRIVE SHAFT COVER AND CLIP. 1G72 3U RTH9SW 20010510001582001051000158SW 2001 5 10 AC2A072824 120010311G62002006508083 BOLT BELL 430 430 1182150SW MAIN ROTOR CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV46 49072 WHILE REMOVING MAIN ROTOR YOKES WATER CAME OUT OF AREA OF MAIN ROTOR DRIVE BUSHINGS AND MAIN ROTOR BOLTS. DRIVE PLATE WAS FOUND NOT TO BE SEALED PROPERLY AND 2 MAIN ROTOR BOLTS WERE FOUND TO HAVE CORROSION PITTING. REPLACED BOLTS AND SEALED PROPERLY. 1G72 3U RTH9SW 20010510001592001051000159SW 2001 5 10 AC2A072825 120010325G6520222342402101 SEAL 222042001103BELL 430 430 1182150SW TAIL ROTOR G/B LEAKING H AC2AK NONE K FLUID LOSS ININSP/MAINT 1 FS01430CV46 A270 49072 TAIL ROTOR GEAR BOX WAS LEAKING FROM OUT PUT SEAL. WHEN SEAL WAS RENOVED IT WAS DISCOVERED THAT THE SEAL LIP HAD SEALENT MIL-S-8784 ON IT. THIS SEALENT IS USED ON THE OUTER SURFACE OF THE SEAL WHEN INSTALLING. REPLACED SEAL. 1G72 3U RTH9SW 20010510001602001051000160SW 2001 5 10 AC2A072826 120010403G3213206323017 CROSSTUBE BELL 206 206L3 1182108SW LANDING GEAR CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0131079602 51526 PART HAS INTERGRANULAR CORROSION SEVERAL PLACES ON TUBE. THIS FORWARD CROSSTUBE HAD ONLY 602 HOURS SINCE INSTALLATION, THE CORROSION WAS EXTENSIVE AND BEYOND LIMITS. REPLACED CROSSTUBE WITH NEW PART. 1G71 3U H2SW 20010510001612001051000161 2001 5 10 AC2A072827 420010416G3425430375002107 DISPLAY BELL 430 430 1182150SW EFIS FAILED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS01430CV105 49072 SCREEN WENT BLANK IN FLIGHT. REPLACED PART. 1G72 3U RTH9SW 20010510001622001051000162SW 2001 5 10 AC2A072828 120010416G2436222375060115 VOLT REGULATOR BELL 430 430 1182150SW ELECTRICAL DEFECTIVE H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH 49037 REGULATOR WAS INOPERATIVE WHEN WE RECEIVED IT FROM BELL. EXCHANGING THIS PART FOR A NEW ONE. 1G72 3U RTH9SW 20010510001632001051000163SW 2001 5 10 AC2A072829 120010419G291070012H000Y264 HOSE BELL 430 430 1182150SW TRANSMISSION CHAFED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV122 49072 PART IS CHAFED. LINE CHAFED ON TRANSMISSION COWLING. INSTALLED NEW LINE. REPOSITIONED ELBOW FOR NEW LINE TO CLEAR TRANSMISSION COWLING. 1G72 3U RTH9SW 20010510001642001051000164SW 2001 5 10 AC2A072830 120010426G262240000MODLE11211 EXTINGUISHER BELL 206 206L3 1182108SW CABIN DISCHARGED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0117237301 51478 FIRE EXTINGUISHER HAD LOW WEIGHT. REPLACED WITH NEW FIRE EXTINGUISHER. 1G71 3U H2SW 20010510001652001051000165SW 2001 5 10 AC2A072831 120010426G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS016533U187 51439 PART IS CRACKED. REPLACED WITH NEW EXHAUST. 1G71 3U H2SW 20010510001662001051000166SW 2001 5 10 AC2A072832 120010426G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0117592815 51535 CRACKED. REPLACED EXHAUST ASSY. 1G71 3U H2SW 20010510001792001051000179GL 2001 5 10 AC2A072834 220010306G732323065123 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NR 1 ENGINE DEBONDED H AC2AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 FS015366Y8130 782 PILOT REPORTED N2 OVERSPEED UNCONTROLLABLE WITH RPM TRIM MOTOR. NR 1 ENGINE RETURNED TO FLIGHT IDLE. FUEL JETTISONED, AND PILOT PERFORMED RUN-ON LANDING. REMOVED GOVERNOR AND FOUND DRIVE SPLINE DISENGAGED FROM GOVERNOR SHAFT. GOVERNOR REPLACEMENT FIXED PROBLEM. 1G72 3U3 U H3EU E4CE 20010510001802001051000180GL 2001 5 10 AC2A072835 220010319G732323004831 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE DEBONDED H AC2AK NONE O OTHER ININSP/MAINT 1 FS015366Y1888 782 UNBONDED SHAFT. 1G72 3U3 U H3EU E4CE 20010510001812001051000181GL 2001 5 10 AC2A072836 220010319G732323065123 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS018776 11601 776 CHECKED DRIVE COUPLING AND FOUND DEFECTIVE. 1G72 3U3 U H3EU E4CE 20010510001822001051000182GL 2001 5 10 AC2A072837 220010319G732323065123 GOVERNOR BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL ENGINE DEBONDED H AC2AK NONE O OTHER ININSP/MAINT 1 FS017131U9381 4111 DRIVE COUPLING DEBONDED. 1G71 3U3 U H2SW E4CE 20010510001832001051000183GL 2001 5 10 AC2A072838 220010425G732323065123 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NR 2 ENGINE BROKEN H AC2AK NONE O OTHER ININSP/MAINT 1 FS018775 7744 775 POTTING ON END OF DRIVE GEAR IS BROKEN LOOSE. REMOVED GOVERNOR. 1G72 3U3 U H3EU E4CE 20010919000042001091900004SW 2001 9 19 AC2A075785 120010502G6310206040272101 SEAL BELL 206 206L3 1182108SW INPUT SHAFT LEAKING H AC2AK NONE O OTHER ININSP/MAINT 1 FS0117237614 51478 PARTS ARE LEAKING GREASE. REPLACED SEALS. 1G71 3U H2SW 20010919000052001091900005EU 2001 9 19 AC2A075786 120010502G781059528AELPSW3 CLAMP BOLKMS105 BO105S 5626006EU EXHAUST STACK CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0159588286 780 PART WAS FOUND CRACKED WHILE WHILE PERFORMONG NDT INSPECTION AS PER ASB BO-105-60-107. REPLACED CLAMP. 1G72 3U H3EU 20010919000062001091900006GL 2001 9 19 AC2A075787 220010502G732323065123 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NR 1 ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS015366Y7199 782 836103 EPOXY DEBONDED ON GOVERNOR DRIVE SHAFT. REMOVED FROM SERVICE AND SENT IN FOR WARRANTY REPAIR. 1G72 3U3 U H3EU E4CE 20010919000072001091900007EU 2001 9 19 AC2A075788 120010507G634032005007 TACH GENERATOR BOLKMS105 BO105S 5626006EU TRANSMISSION DEFECTIVE H AC2AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 FS01826MB18 771 PART IS DEFECTIVE. ROTOR INDICATIONS WERE ZERO ON CRANK-UP REPLACED TACH/GEN 1G72 3U H3EU 20010919000082001091900008EU 2001 9 19 AC2A075789 120010507G624032005007 TACH GENERATOR BOLKMS105 BO105S 5626006EU MAIN ROTOR DEFECTIVE H AC2AA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 FS01826MB2 771 PART IS DEFECTIVE.CAUSED HIGH RPM AUDIO TO SOUND DURING NORMAL OPERATION. REPLACED TACH/GEN 1G72 3U H3EU 20010919000092001091900009EU 2001 9 19 AC2A075790 120010507G771432005023 TACH GENERATOR BOLKMS105 BO105S 5626006EU NR 1 ENGINE ERRATIC H AC2AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 FS01826MB 771 PART IS INDICATIONS.N1 INDICATIONS WERE IRRATIC. REPLACED TACH/GEN. 1G72 3U H3EU 20010919000102001091900010EU 2001 9 19 AC2A075791 120010507G6340KDW021A WARNING SYSTEM BOLKMS105 BO105S 5626006EU ROTOR RPM MALFUNCTIONED H AC2AO OTHER N FALSE WARNING NRNOT REPORTED 1 FS01826MB 771 PART IS INDICATIONS. PILOT EXPERIENCED "HI RPM" LIGHT AND AUDIO DURING NORMAL OPERATION. REPLACED RPM WARNING BOX. 1G72 3U H3EU 20010919000112001091900011EU 2001 9 19 AC2A075792 120010507G624022021002 WARNING SYSTEM BOLKMS105 BO105S 5626006EU ROTOR RPM MALFUNCTIONED H AC2AO OTHER N FALSE WARNING CRCRUISE 1 FS01826MB 771 PART IS INDICATIONS.LOUD STATIC IN HEAD SET AND "HI AUDIO" INDICATIONS DURING NORMAL OPERATION. REPLACED RPM WARNING BOX 1G72 3U H3EU 20010919000122001091900012SW 2001 9 19 AC2A075793 120010507G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0117237597 51478 FOUND CRACKED AT REAR SEAM. REMOVED AND REPLACED STACK. 1G71 3U H2SW 20010919000132001091900013SW 2001 9 19 AC2A075795 120010512G3246206323017 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01172381199 51492 PART IS CORRODED. REMOVED,REPLACED FORWARD CROSS TUBE 1G71 3U H2SW 20010919000142001091900014SW 2001 9 19 AC2A075796 120010514G6410222312753103 BEARING 222016001131BELL 430 430 1182150SW T/R BLADE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH501 A1712 49037 BEARINGS ARE CRACKED. REPLACED BEARINGS WITH NEW. 1G72 3U RTH9SW 20010919000152001091900015SW 2001 9 19 AC2A075797 120010518G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0153702434 51249 FOUNDED CRACKED AT REAR SEAM. REMOVED AND REPLACED STACK. 1G71 3U H2SW 20010919000162001091900016NE 2001 9 19 AC2A075798 120010518G2435230811011 ARMATURE 23081002 SKRSKYS76 S76A 8143006NE SHORTED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01 643 PART IS CIRCUIT-SHORTED. REMOVED DEFECTIVE PART AND INSTALLED A SERVICABLE PART. 1G72 3U H1NE 20010919000172001091900017SW 2001 9 19 AC2A075799 120010529G74301064BH1436 SWITCH BELL 430 430 1182150SW IGNITION SHORTED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS01430CV263 49072 MICRO SWITCH FAILED TO ENGAGE ENGINE STARTER OR HOLDING COIL. REPLACED SWITCH. 1G72 3U RTH9SW 20010919000192001091900019SW 2001 9 19 AC2A075800 120010529G5210NAS5623R7A CAM FOLLOWER BELL 430 430 1182150SW DOOR CRACKED H AC2AO OTHER O OTHER NRNOT REPORTED 1 FS01430CV258 49072 BEARING RACE CRACKED. INSIDE OF BEARING FALLING APART.. REPLACED CAMFOLLOWER. 1G72 3U RTH9SW 20010919000202001091900020SW 2001 9 19 AC2A075801 120010607G6510430010124103 BUSHING BELL 430 430 1182150SW MAIN ROTOR WORN H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH2268 49037 PART IS WORN EXCESSIVELY. ALL EIGHT M/R DRIVE BUSHINGS ARE WORN BEYOND LIMITS ALLOWED IN BHT-430-CR&O-2. 1G72 3U RTH9SW 20010919000212001091900021SW 2001 9 19 AC2A075803 120010612G6230430310461101 BEARING BELL 430 430 1182150SW SWASHPLATE RATCHETING H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH 49037 WITH SWASHPLATE INSTALLED ON ACFT. BEARING FELT RATCHETY. BEARING WAS THE NEW UPDATED STLYE. REMOVED AND REPLACED BEARING. 1G72 3U RTH9SW 20010919000222001091900022SW 2001 9 19 AC2A075804 120010612G6220MS1652245 PIN BELL 430 430 1182150SW MAIN ROTOR BROKEN H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH3447 49037 FOUND SHEAR RESTRAINT LOOSE AND UPON DISASSEMBLY FOR INSP. FOUND PIN BROKEN. REPLACED BROKEN PIN AND WORN RESTRAINT. 1G72 3U RTH9SW 20010919000232001091900023SW 2001 9 19 AC2A075805 120010612G6220430310101107 RESTRAINT 430010100113BELL 430 430 1182150SW MAIN ROTOR LOOSE H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH585 A123 49037 FOUND LOOSE ON INSP. AND UPON DISASSEMBLY FOUND ROLL PIN BROKEN WHICH ALLOWED MOVEMENT IN CLAMP-UP. REPLACED RESTRAINT AND PIN. 1G72 3U RTH9SW 20010919000252001091900025NE 2001 9 19 AC2A075810 120010625G63207635109082105 CHIP DETECTOR SKRSKYS76 S76A 8143006NE M/R GEARBOX SHORTED H AC2AK NONE O OTHER ININSP/MAINT 1 FS017266F 760273 PART IS CIRCUIT-SHORTED. REPLACED WITH SERVICEABLE PART 1G72 3U H1NE 20010919000262001091900026SW 2001 9 19 AC2A075812 120010626G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01715CC1539 51380 EXHAUST IS CRACKED. REPLACED WITH NEW. 1G71 3U3 U H2SW E4CE 20010919000272001091900027GL 2001 9 19 AC2A075813 220010628G72616870032 FILTER ALLSN 250C 250C20B 03013GL ENGINE OIL DETERIORATED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01 PART IS DETERIORATED. THE OUTSIDE SCREEN IS EATEN AWAY EXPOSING THE MORE COARSE SCREEN. REPLACED FILTER ASSY. 3 U E4CE 20010919000302001091900030NE 2001 9 19 AC2A075814 220010702G753223005366 BLEED VALVE BELL 430 430 1182150SW ALLSN 250C 250C40B 03032NE ENGINE LOOSE H AC2AO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 FS01430CV374 49072 POWER ASSURANCE LOW NR 1 ENGINE. FOUND NR 1 ENGINE BLEED VALVE BODY BOLTS LOOSE. REPLACED WITH REPAIRED BLEED VALVE. 1G72 3U3 URTH9SW E1GL 20010919000312001091900031EU 2001 9 19 AC2A075815 120010709G63204638304001 SUN GEAR BOLKMS105 BO105S 5626006EU M/R GEARBOX FLAKING H AC2AK NONE O OTHER ININSP/MAINT 1 FS018775 673 775 DRIVE SIDE TOP CORNER OF TOOTH FLAKING. REPAIRED. 1G72 3U H3EU 20010919000352001091900035GL 2001 9 19 AC2A075817 220010712G723023056634 GEARSHAFT SKRSKYS76 S76A 8143006NE ALLSN 250C 250C* GL ENGINE WORN H AC2AK NONE O OTHER ININSP/MAINT 1 FS015403C702 760141 EXCESSIVE SPLINE WEAR ON AFT END. REPLACED WITH NEW. 1G72 3U3 U H1NE E4CE 20010919000372001091900037GL 2001 9 19 AC2A075818 220010712G723023031922 GEARSHAFT BELL 206 206B3 1181506SW ALLSN 250C 250C* GL SPUR GEAR WORN H AC2AK NONE O OTHER ININSP/MAINT 1 FS017131U962 4111 EXCESSIVELY WORN SPLINES. REPLACED WITH NEW. 1G71 3U3 U H2SW E4CE 20010919000382001091900038SW 2001 9 19 AC2A075819 120010728G2435230321827 STATOR 23081018 BELL 206 206L3 1182108SW STARTER GEN SHORTED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0117238 3794 51492 PART IS CIRCUIT-GROUNDED. REPLACED DEFECTIVE PART 1G71 3U H2SW 20010919000392001091900039SW 2001 9 19 AC2A075820 120010728G2435230811011 ARMATURE BELL 206 206L3 1182108SW STARTER GEN SHORTED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0117238 51492 PART IS CIRCUIT-GROUNDED. 1G71 3U H2SW 20010919000502001091900050NE 2001 9 19 AC2A075821 120010729G243523081002 STARTER GEN SKRSKYS76 S76A 8143006NE ENGINE LOOSE H AC2AK NONE O OTHER ININSP/MAINT 1 FS017266K9962 760283 PART IS LOOSE. DRIVE SHAFT BECAME LOOSE WHEN FRICTION RING DISINTAGRATED. REPLACED STARTER GENERATOR. 1G72 3U H1NE 20010919000642001091900064SW 2001 9 19 AC2A075822 120010808G7931222375077113 TRANSMITTER BELL 430 430 1182150SW ENGINE OIL MALFUNCTIONED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV535 49072 INDICATOR READS 12 PSI WITHOUT ENGINE WARNING. REPLACED WITH NEW TRANSMITTER. 1G72 3U RTH9SW 20010919000852001091900085SW 2001 9 19 AC2A075823 120010811G5311206033107121 FRAME BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS017159H9831 51397 FRAME IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919000872001091900087SW 2001 9 19 AC2A075824 120010811G5320206033107055 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS017159H9831 51397 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919000882001091900088SW 2001 9 19 AC2A075825 120010811G5320206033107051 CLIP BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS017159H9831 51397 CLIP IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919000892001091900089SW 2001 9 19 AC2A075826 120010811G5311206033107121 FRAME BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS017159J10161 51408 FRAME IS CRACKED. REPLACED WITH NEW PART 1G71 3U H2SW 20010919000902001091900090SW 2001 9 19 AC2A075827 120010811G5320206033107051 CLIP BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS017159J10161 51408 CLIP IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919000912001091900091SW 2001 9 19 AC2A075828 120010811G5320206033107055 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS017159J10161 51408 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919000922001091900092SW 2001 9 19 AC2A075829 120010811G5320206033107055 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01310798884 51526 PART IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919000932001091900093SW 2001 9 19 AC2A075830 120010811G5320206033107053 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01310798884 51526 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919000942001091900094SW 2001 9 19 AC2A075831 120010811G5320206033107056 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01310798884 51526 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919000952001091900095SW 2001 9 19 AC2A075832 120010811G5320206033107055 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01172378707 51478 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919000962001091900096SW 2001 9 19 AC2A075833 120010811G5320206033107056 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01172378707 51478 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919000972001091900097SW 2001 9 19 AC2A075834 120010811G5320206033107055 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01175928963 51535 STIFFENER IS CRACKED. REPAIRED WITH DER APPROVAL. 1G71 3U H2SW 20010919000982001091900098SW 2001 9 19 AC2A075835 120010811G5320206033107056 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01175928964 51535 STIFFENER IS CRACKED. REPAIRED WITH DER APPROVAL. 1G71 3U H2SW 20010919000992001091900099SW 2001 9 19 AC2A075836 120010813G7931222375077113 TRANSMITTER BELL 430 430 1182150SW ALLSN 250C 250C* GL ENGINE OIL MALFUNCTIONED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV534 49072 INDICATOR READS 10 PSI STACTICLY. REPLACED WITH NEW PART. 1G72 3U3 URTH9SW E4CE 20010919001002001091900100SW 2001 9 19 AC2A075837 120010814G5320206033107055 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01172388992 51492 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919001012001091900101SW 2001 9 19 AC2A075838 120010814G5320206033107056 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01172388992 51492 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919001022001091900102SW 2001 9 19 AC2A075839 120010814G5320206033107052 CLIP BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01172388992 51492 CLIP IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919001032001091900103GL 2001 9 19 AC2A075840 220010821G7200 ENGINE BELL 430 430 1182150SW ALLSN 250C 250C* GL NR 2 DAMAGED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV 49072 DURING A DAILY SERVICEABILITY CHECK THE NR 2 ENGINE WAS FOUND TO BE DAMAGED. SUSPECT CAUSE OF DAMAGE WAS THE FAILURE OF CAMLOC BLADE ASSY P/N: 40G2-1. THE ENGINE WAS DISASSEMBLED . THE COMPRESSOR WAS REMOVED AND DISASSEMBLED, THE TURBINE ASSY REMOVED. THE COMPRESSOR SCROLL WAS REMOVED AND SENT OUT FOR REPAIR. 1G72 3U3 URTH9SW E4CE 20010919001242001091900124SW 2001 9 19 AC2A075841 120010827G21502730502 VALVE BELL 430 430 1182150SW A/C PACK FAILED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV573 49072 VALVE POPS CIRCUIT BREAKER. REPLACED WITH NEW PART. 1G72 3U RTH9SW 20010919001252001091900125SW 2001 9 19 AC2A075842 120010828G21505861653 TURBINE BELL 430 430 1182150SW ALLSN 250C 250C* GL ENGINE FROZEN H K NONE O OTHER ININSP/MAINT 1 FS01430CV569 49072 COOLING TURBINE FROZEN. IT WOULD NOT TURN. REPLACED WITH NEW PART. 1G72 3U3 URTH9SW E4CE 20010919001262001091900126SW 2001 9 19 AC2A075845 120010904G6720 BEARING BELL 430 430 1182150SW P/C LINK WORN H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV600 49072 OUTBOARD BEARINGS WORN. REPLACED WITH NEW LINKS. 1G72 3U RTH9SW 20010919001272001091900127SW 2001 9 19 AC2A075846 120010904G21502730502 VALVE BELL 430 430 1182150SW A/C PACK FAILED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV600 49072 ECU BREAKER POPPED. REPLACED WITH NEW VALVE. 1G72 3U RTH9SW 20010919001282001091900128SW 2001 9 19 AC2A075847 120010904G71706854255 DRAIN VALVE BELL 430 430 1182150SW ENGINE LEAKING H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV600 49072 VALVE IS EXCESSIVELY LEAKING. 1G72 3U RTH9SW 20010919001292001091900129SW 2001 9 19 AC2A075848 120010904G2913222380009105 PUMP BELL 430 430 1182150SW HYD SYSTEM LEAKING H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV478 49072 LEAKING AT INPUT SEAL. REPLACED PUMP. 1G72 3U RTH9SW 20010919001322001091900132SW 2001 9 19 AC2A075849 120010905G6520222012714001 BEARING BELL 430 430 1182150SW TAIL ROTOR BRINELLED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV600 49072 INNER RACE WORN. IT WAS BRINNELING. REPLACED WITH NEW. 1G72 3U RTH9SW 20010919001362001091900136SW 2001 9 19 AC2A075852 120010905G6420222312753103 BEARING 222012701125BELL 430 430 1182150SW T/R BLADE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV600 A649 49072 CRACKED BEARINGS. REPLACED THE FOUR BEARINGS. 1G72 3U RTH9SW 20010919001392001091900139SW 2001 9 19 AC2A075853 120010905G6310214040812001 SEAL 222044002101BELL 430 430 1182150SW DEFORMED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV600 A218 49072 DURING 600 HOUR INSPECTION, DISASSY. COUPLING FOUND SEAL DEFORMED. REPLACED SEAL. 1G72 3U RTH9SW 20010919001422001091900142GL 2001 9 19 AC2A075854 220010905G732023065147 FUEL CONTROL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 1 ENGINE MALFUNCTIONED H AC2AO OTHER J WARNING INDICATION LDLANDING 1 FS015402T12214 760140 ENGINE WENT TO 40.6 PERCENT N1 UPON LANDING. REPLACED FUEL CONTROL. 1G72 3U3 U H1NE E1GL 20010919001442001091900144SW 2001 9 19 AC2A075855 120010908G5320206033107055 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS015370212265 51249 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919001462001091900146SW 2001 9 19 AC2A075856 120010908G5320206033107056 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS015370212265 51249 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919001472001091900147SW 2001 9 19 AC2A075857 120010908G5320206033107055 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS016533U9821 51439 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919001522001091900152SW 2001 9 19 AC2A075858 120010908G5320206033107056 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS016533U9821 51439 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919001532001091900153SW 2001 9 19 AC2A075859 120010908G5312206033107107B BULKHEAD BELL 206 206L3 1182108SW FUSELAGE CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS016533U9821 51439 BULKHEAD IS CORRODED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919001542001091900154SW 2001 9 19 AC2A075860 120010913G5311206032308003 FRAME BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS016533U9821 51439 FRAME IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919001552001091900155SW 2001 9 19 AC2A075861 120010913G5340206031329003 FITTING BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS016533U9821 51439 FITTING IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20010919001592001091900159SW 2001 9 19 AC2A075862 120010914G6220430310101105 SHEAR RESTRAINT BELL 430 430 1182150SW ROTOR SYSTEM DELAMINATED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CH3732 49037 SHEAR RESTRAINT DELAMINATED FROM CENTER PIN AND CAUSED DAMAGE TO CLAMP PLATE P/N 430-010-105-105. 1G72 3U RTH9SW 20010919001612001091900161SW 2001 9 19 AC2A075863 120010918G2432RG222 BATTERY BELL 206 206L3 1182108SW MAIN BATTERY WILL NOT TEST H AC2AK NONE L NO TEST ININSP/MAINT 1 FS0117237153 51478 BATTERY FAILED TEST. REPLACED BATTERY. CHARGED BATTERY. PERFORMED CAPACITY CHECK. BATTERY FAILED CAPACITY 1G71 3U H2SW 20011015000962001101500096SW 2001 10 15 AC2A076110 120010917G632040621 CLIP 430061829101BELL 430 430 1182150SW XMSN COWL CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV600 49072 PART IS CRACKED. SOME REMOVED TO REDUCE RISK OF ENG. F.O.D. R & R CLIPS 1G72 3U RTH9SW 20011015000982001101500098SW 2001 10 15 AC2A076111 120010917G1400214165 RECEPTACLE BELL 430 430 1182150SW UPPER FAIRING WORN H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV600 49072 PREMATURE WEAR R&R RECEPTICLE 1G72 3U RTH9SW 20011015001002001101500100SW 2001 10 15 AC2A076112 120010918G1400430031517135 STRAP BELL 430 430 1182150SW LT FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV600 49072 CRACKED IN BENT RADIUS. REMOVED AND REPLACED 1G72 3U RTH9SW 20011015001022001101500102SW 2001 10 15 AC2A076113 120010918G5411230069900150 FRAME BELL 430 430 1182150SW FIREWALL CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV600 49072 CRACKS IN FRAME. REMOVED AND REPLACED FRAME ASSY. 1G72 3U RTH9SW 20011015001032001101500103SW 2001 10 15 AC2A076114 120010919G2510222320823121 SEAT BELT BELL 430 430 1182150SW COCKPIT DAMAGED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV600 49072 SEAT BELT WAS UNTHREADING. REPLACED WITH NEW SEAT BELT. 1G72 3U RTH9SW 20011015001052001101500105SW 2001 10 15 AC2A076115 120010919G6310222060084101 PRESSURE SWITCH BELL 430 430 1182150SW M/R GEARBOX INOPERATIVE H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV600 49072 PRESSURE SWITCH IS INOPERABLE. REPLACED WITH NEW SWITCH. 1G72 3U RTH9SW 20011015001062001101500106SW 2001 10 15 AC2A076116 120010924G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01715CC306 51380 CRACKED. REPLACED WITH NEW EXHAUST STACK. 1G71 3U H2SW 20011015001072001101500107SW 2001 10 15 AC2A076117 120011001G2520222020742133 CUSHION BELL 430 430 1182150SW CABIN SEAT DAMAGED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV670 49072 FOAM WAS BUSTED AND SEPARATED FROM FRAME. REPLACED SEAT CUSHION. 1G72 3U RTH9SW 20020123000202002012300020SW 2002 1 23 AC2A077049 120011013G3213206323017 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED H AC2AK NONE O OTHER ININSP/MAINT 1 FS017159H10143 51397 THE MANUFACTURED DATE IS JAN. 2001 WITH 619 HOURS. TWO SPOTS OF CORROSION WERE FOUND UNDER THE SUPPORT CLAMPS. THE CROSSTUBE WAS REPLACED. 1G71 3U H2SW 20020123000212002012300021SW 2002 1 23 AC2A077050 120011015G21203136171 SOLENOID BELL 430 430 1182150SW DIVERTER VALVE STUCK H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV694 49072 DIVERTER VALVE NOT OPENING OR CLOSING. TOO MUCH COLD AIR COMING OUT OF LOWER VENTS. REPLACED WITH NEW SOLENOID. IT FIXED PROBLEM. 1G72 3U RTH9SW 20020123000222002012300022SW 2002 1 23 AC2A077051 120011022G5320206033107055 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01715CC10225 51380 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20020123000232002012300023SW 2002 1 23 AC2A077052 120011022G5320206033107053 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01715CC10225 51380 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20020123000242002012300024SW 2002 1 23 AC2A077053 120011022G5320206033107056 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01715CC10225 51380 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20020123000252002012300025SW 2002 1 23 AC2A077054 120011022G5320206033107054 STIFFENER BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01715CC10225 51380 STIFFENER IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20020123000262002012300026SW 2002 1 23 AC2A077055 120011022G5320206033107052 CLIP BELL 206 206L3 1182108SW FUSELAGE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01715CC10225 51380 CLIP IS CRACKED. REPLACED WITH NEW PART. 1G71 3U H2SW 20020123000272002012300027SW 2002 1 23 AC2A077056 120011024G3212206073926103 VALVE BELL 206 206L3 1182108SW MLG FAILED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0117237234 51478 VAVLE FAILING AFTER ONLY 234 HOURS. 1G71 3U H2SW 20020123000282002012300028SW 2002 1 23 AC2A077057 120011024G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS017159J712 51408 EXHAUST STACK CRACKED. REPLACED WITH NEW . 1G71 3U H2SW 20020123000292002012300029SW 2002 1 23 AC2A077058 120011024G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS0153702312 51249 EXHAUST STACK CRACKED. REPLACED WITH SERVICEABLE. 1G71 3U H2SW 20020123000352002012300035SW 2002 1 23 AC2A077536 120011205G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01715CC205 51380 EXHAUST STACK CRACKED. REPLACED WITH NEW. 1G71 3U H2SW 20020123000362002012300036SW 2002 1 23 AC2A077537 120011205G3040222325001027 ARM BELL 430 430 1182150SW WINDSHILD WIPER BROKEN H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV804 49072 WINDSHIELD WIPER GUIDE ARM IS BROKEN. REPLACED WITH NEW PART. 1G72 3U RTH9SW 20020123000392002012300039SW 2002 1 23 AC2A077539 120011211G750023056648 TUBE BELL 430 430 1182150SW BLEED AIR CHAFED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV205 49072 ENGINE COWL ASSY P/N: 430-061-804-101 FORWARD HINGE P/N: 230-061-808-101 IS RUBBING ON BLEED AIR TUBE P/N: 23056648 WHEN COWLING IS OPENED. REPLACED TUBE. PROBLEM WILL CONTINUE DUE TO DESIGN OF COWLING HINGE. 1G72 3U RTH9SW 20020123000402002012300040SW 2002 1 23 AC2A077540 120011211G6730065001620200 SERVO BELL 430 430 1182150SW MAIN ROTOR YAW MALFUNCTIONED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV943 49072 WHEN FD IS COUPLED IN HDG & ALT THE A/C GOES INTO A CLIMBING RIGHT TURN WITH FULL LEFT PEDAL APPLIED. REPLACED WITH NEW YAW SERVO. 1G72 3U RTH9SW 20020123000422002012300042SW 2002 1 23 AC2A077541 120011226G3040222325001028 ARM BELL 430 430 1182150SW WINDSHIED WIPER BROKEN H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV953 49072 LOWER MOUNTING POINT BROKEN. THE MATERIAL THAT THIS PART IS MADE OF IS VERY SUSEPTIBLE TO CORROSION. CORROSION CAUSED THIS PART TO FAIL. UPPER ROD END CORRODED VERY EASILY ALSO. REPLACED WITH NEW PART. 1G72 3U RTH9SW 20020123000432002012300043SW 2002 1 23 AC2A077542 120011226G6410222312753103 BEARING 222016001131BELL 430 430 1182150SW T/R BLADE CRACKED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01430CV281 A1901 49072 TAIL ROTOR BLADE BEARINGS WERE CRACKED. REPLACED TWO BEARINGS. 1G72 3U RTH9SW 20020123000442002012300044NE 2002 1 23 AC2A077543 120011226G760023065125 GOVERNOR SKRSKYS76 S76 8143010NE ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED H AC2AK NONE O OTHER ININSP/MAINT 1 FS01 11057 890384 GOVERNOR VERY SENSITIVE, COULD NOT MATCH TORQUES & SHAFT IS RACHETY. REPLACED WITH SERVICEABLE PART. 1G72 3U3 U H1NE E1GL 20020123000452002012300045NE 2002 1 23 AC2A077544 120011227G792128E252 THERMOSTAT SKRSKYS76 S76A 8143006NE OIL COOLER INACCURATE H AC2AO OTHER N FALSE WARNING CRCRUISE 1 FS015401G 760137 HIGH ENGINE OIL TEMPERATURE IN FLIGHT. REPLACED THERMOSTAT. CURED PROBLEM. 1G72 3U H1NE 20010823000842001082300084CE 2001 8 23 AMB20011 120010814G324422X80010 TIRE CESSNA500 550 2076604CE MLG FAILED B K NONE O OTHER ININSP/MAINT 1 SW17753CC 5500109 DURING A DAILY INSPECTION THE SIDE WALL WAS FOUND TORN OUT WHERE THE SIDE WALL AND TIRE TRED ARE BONDED TOGOTHER. THERE IS ANOTHER AREA APROX. 6 INCHES AWAY FROM THIS TEAR, WHERE YOU CAN SEE THAT THE RUBBER IS ALSO STARTING TO SEPERATE. THE INNER AREA OF THE TEAR HAS SOFT RUBBBER COMMING OUT IT HAS THE CONTIENCY AND FEEL OF RUBBER THAT HAS NOT FULLY CURED. THIS TIRE WAS PULLED FROM SERVICE AND A REPLACEMENT INSTALLED. WE ARE GOING TO SUBMIT THIS TO GOOD YEAR FOR THEM TO EVALUATE. 1L72 4F A22CE 20010111059772001011105977NM 2001 1 11 ANCF200100004 120010107G2751 CONNECTOR BOEING767 767259 1385136NM PWA 4056 PW4056 NE TE FLAPS DIRTY W ANCFO OTHER O OTHER CLCLIMB 1 SW99986AN 24835 AFTER T/O BOTH FLAP POINTERS WERE ON 1° WITH THE FLAP LEVER IN UP POSITION, AIRCRAFT RETURNED TO MEX. CLEANED CONNECTORS AT FSEU PERFORMED BITE TEST AND OPERATIONAL TEST IAW AMM 27-58-05 TEST OK, COULD NOT DUPLICATED FAULT, FLAP/SLAT VISUAL CHECK OK. 2L72 4F4 FRTA1NM E24NE 20010726002482001072600248NM 2001 7 26 ANCF200100010 120010609G2824 VALVE BOEING767 767259 1385136NM FUEL SYSTEM FAILED W ANCFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO23986AN 24835 DURING CRUISE 1:30 HOURS AFTER T/O FUEL CROSSFEED VALVE LIGHT REMAINED ILLUMINATED WHEN VALVE SELECTED OPEN. EICAS MESSAGE FUEL CROSSFEED DISPLAYED. AIRCRAFT RETURNED TO MAD. PERFORMED PROCEDURE IAW FIM 28-22-00/101 FIG 108 BLOCKS 1, 2 AND 14. REPLACED FUEL CROSSFEED VALVE, PERFORMED TEST WITH SATISFACTORY RESULTS. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA1NM 20010802002702001080200270NE 2001 8 2 AO1R200100001 220010717G7230794909 COMPRESSOR WHEEL PWA JT9 JT9D* NE ENGINE FRETTED B K NONE W INADEQUATE Q C ININSP/MAINT 1 SW99 16393 695739 EXCESSIVE FRETTING DAMAGE ON BLADE SLOT PRESSURE FACES BEYOND LIMITS IN ACCORDANCE WITH JT9D OHM P/N 646028 SECTION 72-35-04 REV 109 FRETTING CHECKS 0.0024". REPAIR ORDER RECEIVED FROM P&W SMMO REQUESTED INSPECT TO THE LATEST REVISION OF E/M 646028 DIMENSIONAL INSPECT PART AND REPORT FINDINGS TO JEFF FISCUS. PART WAS RECEIVED IN OVERHAUL CONDITION. 4 F E20EA 20010802002712001080200271NE 2001 8 2 AO1R200100002 220010717G7230500110801 COMPRESSOR WHEEL PWA JT9 JT9D* NE ENGINE FRETTED B K NONE W INADEQUATE Q C ININSP/MAINT 1 SW99 31003 715441 EXCESSIVE FRETTING DAMAGE ON BLADE SLOT PRESSURE FACES BEYOND LIMITS IN ACCORDANCE WITH JT9D OHM P/N 646028 SECTION 72-35-04 REV 109 FRETTING CHECKS 0.0024". FRONT SNAP AND SHOULDER ARE OVERSIZE 0.002", REAR SNAP AND SHOULDER ARE OVERSIZE 0.002" AND OUT OF ROUND 0.004". REPAIR ORDER RECEIVED FROM P&W SMMO REQUESTED INSPECT TO THE LATEST REVISION OF E/M 646028 DIMENSIONAL INSPECT PART AND REPORT FINDINGS TO JEFF FISCUS. PART WAS RECEIVED IN OVERHAUL CONDITION. 4 F E20EA 20010402000812001040200081NE 2001 4 2 AU010001 220010102G7310226311001 PIPE BAC 146 146100A 1500260EU LYC ALF502ALF502R5 41580NE ENGINE FUEL CHAFED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE FUEL PIPE FROM FLOW DIVIDED TO FUEL MANIFOLD CHAFED ON COMBUSTOR HOUSING. 2H74 4F4 FRTA49EU E6NE 20010402000822001040200082CE 2001 4 2 AU010002 120010103G32215842000211 TRUNNION CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C87 GL NLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR TRUNNION PINS CRACKED. FOUND DURING INSPECTION IAW CESSNA SB MEB88-5R2. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010402000832001040200083CE 2001 4 2 AU010003 120010102G323108411066 ARM CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL MLG DOOR CRACKED W O OTHER J WARNING INDICATION LDLANDING 1 AUS (AUS) RT MAIN LANDING GEAR INNER DOOR BELLCRANK IDLER ARM CRACKED. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010402000842001040200084 2001 4 2 AU010004 420010104G2211065006401 COMPUTER REIMS 406 F406 EU PWA PT6 PT6A112 52043NE MCAULY3G34C73GFR34C701 GL AUTOPILOT FAULTY W O OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 AUS 3823 (AUS) AUTOPILOT COMPUTER SUSPECT FAULTY. 1L72 3T3 TRTA54EU E4EA 5 CP60GL 20010402002692001040200269EA 2001 4 2 AU010005 120010107G5230 HANDLE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE CARGO DOOR MALFUNCTIONED W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) CARGO DOOR MASTER CAUTION LIGHT ILLUMINATED. INVESTIGATION FOUNDTHE CARGO DOOR HANDLE PARTIALLY RELEASED. A FUNCTIONAL CHECK OF THE DOOR LATCHING SYSTEM COULD FIND NO FAULT. SUSPECT THAT THEHANDLE WAS INCORRECTLY STOWED. 2L72 4F4 FRTA21EA E15NE 20010402000852001040200085CE 2001 4 2 AU010006 120010103G554010164001419 FITTING BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE HARTZLHCD4N3HCD4N3A GL RUDDER CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RUDDER CENTER HINGE ASSEMBLY ATTACHMENT FITTING CORRODED. 1L72 4T4 T A24CE E4EA 5 CSTC 20010402000862001040200086SO 2001 4 2 AU010007 120010106G3230 DOWNLOCK PIPER PA34 PA34200 7103405SO LYC O360 IO360C1E6 41514EA HARTZLHCC2Y HCC2YK2 GL MLG CONTAMINATED W O OTHER J WARNING INDICATION LDLANDING 1 AUS (AUS) LT MAIN LANDING GEAR DOWNLOCK ARM JAMMED BY A STONE PREVENTING LANDING GEAR FROM CORRECTLY LOCKING IN THE DOWN POSITION. 1L72 3O3 O A7SO 1E10 5 CP920 20010402000872001040200087SO 2001 4 2 AU010008 220010103G8530631996 RETAINER CESSNA172 R172K 2072431CE CONT O360 IO360HB 17025SO MCAULY2A34C 2A34C203 GL ENGINE CYLINDER CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 3 CYLINDER ROCKER HAT REMOVED TO REPAIR OIL LEAK. THE ROCKER PIN RETAINER WAS FOUND TO CRACKED. ON FURTHER INSPECTION OTHER ROCKER PIN RETAINERS SHOWED SIGNS OF INCIPIENT FAILURE. 1H71 3O3 O 3A17 E1CE 5 CP3EA 20010402000882001040200088EU 2001 4 2 AU010009 220010104G73210164168190 FUEL CONTROL SNIAS AS332 AS332L 8680809EU TMECA MAKILAMAKILA1A 60040EU NR 1 ENGINE MALFUNCTIONED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AUS (AUS) NR 1 ENGINE FUEL CONTROL UNIT FAULTY. INVESTIGATION FOUND THE PPNG OF THE FCU INTERNAL CIRCUIT TO BE OPEN CIRCUITED. 2G72 4U4 U H4EU E12NE 20010402000892001040200089WP 2001 4 2 AU010010 220010110G726131080801 PIPE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP ROTOL R321 R321482F8 GL RT ENGINE OIL CHAFED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) RT ENGINE OIL PIPE LEAKING DUE TO CONTINUED CHAFING WITH ANOTHERPIPE. 2L72 4T4 TRTA8SW E4WE 6 CP61GL 20010402002702001040200270CE 2001 4 2 AU010011 120010110G28974410174 WIRE CESSNA C441 CESSNA441 441 2076020CE GARRTTTPE331TPE331* 01514WP HARTZLHCB3T HCB3TN5 GL BOOST PUMP CHAFED W K NONE O OTHER ININSP/MAINT 1 AUS 4410174 (AUS) LT FUEL TANK BOOST PUMP WIRING CHAFED THROUGH TO BARE WIRE. 1L72 3T3 TRTA28CE E2WE 6 CP15EA 20010402000902001040200090 2001 4 2 AU010012 420010103G25657A146723 SLIDE BOEING747 747438 NM RROYCERB211 RB211524G19 NE PAX DOOR DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS 12456 (AUS) NR 4 LT MAIN DOOR ESCAPE SLIDE TORN. 2L74 4F4 FRTA20WE E30NE 20010402000912001040200091NM 2001 4 2 AU010013 120010109G2510 SEAT BACK BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU COCKPIT BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) OBSERVERS SEAT BACK REST SEPARATED FROM SEAT BASE DUE TO A BROKEN BRACKET. 2L72 4F4 FRTA16WE E21EU 20010402000922001040200092NM 2001 4 2 AU010014 120010109G78301275084 ARM RROYCE RB211524G BOEING747 747438 NM RROYCERB211 RB211524G19 NE THRUST REVERSER DAMAGED W K NONE J WARNING INDICATION ININSP/MAINT 1 AUS 31016 (AUS) NR 2 ENGINE THRUST REVERSER COWL POSITION (TRCP) RESOLVER ARM DISCONNECTED AT ADJUSTMENT TURNBUCKLE AND ATTACHED BY ONLY ONE THREAD AT THE RESOLVER. SAFETY WASHER LOCKTABS PARTIALLY BENT AND RESOLVER APPEARS TO HAVE SUFFERED CONTACT DAMAGE. 2L74 4F4 FRTA20WE E30NE 20010402000932001040200093NM 2001 4 2 AU010015 120010109G2823737M28500011 VALVE BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU FUEL SELECTOR FAILED W O OTHER O OTHER NRNOT REPORTED 1 AUS 3161 (AUS) NR 1 ENGINE FUEL SHUTOFF VALVE FAILED IN THE CLOSED POSITION. 2L72 4F4 FRTA16WE E21EU 20010402000942001040200094NM 2001 4 2 AU010016 120010110G3260841005 PSEU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE MLG FAULTY W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) PROXIMITY SENSE ELECTRICAL UNIT (PSEU) FAULTY. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010402000952001040200095SO 2001 4 2 AU010017 120010109G79202W127984S190 HOSE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE OIL DETERIORATED W O OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LDLANDING 1 AUS (AUS) RT ENGINE TURBOCHARGER OIL RETURN HOSE DETERIORATED AND LEAKING.HOSE FAILED PRESSURE TESTING. THE HOSE HAD BEEN AFFECTED BY THE HEAT FROM THE TURBOCHARGER. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010402000972001040200097EU 2001 4 2 AU010018 120010111G2760 BUSHING FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU DRAG CONTROL CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) SPEED BRAKE CABLE INPUT QUADRANT CORRODED. THE FOLLOWING ITEMSWERE FOUND DETERIORATED: GROOVE OF PULLEY ASSEMBLY. WEB ADJACENT TO STOP PIN HOLE OF BRACKET. INTERNAL SPLINE OF LEVER. EXTERNAL SPLINE ON SHAFT AND BUSHING. BEARING AND FOUND CORRODED AND ROUGH TO ROTATE 2L72 4F4 FRTA20EU E2EU 20010402000982001040200098CE 2001 4 2 AU010019 120010104G323051420025 DRAG BRACE CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C87 GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR DRAG BRACE CRACKED IN AREA ADJACENT TO THE ACTUATOR ATTACHMENT LUG. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010402000992001040200099CE 2001 4 2 AU010020 120010112G32215842000211 PIN CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL NLG TRUNNION CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR TRUNNION PIN CRACKED. FOUND DURING INSPECTION IAW CESSNA SB CQB00-3. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20010402001002001040200100CE 2001 4 2 AU010021 120010103G52101313232C12 PIN BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE HARTZLHCB3T HCB3TN3 GL PAX DOOR SHEARED W O OTHER O OTHER CRCRUISE 1 AUS (AUS) DOOR HOOK CLEVIS PIN SHEARED. DOOR DIFFICULT TO OPEN. 1L72 4T4 T A24CE E4EA 6 CP15EA 20010402001012001040200101EU 2001 4 2 AU010022 120010112G291024Q2395 HOSE BRAERO748 HS7482B 1500248EU RROYCEDART DART5322L 54509EU HYDRAULIC SYS CRACKED W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) RT GEARBOX MOUNTED HYDRAULIC PUMP OUTLET HOSE END FITTING CRACKED ON FLARED OLIVE. 2L72 3T4 T A24EU E297 20010402001022001040200102SO 2001 4 2 AU010023 120010115G323040336000 DRAG BRACE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL NLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR DRAG BRACE ACTUATOR ATTACHMENT LUGS CRACKED. FOUND USING VISUAL AND CONFIRMED USING NDI. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010402001032001040200103EU 2001 4 2 AU010024 120010116G3213200877682 PIN BAC 146 146100A 1500260EU LYC ALF502ALF502R5 41580NE RT MLG FRACTURED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR WHEEL LEVER TO OLEO ATTACHMENT PIN FRACTURED AND MIGRATED. 2H74 4F4 FRTA49EU E6NE 20010402001042001040200104GL 2001 4 2 AU010025 220010112G72309380M28P05 TURBINE WHEEL GE GE CF6 CF680C2* GL ENGINE OUT OF TOLERANCEW K NONE O OTHER ININSP/MAINT 1 AUS 6513 (AUS) HIGH PRESSURE COMPRESSOR ROTOR SPOOL NR 3 STAGE TO NR 9 STAGE OUTSIDE OF LIMITS AS PER AD/CF6/41, AD/CF6-43, FAA AD FAD 99-24-15 AND FAA AD FAD 2000-16-12. 4 F E23EA 20010402001052001040200105NM 2001 4 2 AU010026 120010112G80119702038 CLAMP GE CF680C2 BOEING767 767338 1385151NM GE CF6 CF680C2* GL STARTER FAILED W O OTHER J WARNING INDICATION CLCLIMB 1 AUS 4159 9702038 (AUS) RT ENGINE STARTER CLAMP BROKEN AND STARTER LOOSE. SEAL CUT. 2L72 4F4 FRTA1NM E23EA 20010402001062001040200106NM 2001 4 2 AU010027 120010111G2910AV13J5147 VALVE BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU HYDRAULIC SYS SEIZED W K NONE O OTHER ININSP/MAINT 1 AUS 25973 (AUS) HYDRAULIC STANDBY MODULE SHUTOFF VALVE SEIZED. 2L72 4F4 FRTA16WE E21EU 20010402001072001040200107NE 2001 4 2 AU010028 220010103G8500 ENGINE DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE NACELLE SEIZED W A UNSCHED LANDING EY VIBRATION/BUFFET ENGINE STOPPAGE CLCLIMB 1 AUS (AUS) ENGINE RAN ROUGH AND THEN SEIZED. LIMITED INFORMATION PROVIDED. 1H71 3R3 R A806 5E1 20010402001082001040200108EA 2001 4 2 AU010029 220010116G731025765311 FLOW DIVIDER CESSNA182 182S 2072701CE LYC O540 IO540AB1A5 EA MCAULY3D36C B3D36C431 GL FUEL DIST CORRODED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AUS 92 (AUS) ENGINE FUEL FLOW DIVIDED CORRODED. PARTICLES OF CORROSION BLOCKING FUEL INJECTORS. AIRCRAFT HAD BEEN CONTAMINATED WITH EDAAND DECONTAMINATED IAW AD/GEN/80 AND MANUFACTURERS INSTRUCTIONS. 1H71 3O3 ONT3A13 1E4 5 C 20010402001092001040200109SO 2001 4 2 AU010030 120010113G2150MS21346221 SWITCH EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE AIR CONDITIONINGFAULTY W O OTHER J WARNING INDICATION CRCRUISE 1 AUS (AUS) AIR CONDITIONING SYSTEM CROSS BLEED VALVE SWITCH FAULTY. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010402001102001040200110NM 2001 4 2 AU010031 120010104G2530CA16371 CONNECTOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE GALLEY DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LIQUID HEATER CONNECTORS DAMAGED DUE TO OVERHEATING. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010402001112001040200111NM 2001 4 2 AU010032 120010104G2530CA16731 CONNECTOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE GALLEY DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LIQUID HEATER CONNECTORS DAMAGED DUE TO OVERHEATING. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010402001122001040200112NM 2001 4 2 AU010033 120010114G7830 DOOR RROYCE RB211524D4 BOEING747 747338 NM RROYCERB211 RB211524D41954555NE THRUST REVERSER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 1 ENGINE BLOCKER PARTIALLY MISSING. DAMAGE TO CORONA AND COLD STREAM DUCT AT 10 OCLOCK POSITION. 2L72 4F4 FRTA20WE E12EU 20010402001132001040200113 2001 4 2 AU010034 420010115G2330311038 CONTROL BOX BOEING767 767338 1385151NM GE CF6 CF680C2* GL ENTERTAIN SYS FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 311038 (AUS) SEAT 5A HARNESS PLUG TO SEAT ELECTRONICS BOX ARCING. ARCING CONTINUED WITH PLUG DISCONNECTED. NO CIRCUIT BREAKERS POPPED. 2L72 4F4 FRTA1NM E23EA 20010402001142001040200114NM 2001 4 2 AU010035 120010116G7830 DOOR RROYCE RB211524G BOEING747 747438 NM RROYCERB211 RB211524G19 NE THRUST REVERSER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 1 ENGINE THRUST REVERSER NR 9 BLOCKER DOOR PARTLY MISSING. DAMAGE TO CORONA WITH A 76.2MM BY 25.4MM (3IN BY 1IN) HOLE ADJACENT TO BLOCKER DOOR POSITION. DAMAGE ALSO TO LT COMBUSTION FAIRING AND INTEGRATED NOZZLE ASSEMBLY. 2L74 4F4 FRTA20WE E30NE 20010402001412001040200141SO 2001 4 2 AU010036 120010116G27521202001 ACTUATOR PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL TE FLAP WORN W O OTHER J WARNING INDICATION LDLANDING 1 AUS (AUS) FLAP MOTOR BRUSHES AND COMMUTATOR WORN. MOTOR INOPERATIVE. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010404000012001040400001NE 2001 4 4 AU010038 320010111G61117922141 TAPE HAMSTD SFA13MIOA DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE PROPELLER BLADE LOOSE W O OTHER O OTHER CLCLIMB 1 AUS (AUS) LT PROPELLER BLADE LEADING EDGE TAPE LOOSE ON ONE BLADE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010402001212001040200121EU 2001 4 2 AU010039 120010116G2770A78300401 LOCK FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU ELEVATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELEVATOR GUSTLOCK HOUSING MOUNTING LUGS CRACKED. FOUND DURING INSPECTION IAW AD/F28/72 AMDT1. SUSPECT CAUSED BY LOOSE MOUNT.BOLTS. 2L72 4F4 FRTA20EU E2EU 20010402001222001040200122CE 2001 4 2 AU010040 120010116G32215842000211 PIN CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL NLG TRUNNION CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR TRUNNION PIN CRACKED. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20010402001232001040200123NE 2001 4 2 AU010041 220010107G731021631001 PIPE BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE FUEL DIST WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 3 ENGINE LT PRIMARY FUEL PIPE CHAFING ON COMBUSTOR CASE IN AREA OF THE FORWARD FLANGE OF THE CUSTOMER BLEED FLANGE. 2H74 4F4 FRTA49EU E6NE 20010402001242001040200124EU 2001 4 2 AU010042 120010104G7603 CABLE LYC IO540K1B5 BNORM BN2 BN2A26 1520226EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL POWER LEVER LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE THROTTLE CABLE OUTER CONDUIT DISCONNECTED AT FIREWALL. THE NUT SECURING THE CONDUIT HAD NO LOCKWIRE. 1H72 3O3 O A17EU 1E4 5 CP920 20010402001252001040200125EU 2001 4 2 AU010043 120010105G7602 CABLE LYC IO540K1B5 BNORM BN2 BN2A26 1520226EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL MIXTURE CONTROL MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE MIXTURE CONTROL INNER CABLE ONLY ENGAGED IN THE ENGINE CONTROL END BY APPROXIMATELY 1.5 TURNS. 1H72 3O3 O A17EU 1E4 5 CP920 20010402001262001040200126EU 2001 4 2 AU010044 120010110G6120 CONTROL CABLE HARTZL HCC2YK2 BNORM BN2 BN2A26 1520226EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL PROP CONTROL SEIZED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT PROPELLER CSU CONTROL CABLE OUTER CONDUIT WORN THROUGH WITHTHE INNER CABLE CATCHING ON THE WORN AREA. CONTROL SEIZED. 1H72 3O3 O A17EU 1E4 5 CP920 20010402001272001040200127NE 2001 4 2 AU010045 220010117G72603022375 SEAL PILATSPC12 PC12 7090550EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL ENGINE FAILED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) NR 4 ACCESSORY DRIVE SEAL MIGRATED OUT OF SEAL CARRIER PNO 3007737 ALLOWING APPROXIMATELY 3.5 LITRES OF OIL TO LEAK FROM THE ENGINE DRIVEN LOW PRESSURE FUEL PUMP DRIVE SPLINE DRAIN. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010402001282001040200128SW 2001 4 2 AU010046 120010122G3233MS28775116 SEAL EA1568 GULSTM500 500S 0141107SW LYC O540 IO540E1B5 41532EA HARTZLHCA3V HCA3VK2 GL MLG ACTUATOR WORN W O OTHER K FLUID LOSS DEDESCENT 1 AUS 2020 (AUS) MAIN LANDING GEAR RETRACTION ACTUATOR SEAL WORN. 1H72 3O3 O 6A1 1E4 5 CP6EA 20010402001292001040200129SO 2001 4 2 AU010047 220010111G7314 SEAL CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO FUEL PUMP FAILED W C ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LT ENGINE DRIVEN FUEL PUMP SEAL FAILED. FUEL LEAKING FROM VENT. 1L72 3O3 O A7CE E8CE 20010402001302001040200130EU 2001 4 2 AU010048 120010108G5711 SPAR BAC 146 146300A 1500267EU LYC ALF502ALF502R5 41580NE LT & RT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT WING FORWARD AND AFT SPARS CONTAINED PITTING CORROSIONIN AREAS OUTBOARD OF RIB NR 13. HEAVY STAINING FOUND IN WING TANKS SUSPECTED FROM CLADOSPORIUM RESINAE. 2H74 4F4 FRTA49EU E6NE 20010402001312001040200131NM 2001 4 2 AU010049 120010122G324226056623 BRAKE BOEING747 747338 NM RROYCERB211 RB211524D41954555NE LT WING MLG FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 7020 (AUS) LT FORWARD WING LANDING GEAR NR 2 POSITION BRAKE FAILED. 2L72 4F4 FRTA20WE E12EU 20010402001322001040200132NM 2001 4 2 AU010050 120010119G2432401767 BATTERY BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU BATTERY BAY DISCHARGED W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION NRNOT REPORTED 1 AUS 4 (AUS) MAIN AIRCRAFT BATTERY DISCHARGED. 2L72 4F4 FRTA16WE E21EU 20010402001332001040200133EU 2001 4 2 AU010051 120010118G7722897476 COMPENSATOR BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP ROTOL R333 R333482F12 GL EGT/TIT INDICATOOUT OF TOLERANCEW C ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AUS (AUS) LT ENGINE EGT COMPENSATOR OUT OF TOLERANCE. 2L72 4T4 TRTA56EU E4WE 6 CP61GL 20010402001342001040200134NM 2001 4 2 AU010052 120010123G2400S010488308 RELAY DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE ELECTRICAL SEPARATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RELAY BASE SEPARATED AT PRODUCTION BREAK ALLOWING THE RELAY CONTACTS TO COME AWAY FROM THE RELAY. BASE MANUFACTURER CLOVER. THE RELAYS ARE USED IN NUMEROUS AREAS. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010402001352001040200135NE 2001 4 2 AU010053 220010118G73218063023 FUEL CONTROL STBROSSD3 SD360 8100606EU PWA PT6 PT6A67R 52043NE HARTZLHCA6A HCA6A3 NE RT ENGINE FAULTY W O OTHER J WARNING INDICATION LDLANDING 1 AUS (AUS) RT ENGINE FUEL CONTROL UNIT FAULTY. 2H72 4T4 T A41EU E26NE 6 CP14NE 20010402001362001040200136WP 2001 4 2 AU010054 120010121G3234630294W PISTON LKHEED1049 C121C 5262118WP WRIGHTR3350 R3350* 67040EA HAMSTD43E 43E60 NE MLG STRUT BROKEN W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LANDING GEAR SELECTOR VALVE PISTONS (2OFF4) BROKEN ACROSS SHANK IN AN O-RING SEAL GROOVE. BROKEN PISTON JAMMED IN PORT. 2L74 4R4 R 6A5 E272 6 CP871 20010402001372001040200137SO 2001 4 2 AU010055 220010125G8520632043 CONNECTING ROD CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3AF34C3AF34C74 GL ENGINE FAILED W C ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 AUS 847 (AUS) LT ENGINE NR 5 CYLINDER CONNECTING ROD SEPARATED FROM CRANKSHAFT AND PENETRATED THE CRANKCASE. 1L72 3O3 O A25CE E7CE 5 CP22EA 20010402001382001040200138EU 2001 4 2 AU010056 120010128G57537257830022 FITTING 7257800504 SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R390 R3904123F27 NE TE FLAP CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 1114 (AUS) RT FLAP ASSEMBLY OUTBOARD FITTING AFT ATTACHMENT LUG CRACKED. CRACK APPEARS TO HAVE EMANATED FROM THE BOLT/BUSHING HOLE AND PROGRESSED THROUGH ONE SIDE OF THE LUG. FOUND DURING VISUAL INSPECTION IAW SB-340-57-037. 2L72 4T4 TRTA52EU E8NE 6 CP31NE 20010402001392001040200139EA 2001 4 2 AU010057 220010119G853017C21191 KEY ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA ENGINE BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 5 CYLINDER EXHAUST VALVE KEY BROKEN WITH DAMAGE TO TAPPET AND SOCKET. SUSPECT TAPPET DAMAGED AT MANUFACTURE CAUSING INCORRECT VALVE CLEARANCE. 1G71 3O3 O H11NM E295 20010402001402001040200140SW 2001 4 2 AU010058 120010127G2133A6009 ADAPTER SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UA 01514WP MCAULY4HFR344HFR34C652 NE PRESSURE REG FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AUS (AUS) CABIN PRESSURISATION SYSTEM OUTFLOW VALVE SUCTION FITTING FAILED. 2L72 4T4 TRTA5SW E4WE 6 C3PNE 20010402002712001040200271SW 2001 4 2 AU010059 120010123G65102006505008 BOLT BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE TAIL ROTOR DRIVEWORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAIL ROTOR DRIVESHAFT TO TAIL ROTOR GEARBOX INPUT COUPLING BOLT SEPARATED. MARKS ON BOLT INDICATE THAT IT HAD BEEN LOOSE FOR SOME TIME. 1G72 4U4 U H4SW E22EA 20010402002722001040200272SW 2001 4 2 AU010060 120010113G733442D218 PRESSURE SWITCH BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE FUEL PRESSURE LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 2 ENGINE FUEL PRESSURE SWITCH LEAKING FUEL FROM SOLDERED JOINT AT BASE OF CONNECTOR PLUG CONNECTOR. 1G72 4U4 U H4SW E22EA 20010402002732001040200273SW 2001 4 2 AU010061 120010113G733442D218 PRESSURE SWITCH BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE FUEL PRESSURE LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) FUEL PRESSURE SWITCH LEAKING FROM SOLDERED JOINT AT BASE OF CONNECTOR PLUG FITTING. 1G72 4U4 U H4SW E22EA 20010402002742001040200274 2001 4 2 AU010063 420010101G2565B732560135 CABLE BOEING737 737377 NM GE CFM56 CFM563B1 13802NE ESCAPE SLIDE FRAYED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) L2 DOOR SLIDE ATTACHMENT CABLE FRAYED IN LOOP AREA. 2L72 4F4 FRTA16WE E2GL 20010402002752001040200275NM 2001 4 2 AU010064 120010109G28976130024 WIRE BOEING737 737377 NM GE CFM56 CFM563B1 13802NE FUEL SYSTEM DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) KAPTON WIRES LOCATED IN REFUEL PANEL HAVE DAMAGED INSULATION ALLOWING THE WIRES TO BE EXPOSED. 2L72 4F4 FRTA16WE E2GL 20010402002762001040200276EU 2001 4 2 AU010065 120010123G5343 FITTING AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR DOOR ACTUATOR FITTING AND CONNECTING STRIP CRACKED IN TWO PLACES. CRACK LENGTHS 20MM (0.78IN) IN FORWARD FLANGE AND 28MM (1.102IN) IN AFT FLANGE. CONNECTION STRAP CRACKED FROM FASTENER HOLE. CRACK LENGTH 5MM (0.196IN). FOUND DURING NDI INSPECTION IAW SB A320-53A1135 AND AN ENGINEERING RELEASE A32-53-40-9B. 2L72 4F4 FRTA28NM E29NE 20010402002772001040200277CE 2001 4 2 AU010066 120010120G551107326022 SPAR CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULYD3A34 D3A34C401 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HORIZONTAL STABILISER REAR SPAR CRACKED IN AREA BEHIND THERE INFORCED HINGE BRACKET CRACK LENGTH 50MM (1.96IN). CAUSED BY SEVERE CORROSION ON THE DOUBLER BRACKET SECURING THE ATTACHMENT HINGE PNO 0732101-11. 1H71 3O3 O 3A24 E5CE 5 CP47GL 20010402002782001040200278CE 2001 4 2 AU010067 120010131G321310581002375NLH FRAME BEECH 76 76 1153005CE MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT MAIN LANDING GEAR A FRAME CRACKED. 1L72 3O A29CE 20010402002792001040200279CE 2001 4 2 AU010068 120010131G321310581002376RH FRAME BEECH 76 76 1153005CE MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR A FRAME CRACKED. 1L72 3O A29CE 20010402002802001040200280SO 2001 4 2 AU010069 120010128G3250 PIN EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE NLG STEERING LOOSE W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AUS (AUS) NOSE WHEEL STEERING RELAY BOX CONNECTOR PIN LOOSE. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010402002812001040200281 2001 4 2 AU010070 420010124G25657A126130 SLIDE BOEING747 747SP38 NM PAX DOOR FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS 12818 (AUS) RT MAIN ENTRY DOOR SLIDE FAILED TO CORRECTLY DEPLOY DURING TEST. THE SLIDE CAUGHT ON THE DOOR STRUCTURE SUSTAINING A SMALL PUNCTURE AND DAMAGING THE LOWER BUSTLE. 2L74 4F RTA20WE 20010402002822001040200282EU 2001 4 2 AU010071 120010202G7931PDCR3301028 TRANSMITTER BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE OIL PRESSURE FAULTY W O OTHER J WARNING INDICATION CRCRUISE 1 AUS 3153 (AUS) NR 3 ENGINE OIL PRESSURE TRANSMITTER FAULTY. 2H74 4F4 FRTA49EU E6NE 20010402002832001040200283NE 2001 4 2 AU010072 220010203G73218061963 FMU BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE FUEL CONTROL FAULTY W O OTHER J WARNING INDICATION DEDESCENT 1 AUS (AUS) NR 2 ENGINE FUEL METERING UNIT (FMU) AND ELECTRONIC ENGINE CONTROLLER (EEC) FAULTY. 2L72 4F4 FTRA6WE E00061EN 20010402002842001040200284NE 2001 4 2 AU010073 220010203G7321114E6112G117 EEC BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE FUEL CONTROL FAULTY W O OTHER J WARNING INDICATION DEDESCENT 1 AUS (AUS) NR 2 ENGINE ELECTRONIC ENGINE CONTROLLER (EEC) FAULTY. SEE ALSO MDR 01/0072. 2L72 4F4 FTRA6WE E00061EN 20010402002852001040200285NE 2001 4 2 AU010074 320010129G6111RFC11U1R6A BLADE EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE PROPELLER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT PROPELLER BLADE DAMAGED BY MISSING SPINNER ATTACHMENT SCREW. THREE SCREWS MISSING FROM SPINNER. ONE SCREW WAS FOUND EMBEDDED IN THE PROPELLER BLADE. MAINTENANCE HAD BEEN CARRIED OUT ON THE PROPELLER PRIOR TO THE FLIGHT. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010402002862001040200286EA 2001 4 2 AU010075 120010203G3213 BLOCK DHAV DHC6 DHC6300 2802606EA MLG FAILED W O OTHER J WARNING INDICATION LDLANDING 1 AUS (AUS) RT MAIN LANDING GEAR COMPRESSION BLOCKS FAILED WITH RESULTANT DAMAGE TO THE FUSELAGE. BLOCKS FAILED DUE TO RT MLG CONTACTING A RIDGE ON THE AIRSTRIP. 1H72 3T RTA9EA 20010402002872001040200287EA 2001 4 2 AU010076 220010112G7414K3984 CAPACITOR SLICK 4381 CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA MCAULY1A103 1A103TCM GL LT MAGNETO BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS 2068 97020839 (AUS) LT MAGNETO CAPACITOR CONNECTING WIRE BROKEN DUE TO LOOSE BEARING CAP. FURTHER INVESTIGATION FOUND THE BEARINGS TO BE DRY AND AN UNKNOWN SUBSTANCE UNDER THE BEARING CAP HOLD-DOWN PLATES WHICH PREVENTED THE CAP BEING PROPERLY SECURED. 1H71 3O3 ONT3A19 E223 5 NP50GL 20010402002882001040200288SO 2001 4 2 AU010077 220010206G8550 GEAR CONT O520 TSIO520K 17040SO SCAV PUMP FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE OIL SCAVENGE PUMP GEAR FAULTY. ROCKWELL HARDNESS TEST GAVE A READING OF 34 WHICH IS BELOW SPECIFICATION. 3 O E8CE 20010402002892001040200289NM 2001 4 2 AU010078 120010112G5330 SKIN BOEING747 747238B 1384828NM FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE SKIN CRACKED AT TWO FASTENER HOLES IMMEDIATELY FORWARD OF THE FRAME AT STN 980. 2L74 4F A20WE 20010402002902001040200290GL 2001 4 2 AU010079 320010128G6114737568 HUB LYC O360 O360A2A 41514EA MCAULY2D36C 2D36C14 GL PROPELLER DAMAGED W C ABORTED TAKEOFF D INFLIGHT SEPARATION TOTAKEOFF 1 AUS (AUS) PROPELLER HUB FAILED DUE TO CRACK ORIGINATING IN THE ROOT OF THEBLADE RETAINING THREAD. PROPELLER BLADE SEPARATED FROM HUB. 3 O E286 5 CP901 20010402002912001040200291NM 2001 4 2 AU010080 120010127G7110 PANEL RROYCE RB211524D4 BOEING747 747238B 1384828NM RROYCERB211 RB211524D41954555NE COWLING MISSING W K NONE O OTHER ININSP/MAINT 1 AUS 15288 (AUS) NR 1 ENGINE NR 1 AND NR 3 & 4 ACOUSTIC PANELS MISSING. 2L74 4F4 F A20WE E12EU 20010402002922001040200292NM 2001 4 2 AU010081 120010127G291013206001 SWITCH BOEING767 767238 NM PWA JT9 JT9D7R4E 52054NE HYDRAULIC SYS FAULTY W O OTHER J WARNING INDICATION CRCRUISE 1 AUS (AUS) LT HYDRAULIC TAIL SHUTOFF VALVE SWITCH MODULE FAULTY. 2L72 4F4 FRTA1NM E3NE 20010402002932001040200293CE 2001 4 2 AU010082 120010205G321310581002376RH FRAME BEECH 76 76 1153005CE MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR A FRAME CRACKED. 1L72 3O A29CE 20010402002942001040200294CE 2001 4 2 AU010083 120010205G321310581002375LH FRAME BEECH 76 76 1153005CE MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT MAIN LANDING GEAR A FRAME CRACKED. 1L72 3O A29CE 20010402002952001040200295NM 2001 4 2 AU010084 120010130G2741 WIRE BOEING747 747438 NM RROYCERB211 RB211524G19 NE STABILIZER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT STABILISER POSITION ROTARY VARIABLE DISPLACEMENT TRANSDUCER(RVDT) PLUG DM7884 HAD CHAFED WIRING ADJACENT TO PLUG. 2L74 4F4 FRTA20WE E30NE 20010402002962001040200296NM 2001 4 2 AU010085 120010131G2120 UNKNOWN BOEING767 767338 1385151NM RROYCERB211 RB211524* NE AIR CONDITIONINGODOR W O OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS (AUS) FUMES IN CABIN. INVESTIGATION CONTINUING INTO CAUSE. 2L72 4F4 FRTA1NM E12EU 20010403001512001040300151NM 2001 4 3 AU010086 120010130G5730113T161331 PANEL BOEING767 767338 1385151NM GE CF6 CF680C2* GL LT WING FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PANEL 551VB LOCATED ON LT WING LOWER SURFACE AFT OF THE LT MAIN LANDING GEAR MISSING A CENTRE SECTION APPROXIMATELY 6 FEET LONG. 2L72 4F4 FRTA1NM E23EA 20010403001522001040300152NM 2001 4 3 AU010087 120010128G291065C268393152 PIPE BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU HYDRAULIC SYS CHAFED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HYDRAULIC SYSTEM A ENGINE DRIVEN PUMP HYDRAULIC LINE CHAFED BY LOWER AILERON PCU. 2L72 4F4 FRTA16WE E21EU 20010403001532001040300153CE 2001 4 3 AU010088 120010202G551010562000025 HINGE BEECH 76 76 1153005CE HORIZONTAL STAB LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELEVATOR CENTER BEARING SUPPORT BLOCK MOVING IN CLAMPING FLANGES DUE TO APPROXIMATELY 0.127MM TO 0.254MM (0.005IN TO 0.010IN) ELONGATION OF THE RIVET HOLES. 1L72 3O A29CE 20010403001542001040300154SO 2001 4 3 AU010089 120010205G2910D100366 FITTING EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE HYDRAULIC SYS LEAKING W O OTHER K FLUID LOSS CRCRUISE 1 AUS (AUS) HYDRAULIC FITTING LOCATED IN LT OUTBOARD NACELLE LEAKING UNDERPRESSURE. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010403001552001040300155EU 2001 4 3 AU010090 120010119G3610 LOOP AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE PNEUMATIC DIST FAULTY W D RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 AUS (AUS) WING LOOP A PNEUMATIC SYSTEM INOPERATIVE. 2L72 4F RTA35EU E24NE 20010403001562001040300156EU 2001 4 3 AU010091 120010202G3610 DUCT AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE PNEUMATIC DIST LEAKING W O OTHER J WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) NR 1 BLEED AIR SYSTEM LEAKING. 2L72 4F RTA35EU E24NE 20010403001572001040300157EU 2001 4 3 AU010092 120010202G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING CONTAMINATED W O OTHER N FALSE WARNING NRNOT REPORTED 1 AUS (AUS) FORWARD CARGO DOOR MICROSWITCH CONTAMINATED WITH DIRT AND PAINT. 2L72 4F4 FRTA20EU E2EU 20010403001582001040300158EU 2001 4 3 AU010094 120010131G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING OUT OF ADJ W O OTHER N FALSE WARNING CRCRUISE 1 AUS (AUS) SERVICE DOOR MICROSWITCH OUT OF ADJUSTMENT. 2L72 4F4 FRTA20EU E2EU 20010403001592001040300159EU 2001 4 3 AU010095 120010130G3610 DUCT FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU PNEUMATIC DIST LEAKING W O OTHER N FALSE WARNING NRNOT REPORTED 1 AUS (AUS) TAIL SECTION PNEUMATIC DUCT LEAK WARNING. INVESTIGATION COULD FIND NO LEAKS. 2L72 4F4 FRTA20EU E2EU 20010403001632001040300163EU 2001 4 3 AU010096 120010129G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING OUT OF ADJ W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) SERVICE DOOR WARNING LIGHT ILLUMINATED. SUSPECT MICROSWITCHES OUT OF ADJUSTMENT. 2L72 4F4 FRTA20EU E2EU 20010403001642001040300164EU 2001 4 3 AU010097 120010128G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING STUCK W A UNSCHED LANDING N FALSE WARNING CRCRUISE 1 AUS (AUS) CARGO DOOR MICROSWITCHES STICKING INTERMITTENTLY. 2L72 4F4 FRTA20EU E2EU 20010403001652001040300165EU 2001 4 3 AU010098 120010128G243223531 BATTERY FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU BATTERY BAY OVERHEATED W A UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 AUS (AUS) FORWARD BATTERY OVERTEMPERATURE. 2L72 4F4 FRTA20EU E2EU 20010403001662001040300166EU 2001 4 3 AU010099 120010126G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING OUT OF ADJ W A UNSCHED LANDING N FALSE WARNING CRCRUISE 1 AUS (AUS) FORWARD SERVICE DOOR MICROSWITCH OUT OF ADJUSTMENT. 2L72 4F4 FRTA20EU E2EU 20010403001672001040300167EU 2001 4 3 AU010100 120010125G5312 BULKHEAD FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) REAR PRESSURE BULKHEAD CRACKED. 2L72 4F4 FRTA20EU E2EU 20010403001682001040300168EU 2001 4 3 AU010101 120010120G3230 UPLOCK FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU RT MLG LOOSE W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) RT MAIN LANDING GEAR DOOR UPLOCK HOOK LOOSE. 2L72 4F4 FRTA20EU E2EU 20010403001692001040300169EU 2001 4 3 AU010102 120010105G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING STUCK W C ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AUS (AUS) CARGO DOOR MICROSWITCHES STICKING INTERMITTENTLY. 2L72 4F4 FRTA20EU E2EU 20010403001702001040300170SO 2001 4 3 AU010103 120010202G273141734078 CONTROL CABLE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ELEVATOR TAB WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELEVATOR TRIM CABLE SEVERELY WORN IN THE AREA AROUND THE TRIM SERVO. ALL WIRE STRANDS BROKEN EXCEPT FOR TWO. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010403001712001040300171EA 2001 4 3 AU010104 220010202G8550LW13383 BAFFLE PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR2 GL ENGINE SUMP LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS 691 (AUS) ENGINE SUMP BAFFLE RIVET MISSING. THREE REMAINING RIVETS LOOSE. METAL IN OIL SYSTEM CAME FROM WORKING RIVETS. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010403001722001040300172EU 2001 4 3 AU010105 220010205G72619584 ENGINE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU OIL PRESSURE LOW W O OTHER EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) NO2 ENGINE LOW OIL PRESSURE. ENGINE REMOVED AND AWAITING STRIPREPORT. 2L72 4F4 FRTA20EU E2EU 20010403001732001040300173NM 2001 4 3 AU010106 120010105G5310 STRUCTURE BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NUMEROUS AREAS OF CORROSION FOUND DURING CPCP INSPECTION IAWAD/B727/128. 2L73 4F4 FRTA3WE E2EA 20010403001742001040300174NM 2001 4 3 AU010107 120010130G252011 BOLT BOEING737 737377 NM GE CFM56 CFM563B1 13802NE SEAT BELT LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS 4006 (AUS) SEAT BELT ATTACHMENT BOLT LOOSE AT SEAT 11E. FOUND DURING INSPECTION IAW ER B73-25-20-246. 2L72 4F4 FRTA16WE E2GL 20010403001752001040300175NE 2001 4 3 AU010108 220010207G72000292005250 ENGINE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE NR 1 SEIZED W K NONE O OTHER ININSP/MAINT 1 AUS 1738 (AUS) NR 1 ENGINE INTERNAL FAILURE. INSPECTION FOUND COMPRESSOR SEIZED AND SEVERAL TURBINE BLADES MISSING/BROKEN. 1G72 3U3 UNCH1NE E19EU 20010403001762001040300176NM 2001 4 3 AU010109 120010123G3230113T1110 FITTING BOEING767 767277 NM GE CF6 CF680A 30025NE MLG CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT MAIN LANDING GEAR SIDE STRUT SWIVEL ASSEMBLY FITTINGS COORODED IN AREA BENEATH BUSHING FLANGE. 2L72 4F4 FRTA1NM E13NE 20010403001772001040300177CE 2001 4 3 AU010110 120010214G5330101120108604 SKIN BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE MCAULY4HFR344HFR34C754 NE FUSELAGE DEBONDED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TOP SKIN DISBONDED. 1L72 4T4 T A24CE E4EA 6 C3PNE 20010403001782001040300178EU 2001 4 3 AU010111 120010211G5102GATES HOSE COLT 160 160A 8970104EU BALLOON REPORTS FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) OUTER SKIN OF THE LPG HOSE RUPTURED. 1B 0 3BEU 20010403001792001040300179EA 2001 4 3 AU010112 120010122G5553C6TFM102227 FITTING DHAV DHC6 DHC6300 2802606EA VERTICAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) VERTICAL STABILISER FORWARD ADAPTER FITTING RIGHT HAND ATTACHMENT LUG CRACKED. 1H72 3T RTA9EA 20010403001802001040300180SO 2001 4 3 AU010113 120010208G2823480700 PIN PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA HARTZLHCE2Y HCE2YK2 GL FUEL SELECTOR BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT FUEL SELECTOR ROLL PINS (2OFF) BROKEN. 1L72 3O3 O 1A10 1E4 5 CP9EA 20010403001812001040300181CE 2001 4 3 AU010114 120010206G2731 BOLT CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C93 GL FLIGHT CONTROL WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) EXCESSIVE TRIM TAB FREE-PLAY DUE TO WORN AFT PUSHROD BOLT. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010403001822001040300182EU 2001 4 3 AU010115 120010129G7933J03040C CONNECTOR FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY62015 04564NE OIL TEMP CONTAMINATED W O OTHER EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION CLCLIMB 1 AUS (AUS) NR 1 ENGINE OIL TEMPERATURE PROBE CONNECTOR PLUG LOOSE AND CONTAMINATED. 2L72 4F4 FRT E25NE 20010403001832001040300183NM 2001 4 3 AU010116 120010122G291082910010113 PIPE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYDRAULIC SYS FRACTURED W C ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) HYDRAULIC PIPE FRACTURED ON RADIUS AT STA. 110.0. LOSS OF HYDRAULIC FLUID. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010403001842001040300184WP 2001 4 3 AU010117 120010130G5720157 FITTING DHAVXXDH82 DH82AROBRTSN2801002WP DHAVXXGIPSY GIPSYMAJOR1 20004WP LT WING FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 157 (AUS) LT WING FRONT LOWER INTERPLANE STRUT ATTACHMENT FITTING BROKEN AWAY DUE TO WOOD ROT. 1Q71 3I3 I A8EU A8EU 20010403001852001040300185NM 2001 4 3 AU010118 120010120G3260 UPLOCK SENSOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE MLG OUT OF ADJ W C ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AUS (AUS) RT MAIN LANDING GEAR UPLOCK SENSOR OUT OF ADJ. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010403001862001040300186CE 2001 4 3 AU010119 120010206G8011PM2407 STARTER CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL LT ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT ENGINE STARTER MOTOR FAULTY. ONE NEGATIVE BRUSH MISSING WITH THE OTHER NEGATIVE BRUSH LOOSE IN THE BRUSH HOLDER AND EVIDENCE OF SEVERE ARCING AROUND THE BRUSH/PIGTAIL SECURING SCREW. BOTHPOSITIVE BRUSHES WERE LOOSE AND THE BRUSH HOLDERS WITHSEVERE ARCING AROUND THE SECURING SCREW. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010403001872001040300187NE 2001 4 3 AU010120 220010216G7200 ENGINE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE HARTZLHCB3T HCB3TN3 GL ENGINE BAY MAKING METAL W K NONE O OTHER ININSP/MAINT 1 AUS 4811 (AUS) ENGINE CHIP DETECTOR CONTAMINATED BY METAL CHIP. SUSPECT CHIP WAS A PART OF A TAB WASHER. 1L72 4T4 T A24CE E4EA 6 CP15EA 20010403001882001040300188CE 2001 4 3 AU010121 120010115G551104320016 RIB CESSNA150 150M 2071830CE CONT O200 O200A 17020SO MCAULY1A102 1A102OCM GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HORIZONTAL STABILISER FORWARD ATTACHMENT RIBS CRACKED. 1H71 3O3 O 3A19 E252 5 NP918 20010403001892001040300189CE 2001 4 3 AU010122 120010115G5511043200146 RIB CESSNA150 150M 2071830CE CONT O200 O200A 17020SO MCAULY1A102 1A102OCM GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HORIZONTAL STABILISER FORWARD ATTACHMENT RIBS CRACKED. 1H71 3O3 O 3A19 E252 5 NP918 20010403001902001040300190EU 2001 4 3 AU010124 220010206G73210164168200 FUEL CONTROL SNIAS AS332 AS332L 8680809EU TMECA MAKILAMAKILA1A 60040EU NR 2 ENGINE FAULTY W A UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 AUS 258 (AUS) NR 2 ENGINE FUEL CONTROL UNIT FAULTY. 2G72 4U4 U H4EU E12NE 20010403001932001040300193SO 2001 4 3 AU010126 120010206G524312007993614 DOOR EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE HYDRAULIC BAY SEPARATED W O OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 AUS (AUS) RT HYDRAULIC BAY DOOR FAILED AND SEPARATED DURING FLIGHT. DOORHAD BEEN OPENED FOR MAINTENANCE BEFORE FLIGHT AND IT IS SUSPECTED THAT IT WAS NOT PROPERLY CLOSED AND LATCHED. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010403001942001040300194NM 2001 4 3 AU010127 120010204G7603 CABLE RROYCE RB211524D4 BOEING747 747SP38 NM RROYCERB211 RB211524D41954555NE POWER LEVER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE THRUST CONTROL SYSTEM CABLES, PULLEYS AND FITTINGS DAMAGED. FOUND DURING INSPECTION IAW AD/B747/229 AND FAAAD/2000-05-30 AMDT39-11640. 2L74 4F4 FRTA20WE E12EU 20010403001952001040300195CE 2001 4 3 AU010128 120010201G270105131679 WHEEL CESSNA182 182C 2072708CE CONT O470 O470L 17026SO HARTZLHCA2X BHCA2XF1 GL CONTROL COLUMN CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) BOTH CONTROL WHEELS CRACKED FROM BOTTOM RIVET HOLE. 1H71 3O3 ONT3A13 E273 5 CP908 20010403001962001040300196NM 2001 4 3 AU010129 120010202G261251291001 FIRE LOOP BOEING747 747338 NM RROYCERB211 RB211524D41954555NE APU BAY MALFUNCTIONED W FA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) APU LOWER DOOR FIRE DETECTOR LOOP HAD HIGH RESISTANCE. FALSE WARNING INDICATION RESULTED IN DISCHARGE OF FIRE BOTTLE. 2L72 4F4 FRTA20WE E12EU 20010403001972001040300197NM 2001 4 3 AU010130 120010202G2910 HOSE BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU HYDRAULIC SYS FAILED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) LT MAIN LANDING GEAR DOWNLOCK HYDRAULIC HOSE SPLIT. LOSS OF HYDRAULIC FLUID. 2L72 4F4 FRTA16WE E21EU 20010403001982001040300198NM 2001 4 3 AU010131 120010110G3260841005 PSEU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE MLG FAULTY W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) LANDING GEAR PROXIMITY SWITCH ELECTRONIC UNIT (PSEU) FAULTY. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010403002002001040300200SO 2001 4 3 AU010132 220010202G8530 EXHAUST VALVE CESSNA206 U206F 2073333CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL ENGINE LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE EXHAUST VALVE LEAKING. 1H71 3O3 O A4CE E5CE 5 CP21EA 20010403002012001040300201SO 2001 4 3 AU010133 120010207G532012043522001LH BEAM EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE CABIN CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLIGHT ATTENDANT SEAT SUPPORT FRAMES CORRODED. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010403002022001040300202SO 2001 4 3 AU010134 120010207G532012025916001RH BEAM EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE CABIN CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLIGHT ATTENDANTS SEAT SUPPORT FRAMES CORRODED. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010403002032001040300203EU 2001 4 3 AU010135 120010203G7712P66230C ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP ROTOL R333 R333482F12 GL LEFT OUT OF ADJ W C ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LT ENGINE RPM ROLLBACK. SUSPECT CAUSED BY NR 1 TORQUE BRIDGE PIT OUT OF ADJUSTMENT. 2L72 4T4 TRTA56EU E4WE 6 CP61GL 20010403002042001040300204SO 2001 4 3 AU010136 120010206G21332091G010800 OUTFLOW VALVE EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE CABIN PRESSURE FAULTY W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AUS 4884 (AUS) PRESSURISATION SYSTEM OUTFLOW VALVE FAULTY. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010403002052001040300205SO 2001 4 3 AU010137 120010126G2751487927 SWITCH PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL LT WING TE FLAPSFAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH WING FLAP UPLIMIT MICROSWITCH FAILED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010403002062001040300206CE 2001 4 3 AU010138 120010220G35101013800491 HOSE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE MCAULY4HFR344HFR34C754 NE CREW OXYGEN SPLIT W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) COPILOTS OXYGEN HOSE FAILED. HOSE HAD BEEN INCORRECTLY FITTED WITH A TIGHT RADIUS. 1L72 4T4 T A24CE E4EA 6 C3PNE 20010403002072001040300207GL 2001 4 3 AU010139 220010123G72106877180 GEARBOX BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 AUS (AUS) ENGINE GEARBOX OUT OF LIMITS. CHIP DETECTORS CONTAMINATED WITHMETAL PARTICLES. 1G71 3U3 U H2SW E4CE 20010403002082001040300208EU 2001 4 3 AU010140 120010119G5302332A2400200001 STRUCTURE SNIAS AS332 AS332L 8680809EU TMECA MAKILAMAKILA1A 60040EU TAIL BOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAIL BOOM CRACKED IN AREA OF PYLON DECK. 2G72 4U4 U H4EU E12NE 20010403002092001040300209SO 2001 4 3 AU010141 120010213G7112 BAFFLE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE AIR DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE BAFFLES DAMAGED. FOUND DURING INSPECTION IAW AD/PA31/96REQ1. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010403002102001040300210EA 2001 4 3 AU010142 220010119G8530LW16740 EXHAUST VALVE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE WORN W K NONE O OTHER ININSP/MAINT 1 AUS 1146 (AUS) LH ENGINE EXHAUST VALVES (2OFF) ERODED. RT ENGINE EXHAUST VALVES(4OFF) ERODED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010403002112001040300211NE 2001 4 3 AU010143 220010215G7200RB211524G ENGINE BOEING747 747438 NM RROYCERB211 RB211524G19 NE NR 4 FIRE W FA ACTIVATE FIRE EXT. UNSCHED LANDING AJ FLAME/FIRE WARNING INDICATION CLCLIMB 1 AUS 16202 (AUS) NR 4 ENGINE FIRE. INVESTIGATION FOUND FIRE/HEAT DAMAGE TO WIRING AND CLAMPS IN AREA OF COMBUSTION CHAMBER COWLING. 2L74 4F4 FRTA20WE E30NE 20010403002122001040300212NM 2001 4 3 AU010144 120010216G2741 WIRE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HORIZONTAL STAB WORN W O OTHER J WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) HORIZONTAL STABILISER SURFACE POSITION INDICATOR WIRE CHAFED ANDSHORT CIRCUITING INSIDE CONDUIT LOCATED BETWEEN THE FORWARD SPAROF THE HORIZONTAL STABILISER AND THE RT ELEVATOR SYNCHRO. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010403002132001040300213NE 2001 4 3 AU010146 220010208G7321CPW3111697503B EEC DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE HAMSTD14SF 14SF23 NE LT ENGINE OUT OF ADJ W C ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LT ENGINE ELECTRONIC UNIT AUTO-FEATHER OPERATION FUNCTION OUT OF ADJUSTMENT. UNIT HAD BEEN ADJUSTED ON THE PREVIOUS NIGHT WITHOUTCHECKING THE AUTO-FEATHER FUNCTION. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010403002142001040300214CE 2001 4 3 AU010147 120010221G321310581002376 FRAME BEECH 76 76 1153005CE MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR A FRAME CRACKED. 1L72 3O A29CE 20010326004952001032600495NM 2001 3 26 AU010148 120010217G2910DSC252A40230 PIPE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYDRAULIC, MAIN LEAKING W K NONE OK OTHER FLUID LOSS ININSP/MAINT 1 AUS (AUS) HYDRAULIC LINE LOCATED IN RH WHEEL BAY CONTAINED A PINHOLE LEAK. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010326000122001032600012SO 2001 3 26 AU010149 220010123G8520652560 CRANKCASE CONT IO520L CESSNA210 210N 2073453CE CONT O520 IO520L 17032SO MCAULYD3A34 D3A34C404 GL RECIPROCATING ENCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 415 567731 (AUS) CRANKCASE CRACKED IN NUMEROUS PLACES. INSPECTION FOUND EXCESSIVE FRETTING ON THE SECOND AND THIRD MAIN BEARING SADDLE FACES WHEN VIEWED FROM THE REAR. LOCTITE OR SIMILAR WAS FOUND ON THE BEARING SADDLE FACES. THE MAIN THROUGH BOLTS WERE OF THE OLDER SIX POINTNUTS. THE HYDRAULIC LIFTERS FITTED IN THE EXHAUST POSITIONS WERE PNO 646288 INSTEAD OF PNO 646277. THE OIL PICKUP SCREEN SUCTION SCREEN WAS THE INCORRECT TYPE AS REQUIRED BY SB M87-11 REV2. NO OVERHAUL HISTORY COULD BE FOUND FOR THE FUEL PUMP OR THE FCU. PERSONNEL/MAINTENANCE ERROR. WRONG PART. 1H71 3O3 O 3A21 E5CE 5 CP47GL 20010326000132001032600013EA 2001 3 26 AU010150 220010213G8530LW16703 CYLINDER LYC O235L2C PIPER PA38 PA38112 7103812SO LYC O235 O235L2C 41505EA SNSNCH72C 72CK EA RECIPROCATING ENCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 810 L1609315 (AUS) ENGINE NO2 CYLINDER CRACKED AT BASE. OIL LEAKING FROM CRACK. 1L71 3O3 O A18SO E223 5 NP9045 20010327004172001032700417NM 2001 3 27 AU010151 120010109G528028489 DOOR BOEING 737400 BOEING757 757* NM CFMINTCFM56 CFM563C 13802EU LANDING GEAR DOOCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 10341 28489 (AUS) RT MAIN LANDING GEAR STRUT DOOR CRACKED THROUGH LOWER ATTACHMENT BOLT HOLDER. 2L72 4F4 FRTA2NM E21EU 20010327004182001032700418SO 2001 3 27 AU010152 120010213G3242RFS1015 DISK BFGOODRICH 214791 EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE BRAKE BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS 0671 (AUS) BRAKE ROTATING DISC (CARRIER AND LINING ASSEMBLY) BROKEN. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010327004192001032700419SO 2001 3 27 AU010153 120010213G5330120056 SKIN EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) SKIN SURROUNDING THE COPILOTS WINDOW FRAME CRACKED. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010327004202001032700420NM 2001 3 27 AU010154 120010202G57536546435274SP SKIN BOEING737 7374Q8 NM CFMINTCFM56 CFM563C 13802EU TE FLAPS DELAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT AFT OUTER FLAP TRAILING EDGE DELAMINATING AT INBOARD AFT CORNER. 2L72 4F4 FRTA16WE E21EU 20010403000012001040300001EA 2001 4 3 AU010155 220010219G7310420218 SWITCH BELL 412 412 1182202SW PWA PT6T PT6T3 52045EA FUEL BYPASS LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) FUEL FILTER BYPASS SWITCH LEAKING FROM SWITCH BODY IN THE AREA WHERE THE ELECTRICAL CONNECTOR IS SOLDERED TO THE SWITCH. FUEL WAS SEEN RUNNING INTO THE ENGINE INTAKE PLENUM. A REPLACEMENT SWITCH HAD POOR SOLDERING OF THE CONNECTOR IN THE SAME AREA ASTHE FAILED ITEM. 1G72 4U4 U H4SW E22EA 20010403000022001040300002EU 2001 4 3 AU010156 120010211G77142454401 SENSOR AEROSPSA365 SA365C 8680667EU TMECA ARRIELARRIEL1A 60030NE ENGINE FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE OVERSPEED SENSOR FAULTY. 1G72 3U3 U H10EU E19EU 20010327004212001032700421CE 2001 3 27 AU010157 120010202G2410646655 GEAR CESSNA ALTERNATOR CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL DC GENERATOR-ALTDAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS 185 EO030305377 (AUS) LH ENGINE ALTERNATOR DRIVE GEAR DAMAGED AND OUTER SHELL DISTORTED. EVIDENCE OF VICE MARKS ON OUTSIDE OF SHELL. FURTHERDAMAGE FOUND:-1. OIL SEAL INSTALLED BACKWARDS.2. SUPPRESSOR CAPACITOR LOOSE INSIDE OF ALTERNATOR AND SCREW LOOSE. 3. PITTING IN CASE HARDENING ON THE SLIP RING END OF THE ROTOR SHAFT. 4. STATOR CORE LAMINATIONS BADLY DISTORTED RENDERING CORE UNSERVICEABLE. THE ROTOR IN ALTERNATOR AT TIME OF STRIP DOWN INSPECTION SHOWED NO SIGNS OF CONTACT WITH STATOR POLES.PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010327004222001032700422CE 2001 3 27 AU010158 120010222G528008411066 BRACKET CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL LANDING GEAR DR BROKEN W K NONE OD OTHER INFLIGHT SEPARATION LDLANDING 1 AUS 5203 (AUS) LH MAIN LANDING GEAR DOOR BRACKET FAILED. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010403000032001040300003EU 2001 4 3 AU010159 120010212G772221186009 COMPUTER BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C653 NE ENGINE FAULTY W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) LT ENGINE SINGLE RED LINE COMPUTER FAULTY. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010403000042001040300004EU 2001 4 3 AU010160 120010223G7160TU195MM660MMCC HOSE BNORM BN2 BN2B20 1520302EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL ENG AIR INTAKE FAILED W C ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NR 1 ENGINE INTAKE HOSE LOCATED BETWEEN THE AIR FILTER AND THE FCU COLLAPSED DUE TO LOOSE INNER SUPPORT WIRE. 1H72 3O3 O A17EU 1E4 5 CP920 20010405002552001040500255NE 2001 4 5 AU010161 220010222G7530216035037 ACTUATOR LYC ALF502R5 BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE COMPRESSOR BLEEDFAULTY W O OTHER E VIBRATION/BUFFET APAPPROACH 1 AUS XRC8122 (AUS) NR 3 ENGINE BLEED BAND ACTUATOR FOLLOWUP ARM RETAINING CLIP AND PIN MISSING ALLOWING THE FOLLOWUP ARM AND THE OPERATING LEVER TO FOUL EACH OTHER WHICH RESULTED IN THE BLEED BAND REMAINING CLOSED. 2H74 4F4 FRTA49EU E6NE 20010405002562001040500256EU 2001 4 5 AU010162 120010221G2450A2043C POWER UNIT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R375 R3754123F21 NE AC POWER DIST FAULTY W O OTHER HBJELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) RT POWER DISTRIBUTION UNIT (PDU) FAULTY. STARTER-GENERATOR WOULDNOT DISENGAGE AND AN OVERTEMPERATURE WAS OBSERVED WITH SMOKE COMING FROM THE COWLS. THE FIRE BOTTLE WAS DISCHARGED AS APRECAUTION. 2L72 4T4 TRTA52EU E8NE 6 CP17NE 20010405002572001040500257WP 2001 4 5 AU010163 220010228G7210851 GEARBOX BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C653 NE LEFT ENGINE MAKING METAL W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT ENGINE REMOVED DUE TO SUSPECT DISTRESS IN THE GEARBOX AND VIBRATION. OIL ANALYSIS FOUND METAL CONTAMINATION. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010405002582001040500258CE 2001 4 5 AU010164 120010222G271050452133 TUBE CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL AILERON CONTROL CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) OUTBOARD PUSH-PULL TUBE LOCATED IN RT WHEEL WELL CORRODED INTERNALLY. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010405002592001040500259SW 2001 4 5 AU010165 120010226G5712273102336 RIB SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP ROTOL R321 R321482F8 GL RT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT WING RIB CRACKED IN BEND RADIUS. RIB FORMS THE INNER WALL OF THE BATTERY BOX. CRACK LENGTH 203.2MM (8IN). 2L72 4T4 TRTA8SW E4WE 6 CP61GL 20010405002602001040500260SW 2001 4 5 AU010166 120010226G5712273102336 RIB SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP ROTOL R321 R321482F8 GL LT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING RIB CRACKED IN BEND RADIUS. RIB FORMS THE INNER WALL OF THE BATTERY BOX. CRACK LENGTH 76.2MM (3IN). 2L72 4T4 TRTA8SW E4WE 6 CP61GL 20010405002612001040500261EU 2001 4 5 AU010167 120010223G7714AG34 TACH GENERATOR BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C653 NE ENGINE FAULTY W O OTHER P NO WARNING INDICATION CLCLIMB 1 AUS (AUS) TACHO-GENERATOR ZERO OUTPUT. INVESTIGATION ALSO FOUND BROKENWIRE STRANDS AT THE ENGINE WIRING DISCONNECT SPLICE. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010405002622001040500262EU 2001 4 5 AU010168 220010219G7230 COMPRESSOR FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU NR 1 ENGINE DAMAGED W O OTHER E VIBRATION/BUFFET CLCLIMB 1 AUS (AUS) NO1 ENGINE VIBRATION. BORESCOPE INSPECTION FOUND DAMAGE TO THESEVENTH STAGE HPC. 2L72 4F4 FRTA20EU E2EU 20010405002632001040500263EU 2001 4 5 AU010169 120010218G2133566920 OUTFLOW VALVE FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY62015 04564NE CABIN COOLING SYFAILED W O OTHER J WARNING INDICATION CRCRUISE 1 AUS 4585 (AUS) AVIONICS COOLING SYSTEM OUTFLOW VALVE FAILED. 2L72 4F4 FRT E25NE 20010405002642001040500264CE 2001 4 5 AU010170 120010201G3260JE1 SWITCH CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL MLG WORN W O OTHER N FALSE WARNING LDLANDING 1 AUS (AUS) RT MAIN LANDING GEAR MICROSWITCH ARM WORN. ARM BROKE OFF DURING FLIGHT. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010405002652001040500265 2001 4 5 AU010172 420010305G3423 COMPASS CESSNA150 150B 2071806CE CONT O200 O200A 17020SO MCAULY1A100 1A100MCM GL COCKPIT OUT OF ADJ W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) COMPASS SWING OUT OF DATE. NO COMPASS CORRECTION CARD FITTED. 1H71 3O3 O 3A19 E252 5 NP918 20010405002662001040500266SO 2001 4 5 AU010173 120010228G551140122002 SPAR PIPER PA31350 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 311274 (AUS) HORIZONTAL STABILISER SPAR CRACKED. FOUND DURING INSPECTION IAW PIPER MSB 1007. WHEN INSPECTED IAW AD/PA31/97 AMDT2 NO CRACKS WERE FOUND DUE TO CRACKS BEING HIDDEN BY THE ELEVATOR OUTBOARD HINGE ATTACHMENT FITTING. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010405002672001040500267SO 2001 4 5 AU010174 120010228G551140122003 SPAR PIPER PA31350 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 311274 (AUS) HORIZONTAL STABILISER SPAR CRACKED. FOUND DURING INSPECTION IAW PIPER MSB 1007. WHEN INSPECTED IAW AD/PA31/97 AMDT2 NO CRACKS WERE FOUND DUE TO CRACKS BEING HIDDEN BY THE ELEVATOR OUTBOARD HINGE ATTACHMENT FITTING. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010405002682001040500268CE 2001 4 5 AU010175 120010223G275208615582 GEAR CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO TE FLAP ACTUATORWORN W O OTHER F FLT CONT AFFECTED LDLANDING 1 AUS (AUS) FLAP ACTUATOR TRANSFER GEAR STRIPPED. 1L72 3O3 O A7CE E8CE 20010405002692001040500269EA 2001 4 5 AU010176 220010225G74144370 SHAFT PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA SNSNCH74D 74DM EA MAGNETO FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAGNETO SHAFT BROKEN IN AREA WHERE THE POINTS CAM ATTACHES. 1L71 3O3 O 2A13 E274 5 NP88614 20010405002702001040500270SO 2001 4 5 AU010177 220010308G8500IO470L ENGINE BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO MCAULY2AF34C2AF34C55 GL RIGHT FAILED W C ABORTED TAKEOFF EYJVIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 AUS 1450 20139971L (AUS) RT ENGINE CATASTROPHIC FAILURE. 1L72 3O3 ORT3A16 3E1 5 CP5EA 20010405002712001040500271WP 2001 4 5 AU010178 120010204G243615891A VOLT REGULATOR DOUG DC4 C54E 3021530WP PWA R2000 R2000* 52023NE HAMSTD23E 23E50 NE DC SYSTEM OVERHEATED W A UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 AUS R704 (AUS) NR 2 GENERATOR VOLTAGE REGULATOR FAULTY. 2L74 4R4 R A762 5E5 6 CP603 20010405002722001040500272SO 2001 4 5 AU010179 220010219G8530649166 CYLINDER CESSNA210 210L 2073448CE CONT O520 IO520L 17032SO MCAULY3A32C D3A32C88 GL ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 397 270089R (AUS) NR 1 AND NR 3 CYLINDERS CRACKED FROM UPPER SPARK PLUG HOLE. CRACK LENGTHS APPROXIMATELY 25.4MM (1IN). BOTH CYLINDERS ARE P0.015IN. 1H71 3O3 O 3A21 E5CE 5 CP21EA 20010405002732001040500273SO 2001 4 5 AU010180 220010220G8520 CRANKCASE CESSNA172 172B 2072406CE CONT O300 O300C 17022SO MCAULY1C172 1C172EM GL ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE IN AN EXTREMELY POOR CONDITION. DEFECTS INCLUDE CRACKED CRANKCASE, WORN CRANKSHAFT, WORN GEARS, WORN CYLINDERS AND VALVES. 1H71 3O3 ONT3A12 E253 5 NP910 20010405002742001040500274NE 2001 4 5 AU010181 320010227G6111RFC11U16A BLADE EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE PROPELLER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT PROPELLER NR 1 BLADE DAMAGED BY FOD. LEADING EDGE SHEATH HAD APIECE MISSING APPROXIMATELY 10MM (0.393IN) IN DIAMETER. THE LEFT FRONT PASSENGER WINDOW BEHIND THE GALLEY HAD A LARGE IMPACT MARK APPROXIMATELY 12MM (0.472IN) IN DIAMETER. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010405002752001040500275EA 2001 4 5 AU010182 220010307G852068606 CRANKSHAFT FUJI FA200 FA200160 3730101WP LYC O320 O320D2A 41508EA MCAULY1C172 1C172MGM GL ENGINE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS L639239A (AUS) CRANKSHAFT INTERNAL BORE CORRODED. FOUND DURING INSPECTION IAWAD/LYC/102 AMDT2 PART 1 AND PART 2. 1L71 3O3 O A4PC E274 5 NP910 20010405002762001040500276SW 2001 4 5 AU010183 120010307G6230206040002109 MAST BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL MAIN ROTOR DAMAGED W O OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 AUS (AUS) MAIN ROTOR MAST SUBJECTED TO TORSIONAL DAMAGE DURING N2 LOCKUP ON START. 1G71 3U3 U H2SW E4CE 20010405002772001040500277EA 2001 4 5 AU010184 220010307G8520L639239A PUSHROD FUJI FA200 FA200160 3730101WP LYC O320 O320D2A 41508EA MCAULY1C172 1C172MGM GL ENGINE MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS L639239A (AUS) ENGINE PUSHRODS AND TAPPETS INCORRECTLY FITTED DURING ASSEMBLY FOLLOWING A BULK STRIP FOLLOWING A PROPELLER STRIKE. METAL CONTAMINATION OF ENGINE. 1L71 3O3 O A4PC E274 5 NP910 20010405002782001040500278SO 2001 4 5 AU010185 120010308G81204091709001 TURBOCHARGER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL RT ENGINE FAULTY W O OTHER EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS 1 (AUS) RT ENGINE TURBOCHARGER FAULTY. LOSS OF ENGINE OIL (4LITRES). 1L72 3O3 O A20SO E14EA 5 CP33EA 20010405002792001040500279NE 2001 4 5 AU010186 320010305G6111RFC11MIRGADE BLADE EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE PROPELLER CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 4860 (AUS) PROPELLER BLADE NICKEL SHEATH CRACKED. CRACK LENGTH APPROXIMATELY 50.8MM (2IN) LOCATED ON THE FACE APPROXIMATELY 50.8MM (2IN) FROMTHE BLADE HEATER. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010405002802001040500280EA 2001 4 5 AU010188 120010311G5610NP1393225 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AUS 9910H4795 (AUS) CAPTAINS SIDE WINDOW OUTER PANE SHATTERED. 2L72 4F4 FRTA21EA E15NE 20010405002812001040500281CE 2001 4 5 AU010189 120010225G2750 WIRE CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL TE FLAPS BROKEN W O OTHER F FLT CONT AFFECTED LDLANDING 1 AUS (AUS) FLAP PRESELECT MICROSWITCH WIRE BROKEN. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010405002822001040500282SO 2001 4 5 AU010190 120010312G521041420002 HINGE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL PAX DOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TOP CABIN DOOR FORWARD HINGE FAILED DUE TO CORROSION INDUCED CRACKING. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010405002832001040500283EA 2001 4 5 AU010191 220010110G7250 ENGINE EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL TURBINE SECTION DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE SKI JUMP SEVERELY CRACKED AND DISTORTED IN AREA AROUND NR 3 BEARING COVER. SOME PIECES OF THE EXHAUST CASING HAVE COMPLETELY BROKEN AWAY CAUSING DAMAGE TO THE POWER TURBINE DISC AND BLADES. POWER TURBINE STATOR CRACKED THROUGH THE INNER BAND. 1L72 4T4 T A21SO E4EA 6 CP15EA 20010405002842001040500284 2001 4 5 AU010192 420010312G3497 WIRE BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE NAVIGATION UNIT LOOSE W O OTHER J WARNING INDICATION CRCRUISE 1 AUS (AUS) NR 2 COMPASS SYSTEM FAULTY. INVESTIGATION FOUND A LOOSE WIRE TERMINAL AND NUT ON THE RT FLUX VALVE TERMINAL BLOCK LOCATED AT THE RH OUTER WING TRAILING EDGE. 2H74 4F4 FRTA49EU E6NE 20010405002852001040500285SO 2001 4 5 AU010193 220010306G7314 PUMP BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MCAULY3AF34C3AF34C502 GL ENGINE CONTAMINATED W O OTHER E VIBRATION/BUFFET CRCRUISE 1 AUS (AUS) RT ENGINE DRIVEN FUEL PUMP ADJUSTABLE ORIFICE CONTAMINATED WITH A SMALL PARTICLE. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20010405002862001040500286NE 2001 4 5 AU010194 220010310G7323430121204 DRIVE SHAFT BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE GOVERNOR SHEARED W O OTHER E VIBRATION/BUFFET CRCRUISE 1 AUS 2238 (AUS) NR 1 ENGINE POWER TURBINE GOVERNOR DRIVE COUPLING SHEARED. 1G72 3U3 U H13EU E5NE10 20010405002872001040500287CE 2001 4 5 AU010195 120010314G28205892000017 LINE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MCAULY3AF34C3AF34C502 GL FUEL DIST LOOSE W O OTHER EYJVIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION LDLANDING 1 AUS 7522 (AUS) RT ENGINE MAIN FUEL LINE FLARE NUT DISCONNECTED ON AFT SIDE OFFIREWALL. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20010405002882001040500288NE 2001 4 5 AU010196 220010312G73238210161E GOVERNOR PWA PW120A DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE NR 1 ENGINE FAULTY W C ABORTED TAKEOFF ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AUS 2248689 (AUS) NR 1 ENGINE OVERSPEED GOVERNOR FAULTY. THE GOVERNOR WAS A NEWLY FITTED ITEM WITH NO HOURS SINCE OVERHAUL. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010405002892001040500289NM 2001 4 5 AU010197 120010226G4900211734219 GCU BOEING767 767338 1385151NM GE CF6 CF680C2* GL APU FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 18690 (AUS) APU GENERATOR CONTROL UNIT (GCU) FAULTY. INVESTIGATION FOUND THETOP COVER COOLING HOLES BLOCKED WITH DUST. 2L72 4F4 FRTA1NM E23EA 20010405002902001040500290NM 2001 4 5 AU010198 120010222G2840BACJ40A204 JUMPER BOEING747 747438 NM RROYCERB211 RB211524G19 NE FUEL WIRING MISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUEL CROSSFEED MANIFOLDS IN CENTER WING TANK HAD MISSING BONDINGJUMPERS. 2L74 4F4 FRTA20WE E30NE 20010405002912001040500291NM 2001 4 5 AU010199 120010227G291065C268393061 LINE BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU HYDRAULIC SYSTEMLEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) HYDRAULIC B SYSTEM RESERVOIR TO STANDBY SYSTEM SUPPLY LINE LEAKING. LOSS OF HYDRAULIC FLUID. 2L72 4F4 FRTA16WE E21EU 20010405002922001040500292NM 2001 4 5 AU010200 120010223G27821267625 ACTUATOR BOEING747 747438 NM RROYCERB211 RB211524G19 NE SLATS JAMMED W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 AUS 41940 (AUS) RH OUTBOARD LEADING EDGE FLAP DRIVE ACTUATOR JAMMED. 2L74 4F4 FRTA20WE E30NE 20010405002932001040500293NM 2001 4 5 AU010201 120010224G2530GENM2585013 OVEN BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU GALLEY BURNED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 AUS 221 (AUS) REAR GALLEY OVEN FAN MOTOR BURNT. 2L72 4F4 FRTA16WE E21EU 20010405002942001040500294NM 2001 4 5 AU010202 120010223G3250 NUT BOEING747 747238B 1384828NM RROYCERB211 RB211524D41954555NE NLG STEERING UNLOCKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT NOSE GEAR STEERING CABLES DID NOT HAVE SPLIT PINS FITTED THROUGH CASTELLATED NUTS. BOTH NUTS WERE ONLY FINGER TIGHT AND THE LT NUT WAS HELD BY ONLY TWO THREADS.PERSONNEL/MAINTENANCE ERROR. 2L74 4F4 F A20WE E12EU 20010405002952001040500295NM 2001 4 5 AU010203 120010220G3320 LIGHT BOEING747 747438 NM RROYCERB211 RB211524G19 NE CABIN CONTAMINATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 AUS (AUS) CROSSOVER CEILING LIGHT LOCATED AT DOOR NR 5 RT HAD SEVERAL PIECES OF TISSUE STUFFED INTO THE LIGHT. THE TISSUE HAD BEGUN TO SMOULDER. THE CROSSOVER LIGHT LENS AND ASSOCIATED METAL GRILL ASSEMBLY WAS MISSING. 2L74 4F4 FRTA20WE E30NE 20010405002962001040500296 2001 4 5 AU010204 420010220G25657A146913 RESERVOIR BOEING747 747438 NM RROYCERB211 RB211524G19 NE ESCAPE SLIDE DISCHARGED W K NONE O OTHER ININSP/MAINT 1 AUS 5336 GJ1033 (AUS) NO5 LH MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE INFLATION RESERVOIR PRESSURE BELOW LIMITS. 2L74 4F4 FRTA20WE E30NE 20010405002972001040500297NM 2001 4 5 AU010205 120010217G3320 SOCKET BOEING747 747338 NM RROYCERB211 RB211524D41954555NE LIGHT BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS (AUS) SIDEWALL WASH LIGHT SOCKET LOCATED AT SEAT 25 HJK BURNED OUT AND ARCING DUE TO WATER CONTAMINATION. AREA AROUND SEATS FOUND TO BE SOAKING WET DUE TO BLOCKAGE OF RT SIDE UPPER DECK DOOR DRAINBLOCKAGE ALLOWING WATER LEAKAGE. AIRCRAFT HAD BEEN ON THE GROUNDDURING A SEVERE RAIN STORM. 2L72 4F4 FRTA20WE E12EU 20010405002982001040500298NM 2001 4 5 AU010206 120010219G2823737M28500011 SHUTOFF VALVE 737M2850001XBOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU FUEL SELECTOR FAILED W O OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) NR 2 ENGINE FUEL SHUTOFF VALVE FAILED. 2L72 4F4 FRTA16WE E21EU 20010405002992001040500299NM 2001 4 5 AU010207 120010207G3244B2700 TIRE BOEING747 747238B 1384828NM LT MLG SEPARATED W O OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 AUS 2096 (AUS) LT BODY MAIN LANDING GEAR FRONT INBOARD WHEEL TIRE (4F) HAD TREAD MISSING. 2L74 4F A20WE 20010405003002001040500300NM 2001 4 5 AU010208 120010309G2910AS11506K0264 HOSE BOEING767 767338 1385151NM GE CF6 CF680C2* GL HYDRAULIC SYSTEMFAILED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) NR 4 BRAKE HYDRAULIC HOSE FAILED. 2L72 4F4 FRTA1NM E23EA 20010405003012001040500301NM 2001 4 5 AU010209 120010305G2610 CONNECTOR BOEING747 747238B 1384828NM DETECTION SYSTEMLOOSE W K NONE P NO WARNING INDICATION ININSP/MAINT 1 AUS (AUS) FIRE WARNING SYSTEM CARD A8 NOT SEATING CORRECTLY DUE TO REAR CONNECTOR ADRIFT FROM HOUSING. 2L74 4F A20WE 20010405003022001040500302 2001 4 5 AU010210 420010306G2565D31591475 SLIDE BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU PAX DOOR FAILED W K NONE L NO TEST ININSP/MAINT 1 AUS 5661 (AUS) NR 1 RT MAIN ENTRY DOOR ESCAPE SLIDE FAILED TO FULLY DEPLOY. INVESTIGATION FOUND THAT THE SLIDE EXHAUST VALVE WAS STUCK OPEN AND THE VALVE ELEMENT HAD BROKEN AWAY FROM THE VALVE BODY. 2L72 4F4 FRTA16WE E21EU 20010405003032001040500303NM 2001 4 5 AU010211 120010304G2610 WARNING HORN BOEING767 767338 1385151NM GE CF6 CF680C2* GL DETECTION SYSTEMINOPERATIVE W K NONE L NO TEST ININSP/MAINT 1 AUS (AUS) FIRE TEST WARNING BELL INOPERATIVE. 2L72 4F4 FRTA1NM E23EA 20010405003042001040500304EU 2001 4 5 AU010213 120010320G7712SELOC29EC INDICATOR FOKKERF27 F27MK50 EU PWA PWA120PW125B NE ENGINE TORQUE MALFUNCTIONED W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AUS 3921 (AUS) LT ENGINE TORQUE INDICATOR SUSPECT FAULTY. 2H72 4T4 TRTA817 E20NE 20010405003052001040500305 2001 4 5 AU010214 420010223G6113C19042 SPINNER GROB G115 G115 EU LYC O360 O360A1F6 41514EA HARTZLHCF2Y HCF2YR1 GL PROPELLER DEBONDED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PROPELLER SPINNERS (7OFF) FOUND TO HAVE DISBONDED OR POOR BONDING BETWEEN THE INTERNAL FORWARD SUPPORT BULKHEAD AND THE SPINNER WALL. THE SPINNERS WERE NEW ASSEMBLIES BEING INSPECTED ON RECEIPT FROM THE MANUFACTURER. 1L71 3O3 ONTA57EU E286 5 CP27EA 20010405003062001040500306NE 2001 4 5 AU010215 220010316G8530114650 CYLINDER DOUG DC3 DC3CS1C3G 3021458WP PWA R1830 R183092 52020NE HAMSTD23E 23E50 NE ENGINE SEPARATED W O OTHER EYJVIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 AUS 381 (AUS) RT ENGINE NNR 1 CYLINDER UPPER BARREL AND HEAD SEPARATED. DAMAGE TO PISTON, RINGS, BARREL, INDUCTION TUBE AND PUSHROD TUBE. OIL FILTER METAL CONTAMINATION. 2L72 4R4 R A669 5E4 6 CP603 20010405003072001040500307EU 2001 4 5 AU010216 120010312G7921 PLUG GARRTT 7997 BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP ROTOL R333 R333482F12 GL DOOR ACTUATOR CONTAMINATED W C ABORTED TAKEOFF EN VIBRATION/BUFFET FALSE WARNING TOTAKEOFF 1 AUS 7921 (AUS) LT ENGINE OIL COOLER DOOR ACTUATOR PLUG CONTAMINATED. 2L72 4T4 TRTA56EU E4WE 6 CP61GL 20010405003082001040500308CE 2001 4 5 AU010217 120010313G323312810013 ACTUATOR CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 6006 (AUS) RT MAIN LANDING GEAR ACTUATOR BODY CRACKED. FOUND FOLLOWING INSPECTION IAW SEB01-2. 1H71 3O3 O 3A17 E286 5 CP7EA 20010405003092001040500309NE 2001 4 5 AU010218 220010307G7321 CONNECTOR PWA 7397 EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE EEC CONTAMINATED W C ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LT ENGINE TORQUE SIGNAL CONDITIONER AND ENGINE ELECTRONIC CONTROL (EEC) ELECTRICAL CONNECTORS CONTAMINATED WITH OIL. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010405003102001040500310GL 2001 4 5 AU010219 320010306G6111A22173QTY2 BLOCK HARTZL HCM2YR1BF BEECH 23 C24R 1151254CE LYC O360 IO360A1B6 41514EA HARTZLHCM2Y HCM2YR GL PROPELLER BLADE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 1240 EN273 (AUS) PROPELLER PITCH CHANGE BLOCKS CRACKED. PITCH CONTROL FORK WORNEXCESSIVELY. HUB PRELOAD PLATE DAMAGED DUE TO PREVIOUS FOREIGN OBJECT STRIKE. 1L71 3O3 O A1CE 1E10 5 CP43GL 20010405003112001040500311SO 2001 4 5 AU010220 220010223G8520629680 COLLAR CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO ENGINE MISMANUFACTURED W O OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 AUS (AUS) LT ENGINE CRANKSHAFT OIL TRANSFER COLLAR HAD INCORRECT CLEARANCE. THE MEASURED CLEARANCE WAS 0.0254MM (0.001IN) WITH THE CORRECTMANUFACTURERS LIMITS BEING 0.127MM TO 0.4572MM (0.005IN TO0.0018IN). 1L72 3O3 O 3A10 E5CE 20010405003122001040500312CE 2001 4 5 AU010221 120010225G3260ICH16 DOWNLOCK SWITCH CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL MLG FAULTY W O OTHER P NO WARNING INDICATION DEDESCENT 1 AUS (AUS) LT MAIN LANDING GEAR DOWNLOCK MICROSWITCH WIRE BROKEN. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010405003132001040500313EU 2001 4 5 AU010222 120010112G533011207 PLATE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LOWER LT FUSELAGE PANEL 95B REBATE PLATE CONTAINED SEVERE EXFOLIATION CORROSION (LEVEL2). 2L72 4F4 FRTA20EU E2EU 20010405003142001040500314 2001 4 5 AU010223 420010304G6122PCE21275 GOVERNOR PWA PT6A20 PILATSPC6 PC6 7090102EU PWA PT6 PT6A20 52043EA HARTZLHCB3T HCB3TN3 GL PROPELLER FAILED W D RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 AUS PCE21275 (AUS) PROPELLER REVERSE GOVERNOR IDLER GEAR BEARING COLLAPSED. METALCONTAMINATION OF ENGINE. 1H71 3O3 T 7A15 E4EA 6 CP15EA 20010405003152001040500315EA 2001 4 5 AU010224 220010202G7261 RELIEF VALVE EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL ENGINE CONTAMINATED W C ABORTED TAKEOFF ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) RT ENGINE OIL PRESSURE RELIEF VALVE CONTAMINATED BY A PIECE OF O-RING SEAL. 1L72 4T4 T A21SO E4EA 6 CP15EA 20010405003162001040500316EU 2001 4 5 AU010226 220010113G72502425 STATOR SNIAS AS332 AS332L 8680809EU TMECA MAKILAMAKILA1A 60040EU TURBINE SECTION CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE FIRST STAGE TURBINE NOZZLE GUIDE VANE INNER RING CRACKED.CRACK RAN FOR APPROXIMATELY 270 DEGREES OF CIRCUMFERENCE. 2G72 4U4 U H4EU E12NE 20010405003172001040500317CE 2001 4 5 AU010227 120010312G5321 SCREW BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MCAULY3AF32C3AF32C512 GL FLOOR PANEL UNAPPROVED PART W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) INCORRECT LENGTH SCREW FITTED TO PILOTS FLOOR PANEL. LONG SCREW CUT A GROOVE IN PIPE. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20010405003182001040500318EA 2001 4 5 AU010228 220010313G7314AN9296J CAP LYC O360A1F6 GROB G115 G115 EU LYC O360 O360A1F6 41514EA ENGINE FUEL PUMPCONTAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELECTRIC FUEL PUMP OUTLET T FITTING BLANKING CAP CONTAMINATED WITH SWARF. THE BLANKING CAPS ARE FITTED DURING MODIFICATION IAW EO E121-01 REV1. 1L71 3O3 ONTA57EU E286 20010405003192001040500319CE 2001 4 5 AU010229 120010320G321110581002376 FRAME BEECH 76 76 1153005CE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH AND RH MAIN LANDING GEAR A FRAMES CRACKED. 1L72 3O A29CE 20010405003202001040500320WP 2001 4 5 AU010230 120010315G6420C1281 HUB ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA TAIL ROTOR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAIL ROTOR HUB CONTAINED STRESS CORROSION AND CRACKING FROM THE TEETER BEARING RACES. 1G71 3O3 O H11NM E295 20010405003212001040500321CE 2001 4 5 AU010232 120010320G321110581002375 FRAME BEECH 76 76 1153005CE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT MAIN LANDING GEAR A-FRAMES CRACKED. 1L72 3O A29CE 20010405003222001040500322CE 2001 4 5 AU010233 120010319G7810 EXHAUST PIPE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE HARTZLHCD4N3HCD4N3A GL ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE EXHAUST DUCT FAILED IN AREA AROUND NR 3 BEARING COVER SUPPORT. 1L72 4T4 T A24CE E4EA 5 CSTC 20010405003232001040500323CE 2001 4 5 AU010234 120010320G321110581002376 FRAME BEECH 76 76 1153005CE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR A-FRAME CRACKED. 1L72 3O A29CE 20010405003242001040500324NM 2001 4 5 AU010235 120010316G2752734374D ACTUATOR DHAV DHC8 DHC8* NM TE FLAPS LACK OF LUBE W O OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 AUS (AUS) RH FLAP INBOARD ACTUATOR BALLSCREW NUT BADLY WORN. INVESTIGATION FOUND MISSING BALLS IN JACKSCREW AND SEVERE DAMAGE TO THE FORCE LIMITER. SUSPECT CAUSED BY LACK OF LUBRICATION. 2H72 4T RTA13NM 20010405003252001040500325EU 2001 4 5 AU010237 120010303G2432 BATTERY FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU E/E BAY OVERHEATED W O OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) AFT BATTERY OVERHEATED. 2L72 4F4 FRTA20EU E2EU 20010405003262001040500326EU 2001 4 5 AU010238 120010223G2910 PIPE FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU HYDRAULIC SYSTEMCHAFED W O OTHER N FALSE WARNING CLCLIMB 1 AUS (AUS) HYDRAULIC PIPES LOCATED IN LT WHEEL WELL RUBBING ON LANDING GEARDOOR PREVENTING REAR UPLOCK SWITCH FROM ACTIVATING. 2L72 4F4 FRTA20EU E2EU 20010405003272001040500327EU 2001 4 5 AU010239 120010222G2910 HYDRAULIC SYSTEM FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU NR 2 LOW W K NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 AUS (AUS) NR 2 HYDRAULIC SYSTEM LOW QUANTITY. INVESTIGATION COULD FIND NOEVIDENCE OF LEAKS. SUSPECT SYSTEM NOT REPLENISHED. 2L72 4F4 FRTA20EU E2EU 20010405003282001040500328EU 2001 4 5 AU010240 120010119G2612 FIRE LOOP AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE LT ENGINE FAULTY W D RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 AUS (AUS) LT ENGINE FIRE LOOP A FAULTY. 2L72 4F RTA35EU E24NE 20010405003292001040500329EU 2001 4 5 AU010241 120010206G2131 CONTROLLER FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU CABIN PRESSURE FAULTY W O OTHER J WARNING INDICATION CLCLIMB 1 AUS (AUS) CABIN PRESSURISATION SYSTEM FAULTY. 2L72 4F4 FRTA20EU E2EU 20010405003302001040500330EU 2001 4 5 AU010242 120010306G2913 PUMP FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU HYDRAULIC SYS LEAKING W C ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NR 2 HYDRAULIC SYSTEM ENGINE DRIVEN PUMP SILENCER LEAKING INTERNALLY. 2L72 4F4 FRTA20EU E2EU 20010405003312001040500331EU 2001 4 5 AU010243 120010226G5610 WINDOW FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU COCKPIT STUCK W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) CAPTAINS SLIDING WINDOW STUCK OPEN. INVESTIGATION FOUND WORN TRACK AND UPPER ROLLER. 2L72 4F4 FRTA20EU E2EU 20010409003892001040900389SO 2001 4 9 AU010245 220010216G8530682995 CYLINDER BEECH 36 A36 1151604CE CONT O550 IO550B SO ENGINE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS 243 (AUS) ENGINE CYLINDERS PNO 649358, LIFTERS PNO 646277 AND CAMSHAFT PNO649322A1 CONTAINED PITTING CORROSION. ENGINE HAS ONLY 242.6 HOURS TOTAL TIME SINCE NEW. 1L71 3O3 O 3A15 E3SO 20010409003902001040900390SO 2001 4 9 AU010246 220010301G8520 CONNECTING ROD CESSNA402 402CESSNA 207590KCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C505 GL ENGINE SEPARATED W O OTHER E VIBRATION/BUFFET CRCRUISE 1 AUS 85 (AUS) RT ENGINE NR 2 AND NR 4 CONNECTING ROD BIG ENDS FAILED. CRANKCASE HOLES AND MAGNETOS SEPARATED. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010409003912001040900391CE 2001 4 9 AU010247 120010115G8120C1650040604 SEAL CONT TSIO520VB CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO TURBOCHARGER LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS 183 (AUS) LT ENGINE VAPC LEAKING OIL PAST PISTON DUE TO INTERNAL SEAL FAILURE. 1L72 3O3 O A7CE E8CE 20010409003922001040900392SW 2001 4 9 AU010248 120010321G5540304566 STRUCTURE AIRTRCAT802 AT802A SW PWA PT6 PT6A65AG 52043NE HARTZLHCB5M HCB5MP3 GL RUDDER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RUDDER CRACKED AND SKIN DEFORMED IN UPPER AREA WHERE THE BALANCEHORN ATTACHES TO THE RUDDER STRUCTURE. 1L71 3T4 TNCA19SW E4EA 6 CP44GL 20010409003932001040900393SW 2001 4 9 AU010249 120010319G71209388013 MOUNT AIRTRCAT802 AT802A SW PWA PT6 PT6A65AG 52043NE HARTZLHCB5M HCB5MP3 GL ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT SIDE ENGINE MOUNT RUBBER ISOLATION MOUNTS FAILED. ENGINE LOW ON LT SIDE CAUSING CHAFING OF THE FIRE SEALS ON THE BEARER. 1L71 3T4 TNCA19SW E4EA 6 CP44GL 20010409003942001040900394EA 2001 4 9 AU010250 220010323G8530G4299 COLLET LYC BEECH 65 A658200 1152805CE LYC O480 GSO480B1A6 41529EA HARTZLHCB3Z HCB3Z202 GL LT ENGINE FAILED W O OTHER E VIBRATION/BUFFET DEDESCENT 1 AUS 20 (AUS) LT ENGINE NR 6 CYLINDER VALVE COLLETS FAILED. INLET VALVE DROPPED. METAL CONTAMINATION OF OIL SYSTEM. OTHER COLLETS INSPECTED HADSIGNS OF ABNORMAL WEAR. SUSPECT UNAPPROVED PARTS. 1L72 3O3 O 3A20 E284 5 CP907 20010405003322001040500332CE 2001 4 5 AU010251 120010322G270105600144 CONTROL COLUMN CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA MCAULY1C160 1C160DTM GL COCKPIT CONTAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) CONTROL YOKE CONTAMINATED INTERNALLY WITH WATER. FOUND DURING INSPECTION IAW CESSNA SEB 01-3 1H71 3O3 ONT3A12 E274 5 NP910 20010405003332001040500333EA 2001 4 5 AU010252 220010312G7414 PIN BNORM BN2 BN2A21 1520221EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YR2 GL IMPULSE COUPLINGFAILED W O OTHER EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION LDLANDING 1 AUS (AUS) RT ENGINE MAGNETO IMPULSE COUPLING PIN MIGRATED OUT, ALLOWING THE FLANGE SECURING PIN AND FLANGE TO FAIL. LOSS OF ENGINE OIL. 1H72 3O3 O A17EU 1E4 5 CP920 20010405003342001040500334 2001 4 5 AU010253 420010319G341628702501 ALTIMETER BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA COCKPIT FAILED W O OTHER O OTHER CLCLIMB 1 AUS (AUS) ALTIMETER INTERNAL FAILURE. 2L72 4T4 TRTA24CE E4EA 20010405003352001040500335NE 2001 4 5 AU010254 220010326G73216068T72P09 HMU SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R375 R3754123F21 NE FUEL CONTROL FAULTY W O OTHER ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AUS (AUS) RT ENGINE HYDROMECHANICAL UNIT (HMU) FAULTY. 2L72 4T4 TRTA52EU E8NE 6 CP17NE 20010405003362001040500336EA 2001 4 5 AU010255 220010313G74144370 MAGNETO PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA RIGHT FAILED W O OTHER ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) RT MAGNETO FAILED. 1L71 3O3 O 2A13 E286 20010405003372001040500337CE 2001 4 5 AU010256 120010313G5512 SKIN CESSNA210 210N 2073453CE CONT O520 IO520L 17032SO MCAULYD3A34 D3A34C404 GL HORIZONTAL STAB CHAFED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT HORIZONTAL STABILIZER LOWER SKINS CHAFED BY THE GAP SEAL STRIP / ANGLE AT THE FUSELAGE TO STABILISER JUNCTION.REDUCTION IN SKIN THICKNESS FROM 0.635MM (0.025IN) TO 0.33MM(0.013IN). 1H71 3O3 O 3A21 E5CE 5 CP47GL 20010405003382001040500338EU 2001 4 5 AU010257 120010213G5711 SPAR BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE LT & RT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED. 2H74 4F4 FRTA49EU E6NE 20010405003392001040500339EU 2001 4 5 AU010258 120010212G5711 SPAR BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R3A 41580NE LT & RT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT WING FORWARD AND AFT LOWER SPAR CAPS CRACKED IN AREABETWEEN RIBS NR 13 AND NR 18. CORROSION ALSO FOUND ON LOWER SKINS AT RIB BAYS NR 13 TO NR 18. 2H74 4F4 FRTA49EU E6NE 20010405003402001040500340EU 2001 4 5 AU010259 120010212G5730 SKIN BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE LT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING LOWER SKIN CORRODED AT RIB BAYS NR 14 TO NR 16. RT WING LOWER SKIN CORRODED AT RIB BAYS NR 14 AND NR 15. 2H74 4F4 FRTA49EU E6NE 20010405003412001040500341NM 2001 4 5 AU010260 120010318G2897W60000818R WIRE BOEING747 747438 NM RROYCERB211 RB211524G19 NE FUEL SYSTEM SHORTED W O OTHER N FALSE WARNING CLCLIMB 1 AUS (AUS) FUEL SYSTEM CONTROL VALVE WIRE PNO W6400-008-18R LOCATED IN NR 4 STRUT KNEE CAP DISCONNECT PLUG D14300P CHAFED AND SHORT CIRCUITING TO GROUND. 2L74 4F4 FRTA20WE E30NE 20010405003422001040500342NM 2001 4 5 AU010261 120010309G324226088127 BRAKE BOEING767 767338 1385151NM GE CF6 CF680C2* GL RT MLG DELAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS 15104 (AUS) RT MAIN LANDING GEAR NR 7 BRAKE STATORS DELAMINATED. 2L72 4F4 FRTA1NM E23EA 20010405003432001040500343NM 2001 4 5 AU010262 120010318G324226088127 BRAKE BOEING767 767338 1385151NM GE CF6 CF680C2* GL LT MLG FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 13318 (AUS) LT NR 4 MAIN WHEEL BRAKE ASSEMBLY ROTORS DISINTEGRATED. 2L72 4F4 FRTA1NM E23EA 20010405003442001040500344EU 2001 4 5 AU010263 120010325G21607828602 CONTROL VALVE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R375 R3754123F21 NE CABIN TEMP SEIZED W C ABORTED TAKEOFF BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TOTAKEOFF 1 AUS 16660 (AUS) DUAL TEMPERATURE CONTROL VALVE SEIZED IN OPEN POSITION. 2L72 4T4 TRTA52EU E8NE 6 CP17NE 20010405003452001040500345NE 2001 4 5 AU010264 220010323G73216078T55P18 FUEL CONTROL GE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE RT ENGINE LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) RT ENGINE FUEL CONTROL UNIT LEAKING FROM THE AREA OF THE THROTTLE CONTROL INPUT ARM. 2L72 4F4 FRTA21EA E15NE 20010405003462001040500346GL 2001 4 5 AU010265 320010325G6111660715698 EROSION SHIELD ROTOL 6607152727 FOKKERF27 F27MK50 EU PWA PWA120PW125B NE ROTOL R352 R3526123F1 GL PROPELLER BLADE SEPARATED W O OTHER D INFLIGHT SEPARATION CLCLIMB 1 AUS 1779 F50470 (AUS) PROPELLER BLADE EROSION SHIELD SEPARATED. 2H72 4T4 TRTA817 E20NE 6 CP16NG 20010405003472001040500347EU 2001 4 5 AU010266 220010324G7321B12597 AMPLIFIER FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU FUEL CONTROL FAULTY W C ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 AUS 7419 (AUS) NR 1 ENGINE POWER FLUCTUATIONS. ENGINE CONTROL AMPLIFIER AND TEMPERATURE CONTROL ACTUATOR CHANGED. 2L72 4F4 FRTA20EU E2EU 20010405003482001040500348EU 2001 4 5 AU010267 120010324G2913 COUPLING FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU HYDRAULIC PUMP CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) NR 1 HYDRAULIC SYSTEM HYDRAULIC PUMP PRESSURE LINE ELBOW COUPLING THREADED SECTION CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID. 2L72 4F4 FRTA20EU E2EU 20010405003492001040500349SW 2001 4 5 AU010268 120010320G6210206015001117AS BLADE BELL 206 206L 1181522SW ALLSN 250C 250C30 03013GL MAIN ROTOR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN ROTOR BLADE CORRODED IN AREA BETWEEN PAINT AND LEADING EDGESTRIP ON UNDERSIDE OF BLADE. CORROSION DEPTH APPROXIMATELY 1.52MM (0.060IN). FOUND BEFORE FITMENT. 1G71 3U3 U H2SW E1GL 20010405003502001040500350EU 2001 4 5 AU010269 120010309G5270 WARNING SYSTEM FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU PAX DOOR INTERMITTENT W O OTHER N FALSE WARNING NRNOT REPORTED 1 AUS (AUS) PASSENGER DOOR WARNING LIGHT INTERMITTENT IN OPERATION. INVESTIGATION COULD FIND NO FAULT. 2L72 4F4 FRTA20EU E2EU 20010405003512001040500351 2001 4 5 AU010270 420010310G344220412170413 RADAR FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU WEATHER FAULTY W C ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 AUS 780 2673 (AUS) RADAR RECEIVE/TRANSMIT UNIT FAULTY. 2L72 4F4 FRTA20EU E2EU 20010405003522001040500352 2001 4 5 AU010271 420010312G2212637SUE1 WARNING SYSTEM FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU ALTITUDE CONTROLFAILED W A UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 AUS (AUS) ALTITUDE ALERT SYSTEM FAILED. ALTITUDE PRESELECT COUPLER CHANGED. 2L72 4F4 FRTA20EU E2EU 20010405003532001040500353EU 2001 4 5 AU010272 220010314G7200RB18355515H ENGINE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU NR 1 VIBRATES W C ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NR 1 ENGINE VIBRATION AND NOISE. 2L72 4F4 FRTA20EU E2EU 20010405003542001040500354CE 2001 4 5 AU010273 120010316G3260 FASTENER CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL MLG UPLOCK FAILED W O OTHER N FALSE WARNING CRCRUISE 1 AUS (AUS) LANDING GEAR UPLOCK ASSEMBLY HI-LOK FASTENERS FAILED. BRACKETS TORN AWAY FROM SPAR BOX. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010405003552001040500355EU 2001 4 5 AU010274 120010321G2720NB45961 LEVER BNORM BN2 BN2B20 1520302EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL RUDDER CONTROL SLOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RUDDER CONTROL RT IDLER LEVER LOOSE AND CATCHING ON FUSELAGE FRAME OPENING. 1H72 3O3 O A17EU 1E4 5 CP920 20010405003562001040500356 2001 4 5 AU010276 420010317G61221680640 PICKUP WOODWARD 89741016 BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C653 NE PROP GOVERNOR FAULTY W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AUS 2330240 (AUS) LT ENGINE GOVERNOR MAGNETIC PICKUP (MONOPOLE) OUTPUT VOLTAGEUNSTABLE. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010405003572001040500357GL 2001 4 5 AU010277 320010320G6110991996 SPACER MCAULY B3DF36C527 PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA MCAULY3DF36CB3DF36C526 GL PROPELLER ASSY MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS 597 991996 (AUS) RT PROPELLER SPACER INCORRECTLY FITTED. 1L72 3O3 O A20SO E14EA 5 C 20010507004002001050700400EU 2001 5 7 AU010278 120010303G2550A25LT CARGO HOOK BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE CARGO AREA FAULTY W O OTHER D INFLIGHT SEPARATION CLCLIMB 1 AUS (AUS) CARGO HOOK FAILED AND RELEASED LOAD. INVESTIGATION FOUND SCREWLOCATED ON THE LOWER LH SIDE OF THE COVER WAS INTERFERING WITHTHE RETURN OF THE LEVER AND LATCH ASSEMBLY RESULTING IN INTERMITTENT OPERATION OF THE LATCH. EXCESSIVE PLAY IN LINK AND PINS CONTRIBUTED TO THE PROBLEM. 1G72 3U3 U H13EU E5NE10 20010510000712001051000071EA 2001 5 10 AU010279 220010326G8520LW12596 BOLT PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE BROKEN W O OTHER EFKVIBRATION/BUFFET FLT CONT AFFECTED FLUID LOSS DEDESCENT 1 AUS (AUS) LT ENGINE CONNECTING ROD BOLT FAILED. ENGINE SUMP HOLED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010507004012001050700401SW 2001 5 7 AU010281 120010322G6220471202527 GRIP BELL 47 47G5A 1181034SW LYC O435 VO435B1A 41516EA MAIN ROTOR HEAD CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 577 NC5779 (AUS) MAIN ROTOR GRIP CRACKED IN SECOND, THIRD AND FOURTH THREADS. FOUND DURING EDDY CURRENT INSPECTION. X-RAY INSPECTION RESULTSWERE INCONCLUSIVE. 1G71 3O3 O 2H3 E279 20010510000722001051000072SW 2001 5 10 AU010282 120010128G79312719153003 TRANSDUCER SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UA 01514WP MCAULY4HFR344HFR34C652 NE ENGINE OIL PRESSFAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE OIL PRESSURE TRANSDUCER FAILED FOLLOWING FITMENT. 2L72 4T4 TRTA5SW E4WE 6 C3PNE 20010510000732001051000073SW 2001 5 10 AU010284 120010314G2121071040370001 COOLING FAN SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UA 01514WP MCAULY4HFR344HFR34C652 NE AIR DISTRIBUTIONFAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AUS (AUS) AVIONICS COOLING FAN FAILED. CIRCUIT BREAKER POPPED. 2L72 4T4 TRTA5SW E4WE 6 C3PNE 20010511000042001051100004EU 2001 5 11 AU010285 120010329G2910AE7064588 HOSE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R375 R3754123F21 NE HYDRAULIC SYSTEMRUPTURED W C ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NOSE LANDING GEAR ACTUATOR FLEXIBLE DOWN LINE RUPTURED. LOSS OF HYDRAULIC FLUID. 2L72 4T4 TRTA52EU E8NE 6 CP17NE 20010511000052001051100005SO 2001 5 11 AU010286 120010205G2436VSF7203S REGULATOR PIPER PA23 PA23250 7102308SO LYC O540 IO540* 41532EA DC SYSTEM MALFUNCTIONED W O OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 AUS (AUS) REGULATOR OVERVOLTAGE. CHARGING SYSTEM TRIPPED. 1L72 3O3 O 1A10 1E4 20010511000062001051100006 2001 5 11 AU010287 420010325G61228210004 GOVERNOR HARTZL HCB3TN3 DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA HARTZLHCB3T HCB3TN3 GL PROP GOVERNOR FAULTY W A UNSCHED LANDING O OTHER CLCLIMB 1 AUS 103231ST (AUS) RT PROPELLER GOVERNOR FAULTY. 1H72 3T4 TRTA9EA E4EA 6 CP15EA 20010511000072001051100007SO 2001 5 11 AU010288 120010325G2750 CONTROLLER EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE TE FLAPS FAULTY W C ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 AUS (AUS) OUTBOARD FLAP DISAGREEMENT WARNING. INSPECTION COULD FIND NOFAULTS. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010511000082001051100008NE 2001 5 11 AU010289 220010312G72503053556220 BEARING GE CFM565A1 AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE TURBINE SECTION SPALLED W EA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 AUS (AUS) NR 2 ENGINE NR 4 BEARING OUTER RACE SEVERELY SPALLED. 2L72 4F4 FRTA28NM E29NE 20010511000092001051100009EU 2001 5 11 AU010290 120010328G6123HTE123542A PRESSURE SWITCH HARTZL HCA6A3 STBROSSD3 SD360 8100606EU PWA PT6 PT6A67R 52043NE HARTZLHCA6A HCA6A3 NE PROP FEATHER FAULTY W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LH PROPELLER AUTOFEATHER SYSTEM PRESSURE SWITCH FAULTY. 2H72 4T4 T A41EU E26NE 6 CP14NE 20010511000102001051100010CE 2001 5 11 AU010291 120010323G57400811351 FITTING CESSNA 402C CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C505 GL WING SPAR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS 4020625 (AUS) WING SPAR CAP FITTING CONTAINED SEVERE EXFOLIATION CORROSION ON THE FORWARD FACE. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010511000112001051100011NE 2001 5 11 AU010292 220010403G7310230350901 PIPE LYC ALF502R3A BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R3A 41580NE ENGINE FUEL DISTFRACTURED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) ENGINE FUEL PIPE FRACTURED. FUEL LEAKING. 2H74 4F4 FRTA49EU E6NE 20010511000122001051100012NM 2001 5 11 AU010293 120010331G3244A21580664 TIRE 161U00011 BOEING747 747438 NM RROYCERB211 RB211* 54555NE MLG FAILED W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AUS A21580664 (AUS) RH BODY LANDING GEAR OUTBOARD REAR NR 6R TIRE SHREDDED. DAMAGE CAUSED TO BODY FAIRING PANELS 194BR, 194CR, 194GR, RT WING LANDING GEAR DOOR AND HINGE, NR 5R WHEEL, RH BODY LANDING GEAR TRUCK POSITIONING ACTUATOR HYDRAULIC LINE, NR 13 AND NR 14 BRAKELINES. NUMEROUS FUSELAGE DENTS ALSO EVIDENT. 2L74 4F4 FRTA20WE A12EU 20010511000132001051100013NM 2001 5 11 AU010294 120010401G2434727810C GENERATOR BOEING767 767338 1385151NM GE CF6 CF680C2* GL APU FAILED W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION NRNOT REPORTED 1 AUS 52 (AUS) APU GENERATOR FAILED. 2L72 4F4 FRTA1NM E23EA 20010511000142001051100014NM 2001 5 11 AU010295 120010403G5410 FAIRING BOEING747 747400 NM GE CF6 CF680C2* GL NACELLE MISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 2 ENGINE RT COLD STREAM C DUCT MISSING UPPER INBOARD DUCT TO STRUT FILLET FAIRING. 2L74 4F4 FRTA20WE E23EA 20010511000152001051100015EU 2001 5 11 AU010296 120010318G77121090729245 TRANSMITTER AGUSTAA109 A109A 0260109EU ALLSN 25OC 250C20R GL ENGINE FAULTY W A UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 AUS (AUS) ENGINE TORQUE TRANSMITTER FAULTY. 1G72 3U3 U H7EU E4CE 20010511000162001051100016NM 2001 5 11 AU010297 120010406G5742 FITTING BOEING767 767277 NM GE CF6 CF680A 30025NE WING CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT WING PYLON ATTACHMENT FITTING OUTBOARD LUG CRACKED. CRACK PENETRATES THE FULL THICKNESS OF THE LUG AND EXTENDSAPPROXIMATELY 25.4MM (1IN) ALONG THE INBOARD FACE AND APPROXIMATELY 12.7MM (0.5IN) ALONG THE OUTBOARD FACE. FOUND USING EDDY CURRENT INSPECTION IAW BSB 767-57A0070 AND ERB76-57-40-18. 2L72 4F4 FRTA1NM E13NE 20010511000172001051100017NM 2001 5 11 AU010298 120010409G5742 FITTING BOEING767 767277 NM GE CF6 CF680A 30025NE WING CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING PYLON ATTACHMENT FITTING OUTBOARD LUG CRACKED. FOUND DURING VISUAL INSPECTION IAW ER B76-57-40-19. 2L72 4F4 FRTA1NM E13NE 20010511000182001051100018GL 2001 5 11 AU010299 320010320G6111C4451 FERRULE MCAULY 3AF32C75 BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO MCAULY3AF32C3AF32C75 GL PROPELLER BLADE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 1500 (AUS) PROPELLER BLADE FERRULE CRACKED AROUND BEARING SHELF ORIGINATINGFROM A PREVIOUSLY DRILLED ACTUATING PIN HOLE. CRACK LENGTH 50.8MM (2IN). 1L72 3O3 ORT3A16 3E1 5 CP22EA 20010511000192001051100019SO 2001 5 11 AU010300 120010326G27523203001007 ACTUATOR EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE TE FLAPS FAILED W C ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LT OUTBOARD FLAP ACTUATOR FAULTY. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010511000202001051100020NM 2001 5 11 AU010302 120010326G5511 SPAR BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE HORIZONTAL STAB CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD CORRODED AT STN 267.50. LT HORIZONTAL STABILISER REAR SPAR UPPER CHORD CORRODED AT STN 258. 2L72 4F4 FRTA16WE E2GL 20010511000212001051100021CE 2001 5 11 AU010303 120010331G3260JE6 ACTUATOR CESSNA340 340CESSNA 2076404CE CONT O520 TSIO520K 17040SO MCAULY3AF32C3AF32C87 GL LANDING GEAR BROKEN W O OTHER N FALSE WARNING DEDESCENT 1 AUS (AUS) RT MAIN LANDING GEAR MICROSWITCH ACTUATOR FAILED. 1L72 3O3 O 3A25 E8CE 5 CP22EA 20010511000222001051100022CE 2001 5 11 AU010304 120010330G2434ALT9422 ALTERNATOR CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL DC SYSTEM FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 46 (AUS) ENGINE DRIVEN ALTERNATOR SUSPECT REAR BEARING FAILED. DAMAGE TO ENGINE CRANKSHAFT DRIVE GEAR. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010511000232001051100023NM 2001 5 11 AU010305 120010403G1100ASM321032A PLACARD BOEING737 737377 NM GE CFM56 CFM563B1 13802NE MLG MISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TIRE INFLATION PLACARD MISSING. 2L72 4F4 FRTA16WE E2GL 20010511000242001051100024NM 2001 5 11 AU010306 120010404G7997 WIRE BOEING747 747438 NM RROYCERB211 RB211524G19 NE NR 3 ENGINE WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 3 ENGINE OIL PRESSURE INDICATION FAILED. INVESTIGATION FOUNDA SHORT CIRCUIT IN THE WING ROOT/ENGINE DISCONNECT DUE TO WIRECHAFING AT ACCESS PANEL 611BB. 2L74 4F4 FRTA20WE E30NE 20010511000252001051100025NM 2001 5 11 AU010308 120010404G2910BACF8A06EN0700B HOSE BOEING767 767238 NM PWA JT9 JT9D7R4E 52054NE HYDRAULIC SYSTEMLEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR TILT ACTUATOR HYDRAULIC HOSE LEAKING. 2L72 4F4 FRTA1NM E3NE 20010511000262001051100026NM 2001 5 11 AU010309 120010404G2910AS11506K0280 HOSE BOEING767 767330 NM RROYCERB211 RB211524* NE HYDRAULIC SYSTEMLEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR FLEXIBLE BRAIDED BRAKE HOSE HOLED ANDLEAKING. 2L72 4F4 FRTA1NM E12EU 20010511000272001051100027EU 2001 5 11 AU010310 120010314G2920MS24142D1 RELAY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R375 R3754123F21 NE HYDRAULIC SYSTEMFAULTY W O OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 AUS (AUS) AUXILIARY HYDRAULIC CONTROL RELAY FAULTY. 2L72 4T4 TRTA52EU E8NE 6 CP17NE 20010511000282001051100028NM 2001 5 11 AU010311 120010324G52306941730 BUNGEE CORD BOEING737 737377 NM GE CFM56 CFM563B1 13802NE CARGO DOOR BROKEN W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 AUS (AUS) AFT CARGO DOOR RELEASE LANYARD HANDLE JAMMED UNDER DOOR SEAL. INVESTIGATION FOUND THE LANYARD BUNGEE CORD BROKEN. 2L72 4F4 FRTA16WE E2GL 20010511000292001051100029SO 2001 5 11 AU010312 120010330G57404511500 FITTING PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL WING SPAR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT UPPER MAIN SPAR ATTACHMENT FITTINGS CORRODED ANDPARTIALLY EXFOLIATED. WHEN THE FITTINGS WERE REMOVED THE ATTACHMENT RIVETS WERE FOUND TO BE SHEARED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010511000302001051100030SO 2001 5 11 AU010313 120010330G57404511500 FITTING PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL WING SPAR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT UPPER MAIN SPAR ATTACHMENT FITTINGS CORRODED ANDPARTIALLY EXFOLIATED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010511000312001051100031SO 2001 5 11 AU010314 120010330G5720 BRACKET PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL WING SPAR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FORWARD SPAR ATTACHMENT BRACKET LOCATED AT STN 104.6 CRACKED ONFORWARD AND REAR SIDES. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010511000322001051100032SO 2001 5 11 AU010315 120010330G5720 BRACKET PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL WING SPAR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FORWARD SPAR ATTACHMENT BRACKET LOCATED AT STN104.6 CRACKED ONFORWARD AND REAR SIDES. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010511000332001051100033CE 2001 5 11 AU010316 120010319G2434902015 BEARING PRESTOLITE ALU9405 CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL DC GENERATOR FAILED W A UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 AUS 4E000070 (AUS) RT ENGINE ALTERNATOR BEARING FAILED. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010511000342001051100034SO 2001 5 11 AU010317 120010314G52804752932 HINGE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL MLG DOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR INBOARD DOOR FORWARD HINGE CRACKED. FOUNDDURING INSPECTION IAW AD/PA31/93 AMDT1. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010511000352001051100035SO 2001 5 11 AU010319 220010330G8530 VALVE GUIDE CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL ENINE WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 2 AND NR 6 CYLINDER EXHAUST VALVE GUIDES WORN. 1H71 3O3 O A4CE E5CE 5 CP47GL 20010511000362001051100036NM 2001 5 11 AU010320 120010409G7910 OIL SYSTEM DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE ENGINE LOW W C ABORTED TAKEOFF EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NO1 ENGINE OIL LEVEL LOW. SUSPECT OIL LEVEL HAD NOT BEEN TOPPED UP DURING PREFLIGHT INSPECTION. PERSONNEL/MAINTENANCE ERROR. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010511000372001051100037NE 2001 5 11 AU010321 220010410G7320226332003 PIPE LYC ALF502R3A BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R3A 41580NE FUEL CONTROL LOOSE W A UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 AUS (AUS) NO3 ENGINE P3 SENSE LINE TO FCU LOOSE. THE AIRCRAFT HAD A NO3 ENGINE AND FCU CHANGED THE PREVIOUS DAY. PERSONNEL/MAINTENANCEERROR. 2H74 4F4 FRTA49EU E6NE 20010511000382001051100038NM 2001 5 11 AU010322 120010410G5742 MOUNT BOEING767 767277 NM GE CF6 CF680A 30025NE WING CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH WING FITTING OUTBOARD LUG CRACKED DIAGONALLY ACROSS THE UPPERFLANGE FACE THROUGH THE LUG FILLET RADIUS. THE CRACK WAS FOUNDVISUALLY AND CONFIRMED USING NDI. FOUND DURING INSPECTION IAW ERB76-57-40-19. 2L72 4F4 FRTA1NM E13NE 20010511000392001051100039NM 2001 5 11 AU010323 120010409G5742 FITTING BOEING767 767277 NM GE CF6 CF680A 30025NE WING CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT WING FITTING OUTBOARD LUG CRACKED AROUND THE INBOARD AFT CORNER OF THE LUG APPROXIMATELY 10MM (0.393IN) FORWARDAND 5MM (0.196IN) OUTBOARD. CRACK CONFIRMED USING NDI. FOUND DURING INSPECTION IAW ER B76-57-40-18. 2L72 4F4 FRTA1NM E13NE 20010511000402001051100040SO 2001 5 11 AU010324 120010317G5280 DOOR EMB 110 EMB110P2 3260124SO PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL LANDING GEAR DISCONNECTED W C ABORTED TAKEOFF D INFLIGHT SEPARATION TOTAKEOFF 1 AUS (AUS) NOSE LANDING GEAR DOORS DISCONNECTED ON TAKEOFF PREVENTING NOSE LANDING GEAR FROM RETRACTING. SUSPECT DOORS INCORRECTLY ATTACHED. PERSONNEL/MAINTENANCE ERROR. 1L72 4T4 T A21SO E4EA 6 CP15EA 20010511000412001051100041CE 2001 5 11 AU010325 120010326G323057412026 UPLOCK CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C505 GL LANDING GEAR BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH MAIN LANDING GEAR UPLOCK HOOK BROKEN. HOOK WAS AN OLD TYPE. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010511000422001051100042CE 2001 5 11 AU010326 120010410G323045825080 DRAG BRACE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MCAULY3AF34C3AF34C502 GL LANDING GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR AFT DRAG BRACE CRACKED FROM SEALING RIVET. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20010515000012001051500001GL 2001 5 15 AU010327 120010320G2701LS52RS BEARING PAC CT4 CT4A 05623UCGL CONT O360 IO360HB 17025SO HARTZLHCC2Y BHCC2YF1 GL CONTROL COLUMN WORN W O OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 AUS (AUS) RT CONTROL COLUMN TORQUE TUBE BEARING WORN. 1Q71 3I3 ORTA9PC E1CE 5 CP920 20010515000022001051500002CE 2001 5 15 AU010328 120010329G2434ALT9422 ALTERNATOR CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL DC SYSTEM FAILED W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 AUS (AUS) RT ALTERNATOR DISINTEGRATED. SEVERE INTERNAL DAMAGE. SUSPECTCAUSED BY BEARING FAILURE. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010515000032001051500003NM 2001 5 15 AU010329 120010407G5710 DRAIN VALVE BOEING747 747238B 1384828NM RROYCERB211 RB211524D41954555NE WING CLOGGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) DRAINS LOCATED IN WING CENTRE SECTION AFT CAVITY AT BS 1241 WERE BLOCKED BY FOREIGN MATERIALS WITH EIGHT TO TEN LITRES OF WATER PRESENT. TIDE MARKS ALSO PRESENT ON SURROUNDING STRUCTURE INDICATING EVIDENCE OF GREATER QUANTITIES OF WATER RETENTION. 2L74 4F4 F A20WE E12EU 20010515000042001051500004NM 2001 5 15 AU010331 120010413G3520S417T40127 GENERATOR BOEING737 737377 NM GE CFM56 CFM563B1 13802NE PAX OXYGEN FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) OXYGEN GENERATORS LOCATED ABOVE SEATS 9LT, 11LT, 13LT, 15LT AND 17LT HAD THE RELEASE PIN LOCATED IN THE SAFETY PIN HOLE. 2L72 4F4 FRTA16WE E2GL 20010515000052001051500005NM 2001 5 15 AU010332 120010407G2424734284F GCU BOEING767 767338 1385151NM GE CF6 CF680C2* GL AC REGULATOR FAULTY W O OTHER H ELECT. POWER LOSS-50 PC DEDESCENT 1 AUS 21473 (AUS) RH GENERATOR CONTROL UNIT (GCU) FAULTY. 2L72 4F4 FRTA1NM E23EA 20010515000062001051500006SO 2001 5 15 AU010333 220010406G8530539647 PISTON PIN CESSNA182 182Q 2072732CE CONT O470 O470U 17026SO MCAULY2A34C 2A34C203 GL ENGINE FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS 343 (AUS) DURING PRE-PURCHASE INSPECTION IT WAS FOUND THAT THE LOG BOOK ENTRY INDICATED THAT ONLY ONE NEW PISTON PIN HAD BEEN FITTED ANDTHAT THE OTHER FIVE HAD BEEN INSPECTED BY MAGNETIC PARTICLE INSPECTION AND REFITTED. AD/CON/62 AND TCM SB M87-11 REV 2STATES THAT NEW PISTON PINS BE FITTED. OVERHAUL FACILITY STATES THAT ALL OF THE PISTON PINS WERE REPLACED. AN ANOMALY EXISTS BETWEEN THE LOG BOOK AND THE OVERHAUL FACILITY. 1H71 3O3 ONT3A13 E273 5 CP3EA 20010515000072001051500007NM 2001 5 15 AU010334 120010315G52301U1168 ACTUATOR BOEING727 72777C 1380420NM PWA JT8 JT8D15 52051NE CARGO DOOR FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS 495 (AUS) MAIN CARGO DOOR REAR ACTUATOR EYE END BEARING MIGRATED RESULTING IN DISTORTION OF THE EYE END. MINOR DAMAGE TO RETRACTION ARM. 2L73 4F4 F A3WE E2EA 20010515000082001051500008NM 2001 5 15 AU010335 120010405G2910BACH30B01H326R HOSE BOEING747 747238B 1384828NM RROYCERB211 RB211524D41954555NE HYDRAULIC SYSTEMLEAKING W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) LT WING MAIN LANDING GEAR DOOR ACTUATOR FLEXIBLE HOSE LEAKING.LOSS OF HYDRAULIC FLUID. NR 4 ENGINE DRIVEN HYDRAULIC PUMP CHANGED DUE TO OPERATION WITH LOW HYDRAULIC QUANTITY. 2L74 4F4 F A20WE E12EU 20010515000092001051500009NM 2001 5 15 AU010336 120010409G2750 CONTROLLER BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE TE FLAPS FAULTY W O OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 AUS (AUS) DURING APPROACH FLAPS RAN TO 20 DEGREES ON SELECTION OF 25DEGREES. SELECTION TO 30 DEGREES SAW NO FURTHER MOVEMENT. INVESTIGATION COULD FIND NO FAULTS. SUSPECT CAUSED BY MOISTURE IN FLAP DRIVES. 2L72 4F4 FRTA16WE E2GL 20010515000102001051500010WP 2001 5 15 AU010337 120010108G57303787 SKIN DH82A DHAVXXDH82 DH82AROBRTSN2801002WP DHAVXXGIPSY GIPSYMAJOR1 20004WP WINGS PEELING W K NONE O OTHER ININSP/MAINT 1 AUS 73 (AUS) FABRIC COVERING ON WINGS AND TAIL SURFACES HAD PAINT PEELING DUETO PROOFING NOT PENETRATING FABRIC. ALL RIB STITCHING TAPES LOOSE AND NOT ATTACHED TO FABRIC. 1Q71 3I3 I A8EU A8EU 20010515000112001051500011WP 2001 5 15 AU010338 120010108G5711H347377 SPAR DHAVXXDH82 DH82AROBRTSN2801002WP DHAVXXGIPSY GIPSYMAJOR1 20004WP WING CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 73 (AUS) LT UPPER WING MAIN SPAR CRACKED IN SEVERAL PLACES. FURTHER INSPECTION FOLLOWING FABRIC REMOVAL FOUND THAT THE SPAR HAD BEEN DRESSED WITH FILLER AND PAINT UNDER WHICH MORE CRACKS WERE FOUND. 1Q71 3I3 I A8EU A8EU 20010515000122001051500012WP 2001 5 15 AU010339 120010108G5521 SPAR DHAVXXDH82 DH82AROBRTSN2801002WP DHAVXXGIPSY GIPSYMAJOR1 20004WP ELEVATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 73 (AUS) LT ELEVATOR SPAR CRACKED. FOLLOWING FABRIC REMOVAL THE SPAR WAS FOUND TO BE CRACKED IN SEVERAL PLACES INCLUDING AREAS WHICH HAD BEEN BOUND WITH FABRIC. 1Q71 3I3 I A8EU A8EU 20010515000132001051500013EU 2001 5 15 AU010340 120010406G2400 SPLICE BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE ELECTRICAL POWERBURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS (AUS) APU GENERATOR IN LINE SPLICE LOCATED IN THE FORWARD CARGO COMPARTMENT ROOF LINING OVERHEATED AND BURNED. 2H74 4F4 FRTA49EU E6NE 20010515000142001051500014NM 2001 5 15 AU010341 120010409G323065B0154020 ACTUATOR BOEING747 747SP38 NM RROYCERB211 RB211524D41954555NE MLG FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 8931 (AUS) RT WING LANDING GEAR DOWNLOCK ACTUATOR SUFFERED A CATASTROPHIC FAILURE. THE FAILURE OCCURRED DURING THE FIRST OPERATION OF THE ACTUATOR WHICH HAD JUST BEEN FITTED FOLLOWING MAINTENANCE. 2L74 4F4 FRTA20WE E12EU 20010515000152001051500015NE 2001 5 15 AU010342 220010407G7200 ENGINE BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 4 FLAMED OUT W O OTHER EX VIBRATION/BUFFET ENGINE FLAMEOUT DEDESCENT 1 AUS (AUS) NR 4 ENGINE FLAMEOUT. LIMITED INFORMATION PROVIDED. 2H74 4F4 F A49EU E6NE 20010515000162001051500016NE 2001 5 15 AU010343 220010416G7261ST307607 KEY DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE NR 1 ENGINE MISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 1 ENGINE AC GENERATOR OIL SYSTEM SCAVENGE PUMP WOODRUFF KEY NOT FITTED. KEY WAS FOUND LOOSE IN THE BOTTOM OF THE PUMP HOUSING.SUSPECT KEY FELL OUT DURING ASSEMBLY WITHOUT BEING NOTICED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010515000172001051500017EU 2001 5 15 AU010344 120010410G3234 MOTOR BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE MLG FAULTY W O OTHER J WARNING INDICATION CLCLIMB 1 AUS (AUS) LANDING GEAR SELECTOR VALVE ACTUATOR MOTOR FAULTY. 2H74 4F4 FRTA49EU E6NE 20010515000182001051500018EU 2001 5 15 AU010345 120010416G2421 IDG BAG BAE146BAE146200A 1500266EU CFMINTCFM56 CFM565A1 NE AC GENERATOR FAILED W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 AUS (AUS) INTEGRATED DRIVE GENERATOR (IDG) FAILED. 2H74 4F4 FRTA49EU E29NE 20010515000192001051500019NM 2001 5 15 AU010346 120010412G2133 MOTOR BOEING737 737377 NM GE CFM56 CFM563B1 13802NE OUTFLOW VALVE FAILED W O OTHER O OTHER DEDESCENT 1 AUS (AUS) AIRCRAFT PRESSURISATION SYSTEM OUTFLOW VALVE ELECTRIC MOTOR FAILED. OUTFLOW VALVE FAILED TO OPEN. 2L72 4F4 FRTA16WE E2GL 20010515000202001051500020SO 2001 5 15 AU010347 220010407G8530 ROCKER BOSS CESSNA206 U206E 2073350CE CONT O520 IO520F 17032SO HARTZLHCC3Y HCC3YF1 GL ENGINE CRACKED W C ABORTED TAKEOFF ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AUS (AUS) ENGINE CYLINDER ROCKER HATS (2OFF) CRACKED AT PUSHROD END. EVIDENCE OF ROCKER HAT CONTACT ON THREE OTHER CYLINDERS. 1H71 3O3 O A4CE E5CE 5 CP25EA 20010515000212001051500021NM 2001 5 15 AU010348 120010417G2910AS4624J0300SS HOSE BOEING767 767338 1385151NM GE CF6 CF680C2* GL HYDRAULIC SYSTEMLEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR CENTER SYSTEM TILT RETURN HOSE LEAKING. 2L72 4F4 FRTA1NM E23EA 20010515000222001051500022NM 2001 5 15 AU010349 120010414G2910 HOSE BOEING767 767330 NM RROYCERB211 RB211524* NE HYDRAULIC SYSTEMSPLIT W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR UPLINE PRESSURE HOSE SPLIT. 2L72 4F4 FRTA1NM E12EU 20010515000232001051500023NE 2001 5 15 AU010350 220010318G7397 WIRE BOEING747 747438 NM RROYCERB211 RB211524G19 NE FUEL CONTROL WORN W O OTHER E VIBRATION/BUFFET CLCLIMB 1 AUS (AUS) NR 4 ENGINE FUEL SYSTEM WIRE CHAFED AND SHORT CIRCUITING. WIRE W6400-008-18R WAS LOCATED IN NR 4 STRUT KNEECAP DISCONNECT PLUGD14300P. 2L74 4F4 FRTA20WE E30NE 20010515000242001051500024 2001 5 15 AU010351 420010409G2565101651303 SLIDE BOEING767 767204 NM GE CF6 CF680A 30025NE ESCAPE SLIDE MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ESCAPE SLIDE FITTED TO DOOR LT 1 INCORRECTLY FITTED FOLLOWINGHEAVY MAINTENANCE. INSPECTION FOUND THAT THE SLIDE BAR WAS IN THE STOWED (TRANSPORT) POSITION AND WAS NOT CONNECTED TO THE GIRT BAR. FURTHER INVESTIGATION FOUND THAT THE ESCAPE SLIDES ONTHE OTHER THREE DORS (LH2, RH1 AND RH2) WERE SIMILARLY INCORRECTLY FITTED. PERSONNEL/MAINTENANCE ERROR. 2L72 4F4 FRTA1NM E13NE 20010515000252001051500025CE 2001 5 15 AU010352 120010409G271035521189 CONTROL CABLE BEECH 35 S35 1151532CE CONT O520 IO520B 17032SO HARTZLHCC3Y PHCC3YF1 GL AILERON CONTROL BROKEN W O OTHER F FLT CONT AFFECTED LDLANDING 1 AUS (AUS) AILERON THREADED CABLE AND FITTING SEPARATED APPROXIMATELY MIDWAY BETWEEN THE THREADED END AND THE SWAGED NUT. 1L71 3O3 O 3A15 E5CE 5 CP25EA 20010515000262001051500026EA 2001 5 15 AU010353 220010413G8520L2363440A GEAR BNORM BN2 BN2A8 1520209EU LYC O540 O540E4C5 41532EA HARTZLHCC2Y HCC2YK2 GL ENGINE CRANK FAILED W A UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 AUS (AUS) CRANKSHAFT DRIVE GEAR FAILED. 1H72 3O3 O A17EU E295 5 CP920 20010515000272001051500027NM 2001 5 15 AU010354 120010405G5320 WEB BOEING747 747338 NM FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT VERTICAL BEAM WEB OF NOSE WHEEL STRUCTURE CRACKED FROM INSULATION BLANKET STUD HOLE AT BS 320. FOUND DURING INSPECTION IAW EI 747-053-0041 REV5. 2L72 4F RTA20WE 20010515000282001051500028 2001 5 15 AU010355 420010417G256561621469 SLIDE BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU PAX DOOR MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 AUS 875 (AUS) MAIN ENTRY DOOR ESCAPE SLIDE SAFETY PIN INSTALLED. 2L72 4F4 FRTA16WE E21EU 20010515000292001051500029NM 2001 5 15 AU010356 120010417G2752734374D ACTUATOR DHAV DHC8 DHC8103 1386005NM PWA 120 PW123D 52152NE HAMSTD14SF 14SF23 NE TE FLAPS WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TRAILING EDGE FLAP ACTUATORS (3OFF) HAD EXCESSIVE BACKLASH. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010515000302001051500030NM 2001 5 15 AU010357 120010417G2752734374D ACTUATOR DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE HAMSTD14SF 14SF7 NE TE FLAPS WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TRAILING EDGE FLAP ACTUATORS (2OFF) HAD EXCESSIVE BACKLASH. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010515000312001051500031NM 2001 5 15 AU010358 120010417G2752734374D ACTUATOR DHAV DHC8 DHC8315 2809010NM TE FLAPS WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TRAILING EDGE FLAP ACTUATORS (6OFF) HAD EXCESSIVE BACKLASH. 2H72 4T RTA13NM 20010515000322001051500032NM 2001 5 15 AU010359 120010417G2752734374D ACTUATOR DHAV DHC8 DHC8* NM TE FLAPS WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TRAILING EDGE FLAP ACTUATORS (6OFF) HAD EXCESSIVE BACKLASH. 2H72 4T RTA13NM 20010515000332001051500033SO 2001 5 15 AU010360 120010419G52804752932 HINGE PIPER PA31 PA31 7103102SO LYC O540 TIO540A1A 41532EA HARTZLHCE3Y HCE3YR2 GL MLG DOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT MAIN LANDING GEAR INBOARD DOOR FORWARD HINGE ARM CRACKED ONINNER RADIUS. FOUND DURING DYE PENETRANT INSPECTION IAW PIPER MSB 682. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010515000342001051500034 2001 5 15 AU010361 420010417G2565D31591475 SLIDE BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU PAX DOOR FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS 8870 (AUS) MAIN ENTRY DOOR ESCAPE SLIDE FAILED TO INFLATE DUE TO DAMAGE TO THE ASPIRATOR FLAPPER VALVE SUPPORT BRIDGE. INVESTIGATION FOUND THE BRIDGE TO BE LOOSE AND TWISTED PREVENTING THE FLAPPER VALVE HALVES FROM SEATING. 2L72 4F4 FRTA16WE E21EU 20010515000352001051500035EU 2001 5 15 AU010362 120010331G2130K1813 RELAY FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY62015 04564NE PRESSURE CONTROLFAILED W C ABORTED TAKEOFF O OTHER TOTAKEOFF 1 AUS (AUS) PRESSURISATION SYSTEM FAULTY. SUSPECT CAUSED BY HIGH RESISTANCE ACROSS CONTACTS IN RELAYS K1813, K1261, K1819 AND K1821 IN THEGROUND/FLIGHT RELAY BOX. 2L72 4F4 FRT E25NE 20010515000362001051500036CE 2001 5 15 AU010363 120010412G324422X775X10X10 TIRE CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL LT MLG LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS 119 (AUS) LT MAIN WHEEL TYRE CONTAINED A SLOW LEAK FROM ONE OF THE SIDEWALL VENT HOLES. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20010515000372001051500037SO 2001 5 15 AU010364 220010410G8520632043 CONNECTING ROD CONT GTSIO510M CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL ENGINE DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS 1598 272103R (AUS) NR6 CONNECTING ROD RUBBING ON COUNTERWEIGHT. ROD WAS OUT OF ALIGNMENT WITH THE BIG END AND SMALL END AXIS. INSPECTION FOUND THAT THREE COUNTERWEIGHTS HAD MATERIAL GROUND FROM THE BOTTOM SURFACE. THE CRANKCASE WAS ALSO UNSERVICEABLE DUE TO THE BREAKUP OF THE SECOND REAR LT SIDE BEARING SADDLE. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010515000382001051500038EU 2001 5 15 AU010365 120010327G7933 INDICATOR FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY62015 04564NE ENGINE OIL FAULTY W C ABORTED TAKEOFF EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NR 1 ENGINE OIL TEMPERATURE INDICATION SYSTEM FAULTY. WIRING AND INSULATION CHECKED WITH NO FURTHER PROBLEMS. CONNECTORS CLEANED AND INSPECTED. PROBLEM HAS NOT REOCCURRED. 2L72 4F4 FRT E25NE 20010515000392001051500039SO 2001 5 15 AU010366 120010403G6123 CONNECTOR EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF7 NE AUTOFEATHER SYS FAULTY W O OTHER J WARNING INDICATION TOTAKEOFF 1 AUS (AUS) AUTOFEATHER SYSTEM FAULTY. INSPECTION OF THE SYSTEM AND CLEANING OF CONNECTOR PLUGS CARRIED OUT. NO DEFECTS EVIDENT. 2L72 4T4 TRTA31SO E20NE 6 CP7NE 20010515000402001051500040SO 2001 5 15 AU010367 120010223G32216705403 TRUNNION PIPER PA32 PA32R300 7103213SO LYC O540 IO540K1G5 41532EA HARTZLHCC2Y HCC2YK1 GL NLG FRACTURED W O OTHER P NO WARNING INDICATION LDLANDING 1 AUS (AUS) NOSE LANDING GEAR TRUNNION FRACTURED THROUGH THE DRAG LINKATTACHMENT BOLT HOLE. 1L71 3O3 O A3SO 1E4 5 CP920 20010515000412001051500041NE 2001 5 15 AU010368 220010330G8530L2144448A CYLINDER PIPER PA60 PA60602P 7106015NM LYC O540 IO540AA1A 41532NE HARTZLHCC3Y HCC3YR2 NE ENGINE DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT ENGINE CYLINDERS AND PISTONS DAMAGED BY DETONATION. 1M72 3O3 ORTA17WE 1EA 5 CP25EA 20010507004022001050700402NE 2001 5 7 AU010369 120010420G55317620105501101 SPAR CAP SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE VERTICAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) VERTICAL STABILISER FORWARD RH SPAR CAP ANGLE LOCATED AT VS117.25 CRACKED IN THE AREA WHERE THE RIVETS ATTACH THE TOP RIB TO THEANGLE. 1G72 3U3 UNCH1NE E19EU 20010515000422001051500042NM 2001 5 15 AU010370 120010422G56108SC00430780205 WINDSHIELD DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE COCKPIT CRACKED W O OTHER O OTHER LDLANDING 1 AUS (AUS) CAPTAINS WINDSHIELD OUTER PANE CRACKED. CRACK ORIGINATED AT THE HEATER ELEMENT. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010515000432001051500043EA 2001 5 15 AU010371 220010418G8550LW13388 SEAL PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR2 GL ENGINE DETERIORATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE OIL FILTER CONVERTER PLATE SEAL DETERIORATED. REFER TO AD/LYC105. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010515000442001051500044NM 2001 5 15 AU010372 120010421G326011300105 UPLOCK DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE LT MLG FAULTY W O OTHER J WARNING INDICATION CLCLIMB 1 AUS (AUS) LT MAIN LANDING GEAR UPLOCK LATCHING SPRINGS FAULTY. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010515000452001051500045NM 2001 5 15 AU010373 120010420G29109741735 HOSE BOEING747 747438 NM RROYCERB211 RB211524G19 NE HYDRAULIC SYSTEMFAILED W O OTHER J WARNING INDICATION APAPPROACH 1 AUS (AUS) NR 1 HYDRAULIC PUMP PRESSURE HOSE FAILED. LOSS OF HYDRAULIC FLUID. 2L74 4F4 FRTA20WE E30NE 20010515000462001051500046NM 2001 5 15 AU010374 120010422G716012788 PANEL BOEING747 747338 NM RROYCERB211 RB211524G19 NE AIR INTAKE DELAMINATED W O OTHER E VIBRATION/BUFFET TOTAKEOFF 1 AUS 1749 (AUS) NR 1 ENGINE ICE IMPACT PANEL DELAMINATED FROM THE 5 OCLOCK POSITION THROUGH TO THE 11 OCLOCK POSITION. DELAMINATED MATERIAL WAS CAUGHT IN THE INLET GUIDE VANES. BOROSCOPE INSPECTION FOUND NIL INTERNAL DAMAGE. 2L72 4F4 FRTA20WE E30NE 20010515000472001051500047NM 2001 5 15 AU010375 120010420G2910 HYDRAULIC SYSTEM BOEING737 737377 NM A SYSTEM LOW W O OTHER K FLUID LOSS LDLANDING 1 AUS (AUS) HYDRAULIC A SYSTEM QUANTITY AND PRESSURE LOST. 2L72 4F RTA16WE 20010515000482001051500048NM 2001 5 15 AU010376 120010420G2750 CONTROLLER BOEING737 737377 NM TE FLAPS FAULTY W O OTHER F FLT CONT AFFECTED LDLANDING 1 AUS (AUS) FLAPS FAILED TO MOVE PAST 15 DEGREES. 2L72 4F RTA16WE 20010515000492001051500049 2001 5 15 AU010377 420010420G25657A13946 SLIDE BOEING767 767338 1385151NM GE CF6 CF680C2* GL PAX DOOR MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS 10430 GV198 (AUS) NR 1 LH MAIN ENTRY DOOR ESCAPE SLIDE SAFETY PIN INSTALLED. PERSONNEL/MAINTENANCE ERROR. 2L72 4F4 FRTA1NM E23EA 20010515000502001051500050WP 2001 5 15 AU010378 120010418G5511 SPAR DHAVXXDH82 DH82AROBRTSN2801002WP DHAVXXGIPSY GIPSYMAJOR1 20004WP HORIZONTAL STAB DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HORIZONTAL STABILISER REAR SPAR DAMAGED. 1Q71 3I3 I A8EU A8EU 20010515000512001051500051EU 2001 5 15 AU010379 120010406G2760P308450070 SWITCH BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE DRAG CONTROL FAULTY W O OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 AUS (AUS) LT AND RT OUTBOARD SPOILER MICROSWITCHES FAULTY. 2H74 4F4 F A49EU E6NE 20010515000522001051500052 2001 5 15 AU010380 420010422G3423 COMPASS BOEING737 737377 NM COCKPIT FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) BUBBLE IN COMPASS FLUID. FOUND DURING INSPECTION IAW AD/INST/9. 2L72 4F RTA16WE 20010515000532001051500053 2001 5 15 AU010381 420010423G3423 COMPASS BOEING737 737377 NM COCKPIT FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AIR BUBBLE IN STANDBY COMPASS. FOUND DURING INSPECTION IAWAD/INST/9. 2L72 4F RTA16WE 20010507004032001050700403GL 2001 5 7 AU010382 220010426G72506898785 SHAFT SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL TURBINE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 3464 CAG90756 (AUS) ENGINE GEARBOX POWER TAKEOFF SHAFT CRACKED. SUSPECT CAUSED BY OVERTIGHTENING OF THE POWER OUTPUT ADAPTER. 1G72 3U3 U H1NE E1GL 20010515000542001051500054NM 2001 5 15 AU010383 120010424G5313 STRINGER BOEING767 767204 NM GE CF6 CF680A 30025NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) STRINGER 32L LOCATED AT STN 1085 CRACKED. CRACK LENGTH 114.3MM(4.5IN). 2L72 4F4 FRTA1NM E13NE 20010515000552001051500055 2001 5 15 AU010385 420010423G2312 RADIO AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE VHF SYSTEM FAILED W O OTHER O OTHER DEDESCENT 1 AUS (AUS) VHF SYSTEM FAULTY. 2L72 4F4 FRTA28NM E29NE 20010515000562001051500056SO 2001 5 15 AU010386 120010402G2750487377 SPRING PIPER PA32 PA32300 7103212SO LYC O540 IO540K1A5 41532EA HARTZLHCC2Y HCC2YK1 GL TE FLAPS BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLAP RETURN SPRING FAILED AT ATTACHMENT HOOK. 1L71 3O3 O A3SO 1E4 5 CP920 20010515000572001051500057NM 2001 5 15 AU010387 120010426G27512061141 INDICATOR BOEING737 73733A 1384673NM TE FLAPS FAULTY W O OTHER J WARNING INDICATION APAPPROACH 1 AUS (AUS) FLAP POSITION INDICATOR FAULTY. 2L72 4F RTA16WE 20010515000582001051500058CE 2001 5 15 AU010388 120010412G32607401CGE SWITCH CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C87 GL MLG INTERMITTENT W K NONE N FALSE WARNING LDLANDING 1 AUS (AUS) MAIN LANDING GEAR WARNING LIGHT DIMMER SWITCH INTERMITTENT IN OPERATION. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010515000592001051500059NE 2001 5 15 AU010389 220010423G732078639010 HMU EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE RT ENGIEN FAULTY W O OTHER ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) RT ENGINE HYDROMECHANICAL UNIT (HMU) FAULTY. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010807000802001080700080NM 2001 8 7 AUS20010391 120010430G5313 STRINGER BOEING767 767277 NM GE CF6 CF680A 30025NE FUSELAGE MAIN, LCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) STRINGER 39L LOCATED BELOW THE FLOOR IN THE AFT CARGO AREACORRODED BETWEEN BS 1285 AND BS 1307. 2L72 4F4 FRTA1NM E13NE 20010808000012001080800001EU 2001 8 8 AUS20010392 120010425G2430 GENERATOR AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE DC GENERATING SYFAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) DC GENERATION SYSTEM FAULTY. 2L72 4F4 FRTA46NM E29NE 20010808000022001080800002NM 2001 8 8 AUS20010393 120010426G2720 PCU BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU RUDDER CONTROL FAULTY W K NONE F FLT CONT AFFECTED CLCLIMB 1 AUS (AUS) RUDDER CONTROL SYSTEM FAULTY. NUMEROUS ITEMS IN THE CONTROL SYSTEM WERE REPLACED TO CORRECT THE PROBLEM. INVESTIGATION IS CONTINUING INTO THE REPLACED ITEMS. ITEMS REPLACED WERE DFDR PNO 2100-4043-00, RUDDER PCU PNO 65C37053-9, STANDBY RUDDERPCU PNO 1U1150-3 AND YAW DAMPER COUPLER PNO 4030952-906. 2L72 4F4 FRTA16WE E21EU 20010808000032001080800003NM 2001 8 8 AUS20010394 120010424G7110UL26237 FAIRING RROYCE RB211524G BOEING747 747438 NM RROYCERB211 RB211524G19 NE ENGINE COWLING SEPARATED W C ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 AUS 13461 13043 (AUS) NR 3 ENGINE LT AND RT GAS GENERATOR FAIRINGS PNO UL26237 AND PNO UL23239 SEPARATED FROM ENGINE. DAMAGE TO NR 3 ENGINE INTEGRATEDNOZZLE AREA AND RT C' FLAP. 2L74 4F4 FRTA20WE E30NE 20010807000812001080700081SO 2001 8 7 AUS20010395 120010426G2430460620 FILTER PIPER 460620 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL DC GENERATING SYINTERMITTENT W K NONE H ELECT. POWER LOSS-50 PC CRCRUISE 1 AUS (AUS) LH NOISE FILTER INTERMITTENT IN OPERATION. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010808000072001080800007NM 2001 8 8 AUS20010396 120010428G3260 SENSOR BOEING737 737377 NM LANDING GEAR FAILED W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) AIR SENSING TEST CARD FAILED. 2L72 4F RTA16WE 20010808000162001080800016NM 2001 8 8 AUS20010398 120010429G3520S417T40127 GENERATOR BOEING737 737377 NM PASSENGER OXYGENMISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) OXYGEN GENERATORS LOCATED IN THE FLIGHT ATTENDANT SERVICE UNITADJACENT TO CABIN DOORS L1 AND L2 HAD THE RELASE PINS LOCATED INTHE SAFETY PIN HOLES. PERSONNEL/MAINTENANCE ERROR. 2L72 4F RTA16WE 20010807000822001080700082NM 2001 8 7 AUS20010399 120010502G3230EO3600491750S SPRING ROTOL ACTUATOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE LANDING GEAR RETFAILED W K NONE O OTHER ININSP/MAINT 1 AUS DCL30093 (AUS) UPLOCK ACTUATOR SPRING (1OFF2) BROKEN AT THE BASE OF THE UPPERATTACHMENT HOOK. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010808000182001080800018NM 2001 8 8 AUS20010400 120010501G711013453 PANEL RROYCE RB211524H36 BOEING767 767338 1385151NM RROYCERB211 RB211524* NE ENGINE COWLING SEPARATED W K NONE O OTHER ININSP/MAINT 1 AUS 11290 13453 (AUS) NR 1 ENGINE ACOUSTIC PANEL TRAILING EDGE SECTION SEPARATED FROMTHE AIRCRAFT. NR 5 BLOCKER DOOR REPLACED DUE TO DAMAGE. NR 7, NR 8 AND NR 9 BLOCKER DOORS HAD MINOR SKIN DAMAGE. NR 7 DEFLECTOR BOX CASCADE VANE DAMAGED. 2L72 4F4 FRTA1NM E12EU 20010808000202001080800020EU 2001 8 8 AUS20010401 120010416G2450 SPLICE BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE AC POWER DIST OVERHEATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) GENERATOR FEEDER INLINE SPLICE OVERHEATING. FOUND DURINGINSPECTION IAW TSI 146-24-003. 2H74 4F4 FRTA49EU E6NE 20010807000832001080700083NM 2001 8 7 AUS20010402 120010503G3230EO3600491750S SPRING ROTOL ACTUATOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE LANDING GEAR RETBROKEN W K NONE O OTHER ININSP/MAINT 1 AUS DCL30293DCL2 (AUS) LH AND RH MAIN LANDING GEAR UPLOCK ACTUATOR SPRINGS BROKEN. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010808000212001080800021NM 2001 8 8 AUS20010403 120010502G5730 SKIN BOEING737 73733A 1384673NM WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT WING UPPER SKIN LOWER SURFACES AND TOP STRINGERS IN AREA BETWEEN WS557 AND WS583. CORROSION ALSO EVIDENT ON RH REAR SPAR LOWER FLANGE IN AREA BETWEEN WS576 AND WS580. 2L72 4F RTA16WE 20010808000222001080800022EU 2001 8 8 AUS20010404 120010420G5320D5337061320200 FITTING AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR DOOR ACTUATOR FITTINGS (KEEL BEAM) CRACKED. CRACKS FOUND IN LH AFT FITTING PNO D5337061320200 RH AFT AND LH FORWARD FITTINGS PNO D5337961320300. CRACKS EMANATE FROM THE TOPTWO FASTENER HOLES IN THE VERTICAL FLANGE. FOUND DURING INSPECTION IAW ER A32-53-40-9C (SB A320-53-1135). 2L72 4F4 FRTA46NM E29NE 20010807000842001080700084WP 2001 8 7 AUS20010405 120010421G7920R14 FILTER LYC O320B2C ROBSINR22 R22 7640102WP LYC O320 O320B2C 41508EA ENGINE OIL DISTRLEAKING W K NONE EK VIBRATION/BUFFET FLUID LOSS TOTAKEOFF 1 AUS (AUS) ENGINE OIL FILTER O' RING SEAL POPPED OUT ALLOWING OIL TO BE PUMPED OVERBOARD. THE RYCO R14 OIL FILTER IS FITTED TO SOME R22 AIRCRAFT BY AN ENGINEERING ORDER. 1G71 3O3 O H10WE E274 20010807000852001080700085NM 2001 8 7 AUS20010406 120010430G7110LK73708 PANEL RROYCE RB211524D419BOEING747 747238B 1384828NM RROYCERB211 RB211524D41954555NE ENGINE COWLING SSEPARATED W K NONE OD OTHER INFLIGHT SEPARATION ININSP/MAINT 1 AUS 7466 12679 (AUS) NO4 ENGINE VIGV CONTROLLER ACCESS PANEL SEPARATED. DAMAGE CAUSEDTO THE REAR FAN CASE ACOUSTIC LINER. 2L74 4F4 F A20WE E12EU 20010808000232001080800023EA 2001 8 8 AUS20010407 220010430G7310689 LINE PILATSPC6 PC6 7090102EU PWA PT6 PT6A20 52043EA HARTZLHCB3T HCB3TN3 GL FUEL DIST CONTAMINATED W O OTHER EX VIBRATION/BUFFET ENGINE FLAMEOUT LDLANDING 1 AUS (AUS) ENGINE FAILED DUE TO LACK OF FUEL. INVESTIGATION FOUND AIR IN THE FUEL LINE BETWEEN THE FUEL HEATER AND THE FCU. SUSPECT CAUSED BYPOOR VENTING OF THE FUEL HEADER TANK. AD/PC6/42 (PC-6-SB-171) ISENTERED INTO THE LOG BOOK AS HAVING BEEN COMPLIED WITH BUT HASNOT BEEN CARRIED OUT. THE AD AND SB INTRODUCES A VENTING SYSTEM TO THE HEADER TANK. PERSONNEL/MAINTENANCE ERROR. 1H71 3O3 T 7A15 E4EA 6 CP15EA 20010807000862001080700086SO 2001 8 7 AUS20010408 220010510G8550CH48109 FILTER CONT TSIO520VB CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C505 GL RECIPROCATING ENFAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE OIL FILTER ELEMENT END CAP MISSING. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010808000242001080800024NE 2001 8 8 AUS20010409 320010503G6110 PROPELLER BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C653 NE RIGHT OUT OF BALANCE W O OTHER E VIBRATION/BUFFET CLCLIMB 1 AUS (AUS) RT PROPELLER OUT OF BALANCE. PROPELLER HAD BEEN RECENTLY REPLACED BUT HAD NOT BEEN BALANCE CHECKED FOLLOWING FITMENT. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010807000872001080700087 2001 8 7 AUS20010410 420010513G3416WL1107AMMS4 ALTIMETER BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE ALTIMETER, BAROMFAILED W K NONE I FLT. ATTITUDE INST. CLCLIMB 1 AUS 24008 AF756 (AUS) CAPTAINS ALTIMETER FAILED. 2H74 4F4 F A49EU E6NE 20010808000252001080800025SO 2001 8 8 AUS20010411 120010507G3260 SWITCH PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL MLG OUT OF ADJ W K NONE N FALSE WARNING CLCLIMB 1 AUS (AUS) NOSE LANDING GEAR UP LIMIT SWITCH OUT OF ADJUSTMENT. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010808000262001080800026CE 2001 8 8 AUS20010412 120010423G5320MS21047L3 NUT CESSNA303 T303 2073820CE CONT O520 TSIO520AE 17040SO MCAULY3AF32C3AF32C506 GL FUEL CELL WRONG PART W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) LH WING FUEL TANK LEAKING. INVESTIGATION FOUND THAT THE FUEL TANK PANEL ANCHOR NUTS WERE THE INCORRECT TYPE. THE CORRECT NUTS PNO NAS1473A3 ANCHOR NUTS ARE SEALED BUT THE FITTED ANCHOR NUTS PNO MS21047L3 ARE UNSEALED. MANUFACTURING ERROR. UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A34CE E8CE 5 CP57GL 20010807000882001080700088NM 2001 8 7 AUS20010413 120010511G6322A1851 BRACKET ROBSINR22 R22BETA NM LYC O320 O320B2C 41508EA ROTORCRAFT COOLICRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) COOLING FAN SCROLL BRACKET CRACKED. CRACK ORIGINATED AT A SIDESCREWDRIVER NOTCH. FOUND DURING INSPECTION IAW AD/R22/24. 1G71 3O3 O H10WE E274 20010808000272001080800027CE 2001 8 8 AUS20010414 120010504G5720 RIVET CESSNA337 337 2075702CE CONT O360 IO360D 17025SO WING LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING STRUT ATTACHMENT RIB TO OUTBOARD TIP RIVETS LOOSE AND MISSING. LEADING EDGE HAD BEEN REPLACED IN 1972. 1H72 3O3 O A6CE E1CE 20010808000292001080800029CE 2001 8 8 AUS20010415 120010504G3246 WHEEL CESSNA337 337 2075702CE CONT O360 IO360D 17025SO MLG CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE AND MAIN WHEEL HALVES (5OFF6) CORRODED WITH BEARINGS SPINNING IN THE WHEEL HALVES. CORROSION ALSO FOUND IN AREA OF THE FELT SEALS. 1H72 3O3 O A6CE E1CE 20010808000302001080800030SO 2001 8 8 AUS20010416 220010504G8550 FILTER CESSNA337 337 2075702CE CONT O360 IO360D 17025SO ENGINE CONTAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) METAL CONTAMINATION OF THE REAR ENGINE OIL FILTER. SUSPECT MAIN BEARING FAILURE. 1H72 3O3 O A6CE E1CE 20010808000322001080800032CE 2001 8 8 AUS20010417 120010504G5311 FRAME CESSNA337 337 2075702CE CONT O360 IO360D 17025SO FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT ROOF SUPPORT FORMER LOWER EDGE CONTAINED INTERGRANNULARCORROSION. 1H72 3O3 O A6CE E1CE 20010808000332001080800033CE 2001 8 8 AUS20010418 120010504G5310 RIVET CESSNA337 337 2075702CE CONT O360 IO360D 17025SO FUSELAGE DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR WHEEL PAN/FIREWALL STRUCTURE RIVETS PULLED. FAILED RIVETS LOCATED IN THE AFT LT TOP CORNER. 1H72 3O3 O A6CE E1CE 20010808000342001080800034CE 2001 8 8 AUS20010419 120010504G2720 TORQUE TUBE CESSNA337 337 2075702CE CONT O360 IO360D 17025SO RUDDER CONTROL DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RUDDER PEDAL TORQUE TUBE CLAMP SUPPORT STRUCTURE CRACKED ANDWORKING. LOOSE RIVETS AND DAMAGE CAUSED BY BELLCRANK. 1H72 3O3 O A6CE E1CE 20010808000572001080800057CE 2001 8 8 AUS20010420 120010504G2823 SELECTOR VALVE CESSNA337 337 2075702CE CONT O360 IO360D 17025SO FUEL SYSTEM FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FRONT AND REAR FUEL SELECTORS FAULTY. FUEL CAN'T BE TURNED OFF. SUSPECT FAULTY SEALS. 1H72 3O3 O A6CE E1CE 20010808000672001080800067EU 2001 8 8 AUS20010421 120010514G262157333012 FIRE BOTTLE BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE NR 3 ENGINE MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) NR 3 ENGINE FIRE BOTTLE FIRING SWITCH WIRING CONTAINED TWO INLINESPLICES FITTED WITH SMALLER GAUGE WIRES. UNAPPROVED MODIFICATION. PERSONNEL/MAINTENANCE ERROR. 2H74 4F4 FRTA49EU E6NE 20010807000892001080700089CE 2001 8 7 AUS20010422 120010515G270107606331 BEARING CESSNA182 R182 2072734CE LYC O540 O540J3C5 41532EA MCAULY2D34C B2D34C214 GL CONTROL COLUMN SFAILED W K NONE F FLT CONT AFFECTED CRCRUISE 1 AUS 3847 (AUS) COPILOTS CONTROL COLUMN BEARING BLOCK NEEDLE ROLLER BEARING WORNOUT AND THE ROLLERS DISLODGED DUE TO LACK OF LUBRICATION. THE ROLLER BEARING SHAFT GROOVED FROM VIBRATION INDUCED WEAR. 1H71 3O3 ORT3A13 E295 5 CP7EA 20010808000802001080800080 2001 8 8 AUS20010423 420010507G34257003360941 INDICATOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE AHRS FAILED W O OTHER F FLT CONT AFFECTED CLCLIMB 1 AUS (AUS) NR 1 ATTITUDE HEADING REFERENCE SYSTEM (AHRS) FAILED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010808000812001080800081 2001 8 8 AUS20010424 420010503G34166223890002 TRANSCEIVER BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE ALTIMETER INTERMITTENT W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RADIO ALTIMETER TRANSCEIVER INTERMITTENT OPERATION. INVESTIGATION FOUND THE FAULT WAS DUE TO A STRAY VOLTAGE ON A SPARE PIN IN THETRANSCEIVER DUE TO A WIRE FITTED BY A PREVIOUS OPERATOR. THEMODIFICATION WAS NOT NOTIFIED TO THE MANUFACTURER AND THE WIRINGDIAGRAMS WERE NOT AMENDED. PERSONNEL/MAINTENANCE ERROR. 2H74 4F4 FRTA49EU E6NE 20010808000832001080800083SO 2001 8 8 AUS20010425 120010507G5510717002 HINGE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL HORIZONTAL STAB MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT HORIZONTAL STABILISER OUTBOARD HINGES FITTED WITH ONLYTWO RIVETS ON THE TOP AND BOTTOM WHEN THE PIPER MODIFICATION KITPNO 766-646 WHEN THE CORRECT NUMBER SHOULD BE FOUR RIVETS.PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010808000842001080800084CE 2001 8 8 AUS20010426 120010507G555112326231 FITTING CESSNA206 U206F 2073333CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AFT TAILPLANE ATTACHMENT REINFORCEMENT CRACKED. 1H71 3O3 O A4CE E5CE 5 CP21EA 20010807000902001080700090EU 2001 8 7 AUS20010427 120010506G555313708F2 HINGE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP MCAULY4HFR344HFR34C653 NE VERTICAL STABILIBROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RUDDER CENTRE HINGE BRACKET CENTRE LUG FAILED DUE TO CORROSION. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010807000912001080700091EU 2001 8 7 AUS20010428 120010506G55541379036F403 HINGE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP MCAULY4HFR344HFR34C653 NE RUDDER/TAB, ATTACRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RUDDER CENTRE HINGE CRACKED. SUSPECT CAUSED BY EXTRA LOADS DUE TO FAILURE OF THE FIN MOUNTED HALF OF THE HINGE. SEE MDR 01/0427. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010807000922001080700092NM 2001 8 7 AUS20010429 120010424G6310A1843 BEARING ROBSINR22 R22BETA NM LYC O320 O320B2C 41508EA ENGINE/TRANSMISSSPALLED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) UPPER BEARING ROUGH. ONE BALL BADLY SPALLED. 1G71 3O3 O H10WE E274 20010807000932001080700093EU 2001 8 7 AUS20010430 120010504G5711D53 FLANGE PARTEN P68B PARTENP68 P68B EU LYC O360 IO360A1B6 41514EA HARTZLHCC2Y HCC2YK2 GL WING SPAR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS D53 (AUS) AFT WING SPAR WEB FLANGE CRACKED ON THE LH SIDE IN THE AREA OUTBOARD OF THE ATTACHMENT FITTING. FOUND DURING INSPECTION IAW AD/P68/22, AD/P68/45 AND SB 65. 1H72 3O3 O A31EU 1E10 5 CP920 20010807000942001080700094CE 2001 8 7 AUS20010431 120010115G5347121040821 SEAT TRACK CESSNA206 U206F 2073333CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL SEAT/CARGO ATTACCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) SEAT TRACKS CRACKED THROUGH STOP PIN HOLES. 1H71 3O3 O A4CE E5CE 5 CP21EA 20010807000952001080700095CE 2001 8 7 AUS20010432 120010115G531212121365 BULKHEAD CESSNA206 U206F 2073333CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL FUSELAGE MAIN, BCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HORIZONTAL STABILISER ATTACHMENT BULKHEAD CRACKED THROUGH TOP RIVET HOLE. CRACK LENGTH 19.05MM (0.75IN). 1H71 3O3 O A4CE E5CE 5 CP21EA 20010807000962001080700096CE 2001 8 7 AUS20010433 120010115G575312210107 FLAP TRACK CESSNA206 U206F 2073333CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL TRAILING EDGE FLCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLAP TRACKS CONTAINED EXFOLIATION AND INTERGRANNULAR CORROSIONLOCATED IN THE FORWARD END OF THE LOWER SLOT. 1H71 3O3 O A4CE E5CE 5 CP21EA 20010808000862001080800086NE 2001 8 8 AUS20010434 220010103G85203592 LINK ROD DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE ENGINE BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 9 CYLINDER LINKROD BROKEN. SEVERE INTERNAL DAMAGE PREVENTED ESTABLISHING THE CAUSE OF THE FAILURE. 1H71 3R3 R A806 5E1 20010807000972001080700097EA 2001 8 7 AUS20010435 220010503G7310L142368A HOSE LYC LTIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR2 GL ENGINE FUEL DISTFAULTY W K NONE O OTHER ININSP/MAINT 1 AUS L142368A (AUS) FUEL HOSES LOCATED BETWEEN THE FCU AND THE FLOW DIVIDER DID NOT HAVE FIRESLEEVES FITTED. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010807000982001080700098EU 2001 8 7 AUS20010437 120010506G555313708F1 BRACKET BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP MCAULY4HFR344HFR34C653 NE VERTICAL STABILICORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RUDDER HINGE BRACKET CONTAINED EXFOLIATION CORROSION IN THE AREAOF THE BONDING LEAD ATTACHMENT. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010808000872001080800087SO 2001 8 8 AUS20010438 120010401G3220 LANDING GEAR PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA HARTZLHCE3Y HCE3YR2 GL NLG COLLAPSED W O OTHER O OTHER NRNOT REPORTED 1 AUS (AUS) NOSE LANDING GEAR COLLAPSED. INSPECTION COULD FIND NO DEFECTS WITH THE SYSTEM. SUSPECT INCORRECT TECHNIQUE. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010808000892001080800089EU 2001 8 8 AUS20010439 120010504G792070009K000V332A HOSE AGUSTA206AGS206AAGUSTA 0260301EU ALLSN 250C 250C20B 03013GL ENGINE OIL LEAKING W A UNSCHED LANDING EK VIBRATION/BUFFET FLUID LOSS CRCRUISE 1 AUS (AUS) ENGINE OIL HOSE LEAKING IN AN AREA APPROXIMATELY 100MM (4IN) FROM THE FORWARD UNION END. 1G71 3U3 U EXPA1G71E4CE 20010807000992001080700099SO 2001 8 7 AUS20010440 120010427G7170CCA1550 DRAIN VALVE LYC O320D3G PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA SNSNCH74D 74DM EA ENGINE DRAINS LEAKING W K NONE O OTHER TOTAKEOFF 1 AUS (AUS) AIRCRAFT RETURNED TO AIRSTRIP AFTER TAKEOFF FOR A FORCED LANDING. FUEL STAINS FOUND DOWN THE SIDE OF THE AIRCRAFT EMANATING FROMTHE DRAIN VALVE. INSPECTION OF THE VALVE COULD FIND NO DEFECTSAND THE VALVE WAS CLOSED. ENGINE DRAIN VALVE SUSPECT LEFT PARTIALLY OPEN ALLOWING FUEL LEAKAGE AND THEN CLOSED ON LANDING. 1L71 3O3 O 2A13 E274 5 NP88614 20010808000912001080800091EU 2001 8 8 AUS20010441 120010420G5343D5337061320300 FITTING AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE LANDING GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR DOOR ACTUATOR FITTINGS (3OFF4) CRACKED FROM THE TOP TWO FASTENER HOLES IN THE VERTICAL FLANGE. FITTINGS CRACKED ARE PNO D5337061320200 (LH AFT) AND PNO D5337061320300 (RH AFTAND LH FORWARD). FOUND DURING INSPECTION IAW ER A32-53-40-9C(SB A320-53-1135). 2L72 4F4 FRTA46NM E29NE 20010807001002001080700100SO 2001 8 7 AUS20010442 120010321G3397 WIRE BA08006281 EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE PASSENGER COMPARWORN W K NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 AUS (AUS) CABIN LIGHTING SYSTEM INVERTER OUTPUT WIRING CHAFING AGAINST GASPER AIR DUCT CAUSING THE WIRING LOOM AND DUCT INSULATION TO BURN. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010808000932001080800093NM 2001 8 8 AUS20010443 120010417G3520 DOOR BOEING737 737377 NM PASSENGER OXYGENMISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) FORWARD TOILET OXYGEN SYSTEM DROP-DOWN DOOR HAD WHITE SILASTICMATERIAL ACROSS THE FORWARD OUTBOARD CORNER PREVENTING IT FORM OPENING. THE SILASTIC HAD BEEN USED ON THE TOILET CEILING PANEL AND HAD BEEN SMEARED ACROSS THE OXYGEN PANEL DOOR. 2L72 4F RTA16WE 20010807001012001080700101EU 2001 8 7 AUS20010444 120010407G2822 PUMP FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU FUEL BOOST PUMP FAILED W K NONE O OTHER TOTAKEOFF 1 AUS (AUS) AFT BOOST PUMP FAILED. CIRCUIT BREAKER RESET AND PUMP OPERATEDNORMALLY SINCE. 2L72 4F4 FRTA20EU E2EU 20010808000952001080800095NM 2001 8 8 AUS20010445 120010430G3230658005118 DRAG BRACE BOEING737 73733A 1384673NM LANDING GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 21713 (AUS) NOSE LANDING GEAR UPPER DRAG BRACE CRACKED AT RETRACTION ACTUATOR ATTACHMENT. CRACK WAS DETECTED VISUALLY. 2L72 4F RTA16WE 20010807001022001080700102EU 2001 8 7 AUS20010446 120010417G783022100009519 CABLE PWA PW4152 AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE THRUST REVERSER DISTORTED W K NONE O OTHER LDLANDING 1 AUS (AUS) NO1 ENGINE THRUST REVERSER MASTER ACTUATOR FLEXIBLE CABLE DRIVE TO SPLITTER GEARBOX KINKED AND TWISTED. 2L72 4F RTA35EU E24NE 20010807001032001080700103EU 2001 8 7 AUS20010447 120010430G3260 DOOR FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU LANDING GEAR POSFALSE INDICATIONW K NONE ON OTHER FALSE WARNING NRNOT REPORTED 1 AUS (AUS) RH MAIN LANDING GEAR DOOR INDICATIONS INCORRECT. INVESTIGATIONCOULD FIND NO FAULT WITH THE SYSTEM. DEFECT NOT CONFIRMED. 2L72 4F4 FRTA20EU E2EU 20010807001042001080700104EU 2001 8 7 AUS20010448 120010430G324250002685 BRAKE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU BRAKE LEAKING W K NONE OK OTHER FLUID LOSS ININSP/MAINT 1 AUS 58 DEC6976 (AUS) NO2 BRAKE UNIT LEAKING FLUID. 2L72 4F4 FRTA20EU E2EU 20010808000962001080800096EA 2001 8 8 AUS20010450 220010501G8530LW12993 CYLINDER PIPER PA32 PA32R300 7103213SO LYC O540 IO540K1G5 41532EA HARTZLHCC2Y HCC2YK1 GL ENGINE LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS 145 (AUS) ENGINE CYLINDERS IN POOR CONDITION. OIL LEAKING PAST VALVE STEMS. 1L71 3O3 O A3SO 1E4 5 CP920 20010807001052001080700105EA 2001 8 7 AUS20010451 220010420G852071907 WASHER LYC IO540E1B5 GULSTM500 500S 0141107SW LYC O540 IO540E1B5 41532EA HARTZLHCC3Y HCC3YR2 NE RECIPROCATING ENFAILED W K NONE E VIBRATION/BUFFET CRCRUISE 1 AUS L1111148 (AUS) RH ENGINE COUNTERWEIGHT RETAINING WASHER PNO 71907 HAD FAILED ALLOWING THE COUNTERWEIGHT ROLLER PNO 72797 TO MIGRATE ANDCONTACT NO5 CYLINDER CONNECTING ROD AND CAUSING IT TO FAIL WHICHCAUSED SEVERE DAMAGE TO THE CRANKCASE. THE RETAINING CIRCLIPPNO LW14820 REMAINED IN POSITION. 1H72 3O3 O 6A1 1E4 5 CP25EA 20010808000982001080800098EU 2001 8 8 AUS20010452 120010430G324195427193 SENSOR FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU WHEEL SPEED FAILED W O OTHER O OTHER NRNOT REPORTED 1 AUS 351 JUL74569 (AUS) NR 2 WHEEL SPEED GENERATOR FAILED. 2L72 4F4 FRTA20EU E2EU 20010807001062001080700106EA 2001 8 7 AUS20010453 120010417G2432 CONNECTOR DHAV DHC6 DHC6 2802606EA BATTERY/CHARGER MELTED W K NONE H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 AUS (AUS) BATTERY SHUNT GROUND CONNECTION MELTED. 1H72 3T RTA9EA 20010807001072001080700107EU 2001 8 7 AUS20010455 120010505G3260GC1016 RELAY FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU LANDING GEAR POSFAULTY W K NONE O OTHER CLCLIMB 1 AUS (AUS) RH GROUND/FLIGHT RELAY FAULTY. LH AND RH MLG GROUND FLIGHTSWITCHES CONTAMINATED. 2L72 4F4 FRTA20EU E2EU 20010807001082001080700108CE 2001 8 7 AUS20010456 120010406G534307900065 BRACKET CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULYD3A34 D3A34C403 GL LANDING GEAR ATTCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR ATTACHMENT BRACKET SEVERELY CORRODED. 1H71 3O3 O 3A24 E5CE 5 CP47GL 20010807001092001080700109CE 2001 8 7 AUS20010457 120010406G534307900066 BRACKET CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULYD3A34 D3A34C403 GL LANDING GEAR ATTCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR ATTACHMENT BRACKET CRACKED. MLG LEG LOOSE ATWEDGES. 1H71 3O3 O 3A24 E5CE 5 CP47GL 20010807001102001080700110NM 2001 8 7 AUS20010458 120010405G6510A0413 ARM ROBSIN TAILCONE ROBSINR22 R22BETA NM LYC O320 O320B2C 41508EA TAIL ROTOR DRIVEFAILED W K NONE F FLT CONT AFFECTED NRNOT REPORTED 1 AUS 1057 (AUS) TAIL ROTOR DRIVESHAFT DAMPENER ARM FAILED ALLOWING TAIL ROTOR DRIVESHAFT TO WHIP AND BREAK AND CAUSING DESTRUCTION OF THE TAILCONE ASSEMBLY PNO A023-20. 1G71 3O3 O H10WE E274 20010808001002001080800100EU 2001 8 8 AUS20010459 120010505G3260 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU LANDING GEAR STUCK W O OTHER O OTHER CLCLIMB 1 AUS (AUS) MAIN LANDING GEAR GROUND/FLIGHT SWITCHES STICKY. 2L72 4F4 FRTA20EU E2EU 20010808001022001080800102EU 2001 8 8 AUS20010461 220010508G7200 ENGINE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU NACELLE MALFUNCTIONED W C ABORTED TAKEOFF ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AUS (AUS) INCORRECT TAKEOFF THRUST SET BY PILOT. PERSONNEL ERROR. 2L72 4F4 FRTA20EU E2EU 20010808001062001080800106NM 2001 8 8 AUS20010463 120010505G7331AS21515 BOLT RROYCE R211524D419 BOEING747 747SP38 NM RROYCERB211 RB211524D41954555NE FLOW INDICATOR WRONG PART W O OTHER K FLUID LOSS NRNOT REPORTED 1 AUS 6100 12647 (AUS) NR 2 ENGINE FUEL FLOW TRANSMITTER INLET GASKET LEAKING. LOOSEBOLTS RETIGHTENED BUT THE LEAK CONTINUED. FURTHER INVESTIGATION FOUND THAT THE MOUNTING BOLTS WERE PNO AS21515 INSTEAD OF THE CORRECT PNO AS21514. FITMENT OF THE INCORRECT BOLTS HAD DAMAGED THE THREADS IN THE TRANSMITTER REQUIRING REPLACEMENT. UNAPPROVEDPART. PERSONNEL/MAINTENANCE ERROR. 2L74 4F4 FRTA20WE E12EU 20010807001112001080700111EU 2001 8 7 AUS20010464 120010505G3230 LANDING GEAR FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU LANDING GEAR RETFAULTY W K NONE O OTHER CLCLIMB 1 AUS (AUS) LANDING GEAR WOULD NOT RETRACT. 2L72 4F4 FRTA20EU E2EU 20010807001122001080700112EU 2001 8 7 AUS20010465 120010511G2752 BOLT FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU TRAILING EDGE FLSHEARED W K NONE FK FLT CONT AFFECTED FLUID LOSS CLCLIMB 1 AUS (AUS) FLAP MOTOR ASSEMBLY BODY BOLT SHEARED AND BODY HALVES SEPARATED AT JOINT. LOSS OF HYDRAULIC FLUID. 2L72 4F4 FRTA20EU E2EU 20010807001132001080700113EU 2001 8 7 AUS20010466 120010505G3220200725209LOWER TORQUE LINK FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU NOSE/TAIL LANDINCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS DCS6809LOWER (AUS) NOSE LANDING GEAR LOWER TORQUE LINK CRACKED IN GREASE NIPPLEHOLE. FOUND USING VISUAL INSPECTION AND CONFIRMED USING EDDYCURRENT INSPECTION. 2L72 4F4 FRTA20EU E2EU 20010807001142001080700114EU 2001 8 7 AUS20010468 120010507G2760 CONNECTOR FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DRAG CONTROL SYSLOOSE W K NONE FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 AUS (AUS) RH OUTBOARD LIFT DUMPER BELLCRANK INLOCK CONNECTOR LOOSE. 2L72 4F4 FRTA20EU E2EU 20010807001152001080700115EU 2001 8 7 AUS20010469 120010505G3220200725209UPPER TORQUE LINK FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU NOSE/TAIL LANDINCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS DCS6808UPPER (AUS) NOSE LANDING GEAR UPPER TORQUE LINK CRACKED IN GREASE NIPPLEHOLE. FOUND USING VISUAL INSPECTION AND CONFIRMED USING EDDYCURRENT INSPECTION. 2L72 4F4 FRTA20EU E2EU 20010807001162001080700116CE 2001 8 7 AUS20010470 120010407G3222998200005 SHOCK ABSORBER BEECH 9782000061 BEECH 200 200BEECH 1152920CE NOSE/TAIL LANDINFAULTY W K NONE OK OTHER FLUID LOSS ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR SHOCK ABSORBER INNER O' RING SEAT OVERSIZE ALLOWING THE O' RING TO MOVE ON THE HOUSING AND LEAK. 1L72 4T A24CE 20010808001072001080800107EA 2001 8 8 AUS20010471 120010511G3220 LANDING GEAR DHAV DHC6 DHC6 2802606EA NLG FOD W O OTHER C F.O.D. LDLANDING 1 AUS (AUS) NOSE LANDING GEAR FAILED WHEN THE NOSE WHEEL CONTACTED A ROCK ONLANDING. TYRE DEFLATED AND NOSE WHEEL SHATTERED. NLG FORK FAILEDAT THE OLEO AND THE REMAINDER OF THE NLG BENT BACK CAUSING DAMAGE TO THE BULKHEAD, ATTACHMENT FITTINGS AND SURROUNDINGLOWER FUSELAGE STRUCTURE. FIBREGLASS NOSE CONE ALSO BADLY DAMAGED. 1H72 3T RTA9EA 20010807001172001080700117GL 2001 8 7 AUS20010472 220010426G723023007196 SEAL ALLSN 250C30P BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL TURBINE ENGINE CCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS 1371 CAC91190 (AUS) COMPRESSOR REAR DIFFUSER LABYRINTH SEAL EXCESSIVELY CORRODED. 1G71 3U3 U H2SW E1GL 20010808001092001080800109NM 2001 8 8 AUS20010473 120010504G7110LK47717 FAIRING RROYCE RB21152436 BOEING767 767* NM RROYCERB211 RB211524* NE ENGINE COWLING MISSING W O OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 AUS 18631 13462 (AUS) NR 2 ENGINE LT A' FRAME TO FAN CASE AFT LOWER FAIRING MISSING. 2L72 4F4 FRTA1NM E12EU 20010808001112001080800111CE 2001 8 8 AUS20010474 120010427G554051310103 BEARING CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL RUDDER MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LOWER RUDDER HINGE BEARING INCORRECTLY INSTALLED. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010808001132001080800113NM 2001 8 8 AUS20010476 120010511G711013043 PANEL RROYCE RB211524G BOEING747 747438 NM RROYCERB211 RB211524G19 NE ENGINE COWLING SEPARATED W K NONE O OTHER ININSP/MAINT 1 AUS 13720 13043 (AUS) NR 3 ENGINE OGV INFILL PANELS MISSING BETWEEN 4 O'CLOCK AND 6O'CLOCK POSITIONS. DAMAGE TO LH COMPRESSOR CORE PANEL, IP COMPRESSOR BLEED VALVE CONTROL UNIT AIR SENSE PROBE, THRUST REVERSER CORONA AND NO5 AND NO6 THRUST REVERSER BLISTER FAIRINGS. 2L74 4F4 FRTA20WE E30NE 20010808001152001080800115NM 2001 8 8 AUS20010477 120010506G2761NAS161210 O-RING 15425001 BOEING767 767338 1385151NM GE CF6 CF680C2* GL DRAG ACTUATOR DAMAGED W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 AUS 501 (AUS) NR 8 SPOILER POWER CONTROL ACTUATOR (PCA) FILTER BOSS O' RING SEAL DAMAGED AND LEAKING. 2L72 4F4 FRTA1NM E23EA 20010808001172001080800117NM 2001 8 8 AUS20010478 120010505G2620301000223 EXTINGUISHER BOEING767 767* NM CABIN DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS 25012 (AUS) FIRE EXTINGUISHERS LOCATED IN THE MID CABIN LT AND RT TOILETS AND AFT CABIN RT TOILET HAD IMPACT DAMAGE TO THE FUSEABLE TIP AREA. FOUND DURING INSPECTION IAW 767-A2-25-006. 2L72 4F RTA1NM 20010807001182001080700118WP 2001 8 7 AUS20010479 120010406G6310269A55907 RETAINER HUGHES269 269C 4470504WP LYC O360 HO360C1A 41514EA ENGINE/TRANSMISSWORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) THERMOFIT SLEEVE WORN ON RETAINER. 1G71 3O3 O 4H12 E286 20010808001192001080800119EU 2001 8 8 AUS20010480 120010505G2121D92098 COOLING FAN BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE AIR DISTRIBUTIONFAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS 7028 411467 (AUS) CABIN FAN FAILED. INVESTIGATION FOUND BOTH FORE AND AFT FAN MOTOR SHAFT BEARINGS FAILED. THE MOTOR ALSO FAILED ELECTRICALLY WITHSIGNS OF OVERHEATING. BEARING PNO S38SS6CXOG33 AND PNOS100SS6CXOG33. 2H74 4F4 FRTA49EU E6NE 20010808001212001080800121EU 2001 8 8 AUS20010482 120010425G7160TU195MM660MMCC HOSE LYC IO540 BNORM BN2 BN2A 1520204EU LYC O540 IO540* 41532EA ENG AIR INTAKE COLLAPSED W C ABORTED TAKEOFF ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AUS (AUS) ENGINE INDUCTION HOSE COLLAPSED. 1H72 3O3 O A17EU 1E4 20010808001232001080800123NM 2001 8 8 AUS20010483 120010501G3242S160T400510 BRAKE BOEING767 767338 1385151NM GE CF6 CF680C2* GL NR 1 FAILED W O OTHER O OTHER NRNOT REPORTED 1 AUS 3932 QF56035 (AUS) NR 1R BRAKE FAILED. INSPECTION FOUND THAT THE REAR STATOR PLATEWAS DAMAGED WITH EVIDENCE OF REAR STATOR BREAKUP. NO1R WHEEL ALSO DAMAGED TO THE FAILED BRAKE. 2L72 4F4 FRTA1NM E23EA 20010807001192001080700119NM 2001 8 7 AUS20010484 120010514G3242214747300 BRAKE 6558256238 BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU BRAKE LEAKING W K NONE OB OTHER SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 AUS (AUS) LH OUTBOARD AND LH INBOARD BRAKES LEAKING FLUID FROM ACTUATINGPISTONS. TYRES CONTAMINATED WITH HYDRAULIC FLUID. 2L72 4F4 FRTA16WE E21EU 20010807001202001080700120 2001 8 7 AUS20010485 420010424G2230 COMPUTER AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE AUTOTHROTTLE SYSFAULTY W K NONE ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 AUS (AUS) THROTTLE CONTROL COMPUTER (TCC) FAULTY. 2L72 4F RTA35EU E24NE 20010808001242001080800124EU 2001 8 8 AUS20010486 120010331G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING OUT OF ADJ W O OTHER N FALSE WARNING NRNOT REPORTED 1 AUS (AUS) SERVICE DOOR MICROSWITCH OUT OF ADJUSTMENT. 2L72 4F4 FRTA20EU E2EU 20010808001262001080800126EU 2001 8 8 AUS20010487 120010331G492038075411 APU FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU APU BAY FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS 415 (AUS) APU FAULTY. FUMES IN CABIN. 2L72 4F4 FRTA20EU E2EU 20010807001212001080700121EU 2001 8 7 AUS20010489 120010401G5753 SEAL FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU TRAILING EDGE FLSEPARATED W K NONE DF INFLIGHT SEPARATION FLT CONT AFFECTED CRCRUISE 1 AUS (AUS) OUTBOARD TRAILING EDGE FLAP RUBBER SEAL SEPARATED. 2L72 4F4 FRTA20EU E2EU 20010807001222001080700122EU 2001 8 7 AUS20010490 120010409G36106272482 CONTROLLER AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE PNEUMATIC DISTRIFAULTY W K NONE O OTHER CRCRUISE 1 AUS 7141 111C589 (AUS) NO1 PNEUMATIC SYSTEM CONTROLLER FAULTY. 2L72 4F RTA35EU E24NE 20010807001232001080700123NM 2001 8 7 AUS20010491 120010423G3260 SENSOR DHAV DHC8 DHC8* NM PWA 120 PW123D 52152NE LANDING GEAR POSCONTAMINATED W K NONE ON OTHER FALSE WARNING TOTAKEOFF 1 AUS (AUS) MAIN LANDING GEAR DOOR SENSORS AND CONNECTORS CONTAMINATED. 2H72 4T4 TRTA13NM E20NE 20010808001282001080800128EU 2001 8 8 AUS20010492 120010411G7603 THROTTLE PWA PW4152 AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE LT & RT ENGINE FAULTY W O OTHER ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 AUS (AUS) LT AND RT ENGINE THROTTLES REDUCED TOWARDS IDLE. INTERMITTENT DEFECT. CAUSE COULD NOT BE IDENTIFIED. SEE MDR 01/0485 FORFURTHER INFORMATION. 2L72 4F RTA35EU E24NE 20010807001242001080700124SO 2001 8 7 AUS20010493 120010501G3233452383 ROD END PIPER ACTUATOR PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL LANDING GEAR ACTCONTAMINATED W K NONE ON OTHER FALSE WARNING LDLANDING 1 AUS (AUS) RH MAIN LANDING GEAR ACTUATOR RODEND CONTAMINATED AND DRY.SUSPECT CAUSED BY EXHAUST GASES FROM TAILPIPE. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010807001252001080700125NE 2001 8 7 AUS20010494 220010516G7261 PIPE PWA PW120A DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE TURBINE ENGINE OBROKEN W K NONE EX VIBRATION/BUFFET ENGINE FLAMEOUT CRCRUISE 1 AUS (AUS) ENGINE NO6/NO7 BEARING OIL FEED PIPE BROKEN. ENGINE SEIZED WITH EVIDENCE OF FIRE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010808001312001080800131NM 2001 8 8 AUS20010495 120010515G492038042812 APU BOEING737 737377 NM CFMINTCFM56 CFM563B2 13802EU APU BAY FAULTY W K NONE L NO TEST ININSP/MAINT 1 AUS 3989 (AUS) APU FAILED PERFORMANCE MONITORING TEST. EGT ROSE TO 800 DEGREES. 2L72 4F4 FRTA16WE E21EU 20010808001322001080800132GL 2001 8 8 AUS20010496 120010407G2752464300 MOTOR PAC CT4 CT4B GL CONT O360 IO360HB 17025SO HARTZLHCC2Y BHCC2YF1 GL TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 AUS (AUS) FLAP MOTOR BURNED OUT. 1L71 3O3 ORTA9PC E1CE 5 CP920 20010808001662001080800166CE 2001 8 8 AUS20010498 120010508G5500 STRUCTURE CESSNA401 401A 207590DCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C505 GL EMPENNAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) EXTENSIVE SURFACE CORROSION THROUGHOUT THE FIN AND TAIL ASSEMBLY. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010808001702001080800170NE 2001 8 8 AUS20010499 220010510G723017284 GUIDE VANE FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY65015 54557NE ENGINE OUT OF ADJ W A UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 AUS (AUS) RT ENGINE VIBRATION. POWER INCREASE LED TO HIGH ITT WITH LOW N1 AND LOW EPR WITH LOW N2. INVESTIGATION FOUND THE ACCELERATION TIME SLOW DUE TO IGV SCHEDULING OUT OF ADJUSTMENT. 2L72 4F4 FRT E25NE 20010808001722001080800172NM 2001 8 8 AUS20010500 120010517G3260864202 PROXIMITY SENSOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE LANDING GEAR OUT OF ADJ W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) LT MAIN LANDING GEAR DOOR PROXIMITY SWITCH OUT OF ADJUSTMENT. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010808001732001080800173NM 2001 8 8 AUS20010501 120010516G2910MS21904W16 ELBOW BOEING747 747SP38 NM RROYCERB211 RB211524D41954555NE HYDRAULIC SYSTEMCRACKED W O OTHER K FLUID LOSS NRNOT REPORTED 1 AUS (AUS) HYDRAULIC SYSTEM LEAKING FROM CRACKED PRESSURE LINE ELBOW LOCATED UNDER NO3 STRUT REAR SAILBOAT. LOSS OF HYDRAULIC FLUID. 2L74 4F4 FRTA20WE E12EU 20010808001752001080800175NM 2001 8 8 AUS20010502 120010517G711013082 PANEL RROYCE RB211524H36 BOEING767 767* NM RROYCERB211 RB211524* NE ENGINE COWLING SEPARATED W K NONE O OTHER ININSP/MAINT 1 AUS 43385 13082 (AUS) RH ENGINE BULLNOSE SECTION LOCATED AFT OF THE ACOUSTIC PANELMISSING FROM AREA BETWEEN NO4 AND NO7 BLOCKER DOORS. THE MISSINGPIECE WAS APPROXIMATELY 2 METERS (6FT) IN LENGTH. DAMAGE CAUSED TO THREE BLOCKER DOORS, COMBUSTOR FAIRING AND BLISTER FAIRING. 2L72 4F4 FRTA1NM E12EU 20010808001782001080800178NM 2001 8 8 AUS20010503 120010515G711012756 LINER RROYCE RB211524D419BOEING747 747238B 1384828NM RROYCERB211 RB211524D41954555NE ENGINE COWLING MISSING W O OTHER ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 AUS 6756 12756 (AUS) NR 1 ENGINE LOW POWER. INVESTIGATION FOUND ONE SECTION OF FRONTFAN ACOUSTIC LINING BETWEEN 2 O'CLOCK AND 4 O'CLOCK AREAS MISSING AND ONE AREA OF ICE IMPACT PANEL BETWEEN 1 O'CLOCK AND 5 O'CLOCKAREAS MISSING WITH LOOSE MATERIAL STILL TRAPPED BY THEENGINE. 2L74 4F4 F A20WE E12EU 20010807001262001080700126CE 2001 8 7 AUS20010504 120010508G5554513300031 BRACKET CESSNA401 401A 207590DCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C505 GL RUDDER/TAB, ATTACRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RUDDER LOWER HINGE BRACKET CRACKED AT CORNERS. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010808001792001080800179NM 2001 8 8 AUS20010505 120010501G293420044000001 TRANSMITTER BOEING737 7374Y0 1384705NM CFMINTCFM56 CFM563C 13802EU HYD QTY IND FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HYDRAULIC SYSTEM B' OIL QUANTITY TRANSMITTER FAULTY. 2L72 4F4 FRTA16WE E21EU 20010808001812001080800181EU 2001 8 8 AUS20010506 120010520G2612HC924H4913002 FIRE LOOP BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 1 ENGINE WORN W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS 20594 (AUS) NR 1 ENGINE FIRE DETECTOR WIRING LOOM CHAFED. 2H74 4F4 FRTA49EU E6NE 20010808002032001080800203NE 2001 8 8 AUS20010507 220010521G7261 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE LT & RT LACK OF LUBE W C ABORTED TAKEOFF KEJFLUID LOSS VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LT AND RT ENGINES LOW ON OIL. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010807001272001080700127NM 2001 8 7 AUS20010508 120010517G3233980044503 BEARING PIPER PA60 PA60600A 7106002NM LYC O540 IO540K1J5 41532EA HARTZLHCC3Y HCC3YR2 NE LANDING GEAR ACTBROKEN W K NONE OJ OTHER WARNING INDICATION DEDESCENT 1 AUS (AUS) LH MAIN LANDING GEAR ACTUATOR RODEND BEARING FRACTURED. 1M72 3O3 ORTA17WE 1E4 5 CP25EA 20010808002052001080800205CE 2001 8 8 AUS20010509 120010118G534750150191 SEAT TRACK CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO CABIN FRACTURED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PILOTS SEAT TRACK CHANNELS PNO 5015019-1 AND PNO 5015019-3CRACKED THROUGH MOUNT HOLES. ONE CHANNEL HAD BEEN REMANUFACTUREDFROM A LIGHTER MATERIAL AND WAS ALSO SECURED USING COMMERCIAL POP RIVETS. UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A7CE E8CE 20010808002062001080800206NM 2001 8 8 AUS20010510 120010516G5310 PANEL BOEING747 747SP38 NM RROYCERB211 RB211524D41954555NE FUEL CELL LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NO1 MAIN FUEL TANK INTERNAL RIB ACCESS/BAFFLE PANEL LOOSE. THEPANEL WAS FOUND UNSECURED ON THE FLOOR WITH THE MOUNTING SCREWS CONTAINED IN A CANVAS SCREW BAG ATTACHED TO THE PANEL. THE AREA HAD RECENTLY BEEN ACCESSED DURING D4 INSPECTION.PERSONNEL/MAINTENANCE ERROR. 2L74 4F4 FRTA20WE E12EU 20010808002092001080800209NM 2001 8 8 AUS20010511 120010520G3246162T16211 WASHER BOEING767 767338 1385151NM GE CF6 CF680C2* GL WHEEL MISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) WHILE CHANGING THE RH NOSEWHEEL DUE TO FOD IT WAS NOTED THAT THENUT SPACER (WASHER) WAS MISSING. THE LT NOSEWHEEL WAS ALSOCHECKED WHERE IT WAS FOUND THAT THE WASHER WAS ALSO MISSING. 2L72 4F4 FRTA1NM E23EA 20010807001282001080700128NM 2001 8 7 AUS20010512 120010521G3242215211400 BRAKE BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU BRAKE LEAKING W K NONE OB OTHER SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 AUS 3134 (AUS) LH INBOARD BRAKE UNIT LEAKING FROM PISTON ASSEMBLY. 2L72 4F4 FRTA16WE E21EU 20010807001292001080700129NM 2001 8 7 AUS20010513 120010521G252022303001 STUD BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU PASSENGER COMPARLOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PASSENGER SEAT 9ABC LOOSE DUE TO INBOARD SEAT LEG FLOOR SPREADERSTUD UNSCREWING FROM ANCHOR NUT. 2L72 4F4 FRTA16WE E21EU 20010807001302001080700130NM 2001 8 7 AUS20010514 120010508G52306546921528 DOOR BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU CARGO/BAGGAGE DOCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 42473 1359 (AUS) FORWARD CARGO DOOR CRACKED ON THE INSIDE RADIUS OF THE AFT LOWERCORNER EMANATING UPWARDS FROM THE LOWER CROSS BEAM ATTACHMENT POINT. CRACK LENGTH APPROXIMATELY 25.4MM (1IN). 2L72 4F4 FRTA16WE E21EU 20010807001312001080700131NM 2001 8 7 AUS20010515 120010510G5511 SPAR BOEING737 7374Q8 NM CFMINTCFM56 CFM563C 13802EU HORIZONTAL STABIDAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH HORIZONTAL STABILISER LOWER FORWARD SPAR DAMAGED. 2L72 4F4 FRTA16WE E21EU 20010807001322001080700132CE 2001 8 7 AUS20010516 120010412G8011SA539800M015 SPRING CONT IO520A CESSNA206 U206 2073306CE CONT O520 IO520A 17032SO HARTZLHCC3Y HCC3YF1 GL ENGINE STARTER FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 2 552408 (AUS) STARTER CLUTCH SPRING FAILED CAUSING DAMAGE TO THE CRANKSHAFT,CAMSHAFT GEAR AND ATTACHING HARDWARE. ROCKWELL HARDNESS TESTREVEALED INCONSISTANT HARDNESS. 1H71 3O3 O A4CE E5CE 5 CP25EA 20010807001332001080700133NM 2001 8 7 AUS20010517 120010402G750009880645 SEAL GARRTT HP6DUCT BOEING757 75723A 1384967NM RROYCERB211 RB211535E4 54555NE ENGINE BLEED AIRFAILED W K NONE EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 AUS 09880645 (AUS) RH ENGINE HP6 DUCT SEALS FAILED AND LEAKING. 2L72 4F4 FRTA2NM E12EU 20010808002112001080800211NM 2001 8 8 AUS20010518 120010508G493036080004 FCU BOEING737 737377 NM CFMINTCFM56 CFM563B2 13802EU APU ENGINE FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) APU FUEL CONTROL UNIT FAULTY. 2L72 4F4 FRTA16WE E21EU 20010808002122001080800212SW 2001 8 8 AUS20010519 120010521G3234CA3108E12S200210CONNECTOR SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP HARTZLHCB3T HCB3TN5 GL LANDING GEAR FAULTY W O OTHER O OTHER DEDESCENT 1 AUS (AUS) LANDING GEAR SELECTOR VALVE CANNON PLUG WIRE BROKEN. 2L72 4T4 TRTA8SW E4WE 6 CP15EA 20010808002142001080800214NE 2001 8 8 AUS20010520 220010519G726017287 GEARBOX FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY65015 54557NE TURBINE ENGINE MAKING METAL W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH ENGINE HIGH SPEED GEARBOX CHIP DETECTOR AND OIL FILTER CONTAMINATED WITH FINE METAL PARTICLES. FILTER DIFFERENTIAL PRESSURE POP-UP INDICATOR OPERATED. 2L72 4F4 FRT E25NE 20010808002182001080800218 2001 8 8 AUS20010522 420010522G34604058650904 CDU BOEING747 747438 NM RROYCERB211 RB211524G19 NE COCKPIT FAILED W A UNSCHED LANDING BO SMOKE/FUMES/ODORS/SPARKS OTHER CRCRUISE 1 AUS 21528 89020332 (AUS) RT FLIGHT MANAGEMENT COMPUTER CONTROL DISPLAY UNIT (CDU) FAILED. SMOKE IN COCKPIT AND ELECTRICAL BURNING SMELL WITH RT CDU KEYPADWARM TO TOUCH. 2L74 4F4 FRTA20WE E30NE 20010808002192001080800219NE 2001 8 8 AUS20010525 220010523G72006058T82GO1 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R390 R3904123F27 NE RIGHT FAILED W C ABORTED TAKEOFF EX VIBRATION/BUFFET ENGINE FLAMEOUT TOTAKEOFF 1 AUS 13931 (AUS) RT ENGINE FAILED. INVESTIGATION FOUND SOME DAMAGE TO THE FIRSTSTAGE COMPRESSOR WHEEL AND THE CENTRE BODY RETAINING SCREW STUDSSHEARED. BORESCOPE INSPECTION FOUND MAJOR DAMAGE TO THE FIRST STAGE IGVS AND COMPRESSOR WHEEL WITH ONE COMPRESSOR BLADE MISSING ABOUT HALF OF THE AXIAL LENGTH. DOWNSTREAM DAMAGE TO OTHER IGVS AND COMPRESSOR STAGES. THERE IS ALSO SEVERE HEAT DISTRESS DAMAGETO THE FIRST AND SECOND STAGE GAS GENERATOR TURBINES AND NOZZLESAS WELL AS THE FIRST STAGE POWER TURBINE AND NOZZLE. POWERTURBINE COOLING AIR UPPER AND LOWER TRANSFER TUBES SEPARATED AT WELDS. FOUR RETENTION SCREWS ON THE CENTRE BODY HAVE SHEARED OFF. 2L72 4T4 TRTA52EU E8NE 6 CP31NE 20010808002202001080800220NE 2001 8 8 AUS20010526 220010521G7321FFR105MK4S REGULATOR RROYCE RB211524D4 BOEING747 747338 NM RROYCERB211 RB211524D41954555NE FUEL CONTROL FAULTY W O OTHER E VIBRATION/BUFFET APAPPROACH 1 AUS 2196 12775 (AUS) NR 3 ENGINE FUEL FLOW REGULATOR (FFR) FAULTY. 2L72 4F4 FRTA20WE E12EU 20010808002212001080800221EA 2001 8 8 AUS20010527 220010412G8530LW13622 VALVE NEWZE FU24 FU24954 WP LYC O720 IO720A1B 41546EA ENGINE WORN W K NONE O OTHER ININSP/MAINT 1 AUS 394 (AUS) NO2 CYLINDER INLET VALVE DAMAGED IN THE COLLETT RECESS AREA.VALVE STEM CAP SEPARATED AND ONLY ONE COLLETT HALF WAS RETAININGTHE VALVE SPRING. METAL PARTICLES FROM THE DAMAGED VALVE WERE FOUND IN THE OIL FILTER AND PARTICLES OF THE MISSING COLLETT WERE FOUND IN THE SUCTION FILTER. 1L71 3O3 O A9PC 1E15 20010808002222001080800222EA 2001 8 8 AUS20010528 220010418G853015F1995758 PUSHROD NEWZE FU24 FU24954 WP LYC O720 IO720A1B 41546EA ENGINE DISTORTED W A UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 AUS (AUS) NR 7 CYLINDER EXHAUST VALVE PUSHROD BENT AND PUSHROD SHROUDDAMAGED CAUSING OIL LEAK. INVESTIGATION FOUND THE VALVE STEM CAP SEPARATED AND THE PISTON SUFFERING FROM SLIGHT IMPACT DAMAGE WITH THE EXHAUST VALVE. METAL CONTAMINATION OF OIL FILTER. 1L71 3O3 O A9PC 1E15 20010808002232001080800223NM 2001 8 8 AUS20010529 120010507G272265C370539 PCU BOEING737 737377 NM CFMINTCFM56 CFM563B2 13802EU RUDDER ACTUATOR FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS 35274 1899AC (AUS) RUDDER POWER CONTROL UNIT (PCU) INTERNAL LEAK. FOUND DURING INSPECTION IAW ER B73-27-20-15 AND BOEING SL 737-SL-27-119. WORKSHOP INSPECTION FOUND THE LEAK WITHIN LIMITS. 2L72 4F4 FRTA16WE E21EU 20010808002242001080800224NM 2001 8 8 AUS20010532 120010316G492038420723 TURBINE GARRTT GTCP85129H BOEING737 73733A 1384673NM CFMINTCFM56 CFM563B2 13802EU APU CORE ENGINE FAILED W O OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 AUS 3480 (AUS) APU TURBINE WHEEL DISINTEGRATED. SUSPECT CAUSED WAS A BI-HUBFAILURE OF THE TURBINE WHEEL DUE TO UNDETECTABLE HANIUM OXIDE INCLUSION FORMED DURING THE CASTING PROCESS. 2L72 4F4 FRTA16WE E21EU 20010808002252001080800225NM 2001 8 8 AUS20010533 120010305G492038420723 TURBINE GARRTT GTCP85129K BOEING737 73733A 1384673NM CFMINTCFM56 CFM563B2 13802EU APU CORE ENGINE FAILED W O OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 AUS 4146 (AUS) APU TURBINE WHEEL DISINTEGRATED. SUSPECT CAUSED BY TENSILEOVERLOAD ORIGINATING FROM AN UNDETECTABLE SINGLE HAFNIUM OXIDEDROSS CASTING INCLUSION. 2L72 4F4 FRTA16WE E21EU 20010808002262001080800226NE 2001 8 8 AUS20010534 220010207G7250230353601 BEARING LYC ALF502R5 BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE TURBINE SECTION FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 20481 (AUS) NO2 ENGINE NO6 BEARING FAILED. CONTAMINATION OF ENGINE OILSYSTEM. 2H74 4F4 FRTA49EU E6NE 20010808002272001080800227EU 2001 8 8 AUS20010535 120010426G5711 SPAR BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R3A 41580NE LT & RT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED IN AREA BETWEEN RIB 13 AND RIB 18. 2H74 4F4 FRTA49EU E6NE 20010808002282001080800228EU 2001 8 8 AUS20010536 120010330G5711 SPAR BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED IN THE AREA BETWEEN RIB 13 AND RIB 18. 2H74 4F4 FRTA49EU E6NE 20010808002292001080800229EU 2001 8 8 AUS20010537 120010301G5711 SPAR BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED IN THE AREA BETWEEN RIB 13 AND RIB 18. 2H74 4F4 FRTA49EU E6NE 20010808002312001080800231 2001 8 8 AUS20010538 420010528G3130 RECORDER BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE DATA UNSERVICEABLE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) OPERATIONAL CHECK AND CALIBRATION CHECK OF FLIGHT DATA RECORDER (FDR) NOT CARRIED OUT. PERSONNEL/MAINTENANCE ERROR. 2H74 4F4 FRTA49EU E6NE 20010808002322001080800232EU 2001 8 8 AUS20010539 120010528G5330 SKIN BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE SKIN CRACKED IN THE AREA BETWEEN FR 35 AND FR 36 ATSTRINGER LOCATIONS 2L AND 3L. CRACK LENGTH 558.8MM (22IN). 2H74 4F4 FRTA49EU E6NE 20010807001342001080700134NM 2001 8 7 AUS20010540 120010526G32344105DA VALVE BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU LANDING GEAR SELFAULTY W K NONE O OTHER LDLANDING 1 AUS 2087 (AUS) LANDING GEAR CONTROL SELECTOR VALVE FAULTY. 2L72 4F4 FRTA16WE E21EU 20010808002342001080800234NE 2001 8 8 AUS20010541 220010526G73216068T72P09 HMU GE CT79B SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R375 R3754123F21 NE ENGINE FAULTY W A UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 AUS (AUS) HYDROMECHANICAL UNIT (HMU) SUSPECT FAULTY. WORKSHOP INVESTIGATION AND TESTING COULD FIND NO FAULTS. 2L72 4T4 TRTA52EU E8NE 6 CP17NE 20010808002362001080800236NM 2001 8 8 AUS20010543 120010426G27512061141 INDICATOR BOEING737 73733A 1384673NM TE FLAPS FAULTY W O OTHER F FLT CONT AFFECTED APAPPROACH 1 AUS 44431 903 (AUS) FLAP POSITION INDICATOR GAVE CONFLICTING LH AND RH FLAP POSITIONS ALTHOUGH THERE WAS NO EFFECT ON ROLL CONTROL. INSPECTION OF THE INDICATOR REVEALED MINOR FAULTS BUT THE INDICATOR WAS OK AND NOTLIKELY TO HAVE CAUSED THE FAULT. 2L72 4F RTA16WE 20010807001352001080700135WP 2001 8 7 AUS20010544 120010522G6320A0061 GEARBOX ROBSINR22 R22 7640102WP LYC O320 O320B2C 41508EA MAIN ROTOR GEARBCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 0375 (AUS) MAIN ROTOR GEARBOX CRACKED IN LOWER AREA. 1G71 3O3 O H10WE E274 20010808002372001080800237CE 2001 8 8 AUS20010545 120010512G2120CM361210B130 DUCT CESSNA441 441 2076020CE CABIN COOLING DETERIORATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AIRCYCLE MACHINE DUCT DETERIORATED. 1L72 3T RTA28CE 20010808002382001080800238NM 2001 8 8 AUS20010546 120010523G2133 VALVE BOEING737 73733A 1384673NM CABIN PRESSURE FAILED W O OTHER O OTHER CRCRUISE 1 AUS (AUS) PRESSURISATION SYSTEM AUTOMATIC FLOW CONTROL VALVE FAILED TO CLOSE. 2L72 4F RTA16WE 20010808002402001080800240NM 2001 8 8 AUS20010547 120010214G2760BACC2A3A01853FG CONTROL CABLE BOEING737 73733A 1384673NM DRAG CONTROL SYSFAILED W O OTHER F FLT CONT AFFECTED DEDESCENT 1 AUS (AUS) NR 3 FLIGHT SPOILER CONTROL CABLE BROKEN IN THE AREA OF WBL 73.00LT. THE CABLE FAILED APPROXIMATELY 203.2MM (8IN) OUTBOARD OF THETURNBARREL. THE FAILURE WAS A RESULT OF RUST (CORROSION) AND WEAR SUSPECT DUE TO INADEQUATE REAPPLICATION OF PROTECTIVE INHIBITNG FLUID. 2L72 4F RTA16WE 20010808002422001080800242NM 2001 8 8 AUS20010548 120010529G4920737M49503011 APU BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU APU BAY FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS 2976 (AUS) APU FAULTY. SMOKE AND FUMES IN CABIN. OIL IN BLEED DUCT. 2L72 4F4 FRTA16WE E21EU 20010807001362001080700136 2001 8 7 AUS20010549 420010528G256565C1990115 CABLE BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU ESCAPE SLIDE FRAYED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH AND RH AFT MAIN ENTRY DOOR ESCAPE SLIDE RELEASE CABLES CONTAINED BROKEN STRANDS. FOUND DURING INSPECTION IAW AD/B737/42, FAA AD 90-12-11 AND EI 734-025-0086 REV09. 2L72 4F4 FRTA16WE E21EU 20010808002432001080800243 2001 8 8 AUS20010550 420010528G256580330033 CABLE 7A126110 BOEING747 747SP38 1384817NM RROYCERB211 RB211524D41954555NE ESCAPE SLIDE OUT OF ADJ W K NONE L NO TEST ININSP/MAINT 1 AUS 1328 G112 (AUS) NO1 RH DOOR SLIDE FAILED TO DEPLOY DURING TEST. INVESTIGATION FOUND THE DOOR EMERGENCY POWER RESERVOIR FIRING CABLE OUT OFADJUSTMENT AND FAILING TO RUPTURE THE DISC OF THE EPS BOTTLE. THE EPS CABLE WAS ADJUSTED AND THE SLIDE DEPLOYED NORMALLY. 2L74 4F4 FRTA20WE E12EU 20010808002442001080800244NM 2001 8 8 AUS20010551 120010531G3520S417T40127 GENERATOR BOEING737 737377 NM CFMINTCFM56 CFM563B2 13802EU PASSENGER OXYGENMISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) NR 3 TOILET AND PSU 21L OXYGEN GENERATORS HAD THE RELEASE PINS INCORRECTLY INSTALLED IN THE SAFETY PIN HOLES.PERSONNEL/MAINTENANCE ERROR. 2L72 4F4 FRTA16WE E21EU 20010807001372001080700137CE 2001 8 7 AUS20010552 120010426G5711501100037 SPAR CAP BEECH 65 A658200 1152805CE LYC O480 IGSO480A1B6 41529EA HARTZLHCB3Z HCB3Z202 GL WING SPAR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH WING UPPER SPAR CAP CORRODED IN THE AREA OF THE FORWARD HINGEEDGE AND FORWARD CAP FLANGE. 1L72 3O3 O 3A20 E284 5 CP907 20010808002452001080800245NM 2001 8 8 AUS20010554 120010531G332060B4002615 TRANSFORMER BOEING747 747238B 1384828NM CABIN FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AUS (AUS) SIDE WALL LIGHT BALLAST LOCATED IN THE AREA ABOVE SEAT 23J BURNTAND DAMAGED. INVESTIGATION FOUND PIN 14 OF PLUG D2292P IN THE LIGHTING TRANSFORMER PNO 60B40026-15 DAMAGED. 2L74 4F A20WE 20010808002482001080800248SO 2001 8 8 AUS20010555 120010530G262189777601 SQUIB EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE FIRE BOTTLE UNAPPROVED PART W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) APU FIRE BOTTLE SQUIB FAULTY (MODIFIED). THE FIRING DEVICE HAD BEEN CUT OFF AND THE SQUIB USED AS A TRANSPORT BLANK. THE SQUIB HAD NOT BEEN REPLACED WHEN THE FIRE BOTTLE WAS FITTED TO THE AIRCRAFT. UNAPPROVED PART. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010807001382001080700138SW 2001 8 7 AUS20010556 120010528G3213ED12758 PIN GULSTM500 500S 0141107SW LYC O540 IO540E1B5 41532EA HARTZLHCC3Y HCC3YR2 NE MAIN LANDING GEACRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR CLEVIS PIN CRACKED FROM BOLT HOLE. FOUND DURING INSPECTION IAW SL 376. 1H72 3O3 O 6A1 1E4 5 CP25EA 20010807001392001080700139 2001 8 7 AUS20010557 420010518G345274LS02 TRANSPONDER NARCO AT150 CESSNA210 T210M 2073451CE CONT O520 TSIO520R 17040SO MCAULYD3A34 D3A34C402 GL ATC TRANSPONDER FAULTY W K NONE O OTHER DEDESCENT 1 AUS 18821 (AUS) TRANSPONDER GIVING FALSE ALTITUDE READINGS. 1H71 3O3 O 3A21 E8CE 5 CP47GL 20010807001402001080700140EU 2001 8 7 AUS20010558 120010519G8012P90018 VALVE GARRTT TPE3312201A STBROSSC7 SC7SERIES3 8100512EU GARRTTTPE331TPE3312201A WP HARTZLHCB3T HCB3TN5 GL ENGINE START VALFAULTY W K NONE EM VIBRATION/BUFFET OVER TEMP NRNOT REPORTED 1 AUS P90018 (AUS) START PRESSURE REGULATOR INTERNAL FAULT. EGT OVERTEMP ON START. OVERTEMP INSPECTION FOUND NO DEFECTS WITH THE ENGINE. 1H72 3T4 TNTA15EU E3WE 6 CP15EA 20010807001412001080700141WP 2001 8 7 AUS20010559 220010524G7240P90018 GASKET GARRTT TPE3312201A STBROSSC7 SC7SERIES3 8100512EU GARRTTTPE331TPE3312201A WP HARTZLHCB3T HCB3TN5 GL TURBINE ENGINE CFAILED W K NONE ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 AUS P90018 (AUS) LH ENGINE IGNITER PLUG BLANK GASKET FAILED. 1H72 3T4 TNTA15EU E3WE 6 CP15EA 20010808002492001080800249NM 2001 8 8 AUS20010560 120010507G272265C370539 PCU BOEING737 737377 NM RUDDER ACTUATOR LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS 35274 1899AC (AUS) RUDDER POWER CONTROL UNIT (PCU) LEAKING INTERNALLY. 2L72 4F RTA16WE 20010807001422001080700142EU 2001 8 7 AUS20010561 120010527G2820 SWITCH FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY62015 04564NE AIRCRAFT FUEL DIFAULTY W K NONE K FLUID LOSS TOTAKEOFF 1 AUS (AUS) FUELLING CONTROL PANEL POWER SWITCH FAULTY. PANEL POWER REMAINEDON WITH THE SWITCH IN THE OFF' POSITION. INVESTIGATION FOUND THE ACCESS PANEL CAM OPERATING THE PANEL POWER SWITCH WHEN THE PANEL IS CLOSED WAS OUT OF ADJUSTMENT AND NOT OPERATING THESWITCH. 2L72 4F4 FRT E25NE 20010808002512001080800251NE 2001 8 8 AUS20010562 220010531G72006058T87G01 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R354 R3544123F13 NE RIGHT OVERHEATED W A UNSCHED LANDING EM VIBRATION/BUFFET OVER TEMP CRCRUISE 1 AUS (AUS) RT ENGINE OVERTEMPED DURING START UP AFTER INTENTIONAL SHUTDOWN. OVERTEMP WAS ABOVE 1000 DEGREES FOR 9 SECONDS. PERSONNEL ERROR. 2L72 4T4 TRTA52EU E8NE6 6 CP61GL 20010808002532001080800253NM 2001 8 8 AUS20010563 120010420G27525701802 JACKSCREW BOEING737 737377 NM TE FLAPS CORRODED W O OTHER F FLT CONT AFFECTED APAPPROACH 1 AUS 18978 2773 (AUS) NR 3 TRAILING EDGE FLAP JACKSCREW CORRODED. SPALLING ON SCREWJACKBALL AND NUT. SUSPECT INCORRECT LUBRICANT USED. 2L72 4F RTA16WE 20010808002542001080800254EU 2001 8 8 AUS20010564 120010531G3213350A41107620 SKID SHOE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE MAIN LANDING SEPARATED W O OTHER D INFLIGHT SEPARATION LDLANDING 1 AUS (AUS) RT SIDE SKID HEEL AND ATTACHMENT RING SEPARATED FROM AIRCRAFT. 1G71 3U3 UNCH9EU E19EU 20010808002562001080800256NM 2001 8 8 AUS20010565 120010602G3240 BRAKE BOEING747 747238B 1384828NM RROYCERB211 RB211524D41954555NE PARKING BRAKE FAULTY W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AUS (AUS) PARKING BRAKES WOULD NOT RELEASE. 2L74 4F4 F A20WE E12EU 20010807001432001080700143NM 2001 8 7 AUS20010566 120010602G3230651781914 ACTUATOR 654462514 BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU LANDING GEAR RETFAILED W K NONE ON OTHER FALSE WARNING APAPPROACH 1 AUS 29119 SC478 (AUS) NOSE LANDING GEAR DOWNLOCK ACTUATOR FAILED AT RODEND. 2L72 4F4 FRTA16WE E21EU 20010808002572001080800257SW 2001 8 8 AUS20010567 120010604G3230OAS54535 DRAG BRACE SWRNGNSA227 SA227AC 8780603SW ROTOL R321 R321482F8 GL LANDING GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR DRAG BRACE CRACKED IN UPPER GREASE FITTING SPOT FACE WEB. FOUND DURING FLUORESCENT DYE PENETRANT INSPECTION IAW AD/SWSA/226/89 AND SB 227-32-043. 2L72 4T RTA8SW 6 CP61GL 20010808002592001080800259EU 2001 8 8 AUS20010568 120010525G2910D2907019000200 MANIFOLD AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE HYDRAULIC SYSTEMCRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) HYDRAULIC POWER TRANSFER UNIT (PTU) MANIFOLD CRACKED AND LEAKING IN AREA OF CHECK VALVE MOUNTING FLANGE. 2L72 4F4 FRTA46NM E29NE 20010808002612001080800261NM 2001 8 8 AUS20010569 120010602G3250 CONTROL UNIT BOEING767 767338 1385151NM GE CF6 CF680C2* GL NLG STEERING MALFUNCTIONED W D RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 AUS (AUS) AIRCRAFT STEERING SYSTEM INTERMITTENT IN OPERATION. THE CABLESAND PULLEYS WERE CHECKED OK AND THE RUDDER PEDAL INTERCONNECT MECHANISM WAS LUBRICATED. 2L72 4F4 FRTA1NM E23EA 20010808002632001080800263SW 2001 8 8 AUS20010570 120010531G2160BYLB504371 VALVE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP HARTZLHCB3T HCB3TN5 GL CABIN TEMP SEIZED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MIXING VALVE ACTUATOR FAILED. 2L72 4T4 TRTA8SW E4WE 6 CP15EA 20010808002652001080800265SO 2001 8 8 AUS20010571 220010522G8520466080 CRANKCASE CESSNA182 182Q 2072732CE CONT O470 O470U 17026SO MCAULY2A34C 2A34C203 GL ENGINE MISOVERHAULED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) ENGINE CRANKCASE HALVES ASSEMBLED WITH A CONSIDERABLE AMOUNT OF SEALANT BETWEEN THE MATING FACES OF THE MAIN BEARING PEDESTALS. THIS RESULTED IN CRANKCASE FRETTING AND BEARING MOVEMENT. PERSONNEL/MAINTENANCE ERROR. INCORRECT ASSEMBLY. 1H71 3O3 ONT3A13 E273 5 CP3EA 20010808002662001080800266NM 2001 8 8 AUS20010572 120010531G3246165T01100530 WHEEL BOEING767 767338 1385151NM GE CF6 CF680C2* GL MLG LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS 1154 (AUS) NR 1 MAIN WHEEL TIRE REMOVED FOR WEAR. DURING REMOVAL THE WHEELNUT RETENTION BOLTS, WASHER AND NUTS WERE FOUND TO BE ADRIFT AND THE WHEEL NUT WAS LOOSE AND BACKED OFF APPROXIMATELY FIVE TURNS.THE ANTI-SKID TRANSDUCER HOUSING WAS DAMAGED. THE WHEEL NUT HAD IMPACT DAMAGE AND WHEEL NUT WASHER HAD EVIDENCE OF GALLING. NR 1 FRONT WHEEL ASSEMBLY REPLACED.ALSO REPLACED WERE THE ANTI-SKIDTRANSDUCER PNO 140-025-2, HUB CAP PNO 165T0101-107, WHEEL RETENTION NUT PNO 161T1204-1 ALONG WITH RETENTION BOLTS WASHERS AND NUTS. 2L72 4F4 FRTA1NM E23EA 20010808002672001080800267NM 2001 8 8 AUS20010573 120010603G7603 CABLE RROYCE RB211524D4 BOEING747 747338 NM RROYCERB211 RB211524D41954555NE POWER LEVER WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) DURING INSPECTION OF ENGINE THRUST CONTROL CABLES, FITTINGS AND PULLEYS IAW EI 743-076-0002 REV01 FIVE SEPARATE AREAS OF CABLEWEAR WERE FOUND. FOUND DURING INSPECTION IAW AD/B747/229 AND FAAAD 2000-05-30 AMDT 39-11640. 2L72 4F4 FRTA20WE E12EU 20010808002682001080800268WP 2001 8 8 AUS20010574 220010605G721031071627 GEAR SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C652 NE RT ENGINE FAILED W E ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 AUS 2490 (AUS) RT ENGINE FAILED. ENGINE OIL SYSTEM HEAVILY CONTAMINATED WITH METAL. INVESTIGATION FOUND FAILURE OF THE SUN/BULL GEAR.APPROXIMATELY 12 PERCENT OF THE BULL GEAR RIM HAD SEPARATED. DISASSEMBLY OF THE BULL GEAR FROM THE SUN GEAR REVEALED SEVERE FRETTING BETWEEN THE SUN GEAR REAR RACE FACE TO BULL GEAR INNER FORWARDINNER RACE FACE AND IN THE SUN GEAR TO BULL GEAR SPLINES. 2L72 4T4 TRTA5SW E4WE 6 C3PNE 20010808002692001080800269CE 2001 8 8 AUS20010575 120010522G293351170071R SIGHT GLASS CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C93 GL HYD QUANTITY SPLIT W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) HYDRAULIC SYSTEM SIGHT TUBE SPLIT. PARTIAL LOSS OF HYDRAULICFLUID. SIGHT TUBE HAD ONLY RECENTLY BEEN REPLACED. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010807001442001080700144CE 2001 8 7 AUS20010576 120010418G2932991028710 PRESSURE SWITCH CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C93 GL HYDRAULIC PRESSUFAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HYDRAULIC PRESSURE SWITCH FAULTY. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010807001452001080700145SO 2001 8 7 AUS20010577 220010521G7414 IMPULSE COUPLINGCONT IO520F CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL MAGNETO/DISTRIBUWORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH MAGNETO IMPULSE COUPLING WORN BEYOND LIMITS. FOUND DURINGINSPECTION IAW AD/ELEC/68. 1H71 3O3 O A4CE E5CE 5 CP21EA 20010807001462001080700146CE 2001 8 7 AUS20010578 120010529G2410646655 COUPLING CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C93 GL ALTERNATOR-GENERFAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH ALTERNATOR ELASTOMER DRIVE COUPLING SLIPPING. FOUND DURING INSPECTION IAW MEB 01-3. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010807001472001080700147EA 2001 8 7 AUS20010579 220010604G7414ES10357426 DISTRIBUTOR BENDIX 101630509 PIPER PA24 PA24250 7102404SO LYC O540 O540A1D5 41532EA MCAULY2D36C 2D36C28 GL MAGNETO/DISTRIBUFAULTY W K NONE E VIBRATION/BUFFET TOTAKEOFF 1 AUS A34026 (AUS) MAGNETO DISTRIBUTOR BLOCK CENTRAL BUSH LOOSE ALLOWING THE DISTRIBUTOR GEAR TO PARTIALLY DISENGAGE AND SHEAR THE TEETH. 1L71 3O3 O 1A15 E295 5 CP901 20010807001482001080700148NM 2001 8 7 AUS20010580 120010424G3520417T42050 OXYGEN MASK BOEING767 767204 NM GE CF6 CF680A 30025NE PASSENGER OXYGENFAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PASSENGER OXYGEN MASKS (7OFF) SUSPECT FAULTY. FOUND DURINGINSPECTION IAW AD/B767/125. 2L72 4F4 FRTA1NM E13NE 20010808002702001080800270NM 2001 8 8 AUS20010581 120010406G2450941D3352 CIRCUIT BREAKER BOEING737 737377 NM AC POWER DISTRIBFAILED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 AUS 42099 (AUS) NR 1 GENERATOR BREAKER FAILED. 2L72 4F RTA16WE 20010807001492001080700149NE 2001 8 7 AUS20010582 220010227G732177390010 FCU LYC ALF502R5 BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE FUEL CONTROL/TURFAULTY W K NONE E VIBRATION/BUFFET NRNOT REPORTED 1 AUS 7600 F12203 (AUS) NO1 ENGINE FUEL CONTROL UNIT FAULTY. 2H74 4F4 F A49EU E6NE 20010808002712001080800271NM 2001 8 8 AUS20010583 120010605G5610NAS71037 SCREW DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE WINDOW WRONG PART W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLIGHT DECK SIDE WINDOW REPLACEMENT BOLTS TOO LONG. SB DHC8-56-05 SPECIFIES SCREW PNO NAS7103-7 WHICH WHEN FITTED ARE TOO LONG ANDBECOME SHANK BOUND. CONTACT WITH THE AIRCRAFT MANUFACTURER FOUND THAT THE SCREWS SHOULD BE PNO NAS7103-6. THE RETORQUE PERIOD REQUIREMENT IN THE SERVICE BULLETIN IS ALSO SUSPECT BEING STATEDAS AFTER 24 HOURS'. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010808002722001080800272NM 2001 8 8 AUS20010584 120010605G2910B4706640192 HOSE BOEING737 737377 NM HYDRAULIC SYSTEMLEAKING W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 AUS (AUS) LH MAIN LANDING GEAR UPLOCK ACTUATOR HOSE LEAKING. METALCONTAMINATION OF NO1 HYDRAULIC PUMP FILTERS. 2L72 4F RTA16WE 20010808002732001080800273NM 2001 8 8 AUS20010585 120010601G2621301000223 EXTINGUISHER BOEING767 767338 1385151NM GE CF6 CF680C2* GL LAVATORY MISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NO AUTOMATIC FIRE EXTINGUISHER FITTED TO THE FORWARD MID LAVATORY M-37. FOUND DURING INSPECTION IAW CAA AD GENERAL/48 AND FAA AD74-08-09. 2L72 4F4 FRTA1NM E23EA 20010807001502001080700150SO 2001 8 7 AUS20010586 120010515G81204066109020 TURBOCHARGER LYC TIO540A2C PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA HARTZLHCE3Y HCE3YR2 GL EXHAUST TURBOCHAFAILED W K NONE E VIBRATION/BUFFET CRCRUISE 1 AUS 415 (AUS) LH ENGINE TURBOCHARGER LEAKING OIL. SUSPECT BEARING OR SEAL DAMAGED. AIRCRAFT HAD BEEN OUT OF SERVICE FOR APPROXIMATELY NINEMONTHS FOR A SPAR REPLACEMENT. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010807001512001080700151SO 2001 8 7 AUS20010587 220010604G8550S19644 DRAIN VALVE CONT IO520F CESSNA207 207 2073602CE CONT O520 IO520F 17032SO MCAULY2A34C D2A34C58 GL RECIPROCATING ENCRACKED W KE NONE ENGINE SHUTDOWN EK VIBRATION/BUFFET FLUID LOSS NRNOT REPORTED 1 AUS (AUS) ENGINE OIL DRAIN VALVE SHAFT CRACKED RADIALLY. OIL LEAKING ON SHUTDOWN. 1H71 3O3 O A16CE E5CE 5 CP3EA 20010808002742001080800274EU 2001 8 8 AUS20010588 120010601G7930154 CONNECTOR AEROSPAS365 AS365N2 8680815EU TMECA ARRIELARRIEL1A 60030NE CHIP DETECTOR FAULTY W A UNSCHED LANDING N FALSE WARNING CRCRUISE 1 AUS (AUS) NR 2 ENGINE CHIP DETECTOR WIRING FAULTY. 1G72 3U3 URTH10EU E19EU 20010808002752001080800275EU 2001 8 8 AUS20010589 120010528G3510MC1012100 OXYGEN MASK AMD FALC50FALCON900 2700160EU COCKPIT LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PILOTS OXYGEN MASK LEAKING AT OXYGEN SUPPLY QUICK DISCONNECT. THIS DEFECT WAS RECEIVED FROM NO34 SQUADRON RAAF AND IS FOR INFORMATION ONLY. AIRCRAFT SERIAL A26-073. 2L73 4F RTA46EU 20010808002762001080800276EU 2001 8 8 AUS20010590 120010604G3240C24837010 MANIFOLD AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE LANDING GEAR CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS 29336 B728 (AUS) LT BRAKE MANIFOLD LEAKING. INVESTIGATION FOUND A CRACK LOCATEDBETWEEN PORT A (SUPPLY LINE) AND FILTER CHAMBER. 2L72 4F4 FRTA46NM E29NE 20010808002772001080800277SO 2001 8 8 AUS20010591 220010517G8530 EXHAUST VALVE CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO ENGINE STUCK W K NONE O OTHER ININSP/MAINT 1 AUS 141 (AUS) NR 2 CYLINDER EXHAUST VALVE STICKING IN VALVE GUIDE. FURTHER INSPECTION FOUND ALL EXHAUST VALVES STICKING AND ALL EXHAUST PUSHRODS BENT. SUSPECT VAVLE TO GUIDE CLEARANCE INSUFFICIENT AT MANUFACTURE. 1H71 3O3 O A4CE E5CE 20010807001522001080700152NM 2001 8 7 AUS20010592 120010528G5610NP15790114 WINDSHIELD DHAV DHC8 DHC8* NM FLIGHT COMPARTMECRACKED W K NONE O OTHER CRCRUISE 1 AUS (AUS) RH WINDSHIELD CRACKED. 2H72 4T RTA13NM 20010807001532001080700153SW 2001 8 7 AUS20010593 120010529G5302206023119063 SUPPORT BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ROTORCRAFT TAIL CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HORIZONTAL STABILISER UPPER LH SUPPORT CRACKED LONGITUDINALLY ALONG BEND RADIUS. CRACK LENGTH 30MM (1.181IN). 1G71 3U3 U H2SW E1GL 20010807001542001080700154SW 2001 8 7 AUS20010594 120010530G5302206032400027 BULKHEAD BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ROTORCRAFT TAIL CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAILBOOM BULKHEAD CRACKED ALONG THE BEND RADIUS OUTER CIRCUMFERENCE AT THE TOP RH BOLT ATTACHMENT INTERCOSTAL. CRACKLENGTH 10MM (0.393IN). 1G71 3U3 U H2SW E1GL 20010808002782001080800278EU 2001 8 8 AUS20010595 120010517G2760 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DRAG CONTROL OUT OF ADJ W O OTHER F FLT CONT AFFECTED LDLANDING 1 AUS (AUS) LIFT DUMPER MANIFOLD NR 2 BYPASS SWITCH OUT OF ADJUSTMENT. 2L72 4F4 FRTA20EU E2EU 20010808002792001080800279NE 2001 8 8 AUS20010597 220010518G7310 FILTER DHAV DHC8 DHC8* NM PWA PW120 PW123 NE ENGINE FUEL CONTAMINATED W C ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NR 2 HP OUTLET FUEL FILTER CONTAMINATED WITH A DARK BROWN SLUDGE. 2H72 4T4 TRTA13NM E20NE 20010807001552001080700155EU 2001 8 7 AUS20010598 120010519G324195427193 GENERATOR FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU BRAKE ANTISKID SFAULTY W K NONE OP OTHER NO WARNING INDICATION LDLANDING 1 AUS 3588 OCT7043 (AUS) RH INBOARD WHEEL SPEED GENERATOR FAULTY. 2L72 4F4 FRTA20EU E2EU 20010807001562001080700156EU 2001 8 7 AUS20010601 120010526G2410 GENERATOR FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU ALTERNATOR-GENERFAILED W K NONE H ELECT. POWER LOSS-50 PC CRCRUISE 1 AUS (AUS) NO1 GENERATOR FAILED. SUSPECT FAULTY CONSTANT SPEED DRIVE SWITCH. 2L72 4F4 FRTA20EU E2EU 20010807001572001080700157EU 2001 8 7 AUS20010602 120010530G2421976J2555 GENERATOR FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU AC GENERATOR-ALTFAILED W K NONE H ELECT. POWER LOSS-50 PC DEDESCENT 1 AUS 397 MC823 (AUS) NO2 (RH) GENERATOR FAILED. 2L72 4F4 FRTA20EU E2EU 20010807001582001080700158EU 2001 8 7 AUS20010603 120010526G5330 SKIN FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU FUSELAGE MAIN, PCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TOP FUSELAGE SKIN CRACKED IN AREA BETWEEN STN3845 AND STN4875.CRACK LENGTH 406.4MM (16IN). 2L72 4F4 FRTA20EU E2EU 20010808002802001080800280WP 2001 8 8 AUS20010604 220010604G725031038381 ROTOR BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C653 NE TURBINE SECTION DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT ENGINE T3 TURBINE BLADE DAMAGED. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010808002812001080800281NM 2001 8 8 AUS20010605 120010221G254010101000BA VALVE BOEING737 737377 NM LAVATORIES FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS 3340 (AUS) TOILET DRAIN VALVE FAULTY. FOUND DURING TESTING IAW ER B73-30-11. 2L72 4F RTA16WE 20010807001592001080700159NM 2001 8 7 AUS20010607 120010520G27507321870011 VALVE BOEING767 767277 NM GE CF6 CF680A 30025NE TRAILING EDGE FLFAILED W K NONE FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 AUS 93043 (AUS) FLAP/SLAT SHUTOFF VALVE FAILED. 2L72 4F4 FRTA1NM E13NE 20010808002822001080800282EU 2001 8 8 AUS20010608 120010607G2910AE7064588 HOSE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R375 R3754123F21 NE HYDRAULIC SYSTEMFAILED W C ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 AUS 21142 (AUS) NOSE LANDING GEAR HYDRAULIC UP LINE FAILED. LOSS OF HYDRAULIC FLUID. 2L72 4T4 TRTA52EU E8NE 6 CP17NE 20010808002832001080800283SO 2001 8 8 AUS20010609 220010525G8530641917 CYLINDER CESSNA150 150F 2071814CE CONT O200 O200A 17020SO MCAULY1A100 1A100MCM GL ENGINE CRACKED W A UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 AUS 1500 (AUS) ENGINE CYLINDER ROCKER SHAFT SUPPORT CRACKED AND SEPARATED FROM CYLINDER HEAD. 1H71 3O3 O 3A19 E252 5 NP918 20010808002842001080800284EA 2001 8 8 AUS20010611 220010613G8530 PISTON RING PIPER PA28 PA28180 7102808SO LYC O360 O360A3A 41514EA ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 1015 (AUS) NR 3 CYLINDER FIRST AND SECOND PISTON RINGS BROKEN. PISTON LANDERODED. NR 4 CYLINDER NO1 PISTON RING BROKEN. PISTON RINGS WERECAST IRON IN CHROME CYLINDERS. SMALL AMOUNT OF ALUMINIUM ALLOYMETAL IN OIL FILTER. 1L71 3O3 O 2A13 E286 20010807001602001080700160CE 2001 8 7 AUS20010612 120010608G5610 WINDSHIELD CESSNA 421C CESSNA421 421C 2076016CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL FLIGHT COMPARTMEFAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) WINDSHIELD LEAKING. HEATING SYSTEM PIPES BROKEN CAUSING EXCESSHEAT AND WARPING OF WINDSHIELD. 1L72 3O3 O A7CE E7CE 5 CP45GL 20010808002852001080800285CE 2001 8 8 AUS20010613 120010612G61205052447815 SPRING BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HARTZLHCB4M HCB4MP3 GL PROPELLER BROKEN W O OTHER O OTHER NRNOT REPORTED 1 AUS (AUS) LH PROPELLER PITCH CONTROL LEVER FEATHER DETENT FEEL SPRING BROKEN. 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20010807001612001080700161SO 2001 8 7 AUS20010614 220010612G7421RHB32E SPARK PLUG CONT TSIO520VB CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C93 GL SPARK PLUG/IGNITCORRODED W K NONE E VIBRATION/BUFFET CRCRUISE 1 AUS (AUS) LH ENGINE SPARK PLUG CORRODED AND FOULED. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010808002862001080800286NM 2001 8 8 AUS20010615 120010508G493036080004 FCU BOEING737 737377 NM APU ENGINE FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) APU FUEL CONTROL UNIT FAULTY. INVESTIGATION FOUND PISTON ANDSHAFT SET IN TIMER WORN. THE GOVERNOR SHAFT WAS WORN. FLYWEIGHT TOES WORN. PACKINGS AND SEALS FLAT AND WORN. 2L72 4F RTA16WE 20010808002872001080800287NM 2001 8 8 AUS20010616 120010426G28226075504 PUMP BOEING747 747238B 1384828NM FUEL BOOST PUMP LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS 7670 069714832A (AUS) NR 3 AFT FUEL BOOST PUMP LEAKING FROM AREA BEHIND ELECTRICAL CONNECTOR. 2L74 4F A20WE 20010808002882001080800288NM 2001 8 8 AUS20010617 120010415G5320 WEB BOEING747 747238B 1384828NM FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE WHEEL WELL UPPER WEB LOCATED AT STN291 CRACKED AT RBL19 ANDLBL19. 2L74 4F A20WE 20010807001622001080700162NM 2001 8 7 AUS20010618 120010420G5313146T30037 STRINGER BOEING767 767277 NM GE CF6 CF680A 30025NE FUSELAGE MAIN, LCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) STRINGER 39L BADLY CORRODED IN THE AREA LOCATED BETWEEN BS1285AND BS1307. APPROXIMATELY 304.8MM (12IN) OF THE HAT SECTIONED STRINGER LOWER CHANNEL WAS SEVERELY CORRODED WITH PORTIONS OF THE CHANNEL TOTALLY DESTROYED. 2L72 4F4 FRTA1NM E13NE 20010808002892001080800289NE 2001 8 8 AUS20010619 220010616G7200 ENGINE BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE NR 2 LEAKING W K NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 AUS (AUS) NR 2 ENGINE LEAKING CONTAMINATED AIR INTO CABIN. 2H74 4F4 FRTA49EU E6NE 20010808002902001080800290CE 2001 8 8 AUS20010620 120010612G2752100384040 MOTOR BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE MCAULY4HFR344HFR34C754 NE TE FLAPS BURNED OUT W A UNSCHED LANDING F FLT CONT AFFECTED DEDESCENT 1 AUS 514 (AUS) TRAILING EDGE FLAP ELECTRIC MOTOR WINDINGS BURNT OUT. SUSPECT CAUSED BY FAILURE OF DYNAMIC BRAKE. 1L72 4T4 T A24CE E4EA 6 C3PNE 20010807001632001080700163CE 2001 8 7 AUS20010621 120010608G321345815237 PIN BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MCAULY3AF32CD3AF32C35 GL MAIN LANDING GEACRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH AND RH MAIN LANDING GEAR LOWER TORQUE LINK PINS CRACKED IN THE POSITIONING HOLES. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20010808002912001080800291EU 2001 8 8 AUS20010622 120010616G5330 SKIN BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R3A 41580NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE SKIN CRACKED IN AREA LOCATED IMMEDIATELY AFT OF FRAME 29 BENEATH THE WING ROOT DOUBLER. FOUND DURING INSPECTION IAWISB53-144 AND AD/BAE146/70. 2H74 4F4 FRTA49EU E6NE 20010808002922001080800292NE 2001 8 8 AUS20010623 220010613G7230230318706 SEAL BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE ENGINE LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS 4333 (AUS) NR 2 ENGINE OIL LEAKING IN BLEED BAND AREA. OIL SMELL IN COCKPIT.SUSPECT CAUSED BY NO1 OIL SEAL WORN AND LEAKING. 2H74 4F4 F A49EU E6NE 20010808002932001080800293EU 2001 8 8 AUS20010624 120010607G3240C24837010 MANIFOLD AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE LANDING GEAR CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS B353 (AUS) LT MAIN LANDING GEAR BRAKE SERVO MANIFOLD LEAKING FROM AREA OFFILTER CAP. INVESTIGATION FOUND A 19.05MM (0.75IN) CRACK IN THE FILTER CHAMBER THREADS. 2L72 4F4 FRTA46NM E29NE 20010807001642001080700164CE 2001 8 7 AUS20010625 120010603G272007331131 CLIP CESSNA182 182Q 2072732CE CONT O470 O470U 17026SO MCAULY2A34C 2A34C203 GL RUDDER CONTROL SFAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH RUDDER STOP T' CLIP PNO 733113-1 TO SUPPORT PNO 1231021-8 ATTACHMENT RIVETS (2OFF) PNO MS20426-AD4 SHEARED. SUSPECT CAUSED BY WIND GUSTS. 1H71 3O3 ONT3A13 E273 5 CP3EA 20010808002942001080800294NM 2001 8 8 AUS20010626 120010615G5330149T7500145 PANEL BOEING767 767338 1385151NM GE CF6 CF680C2* GL FUSELAGE MISSING W O OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 AUS (AUS) FUSELAGE PANEL MISSING FROM LH WING ROOT AREA LOCATED FORWARD OFTHE LH OFF-WING ESCAPE SLIDE DOOR. SCORE MARKS EVIDENT ON ADJACENT WING TO BODY FAIRING AND FUSELAGE AT STN1131. 2L72 4F4 FRTA1NM E23EA 20010808002952001080800295NM 2001 8 8 AUS20010627 120010618G750065B899268 DUCT BOEING747 747438 NM RROYCERB211 RB211524G19 NE ENGINE BLEED AIRFAILED W A UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 AUS (AUS) NR 3 ENGINE STRUT DUCT HOLED AND DEFORMED. INVESTIGATION COULD FIND NO HEAT DAMAGE IN THE STRUT. 2L74 4F4 FRTA20WE E30NE 20010807001652001080700165CE 2001 8 7 AUS20010629 120010608G57110001100132 SPAR CAP BEECH 58 BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MCAULY3AF32CD3AF32C35 GL WING SPAR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS TH181 (AUS) RH WING UPPER SPAR CAP CONTAINED PITTING CORROSION IN AN AREA LOCATED 355.6MM (14IN) OUTBOARD OF THE ENGINE NACELLE. THE PITTED AREA MEASURES APPROXIMATELY 152.4MM (6IN) SPANWISE AND 19.05MM(0.75IN) CHORDWISE. DEPTH OF CORROSION APPROXIMATELY 0.508MM(0.020IN). FOUND FOLLOWING STRIPPING FOR REPAINT. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20010807001662001080700166NM 2001 8 7 AUS20010630 120010127G291013206001 SWITCH 13206XXX BOEING767 767238 NM PWA JT9 JT9D7R4E 52054NE HYDRAULIC SYSTEMFAULTY W K NONE J WARNING INDICATION CRCRUISE 1 AUS (AUS) LH HYDRAULIC TAIL SHUTOFF VALVE SWITCH MODULE FAULTY. 2L72 4F4 FRTA1NM E3NE 20010808002962001080800296NM 2001 8 8 AUS20010631 120010619G27202417001007 MODULE BOEING747 747SP38 NM RROYCERB211 RB211524D41954555NE RUDDER CONTROL LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS 18014 105 (AUS) RUDDER CONTROL MODULE LEAKING. 2L74 4F4 FRTA20WE E12EU 20010808002972001080800297CE 2001 8 8 AUS20010632 120010611G534312116013 FITTING CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO LANDING GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH OUTBOARD LANDING GEAR ATTACHMENT FITTING CRACKED. CRACK LENGTH 19.05MM (0.75IN). 1H71 3O3 O A4CE E5CE 20010807001672001080700167EA 2001 8 7 AUS20010633 220010530G852038125015 STUD LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL RECIPROCATING ENBROKEN W K NONE OEKOTHER VIBRATION/BUFFET FLUID LOSS ININSP/MAINT 1 AUS L778561A (AUS) LH ENGINE NO3 CYLINDER HOLDDOWN STUDS BROKEN. CYLINDER WAS HELD IN PLACE BY THE THROUGH BOLTS ONLY. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010808002982001080800298EU 2001 8 8 AUS20010634 120010619G6220350A31190703 STARFLEX AEROSP 355A310002 SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE MAIN ROTOR HEAD DEBONDED W O OTHER F FLT CONT AFFECTED LDLANDING 1 AUS M1803 (AUS) MAIN ROTOR STAR BEARING BUSH DEBONDED AND MOVED OUTBOARD ALLOWING THE MAIN ROTOR BLADE TO LAG AND CAUSE LATERAL VIBRATION. 1G71 3U3 U H9EU E00054EN 20010808002992001080800299NM 2001 8 8 AUS20010635 120010618G21507744694 ACM BOEING747 747438 NM RROYCERB211 RB211524G19 NE CABIN COOLING SYFAULTY W D RETURN TO BLOCK FB FLT CONT AFFECTED SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 AUS 668 (AUS) NR 1 AIRCONDITIONING SYSTEM AIR CYCLE MACHINE FAULTY. 2L74 4F4 FRTA20WE E30NE 20010808003012001080800301NE 2001 8 8 AUS20010636 220010617G8520 MASTER ROD DOUG DC3 DC3CS1C3G 3021458WP PWA R1830 R183092 52020NE HAMSTD23E 23E50 NE ENGINE FAILED W C ABORTED TAKEOFF EK VIBRATION/BUFFET FLUID LOSS TOTAKEOFF 1 AUS (AUS) RT ENGINE NR 5 CYLINDER MASTER ROD FAILED AT BASE. LOSS OF ENGINEOIL. 2L72 4R4 R A669 5E4 6 CP603 20010808003022001080800302EU 2001 8 8 AUS20010637 120010607G3240C24837010 MANIFOLD AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE LANDING GEAR CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS B353 (AUS) LH MAIN LANDING GEAR BRAKE SERVO MANIFOLD CRACKED. INVESTIGATIONFOUND A CRACK IN THE FILTER CHAMBER THREADS. CRACK LENGTH 19.05MM (0.75IN). 2L72 4F4 FRTA46NM E29NE 20010808003032001080800303EU 2001 8 8 AUS20010638 120010510G5343D5337061320200 FITTING AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE LANDING GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR DOOR ACTUATOR FITTINGS CRACKED FROM FASTENERHOLES. FOUND DURING INSPECTION IAW SB A320-53-1135 AND ANSETT ERA32-53-40-9C. 2L72 4F4 FRTA46NM E29NE 20010808003042001080800304NM 2001 8 8 AUS20010639 120010617G71103859741B12130620BRACKET GE CF680C2 BOEING767 767338 1385151NM GE CF6 CF680C2* GL ENGINE COWLING BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS R648117 (AUS) NR 1 ENGINE INBOARD THRUST REVERSER COWL V' BAND HOOK BRACKET BROKEN. 2L72 4F4 FRTA1NM E23EA 20010807001682001080700168SW 2001 8 7 AUS20010640 120010603G2460A1077V RELAY BELL 206 206L1 1182107SW ALLSN 250C 250C30 03013GL DC POWER DISTRIBFAILED W K NONE H ELECT. POWER LOSS-50 PC CRCRUISE 1 AUS (AUS) GENERATOR LINE CONTACT RELAY FAULTY. 1G71 3U3 U H2SW E1GL 20010808003052001080800305SW 2001 8 8 AUS20010641 120010606G29102281032135 PIPE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TFE33112UHR WP ROTOL R321 R321482F8 GL HYDRAULIC SYSTEMWORN W A UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 AUS (AUS) HYDRAULIC PIPE CHAFING AGAINST ADJOINING PIPE. LOSS OF HYDRAULICSYSTEM FLUID. 2L72 4T4 TRTA8SW E4WE 6 CP61GL 20010807001692001080700169SW 2001 8 7 AUS20010642 120010614G5740AN616 BOLT BBAVIA7 7GCAA 21101N8SW LYC O320 O320A2D 41508EA SNSNCH74D 74DM EA WING, ATTACH FITCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LOWER RH SIDE STRUT LOWER BOLT SEIZED. FOLLOWING BOLT REMOVAL ITWAS FOUND TO BE VERY RUSTED AND PITTED. 1H71 3O3 O A759 E274 5 NP88614 20010807001702001080700170CE 2001 8 7 AUS20010643 120010601G2720530040050 CONTROL CABLE CESSNA340 340A 2076405CE CONT O520 TSIO520N 17040SO MCAULY3AF32C3AF32C93 GL RUDDER CONTROLS FRAYED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) YAW DAMPER CABLE FRAYED AND STRANDS BROKEN IN AREA WHERE THECABLE PASSES INTO THE TERMINAL FITTING AT THE RUDDER BELLCRANK. 1L72 3O3 O 3A25 E8CE 5 CP22EA 20010808003072001080800307NM 2001 8 8 AUS20010644 120010620G21317120977 CONTROLLER BOEING747 747338 NM RROYCERB211 RB211524D41954555NE CABIN PRESSURE FAULTY W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 AUS 79G1173 (AUS) PRESSURISATION SYSTEM OUTFLOW VALVES SLIGHTLY OPEN. INVESTIGATION COULD FIND NO CAUSE OF THE DEFECT. THE CABIN PRESSURE CONTROLLERWAS REPLACED BUT FOUND TO SERVICEABLE WHEN WORKSHOP TESTED. 2L72 4F4 FRTA20WE E12EU 20010807001712001080700171CE 2001 8 7 AUS20010645 120010612G2434 BEARING ALV9510R CESSNA421 421C 2076016CE CONT O520 GTSIO520N 17032SO MCAULY3FF32 3FF32C501 GL DC GENERATOR-ALTFAILED W K NONE H ELECT. POWER LOSS-50 PC CRCRUISE 1 AUS 18 (AUS) LH ALTERNATOR. INVESTIGATION FOUND REAR BEARING COLLAPSED CAUSING DRIVE ADAPTER FAILURE AND METAL CONTAMINATION OF THE ENGINE. 1L72 3O3 O A7CE E7CE 5 CP45GL 20010807001722001080700172CE 2001 8 7 AUS20010647 120010621G3710212CW PUMP AIRBORNE 212CW BEECH 55 D55 1152730CE CONT O520 IO520C 17032SO MCAULY2AF34C2AF34C55 GL VACUUM DISTRIBUTFAILED W K NONE I FLT. ATTITUDE INST. NRNOT REPORTED 1 AUS 23J119 (AUS) LH ENGINE DRIVEN VACUUM PUMP ROTOR SEIZED AND DRIVESHAFT SHEARED. 1L72 3O3 O 3A16 E5CE 5 CP5EA 20010807001732001080700173EA 2001 8 7 AUS20010648 220010531G854067583 GEAR LYC VO540C2A HILLERUH12 UH12E 4360122WP LYC O540 VO540C2A 41532EA RECIPROCATING ENFAILED W K NONE EY VIBRATION/BUFFET ENGINE STOPPAGE NRNOT REPORTED 1 AUS L146243 (AUS) ENGINE DRIVE GEAR PNO 67583 HAD SHEARED ALL THE BOLTS ATTACHING IT TO ACCESSORY DRIVE PNO 67609. 1G71 3O3 O 4H11 E304 20010808003152001080800315NM 2001 8 8 AUS20010649 120010621G3244A2409 TIRE BOEING747 747438 NM RROYCERB211 RB211524G19 NE MLG FAILED W C ABORTED TAKEOFF O OTHER TOTAKEOFF 1 AUS 9652 (AUS) LT REAR INBOARD MAIN BODY GEAR TYRE (NO4) FAILED. DAMAGE CAUSED TO FUSELAGE AND FAIRINGS AND LANDING GEAR WIRING LOOM. 2L74 4F4 FRTA20WE E30NE 20010807001742001080700174SW 2001 8 7 AUS20010650 120010623G5313206031314037 LONGERON BELL 206L1 BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL FUSELAGE MAIN, LCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 10824 45323 (AUS) FUSELAGE LONGERON CRACKED BETWEEN TWO RIVETS. 1G71 3U3 U H2SW E1GL 20010808003162001080800316EU 2001 8 8 AUS20010652 120010622G5610NP1701012 WINDSHIELD BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE COCKPIT FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 96249H6419 (AUS) RT A' WINDSHIELD ASSEMBLY OUTER PANE SHATTERED. 2H74 4F4 FRTA49EU E6NE 20010808003202001080800320EU 2001 8 8 AUS20010653 120010607G5210FGFB222030060A2 CLEVIS AMD FALC50FALCON900 2700160EU GARRTTTFE731TFE7315BR WP PAX/CREW DOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN ENTRY DOOR COMPENSATING SPRING CLEVIS CRACKED ACROSS ALL THREE CABLE ATTACHMENT LUGS. AIRCRAFT SERIAL NUMBER A26-074.FLEET INSPECTION FOUNDTHE CLEVIS CRACKED ON ALL OTHER AIRCRAFTIN THE RAAF FLEET. THIS DEFECT WAS RECEIVED FROM THE RAAF AND ISENTERED FOR INFORMATION ONLY. 2L73 4F4 FRTA46EU E6WE 20010808003222001080800322 2001 8 8 AUS20010655 420010626G341818617RX DETECTOR REIMS 406 F406 EU PWA PT6 PT6A112 52043NE MCAULY3G34C73GFR34C701 GL STALL WARNING SYFAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LIFT DETECTOR FAULTY. SWITCH OPERATES IN OPPOSITE SENSE. 1L72 3T3 TRTA54EU E4EA 5 CP60GL 20010808003232001080800323 2001 8 8 AUS20010656 420010620G341818617RX DETECTOR REIMS 406 F406 EU PWA PT6 PT6A112 52043NE MCAULY3G34C73GFR34C701 GL STALL WARNING FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS 263 (AUS) LIFT DETECTOR FAULTY. DETECTOR MICROSWITCH OPERATES IN OPPOSITE SENSE. SWITCH SPRING LOADED UP. PERSONNEL/MAINTENANCE ERROR.MANUFACTURING ERROR. 1L72 3T3 TRTA54EU E4EA 5 CP60GL 20010808003242001080800324NE 2001 8 8 AUS20010657 220010625G7250UL36853 SUPPORT RROYCE RB211524G BOEING747 747438 NM RROYCERB211 RB211524G19 NE TURBINE SECTION LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS 576 13044 (AUS) ENGINE HP/IP TURBINE BEARING SUPPORT OIL PIPE LEAKING AT SUPPORTATTACHMENT. 2L74 4F4 FRTA20WE E30NE 20010808003252001080800325EU 2001 8 8 AUS20010658 120010430G5343D5337061320200 FITTING D53370613203AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE LANDING GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR DOOR ACTUATOR FITTINGS (4OFF) CRACKED FROM THEUPPER TWO FASTENER HOLES IN THE VERTICAL FLANGE. 2L72 4F4 FRTA46NM E29NE 20010808003272001080800327NM 2001 8 8 AUS20010659 120010503G5755656718613 FITTING BOEING737 737377 NM SPOILERS FRACTURED W K NONE O OTHER ININSP/MAINT 1 AUS MA2489 (AUS) LT INBOARD GROUND SPOILER CENTRE OUTBOARD HINGE FITTING HAD A MISSING PIECE ALLOWING THE HINGE BEARING TO LOOSEN IN THE FITTING. 2L72 4F RTA16WE 20010807001752001080700175NM 2001 8 7 AUS20010660 120010615G6310A1681 PLATE ROBSINR22 R22BETA NM LYC O360 O360J2A 41514EA ENGINE/TRANSMISSCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) CLUTCH SEAL PLATE CRACKED IN MORE THAN ONE PLACE ON BOTH SIDES. 1G71 3O3 O H10WE E286 20010808003282001080800328EU 2001 8 8 AUS20010661 120010510G5343D5337061320200 FITTING AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE LANDING GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR DOOR ACTUATOR ATTACHMENT FITTINGS (4OFF)CRACKED FROM TOP TWO FASTENER HOLES IN THE VERTICAL FLANGE. 2L72 4F4 FRTA46NM E29NE 20010807001762001080700176SO 2001 8 7 AUS20010662 120010626G55404004009 TORQUE TUBE PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA HARTZLHCE2Y HCE2YK2 GL RUDDER STRUCTURECORRODED W K NONE O OTHER ININSP/MAINT 1 AUS 7066 (AUS) RUDDER TORQUE TUBE CORRODED BOTH INTERNALLY AND EXTERNALLY. 1L72 3O3 O A20SO E14EA 5 CP9EA 20010807001772001080700177NM 2001 8 7 AUS20010663 120010625G3230DSC1831 RELAY DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE LANDING GEAR RETFAULTY W K NONE O OTHER DEDESCENT 1 AUS (AUS) LANDING GEAR DOOR SEQUENCE CONTROL RELAY K12 FAULTY. DURING FUNCTION CHECKS RELAY K13 PNO DSC183-2 WAS ALSO FOUND TO BE FAULTY. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010808003302001080800330NM 2001 8 8 AUS20010664 120010308G5210BACB10FK6F6HS ROLLER BOEING737 73733A 1384673NM PAX DOOR SEIZED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PASSENGER DOOR R1 SEQUENCING CAM ROLLER SEIZED AND DISINTEGRATEDPREVENTING CORRECT OPERATION OF DOOR. 2L72 4F RTA16WE 20010807001782001080700178CE 2001 8 7 AUS20010665 120010426G324398820104 CYLINDER CESSNA182 182S 2072701CE LYC O540 IO540AB1A5 EA MCAULY3D36C B3D36C431 GL MASTER CYLINDER/LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH BRAKE MASTER CYLINDER LEAKING AT ELBOW FITTING. INVESTIGATIONFOUND THAT THE ELBOW HAD NOT BEEN FULLY SCREWED IN AND THESEALING O' RING WAS DISPLACED ONTO THE THREADS OF THE ELBOW INSTEAD OF FITTING INTO THE SEAL RECESS DUE TO THE B' NUTCOVERING THE RECESS. 1H71 3O3 ONT3A13 1E4 5 C 20010808003312001080800331NE 2001 8 8 AUS20010666 220010624G7260208315905 MOUNT BAC 146 146100A 1500260EU LYC ALF502ALF502R5 41580NE ENGINE BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 1 ENGINE CSD MOUNTING RING MOUNTING BOSSES (5OFF) BROKEN AWAY. 2H74 4F4 FRTA49EU E6NE 20010808003322001080800332NM 2001 8 8 AUS20010667 120010628G783013169 DOOR RROYCE RB211524G BOEING747 747438 NM RROYCERB211 RB211524G19 NE THRUST REVERSER FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 12575 13169 (AUS) NR 3 ENGINE NR 10 THRUST REVERSER BLOCKER DOOR PARTLY MISSING WITH DAMAGE TO THE CORONA LOCATED AFT OF THE DOOR POSITION AND A SMALL TEAR ON THE CORONA ACOUSTIC PANEL. 2L74 4F4 FRTA20WE E30NE 20010808003342001080800334NE 2001 8 8 AUS20010668 220010628G7200RB211524D419 ENGINE BOEING747 747338 NM RROYCERB211 RB211524D41954555NE NR 2 VIBRATES W A UNSCHED LANDING EF VIBRATION/BUFFET FLT CONT AFFECTED CRCRUISE 1 AUS 254 (AUS) NR 2 ENGINE EXCESSIVE VIBRATION. ENGINE INSPECTED IAW MAINTENANCEMANUALS WITH NO FAULTS FOUND. HPC STAGES 5/6 BOROSCOPED AND FOUND OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA20WE E12EU 20010807001792001080700179NM 2001 8 7 AUS20010669 120010620G52306546921225 DOOR BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU CARGO/BAGGAGE DOCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 35309 001895 (AUS) FORWARD CARGO DOOR CRACKED IN THE RADIUS OF THE FORWARD OUTBOARDCORNER ANGLE. CRACK LENGTH 35.56MM (1.4IN). FOUND DURINGINSPECTION IAW EI 737-052-0003, FAA AD2000-07-06 AND AD/B737/142. 2L72 4F4 FRTA16WE E21EU 20010808003352001080800335SO 2001 8 8 AUS20010670 120010627G5741401187 BOLT PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA SNSNCH74D 74DM EA WING LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING REAR SPAR ATTACHMENT BOLTS LOOSE WITH NUT HOLDING BY ONLY THREE THREADS. SUSPECT NUTS NOT TIGHTENED AT LAST MAINTENANCE INSPECTION FOLLOWING WORK CARRIED OUT IN THE AREA.PERSONNEL/MAINTENANCE ERROR. 1L71 3O3 O 2A13 E274 5 NP88614 20010808003372001080800337NM 2001 8 8 AUS20010671 120010626G3520335841 COMPENSATOR BOEING747 747238B 1384828NM RROYCERB211 RB211524D41954555NE PASSENGER OXYGENCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS 10501 (AUS) NO6 PASSENGER OXYGEN BOTTLE THERMAL COMPENSATOR SWAGED FITTINGCORRODED. AIRCRAFT IS REGISTERED DQ-FJE. 2L74 4F4 F A20WE E12EU 20010808003382001080800338NM 2001 8 8 AUS20010672 120010628G57537337515505 PIN BOEING767 767204 NM GE CF6 CF680A 30025NE TE FLAPS MISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLAP BYPASS VALVE ROTARY ACTUATOR PIN MIGRATED OUT OF POSITIONLEVER. 2L72 4F4 FRTA1NM E13NE 20010807001802001080700180SW 2001 8 7 AUS20010673 120010621G28411820002 INDICATOR GULSTM500 500B 0141106SW LYC O540 IO540E1B5 41532EA HARTZLHCA3V HCA3VK4 GL FUEL QUANTITY INFAILED W K NONE I FLT. ATTITUDE INST. CRCRUISE 1 AUS 1 (AUS) TRIPLE GAUGE FAILED AND FILLED WITH FUEL. 1H72 3O3 O 6A1 1E4 5 CP6EA 20010807001812001080700181CE 2001 8 7 AUS20010674 120010619G321351411021 BARREL CESSNA402 402C 207590RCE MAIN LANDING GEACRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR LOWER TORQUE LINK ATTACHMENT LUGS CRACKED.FOUND DURING FLUORESCENT MAGNETIC PARTICLE INSPECTION IAW MEB 89-2R1. LOWER ATTACHMENT LUGS ARE NOT CALLED FOR IN THISINSPECTION. 1L72 3O A7CE 20010808003472001080800347EU 2001 8 8 AUS20010675 120010628G6220206010102121 GRIP BELL AGUSTA206AGS206AAGUSTA 0260301EU ALLSN 250C 250C20B 03013GL MAIN ROTOR HEAD DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS 583 GDLM11933 (AUS) MAIN ROTOR GRIP BLADE BOLT BORES DAMAGED. INVESTIGATION FOUND THAT THE MAIN ROTOR BLADE BUFFER PAD WAS DISLODGED DURING BLADE INSTALLATION. THE BLADE BOLT WAS FORCED IN CAUSING THE EDGE OFTHE BUFFER PAD INTO THE BLADE BOLT HOLE. DAMAGE CAUSED TO BLADE BOLT PNO 206-010-152-003 AND MAIN ROTOR BLADE PNO 206-010-200-033. PERSONNEL/MAINTENANCE ERROR. 1G71 3U3 U EXPA1G71E4CE 20010808003502001080800350NM 2001 8 8 AUS20010676 120010630G4920 APU BOEING747 747338 NM RROYCERB211 RB211524D41954555NE APU BAY FIRE W K NONE A FLAME/FIRE ININSP/MAINT 1 AUS (AUS) FOLLOWING APU BATTERY FITMENT AND WHILE INSTALLATION CHECKS WERE CARRIED OUT ON THE THERMAL SWITCH, A FLASH FIRE OCCURRED WHICH SET FIRE TO THE THERMAL BLANKET LOCATED UNDER THE APU BATTERY TRAY AND ALSO CAUSED FLASH BURNS TO MAINTENANCE PERSONNEL. THEFIRE WAS CONTAINED AND QUICKLY EXTINGUISHED. THE FIRE MAY HAVE BEEN CAUSED BY COMBINATION OF AN IGNITION SOURCE FROM A PREVIOUSLY UNDISCOVERED BROKEN/CHAFFED WIRING IN LOOM ADJACENT TO APU BATTERY TRAY AND USE OF AN UNAPPROVED COOLANT SOURCE THAT WAS INFLAMMABLE. 2L72 4F4 FRTA20WE E12EU 20010807001822001080700182CE 2001 8 7 AUS20010677 120010627G5753052390134 FLAP CESSNA182 R182 2072734CE LYC O540 O540J3C5 41532EA MCAULY2D34C B2D34C214 GL TRAILING EDGE FLDAMAGED W K NONE F FLT CONT AFFECTED TOTAKEOFF 1 AUS (AUS) RH TRAILING EDGE FLAP TOP AND BOTTOM SKINS, LEADING EDGE SKIN AND SPAR DAMAGED. INVESTIGATION FOUND THE DAMAGE WAS CAUSED BY THEINBOARD FORWARD FLAP ROLLER JAMMING DUE TO EXCESSIVE WEAR OF THEFLAP TRACK AND ROLLERS. 1H71 3O3 ORT3A13 E295 5 CP7EA 20010807001832001080700183CE 2001 8 7 AUS20010678 120010626G561010132402522 WINDSHIELD BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE MCAULY4HFR344HFR34C754 NE FLIGHT COMPARTMECRACKED W K NONE O OTHER CRCRUISE 1 AUS (AUS) RH WINDSHIELD INNER PANE CRACKED. 1L72 4T4 T A24CE E4EA 6 C3PNE 20010808003522001080800352NE 2001 8 8 AUS20010679 320010629G6114660714255 HUB ROTOL R3904123F SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R390 R3904123F27 NE PROPELLER CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 5054 DRG1268390 (AUS) PROPELLER HUB CRACKED IN AREA AROUND TWO OF THE MOUNT BOLT HOLES. FOUND USING EDDY CURRENT INSPECTION IAW AD/PR/33. 2L72 4T4 TRTA52EU E8NE 6 CP31NE 20010807001842001080700184NM 2001 8 7 AUS20010680 120010701G2750285T004953 FSEU BOEING767 767238 NM PWA JT9 JT9D7R4E 52054NE TRAILING EDGE FLFAULTY W K NONE FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 AUS 6848 (AUS) FLAP/SLAT ELECTRONIC UNIT (FSEU) SUSPECT FAULTY. 2L72 4F4 FRTA1NM E3NE 20010808003532001080800353NM 2001 8 8 AUS20010681 120010621G7603 CABLE RROYCE RB211524D4 BOEING747 747238B 1384828NM RROYCERB211 RB211524D41954555NE POWER LEVER WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE THRUST CONTROL CABLE GUARDS AND COVERS CRACKED/DAMAGED.GUARDS ARE FOR CABLES T1, T2, T3, T4A, T4B, STN940 TO STN960 LT AND RT. CABLE PULLEY FOR CABLE T3A CRACKED AND CABLE T3A WORN AT RT WING INBOARD LOCATION 352.00. FOUND DURING INSPECTION IAW EI 742-076-0005 REV02, CASA AD/B747/299 AND FAA AD 2000-05-30 AMDT 39-11640. AIRCRAFT IS FOREIGN REGISTRATION DQ-FJE. 2L74 4F4 F A20WE E12EU 20010808003542001080800354NM 2001 8 8 AUS20010682 120010626G2530GENM2585015 OVEN BOEING737 737400 NM CFMINTCFM56 CFM563C 13802EU GALLEY FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AUS 19905 (AUS) OVEN C207 CONTAMINATED. WHEN THE OVEN WAS OPERATED A LARGE AMOUNT OF SMOKE WAS GENERATED DUE TO EXCESS OIL IN THE OVEN COMPARTMENT. 2L72 4F4 FRTA16WE E21EU 20010807001852001080700185NE 2001 8 7 AUS20010683 220010704G7260310623101 SHAFT PWA PW123D DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE HAMSTD14SF 14SF23 NE TURBINE ENGINE ASHEARED W K NONE O OTHER ININSP/MAINT 1 AUS 123308 (AUS) NO2 ENGINE ACCESSORY GEARBOX TOWER SHAFT SHEARED AT THE MATINGPOINT WITH GEAR CAUSING THE SHEARED STUB TO JAM BETWEEN THE DRIVESHAFT BEVEL GEARS. SUSPECT CAUSED BY INCORRECT ASSEMBLYPROCEDURE DURING PRODUCTION. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010808003552001080800355GL 2001 8 8 AUS20010684 120010530G5710 STRUCTURE AMTR MK1 MK1 05620JYGL WING DELAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) INTERNAL DELAMINATION OF WING/FUEL TANK. SEVERE FUEL LEAKAGE. THE AIRCRAFT IS A HOMEBUILT AND IT IS SUSPECTED THAT INCORRECTTECHNIQUES WERE USED IN THE CONSTRUCTION. 1H71 3O NCEXPA1H71 20010808003562001080800356SO 2001 8 8 AUS20010685 220010621G8530654961 CYLINDER CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL ENGINE LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 2 CYLINDER LEAKING PAST EXHAUST VALVE AND PISTON RINGS. 1H71 3O3 O A4CE E5CE 5 CP21EA 20010807001862001080700186CE 2001 8 7 AUS20010686 120010622G37101H59 VALVE AIRBORNE 1H59 CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C87 GL VACUUM DISTRIBUTFAULTY W K NONE I FLT. ATTITUDE INST. CRCRUISE 1 AUS 8A (AUS) RH VACUUM SYSTEM MANIFOLD CHECK VALVE FAULTY. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010808003572001080800357SO 2001 8 8 AUS20010687 120010704G24321406902 LEAD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL BATTERY/CHARGER FRACTURED W O OTHER H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 AUS (AUS) BATTERY POSITIVE LEAD LOCATED INSIDE THE BATTERY BOX FRACTURED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010808003622001080800362EA 2001 8 8 AUS20010688 220010617G8530LW12966 CYLINDER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE FAILED W A UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 AUS 1677 (AUS) ENGINE CYLINDER HEAD SEPARATED FROM BARREL IN THREADED AREA. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010808003632001080800363EA 2001 8 8 AUS20010689 220010622G8530LW13532 CYLINDER GULSTM500 500S 0141107SW LYC O540 IO540E1B5 41532EA HARTZLHCC3Y HCC3YR2 NE ENGINE DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS 632 (AUS) ENGINE CYLINDER HOLED IN AREA ADJACENT TO TOP SPARK PLUG HOLE. 1H72 3O3 O 6A1 1E4 5 CP25EA 20010808003642001080800364 2001 8 8 AUS20010690 420010702G341818617 DETECTOR REIMS 406 F406 EU PWA PT6 PT6A112 52043NE MCAULY3G34C73GFR34C701 GL STALL WARNING FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LIFT DETECTOR FAULTY. INVESTIGATION FOUND THAT THE AIRCRAFT WIRING (WIRE NO A2K4S-20P3) HAD BEEN CUT APPROXIMATELY 76.2MM (3IN) UP FROM THE FORWARD SIDE CONSOLE CONNECTOR AND CONNECTED TO THE STALL WARNING HORN. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED MODIFICATION. 1L72 3T3 TRTA54EU E4EA 5 CP60GL 20010808003652001080800365NE 2001 8 8 AUS20010691 220010707G7200200304004 ENGINE BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 2 MALFUNCTIONED W O OTHER EK VIBRATION/BUFFET FLUID LOSS DEDESCENT 1 AUS (AUS) NR 2 ENGINE HAD NO OIL PRESSURE. LIMITED INFORMATION PROVIDED. 2H74 4F4 FRTA49EU E6NE 20010808003662001080800366SW 2001 8 8 AUS20010692 120010706G32102751540003 PIN SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UA 01514WP MCAULY4HFR344HFR34C652 NE LANDING GEAR SHEARED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH MAIN LANDING GEAR UPPER TORQUE LINK PIN SHEARED. 2L72 4T4 TRTA5SW E4WE 6 C3PNE 20010807001872001080700187CE 2001 8 7 AUS20010693 120010709G76025038901019 CABLE CONT IO470L BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO MCAULY2AF34C2AF34C55 GL MIXTURE CONTROL FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH ENGINE MIXTURE CUTOFF CONTROL CABLE WORN AND BROKEN AT A POINT 190MM (7.48IN) FROM THE ENGINE END ATTACHMENT BEARING. 1L72 3O3 ORT3A16 3E1 5 CP5EA 20010808003672001080800367WP 2001 8 8 AUS20010694 220010630G7210310703710 GEAR SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C652 NE GEARBOX WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE SUN/BULL GEAR TEETH AND CORRESPONDING HIGH SPEED PINIONGEARSHAFT TEETH WORN. FOUND DURING ENGINE DISASSEMBLY FOLLOWING SOAP ANALYSIS WHICH SHOWED CARBON STEEL FINES. SERVICE BULLETIN A72-2062 HAD NOT BEEN COMPLIED WITH. 2L72 4T4 TRTA5SW E4WE 6 C3PNE 20010808003682001080800368 2001 8 8 AUS20010695 420010624G34141013840743 INDICATOR BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA HARTZLHCB3T HCB3TN3 GL COCKPIT OUT OF ADJ W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AIRSPEED INDICATOR READING 5 KNOTS OUT OVER THE ENTIRE RANGE. FOUND DURING INSPECTION IAW AD/INST/9 AMDT5. 1L72 4T4 T A24CE E4EA 6 CP15EA 20010808003692001080800369EU 2001 8 8 AUS20010696 120010703G78104606AC CLAMP ALLSN 250C20B AGUSTA206AGS206AAGUSTA 0260301EU ALLSN 250C 250C20B 03013GL ENGINE COLLECTORCRACKED W K NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 AUS (AUS) ENGINE EXHAUST STACK CLAMP LOOSE DUE TO A FRACTURE ORIGINATINGFROM THE ATTACHMENT LUG SECURING RIVET. COWLING DISCOLOURED AND BURNT. 1G71 3U3 U EXPA1G71E4CE 20010808003702001080800370EU 2001 8 8 AUS20010697 120010627G71209448121409 MOUNT PILATSPC12 PC12 7090550EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL ENGINE SEPARATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE SHOCK MOUNT RUBBERS SEPARATED FROM METAL BACKING ALLOWINGENGINE TO SLUMP. SUSPECT MANUFACTURING FAULT. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010807001882001080700188SO 2001 8 7 AUS20010698 220010626G8530 PISTON RING CONT IO520F CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL RECIPROCATING ENWORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NO3 CYLINDER PISTON RINGS WORN AND LEAKING. 1H71 3O3 O A4CE E5CE 5 CP47GL 20010808003712001080800371CE 2001 8 8 AUS20010699 120010705G2797 WIRE CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL FLIGHT CONTROLS BROKEN W O OTHER F FLT CONT AFFECTED LDLANDING 1 AUS (AUS) FLAP SELECTOR LOOM WIRE BROKEN FROM CRIMP TO FLAP MICROSWITCH. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20010807001892001080700189SO 2001 8 7 AUS20010700 120010705G28408004804 HOSE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL FUEL INDICATING LEAKING W K NONE OK OTHER FLUID LOSS ININSP/MAINT 1 AUS (AUS) FUEL PRESSURE HOSE TO FUEL FLOW GAUGE LEAKING UNDER PRESSURE. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010808003722001080800372NM 2001 8 8 AUS20010701 120010704G552085520271003 STOP DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE HAMSTD14SF 14SF23 NE ELEVATOR DETERIORATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELEVATOR BUMPER RUBBER DETERIORATED AND PERISHED. FOUND DURINGINSPECTION IAW AD/DHC-8/078. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010808003732001080800373EU 2001 8 8 AUS20010702 120010601G2130 CONTROLLER FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU CABIN PRESSURE ERRATIC W O OTHER O OTHER CLCLIMB 1 AUS (AUS) PRESSURISATION SYSTEM ERRATIC IN OPERATION. INVESTIGATION FOUND THAT THE AIR FILTER AND VENTURI LINES WERE TRANSPOSED AT THE PRESSURISATION CONTROLLER CONNECTIONS. PERSONNEL/MAINTENANCEERROR. 2L72 4F4 FRTA20EU E2EU 20010807001902001080700190EU 2001 8 7 AUS20010703 120010601G2910 PIPE FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU HYDRAULIC SYSTEMLEAKING W K NONE OK OTHER FLUID LOSS ININSP/MAINT 1 AUS (AUS) UTILITY HYDRAULIC SYSTEM SUCTION PIPE CONTAINED A PIN HOLE LEAK.LOSS OF HYDRAULIC FLUID. 2L72 4F4 FRTA20EU E2EU 20010807001912001080700191EU 2001 8 7 AUS20010704 120010601G3234 LEVER FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU LANDING GEAR SELSTUCK W K NONE O OTHER TOTAKEOFF 1 AUS (AUS) LANDING GEAR LEVER OBSTRUCTED IN DOWN POSITION. 2L72 4F4 FRTA20EU E2EU 20010807001922001080700192EU 2001 8 7 AUS20010705 120010527G3610 DUCT FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU PNEUMATIC DISTRIMISALIGNED W K NONE J WARNING INDICATION CLCLIMB 1 AUS (AUS) LH BLEED AIR SYSTEM LEAKING AT ENGINE HP OUTLET CHECK VALVE DUCT. INVESTIGATION FOUND THE DUCT MATING SURFACES TO BE BADLY ALIGNED. 2L72 4F4 FRTA20EU E2EU 20010808003742001080800374 2001 8 8 AUS20010706 420010625G2565 CABLE BOEING737 737377 NM CFMINTCFM56 CFM565B4 NE ESCAPE SLIDE FRAYED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FORWARD GALLEY DOOR ESCAPE SLIDE RELEASE CABLE FRAYED. FOUNDDURING INSPECTION IAW AD/B737/042. 2L72 4F4 FRTA16WE E38NE 20010807001932001080700193NE 2001 8 7 AUS20010707 220010509G72509234M22G07 SUPPORT GE CF680A BOEING767 767277 NM GE CF6 CF680A 30025NE TURBINE SECTION CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE FIRST STAGE HPT INNER NOZZLE SUPPORT CRACKED. TURBINEDAMAGE AND METAL IN TAILPIPE. 2L72 4F4 FRTA1NM E13NE 20010808003752001080800375EU 2001 8 8 AUS20010708 120010707G3260 SWITCH STBROSSD3 SD360 8100606EU PWA PT6 PT6A67R 52043NE HARTZLHCA6A HCA6A3 NE LANDING GEAR OUT OF ADJ W O OTHER N FALSE WARNING LDLANDING 1 AUS (AUS) NOSE LANDING GEAR MICROSWITCH OUT OF ADJUSTMENT. 2H72 4T4 T A41EU E26NE 6 CP14NE 20010808003762001080800376NM 2001 8 8 AUS20010709 120010701G2540 VALVE BOEING737 737377 NM CFMINTCFM56 CFM565B4 NE LAVATORIES BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FORWARD TOILET DRAIN VALVE POPPET BROKEN. INNER POPPET WASMISSING. 2L72 4F4 FRTA16WE E38NE 20010808003772001080800377NM 2001 8 8 AUS20010710 120010706G2910AS154A06NN0336T HOSE BOEING737 737377 NM CFMINTCFM56 CFM563B2 13802EU HYDRAULIC SYSTEMRUPTURED W K NONE K FLUID LOSS NRNOT REPORTED 1 AUS (AUS) NOSE LANDING GEAR EXTENSION FLEXIBLE HOSE RUPTURED. LOSS OF SYSTEM A' HYDRAULIC FLUID. 2L72 4F4 FRTA16WE E21EU 20010808003782001080800378EU 2001 8 8 AUS20010711 120010627G5610 WINDSHIELD AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CRCRUISE 1 AUS (AUS) FRONT LH WINDSHIELD CRACKED FOLLOWING FAILURE OF WINDSHIELD HEATING. 2L72 4F4 FRTA46NM E29NE 20010809000032001080900003EU 2001 8 9 AUS20010712 120010703G5415 BOLT BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE PYLON CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) WING/PYLON BOLT CORRODED UNDER HEAD. FOUND DURING INSPECTION IAWER BA6-54-40-4. 2H74 4F4 FRTA49EU E6NE 20010809000042001080900004 2001 8 9 AUS20010713 420010614G2210 AUTOPILOT SYS BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE COCKPIT FAULTY W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 AUS (AUS) AUTOPILOT FAULTY. 2H74 4F4 F A49EU E6NE 20010809000052001080900005EU 2001 8 9 AUS20010714 120010704G5415 BOLT BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE NACELLE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) WING/PYLON BOLTS (3OFF) CORRODED UNDER THE HEAD AND ON THE BOLT SHANK. FOUND DURING INSPECTION IAW ER BA6-54-40-4 REV E. 2H74 4F4 FRTA49EU E6NE 20010807001942001080700194SO 2001 8 7 AUS20010716 220010703G8530654004 EXHAUST VALVE CONT O200A CESSNA150 150L 2071826CE CONT O200 O200A 17020SO MCAULY1A102 1A102OCM GL RECIPROCATING ENERODED W K NONE O OTHER ININSP/MAINT 1 AUS 205622 (AUS) ALL ENGINE EXHAUST VALVES EXHIBITED SEVERE EROSION BETWEEN THEVALVE STEM AND VALVE HEAD. 1H71 3O3 O 3A19 E252 5 NP918 20010807001952001080700195EA 2001 8 7 AUS20010717 220010613G8520L801776 CRANKCASE LYC O320H2AD CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA MCAULY1C160 1C160DTM GL RECIPROCATING ENFAULTY W K NONE O OTHER ININSP/MAINT 1 AUS L801776 (AUS) CRANKCASE INCORRECTLY LINE BORED REDUCING DECK HEIGHT BY 1.016MM(0.040IN). THIS ALLOWED NO3 PISTON TO CONTACT THE CYLINDER HEAD.METAL CONTAMINATION OF ENGINE. PERSONNEL/MAINTENANCE ERROR. 1H71 3O3 ONT3A12 E274 5 NP910 20010809000062001080900006NE 2001 8 9 AUS20010718 220010708G7321FFR105MK2S REGULATOR RROYCE RB211524D4 BOEING747 747338 NM RROYCERB211 RB211524D41954555NE FUEL CONTROL FAULTY W A UNSCHED LANDING ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AUS 9145 B1734 (AUS) NO2 ENGINE FUEL FLOW REGULATOR FAULTY. 2L72 4F4 FRTA20WE E12EU 20010809000072001080900007NM 2001 8 9 AUS20010719 120010710G3242S160T400510 BRAKE MESSIER MAINWHEEL BOEING767 767338 1385151NM GE CF6 CF680C2* GL NR 2 FIRE W D RETURN TO BLOCK A FLAME/FIRE TXTAXI/GRND HDL 1 AUS 2667 QF15175 (AUS) NR 2 RT BRAKE FIRE. FIRE SELF-EXTINGUISHED. 2L72 4F4 FRTA1NM E23EA 20010807001962001080700196EA 2001 8 7 AUS20010720 220010703G732125244405 FCU BENDIX DPF2 DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA HARTZLHCB3T HCB3TN3 GL FUEL CONTROL/TURFAULTY W K NONE E VIBRATION/BUFFET DEDESCENT 1 AUS A48954 (AUS) FUEL CONTROL UNIT FAULTY. INVESTIGATION FOUND THE PY RESTRICTOR PARTIALLY BLOCKED BY SUSPECTED PAINT FLAKES. 1H72 3T4 TRTA9EA E4EA 6 CP15EA 20010807001972001080700197CE 2001 8 7 AUS20010721 120010702G3710 HOSE CESSNA210 210R 2073458CE CONT O520 IO520L 17032SO MCAULY3AF32C3AF32C87 GL VACUUM DISTRIBUTDETERIORATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) INSTRUMENT VACUUM HOSES LOCATED BEHIND THE INSTRUMENT PANEL DETERIORATED. HOSES ARE BRANDED IMPERIAL EASTMAN REDI-SEAL. 1H71 3O3 ORT3A21 E5CE 5 CP22EA 20010809000092001080900009NM 2001 8 9 AUS20010722 120010706G3040 HEATER 8SC004301 DHAV DHC8 DHC8106 NM PWA PW121 PW121 52124NE HAMSTD14SF 14SF7 NE WINDSHIELD FAULTY W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AUS (AUS) LT WINDSHIELD HEATING TERMINAL BLOCK OVERHEATING. NO EVIDENCE OFHEAT DAMAGE TO THE WINDSHIELD. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010809000102001080900010 2001 8 9 AUS20010723 420010711G34604081600930 DISPLAY BOEING737 737724 NM CFMINTCFM56 CFM565A1 NE FMC FAULTY W A UNSCHED LANDING O OTHER CRCRUISE 1 AUS (AUS) NR 1 DISPLAY ELECTRONIC UNIT (DEU) FAULTY. 2L72 4F4 FRTA16WE E29NE 20010807001982001080700198GL 2001 8 7 AUS20010724 120010525G6220281432015 BEARING ENSTRMF28 280C 3300505GL LYC O360 HIO360E1AD 41514EA MAIN ROTOR HEAD FAILED W K NONE F FLT CONT AFFECTED TOTAKEOFF 1 AUS (AUS) MAIN ROTOR HEAD LAMIFLEX BEARING FAILED. SUSPECT CAUSED BY GREASE CONTAMINATION. 1G71 3O3 O H1CE 1E10 20010807001992001080700199EA 2001 8 7 AUS20010725 220010624G8520 BOLT LYC IO540K1G5 PIPER PA32 PA32R301 7103218SO LYC O540 IO540K1G5 41532EA HARTZLHCC2Y HCC2YK1 GL RECIPROCATING ENFAILED W K NONE ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS DEDESCENT 1 AUS (AUS) CYLINDER HOLDDOWN BOLTS FAILED. 1L71 3O3 O A3SO 1E4 5 CP920 20010807002002001080700200SO 2001 8 7 AUS20010726 120010706G324293956 PLATE EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE BRAKE WORN W K NONE O OTHER ININSP/MAINT 1 AUS 0480 (AUS) LH OUTBOARD BRAKE WORN TO LIMITS. STRIP INSPECTION FOUND THAT WEAR PLATES HAD SPREAD PAST THE OUTER DIAMETER OF THE BRAKE PLATES AND CONTACTED THE WHEEL PNO 3-1544. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010809000112001080900011NE 2001 8 9 AUS20010727 220010710G7200 ENGINE BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 3 FAILED W A UNSCHED LANDING KEJFLUID LOSS VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 AUS (AUS) NR 3 ENGINE OIL PRESSURE LOSS. 2H74 4F4 FRTA49EU E6NE 20010809000132001080900013NM 2001 8 9 AUS20010728 120010711G3242S160T400510 BRAKE BOEING767 767338 1385151NM GE CF6 CF680C2* GL NR 3 MLG LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS 2907 (AUS) NR 3 MAIN LANDING GEAR BRAKE LEAKING. FURTHER INVESTIGATION SHOWED EVIDENCE OF DISINTEGRATION OF THE REAR STATOR. 2L72 4F4 FRTA1NM E23EA 20010809000142001080900014NM 2001 8 9 AUS20010729 120010711G2910K2231 LINE ABEX PUMP BOEING737 737724 NM CFMINTCFM56 CFM565A1 NE HYDRAULIC SYSTEMDISCONNECTED W K NONE O OTHER ININSP/MAINT 1 AUS K2231 (AUS) HYDRAULIC SUPPLY LINE FOUND DISCONNECTED. SUSPECT LINE NOTRECONNECTED FOLLOWING MAINTENANCE. SYSTEM A' HYDRAULIC PUMP INTERNAL FAILURE DUE TO LACK OF FLUID. PERSONNEL/MAINTENANCE ERROR. 2L72 4F4 FRTA16WE E29NE 20010809000162001080900016NE 2001 8 9 AUS20010731 220010712G72000292005250 ENGINE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE NACELLE FAILED W A UNSCHED LANDING ETJVIBRATION/BUFFET ENGINE CASE PENETRATION WARNING INDICATION CRCRUISE 1 AUS (AUS) ENGINE SUFFERED SEVERE INTERNAL FAILURE. COMPRESSOR AND TURBINE SEIZED. GAS GENERATOR AND POWER TURBINE BLADES BADLY DAMAGED. EXTERNAL DAMAGE ALSO EVIDENT. 1G72 3U3 UNCH1NE E19EU 20010809000172001080900017SW 2001 8 9 AUS20010732 120010309G612086913019 BETA SWITCH HARTZL HCB3TN5 SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE331* 01514WP HARTZLHCB3T HCB3TN5 GL PROPELLER FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PROPELLER BETA SWITCH FAULTY. 2L72 4T3 TRTA8SW E2WE 6 CP15EA 20010809000192001080900019WP 2001 8 9 AUS20010733 220010705G72613199741 VALVE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE3313UW 01514WP HARTZLHCB3T HCB3TN5 GL ENGINE STUCK W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) OIL VENT VALVE STUCK OPEN. 2L72 4T4 TRTA8SW E4WE 6 CP15EA 20010807002012001080700201EU 2001 8 7 AUS20010734 120010622G2710 CONTROL CABLE REIMS 406 F406 7535723EU PWA PT6 PT6A112 52043NE MCAULY3G34C73GFR34C701 GL AILERON CONTROL WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH AND RH AILERON CABLES (4OFF) LOCATED IN WING WORN. 1L72 3T3 TRTA54EU E4EA 5 CP60GL 20010809000202001080900020NM 2001 8 9 AUS20010735 120010715G7714 WIRE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE ENGINE INDICATORFAULTY W D RETURN TO BLOCK EN VIBRATION/BUFFET FALSE WARNING TXTAXI/GRND HDL 1 AUS 35105 (AUS) NR 1 ENGINE ITT GAUGE FLUCTUATING. SUSPECT WIRING PROBLEM. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010809000252001080900025 2001 8 9 AUS20010736 420010711G256563800103 LIFE RAFT CABIN MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS 10392 (AUS) DURING SERVICING OF LIFERAFT IT WAS FOUND THAT THE PACKING STRAP WAS STILL IN PLACE AROUND THE CIRCUMFERENCE OF THE RAFT. STRAP WOULD PROBABLY PREVENTED CORRECT DEPLOYMENT. LIFERAFT HAD BEEN IN SERVICE FOR APPROXIMATELY THREE YEARS. PERSONNEL/MAINTENANCEERROR. 20010807002022001080700202SO 2001 8 7 AUS20010737 220010714G74141051676 CAPACITOR BENDIX 107902016 CESSNA337 T337G 2075726CE CONT O360 TSIO360C 17025SO MCAULY2AF34CD2AF34C303 GL MAGNETO/DISTRIBUUNSERVICEABLE W K NONE O OTHER ININSP/MAINT 1 AUS A98935 (AUS) MAGNETO CAPACITOR FAULTY. CAPACITOR LEAD LOOSE. 1H72 3O3 O A6CE E9CE 5 CP5EA 20010809000272001080900027NE 2001 8 9 AUS20010738 220010712G732312664 GOVERNOR BOEING747 747338 NM RROYCERB211 RB211524D41954555NE NR 2 ENGINE FAULTY W D RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 AUS (AUS) NR 2 ENGINE RPM DECREASED AND EGT INCREASED. VIGV AIR FLOW CONTROL UNIT PNO 754-1-32148-019A AND PUMP AND GOVERNOR UNIT (PAG) PNOPAC102MK4S CHANGED. 2L72 4F4 FRTA20WE E12EU 20010809000292001080900029NE 2001 8 9 AUS20010739 220010712G72601765MK1 HOUSING BOEING747 747438 NM RROYCERB211 RB211524G19 NE GENERATOR FAILED W A UNSCHED LANDING EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) NR 4 ENGINE DEDICATED GENERATOR DAMAGED AND ADRIFT FROM ADAPTER GEARBOX. LOSS OF ENGINE OIL. 2L74 4F4 FRTA20WE E30NE 20010809000302001080900030EU 2001 8 9 AUS20010740 120010716G3040S2653010 CIRCUIT BREAKER BAC 146 146100A 1500260EU LYC ALF502ALF502R3A 41580NE WINDSHIELD HEAT FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 AUS (AUS) LT A' SCREEN HEAT CIRCUIT BREAKER FAULTY. INVESTIGATION FOUND THE CIRCUIT BREAKER BURNED OUT ON A' PHASE. 2H74 4F4 FRTA49EU E6NE 20010807002032001080700203NM 2001 8 7 AUS20010741 120010716G2520 SEAT BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU PASSENGER COMPARLOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PASSENGER SEAT 10ABC LOOSE IN TRACKS. 2L72 4F4 FRTA16WE E21EU 20010809000322001080900032NM 2001 8 9 AUS20010742 120010716G5330149T76086 PANEL BOEING767 767338 1385151NM GE CF6 CF680C2* GL FUSELAGE SEPARATED W O OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 AUS (AUS) ADP ACCESS PANEL/DOOR 195SL MISSING. DAMAGE TO FUSELAGE PANELS195LL, 195QL AND 195NL. 2L72 4F4 FRTA1NM E23EA 20010807002042001080700204SO 2001 8 7 AUS20010743 120010519G321379543002 BOLT PIPER PA32 PA32260 7103206SO LYC O540 O540E4B5 41532EA HARTZLHCC2Y HCC2YK1 GL MAIN LANDING GEAFAILED W K NONE O OTHER LDLANDING 1 AUS (AUS) LH MAIN LANDING GEARLOWER LEG SEPARATED FROM UPPER LEG. SUSPECT CAUSED BY FAILURE OF THE CENTRE TORQUE LINK BOLT. LOWER LEG HOLED LH FLAP DURING SEPARATION. 1L71 3O3 O A3SO E295 5 CP920 20010809000332001080900033EA 2001 8 9 AUS20010744 120010712G5610NP1393225 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER DEDESCENT 1 AUS 99343H5435 (AUS) LT PILOTS SIDE WINDSHIELD INNER PLY CRACKED DIAGONALLY FROM THE FORWARD LOWER CORNER. 2L72 4F4 FRTA21EA E15NE 20010809000342001080900034NM 2001 8 9 AUS20010745 120010716G575369577055 FAIRING BOEING737 737400 NM CFMINTCFM56 CFM565A1 NE TE FLAPS BROKEN W O OTHER F FLT CONT AFFECTED DEDESCENT 1 AUS (AUS) NR 3 TRAILING EDGE FLAP CANOE/FAIRING ASSEMBLY INBOARD END DOORPOSITION DATA BROKEN OFF AND JAMMING FLAP. 2L72 4F4 FRTA16WE E29NE 20010809000362001080900036CE 2001 8 9 AUS20010746 120010713G324616110900 WHEEL CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL MLG WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR WHEEL INNER HALF WORN IN BEARING BORE. BEARING SPINNING IN HUB. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20010809000372001080900037NM 2001 8 9 AUS20010747 120010717G3520117003 GENERATOR BOEING767 767277 NM GE CF6 CF680A 30025NE PASSENGER OXYGENMISINSTALLED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) OXYGEN GENERATORS LOCATED AT SEATS 24AB, 25AB, 27AB AND 30FG HADTHE RELEASE PINS INCORRECTLY INSTALLED. 2L72 4F4 FRTA1NM E13NE 20010807002052001080700205CE 2001 8 7 AUS20010748 120010717G55210532001103 RIB CESSNA172 172G 2072420CE CONT O300 O300C 17022SO MCAULY1C172 1C172EM GL ELEVATOR, SPAR/RCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS 8881 (AUS) ELEVATOR END RIB EXTENSIVELY CORRODED. 1H71 3O3 ONT3A12 E253 5 NP910 20010809000382001080900038SO 2001 8 9 AUS20010749 120010711G3260MS3126E106P CONNECTOR EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE LANDING GEAR SHORTED W O OTHER O OTHER NRNOT REPORTED 1 AUS (AUS) RT LANDING GEAR AIR/GROUND PROXIMITY SENSOR ELECTRICAL CONNECTORMOISTURE CONTAMINATION AND SHORT CIRCUIT. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010809000392001080900039SO 2001 8 9 AUS20010750 120010713G3260XAIN103 RELAY EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE LANDING GEAR FAULTY W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) GROUND/FLIGHT RELAY BOX RELAY K0290 FAULTY. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010807002062001080700206NE 2001 8 7 AUS20010751 220010717G73217863911028 HMU PWA PW120A DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE FUEL CONTROL/TURUNSERVICEABLE W K NONE E VIBRATION/BUFFET CLCLIMB 1 AUS 2034 F26904 (AUS) RH ENGINE HYDRO MECHANICAL UNIT (HMU) FAULTY. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010809000402001080900040NM 2001 8 9 AUS20010752 120010718G28226072101 PUMP BOEING747 747438 NM RROYCERB211 RB211524G19 NE FUEL SYSTEM MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) TRANSFER PUMP CONNECTORS INCORRECTLY WIRED. THE PUMPS HAD WIRINGSWAPPED AT PIN 2 AND PIN 3. THE WIRES WERE RECONNECTED IN THE BELIEF THAT THE WIRING CONFIGURATION WAS INCORRECT. THE AIRCRAFTHAD BEEN SUPPLIED WITH THE WIRING IN A NON-STANDARD FORMAT. INVESTIGATION FOUND THAT SOME AIRCRAFT HAD BEEN WIRED DIFFERENTLY AT MANUFACTURE. THIS WIRING CHANGE WAS NOT INCORPORATED IN THESERVICE BULLETIN. 2L74 4F4 FRTA20WE E30NE 20010809000412001080900041NM 2001 8 9 AUS20010753 120010717G28226072101 PUMP BOEING747 747438 NM RROYCERB211 RB211524G19 NE FUEL SYSTEM MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 AUS 210 (AUS) HORIZONTAL STABILISER FUEL TANK RT TRANSFER / JETTISON PUMP WIRINGCONNECTIONS AT PIN 2 AND PIN 3 REVERSED AT PUMP CONNECTOR PLUGDM7863. WIRING WAS CORRECT AS PER WIRING DIAGRAM BUT INCORRECT AS PER BSB 747-28-2217 FIG10. INVESTIGATION FOUND THAT SOME AIRCRAFT HAD BEEN WIRED DIFFERENTLY AT MANUFACTURE. THIS WIRING CHANGE WAS NOT INCORPORATED IN THE SERVICE BULLETIN. 2L74 4F4 FRTA20WE E30NE 20010809000422001080900042 2001 8 9 AUS20010754 420010706G6122B41832 FLYWEIGHT HARTZL F624L PROP GOVERNOR BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS B1798T (AUS) ENGINE CONSTANT SPEED UNIT FLYWEIGHT ASSEMBLY BROKEN. 20010807002072001080700207CE 2001 8 7 AUS20010755 120010705G55511016200191 FITTING BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA HARTZLHCB3T HCB3TN3 GL HORIZONTAL STABICORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HORIZONTAL STABILISER AFT UPPER FITTING CONTAINED SEVEREINTERGRANNULAR CORROSION. NDI CARRIED OUT ON FITTING FOLLOWINGREMOVAL FOUND THREE CRACKS BETWEEN THE BOLT HOLES. 1L72 4T4 T A24CE E4EA 6 CP15EA 20010809000482001080900048CE 2001 8 9 AUS20010756 120010710G32301068100111 UPLOCK CABLE 358150722 BEECH 58 58 1152740CE CONT O520 IO520C 17032SO HARTZLHCJ3Y PHCJ3YF2 GL LANDING GEAR LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR DOWNLOCK CABLE LOOSE. FURTHER INVESTIGATION FOUND THAT THE UPLOCK BLOCK HAD BEEN CONTACTED BY THE UPLOCK ROLLER AND HAD BEEN MOVED OUT OF POSITION. UPLOCK CABLE RETAINING NUTS HAD TORN THROUGH NR 1 WING RIB. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20010809000502001080900050CE 2001 8 9 AUS20010757 120010710G323035810142 SHAFT BEECH 58 58 1152740CE CONT O520 IO520C 17032SO HARTZLHCJ3Y PHCJ3YF2 GL LANDING GEAR MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) LANDING GEAR ACTUATOR MANUAL EXTENSION HANDLE SHAFT INSTALLED 120 DEGREES OUT OF POSITION PREVENTING CORRECT OPERATION OF HANDLE. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20010809000522001080900052CE 2001 8 9 AUS20010758 120010710G3242 HOSE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO HARTZLHCJ3Y PHCJ3YF2 GL BRAKE FOULED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) LT AND RT MAIN LANDING GEAR BRAKE LINES FOULING ON LANDING GEAR DOORS DURING RETRACTION. INVESTIGATION FOUND THAT THE BRAKE HOSES WERE APPROXIMATELY 53.975MM (2.125IN) LONGER THAN THOSE FITTED TO SIMILAR AIRCRAFT. IN ADDITION THE BRACKETS PNO 35-815264-1 AND PNO 35-815264-2 WHICH ATTACH THE HOSES TO THE MLG LEGS WERE FITTED TO THE WRONG SIDES. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20010807002082001080700208CE 2001 8 7 AUS20010759 120010705G800008504691 CONTACTOR CONT GTSIO520L CESSNA421 421C 2076016CE CONT O520 GTSIO520L 17032SO MCAULY3FF32 3FF32C501 GL ENGINE STARTING STUCK W K NONE EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS (AUS) LH ENGINE STARTER CONTACTOR STUCK CLOSED. LH ALTERNATOR DAMAGED.STARTER MOTOR TERMINAL POST DAMAGED. 1L72 3O3 O A7CE E7CE 5 CP45GL 20010809000552001080900055EU 2001 8 9 AUS20010760 220010714G7200 ENGINE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU LEFT FAULTY W O OTHER J WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) LT ENGINE OIL CONSUMPTION EXCESSIVE AT APPROXIMATELY 0.8 LITRES TO 1 LITRE PER HOUR. 2L72 4F4 FRTA20EU E2EU 20010809000622001080900062NM 2001 8 9 AUS20010761 120010718G262135207900M SQUIB BOEING747 747SP38 NM RROYCERB211 RB211524D41954555NE FIRE BOTTLE WRONG PART W K NONE O OTHER ININSP/MAINT 1 AUS 15092 (AUS) NR 1 MAIN CARGO FIRE EXTINGUISHER BOTTLE FORWARD AND AFT SQUIBSCROSS CONNECTED. 2L74 4F4 FRTA20WE E12EU 20010809000682001080900068GL 2001 8 9 AUS20010762 220010712G726123038160 OIL SYSTEM HUGHES500N 500N 3027374SW ALLSN 25OC 250C20R GL ENGINE BLOCKED W J DUMP FUEL EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 AUS (AUS) NR 6 AND NR 7 BEARING OIL SCAVENGE PORT PARTIALLY BLOCKED BY CARBON DEPOSITS. OIL TYPE HAD BEEN CHANGED FROM MOBIL 254 TO MOBIL 291. 1G71 3U3 UNCH3WE E4CE 20010809000692001080900069NE 2001 8 9 AUS20010763 220010715G7200 ENGINE BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 3 LEAKING W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS (AUS) NR 3 ENGINE HP COMPRESSOR CONTAMINATED WITH OIL. FUMES IN CABIN. 2H74 4F4 FRTA49EU E6NE 20010807002092001080700209SW 2001 8 7 AUS20010764 120010718G6322209062502101 FAN BLADE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ROTORCRAFT COOLIFAILED W K NONE EK VIBRATION/BUFFET FLUID LOSS CRCRUISE 1 AUS (AUS) NO1 ENGINE OIL COOLER BLOWER FAN BLADES SEPARATED FROM HUB. 1G72 4U4 U H4SW E22EA 20010807002102001080700210SW 2001 8 7 AUS20010765 120010608G8120 BEARING PWA R1340AN1 GULSTMG73 G73 3951802SW PWA R1340 R1340AN1 52016NE HAMSTD23D 23D40 NE EXHAUST TURBOCHAFAILED W K NONE E VIBRATION/BUFFET TXTAXI/GRND HDL 1 AUS 1159 (AUS) RH ENGINE FAILED. CAUSED BY FAILURE OF SUPERCHARGER SUPPORT BEARING. 1H72 3R3 R A783 5E2 6 CP719 20010809000712001080900071EU 2001 8 9 AUS20010766 120010719G7700 CONNECTOR BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502* 41580EA INDICATOR LOOSE W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) NR 4 ENGINE VIBRATION HARNESS PLUG LOOSE. 2H74 4F4 FRTA49EU E6NE 20010809000722001080900072NM 2001 8 9 AUS20010767 120010722G3620 PRESSURE SWITCH BOEING767 767338 1385151NM GE CF6 CF680C2* GL PNEUMATIC SYS CONTAMINATED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AUS (AUS) PNEUMATIC SYSTEM OVERPRESSURE SWITCHES CONTAMINATED WITH WATER. 2L72 4F4 FRTA1NM E23EA 20010809000732001080900073NM 2001 8 9 AUS20010768 120010215G2910BACH8AEE0250T HOSE BOEING737 737377 NM CFMINTCFM56 CFM563B2 13802EU HYDRAULIC SYSTEMRUPTURED W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 AUS (AUS) LT MAIN LANDING GEAR ACTUATOR UP HOSE BURST. LOSS OF SYSTEM A' HYDRAULIC FLUID. 2L72 4F4 FRTA16WE E21EU 20010809000742001080900074NM 2001 8 9 AUS20010769 120010705G7112 SHROUD LYC O320B2C ROBSINR22 R22BETA NM LYC O320 O320B2C 41508EA AIR BAFFLE MISINSTALLED W A UNSCHED LANDING EK VIBRATION/BUFFET FLUID LOSS CRCRUISE 1 AUS (AUS) ENGINE TO OIL COOLER WORN AND HOLED BY RUBBING ON CARBURETTOR HEAT SHROUD. 1G71 3O3 O H10WE E274 20010809000752001080900075NE 2001 8 9 AUS20010770 320010724G6114660714259 HUB SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R390 R3904123F27 NE PROPELLER CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 6574 (AUS) PROPELLER HUB SUSPECT CRACKED AROUND THE MOUNTING BOLT HOLE LOCATED AT THE 6.30 POSITION. FOUND DURING EDDY CURRENT INSPECTION IAW AD/PR/33. 2L72 4T4 TRTA52EU E8NE 6 CP31NE 20010807002112001080700211NE 2001 8 7 AUS20010771 220010726G7260 MOUNT LYC ALF502R5 BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE TURBINE ENGINE ADAMAGED W K NONE H ELECT. POWER LOSS-50 PC CRCRUISE 1 AUS (AUS) NO4 INTEGRATED DRIVE GENERATOR (IDG) BROKEN AWAY FROM GEARBOX DUE TO FAILURE OF THE MOUNT. 2H74 4F4 F A49EU E6NE 20010807002122001080700212SO 2001 8 7 AUS20010772 120010721G3260922AA2YA6PZ722 SENSOR EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE LANDING GEAR POSFAULTY W K NONE ON OTHER FALSE WARNING LDLANDING 1 AUS (AUS) LH MAIN LANDING GEAR DOWNLOCK PROXIMITY SENSOR INTERNAL FAULT. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010809000762001080900076EA 2001 8 9 AUS20010773 220010723G73242538993 GASKET LYC IO720A1B LYC O720 IO720A1B 41546EA FUEL DIVIDER FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLOW DIVIDER GASKET FAULTY. NEW ITEM FROM MANUFACTURER. 3 O 1E15 20010807002132001080700213NM 2001 8 7 AUS20010774 120010323G292059855 VALVE SUNDSTRANDEM729550C BOEING767 767277 NM GE CF6 CF680A 30025NE HYDRAULIC SYSTEMCRACKED W K NONE JK WARNING INDICATION FLUID LOSS DEDESCENT 1 AUS 49754 129 (AUS) RAM AIR TURBINE (RAT) MODULE LEAKING DUE TO CRACKED CHECK VALVE. 2L72 4F4 FRTA1NM E13NE 20010809000842001080900084EU 2001 8 9 AUS20010775 120010726G32425008744 DISK 50079961 FOKKERF27 F27MK50 EU PWA PWA120PW125B NE ROTOL R352 R3526123F1 GL BRAKE CRACKED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AUS JAN8761 (AUS) BRAKE ROTATING DISC FAILED. A PART OF THE FAILED DISC PUNCTURED THE WHEEL INNER HALF AND DEFLATED THE TUBE. INVESTIGATION FOUND NO DISCOLOURATION BUT FOUND THAT THE SLOTS HAD SPREAD FLATTENING THE OUTER CIRCUMFERENCE BETWEEN THE DRIVE RECESSES. THE THREE ROTATING DISCS ON THE BRAKE UNIT HAD CRACKS EMINATING FROM THEEXPANSION SLOTS. 2H72 4T4 TRTA817 E20NE 6 CP16NG 20010807002142001080700214NE 2001 8 7 AUS20010776 220010709G7260 MOUNT LYC ALF502R5 BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE TURBINE ENGINE AFAILED W K NONE H ELECT. POWER LOSS-50 PC CRCRUISE 1 AUS (AUS) NO4 CSD MOUNT FAILED. IDG ASSEMBLY SEPARATED FROM GEARBOX. 2H74 4F4 F A49EU E6NE 20010807002152001080700215SO 2001 8 7 AUS20010777 220010725G7310641486 PIPE CONT GTSIO520M CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL ENGINE FUEL DISTFRACTURED W K NONE E VIBRATION/BUFFET CRCRUISE 1 AUS 1012 (AUS) RH ENGINE NO6 CYLINDER FUEL INJECTION LINE NIPPLE BROKEN OFF. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010807002162001080700216CE 2001 8 7 AUS20010778 120010723G781024540250 CLAMP CONT TSIO520P CESSNA210 P210N 2073454CE CONT O520 TSIO520P 17040SO MCAULYD3A34 D3A34C402 GL ENGINE COLLECTORBROKEN W K NONE OEROTHER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS ININSP/MAINT 1 AUS (AUS) ENGINE FORWARD LH EXHAUST CLAMP BROKEN. FORWARD AIRFRAMESTRUCTURE, COWL AND NOSE TYRE TORCHED. 1H71 3O3 O 3A21 E8CE 5 CP47GL 20010809000862001080900086CE 2001 8 9 AUS20010779 120010723G551207326133781 STRUCTURE CESSNA 185 CESSNA185 185 2072802CE CONT O520 IO520D 17032SO MCAULY2A34C D2A34C58 GL HORIZONTAL STAB DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS 1850271 (AUS) HORIZONTAL STABILISER TIP DAMAGED. 1H71 3O3 ONC3A24 E5CE 5 CP3EA 20010809000902001080900090EU 2001 8 9 AUS20010781 120010626G2742MC103 ACTUATOR FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU STABILIZER LEAKING W O OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 AUS 110 (AUS) STABILIZER ACTUATOR LEAKING. LOSS OF HYDRAULIC FLUID. 2L72 4F4 FRTA20EU E2EU 20010807002172001080700217EU 2001 8 7 AUS20010782 120010701G3411 DRAIN VALVE FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU PITOT/STATIC SYSSTUCK W K NONE I FLT. ATTITUDE INST. NRNOT REPORTED 1 AUS (AUS) PITOT STATIC SYSTEM DRAIN LINE VALVE STUCK IN OPEN POSITION. 2L72 4F4 FRTA20EU E2EU 20010807002182001080700218EU 2001 8 7 AUS20010784 120010705G5210 CABLE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU PAX DOOR BROKEN W O OTHER O OTHER NRNOT REPORTED 1 AUS (AUS) PASSENGER DOOR DECLUTCH CABLE TERMINAL END BROKEN. 2L72 4F4 FRTA20EU E2EU 20010807002192001080700219 2001 8 7 AUS20010785 420010715G3460B471ABM3 COMPUTER AIRBUS310 A310304 EU PWA 4152 PW4152 NE FLIGHT MANAGEMENFAULTY W K NONE F FLT CONT AFFECTED TOTAKEOFF 1 AUS 4363 303 (AUS) FLIGHT AUGMENTATION COMPUTER FAULTY. 2L72 4F RTA35EU E24NE 20010809000972001080900097EU 2001 8 9 AUS20010786 120010722G2910296801 REDUCER FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU HYDRAULIC SYSTEMCRACKED W O OTHER K FLUID LOSS NRNOT REPORTED 1 AUS 55929 640 (AUS) LANDING GEAR HYDRAULIC SYSTEM PRESSURE REDUCER CRACKED. LOSS OF HYDRAULIC FLUID. 2L72 4F4 FRTA20EU E2EU 20010809000982001080900098EU 2001 8 9 AUS20010787 120010724G5270 BOSS FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING SYSOUT OF ADJ W O OTHER N FALSE WARNING NRNOT REPORTED 1 AUS (AUS) SERVICE / EMERGENCY DOOR STRIKER BOSS LOOSE AND MISALIGNED. 2L72 4F4 FRTA20EU E2EU 20010807002202001080700220SW 2001 8 7 AUS20010788 120010630G5313206031314125 LONGERON BELL 206L1 BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL FUSELAGE MAIN, LCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 45323 (AUS) FUSELAGE UPPER FORWARD LONGERON CRACKED. 1G71 3U3 U H2SW E1GL 20010807002212001080700221SW 2001 8 7 AUS20010789 120010630G5320206032307031 ANGLE BELL 206L1 BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL FUSELAGE, MISCELCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 45323 (AUS) FUSELAGE ANGLE CRACKED. 1G71 3U3 U H2SW E1GL 20010809000992001080900099NM 2001 8 9 AUS20010790 120010730G2910BACC27AC12121006FITTING BOEING747 747430 1384942NM RROYCERB211 RB211524* NE HYDRAULIC SYSTEMCRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) LTBODY LANDING GEAR RETRACTION ACTUATOR LINE UNION CRACKED AND LEAKING. HYDRAULIC PIPE ALSO LEAKING. 2L74 4F4 FRTA20WE E12EU 20010905001952001090500195SO 2001 9 5 AUS20010791 120010724G2752 CONNECTOR EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE FLAP ACTUATOR CONTAMINATED W K NONE FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 AUS (AUS) RT OUTBOARD FLAP ACTUATOR ELECTRICAL CONNECTOR CONTAMINATED WITH MOISTURE. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010905001962001090500196EU 2001 9 5 AUS20010793 120010710G2913716988 PUMP BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE HYDRAULIC PUMP WORN W K NONE O OTHER ININSP/MAINT 1 AUS 3740 (AUS) ENGINE DRIVEN HYDRAULIC PUMP INTERNAL AND EXTERNAL DRIVE SPLINES WORN EXCESSIVELY. 2H74 4F4 FRTA49EU E6NE 20010905001972001090500197EA 2001 9 5 AUS20010797 220010801G8530LW12933 COLLET LYC O540 IO540K1G5 41532EA CYLINDER INCORRECT W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE CYLINDER KIT PN 05K21102 FAULTY. CYLINDER PN LW012993 CONTAINED ONE CORRECT AND ONE INCORRECT (SMALLER) VALVE RETAINING COLLET FITTED TO THE EXHAUST VALVE. THE INCORRECT COLLET HAD DAMAGED THE VALVE STEM RENDERING IT UNSERVICEABLE. 3 O 1E4 20010905002042001090500204WP 2001 9 5 AUS20010798 220010724G726131032173 PUMP CESSNA441 441 2076020CE GARRTTTPE331TPE331* 01514WP HARTZLHCB3T HCB3TN5 GL OIL SYSTEM CRACKED W K NONE KE FLUID LOSS VIBRATION/BUFFET NRNOT REPORTED 1 AUS 90 (AUS) LT ENGINE OIL PUMP HOUSING CRACKED. 1L72 3T3 TRTA28CE E2WE 6 CP15EA 20010905000542001090500054EU 2001 9 5 AUS20010799 120010725G5344350A25122726 HINGE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1A 60030NE FUSELAGE DOOR HIBROKEN W K NONE D INFLIGHT SEPARATION CRCRUISE 1 AUS (AUS) DOOR HINGE BROKEN. 1G71 3U3 UNCH9EU E19EU 20010905002312001090500231CE 2001 9 5 AUS20010800 120010726G76031317652F ROD END BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE HARTZLHCB3T HCB3TN5 GL POWER LEVER OUT OF ADJ W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) LT ENGINE POWER LEVER CABLE TO POWER INPUT LEVER ROD END OUT OF ADJUSTMENT AND THE LOCKNUT WAS LOOSE. THE ROD END AND LOCKNUT HAD NOT BEEN CORRECTLY INSTALLED FOLLOWING FCU CHANGE.PERSONNEL/MAINTENANCE ERROR. 1L72 4T4 T A24CE E4EA 6 CP15EA 20010905002322001090500232NM 2001 9 5 AUS20010801 120010729G324226056623 ROTOR BOEING747 747338 NM RROYCERB211 RB211524D41954555NE BRAKE FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 13222 (AUS) NR 7 MAIN BODY WHEEL BRAKE ROTOR SEGMENT FAILED. 2L72 4F4 FRTA20WE E12EU 20010913002552001091300255NM 2001 9 13 AUS20010802 120010731G253041610015 COFFEEMAKER BOEING767 767330 NM GALLEY FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS 0632 (AUS) FORWARD GALLEY CENTRE COFFEE MAKER FAULTY. DURING RECTIFICATION OF THE FAULT IT WAS FOUND THAT THE COFFEEMAKER WAS THE INCORRECT PART NUMBER FOR FITMENT TO THIS MODEL AIRCRAFT. UNAPPROVED PART. 2L72 4F RTA1NM 20010905000552001090500055NM 2001 9 5 AUS20010803 120010731G3230273T63041 ACTUATOR BOEING 273T63016 BOEING767 767204 NM GE CF6 CF680A 30025NE LANDING GEAR RETFAULTY W K NONE ON OTHER FALSE WARNING TOTAKEOFF 1 AUS 40536 00164 (AUS) LH MAIN LANDING GEAR FORWARD DRAG BRACE DOWNLOCK ACTUATOR FAULTY. INVESTIGATION FOUND THE ACTUATOR PISTON ROD DETACHED FROM THE ACTUATOR BODY DUE TO FAILURE OF THE PISTON ROD IN THE THREADEDAREA WHICH ENGAGES THE PISTON RETAINING NUT. 2L72 4F4 FRTA1NM E13NE 20010913002612001091300261NE 2001 9 13 AUS20010804 220010726G731040885 CONTROL UNIT BOEING747 747338 NM RROYCERB211 RB211524* NE FUEL DIST LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS 3474 (AUS) NR 4R REFUEL VALVE CONTROL UNIT HOUSING LEAKING. 2L72 4F4 FRTA20WE E12EU 20010913002672001091300267CE 2001 9 13 AUS20010805 120010726G32303581507715 BRACKET BEECH 36 A36 1151604CE LANDING GEAR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR UPLOCK BRACKET CORRODED AT PIVOT POINT. 1L71 3O 3A15 20010913002682001091300268SO 2001 9 13 AUS20010806 120010730G2910 RESERVOIR EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE HYDRAULIC SYSTEMLEAKING W O OTHER K FLUID LOSS NRNOT REPORTED 1 AUS (AUS) LOSS OF FLUID FROM GREEN HYDRAULIC SYSTEM. SUSPECT CAUSED BY INCORRECT BRAKING SEQUENCE. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010913002692001091300269EA 2001 9 13 AUS20010807 220010724G8500L575861A ENGINE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL LEFT FAILED W O OTHER ERFVIBRATION/BUFFET PARTIAL RPM/PWR LOSS FLT CONT AFFECTED CLCLIMB 1 AUS 1041 (AUS) LT ENGINE POWER LOSS AND VIBRATION. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010913002702001091300270SO 2001 9 13 AUS20010808 120010510G2730 BOLT PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ELEVATOR CONTROLUNAPPROVED PART W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELEVATOR PUSHROD BOLTS INCORRECT TYPE AS REQUIRED BY AD/PA31/121AMDT1. UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000562001090500056EA 2001 9 5 AUS20010809 220010428G7310 FILTER LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE FUEL DISTLEAKING W K NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AUS (AUS) RH ENGINE FUEL FILTER SEAL LEAKING. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010913002712001091300271SO 2001 9 13 AUS20010810 120010515G52104225000 HANDLE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL PAX DOOR MISREPAIRED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) CABIN DOOR INNER HANDLE HAD UNAPPROVED REPAIR. HANDLE HAD BEENWELDED IN TWO PLACES. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED REPAIR. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000572001090500057SO 2001 9 5 AUS20010811 120010424G79203999502 HOSE LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE OIL DISTRDETERIORATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE OIL PRESSURE HOSE LOCATED BETWEEN VERNATHERM AND OIL COOLER INCORRECTLY ROUTED CAUSING PREMATURE DETERIORATION DUE TOHEAT DAMAGE. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000582001090500058EA 2001 9 5 AUS20010812 220010419G731074134 FILTER LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE FUEL DISTLEAKING W K NONE OK OTHER FLUID LOSS ININSP/MAINT 1 AUS (AUS) FUEL FILTER LEAKING. FILTER BOWL LOOSE. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000592001090500059EA 2001 9 5 AUS20010813 220010212G731074134 FILTER LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE FUEL DISTLEAKING W K NONE OK OTHER FLUID LOSS ININSP/MAINT 1 AUS (AUS) FUEL FILTER BOWL LEAKING. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010913002722001091300272SO 2001 9 13 AUS20010814 120010419G760324894 CABLE LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL POWER LEVER MISRIGGED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) THROTTLE CABLE INCORRECTLY ASSEMBLED AND RIGGED.PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000602001090500060SO 2001 9 5 AUS20010815 120010329G3230 UPLOCK PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL LANDING GEAR RETSHEARED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH MAIN LANDING GEAR UPLOCK EYE SHEARED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000612001090500061SO 2001 9 5 AUS20010816 120010410G76032489402 CABLE LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL POWER LEVER SEPARATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH ENGINE THROTTLE CABLE SECTIONS LOCKWIRED TOGETHER. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010917001852001091700185SO 2001 9 17 AUS20010817 120010412G760324894 ROD END LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL POWER LEVER WRONG PART W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT ENGINE CONTROL ARM RODEND INCORRECTLY ASSEMBLED ON THE WRONG SIDE OF THE ARM CAUSING LOAD ON THE CABLE BALL END. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000622001090500062SO 2001 9 5 AUS20010818 120010412G79203999505 HOSE LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE OIL DISTRDETERIORATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE OIL COOLER HOSE DETERIORATED DUE TO BEING INCORRECTLYROUTED CLOSE TO TURBOCHARGER. HOSE ALSO HAD EXCESSIVE BENDRADIUS. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000632001090500063SO 2001 9 5 AUS20010819 120010412G7810 EXHAUST PIPE LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE COLLECTORCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE EXHAUST SYSTEM TRANSITIONS HOLED AND CRACKED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010917001872001091700187SO 2001 9 17 AUS20010820 120010412G7810 EXHAUST PIPE LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE COLLECTORMISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) LT TAILPIPE INCORRECTLY FITTED TO TURBOCHARGER CAUSING BURNING OF THE EXHAUST CLAMP. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000642001090500064SO 2001 9 5 AUS20010821 120010412G7810 GASKET LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE COLLECTORMISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH ENGINE TURBOCHARGER EXHAUST TRANSITIONS FITTED WITHOUT A CRUSH GASKET. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000652001090500065EA 2001 9 5 AUS20010823 220010803G731374151 INJECTOR LYC IO540K1B5 BNORM BN2 BN2A20 1520220EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL FUEL INJECTOR NOBLOCKED W K NONE EA VIBRATION/BUFFET FLAME/FIRE LDLANDING 1 AUS (AUS) NO1 ENGINE FUEL INJECTOR NOZZLE PARTIALLY BLOCKED. 1H72 3O3 O A17EU 1E4 5 CP920 20010905000672001090500067CE 2001 9 5 AUS20010825 120010710G571208221757 RIB CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL WING, RIB/BULKHECRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) WING RIBS LOCATED IN LH WHEEL BAY CRACKED AS INDICATED IN CESSNASERVICE LETTER ME76-2. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010905000682001090500068CE 2001 9 5 AUS20010826 120010731G7920111F4176S0220 HOSE LYC O320E2D CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160DTM GL ENGINE OIL DISTRLEAKING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE OIL COOLER HOSE POROUS AND LEAKING IN THE AREA ON THEOUTSIDE OF THE BEND AT THE ENGINE END. FIRE SLEEVINGCONTAMINATED. HOSE MANUFACTURED 30 DECEMBER 1996. 1H71 3O3 ONT3A12 E274 5 NP910 20010905000692001090500069SO 2001 9 5 AUS20010827 120010419G7920 HOSE LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE OIL DISTRDETERIORATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TURBOCHARGER OIL SUPPLY LINE DETERIORATED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010917001912001091700191SO 2001 9 17 AUS20010828 120010805G3260487862 SWITCH PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL MLG OUT OF ADJ W O OTHER J WARNING INDICATION DEDESCENT 1 AUS (AUS) LT AND RT MAIN LANDING GEAR DOOR MICROSWITCHES OUT OF ADJUSTMENT. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000702001090500070SO 2001 9 5 AUS20010829 120010424G7920 HOSE LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE OIL DISTRDETERIORATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TURBOCHARGER OIL PRESSURE HOSE INCORRECTLY ROUTED. HOSE DETERIORATED DUE TO HEAT. HOSE LOOSE ON END FITTING.PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000712001090500071SO 2001 9 5 AUS20010830 120010402G7112 BAFFLE LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE AIR BAFFLMISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LOWER ENGINE BAFFLE MISSING. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010917001922001091700192EA 2001 9 17 AUS20010831 220010727G8530 CYLINDER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT ENGINE NR 2 CYLINDER FAILED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000722001090500072SO 2001 9 5 AUS20010832 120010727G2140 HEATER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL HEATING SYSTEM FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS (AUS) HEATER FAILED. SPARKING BEHIND INSTRUMENT PANEL CAUSED BY FOREIGN OBJECT FALLING ACROSS TERMINALS. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010917001932001091700193EA 2001 9 17 AUS20010833 220010727G8530 CYLINDER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT ENGINE NR 2 CYLINDER FAILED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010917001952001091700195EA 2001 9 17 AUS20010834 220010529G8530 CYLINDER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT ENGINE NR 2 CYLINDER FAILED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010917001972001091700197SW 2001 9 17 AUS20010836 120010801G2910212076176001 PIPE BELL 412 412 1182202SW PWA PT6T PT6T3 52045EA HYDRAULIC SYSTEMCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HYDRAULIC PIPE CRACKED IN RADIUS. 1G72 4U4 U H4SW E22EA 20010917001992001091700199SO 2001 9 17 AUS20010837 120010609G575162373000 DOUBLER PIPER PA28 PA28140 7102802SO AILERONS CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT AILERON DOUBLER CRACKED. 1L71 3O 2A13 20010917002022001091700202NE 2001 9 17 AUS20010839 220010731G732112773 FUEL CONTROL BOEING747 747238B 1384828NM RROYCERB211 RB211524D41954555NE NR 4 ENGINE FAULTY W E ENGINE SHUTDOWN EK VIBRATION/BUFFET FLUID LOSS DEDESCENT 1 AUS 6396 (AUS) NR 4 ENGINE FUEL FLOW REGULATOR FAULTY. AIRCRAFT IS FOREIGN REGISTRATION DQ-FJE. 2L74 4F4 F A20WE E12EU 20010905000732001090500073CE 2001 9 5 AUS20010840 120010614G323098820152 ACTUATOR CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL LANDING GEAR RETUNSERVICEABLE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR ACTUATOR FAULTY. 1H71 3O3 O 3A17 E286 5 CP7EA 20010917002072001091700207CE 2001 9 17 AUS20010843 120010803G554051310103 HINGE CESSNA441 441 2076020CE RUDDER MISMANUFACTURED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LOWER RUDDER HINGE BRACKET INSTALLED UPSIDE DOWN. FOUND DURINGINSPECTION IAW CESSNA CQB00-2 R1. MANUFACTURING ERROR. 1L72 3T RTA28CE 20010917002082001091700208 2001 9 17 AUS20010844 420010713G61225AA228 GOVERNOR LKHEED1049 C121C 5262118WP WRIGHTR3350 R3350* 67040EA HAMSTD43E 43E60 NE PROPELLER FAULTY W C ABORTED TAKEOFF O OTHER TOTAKEOFF 1 AUS (AUS) NR 4 ENGINE GOVERNOR FAULTY. 2L74 4R4 R 6A5 E272 6 CP871 20010917002102001091700210NE 2001 9 17 AUS20010845 220010714G8500 ENGINE DOUG DC3 C47B 3021467WP PWA R1830 R183092 52020NE HAMSTD23E 23E50 NE LEFT MAKING METAL W O OTHER EK VIBRATION/BUFFET FLUID LOSS CRCRUISE 1 AUS (AUS) LT ENGINE OIL FILTER METAL CONTAMINATION. ENGINE CHANGED. 2L72 4R4 R A669 5E4 6 CP603 20010905000742001090500074GL 2001 9 5 AUS20010846 220010728G72306898607 BEARING ALLSN 250C20F AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20F 03013GL TURBINE ENGINE CDAMAGED W K NONE E JVIBRATION/BUFFET WARNING INDICATION DEDESCENT 1 AUS CAC40345 (AUS) NO2 ENGINE NO1 BEARING FAILED. 1G72 3U3 U H11EU E4CE 20010917002142001091700214NE 2001 9 17 AUS20010848 220010626G7230 SEAL BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE TURBINE ENGINE LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 AUS (AUS) NR 1 ENGINE OIL LEAKING AROUND BLEED BAND AREA. NR 1 SEAL LEAKING. 2H74 4F4 FRTA49EU E6NE 20010917002152001091700215NM 2001 9 17 AUS20010850 120010807G6310A1902 BELT ROBSINR22 R22BETA NM LYC O320 O320B2C 41508EA TRANSMISSION FRAYED W O OTHER E VIBRATION/BUFFET CRCRUISE 1 AUS 7390 (AUS) REAR DRIVE BELT FRAYED, SPLIT AND ROLLED OFF PULLEY. 1G71 3O3 O H10WE E274 20010917002172001091700217SO 2001 9 17 AUS20010851 120010723G3260 SWITCH PIPER PA24 PA24250 7102404SO LYC O540 O540A1A 41532EA MCAULY2D36C 2D36C28 GL MLG MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR DOWN LIMIT MICROSWITCH INCORRECTLY WIRED.WHEN THE NLG MICROSWITCH WIRES WERE DISCONNECTED THE DOWN LIGHT WAS STILL ON. INVESTIGATION FOUND THE RT LANDING GEAR MICROSWITCH WIRING WAS INCORRECT. PERSONNEL/MAINTENANCE ERROR. 1L71 3O3 O 1A15 E295 5 CP901 20010917002192001091700219SW 2001 9 17 AUS20010852 120010802G6210212015501115 BLADE BELL 212 212 1181420SW PWA PT6T PT6T3B 52045NE MAIN ROTOR DELAMINATED W O OTHER O OTHER CRCRUISE 1 AUS (AUS) MAIN ROTOR BLADE SKIN DELAMINATED AT THE BLADE TIP JUST AFT OFTHE D' SPAR. AREA OF DELAMINATION 55MM BY 75MM (2IN BY 3IN). 1G71 4U4 U H4SW E22EA 20010917002222001091700222NM 2001 9 17 AUS20010855 120010803G5311A0202 FRAME ROBSINR22 R22BETA NM LYC O320 O320B2C 41508EA FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) UPPER FUSELAGE FRAME CRACKED. FOUND DURING MAGNETIC PARTICLE INSPECTION. 1G71 3O3 O H10WE E274 20010917002232001091700223CE 2001 9 17 AUS20010856 120010808G2434ALV9501R ALTERNATOR CESSNA404 404CESSNA 2075901CE ENGINE FAILED W O OTHER H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 AUS (AUS) ALTERNATOR FAILED IN FLIGHT. INVESTIGATION FOUND THE ALTERNATOR HOUSING ASSEMBLY BOLTS LOOSE WITH TWO OF THE BOLTS HAVING COMPLETELY SEPARATED AND LAYING IN THE BOTTOM OF THE ENGINE COWL. REAR BEARING COLLAPSED. INCORRECT TAB WASHERS USED. TAB WASHERS WERE FOR USE ON A 6.35MM (0.25IN) BOLT WHEREAS THE BOLTS USED ONTHE ALTERNATOR WERE 4.762MM (0.185IN). UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR. 1L72 3O A25CE 20010917002242001091700224EU 2001 9 17 AUS20010857 120010716G5730 SKIN BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE LT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING LOWER SKIN CORRODED IN AREA BETWEEN RIB 13 AND RIB 15.CORROSION WAS BEYOND ALLOWIABLE LIMITS. 2H74 4F4 FRTA49EU E6NE 20010917002262001091700226CE 2001 9 17 AUS20010858 120010809G32331CH1066 SWITCH TEIJINSEIKI 99101393 CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL MLG ACTUATOR OUT OF ADJ W K NONE O OTHER ININSP/MAINT 1 AUS 1851 (AUS) NOSE LANDING GEAR ACTUATOR POSITION SWITCH INCORRECTLY ADJUSTED.PERSONNEL/MAINTENANCE ERROR. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20010917002282001091700228NM 2001 9 17 AUS20010859 120010809G5270284A3539 SWITCH BOEING737 737* NM CFMINTCFM56 CFM565A1 NE DOOR WARNING FAULTY W C ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AUS (AUS) LT OVERWING EXIT WARNING SWITCH FAULTY. 2L72 4F4 FRTA16WE E29NE 20010905000772001090500077CE 2001 9 5 AUS20010860 120010713G2434ALV9510R ALTERNATOR CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL DC GENERATOR-ALTFAILED W K NONE H ELECT. POWER LOSS-50 PC CRCRUISE 1 AUS 100 9011080 (AUS) ALTERNATOR ROTOR SHAFT WORN IN AREA OF FORWARD ARMATURE SLIPRING. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010917002292001091700229NE 2001 9 17 AUS20010861 220010807G7421CH34055 IGNITER BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS (AUS) NR 1 ENGINE LOWER IGNITER CENTRE CORE MISSING. P3 AIR LEAKING INTO ENGINE BAY. 1G72 4U4 U H4SW E22EA 20010917002322001091700232NM 2001 9 17 AUS20010862 120010201G5311 FRAME BOEING767 767277 NM GE CF6 CF680A 30025NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT BULKHEAD OUTER CHORD LOCATED AT BS1809.5 CRACKED IN AREA OFLOWER TWO FASTENERS IN INSPECTION AREA 1. 2L72 4F4 FRTA1NM E13NE 20010905000782001090500078CE 2001 9 5 AUS20010863 120010810G7931 PIPE CONT O470R CESSNA182 182H 2072718CE CONT O470 O470R 17026SO MCAULY2A34C 2A34C66 GL ENGINE OIL PRESSCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS 7167 (AUS) ENGINE OIL PRESSURE PIPE FROM FIREWALL TO GAUGE CORRODED IN AREAOF CONTACT WITH SOUNDPROOFING MATERIAL. PIPE IS MANUFACTURED FROM ALUMINIUM. 1H71 3O3 ONT3A13 E273 5 CP3EA 20010918000022001091800002EU 2001 9 18 AUS20010864 120010813G6410109813201107 BLADE AGUSTAA109 A119 0261102EU PWA PT6T PT6T3 52045EA TAIL ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 113 (AUS) TAIL ROTOR BLADE CRACKED ON INNER FACE. THE CRACK LENGTH RUNS FOR ALMOST THE FULL CHORD OF THE BLADE. FOUND DURING INSPECTION IAW AD/119/1 PT1. 1G72 3U4 U H7EU E22EA 20010905000792001090500079NM 2001 9 5 AUS20010865 120010323G292059855 VALVE BOEING767 767277 NM GE CF6 CF680A 30025NE HYDRAULIC SYSTEMCRACKED W K NONE K FLUID LOSS DEDESCENT 1 AUS 49754 129 (AUS) RAM AIR TURBINE (RAT) MODULE CHECK VALVE CRACKED. LOSS OF HYDRAULIC FLUID. INVESTIGATION FOUND THAT THE HEX HEAD SEPARATEDFROM THE CHECK VALVE BODY DUE TO A FRACTURE BETWEEN THE UPPER O' RING GROOVE AND THE INTERNAL BODY THREAD RELIEF. 2L72 4F4 FRTA1NM E13NE 20010918000042001091800004NM 2001 9 18 AUS20010867 120010313G5312 BULKHEAD BOEING737 737377 NM FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FORWARD PRESSURE BULKHEAD LOCATED AT BS178 CRACKED IN TWO LOCATIONS. ONE CRACK FOUND IN LBL 5.7 LOCATED THROUGH INSULATIONBLANKET HOLE. CRACK LENGTH 15.875MM (0.625IN). ONE CRACK FOUND IN RBL 17.1 LOCATED THROUGH INSULATION BLANKET HOLE. CRACK LENGTH15.875MM (0.625IN). FOUND DURING HIGH FREQUENCY EDDY CURRENTINSPECTION. 2L72 4F RTA16WE 20010918000052001091800005SO 2001 9 18 AUS20010868 120010716G2912756164 SPRING PIPER PA23 PA23250 7102308SO LYC O540 IO540K1A5 41532EA HYDRAULIC FILTERMISSING W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) HYDRAULIC FILTER SPRING MISSING. 1L72 3O3 O 1A10 1E4 20010918000062001091800006SO 2001 9 18 AUS20010869 120010716G324216405700 DISK CLEVELAND 16405700 PIPER PA23 PA23250 7102308SO LYC O540 IO540K1A5 41532EA BRAKE WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) BRAKE DISCS WORN BELOW MINIMUM THICKNESS. BOTH DISCS ALSO EXHIBITED EVIDENCE OF RADIAL HEAT STRESS CRACKING. 1L72 3O3 O 1A10 1E4 20010905000812001090500081SO 2001 9 5 AUS20010871 120010808G2910 PIPE PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA HARTZLHCE3Y HCE3YR2 GL HYDRAULIC SYSTEMFRACTURED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HYDRAULIC PIPE FRACTURED. PIPE IS LOCATED IN RH NOSE AREA. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010918000072001091800007CE 2001 9 18 AUS20010872 120010814G324429X111010PR TIRE CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL MLG FAULTY W O OTHER O OTHER LDLANDING 1 AUS (AUS) MAIN LANDING GEAR TIRE SUSPECT FAULTY. DURING LANDING THE TIRE EXHIBITED EXCESSIVE SIDEWARD DEFLECTION COUPLED WITH MINIMAL CLEARANCE CAUSED THE INSIDE WALL OF THE TIRE TO CONTACT THE BRAKE ASSEMBLY. 1H71 3T3 T A37CE E4EA 5 CP60GL 20010905000822001090500082CE 2001 9 5 AUS20010873 120010612G5343244110010 PIVOT CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL LANDING GEAR ATTFAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN LANDING GEAR PIVOTS FAILED PROVISIONS OF CESSNA SERVICEBULLETIN SEB 90-1 REVISION3. 1H71 3O3 O 3A17 E286 5 CP7EA 20010918000082001091800008NE 2001 9 18 AUS20010874 220010625G72502303713 SEAL LYC ALF502R5 BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE TURBINE SECTION LEAKING W O OTHER O OTHER NRNOT REPORTED 1 AUS (AUS) NR 1 ENGINE NR 9 BEARING SEAL LEAKING. SUSPECT FUMES ENTERING CABIN AND CAUSING CREW PROBLEMS. 2H74 4F4 F A49EU E6NE 20010905000832001090500083EA 2001 9 5 AUS20010875 220010813G8520SL13884M06 BEARING LYC IO540E1B5 GULSTM500 500S 0141107SW LYC O540 IO540E1B5 41532EA HARTZLHCC3Y HCC3YR2 NE RECIPROCATING ENDELAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS 118 L595548 (AUS) ENGINE FRONT MAIN BEARING DEFECTIVE. BEARING MATERIAL APPEARS TOBE DELAMINATED FROM BEARING SHELL. METAL CONTAMINATION OF OIL SYSTEM. SUSPECT MANUFACTURING FAULT. 1H72 3O3 O 6A1 1E4 5 CP25EA 20010918000092001091800009NE 2001 9 18 AUS20010876 220010726G7230230318706 SEAL BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE TURBINE ENGINE WORN W O OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 AUS (AUS) NR 3 ENGINE LEAKING OIL FROM BLEED BAND AREA. FUMES ENTERING CABIN THROUGH AIR CONDITIONING SYSTEM. INVESTIGATION FOUND NO1 BEARINGSEAL AND FACE PLATE ASSEMBLY WORN. 2H74 4F4 F A49EU E6NE 20010918000102001091800010EU 2001 9 18 AUS20010877 120010509G2120 HOSE GROB G115 G115C 1660303EU LYC O360 O360A1F6 41514EA HARTZLHCF2Y HCF2YR1 GL AIR DISTRIBUTIONCHAFED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS (AUS) AVIONICS COOLING SCAT HOSE CHAFED ON PRINTED CIRCUIT BOARD. HOSEINNER WIRE SHORT CIRCUITED CAUSING HOSE TO BURN. 1L71 3O3 ONTA57EU E286 5 CP27EA 20010905000842001090500084SO 2001 9 5 AUS20010878 120010515G575312021940001 BRACKET EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE TRAILING EDGE FLBROKEN W K NONE FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LH OUTBOARD FLAP SHROUD INBOARD ROLLER AND BRACKET BROKEN OFF CAUSING FLAP TRACK TO FOUL ON SHROUD. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010905000872001090500087EA 2001 9 5 AUS20010882 220010801G8520 CRANKCASE LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL RECIPROCATING ENDAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE CRANKCASE DAMAGED. NO3 CYLINDER EXHAUST TAPPET BODY ALSO DAMAGED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010918000132001091800013EA 2001 9 18 AUS20010885 220010813G72503010311 ENGINE DHAV DHC6 DHC6100 EA PWA PT6 PT6A20 52043EA HARTZLHCB3T HCB3TN3 GL RIGHT MISREPAIRED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FOLLOWING REPAIR FOR OVERTEMP AND FOD IN THE USA THE RT ENGINE WAS FITTED AND PREPARED FOR STARTING. THE ENGINE WAS WOUND OVER WITHOUT LIGHTING UP AND AN INTERNAL RUBBING NOISE WAS HEARD. THE ENGINE WAS PARTIALLY DISMANTLED AND INSPECTION FOUND THE COMPRESSOR TURBINE RUBBING ON SEGMENTS IN SMALL EXIT DUCT.FURTHER STRIPPING AND INSPECTION FOUND ABRASIVE MATERIAL IN THE COMBUSTION CHAMBER. INSPECTION ALSO FOUND THAT THE POWER TURBINE LOCK WIRING WAS CARRIED OUT WITH STAINLESS STEEL LOCKWIRE INSTEAD OF ICONEL LOCKWIRE. THE ITT PROBES WERE FOUND TO BE FINGER TIGHT AND INCORRECTLY SECURED. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART. 1H72 3T3 T A9EA E4EA 6 CP15EA 20010918000142001091800014NM 2001 9 18 AUS20010886 120010117G3230BACB10A554 BEARING BOEING737 737377 NM CFMINTCFM56 CFM563B2 13802EU NLG SEIZED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR MANUAL EXTENSION RELEASE MECHANISM TORQUE SHAFT BEARINGS SEIZED. 2L72 4F4 FRTA16WE E21EU 20010918000152001091800015EU 2001 9 18 AUS20010888 120010805G2731NB45C1867 ROD END BNORM BN2 BN2B20 1520302EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL ELEVATOR TAB WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELEVATOR TRIM TAB DRIVE ROD END WORN. INSPECTION FOUND THE LEFT THREADED LOCKNUT STRIPPED. 1H72 3O3 O A17EU 1E4 5 CP920 20010905000882001090500088CE 2001 9 5 AUS20010889 120010816G2910581710219 PIPE CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL HYDRAULIC SYSTEMCRACKED W K NONE K FLUID LOSS CRCRUISE 1 AUS (AUS) MAIN LANDING GEAR EXTENSION SYSTEM HYDRAULIC PIPE CRACKED INBEND. LOSS OF HYDRAULIC FLUID. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010905000892001090500089NE 2001 9 5 AUS20010890 220010811G7230 SEAL LYC ALF502R5 BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE TURBINE ENGINE CLEAKING W K NONE B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 AUS (AUS) NO1 ENGINE NO9 BEARING SEAL LEAKING. FUMES IN CABIN. 2H74 4F4 F A49EU E6NE 20010905000902001090500090NE 2001 9 5 AUS20010892 220010817G7321324476812 FCU PWA PT6A42 BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE HARTZLHCD4N3HCD4N3A GL FUEL CONTROL/TURUNSERVICEABLE W K NONE E VIBRATION/BUFFET CRCRUISE 1 AUS 3597 (AUS) LH ENGINE FUEL CONTROL UNIT FAULTY. 1L72 4T4 T A24CE E4EA 5 CSTC 20010918000172001091800017SW 2001 9 18 AUS20010893 120010712G6420206011812001 TRUNNION BELL 206011810 BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL TAIL ROTOR HEAD CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 2400 AAG00543 (AUS) TAIL ROTOR TRUNNION SUSPECT CRACKED. TRUNNION GAVE A POSITIVE CRACK INDICATION USING BOTH MPI AND FPI INSPECTIONS. 1G71 3U3 U H2SW E4CE 20010918000182001091800018GL 2001 9 18 AUS20010894 220010614G725023063354 ENGINE DOUG 600N 600N 3027377NM ALLSN 250C 250C47B GL NACELLE OVERHEATED W E ENGINE SHUTDOWN EM VIBRATION/BUFFET OVER TEMP NRNOT REPORTED 1 AUS (AUS) TURBINE OVER TEMPERATURE DURING ENGINE SHUTDOWN. 1G71 3U3 UNCH3WE E1GL 20010905000912001090500091EU 2001 9 5 AUS20010895 120010601G7710 LINE RROYCE SPEY55515 FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU POWER INDICATINGLOOSE W K NONE ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AUS (AUS) NO2 ENGINE THRUST FEED SENSE LINE TO GAUGE LOOSE. 2L72 4F4 FRTA20EU E2EU 20010918000192001091800019EU 2001 9 18 AUS20010897 120010605G3232AH533 ACTUATOR FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU MLG DOOR CRACKED W O OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 AUS 6320 (AUS) LT MAIN LANDING GEAR DOOR AFT ACTUATOR CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID. 2L72 4F4 FRTA20EU E2EU 20010905000922001090500092EU 2001 9 5 AUS20010898 120010621G3230 LEVER FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU LANDING GEAR RETSTUCK W K NONE OF OTHER FLT CONT AFFECTED TOTAKEOFF 1 AUS (AUS) LANDING GEAR RETRACTION LEVER STUCK IN DOWN POSITION. CIRCUIT BREAKER L8 POPPED. 2L72 4F4 FRTA20EU E2EU 20010918000202001091800020EU 2001 9 18 AUS20010899 120010726G7931642514172 TRANSMITTER AMD FALC50FALCON900 2700160EU GARRTTTFE731TFE7315R 01518WP ENGINE OIL PRESSFAILED W O OTHER EK VIBRATION/BUFFET FLUID LOSS NRNOT REPORTED 1 AUS 266 (AUS) NR 3 ENGINE OIL PRESSURE TRANSMITTER FAULTY. 2L73 4F4 FRTA46EU E6WE 20010918000232001091800023EU 2001 9 18 AUS20010902 220010627G7250 BLADE BOEING737 737400 NM CFMINTCFM56 CFM563C 13802EU TURBINE SECTION CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 20631 (AUS) NR 1 ENGINE HIGH PRESSURE TURBINE BLADE CRACKED FROM HOLE. FOUND DURING BOROSCOPE INSPECTION IAW EI 737-72-525. 2L72 4F4 FRTA16WE E21EU 20010919001662001091900166SO 2001 9 19 AUS20010903 120010515G2710 CONTROL UNIT PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL AILERON LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AILERON CONTROL SYSTEM HAD EXCESSIVE PLAY. INVESTIGATION FOUNDUNIVERSAL PNO 46203-02 WORN COMPLETELY THROUGH BUSH PNO 453-824 AND INTO BRACKET PNO 29197-02 MOUNTED ON FORWARD BULKHEAD. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010905000932001090500093EA 2001 9 5 AUS20010904 220010814G8520L1959448 STUD LYC IO540E1B5 GULSTM500 500S 0141107SW LYC O540 IO540E1B5 41532EA HARTZLHCA3V HCA3VK2 GL RECIPROCATING ENSHEARED W K NONE OK OTHER FLUID LOSS ININSP/MAINT 1 AUS 1340 L1959448 (AUS) LH ENGINE NO4 CYLINDER HOLDDOWN STUDS (3OFF) SHEARED. FOLLOWING REMOVAL OF THE CYLINDER THE CRANKCASE WAS FOUND TO BE CRACKED THROUGH THE AREA OF THE HOLDDOWN STUDS. 1H72 3O3 O 6A1 1E4 5 CP6EA 20010905000942001090500094CE 2001 9 5 AUS20010908 120010712G2711AN36A BOLT BEECH 58 58 1152740CE CONT O520 IO520C 17032SO HARTZLHCJ3Y PHCJ3YF2 GL AILERON TAB CONTWORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELEVATOR TRIM TAB ACTUATOR TO TRIM TAB ROD ATTACHMENT BOLTS WORN. FOUND DURING INSPECTION IAW AD/B55/59. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20010905000992001090500099WP 2001 9 5 AUS20010919 220010731G73148974007 PUMP GARRTT TPE33112UA BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP MCAULY4HFR344HFR34C653 NE ENGINE FUEL PUMPUNSERVICEABLE W K NONE O OTHER ININSP/MAINT 1 AUS 4306 P6012 (AUS) ENGINE FUEL PUMP HOUSING CRACKED IN AREA OF CONCENTRIC SHAFTSUPPORT. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010905001012001090500101NE 2001 9 5 AUS20010921 220010628G7230PCE93406 COMPRESSOR PWA PT6A42 BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE HARTZLHCB3T HCB3TN3 GL TURBINE ENGINE CFOD W K NONE EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 AUS PCE93406 (AUS) ENGINE COMPRESSOR EXTENSIVELY DAMAGED BY FOD. INVESTIGATION FOUND A DAMAGED WASHER IN THE COWL. SUSPECT CAME FROM BOLT SECURING COMPRESSOR SCREEN REMOVED DURING MAINTENANCE PRIOR TO THISFLIGHT. PERSONNEL/MAINTENANCE ERROR. 1L72 4T4 T A24CE E4EA 6 CP15EA 20010919001802001091900180CE 2001 9 19 AUS20010923 120010814G324429X111010PR TIRE CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL MLG FAULTY W O OTHER O OTHER LDLANDING 1 AUS (AUS) MAIN LANDING GEAR TYRE HAD EXCESSIVE SIDEWARDS DEFLECTION DURING LANDING CAUSING THE TYRE TO CONTACT THE BRAKE ASSEMBLY. TYRE SIZE 29X11.0X10 10PLY. 1H71 3T3 T A37CE E4EA 5 CP60GL 20010905001032001090500103WP 2001 9 5 AUS20010925 120010824G6520369A54083 SHAFT HUGHES 369A5400 HUGHES369 369HS 4470728WP ALLSN 250C 250C20 03013GL TAIL ROTOR GEARBDISTORTED W K NONE O OTHER ININSP/MAINT 1 AUS 344 B222 (AUS) TAIL ROTOR GEARBOX OUTPUT SHAFT BEARINGS BREAKING UP AND SHAFTRUNOUT EXCESSIVE. SHAFT RUNOUT APPROXIMATELY 0.457MM (0.018IN). MAXIMUM RUNOUT 0.0254MM (0.001IN). 1G71 3U3 U H3WE E4CE 20010919001852001091900185 2001 9 19 AUS20010927 420010205G2565D30665101MOD SLIDE AIRBUS320 A320* EU CFMINTCFM56 CFM565A1 NE CABIN FAILED W K NONE L NO TEST ININSP/MAINT 1 AUS 5003 (AUS) SLIDERAFT SEAL FAILED DURING INFLATION TEST. SEAL SEPARATION OCCURRED IN THE UPPER CHAMBER AT THE INTERSECTION OF THE UPPERAND SIDE TUBES. LENGTH OF TEAR 304.8MM (12IN). SLIDE HAD BEEN SENT TO WORKSHOP FOR REPAIR FOLLOWING AN INCIDENT WITH MOBILE STAIRS. 2L72 4F4 FRTA46NM E29NE 20010905001052001090500105EA 2001 9 5 AUS20010930 220010822G732230804 FLOAT FACET MA4SPA CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160DTM GL FUEL CONTROL/RECDAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS 163 BL198636 (AUS) CARBURETTOR FLOAT CONTAMINATED WITH FUEL CAUSING CARBURETTOR TO FLOOD. 1H71 3O3 ONT3A12 E274 5 NP910 20010905001062001090500106GL 2001 9 5 AUS20010932 120010726G81203BT5EE10J2 TURBOCHARGER LYC HIO360E1AD ENSTRMF28 F28C 3300407GL LYC O360 HIO360E1AD 41514EA EXHAUST TURBOCHAFOD W K NONE O OTHER TOTAKEOFF 1 AUS (AUS) ENGINE TURBOCHARGER INGESTED A NUT FROM THE AIR STATIC TUBE LOCATED INSIDE THE AIR CLEANER. FOD. 1G71 3O3 O H1CE 1E10 20010920000292001092000029CE 2001 9 20 AUS20010934 120010823G553107310292 SPAR CESSNA185 185F 2072820CE CONT O470 O470R 17026SO VERTICAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS PN073100149 (AUS) VERTICAL STABILISER REAR SPAR ASSEMBLY CRACKED IN TWO AREAS ADJACENT TO THE FUSELAGE BULKHEAD ATTACHMENT POINT. 1H71 3O3 O 3A24 E273 20010905001072001090500107CE 2001 9 5 AUS20010935 120010810G3230HMX5FG ROD END CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL LANDING GEAR RETBROKEN W K NONE OE OTHER VIBRATION/BUFFET TOTAKEOFF 1 AUS (AUS) LH LANDING GEAR INBOARD RETRACTION ROD OUTBOARD RODEND BALL SOCKET FRACTURED. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010905001082001090500108SO 2001 9 5 AUS20010936 220010827G8520 CRANKSHAFT CONT IO520F CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL RECIPROCATING ENBROKEN W K NONE E VIBRATION/BUFFET NRNOT REPORTED 1 AUS (AUS) CRANKSHAFT BROKEN AT NO4 MAIN BEARING JOURNAL. 1H71 3O3 O A4CE E5CE 5 CP21EA 20010919001942001091900194SO 2001 9 19 AUS20010938 220010214G8530 PISTON CESSNA172 R172K 2072431CE CONT O360 IO360K 17025SO MCAULY2A34C 2A34C203 GL ENGINE DAMAGED W O OTHER EK VIBRATION/BUFFET FLUID LOSS CRCRUISE 1 AUS (AUS) NR 2 CYLINDER PISTON HOLED IN AREA OF RING GROOVES. EXCESSIVE CRANKCASE PRESSURE VENTED OIL THROUGH THE BREATHER. LOSS OF OIL PRESSURE CAUSED NR 1 CYLINDER CONNECTING ROD BIGEND FAILURE. INVESTIGATION FOUND A PIECE OF BROKEN PISTON RING HAD BEEN WORKING IN THE RING GROOVE CAUSING FAILURE OF THE LAND. 1H71 3O3 O 3A17 E1CE 5 CP3EA 20010919001972001091900197SW 2001 9 19 AUS20010939 120010827G5620412670101 WINDOW BELL 412 412 1182202SW PWA PT6T PT6T3 52045EA COCKPIT FAILED W O OTHER E VIBRATION/BUFFET DEDESCENT 1 AUS (AUS) LT SLIDING DOOR REAR WINDOW FAILED. MINOR DAMAGE TO HF RADIO ANTENNA CONNECTOR AND HORIZONTAL STABILISER. 1G72 4U4 U H4SW E22EA 20010919002032001091900203NM 2001 9 19 AUS20010941 120010401G5310 STRUCTURE BOEING737 737377 NM FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) CORROSION CONTROL INSPECTION FOUND AREAS OF LEVEL 2 CORROSION.FOUND DURING INSPECTION IAW AD/B737/52 AMDT2. 2L72 4F RTA16WE 20010919002042001091900204NM 2001 9 19 AUS20010942 120010401G5310 STRUCTURE BOEING737 73733A 1384673NM FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) CORROSION CONTROL INSPECTION FOUND AREAS OF LEVEL 2 CORROSION.FOUND DURING INSPECTION IAW AD/B737/52 AMDT2. 2L72 4F RTA16WE 20010905001092001090500109SO 2001 9 5 AUS20010943 220010820G8520634503 BEARING CONT GTSIO520H CESSNA421 421B 2076014CE CONT O520 GTSIO520H 17032SO MCAULY3AF34C3AF34C92 GL RECIPROCATING ENFAILED W K NONE O OTHER ININSP/MAINT 1 AUS 600 235015R (AUS) ENGINE OIL FILTER CONTAMINATED WITH METAL. INVESTIGATION FOUNDNO1 AND NO2 BEARINGS HAD COMPLETELY FAILED WITH THE BEARING SHELLS BROKEN IN HALF. TRANSVERSE CRACKS WERE FOUND AROUND THECRANKSHAFT NO2 MAIN JOURNAL WITH CATASTROPHIC FAILURE IMMINENT. 1L72 3O3 O A7CE E7CE 5 CP22EA 20010919002372001091900237CE 2001 9 19 AUS20010944 120010824G3260727725 CIRCUIT BREAKER BEECH 200 B200C 1152924CE PWA PT6 PT6A42 52043NE MLG INDICATOR FAULTY W O OTHER N FALSE WARNING DEDESCENT 1 AUS (AUS) LANDING GEAR INDICATION SYSTEM CIRCUIT BREAKER HAD HIGH RESISTANCE. 1L72 4T4 T A24CE E4EA 20011015000282001101500028CE 2001 10 15 AUS20010947 120010824G7602MC98620661 LEVER CONT IO520F CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL MIXTURE CONTROL FAILED W K NONE O OTHER CLCLIMB 1 AUS (AUS) MIXTURE CONTROL VERNIER FAILED. CENTRE KNOB AND SHAFT SEPARATED FROM MIXTURE CONTROL. 1H71 3O3 O A4CE E5CE 5 CP21EA 20020108000022002010800002GL 2002 1 8 AUS20010948 120010825G3211AN531A BOLT AMTR MK1 MK1 05620JYGL MLG BROKEN W O OTHER O OTHER LDLANDING 1 AUS (AUS) LANDING GEAR REAR MOUNT BOLT FAILED DURING HEAVY LANDING. MINOR DAMAGE TO REAR OF SPAR. 1H71 3O NCEXPA1H71 20011015000302001101500030EA 2001 10 15 AUS20010952 220010829G73103011849 PIPE PWA PT6A34 EMB 110 EMB110P2 3260124SO PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL ENGINE FUEL DISTCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PIPE LOCATED BETWEEN FCU AND START CONTROL VALVE CRACKED AT FITTING. 1L72 4T4 T A21SO E4EA 6 CP15EA 20020108000062002010800006CE 2002 1 8 AUS20010955 120010823G2612473275 DETECTOR BEECH 200 B200C 1152924CE PWA PT6 PT6A42 52043NE FIRE DETECTION UNSERVICEABLE W O OTHER NO FALSE WARNING OTHER CRCRUISE 1 AUS (AUS) FIRE DETECTOR FAULTY. 1L72 4T4 T A24CE E4EA 20011015000312001101500031NM 2001 10 15 AUS20010956 120010904G352028003101 LANYARD BOEING767 767238 NM PWA JT9 JT9D7R4E 52054NE PASSENGER OXYGENMISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) OXYGEN MASKS LOCATED AT SEATS 26J/K HAD MISSING LANYARDS (3OFF). 2L72 4F4 FRTA1NM E3NE 20011015000332001101500033EU 2001 10 15 AUS20010960 120010820G5720 BRACKET PARTEN P68 PARTENP68 P68B EU LYC O360 IO360A1B6 41514EA HARTZLHCC2Y HCC2YR2 GL WING, MISCELLANECORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH WING LEADING EDGE TOP FORWARD ATTACHMENT BRACKET CORRODED. 1H72 3O3 O A31EU 1E10 5 CP920 20011015000342001101500034GL 2001 10 15 AUS20010962 120010822G3710215CC PUMP PAC CT4 CT4B GL CONT O360 IO360HB 17025SO HARTZLHCC2Y BHCC2YF1 GL VACUUM DISTRIBUTFAILED W K NONE I FLT. ATTITUDE INST. NRNOT REPORTED 1 AUS 11609 (AUS) VACUUM PUMP SEIZED AND DRIVE SHAFT SHEARED. 1L71 3O3 ORTA9PC E1CE 5 CP920 20020108000092002010800009CE 2002 1 8 AUS20010963 120010828G2434 SEAL CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C93 GL DC GENERATOR-ALTLEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS 9 (AUS) LT ENGINE DRIVEN ALTERNATOR DRIVE SEAL LEAKING. INVESTIGATION FOUND THAT THE SEAL WAS INCORRECTLY FITTED. 1L72 3O3 O A7CE E8CE 5 CP22EA 20011015000352001101500035CE 2001 10 15 AUS20010964 120010903G5730552212126 SPLICE CESSNA 550 CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE WING, PLATES/SKICORRODED W K NONE O OTHER ININSP/MAINT 1 AUS 550054 (AUS) RH WING SKIN SPLICE CORRODED. AREAS OF SPLICE ASSEMBLY DISBONDED. 1L72 4F4 F A22CE E1NE 20020108000102002010800010NM 2002 1 8 AUS20010965 120010904G3242AS11506K0346 HOSE BOEING737 737400 138449ANM CFMINTCFM56 CFM563B1US GL BRAKE FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 2 BRAKE HOSE FRACTURED AND LEAKING. 2L72 4F4 FRTA16WE E2GL 20020108000152002010800015NE 2002 1 8 AUS20010970 220010905G7230MS9390290 PIN LYC ALF502ALF502R3A 41580NE ENGINE MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE FAN DISC RETAINING NUT LOCK CUP WASHER LOCKING PINS FLUSHWITH SHAFT MAKING LOCKING MECHANISM NON FUNCTIONAL. THE FAN HAD BEEN REMOVED TO SERVICE ANOTHER ENGINE. 4 F E6NE 20011015000362001101500036CE 2001 10 15 AUS20010971 120010822G561010138402521 WINDSHIELD BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE MCAULY4HFR344HFR34C754 NE FLIGHT COMPARTMEFAILED W K NONE O OTHER CLCLIMB 1 AUS (AUS) LH WINDSHIELD SHATTERED. 1L72 4T4 T A24CE E4EA 6 C3PNE 20020108000162002010800016NE 2002 1 8 AUS20010972 220010829G7260PLE94397 GEARBOX BEECH 200 B200C 1152924CE PWA PT6 PT6A42 52043NE HARTZLHCD4N3HCD4N3A GL ENGINE ACCESSORYDISCONNECTED W O OTHER EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 AUS (AUS) ENGINE ACCESSORY GEARBOX DECOUPLED PREVENTING ACCESSORIES FROM OPERATING. 1L72 4T4 T A24CE E4EA 5 CSTC 20011015000372001101500037SO 2001 10 15 AUS20010973 220010820G8520634503 BEARING CONT GTSIO520M CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL RECIPROCATING ENBROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE MAIN BEARING BROKEN INTO SEVERAL PIECES. METAL CONTAMINATION OF OIL SYSTEM. BEARING WAS A GENUINE CONTINENTALITEM. 1L72 3O3 O A25CE E7CE 5 CP45GL 20011015000382001101500038SO 2001 10 15 AUS20010974 220010820G8520634503 BEARING CONT GTSIO520M CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL RECIPROCATING ENBROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE MAIN BEARING BROKEN INTO THREE PIECES. METAL CONTAMINATION OF ENGINE. 1L72 3O3 O A25CE E7CE 5 CP45GL 20020108000182002010800018EU 2002 1 8 AUS20010977 120010807G29132912 MOTOR PILATSPC12 PC12 7090550EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL HYDRAULIC PUMP DIRTY W O OTHER O OTHER DEDESCENT 1 AUS (AUS) LANDING GEAR HYDRAULIC POWER PACK ELECTRIC MOTOR FAULTY.INVESTIGATION FOUND LIGHT CORROSION IN COMMUTATOR END OF MOTOR. THE MOTOR WAS ALSO DIRTY WITH THE BRUSHES STICKING IN THE BRUSH HOLDERS. HYDRAULIC RETURN FILTER DIRTY. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20011015000402001101500040CE 2001 10 15 AUS20010979 120010901G7602MC98620661 SHAFT CONT IO520F CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL MIXTURE CONTROL SEPARATED W K NONE O OTHER CRCRUISE 1 AUS (AUS) MIXTURE CONTROL VERNIER FAILED CAUSING CENTRE KNOB AND 177.8MM(7IN) OF SHAFT TO SEPARATE FROM MIXTURE CONTROL. 1H71 3O3 O A4CE E5CE 5 CP21EA 20020108000212002010800021NE 2002 1 8 AUS20010981 220010903G72409560151480 SWIVEL SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S 60030NE COMBUST CHAMBER LOOSE W O OTHER EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS (AUS) NR 1 ENGINE COMBUSTION CHAMBER P2 AIR TAP SWIVEL UNION ASSEMBLY CONE LOOSE. 1G72 3U3 U H1NE E19EU 20011015000422001101500042EA 2001 10 15 AUS20010986 220010829G741410349234 GEAR CONT BL3493704 PIPER PA32 PA32300 7103212SO LYC O540 IO540K1G5 41532EA HARTZLHCC2Y HCC2YK1 GL MAGNETO/DISTRIBUBROKEN W K NONE E VIBRATION/BUFFET NRNOT REPORTED 1 AUS 727 A250007FR (AUS) LH MAGNETO FAULTY. INSPECTION FOUND THAT ONE OF THE COILRETAINING WEDGES PNO 10-349219 WAS ADRIFT INSIDE THE CASE. THEDISTRIBUTOR GEAR PNO 10-349234 WAS FOUND TO HAVE THREE TEETHMISSING. SUSPECT WEDGE JAMMED GEAR CAUSING TEETH TO STRIP AND ALLOW THE INTERNAL TIMING TO CHANGE. 1L71 3O3 O A3SO 1E4 5 CP920 20011015000442001101500044CE 2001 10 15 AUS20010990 120010904G7810K9695000277 EXHAUST PIPE CONT IO520C BEECH 55 95C55 1152708CE CONT O520 IO520C 17032SO MCAULY3AF32C3AF32C75 GL ENGINE COLLECTORFAULTY W K NONE I FLT. ATTITUDE INST. NRNOT REPORTED 1 AUS (AUS) LH ENGINE EXHAUST PIPE HELD ON BY REAR CLAMP ONLY AND TOUCHINGFIREWALL. HEAT AFFECTED PLASTIC JOINER TUBE FOR PITOT SYSTEMLOCATED BEHIND FIREWALL. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20020108000252002010800025CE 2002 1 8 AUS20010991 120010829G5220 DOOR CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL EMERGENCY EXIT SEPARATED W A UNSCHED LANDING D INFLIGHT SEPARATION CRCRUISE 1 AUS (AUS) EMERGENCY EXIT SEPARATED DURING FLIGHT. NO DAMAGE TO AIRCRAFT. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20011015000452001101500045GL 2001 10 15 AUS20010992 120010803G7820 MUFFLER CONT IO360HB PAC CT4 CT4B GL CONT O360 IO360HB 17025SO HARTZLHCC2Y BHCC2YF1 GL ENGINE NOISE SUPCRACKED W K NONE O OTHER CRCRUISE 1 AUS (AUS) RH MUFFLER CRACKED. CARBON MONOXIDE FUMES IN COCKPIT. 1L71 3O3 ORTA9PC E1CE 5 CP920 20011015000462001101500046GL 2001 10 15 AUS20010993 120010908G5720 TAPE PAC CT4 CT4B GL CONT O360 IO360HB 17025SO HARTZLHCC2Y BHCC2YF1 GL WING, MISCELLANESEPARATED W K NONE O OTHER CRCRUISE 1 AUS (AUS) LH WING ROOT SEALING TAPE SEPARATED. CARBON MONOXIDE FUMESENTERED COCKPIT. 1L71 3O3 ORTA9PC E1CE 5 CP920 20011015000472001101500047CE 2001 10 15 AUS20010994 120010831G321350450182 WASHER CESSNA402 402CESSNA 207590KCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C87 GL MAIN LANDING GEAMISSING W K NONE O OTHER LDLANDING 1 AUS (AUS) LH MAIN LANDING GEAR TORQUE LINK CENTRE PIVOT WASHER NOT FITTED.TORQUE LINKS SEPARATED ALLOWING AIRCRAFT TO GROUND LOOP. 1L72 3O3 O A7CE E8CE 5 CP22EA 20011015000482001101500048CE 2001 10 15 AUS20010997 120010915G71205854002 MOUNT CONT GTSIO520M CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL ENGINE MOUNT SECCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE MOUNT CROSS MEMBER CRACKED. 1L72 3O3 O A25CE E7CE 5 CP45GL 20011015000492001101500049 2001 10 15 AUS20010998 420010906G2565D31591478 SLIDE ESCAPE SLIDE FAULTY W K NONE OJ OTHER WARNING INDICATION ININSP/MAINT 1 AUS 225 2321 (AUS) ESCAPE SLIDE TEST LIGHTS FAILED TO ILLUMINATE DURING TEST.INSPECTION FOUND SWITCH PIN LANYARD TOO LONG. 20020108000282002010800028CE 2002 1 8 AUS20010999 120010605G281033400512 FUEL TANK BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO FUSELAGE DETERIORATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUEL TANKS DETERIORATED. FUEL SYSTEM AND FUEL FILTERS CONTAMINATED WITH FOAM MATERIAL. 1L72 3O3 ORT3A16 3E1 20011015000502001101500050EU 2001 10 15 AUS20011004 120010918G291399101371 PUMP REIMS 406 F406 EU PWA PT6 PT6A112 52043NE MCAULY3G34C73GFR34C701 GL HYDRAULIC PUMP, FAILED W K NONE K FLUID LOSS CLCLIMB 1 AUS 1107 (AUS) HYDRAULIC PUMP FAULTY. INVESTIGATION FOUND THE PUMP CIRCLIP GROOVE WORN ALLOWING THE CIRCLIP TO SEPARATE AND THE SPLINE ADAPTER PNO 24100-646 TO DISENGAGE FROM THE ENGINE DRIVE. 1L72 3T3 TRTA54EU E4EA 5 CP60GL 20020108000332002010800033CE 2002 1 8 AUS20011006 120010912G3260S13771 SWITCH CESSNA210 210N 2073453CE CONT O520 IO520L 17032SO MCAULYD3A34 D3A34C404 GL MLG DOWNLOCK FAULTY W O OTHER P NO WARNING INDICATION DEDESCENT 1 AUS (AUS) RT MAIN LANDING GEAR DOWNLOCK MICROSWITCH WIRE BROKEN FROM SWITCH BODY. 1H71 3O3 O 3A21 E5CE 5 CP47GL 20011015000512001101500051CE 2001 10 15 AUS20011007 120010830G3230MS16562130 PIN CESSNA340 340CESSNA 2076404CE CONT O520 TSIO520K 17040SO MCAULY3AF32C3AF32C87 GL LANDING GEAR RETSHEARED W K NONE O OTHER LDLANDING 1 AUS (AUS) LANDING GEAR UPPER MANUAL EMERGENCY EXTENSION SYSTEM INTERCONNECT SHAFT SPROCKET ROLL PIN SHEARED. 1L72 3O3 O 3A25 E8CE 5 CP22EA 20011015000522001101500052SO 2001 10 15 AUS20011008 220010916G8597 WIRE CONT IO520F CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL RECIPROCATING ENWORN W K NONE EA VIBRATION/BUFFET FLAME/FIRE CRCRUISE 1 AUS (AUS) ELECTRICAL WIRES (2OFF) LOCATED IN ENGINE COMPARTMENT CHAFING ONSOLID FUEL LINE. WIRES ARCED AND BLEW A SMALL HOLE IN THE FUELLINE RESULTING IN A FIRE IN THE ENGINE COMPARTMENT. INADEQUATEMAINTENANCE. PERSONNEL/MAINTENANCE ERROR. 1H71 3O3 O A4CE E5CE 5 CP21EA 20011015000532001101500053EA 2001 10 15 AUS20011009 220010915G8520 CRANKCASE LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL RECIPROCATING ENCRACKED W K NONE OEBOTHER VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 AUS (AUS) RH ENGINE NO4 CYLINDER HOLDDOWN STUDS (2OFF) BROKEN. CRANKCASECRACKED VERTICALLY UP FROM TOP STUD. CRACK LENGTH 76.2MM (3IN). 1L72 3O3 O A20SO E14EA 5 CP33EA 20020108000342002010800034SO 2002 1 8 AUS20011010 220010910G7414K3823 DISTRIBUTOR CESSNA206 U206F 2073333CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL MAGNETO BURNED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAGNETO DISTRIBUTOR BLOCK BADLY BURNT DUE TO TRACKING FROM DISTRIBUTOR WHEEL SPRING TO MAGNETO HOUSING. 1H71 3O3 O A4CE E5CE 5 CP21EA 20020108000352002010800035EA 2002 1 8 AUS20011011 220010819G7414K3823 DISTRIBUTOR LYC O540 IO540K1A5 41532EA HARTZLHCC2Y HCC2YR1 GL MAGNETO BURNED W O OTHER E VIBRATION/BUFFET LDLANDING 1 AUS (AUS) MAGNETO DISTRIBUTOR BLOCK BADLY BURNT BY TRACKING FROM SPRING INDISTRIBUTOR WHEEL TO MAGNETO HOUSING. 3 O 1E4 5 CP920 20011015000562001101500056SW 2001 10 15 AUS20011017 120010921G5730 PLATE GULSTM500 500S 0141107SW LYC O540 IO540E1A5 41532EA HARTZLHCA3X HCA3XK2 GL WING, PLATES/SKICORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) EXTERNAL SPAR CAP SUPPORT PLATE RH SIDE CORRODED IN AREA OF JOINT BETWEEN TWO PLATES. EVIDENCE OF CORROSION IN SIMILAR AREA ON LH SIDE. 1H72 3O3 O 6A1 1E4 5 CP913 20011015000572001101500057SO 2001 10 15 AUS20011018 120010922G2140461731 REGULATOR PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL HEATING SYSTEM LEAKING W K NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS (AUS) FUEL PRESSURE REGULATOR DIAPHRAGM LEAKING WHEN CABIN HEATER TURNS OFF. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020108000402002010800040GL 2002 1 8 AUS20011019 120010918G2821 FILTER NAMER NA260 T28* GL WRIGHTR1820 R1820* 67020EA HAMSTD43D 43D50 NE FUEL SYSTEM CONTAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AIRCRAFT FUEL FILTER CONTAMINATED. CONTAMINATION ALSO FOUND IN CARBURETTOR FUEL FILTER. 1L71 4R4 R 1A18 5E10 6 CP8879 20020108000442002010800044CE 2002 1 8 AUS20011022 120010914G5751NAS2219 SCREW BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MCAULY3AF34C3AF34C502 GL LT AILERON MISINSTALLED W O OTHER W INADEQUATE Q C CRCRUISE 1 AUS (AUS) LT AILERON ATTACHMENT SCREWS INCORRECTLY LOCATED. AILERON HAD PREVIOUSLY BEEN REMOVED FOR ACCESS AND SCREWS HAD MISSED THE ANCHOR NUTS DURING REPLACEMENT. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20020108000452002010800045SO 2002 1 8 AUS20011023 120010921G3260487862ALT1CH214 SWITCH PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL MLG DOWLOCK OUT OF ADJ W O OTHER PO NO WARNING INDICATION OTHER LDLANDING 1 AUS (AUS) LT MAIN LANDING GEAR DOWNLOCK MICROSWITCH OUT OF ADJUSTMENT. 1L72 3O3 O A20SO E14EA 5 CP33EA 20011015000582001101500058EA 2001 10 15 AUS20011024 220010925G7250310103702 DUCT PWA PT6A27 AMTR MK1 MK1 05620JYGL PWA PT6 PT6A27 52043EA TURBINE SECTION CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 1448 PS41991100 (AUS) ENGINE POWER SECTION EXHAUST DUCT EXTENSIVELY CRACKED. AIRCRAFT IS FOREIGN REGISTRATION 5W-FAY. 1H71 3O4 TNCEXPA1H71E4EA 20011015000592001101500059CE 2001 10 15 AUS20011026 120010917G2434DOFF10300R ALTERNATOR CESSNA172 172N 2072434CE LYC O360 O360A4M 41514EA SNSNCH76E 76EM8 EA DC GENERATOR-ALTFAILED W K NONE H ELECT. POWER LOSS-50 PC CRCRUISE 1 AUS 5110753 (AUS) ALTERNATOR OUTPUT TERMINAL FRACTURED AND ADJACENT WIRING MELTED. 1H71 3O3 ONT3A12 E286 5 NP4EA 20011204000692001120400069SO 2001 12 4 AUS20011032 120010924G57113516808 SPAR PIPER PA28161 PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA SNSNCH74D 74DM EA WING SPAR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS 288216109 (AUS) LH AND RH WING SPARS PNO 35168-08 (LH) AND PNO 35168-09 (RH)CONTAINED SEVERE EXFOLIATION CORROSION. 1L71 3O3 O 2A13 E274 5 NP88614 20020114000032002011400003EA 2002 1 14 AUS20011033 220010914G8520SL743001 BEARING GIPPLDGA200 GA200 EU LYC O540 IO540K1A5 41532EA HARTZLHCC2Y HCC2YR1 GL ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) CONNECTING ROD BIG END BEARING MATERIAL FLAKING OFF FROM BEARING BASE. 1L71 3O3 ONCA00001LA1E4 5 CP920 20011204000702001120400070EA 2001 12 4 AUS20011034 220010927G8520 STUD LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL RECIPROCATING ENFAILED W K NONE E VIBRATION/BUFFET NRNOT REPORTED 1 AUS 218 (AUS) LH ENGINE NO1 CYLINDER HOLDDOWN STUDS FAILED. CRANKCASE CRACKED IN TOP RIGHT STUD HOLE. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020108000612002010800061SO 2002 1 8 AUS20011035 220010912G8530 PISTON CONT O520 IO520M 17032SO ENGINE MISMANUFACTURED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) NEW CYLINDER KIT FAULTY. OIL HOLES NOT DRILLED IN PISTON DURING MANUFACTURE. 3 O E5CE 20011204000712001120400071CE 2001 12 4 AUS20011036 120010928G2710S1997610 BEARING CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL AILERON CONTROL FAILED W K NONE F FLT CONT AFFECTED TOTAKEOFF 1 AUS (AUS) LH AILERON OUTBOARD BELLCRANK UPPER AND LOWER BEARINGS STIFF DUETO LACK OF LUBRICATION AND CORROSION. SUSPECT INADEQUATE SEALINGOF RUBBER BUNG ON TOP OF WING ALLOWED WATER TO WASH OUT THE LUBRICATION FROM THE BEARINGS. 1H71 3O3 O A4CE E5CE 5 CP21EA 20011204000722001120400072CE 2001 12 4 AUS20011037 120010929G531207126161 BULKHEAD CESSNA182 182K 2072724CE CONT O470 O470R 17026SO MCAULY2A34C 2A34C66 GL FUSELAGE MAIN, BCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) AFT TAILCONE BULKHEAD CRACKED IN AREA AT TOP OF RUDDER CABLECUTOUT. 1H71 3O3 ONT3A13 E273 5 CP3EA 20011204000732001120400073CE 2001 12 4 AUS20011038 120010929G5511 SPAR CESSNA182 182K 2072724CE CONT O470 O470R 17026SO MCAULY2A34C 2A34C66 GL HORIZONTAL STABICORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAILPLANE REAR SPAR CONTAINED SEVERE EXFOLIATION CORROSION IN THREE SEPARATE AREAS. SUSPECT CORROSION CAUSED BY WATER INGRESS.PNO 1232610-3 (X2), PNO 0732603-2 AND PNO 1232114-1 AFFECTED. OTHER PARTS ALSO FOUND CORRODED WAS RIB PNO 1231006-1 INTHE FIN AND THE LEFT HAND ELEVATOR TORQUE TUBE AND INBOARD ADAPTOR PNO 0734110-3 AND PNO 0734110-7. THE AFFECTED AREAS WERE NOT PRIMED DURING MANUFACTURE AND THE AIRCRAFT SPENT A CONSIDERABLE AMOUNT OF ITS LIFE IN THE OPEN IN COASTAL AREAS. 1H71 3O3 ONT3A13 E273 5 CP3EA 20011204000742001120400074EA 2001 12 4 AUS20011039 220010924G853073111 EXHAUST VALVE LYC IO360A1B6D MOONEYM20 M20J 5870219SW LYC O360 IO360A1B6 41514EA HARTZLHCC2Y HCC2YK1 GL RECIPROCATING ENFAILED W K NONE E VIBRATION/BUFFET CRCRUISE 1 AUS 1462 L1721451A (AUS) ENGINE NO3 CYLINDER EXHAUST VALVE FAILED. 1L71 3O3 O 2A3 1E10 5 CP920 20020108000762002010800076CE 2002 1 8 AUS20011042 120010907G3233358251722 ARM BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MLG ACTUATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LANDING GEAR RETRACTION MOTOR ARM CRACKED. 1L72 3O3 O 3A16 E5CE 20011204000762001120400076NM 2001 12 4 AUS20011043 120010705G7810320006519 TAILPIPE LYC IO540S1A5 PIPER PA60 PA60601 7106010NM LYC O540 IO540S1A5 41532EA HARTZLHCC3Y HCC3YR2 NE ENGINE COLLECTORCRACKED W K NONE EBJVIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 AUS (AUS) RH ENGINE TAILPIPE CRACKED ALLOWING HOT EXHAUST GAS TO ACTIVATE FIRE WARNING SYSTEM. 1M72 3O3 ORTA17WE 1E4 5 CP25EA 20011204000782001120400078CE 2001 12 4 AUS20011045 120010918G5730552212126 SKIN CESSNA C550 CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE WING, PLATES/SKICORRODED W K NONE O OTHER ININSP/MAINT 1 AUS 5500054 (AUS) RH WING SKIN SPLICE CORRODED. SUBSEQUENT INVESTIGATION REVEALED EXTENSIVE DEBONDING. ULTRASONIC INSPECTION OF LH WING FOUND SIMILAR RESULTS. 1L72 4F4 F A22CE E1NE 20020108000782002010800078CE 2002 1 8 AUS20011047 120011001G2810 FUEL CELL CESSNA402 402A 207590MCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C87 GL LEFT CONTAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS 54 (AUS) LH FUEL SYSTEM CONTAINED SIGNIFICANT AMOUNTS OF SOLID CONTAMINATION. SUSPECT CONTAMINATION IS FROM FUEL STORAGE SYSTEM. 1L72 3O3 O A7CE E8CE 5 CP22EA 20020108000792002010800079WP 2002 1 8 AUS20011048 120010918G5711U2727MK2 SPAR DHAVXXDH82 DH82AROBRTSN2801002WP DHAVXXGIPSY GIPSYMAJOR1 20004WP AMTR C8289 C8289 GL WING DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS BATCHNO48601 (AUS) ALL FOUR WINGS PNO U2727 MK2 (LT LOWER), PNO U2728 MK2 (RT LOWER), PNO U2729 MK2 (LT UPPER) AND PNO U2730 MK2 (RT UPPER) WERE REJECTED FOLLOWING REBUILD. NUMEROUS HOLES DRILLED IN ALL FOUR WING SPARS WERE OVERSIZE OR DRILLED IN A FIGURE 8. AILERON BELLCRANK CONTROL BOX ALSO CRACKED. PERSONNEL/MAINTENANCE ERROR. 1Q71 3I3 I A8EU A8EU 5 NEXPP5N 20020108000802002010800080CE 2002 1 8 AUS20011049 120010926G2460W31X100050 CIRCUIT BREAKER CESSNA441 441 2076020CE DC POWER FAILED W O OTHER O OTHER NRNOT REPORTED 1 AUS (AUS) NR 1 AVIONICS SWITCH / CIRCUIT BREAKER FAILED INTERNALLY. SUSPECT CAUSED BY RAIN WATER CORROSION DUE TO LOCATION OF CIRCUIT BREAKER BELOW THE LT OPENING WINDOW. 1L72 3T RTA28CE 20011204000802001120400080EA 2001 12 4 AUS20011053 220010715G8530 EXHAUST VALVE LYC O235L2C CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA MCAULY1A103 1A103TCM GL RECIPROCATING ENFAILED W K NONE E VIBRATION/BUFFET CRCRUISE 1 AUS (AUS) NO3 CYLINDER EXHAUST VALVE HEAD SEPARATED FROM VALVE STEM CAUSING MAJOR DAMAGE TO CYLINDER AND PISTON. SUSPECT CAUSED BY CORROSIONAND EROSION DAMAGE. INVESTIGATION FOUND TWO OF THE OTHER THREEEXHAUST VALVES IN SIMILAR CONDITION WITH THE LAST EXHAUST VALVE NOT AS BADLY ERODED BUT STILL CONSIDERED UNSERVICEABLE. FURTHER INVESTIGATION FOUND THE CAMSHAFT AND CAM FOLLOWERS PITTED AND WORN DUE TO CORROSION.AIRCRAFT IS ONLY OPERATED FOR APPROXIMATELY 20 TO 50 HOURS PER YEAR. 1H71 3O3 ONT3A19 E223 5 NP50GL 20020108000852002010800085WP 2002 1 8 AUS20011055 120010930G5311269A2234 FRAME HUGHES269 269C 4470504WP LYC O360 HIO360D1A 41514EA FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FRAME CRACKED AT LT CLUSTER. FOUND VISUALLY AND CONFIRMED USING DYE PENETRANT INSPECTION. AIRCRAFT HAD OPERATED FOR 192.2 HOURS SINCE AD/HU269/57 AMDT2 WAS CARRIED OUT.AD/HU269/57 AMDT2 IS CARRIED OUT EVERY 200 HOURS. 1G71 3O3 O 4H12 1E10 20011204000822001120400082CE 2001 12 4 AUS20011057 120010715G2700 CABLE CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA MCAULY1A103 1A103TCM GL FLIGHT CONTROL SCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) SEVERAL FLIGHT CONTROL CABLES RUSTY. THE FOLLOWING CABLES WEREFOUND TO BE UNSERVICEABLE:- 1. PNO 0400107-41 AILERON CABLE (2OFF)2. PNO 0400107-21 BALANCE CABLE 3. PNO 0400107-45 FLAP CABLE4. PNO 0400107-46 FLAP CABLES 5. PNO 0400107-30 TRIM CABLE6. PNO 0400107-57 TRIM CABLE7. PNO 0400107-49 RUDDER CABLE 1H71 3O3 ONT3A19 E223 5 NP50GL 20011204000832001120400083EA 2001 12 4 AUS20011059 220011003G8520LW13827 CRANKCASE LYC LTIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR2 GL RECIPROCATING ENCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH ENGINE CRANKCASE CRACKED ON NO5 CYLINDER BASE PAD IN THE 8 O'CLOCK POSITION. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020108000952002010800095GL 2002 1 8 AUS20011060 220011004G723023064577A VANE DOUG 600N 600N 3027377NM ALLSN 250C 250C47B GL COMPRESSOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) COMPRESSOR SCROLL ASSEMBLY RT TURNING VANE CRACKED. A PIECE OF THE VANE APPROXIMATELY 38.1MM BY 17.78MM (1.5IN BY 0.7IN) WAS MISSING. A SMALL PIECE OF THE LT VANE ALSO APPEARS TO BE MISSING. 1G71 3U3 UNCH3WE E1GL 20011204000892001120400089CE 2001 12 4 AUS20011076 120011012G5751122005312 BRACKET CESSNA207 207 2073602CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL AILERONS CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH AILERON INBOARD AND OUTBOARD HINGE BRACKETS CRACKED ANDDISTORTED. 1H71 3O3 O A16CE E5CE 5 CP47GL 20020114000042002011400004EU 2002 1 14 AUS20011077 120010928G5551GA538021233 BRACKET GIPPLDGA8 GA8 EU LYC O540 IO540K1A5 41532EA HARTZLHCC2Y HCC2YR1 GL HORIZONTAL STAB SHEARED W O OTHER F FLT CONT AFFECTED CLCLIMB 1 AUS 745 (AUS) RT HORIZONTAL STABILISER ATTACHMENT BRACKET RIVETS SHEARED. 1H71 3O3 ONT 1E4 5 CP920 20020108001142002010800114SO 2002 1 8 AUS20011078 220011010G8530SA10200A20P CYLINDER CESSNA150 150H 2071818CE CONT O200 O200A 17020SO AMTR C8289 C8289 GL ENGINE CRACKED W O OTHER ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 AUS (AUS) NR 2 CYLINDER CRACKED FOR APPROXIMATELY 80 PERCENT OF CIRCUMFERENCE ATTHE BASE OF THE THREAD ON THE CYLINDER BARREL BETWEEN THE TOP BARREL FIN AND THE BOTTOM FIN ON THE CYLINDER HEAD. 1H71 3O3 O 3A19 E252 5 NEXPP5N 20011204000902001120400090CE 2001 12 4 AUS20011079 120011011G2612303267 AMPLIFIER BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE MCAULY4HFR344HFR34C754 NE FIRE DETECTION FAULTY W K NONE EBJVIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 AUS 0079 (AUS) LH ENGINE FIRE WARNING SYSTEM CONTROL AMPLIFIER SUSPECT FAULTY. 1L72 4T4 T A24CE E4EA 6 C3PNE 20020108001222002010800122EA 2002 1 8 AUS20011082 220011010G8520LW17828 CRANKSHAFT PIPER PA36 PA36375 7103620SO LYC O720 IO720D1C 41546EA ENGINE BROKEN W K NONE E VIBRATION/BUFFET ININSP/MAINT 1 AUS (AUS) ENGINE CRANKSHAFT BROKEN IN WEB LOCATED FORWARD OF MAIN BEARING JOURNAL BETWEEN NO5/NO6 AND NO7/NO8 CYLINDER BANKS. ONE CONNECTING ROD CRACKED. 1L71 3O3 O A10SO 1E15 20011204000912001120400091SO 2001 12 4 AUS20011083 220010906G7322626813 PIN CONT 6297032 CESSNA210 210L 2073448CE CONT O520 IO520L 17032SO MCAULY3A32C D3A32C88 GL FUEL CONTROL/RECMISSING W K NONE E VIBRATION/BUFFET NRNOT REPORTED 1 AUS G148205RA (AUS) FUEL CONTROL UNIT FUEL METERING LEVER TO SHAFT ATTACHMENT PIN MISSING. 1H71 3O3 O 3A21 E5CE 5 CP21EA 20011204000922001120400092GL 2001 12 4 AUS20011085 120011009G760307431031 SHAFT CONT IO360HB PAC CT4 CT4B GL CONT O360 IO360HB 17025SO HARTZLHCC2Y BHCC2YF1 GL POWER LEVER BROKEN W K NONE E VIBRATION/BUFFET TXTAXI/GRND HDL 1 AUS (AUS) THROTTLE LAYSHAFT CABLE CONNECTION FITTING BROKEN. 1L71 3O3 ORTA9PC E1CE 5 CP920 20011204000932001120400093CE 2001 12 4 AUS20011086 120010214G551104320016 RIB CESSNA 150M CESSNA150 150M 2071830CE CONT O200 O200A 17020SO AMTR C8289 C8289 GL HORIZONTAL STABICRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HORIZONTAL STABILISER RIBS PNO 0432001-6 AND PNO 0432001-36 CRACKED FROM FORWARD ATTACHMENT POINT NUTPLATE RIVETS. 1H71 3O3 O 3A19 E252 5 NEXPP5N 20011204000942001120400094EA 2001 12 4 AUS20011087 220011015G8520640761A BEARING LYC TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL RECIPROCATING ENWORN W K NONE O OTHER ININSP/MAINT 1 AUS 640761A (AUS) DURING LH ENGINE STRIP FOR REPAIR TO A CRACKED CRANKCASE, THE CENTRE MAIN BEARING WAS FOUND TO BE BADLY WORN AND THE LOCATING LUGS WERE BADLY DAMAGED. THE CRANKSHAFT WAS ALSO FOUND TO BEDAMAGED ON THE FORWARD AND REAR SURFACES CONTACTED BY THE BEARING DUE TO EXTREME LONGITUDINAL MOVEMENT OF THE BEARING. SEALANT WASFOUND ON THE BEARING WEBS. THE THROUGH STUD SEALING O'RINGS BETWEEN THE CRANKCASE HALVES WERE MISSING. TO STOP THE OIL LEAK SILK THREAD AND LOCTITE 515 WAS AROUND THE THROUGH BOLT HOLES. NON-APPROVED REPAIR. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020110000022002011000002CE 2002 1 10 AUS20011088 120010822G2434ES4118 BRUSHES CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160DTM GL DC GENERATOR-ALTWORN W O OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 AUS (AUS) ALTERNATOR BRUSHES WORN PREMATURELY. 1H71 3O3 ONT3A12 E274 5 NP910 20011204000952001120400095SO 2001 12 4 AUS20011091 220010911G8520654811 BOLT CONT IO470L BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO HARTZLHCC3Y PHCC3YF2 GL RECIPROCATING ENBROKEN W K NONE E VIBRATION/BUFFET DEDESCENT 1 AUS 27214R (AUS) LH ENGINE NO4 CYLINDER CONNECTING ROD BOLT BROKEN. COWLING HOLED. 1L72 3O3 ORT3A16 3E1 5 CP25EA 20020110000052002011000005SO 2002 1 10 AUS20011092 120010925G27200106Y10 SERVO PIPER PA46 PA46500TP 7104622SO RUDDER CONTROL FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) YAW DAMPER SERVO FAULTY. DUST COVER OVER THE MOTOR COLLECTING WATER (CONDENSATION). THE MOISTURE DRAIN HOLE IS LOCATED AT THE 12 O'CLOCK POSITION INSTEAD OF THE 6 O'CLOCK POSITION. AS A RESULT THE SERVO MOTOR IS BADLY CORRODED AND BURNT. 1L71 3O RTA25SO 20020110000062002011000006SO 2002 1 10 AUS20011093 120010925G5712102718005 RIB PIPER PA46 PA46500TP 7104622SO RT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT WING LEADING EDGE RIB CRACKED IN STIFFENER. 1L71 3O RTA25SO 20011204000962001120400096EU 2001 12 4 AUS20011094 120011019G2612173462410 FIRE DETECTOR BOLKMS117 BK117B2 5626013EU LYC LTS101LTS101750B1 41560NE FIRE DETECTION FAULTY W K NONE EJBVIBRATION/BUFFET WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AUS 173462600 (AUS) NO2 ENGINE FIRE DETECTOR ACTIVATION. FIRE BOTTLE OPERATED.INVESTIGATION FOUND THAT THE AIRCRAFT WAS IN AN UNUSUAL NOSE HIGH TURN AT THE TIME WHICH HAS IN THE PAST CAUSED THE FIRE DETECTOR TO ACTIVATE FOR SHORT PERIODS. 1G72 3U3 UNCH13EU E5NE10 20020110000072002011000007GL 2002 1 10 AUS20011095 320011020G6114 HUB AMTR VANS RV8 GL AMTR CHEVY8CHEVYV8 GL AMTR C8289 C8289 GL PROPELLER CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 317 (AUS) PROPELLER HUB CRACKED. FOUND DURING INSPECTION IAW AIRCRAFT MANUFACTURERS ALERT. 1L71 3O3 VNTEXPA1L71EXPE3V 5 NEXPP5N 20020110000102002011000010SO 2002 1 10 AUS20011098 220011012G8520571043 CRANKCASE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO HARTZLHCJ3Y PHCJ3YF2 GL ENGINE DAMAGED W O OTHER E VIBRATION/BUFFET CRCRUISE 1 AUS 11 (AUS) ENGINE CRANKCASE HOLED IN AREA OF NR 5 AND NR 6 CYLINDERS. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20011204000972001120400097SO 2001 12 4 AUS20011099 120011019G56107929616 WINDSHIELD PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA SNSNCH74D 74DM EA FLIGHT COMPARTMEUNAPPROVED PART W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH WINDSHIELD INCORRECT PART. WINDSHIELD THICKNESS OF 2.5146MM(0.100IN) INSTEAD OF 6.858MM (0.270IN). EXCESSIVE SILASTIC SEALER USED TO FILL GAPS CAUSED BY POOR FIT. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART. 1L71 3O3 O 2A13 E274 5 NP88614 20020110000132002011000013EU 2002 1 10 AUS20011102 120010621G3246C201801202A WHEEL AMD FALC50FALCON900 2700160EU MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN WHEEL INBOARD HALF CRACKED ADJACENT TO BRAKE TANG. FOUND DURING EDDY CURRENT INSPECTION. 2L73 4F RTA46EU 20020110000142002011000014EU 2002 1 10 AUS20011103 120010626G3246C201801202A WHEEL AMD FALC50FALCON900 2700160EU GARRTTTFE731TFE7315R 01518WP MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS U285 (AUS) MAIN WHEEL INBOARD HALF CRACKED ADJACENT TO BRAKE TANG. FOUND DURING EDDY CURRENT INSPECTION. 2L73 4F4 FRTA46EU E6WE 20020110000152002011000015EU 2002 1 10 AUS20011104 120010714G3246C201801202A WHEEL AMD FALC50FALCON900 2700160EU MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS U1010 (AUS) MAIN WHEEL INBOARD HALF CRACKED ADJACENT TO BRAKE TANG. FOUND DURING EDDY CURRENT INSPECTION. 2L73 4F RTA46EU 20011204000982001120400098GL 2001 12 4 AUS20011106 120011019G3710 PUMP PAC CT4 CT4B GL CONT O360 IO360HB 17025SO HARTZLHCC2Y BHCC2YF1 GL VACUUM DISTRIBUTFAILED W K NONE I FLT. ATTITUDE INST. APAPPROACH 1 AUS (AUS) VACUUM PUMP FAILED AND DRIVE SHAFT SHEARED. 1L71 3O3 ORTA9PC E1CE 5 CP920 20011204000992001120400099CE 2001 12 4 AUS20011107 120011012G5744122005317 BRACKET CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL WING, CONTROL SUCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) INBOARD AILERON BRACKET BROKEN INTO TWO PIECES. 1H71 3O3 O A4CE E5CE 5 CP21EA 20020110000182002011000018CE 2002 1 10 AUS20011108 120011012G571165110387 SPAR CAP CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE LT & RT WING DEBONDED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT WING SPAR CAPS DEBONDED AND CORRODED. FOUND DURING ULTRASONIC INSPECTION IAW JWP/2531/01 AND JWP/2503/01. 1L72 4F4 F A22CE E1NE 20020110000192002011000019EU 2002 1 10 AUS20011109 120011024G6410109813201111 BLADE AGUSTAA109 A119 0261102EU TAIL ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAIL ROTOR BLADE CRACKED IN AREA OF DOUBLER WHERE THE FINGERS ARE BLENDED INTO THE BLADE SKIN. CRACKS FOUND USING THE NAKED EYE AND CONFIRMED USING DYE PENETRANT INSPECTION. 1G72 3U H7EU 20020110000212002011000021SO 2002 1 10 AUS20011110 120011008G55404004626 STRUCTURE PIPER PA31 PA31 7103102SO LYC O540 TIO540A2B 41532EA HARTZLHCE3Y HCE3YR2 GL RUDDER CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RUDDER CORRODED IN AREA BETWEEN TORQUE TUBE AND LOWER END CAP. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020110000232002011000023NE 2002 1 10 AUS20011112 220011019G7230 COMPRESSOR BEECH 200 B200C 1152924CE PWA PT6 PT6A42 52043NE ENGINE FOD W O OTHER EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS (AUS) ENGINE FIRST STAGE COMPRESSOR DAMAGE. FOD. 1L72 4T4 T A24CE E4EA 20020110000242002011000024CE 2002 1 10 AUS20011113 120011008G531057111455 DOOR FRAME CESSNA441 441 2076020CE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LOWER CABIN DOOR FRAME CRACKED IN AREA ADJACENT TO AFT HINGEPOINT. 1L72 3T RTA28CE 20011204001002001120400100CE 2001 12 4 AUS20011114 120011022G274103101243 PIN CESSNA 55657544 CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE STABILIZER POSITWORN W K NONE FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 AUS (AUS) ELEVATOR TRIM INDICATOR SKIPPED GROOVES ON TRIM WHEEL GIVINGINCORRECT TRIM POSITION INDICATION. BOTH WHEEL FUSE PLUGS BLEWDUE TO EXCESSIVE BRAKING. 1L72 4F4 F A22CE E1NE 20020110000252002011000025CE 2002 1 10 AUS20011116 120011001G5751122005217 BRACKET CESSNA206 U206E 2073350CE CONT O520 IO520F 17032SO HARTZLHCC3Y HCC3YF1 GL LT AILERON CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AILERON HINGE BRACKET CRACKED AND BROKEN AT LOWER ATTACHMENT POINTS. LT INBOARD AND RT OUTBOARD BRACKETS ALSO CRACKED. SPAR AND RIB ALSO CRACKED. 1H71 3O3 O A4CE E5CE 5 CP25EA 20020114000052002011400005EA 2002 1 14 AUS20011117 220010925G7414 GEAR GIPPLDGA200 GA200 EU LYC O540 O540A1D5 41532EA MCAULY1A200 1A200FA GL MAGNETO FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAGNETO TIMING GEAR DRIVESHAFT FAILED. 1L71 3O3 ONCA00001LAE295 5 NP874 20020110000262002011000026SO 2002 1 10 AUS20011120 220010821G7414 IMPULSE COUPLING BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MAGNETO MISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT ENGINE RT MAGNETO IMPULSE COUPLING NOT INSTALLED. 1L72 3O3 O 3A16 E5CE 20020110000282002011000028CE 2002 1 10 AUS20011121 120010821G5610964200291 WINDSHIELD BEECH 58 58 1152740CE CONT O520 IO520C 17032SO COCKPIT CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) WINDSHIELD CRACKED AND INCORRECTLY INSTALLED. 1L72 3O3 O 3A16 E5CE 20020110000292002011000029CE 2002 1 10 AUS20011122 120010821G27209652400029P CONTROL CABLE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO RUDDER MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) RT REAR RUDDER CABLE INCORRECTLY ROUTED. CABLE EXCESSIVELY WORN. 1L72 3O3 O 3A16 E5CE 20020110000302002011000030CE 2002 1 10 AUS20011123 120010821G5340951100172 FITTING BEECH 58 58 1152740CE CONT O520 IO520C 17032SO FUSELAGE DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT REAR LOWER BATHTUB FITTING DAMAGED. 1L72 3O3 O 3A16 E5CE 20020110000312002011000031CE 2002 1 10 AUS20011124 120010215G79218526250 OIL COOLER CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL ENGINE MISREPAIRED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) ENGINE OIL COOLER CONTAINED UNAUTHORISED REPAIRS AND WELDING. 1H71 3O3 O 3A17 E286 5 CP7EA 20020110000362002011000036EA 2002 1 10 AUS20011125 220010215G7310240001046 LINE CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL FUEL DIST MISREPAIRED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) ENGINE FUEL PRIMER LINE CHAFED THROUGH AND THEN INCORRECTLY REPAIRED. ELECTRICAL TAPE HAD BEEN WRAPPED AROUND THE LINE TO STOP FUEL LEAKS. 1H71 3O3 O 3A17 E286 5 CP7EA 20020110000372002011000037CE 2002 1 10 AUS20011126 120010215G2820240001058 LINE CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL FUEL DIST MISREPAIRED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) MAIN FUEL SUPPLY LINE CHAFED THROUGH BY COWL FLAP CABLE. NYLONWRAP USED TO PROTECT WORN AREA. 1H71 3O3 O 3A17 E286 5 CP7EA 20011204001032001120400103CE 2001 12 4 AUS20011127 120010215G2910248000119 PIPE CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL HYDRAULIC SYSTEMWORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HYDRAULIC PRESSURE LINE WORN. LINE WAS INADEQUATELY SECURED.PERSONNEL/MAINTENANCE ERROR. 1H71 3O3 O 3A17 E286 5 CP7EA 20020110000382002011000038CE 2002 1 10 AUS20011128 120010124G532104102361 FLOOR PANEL CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA MCAULY1A103 1A103TCM GL CABIN FLOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLOOR CRACKED EXCESSIVELY. 1H71 3O3 ONT3A19 E223 5 NP50GL 20020110000392002011000039CE 2002 1 10 AUS20011129 120010319G532104102361 FLOOR PANEL CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA MCAULY1A103 1A103TCM GL CABIN FLOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUSELAGE FLOOR CRACKED EXCESSIVELY. 1H71 3O3 ONT3A19 E223 5 NP50GL 20020110000432002011000043SO 2002 1 10 AUS20011134 220010719G8520630066A CRANKSHAFT AMTR VANS RV8 GL CONT O200 O200* 17020SO AMTR C8289 C8289 GL ENGINE CRACKED W O OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 AUS 38 (AUS) CRANKSHAFT CRACKED. SUSPECT CAUSED BY UNREPORTED PROPELLER STRIKE. CAM DRIVE BOLTS SHEARED. NO EVIDENCE OF LOCKWIRING ON BOLTS. 1L71 3O3 ONTEXPA1L71E252 5 NEXPP5N 20020110000442002011000044CE 2002 1 10 AUS20011135 120011023G243503601018 BEARING LEARSIEGLER CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL STARTER GEN FAILED W O OTHER E VIBRATION/BUFFET CRCRUISE 1 AUS 5135 (AUS) STARTER-GENERATOR BEARINGS FAILED. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20011204001042001120400104EU 2001 12 4 AUS20011136 120011025G5730 SKIN MUDRY 10 CAP10B 0950102EU LYC O360 AEIO360B2F 41514EA HOFMANHO29 HO29HM180 EU WING, PLATES/SKIFRACTURED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH WING LOWER SKINFRACTURED BETWEEN SPARS ADJACENT TO NO3 RIB.CRACK LENGTH 600MM (23.6IN). 1L71 3O3 O A36EU 1E10 5 NP3EU 20020110000452002011000045SO 2002 1 10 AUS20011137 120011025G3231 BOLT PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL LT MLG DOOR WRONG PART W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) LT MAIN LANDING GEAR TO LANDING GEAR DOOR FORWARD ROD BOLT FAILED. INSPECTION OF REMAINING THREE ATTACHMENT BOLTS FOUND THEM TO BE THE INCORRECT PART. 1L72 3O3 O A20SO E14EA 5 CP33EA 20011204001052001120400105SO 2001 12 4 AUS20011138 120011025G3260 SWITCH PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL LANDING GEAR POSFAULTY W K NONE O OTHER CLCLIMB 1 AUS (AUS) MAIN LANDING GEAR SQUAT SWITCH WIRE BROKEN. 1L72 3O3 O A20SO E14EA 5 CP33EA 20011204001062001120400106CE 2001 12 4 AUS20011139 120011024G5230 HINGE CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C87 GL CARGO/BAGGAGE DOFAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH REAR NOSE BAGGAGE DOOR AFT HINGE FAILED DURING DOOR CLOSURE. DOOR STAY WAS BENT SLIGHTLY. 1L72 3O3 O A7CE E8CE 5 CP22EA 20011204001072001120400107CE 2001 12 4 AUS20011140 120011012G2823SL60043 LEVER CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL FUEL SELECTOR/SHBROKEN W KE NONE ENGINE SHUTDOWN O OTHER NRNOT REPORTED 1 AUS (AUS) FUEL CONDITION LEVER BROKE AT THE LOWER BEND IN THE CONTROL KNOBARM. 1H71 3T3 T A37CE E4EA 5 CP60GL 20020110000462002011000046SO 2002 1 10 AUS20011142 120011022G3250 BOLT PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL NLG STEERING SHEARED W O OTHER W INADEQUATE Q C LDLANDING 1 AUS (AUS) NOSE WHEEL STEERING BRACKET TO NOSE LEG ATTACHMENT BOLTS (2OFF3) SHEARED. INVESTIGATION OF NLG LEG FOUND ONE OF THE BOLTS HOLES WAS FITTED WITH A HELICOIL INSERT. SUSPECT UNAPPROVED PART. 1L72 3O3 O A20SO E14EA 5 CP33EA 20011204001092001120400109SO 2001 12 4 AUS20011144 120011026G28205052012035 TUBE PIPER PA31350 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL AIRCRAFT FUEL DICORRODED W K NONE OK OTHER FLUID LOSS ININSP/MAINT 1 AUS 317652119 (AUS) FUEL CROSSFEED PIPE LOCATED BELOW CABIN FLOOR CORRODED INTERNALLY PRODUCING A SMALL PIN HOLE LEAK. LEAKING FUEL CONTAMINATED THESURROUNDING INSULATION. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020110000482002011000048SO 2002 1 10 AUS20011145 120011028G28446770055 LINE PIPER PA28 PA28161 7102803SO LYC O320 O320* 41508EA AMTR C8289 C8289 GL FUEL PRESS IND FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RIGID COPPER FUEL LINE TO GAUGE FRACTURED. SUSPECT INADEQUATE SUPPORT. 1L71 3O3 O 2A13 E274 5 NEXPP5N 20020110000492002011000049EA 2002 1 10 AUS20011146 120010609G32306A09000097 HOSE DHAV DHC2 DHC2* 2800108EA PWA R985 R985AN1 52008NE HAMSTD2D 2D30 NE FLOAT STRUT FAILED W O OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 AUS (AUS) RT LANDING GEAR HYDRAULIC HOSE CHAFED INSIDE FLOAT STRUT. HOSE BURST. LOSS OF HYDRAULIC FLUID. AIRCRAFT IS A FLOATPLANE. 1H71 3R3 R A806 5E1 5 CP206 20020110000502002011000050CE 2002 1 10 AUS20011148 120011023G53110024300536 FRAME BEECH 58 58 1152740CE CONT O520 IO520C 17032SO FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT EXIT FRAME CRACKED. 1L72 3O3 O 3A16 E5CE 20020110000512002011000051CE 2002 1 10 AUS20011149 120011016G323000241003217 BRACKET BEECH 58 58 1152740CE CONT O520 IO520C 17032SO NLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR ALIGNMENT GUIDE BRACKET CRACKED. 1L72 3O3 O 3A16 E5CE 20020110000522002011000052CE 2002 1 10 AUS20011150 120011016G32339581001723 WORM GEAR BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LANDING GEAR GEARBOX / ACTUATOR HOURS UNKNOWN (2000 HOURS OVERHAUL). LANDING GEAR GEARBOX FOUND TO HAVE NO OIL. GEAR ACTUATOR WORM DRIVE PNO 35-810076-3 FOUND TO HAVE FATIGUE CRACKS (MECHANICAL HANDLE ATTACHMENT END). 1L72 3O3 O 3A16 E5CE 20011204001102001120400110SO 2001 12 4 AUS20011152 120011026G3245 TUBE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL TIRE TUBE PUNCTURED W K NONE O OTHER LDLANDING 1 AUS (AUS) NOSEWHEEL TYRE AND TUBE PUNCTURED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020110000542002011000054SO 2002 1 10 AUS20011153 120011027G3260 SWITCH PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL RT MLG DOWNLOCK STUCK W O OTHER N FALSE WARNING LDLANDING 1 AUS (AUS) RT MAIN LANDING GEAR DOWNLOCK MICROSWITCH STICKING. 1L72 3O3 O A20SO E14EA 5 CP33EA 20011204001112001120400111NE 2001 12 4 AUS20011154 220011012G7230 SEAL LYC LTS101 BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE TURBINE ENGINE CLEAKING W K NONE E VIBRATION/BUFFET CRCRUISE 1 AUS (AUS) ENGINE NO1 CARBON SEAL LEAKING. 1G72 3U3 U H13EU E5NE10 20011204001122001120400112SO 2001 12 4 AUS20011157 220011030G8530646657 STUD CONT TSIO520VB CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C93 GL RECIPROCATING ENMISSING W K NONE E VIBRATION/BUFFET CLCLIMB 1 AUS (AUS) RH ENGINE NO4 CYLINDER EXHAUST STUDS (4OFF) MISSING ALLOWINGEXHAUST GAS TO BE DIRECTED ONTO THE CHT PROBE. 1L72 3O3 O A7CE E8CE 5 CP22EA 20011204001132001120400113EA 2001 12 4 AUS20011158 220011030G7414S4LN200 MAGNETO LYC O360A1D MOONEYM20 M20C 5870208SW LYC O360 O360A1D 41514EA MCAULY2D34C 2D34C53 GL MAGNETO/DISTRIBUFAULTY W K NONE OEROTHER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS ININSP/MAINT 1 AUS 915094919614 (AUS) MAGNETOS INTERMITTENT IN OP. INSP FOU NDFOLLOWING FAULTS ON BOTH UNITS:-1. CAPACITORS FOUND TO LEAKING ELECT.LY.2. SPUR GEAR FOUND TO BE OF NYLON TYPE WHICH HAS BEEN OBSOLETE FOR MANY YRS&REQD AS PER BENDIX MASTER MANUAL TO BE REPL. 3. DISTRIBUTOR BLOCK CONTAMINATED WITH FOREIGN MATERIAL &CRACKS WERE FOUND RADIATING OUT FROM THE ELECTRODES& THERE EVIDENCE OF TRACKING ALONG THESE CRACKS4. INTERNAL TIMING FOUND TO BE SET AT 6 DEGS MOST LIKELY DUE TO CAM FOLLOWER WEAR ON CONTACTS AS CONTACT GAPAT 0.1778MM (0.007IN).THESE VALUES COMPARED TOACCEPTABLE LIMITS OF 10 DEGS +/-2 DEGS&CONTACT GAPOF APPROX 0.4064MM (0. 016IN) SUGGESTS THAT THESE MAGNETOS HAVE NOT BEEN REMVD FOR SOME TIME.01115830- 1L71 3O3 O 2A3 E286 5 CP7EA 20020110000642002011000064EU 2002 1 10 AUS20011160 120011029G29329738114306 SWITCH PILATSPC12 PC12 7090550EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL HYD PRESSURE FAILED W O OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 AUS (AUS) HYDRAULIC PRESSURE SWITCH FAILED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20011204001152001120400115EA 2001 12 4 AUS20011163 220011103G8520L206168A STUD LYC LTIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR2 GL RECIPROCATING ENCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 1723 L206168A (AUS) RH ENGINE CYLINDER HOLDDOWN STUDS CRACKED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020110000652002011000065EU 2002 1 10 AUS20011164 120011106G5302109037043205 STRUCTURE AGUSTAA109 A119 0261102EU TAIL BOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAIL BOOM CRACKED. 1G72 3U H7EU 20020110000662002011000066NE 2002 1 10 AUS20011165 220010210G7321105MK2S REGULATOR BOEING747 747338 NM RROYCERB211 RB211524D41954555NE NR 4 FUEL FLOW FAULTY W O OTHER O OTHER NRNOT REPORTED 1 AUS 2766 (AUS) NR 4 ENGINE FUEL FLOW REGULATOR (FFR) FAULTY. INVESTIGATION FOUND THE CAUSE TO BE FAILURE OF THE VMO QUILLSHAFT CUP WASHER DUE TO HIGH CYCLE FATIGUE. 2L72 4F4 FRTA20WE E12EU 20020110000682002011000068 2002 1 10 AUS20011168 420011105G346009601820038 CAPACITOR MOONEYM20 M20J 5870219SW LYC O360 IO360A3B6 41514EA MCAULY2D34C B2D34C214 GL FLT MANAGEMENT BURNED OUT W O OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 AUS (AUS) NAVCOM CAPACITOR C491 BURNT. 1L71 3O3 O 2A3 1E10 5 CP7EA 20011204001172001120400117SO 2001 12 4 AUS20011169 220011017G8520632018 GEAR CONT IO520M CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL RECIPROCATING ENLOOSE W K NONE OHJOTHER ELECT. POWER LOSS-50 PC WARNING INDICATION ININSP/MAINT 1 AUS 721 811610R (AUS) RH ENGINE ALTERNATOR DRIVE GEAR TO CRANKSHAFT ATTACHMENT BOLTSPNO 649205 LOOSE AND GEAR PNO 632018 LOOSE AND TEETH DAMAGED. ALTERNATOR BEARINGS FAILED. METAL CONTAMINATION OF OIL FILTER. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20020110000692002011000069SW 2002 1 10 AUS20011170 120011101G2710705541 CONTROL ROD AIRTRCAT802 AT802 0390305SW AILERON CONTROL BENT W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AILERON CONTROL ROD BENT. SUSPECT CAUSED BY WIND GUST. 1L71 3T NCA19SW 20020110000702002011000070NM 2002 1 10 AUS20011171 120011106G492038002981 APU BOEING767 767* NM APU BAY FAILED W O OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 AUS 3562 P1022 (AUS) APU FAILED TO START. 2L72 4F RTA1NM 20011204001192001120400119CE 2001 12 4 AUS20011174 120011108G5711 SPAR BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO MCAULY2AF34C2AF34C55 GL WING SPAR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) WING RH FORWARD SPAR WEB CRACKED AROUND BEND RADIUS AND FORWARD FACE. FOUND DURING INSPECTION IAW BEECH SB 2269 REV1 ANDAD/BEECH55/62 AMDT4. 1L72 3O3 ORT3A16 3E1 5 CP5EA 20011204001202001120400120CE 2001 12 4 AUS20011175 120011102G7820125025116 MUFFLER CONT IO520F CESSNA207 207 2073602CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL ENGINE NOISE SUPFAILED W K NONE OEROTHER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS ININSP/MAINT 1 AUS (AUS) RH EXHAUST MUFFLER INTERNAL BAFFLE COLLAPSED PARTIALLY BLOCKING MUFFLER AND CAUSING LOSS OF ENGINE PERFORMANCE. 1H71 3O3 O A16CE E5CE 5 CP47GL 20011204001212001120400121CE 2001 12 4 AUS20011176 120011107G323008411132 SCREW CESSNA 310R CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL LANDING GEAR RETBROKEN W K NONE O OTHER LDLANDING 1 AUS (AUS) RH MAIN LANDING GEAR DOWNLOCK ADJUSTING SCREW FAILED IN THREADEDAREA. RH MLG COLLAPSED. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20020110000782002011000078SO 2002 1 10 AUS20011181 120011009G2140A99100009 COMBUST CHAMBER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL HEATING SYSTEM DISTORTED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HEATER COMBUSTION TUBE DISTORTED IN AREA OF FIRST AIR REVERSAL. SUSPECT CAUSED BY FAILURE OF TUBE MATERIAL TO COPE WITH THE HIGHTEMPERATURE OF THE HEATER. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020110000792002011000079SO 2002 1 10 AUS20011182 220011106G8550 O-RING CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C87 GL ENGINE FAILED W D RETURN TO BLOCK EK VIBRATION/BUFFET FLUID LOSS TXTAXI/GRND HDL 1 AUS (AUS) RT ENGINE UPPER APC OIL FITTING O' RING SEAL FAILED AND LEAKING. 1L72 3O3 O A7CE E8CE 5 CP22EA 20011204001242001120400124SO 2001 12 4 AUS20011183 120011102G8120LH1398RH170 HOUSING CONT TSIO360E PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360E 17025SO HARTZLHCC2Y BHCC2YF2 GL EXHAUST TURBOCHACRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 339 LH1398RH170 (AUS) LH AND RH ENGINE TURBOCHARGER TURBINE HOUSINGS CRACKED. FOUND DURING INSPECTION IAW AD/TURBO/1. LH ENGINE - CONTINENTAL TSIO-360-E - SERIAL NUMBER 307156 TSO 338.6 HOURS - TSLSV 119.6 HOURS RH ENGINE - CONTINENTAL LTSIO-360-E - SERIAL NUMBER 306161TSO 338.6 HOURS - TSLSV 119.6 HOURS 1L72 3O3 O A7SO E9CE 5 CP920 20011204001252001120400125CE 2001 12 4 AUS20011184 120011102G71101019100251 COWLING PWA PT6A41 BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA HARTZLHCB3T HCB3TN3 GL ENGINE COWLING SSEPARATED W K NONE D INFLIGHT SEPARATION CLCLIMB 1 AUS (AUS) LH ENGINE FORWARD UPPER COWL ASSEMBLY SEPARATED IN FLIGHT. PILOTHAD RECENTLY PERFORMED MAINTENANCE ON THE COWL. MINOR DAMAGE TO COWLS AND LEADING EDGE CAUSED BY COWL SEPARATION. PERSONNEL/MAINTENANCE ERROR. 1L72 4T4 T A24CE E4EA 6 CP15EA 20011204001272001120400127EA 2001 12 4 AUS20011186 220011107G8520LW11021 BEARING LYC IO320B1A PIPER PA30 PA30 7103002SO LYC O320 IO320B1A 41508EA HARTZLHCE2Y HCE2YL2 GL RECIPROCATING ENFAILED W K NONE O OTHER ININSP/MAINT 1 AUS 285 L246155A (AUS) CONNECTING ROD BIGEND BEARING MATERIAL SEPARATED FROM BEARING SHELL. 1L72 3O3 O A1EA 1E12 5 CP9EA 20020110000802002011000080SW 2002 1 10 AUS20011187 120011102G6410212010750105 BLADE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE TAIL ROTOR CONTAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS 281 (AUS) TAIL ROTOR BLADE CORE CONTAMINATED WITH WATER. FOUND DURING X-RAY INSPECTION AFTER BLADE WAS UNABLE TO BE BALANCED AND WAS FOUND TO BE 66 GRAMS HEAVIER THAN THE MASTER BLADE. 1G72 4U4 U H4SW E22EA 20020110000812002011000081SO 2002 1 10 AUS20011188 220011107G8530 EXHAUST VALVE CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL ENGINE BURNED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 1 AND NR 3 CYLINDER EXHAUST VALVES BURNED AND ERRODED. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20011204001322001120400132EU 2001 12 4 AUS20011195 120011110G5311 FASTENER BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE FUSELAGE MAIN, FSHEARED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FRAME 29 RH SIDE HILOK FASTENER SHEARED IN AREA ADJACENT TO STRINGER NO11. 2H74 4F4 F A49EU E6NE 20011204001342001120400134CE 2001 12 4 AUS20011197 120011113G5341NAS15035M BOLT BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO MCAULY2AF34C2AF34C55 GL FUSELAGE, WING ACRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) WING ATTACHMENT BOLT CRACKED. FURTHER INVESTIGATION FOUND THATTHE WASHER HAD BEEN INCORRECTLY FITTED WITH THE WASHER BEVELLED EDGE FACING AWAY FROM THE BOLT HEAD. THE WASHER WAS ALSO DAMAGED. FOUND DURING INSPECTION IAW AD/BEECH55/79 AMDT1.PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 ORT3A16 3E1 5 CP5EA 20011204001362001120400136NM 2001 12 4 AUS20011199 120010404G3230BACF8A06EN0700B HOSE BOEING767 767238 1385114NM PWA JT9 JT9D7R4E 52054NE LANDING GEAR RETLEAKING W K NONE OK OTHER FLUID LOSS ININSP/MAINT 1 AUS (AUS) RH MAIN LANDING GEAR TILT ACTUATOR HYDRAULIC HOSE LEAKING. 2L72 4F4 FRTA1NM E3NE 20011204001372001120400137CE 2001 12 4 AUS20011201 120011113G7430A3600 IGNITION SWITCH LYC O360F1A6 CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL IGNITION SWITCHIWORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) IGNITION SWITCH CONTACTS WORN BEYOND LIMITS AS DETAILED INSEB91-5. 1H71 3O3 O 3A17 E286 5 CP7EA 20020110000872002011000087EU 2002 1 10 AUS20011205 120011102G27529787320003 PDU PILATSPC12 PC12 7090550EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL TE FLAPS FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLAP POWER DRIVE UNIT (PDU) FAILED. INTERNAL THERMAL SWITCH TRIPPED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20011204001392001120400139CE 2001 12 4 AUS20011207 120011016G3411 PIPE CESSNA402 402C 207590RCE CONT O520 GTSIO520E 17032SO MCAULY3AF32C3AF32C87 GL PITOT/STATIC SYSCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ALTITUDE ENCODER STATIC PIPE CRACKED. FOUND DURING INSPECTION IAW AD/RAD/43 AND AD/RAD/47. 1L72 3O3 O A7CE E7CE 5 CP22EA 20020110000902002011000090 2002 1 10 AUS20011212 420011104G6122L16694SIA CLAMP BEECH 23 C24R 1151254CE LYC O360 IO360A1B6 41514EA HARTZLHCM2Y HCM2YR GL PROP GOVERNOR MISSING W O OTHER KF FLUID LOSS FLT CONT AFFECTED CRCRUISE 1 AUS 1070 (AUS) PROPELLER GOVERNOR OIL LINE CRACKED AT FLANGE IN AREA OF ATTACHMENT TO THE GOVERNOR. LOSS OF ENGINE OIL CAUSED ENGINE TO SEIZE. INVESTIGATION FOUND THAT THE TWO CLAMPS REQUIRED BYAD/LYC/86 AMDT2 WERE NOT FITTED. PERSONNEL/MAINTENANCE ERROR. 1L71 3O3 O A1CE 1E10 5 CP43GL 20011204001422001120400142SO 2001 12 4 AUS20011213 120011103G7332633869 LINE CONT LTSIO360E PIPER PA34 PA34200T 7103406SO CONT O360 LTSIO360E 17025SO HARTZLHCC2Y BHCC2YF2 GL FUEL PRESSURE INCRACKED W K NONE ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 AUS 1513 304379 (AUS) RH ENGINE FUEL PUMP SENSE LINE CRACKED APPROXIMATELY 10MM (0.393IN) FROM THE FLARED END. 1L72 3O3 O A7SO E9CE 5 CP920 20020110000912002011000091SO 2002 1 10 AUS20011214 120011101G3233452729 BEARING PIPER PA28 PA28R201 7102816SO CONT IO360 IO360* 17025CE MCAULY2D34C B2D34C213 GL MLG ACTUATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR ACTUATOR BEARING CRACKED AND BROKEN. 1L71 3O3 O 2A13 E1CE 5 CP7EA 20011204001432001120400143CE 2001 12 4 AUS20011215 120010903G323312810013 ACTUATOR CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL LANDING GEAR ACTCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH AND RH MAIN LANDING GEAR ACTUATOR BODIES CRACKED IN AREA INDICATED BY SEB 01-2 FIG1 PAGE4. 1H71 3O3 O 3A17 E286 5 CP7EA 20011204001442001120400144CE 2001 12 4 AUS20011216 120010903G323024411001 PIVOT CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL LANDING GEAR RETCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH AND RH MAIN LANDING GEAR PIVOT ASSEMBLIES CRACKED IN INSPECTION AREA 1B OF SEB 90-1 REV3. 1H71 3O3 O 3A17 E286 5 CP7EA 20011204001452001120400145CE 2001 12 4 AUS20011219 120011106G321312412021 FITTING CESSNA207 207 2073602CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL MAIN LANDING GEACRACKED W K NONE O OTHER LDLANDING 1 AUS (AUS) RH MAIN LANDING GEAR FITTING CRACKED AND RUBBING ON BRAKE DISC. 1H71 3O3 O A16CE E5CE 5 CP47GL 20011204001462001120400146SO 2001 12 4 AUS20011220 120011030G2810 VALVE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL FUEL STORAGE MISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH MAIN FUEL CELL RH FLAPPER VALVE DOOR MISSING. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020110000972002011000097SO 2002 1 10 AUS20011221 120011110G3230 LANDING GEAR PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL NOSE OUT OF ADJ W O OTHER N FALSE WARNING CLCLIMB 1 AUS (AUS) NOSE LANDING GEAR OUT OF ADJUSTMENT. NLG NOT COMPLETELY ENGAGING WITH UPLOCK HOOK DURING RETRACTION. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020110000982002011000098SO 2002 1 10 AUS20011222 120011111G3260487862 SWITCH PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL NLG UPLOCK INTERMITTENT W O OTHER N FALSE WARNING CLCLIMB 1 AUS (AUS) NOSE LANDING GEAR UPLOCK MICROSWITCH INTERMITTENT IN OPERATION. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020110001022002011000102WP 2002 1 10 AUS20011224 220011112G726111405700182 HOUSING CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL OIL PUMP CRACKED W O OTHER EK VIBRATION/BUFFET FLUID LOSS CRCRUISE 1 AUS 333 (AUS) ENGINE OIL PUMP HOUSING CRACKED. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20011204001482001120400148CE 2001 12 4 AUS20011225 120011120G5741082255014 FITTING CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL WING, FUSELAGE ACORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH WING UPPER FORWARD ATTACHMENT FITTING CONTAINED INTERGRANNULAR CORROSION IN THE UPPER SURFACES AND TWO AREAS OF PITTINGCORROSION. FOUND DURING INSPECTION IAW AD/C310/53. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20020110001032002011000103NE 2002 1 10 AUS20011226 220011113G7200 ENGINE BEECH 200 B200C 1152924CE PWA PT6 PT6A42 52043NE NACELLE MALFUNCTIONED W O OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 AUS (AUS) NEWLY INSTALLED ENGINE FAILED TO CORRECTLY CONTROL PROPELLER. 1L72 4T4 T A24CE E4EA 20011204001492001120400149CE 2001 12 4 AUS20011227 120011108G53120512187 BULKHEAD CESSNA172 172M 2072418CE LYC O320 O320E2H 41508EA MCAULY1C160 1C160DTM GL FUSELAGE MAIN, BCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) BULKHEAD CRACKED. FOUND DURING INSPECTION IAW CESSNA SEB 97-1 AND AAC 1-95. 1H71 3O3 ONT3A12 E274 5 NP910 20020114000072002011400007CE 2002 1 14 AUS20011228 120011119G270105131822 WHEEL CESSNA172 172D 2072410CE CONT O300 O300C 17022SO MCAULY1C172 1C172EM GL CONTROL COLUMN FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 AUS (AUS) PILOTS CONTROL WHEEL BROKE INTO SEVERAL PIECES. INVESTIGATION FOUND THE COPILOTS CONTROL WHEEL CRACKED BEYOND LIMITS. 1H71 3O3 ONT3A12 E253 5 NP910 20020114000082002011400008GL 2002 1 14 AUS20011230 320011119G6114C471698 HUB CESSNA188 A188A 2073008CE MCAULY2A34C D2A34C98 GL PROPELLER CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PROPELLER HUB CRACKED IN AREA OF NR 1 BLADE SOCKET. FOUND DURING EDDY CURRENT INSPECTION. 1L71 3O A9CE 5 CP3EA 20011204001522001120400152SO 2001 12 4 AUS20011237 120011108G55414006805 SPAR PIPER PA31 PA31 7103102SO LYC O540 TIO540A2B 41532EA HARTZLHCE3Y HCE3YR2 GL RUDDER, SPAR/RIBCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RUDDER FORWARD SPAR CRACKED. FOUND DURING INSPECTION IAWAD/PA31/129. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020114000132002011400013GL 2002 1 14 AUS20011238 220011114G72306858348 BLADE HUGHES369 369HS 4470728WP ALLSN 250C 250C18 03011GL COMPRESSOR FAILED W O OTHER E VIBRATION/BUFFET TOTAKEOFF 1 AUS 1483 (AUS) SECOND STAGE COMPRESSOR BLADES (2OFF) FAILED). MAJOR DOWNSTREAM DAMAGE. SEVERAL OTHER SECOND STAGE ROTOR BLADES WERE FOUND TO BECRACKED FROM THE TRAILING EDGE. 1G71 3U3 U H3WE E4CE 20020114000142002011400014CE 2002 1 14 AUS20011239 120011121G32976508012202 WIRE HARNESS CESSNA500 S550 2076607CE PWA JT15 JT15D1 52060NE MLG INTERMITTENT W O OTHER N FALSE WARNING LDLANDING 1 AUS (AUS) LT ANTISKID TRANSDUCER WIRING HAD AN INTERMITTENT FAULT. NO BRAKING DURING LANDING RESULTED IN EMERGENCY BRAKING SYSTEM OPERATION. RH TYRE FAILED DUE TO WHEEL SKIDDING. RT MAIN WHEEL HUB ALSO DAMAGED. 1L72 4F4 FRTA22CE E1NE 20011204001532001120400153CE 2001 12 4 AUS20011241 120011109G5412402B0622 BEAM CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C93 GL NACELLE/PYLON, BCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS 402B0622 (AUS) ENGINE BEAMS AND CANTED BULKHEADS CORRODED BEYOND LIMITS. FOUND DURING NDT INSPECTION. 1L72 3O3 O A7CE E8CE 5 CP22EA 20011204001542001120400154CE 2001 12 4 AUS20011242 120011109G3221584200111 TRUNNION CESSNA 402B CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C93 GL NOSE/TAIL LANDINCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 402B0622 (AUS) NOSE LANDING GEAR TRUNNION CRACKED. 1L72 3O3 O A7CE E8CE 5 CP22EA 20011204001552001120400155SO 2001 12 4 AUS20011243 220010914G85206419311075 BOLT CONT IO520M CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL RECIPROCATING ENBROKEN W K NONE E VIBRATION/BUFFET CRCRUISE 1 AUS 637 574058 (AUS) LH ENGINE CRANKCASE THOUGH BOLT BROKEN. SEE ALSO MDR 01/1244. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20011204001562001120400156SO 2001 12 4 AUS20011244 220010914G85206461401 STUD CONT IO520M CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL RECIPROCATING ENBROKEN W K NONE E VIBRATION/BUFFET CLCLIMB 1 AUS 574058 (AUS) LH ENGINE CYLINDER HOLDDOWN STUD BROKEN. CRANKCASE CRACKED. SEE ALSO MDR 01/1243. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20011204001572001120400157NE 2001 12 4 AUS20011245 220011001G7321164448480 FCU TMECA 164448480 SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE FUEL CONTROL/TURFAULTY W K NONE OK OTHER FLUID LOSS ININSP/MAINT 1 AUS A444B (AUS) FUEL CONTROL UNIT LEAKING. FUEL LEAKING FROM FCU DRAIN WITH BOOST PUMP ON AND ENGINE NOT RUNNING. 1G71 3U3 U H9EU E19EU 20011204001582001120400158NE 2001 12 4 AUS20011246 220011003G7321164448480 FCU TMECA 164448480 SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE FUEL CONTROL/TURFAULTY W K NONE E VIBRATION/BUFFET NRNOT REPORTED 1 AUS 8 98B (AUS) FCU FAULTY. ENGINE HUNG ON START. 1G71 3U3 U H9EU E19EU 20020114000172002011400017 2002 1 14 AUS20011250 420011123G2561P0640101 LIFE VEST CABIN MISMARKED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) OVERHAULED LIFE JACKETS INCORRECTLY MARKED. LIFE JACKETS ARE EITHER INFANT OR ADULT FIT ITEMS BUT ARE ALL MARKED ON THE OUTSIDE OF THE STORAGE BAGS AS KSE-35L8 WHICH ARE ADULT FIT ITEMS. THE INFANT FIT JACKETS SHOULD BE MARKED P0640.101. THE INCORRECT MARKING ON THE STORAGE BAGS COULD RESULT IN THE INCORRECT ITEM BEING USED IN AN EMERGENCY. THE OVERHAUL FACILITYHAS BEEN NOTIFIED AND WILL CORRECTLY MARK ALL LIFE JACKETS FROM NOW ON. INCORRECTLY MARKED LIFE JACKETS IN THE SYSTEM WILL BE IDENTIFIED AND CORRECTLY MARKED BY MAINTENANCE. 20011204001602001120400160WP 2001 12 4 AUS20011251 120011119G3213269A3150 DAMPER HUGHES269 269C 4470504WP LYC O360 HIO360D1A 41514EA MAIN LANDING GEALOOSE W K NONE O OTHER LDLANDING 1 AUS (AUS) LH REAR LANDING GEAR DAMPER UPPER CAP UNSCREWED AND SEPARATED FROM PISTON. SUSPECT CAUSED BY VIBRATION. 1G71 3O3 O 4H12 1E10 20011204001612001120400161SO 2001 12 4 AUS20011252 120011113G32309564308 BRACKET PIPER PA44 PA44180 7104402SO LYC O360 O360E1A6 41514EA HARTZLHCC3Y HCC3YR2 NE LANDING GEAR RETCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH MAIN LANDING GEAR DOWNLOCK BRACKET CRACKED. 1L72 3O3 O A19S0 E286 5 CP25EA 20011204001622001120400162EA 2001 12 4 AUS20011253 220011113G8520LW16508 CAMSHAFT LYC O360E1A6 PIPER PA44 PA44180 7104402SO LYC O360 O360E1A6 41514EA HARTZLHCC3Y HCC3YR2 NE RECIPROCATING ENUNSERVICEABLE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH ENGINE CAMSHAFT NO1 AND NO4 TAPPETS UNSERVICEABLE. FOUND DURING INSPECTION IAW PIPER MSB 446D. 1L72 3O3 O A19S0 E286 5 CP25EA 20011204001632001120400163SO 2001 12 4 AUS20011254 120011113G57127847506 RIB PIPER PA44 PA44180 7104402SO LYC O360 O360E1A6 41514EA HARTZLHCC3Y HCC3YR2 NE WING, RIB/BULKHECRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) WING RIB CRACKED. RIB SUPPORTS UNDERCARRIAGE DOWNLOCK. 1L72 3O3 O A19S0 E286 5 CP25EA 20011204001642001120400164SO 2001 12 4 AUS20011255 120011113G57127847507 RIB PIPER PA44 PA44180 7104402SO LYC O360 O360E1A6 41514EA HARTZLHCC3Y HCC3YR2 NE WING, RIB/BULKHECRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) WING RIB CRACKED. RIB SUPPORTS UNDERCARRIAGE DOWNLOCK. 1L72 3O3 O A19S0 E286 5 CP25EA 20011204001652001120400165SO 2001 12 4 AUS20011256 120011113G32309564309 BRACKET PIPER PA44 PA44180 7104402SO LYC O360 O360E1A6 41514EA HARTZLHCC3Y HCC3YR2 NE LANDING GEAR RETCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RH MAIN LANDING GEAR UPLOCK BRACKET CRACKED. 1L72 3O3 O A19S0 E286 5 CP25EA 20020114000182002011400018CE 2002 1 14 AUS20011257 120011030G275245521212607 ACTUATOR BEECH 58 58 1152740CE CONT O520 IO520C 17032SO TE FLAP MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT WING FLAP ACTUATOR INCORRECTLY INSTALLED. 1L72 3O3 O 3A16 E5CE 20020114000192002011400019CE 2002 1 14 AUS20011258 120011030G572000243002027 FITTING BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MLG ACTUATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LANDING GEAR ACTUATOR SUPPORT FITTING CRACKED. 1L72 3O3 O 3A16 E5CE 20020114000202002011400020CE 2002 1 14 AUS20011259 120011030G323345521212604 ACTUATOR BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MLG ACTUATOR MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) LT MAIN LANDING GEAR ACTUATOR INCORRECTLY FITTED. 1L72 3O3 O 3A16 E5CE 20020114000212002011400021CE 2002 1 14 AUS20011260 120011105G2752355212133 ATTACH FITTING BEECH 58 58 1152740CE CONT O520 IO520C 17032SO TE FLAP ACTUATORCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS 204 (AUS) TRAILING EDGE FLAP ACTUATOR INTERNALLY CORRODED. ATTACHMENT LUG ALSO CORRODED. 1L72 3O3 O 3A16 E5CE 20020114000222002011400022CE 2002 1 14 AUS20011261 120011105G27523536415157 BRUSH HOLDER BEECH 58 58 1152740CE CONT O520 IO520M 17032SO TE FLAP ACTUATORCRACKED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS 120 (AUS) TRAILING EDGE FLAP ACTUATOR MOTOR BRUSH HOLDER ASSEMBLIES CRACKED. EXCESSIVE HEAT THROUGH FIELD WINDINGS. INSUFFICIENT GREASE OF INCORRECT TYPE IN GEARBOX ASSEMBLY. UNAPPROVED PART. 1L72 3O3 O 3A16 E5CE 20020114000232002011400023CE 2002 1 14 AUS20011262 120011105G2520 SEAT BEECH 58 58 1152740CE CONT O520 IO520C 17032SO PASSENGER COMPARUNSERVICEABLE W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) CABIN SEATS UNSERVICEABLE. PARTS MISSING. REAR SEAT LUMBAR SUPPORTS CRACKED. VARIOUS SEAT ASSEMBLIES MODIFIED. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O 3A16 E5CE 20020114000242002011400024CE 2002 1 14 AUS20011263 120011105G2820002920000191 LINE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO FUEL DIST CHAFED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) FUEL CROSSFEED LINE LOCATED IN RT WHEEL BAY CHAFING ON UNDERCARRIAGE DOWNLOCK BACKUP CABLE. SUSPECT LINE INADEQUATELY SECURED. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O 3A16 E5CE 20020114000252002011400025CE 2002 1 14 AUS20011264 120011105G282000292000077 LINE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO FUEL DIST CHAFED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) CROSSFEED FUEL LINE LOCATED IN LT WHEEL WELL CHAFING ON UNDERCARRIAGE ACTUATOR CONTROL ROD. THE FUEL LINE HAD BEEN COVERED WITH A PLASTIC SLEEVE AFTER THE DAMAGE HAD OCCURRED. SUSPECT CAUSED BY INADEQUATE SECURING OF FUEL LINE. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O 3A16 E5CE 20020114000262002011400026CE 2002 1 14 AUS20011266 120011123G3297 WIRE CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL MLG DOWNLOCK MISINSTALLED W A UNSCHED LANDING WN INADEQUATE Q C FALSE WARNING CLCLIMB 1 AUS (AUS) RT MAIN LANDING GEAR DOWNLOCK MICROSWITCH WIRING INCORRECTLY ROUTED CAUSING A STRAIN ON THE MICROSWITCH. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20020114000272002011400027EU 2002 1 14 AUS20011267 120011123G3233C243532 ACTUATOR SNIAS AS332 AS332L 8680809EU TMECA MAKILAMAKILA1A 60040EU RT MLG LEAKING W O OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 AUS 7803 (AUS) RT MAIN LANDING GEAR ACTUATOR HYDRAULIC UNIT FAULTY. 2G72 4U4 U H4EU E12NE 20011204001662001120400166EA 2001 12 4 AUS20011268 220011122G73105011849 PIPE PWA PT6A34 EMB 110 EMB110P2 3260124SO PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL ENGINE FUEL DISTCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PIPE LOCATED BETWEEN FCU AND START CONTROL VALVE CRACKED AT FITTING. 1L72 4T4 T A21SO E4EA 6 CP15EA 20020104000402002010400040CE 2002 1 4 AUS20011271 120011119G2731455260053 SPROCKET BEECH 55 E55 1152732CE CONT O520 IO520C 17032SO MCAULY3AF32C3AF32C75 GL ELEVATOR TAB CONWORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELEVATOR TRIM TAB ACTUATOR SPROCKET SHAFT BADLY WORN. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20020104000412002010400041NE 2002 1 4 AUS20011272 120011129G32607655200904045 WIRE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE LANDING GEAR POSBROKEN W K NONE ON OTHER FALSE WARNING DEDESCENT 1 AUS (AUS) RH MAIN LANDING GEAR DOWNLOCK SENSOR HARNESS WIRE BROKEN. 1G72 3U3 UNCH1NE E19EU 20020114000302002011400030CE 2002 1 14 AUS20011273 120011006G3246 PANEL CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL FLOAT COVER SEPARATED W O OTHER DF INFLIGHT SEPARATION FLT CONT AFFECTED NRNOT REPORTED 1 AUS (AUS) RIGHT HAND FLOAT HATCH COVER SEPARATED IN FLIGHT. THE COVER CONTACTED THE RIGHT HAND TAILPLANE CAUSING CONSIDERABLE DAMAGE AND CONTROL PROBLEMS. VIBRATION CAUSED FAILURE OF SEVERAL HYDRAULIC LINES IN THE RIGHT HAND FLOAT. LOSS OF HYDRAULIC FLUID THEN LEAD TO ONLY PARTIAL LANDING GEAR EXTENSION. 1H71 3O3 O A4CE E5CE 5 CP47GL 20020114000352002011400035 2002 1 14 AUS20011279 420011023G3414610400106 INDICATOR CESSNA340 340CESSNA 2076404CE CONT O520 TSIO520K 17040SO MCAULY3AF32C3AF32C93 GL AIRSPEED READS HIGH W A UNSCHED LANDING O OTHER CLCLIMB 1 AUS (AUS) AIRSPEED INDICATOR FAULTY. INDICATOR WAS READING 180 KNOTS WHEN THE AIRCRAFT WAS STATIONARY. PITOT AND STATIC LINES CHECKED WITH NO FAULTS. ARTIFICIAL HORIZON ALSO TOPPLING IN FLIGHT. 1L72 3O3 O 3A25 E8CE 5 CP22EA 20020114000362002011400036SW 2002 1 14 AUS20011280 120011129G2720472105 CONTROL CABLE GULSTM112 114 7630314SW LYC O540 IO540T4B5 41532EA HARTZLHCC2Y HCC2YR1 GL RUDDER MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) LT RUDDER CONTROL CABLE INCORRECTLY ROUTED UNDER SUPPORT BRACKET. CABLE RUBBING ON PULLEY SUPPORT BRACKET. ELEVATOR TRIM CABLE ALSO INCORRECTLY ROUTED AND FOULING ON STRUCTURE. PERSONNEL/MAINTENANCE ERROR. 1L71 3O3 O A12SO 1E4 5 CP920 20020104000432002010400043EU 2002 1 4 AUS20011281 120011127G3240 BRAKE PARTENP68 P68B 6780104EU LYC O360 IO360A1B6 41514EA HARTZLHCC2Y HCC2YK2 GL LANDING GEAR BRAMISSING W K NONE OC OTHER F.O.D. TXTAXI/GRND HDL 1 AUS (AUS) AIRCRAFT NOSE SPAT AND PITOT TUBE DAMAGE WHEN AIRCRAFT RAN INTO THE SIDE OF THE HANGAR WHILE BEING TAXIED FOR REFUELLING. INVESTIGATION FOUND THAT THE PILOT WAS SITTING IN THE RH SEAT AND THAT THE BRAKES HAD BEEN REMOVED FROM THE RH SIDE POSITION. THE REMOVAL OF THE BRAKES HAD NOT BEEN PLACARDED. PERSONNEL/MAINTENANCE ERROR. 1H72 3O3 O A31EU 1E10 5 CP920 20020104000442002010400044NM 2002 1 4 AUS20011282 120011124G28205324 VALVE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C 13802EU AIRCRAFT FUEL DIFOD W K NONE O OTHER CRCRUISE 1 AUS 5324 (AUS) FUEL SYSTEM NON-RETURN VALVE JAMMED OPEN BY FOD CAUSING A FUELIMBALANCE BETWEEN NO1 AND NO2 TANKS. INVESTIGATION FOUND APLASTIC BLANK WAS JAMMING THE VALVE OPEN. SUSPECT FOD WAS A BLANKING CAP FROM BOOST PUMP PRESSURE LINE. BOOST PUMP HAD BEEN REPLACED PRIOR TO RECEIPT BY VIRGIN BLUE. PERSONNEL/MAINTENANCE ERROR. FOD. 2L72 4F4 FRTA16WE E21EU 20020114000372002011400037SO 2002 1 14 AUS20011283 120011203G522040979 DOOR PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL EMERGENCY EXITS SEPARATED W A UNSCHED LANDING DJ INFLIGHT SEPARATION WARNING INDICATION CLCLIMB 1 AUS (AUS) CABIN EMERGENCY EXIT DOOR SEPARATED FROM AIRCRAFT. INVESTIGATIONOF THE LATCH MECHANISM FOUND THAT THE LATCH HAD NOT BEEN FULLY ENGAGING FOR A CONSIDERABLE TIME. LATCHES HAD ONLY BEEN CLOSING APPROXIMATELY 30 DEGREES INSTEAD OF THE FULL 90 DEGREES. CLOSEINSPECTION OF THE HANDLE ASSEMBLY SHOWED THAT IT WAS BENT IN THEAREA WHERE THE VERTICAL TUBE IS WELDED TO THE BELLCRANK CROSSTUBE RESULTING IN LIMITED TRAVEL OF THE DOOR LATCHES. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020114000452002011400045SO 2002 1 14 AUS20011293 220011129G8530 EXHAUST VALVE CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL NR 1 CYLINDER LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 1 CYLINDER EXHAUST VALVE LEAKING PAST VALVE SEAT. 1H71 3O3 O A4CE E5CE 5 CP21EA 20020104000472002010400047EU 2002 1 4 AUS20011294 120011209G2120 COOLING FAN REIMS 406 F406 7535723EU PWA PT6 PT6A112 52043NE MCAULY3G34C73GFR34C701 GL AIR DISTRIBUTIONFAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS (AUS) SURVEILLANCE RADAR COOLING FAN FAILED. 1L72 3T3 TRTA54EU E4EA 5 CP60GL 20020104000482002010400048EU 2002 1 4 AUS20011298 120010904G31501097811 WARNING SYSTEM FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU CENTRAL WARNING FAULTY W K NONE FN FLT CONT AFFECTED FALSE WARNING TOTAKEOFF 1 AUS (AUS) UNSAFE CONFIGURATION WARNING SOUNDED. INVESTIGATION COULD FIND NO CAUSE FOR THE PROBLEM. LH ELEVATOR BYPASS SWITCH CHANGED AS A PRECAUTION. 2L72 4F4 FRTA20EU E2EU 20020104000512002010400051EA 2002 1 4 AUS20011304 220011203G7322229164 NOZZLE LYC O320H2AD CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA MCAULY1C160 1C160DTM GL FUEL CONTROL/RECMISSING W K NONE ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AUS 501 CK10488V (AUS) CARBURETTOR DISCHARGE NOZZLE MISSING. 1H71 3O3 ONT3A12 E274 5 NP910 20020114000552002011400055EU 2002 1 14 AUS20011309 120011206G2731 ACTUATOR REIMS 406 F406 7535723EU PWA PT6 PT6A112 52043NE MCAULY3G34C73GFR34C701 GL ELEVATOR TAB CONTAMINATED W O OTHER W INADEQUATE Q C NRNOT REPORTED 1 AUS (AUS) ELEVATOR TRIM TAB ACTUATORS LUBRICATED WITH THE INCORRECT GREASE. ACTUATORS FREEZING IN FLIGHT. MAINTENANCE MANUAL SPECIFIES "TRIBOLUBE" ONLY. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART. 1L72 3T3 TRTA54EU E4EA 5 CP60GL 20020104000542002010400054EU 2002 1 4 AUS20011310 120011206G5343571304013 CHANNEL REIMS 406 F406 7535723EU PWA PT6 PT6A112 52043NE MCAULY3G34C73GFR34C701 GL LANDING GEAR ATTCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR ACTUATOR ATTACHMENT STRUCTURE CHANNEL CRACKED.FOUND DURING INSPECTION IAW AD/F406/7. 1L72 3T3 TRTA54EU E4EA 5 CP60GL 20020114000562002011400056NE 2002 1 14 AUS20011311 220011206G7420 IGNITION LEAD REIMS 406 F406 7535723EU PWA PT6 PT6A112 52043NE MCAULY3G34C73GFR34C701 GL RT ENGINE CHAFED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT IGNITER LEAD ON BOTH ENGINES CHAFING ON FUEL LINE TO FLOW DIVIDER. 1L72 3T3 TRTA54EU E4EA 5 CP60GL 20020104000552002010400055WP 2002 1 4 AUS20011318 120011211G6310269A55177 BRACKET HUGHES269 269C 4470504WP LYC O360 HIO360D1A 41514EA ENGINE/TRANSMISSCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LOWER DRIVE PULLEY SUPPORT BRACKET CRACKED. ONE ATTACHMENT LUGSEPARATED. 1G71 3O3 O 4H12 1E10 20020104000562002010400056CE 2002 1 4 AUS20011319 120011211G7810265401415 EXHAUST PIPE PWA PT6A114A CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL ENGINE COLLECTORCRACKED W K NONE B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 AUS PCE19248 (AUS) ENGINE PRIMARY EXHAUST DUCT CRACKED AND HOLED. HOLE WAS APPROXIMATELY228.6MM (9IN) BY 146MM (5.75IN). ESCAPING EXHAUSTGAS DAMAGED OIL COOLER SHROUD RUBBERS AND DISCOLOURED THE PAINT ON THE LOWER RH COWL. 1H71 3T3 T A37CE E4EA 5 CP60GL 20020114000612002011400061NE 2002 1 14 AUS20011320 220011209G7420CH5339907 IGNITION LEAD BEECH 200 B200C 1152924CE PWA PT6 PT6A42 52043NE ENGINE SHORTED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) IGNITER LEAD INSULATION SHORT. 1L72 4T4 T A24CE E4EA 20020114000622002011400062EU 2002 1 14 AUS20011324 120010811G2421 WARNING SYSTEM FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU AC GENERATOR FALSE ACTIVATIONW A UNSCHED LANDING N FALSE WARNING CRCRUISE 1 AUS (AUS) NR 2 GENERATOR HIGH INLET TEMPERATURE. INVESTIGATION COULD FIND NO CAUSE FOR THE PROBLEM. PLUGS AND CONNECTORS CLEANED. 2L72 4F4 FRTA20EU E2EU 20020114000662002011400066NM 2002 1 14 AUS20011330 120011123G6210 BLADE ROBSINR22 R22MARINER 7640115NM LYC O320 O320B2C 41508EA MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN ROTOR BLADES SUSPECT CRACKED. 1G71 3O3 O H10WE E274 20020104000592002010400059EA 2002 1 4 AUS20011331 220010903G741410357584 GEAR LYC O320B2C ROBSINR22 R22BETA 7640110NM LYC O320 O320B2C 41508EA MAGNETO/DISTRIBUBROKEN W K NONE O OTHER ININSP/MAINT 1 AUS 400 (AUS) MAGNETO GEAR TEETH BROKEN. 1G71 3O3 O H10WE E274 20020114000672002011400067CE 2002 1 14 AUS20011336 120011210G24507270530 CIRCUIT BREAKER CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL AC DISTRIBUTION FAILED W O OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 AUS (AUS) NR 1 AVIONICS BUS CIRCUIT BREAKER/SWITCH INTERNAL FAILURE. 1H71 3T3 T A37CE E4EA 5 CP60GL 20020114000682002011400068CE 2002 1 14 AUS20011337 120011211G2820314200 VALVE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO FUEL DIST CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUEL SYSTEM CHECK VALVE EXCESSIVELY CORRODED AND CONTAMINATED DUE TO WATER IN FUEL CROSSFEED LINE. 1L72 3O3 O 3A16 E5CE 20020114000692002011400069CE 2002 1 14 AUS20011338 120011211G282060292000031 LINE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO FUEL DIST CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUEL LINE EXCESSIVELY COORODED DUE TO WATER CONTAMINATION. 1L72 3O3 O 3A16 E5CE 20020114000702002011400070CE 2002 1 14 AUS20011340 120011211G245070HF10 DIODE BEECH 200 B200C 1152924CE PWA PT6 PT6A42 52043NE AC POWER DIST FAILED W O OTHER G MULTIPLE FAILURE TXTAXI/GRND HDL 1 AUS (AUS) NR 2 BUS SYSTEM FEED DIODES FAILED. 1L72 4T4 T A24CE E4EA 20020114000712002011400071SO 2002 1 14 AUS20011341 120011214G5342553266 BOLT PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360E 17025SO HARTZLHCC2Y BHCC2YF2 GL HORIZONTAL STABBROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) STABILISER ATTACHMENT FITTING BOLTS BENT (2OFF) AND BROKEN(2OFF). INVESTIGATION FOUND THAT THE BOLTS WERE THE INCORRECT TYPE. THE PART NUMBER OF THE INCORRECT BOLTS WAS PNO NAS425-3-7.UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O A7SO E9CE 5 CP920 20020114000752002011400075SO 2002 1 14 AUS20011347 220011211G8530639272P1O CYLINDER BEECH 55 95C55 1152708CE CONT O520 IO520C 17032SO MCAULY3AF32C3AF32C75 GL RT ENGINE SEPARATED W A UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 AUS 456 (AUS) RT ENGINE NR 4 CYLINDER AND PISTON SEPARATED IN FLIGHT. RT ENGINE COWL SEPARATED ALONG HINGE. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20020114000782002011400078NE 2002 1 14 AUS20011350 120011212G62107615009000046 BLADE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN ROTOR BLADE CRACKED. 1G72 3U3 U H1NE E1GL 20020104000672002010400067EA 2002 1 4 AUS20011357 220011214G7414104001678 CAM BENDIX S6LN1227 BNORM BN2 BN2A20 1520220EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL MAGNETO/DISTRIBUFAILED W K NONE O OTHER ININSP/MAINT 1 AUS C0891 (AUS) MAGNETO CAM PIVOT PIN HAD EXCESSIVE PLAY. PIN HAD APPROXIMATELY 0.508MM (0.020IN) OF PLAY. MAXIMUM PLAY 0.3556MM (0.014IN). 1H72 3O3 O A17EU 1E4 5 CP920 20020114000852002011400085CE 2002 1 14 AUS20011361 120011213G3260574122215 HOOK CESSNA441 441 2076020CE LT MLG UPLOCK FAILED W C ABORTED TAKEOFF O OTHER TOTAKEOFF 1 AUS (AUS) LT MAIN LANDING GEAR UPLOCK HOOK FAILED AT PIVOT POINT. 1L72 3T RTA28CE 20020114000882002011400088 2002 1 14 AUS20011365 420011218G2350IU396002 AUDIO PANEL DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA HARTZLHCB3T HCB3TN3 GL COCKPIT FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS 1446 (AUS) AUDIO PANEL FAILED. SUSPECT INTERNAL TRANSFORMER BURNT. 1H72 3T4 TRTA9EA E4EA 6 CP15EA 20020114000892002011400089EU 2002 1 14 AUS20011366 120011121G5523BURKLIN12H3668 CAP GROB G115 G115C 1660303EU LYC O360 O360A1F6 41514EA HARTZLHCF2Y HCF2YR1 GL ELEVATOR DISLODGED W O OTHER F FLT CONT AFFECTED LDLANDING 1 AUS (AUS) ELEVATOR BALANCE HORN BLANKING CAP DISLODGED AND RESTRICTED ELEVATOR MOVEMENT. FOD. 1L71 3O3 ONTA57EU E286 5 CP27EA 20020114000912002011400091EA 2002 1 14 AUS20011369 220011218G8530IO540K1B5 ROCKER GIPPLDGA200 GA200 EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YR1 GL ENGINE MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS (AUS) ENGINE ROCKER COVER GASKETS INCORRECTLY FITTED. FOLLOWING REMOVAL OF THE ROCKER COVERS IT WAS FOUND THAT THE ROCKERS WERE ALSO INCORRECTLY FITTED. SOME INLET ROCKERS WERE FITTED TO EXHAUST POSITIONS AND VICE VERSA. NR 5 CYLINDER EXHAUST VALVE ALSO HAD EXCESSIVE CLEARANCE OF 3.2MM (0.126IN) WHEN THE RECOMMENDED CLEARANCE WAS BETWEEN 0.711MM (0.028IN) AND 2.032MM (0.080IN).THE ENGINE HAD JUST BEEN RECEIVED FROM OVERHAUL AND WAS BEING BUILT UP TO QEC STATUS. PERSONNEL/MAINTENANCE ERROR. 1L71 3O3 ONCA00001LA1E4 5 CP920 20020205001502002020500150EA 2002 2 5 AUS20011373 220011218G8520SL13885M10 BEARING LYC IO720B1B GULSTM680 680FL 0141608SW LYC O720 IO720B1B 41546EA HARTZLHCB3Z HCB3Z302 GL RECIPROCATING ENDELAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE NO1 MAIN BEARING DELAMINATED. METAL CONTAMINATION OF OIL FILTER. 1H72 3O3 O 2A4 1E15 5 CP907 20020205001522002020500152SO 2002 2 5 AUS20011375 120011219G3213AN3104 NUT PIPER PA34 PA34200 7103405SO LYC O360 IO360C1E6 41514EA HARTZLHCC2Y HCC2YK2 GL MAIN LANDING GEAMISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH MAIN LANDING GEAR TORQUE LINK CONNECTING BOLT NUT MISSING. 1L72 3O3 O A7SO 1E10 5 CP920 20020205001532002020500153SO 2002 2 5 AUS20011376 220011219G7414103493504 MAGNETO CONT IO520F CESSNA207 207 2073602CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL MAGNETO/DISTRIBUWORN W K NONE O OTHER ININSP/MAINT 1 AUS 807 (AUS) RH MAGNETO COUPLING PINS WORN EXCESSIVELY. 1H71 3O3 O A16CE E5CE 5 CP47GL 20020205001542002020500154SO 2002 2 5 AUS20011378 120011214G32136531904 CYLINDER PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA SNSNCH74D 74DM EA MAIN LANDING GEABROKEN W K NONE O OTHER LDLANDING 1 AUS (AUS) AFTER A HEAVY LANDING THE LH LANDING GEAR WAS FOUND TO BE LOWER THAN THE RH GEAR AND SITTING AT AN ODD ANGLE. INVESTIGATION FOUND THAT THE LH MAIN LANDING GEAR CYLINDER TORQUE LINK ATTACHMENT LUGS BROKEN OFF. 1L71 3O3 O 2A13 E274 5 NP88614 20020205001552002020500155EA 2002 2 5 AUS20011379 220011212G8520LW11021 BEARING LYC IO540E1B5 GULSTM500 500U 0141108SW LYC O540 IO540E1B5 41532EA HARTZLHCA3X HCA3XK2 GL RECIPROCATING ENDELAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NO3 MAIN BEARING SHELL DELAMINATED AND SHEDDING LARGE FLAKES OF BEARING MATERIAL. METAL CONTAMINATION OF OIL FILTER. BEARING HADA MANUFACTURERS STAMP (ML-KS) DATE 2-00. 1H72 3O3 O 6A1 1E4 5 CP913 20020205001562002020500156EA 2002 2 5 AUS20011380 220011218G7414104001678 CAM BENDIX 10349370A PIPER PA32 PA32300 7103212SO LYC O540 IO540K1A5 41532EA HARTZLHCC2Y HCC2YK1 GL MAGNETO/DISTRIBUWORN W K NONE O OTHER ININSP/MAINT 1 AUS D299916FR (AUS) MAGNETO IMPULSE CAM PAWL PIVOTS WORN TO LIMITS. 1L71 3O3 O A3SO 1E4 5 CP920 20020205001572002020500157SO 2002 2 5 AUS20011382 220011010G8530646640 EXHAUST VALVE CONT IO360K CESSNA172 R172K 2072431CE CONT O360 IO360K 17025SO MCAULY2A34C 2A34C203 GL RECIPROCATING ENWORN W K NONE E VIBRATION/BUFFET NRNOT REPORTED 1 AUS 1459 (AUS) EXHAUST VALVE GUIDE WORN EXCESSIVELY. INVESTIGATION FOUND SPRINGCAP RIDING UP ON VALVE AND CONTACTING ROCKER ARM DUE TO WORNCOLLETS. 1H71 3O3 O 3A17 E1CE 5 CP3EA 20020206000032002020600003CE 2002 2 6 AUS20011384 120011205G781031015828 EXHAUST STACK CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE EXHAUST DUCT CRACKED AT AFT FLANGE ATTACHMENT WELD. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20020205001582002020500158CE 2002 2 5 AUS20011385 120011130G7430C2925010100 IGNITION SWITCH CONT IO520F CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL IGNITION SWITCHIWORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) IGNITION SWITCH TERMINALS WORN BEYOND LIMITS. 1H71 3O3 O A4CE E5CE 5 CP21EA 20020206000042002020600004CE 2002 2 6 AUS20011386 120011218G3260GE327 BULB CESSNA340 340CESSNA 2076404CE CONT O520 TSIO520K 17040SO MCAULY3AF32C3AF32C87 GL MLG INDICATOR BURNED OUT W O OTHER P NO WARNING INDICATION LDLANDING 1 AUS (AUS) NOSE LANDING GEAR DOWN AND LOCKED LIGHT BULBS (2OFF) BLOWN. 1L72 3O3 O 3A25 E8CE 5 CP22EA 20020206000062002020600006EA 2002 2 6 AUS20011388 220011227G7321312275805 FUEL CONTROL AGUSTAA109 A119 0261102EU PWA PT6 PT6B36 52043EA ENGINE CONTAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUEL CONTROL UNIT CONTAMINATED WITH BRONZE PARTICLES. 1G72 3U4 U H7EU E4EA 20020206000082002020600008WP 2002 2 6 AUS20011390 120011211G7921111F4178D0440 HOSE GARRTT TPE3316252M FLTCHR24 FU24AIRPTS 3530202WP GARRTTTPE331TPE3316252M 01514NE ENG OIL COOLER DETERIORATED W O OTHER EK VIBRATION/BUFFET FLUID LOSS NRNOT REPORTED 1 AUS (AUS) ENGINE OIL COOLER FAILED FROM OVER-PRESSURISATION. INVESTIGATION FOUND PARTICLES OF RUBBER IN THE OIL COOLER BLOCKING THE RETURN OIL FLOW TO THE OIL TANK. THE RUBBER PARTICLES APPEAR TO HAVE COME FROM INTERNAL FAILURE OF OIL HOSE PNO 111F417-8D0440. THE BLOCKAGE OF THE OIL COOLER CAUSED AN OVER-PRESSURISATION OF APPROXIMATELY 300 PSI. 1L71 3O 4A12 E2WE 20020206000092002020600009WP 2002 2 6 AUS20011393 220011227G8530802 EXHAUST VALVE DHAVXXDH82 DH82AROBRTSN2801002WP DHAVXXGIPSY GIPSYMAJOR1 20004WP NR 2 CYLINDER FAULTY W O OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 AUS (AUS) NR 2 CYLINDER EXHAUST VALVE FAULTY. 1Q71 3I3 I A8EU A8EU 20020205001612002020500161EA 2002 2 5 AUS20011394 220011217G741410401678 CAM BENDIX S6LN1227 BNORM BN2 BN2A20 1520220EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL MAGNETO/DISTRIBUWORN W K NONE O OTHER ININSP/MAINT 1 AUS K069918FR (AUS) MAGNETO IMPULSE CAM WORN BEYOND LIMITS. 1H72 3O3 O A17EU 1E4 5 CP920 20020205001622002020500162EU 2002 2 5 AUS20011395 120011113G2742 ACTUATOR FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU STABILIZER ACTUAFAILED W K NONE F FLT CONT AFFECTED CRCRUISE 1 AUS (AUS) STABILISER ACTUATOR FAILED. 2L72 4F4 FRTA20EU E2EU 20020205001632002020500163EU 2002 2 5 AUS20011396 120011116G2742 ACTUATOR FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU STABILIZER ACTUAFAULTY W K NONE FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 AUS (AUS) STABILISER ACTUATOR SUSPECT FAULTY. 2L72 4F4 FRTA20EU E2EU 20020205001662002020500166SW 2002 2 5 AUS20011399 120010826G2510206031121023 WEB BELL 206L3 BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL FLIGHT COMPARTMECRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) COPILOTS SEAT WEB CRACKED. 1G71 3U3 U H2SW E1GL 20020206000112002020600011EU 2002 2 6 AUS20011400 120010804G2821 CLAMP BNORM BN2 BN2A26 1520226EU GASCOLATOR MISMANUFACTURED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) GASCOLATOR FILTER BOWL UNSECURELY CLAMPED. INVESTIGATION FOUND INADEQUATE DEPTH OF HOLE PREVENTED FULL ENGAGEMENT OF ONE LEG OFTHE SADDLE CLAMP. 1H72 3O A17EU 20020206000132002020600013WP 2002 2 6 AUS20011402 220010616G726131080261 SCAVENGE PUMP SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UHR WP ENGINE SEIZED W O OTHER EK VIBRATION/BUFFET FLUID LOSS CRCRUISE 1 AUS 2521 (AUS) RT ENGINE TURBINE SCAVENGE PUMP SHAFT SEIZED AND TEETH STRIPPED FROM SCAVENGE PUMP GEAR PNO 3108028-1 AND DRIVESHAFT SPUR GEARPNO 3102270-4. 2L72 4T4 TRTA5SW E4WE 20020206000142002020600014CE 2002 2 6 AUS20011403 120011129G7120121343316 MOUNT CESSNA206 U206F 2073333CE CONT O520 IO520* 17032SO ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT REAR ENGINE MOUNT SUPPORT BRACKETS CRACKED FROM REAR INBOARD BEND RADIUS. NUMEROUS RIVETS IN SURROUNDING STRUCTURE FRETTING. 1H71 3O3 O A4CE E5CE 20020205001672002020500167SW 2002 2 5 AUS20011404 120011123G5521206023119007 SPAR BELL 206 206L3 1182108SW ELEVATOR, SPAR/RCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 6357 AO00972 (AUS) ELEVATOR SPAR CRACKED. CRACK LENGTH 82.5MM (3.25IN). 1G71 3U H2SW 20020206000152002020600015EA 2002 2 6 AUS20011405 220011126G7250 BLADE DHAV DHC6 DHC6200 2802620EA PWA PT6 PT6A20 52043EA HARTZLHCB3T HCB3TN3 GL TURBINE SECTION FAILED W A UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 AUS (AUS) LT ENGINE INTERNAL FAILURE. INITIAL REPORTS INDICATE POWER TURBINE BLADE FAILURE. 1H72 3T3 TRTA9EA E4EA 6 CP15EA 20020206000162002020600016SO 2002 2 6 AUS20011406 120010721G3242PBA920 PAD EMB 110 EMB110* SO BRAKE MISSING W K NONE O OTHER ININSP/MAINT 1 AUS 2564 (AUS) BRAKE PRESSURE PLATE WORN. BOTH BRAKE PADS ON PRESSURE PLATE MISSING. SUSPECT PAD HAD SEPARATED FROM PLATE CAUSING THE OTHER PAD TO SEPARATE AS WELL. 1L72 4T RTA21SO 20020205001682002020500168EU 2002 2 5 AUS20011407 120010723G2410 CSD FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU ALTERNATOR-GENERDISCONNECTED W K NONE J WARNING INDICATION CRCRUISE 1 AUS (AUS) NO1 CONSTANT SPEED DRIVE (CSD) DISCONNECTED IN FLIGHT. 2L72 4F4 FRTA20EU E2EU 20020205001692002020500169EU 2002 2 5 AUS20011408 120010727G2163 LINE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU CABIN TEMPERATURLEAKING W K NONE OJ OTHER WARNING INDICATION CRCRUISE 1 AUS (AUS) TURBINE BYPASS VALVE DOWNSTREAM SENSE LINE LEAKING. 2L72 4F4 FRTA20EU E2EU 20020205001702002020500170EA 2002 2 5 AUS20011411 220011215G852013F17751 CRANKSHAFT LYC LTIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR2 GL RECIPROCATING ENSHEARED W K NONE E VIBRATION/BUFFET CRCRUISE 1 AUS L209668A (AUS) ENGINE CRANKSHAFT SHEARED AT NO6 BEARING JOURNAL. INTERNAL DAMAGE TO ENGINE. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020205001712002020500171CE 2002 2 5 AUS20011412 120011224G7160265895716 LEVER PWA PT6A114A CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL ENGINE AIR INTAKCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE INERTIAL SEPARATOR SELECTION LEVER CRACKED AT MID POINT. 1H71 3T3 T A37CE E4EA 5 CP60GL 20020206000182002020600018EU 2002 2 6 AUS20011415 120010811G3620 INDICATOR FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU PNEUMATIC SYS STUCK W O OTHER J WARNING INDICATION CLCLIMB 1 AUS (AUS) NR 1 HIGH PRESSURE VALVE SWITCH INDICATOR STICKING. 2L72 4F4 FRTA20EU E2EU 20020206000322002020600032WP 2002 2 6 AUS20011439 220011224G726131032173 HOUSING CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL ENG OIL PUMP CRACKED W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) ENGINE OIL PUMP HOUSING CRACKED. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20020206000332002020600033SO 2002 2 6 AUS20011440 220011224G8530 CYLINDER BEECH 55 E55 1152732CE CONT O520 IO520C 17032SO MCAULY2AF34C2AF34C55 GL ENGINE CRACKED W O OTHER EF VIBRATION/BUFFET FLT CONT AFFECTED CRCRUISE 1 AUS 636 (AUS) RT ENGINE NR 2 AND NR 4 CYLINDERS CRACKED IN AREA OF HEAD / BARRELJOINT. 1L72 3O3 O 3A16 E5CE 5 CP5EA 20020205001782002020500178SO 2002 2 5 AUS20011441 220011224G8530 CONNECTING ROD CONT GTSIO520M CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL RECIPROCATING ENFAILED W K NONE E VIBRATION/BUFFET CLCLIMB 1 AUS 127 (AUS) NO5 CONNECTING ROD FAILED. NO1, NO2 AND NO4 MAIN BEARINGS OVERHEATED. SIGNS OF OVERHEATING ON ALL BIGEND BEARINGS.INVESTIGATION INDICATES INCORRECT MACHINING OF CRANKCASE OILPASSAGES IN MAIN BEARING SUPPORT. 1L72 3O3 O A25CE E7CE 5 CP45GL 20020206000512002020600051NM 2002 2 6 AUS20011445 120010326G243218850 BATTERY BOEING767 767300 1385204NM RROYCERB211 RB211524* NE MAIN OVERHEATED W O OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) MAIN BATTERY OVERHEATED. INVESTIGATION COULD FIND NO CAUSE FOR THE DEFECT AND THE BATTERY HAS OPERATED OK SINCE. THE BATTERY CHARGER WAS ALSO REMOVED FOR TESTING WITH NO FAULT FOUND. 2L72 4F4 FRTA1NM E12EU 20020205001802002020500180EA 2002 2 5 AUS20011446 120011208G3213 BLOCK DHAV DHC6 DHC6300 2802606EA MAIN LANDING GEAFAILED W K NONE O OTHER LDLANDING 1 AUS (AUS) RH MAIN LANDING GEAR COMPRESSION BLOCKS FAILED. DAMAGE CAUSED TOTHE FUSELAGE LOCATED INBOARD OF THE RH MLG. 1H72 3T RTA9EA 20020206000532002020600053EU 2002 2 6 AUS20011451 220010611G7250 BLADE FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU TURBINE SECTION DAMAGED W C ABORTED TAKEOFF ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NR 1 ENGINE HP TURBINE BLADES (6OFF) DAMAGED. 2L72 4F4 FRTA20EU E2EU 20020206000562002020600056EA 2002 2 6 AUS20011452 220011212G8530LW13820 CONNECTING ROD LYC O360 O360A4M 41514EA NR 2 CYLINDER MISMANUFACTURED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS 120 (AUS) FOLLOWING BULK STRIP DUE TO FAILURE OF THE NR 2 CYLINDER CONNECTING ROD IT WAS FOUND THAT THE OIL GALLERY SUPPLYING NR 2 MAIN BEARING WAS NOT DRILLED INTO THE MAIN OIL GALLERY. 3 O E286 20020206000572002020600057NE 2002 2 6 AUS20011453 220010112G72309380M28P05 COMPRESSOR GE CF6 CF680C2B6 30025NE ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 6513 (AUS) HPC ROTOR SPOOL 3-9 GAVE CRACK INDICATIONS DURING ULTRASONIC INSPECTION IAW EI GEN-072-1792R05. FURTHER INSPECTION AT MANUFACTURER FOLLOWING ENGINE STRIP COULD NOT CONFIRM THE CRACKING. 4 F E13NE 20020205001832002020500183SW 2002 2 5 AUS20011454 120011228G3222AN723 BOLT SCOTT CITABRIATYP BBAVIA7 7GCAA 21101N8SW LYC O320 O320A2D 41508EA AMTR C8289 C8289 GL NOSE/TAIL LANDINFAILED W K NONE O OTHER TXTAXI/GRND HDL 1 AUS (AUS) TAIL WHEEL ATTACHMENT BOLT FAILED. TAIL WHEEL SEPARATED FROM TAIL LEAF SPRING. 1H71 3O3 O A759 E274 5 NEXPP5N 20020205001842002020500184SW 2002 2 5 AUS20011455 120011217G63202060401223 GEAR BELL 206040002025BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL MAIN ROTOR GEARBDAMAGED W K NONE J WARNING INDICATION CRCRUISE 1 AUS 707 BKW841 (AUS) MAIN TRANSMISSION SUN GEAR TEETH (2OFF) CHIPPED WITH SUBSTANTIALSECONDARY DAMAGE. METAL CONTAMINATION OF TRANSMISSION. SUSPECTPNO 206-040-122-3 GEAR IS NOT TO BE USED IN A PNO 206-040-002-025 MODEL TRANSMISSION AS PER TB 206-75-12. 1G71 3U3 U H2SW E4CE 20020205001852002020500185SO 2002 2 5 AUS20011456 120011219G5753 RIB PIPER PA28 PA28140 7102802SO LYC O320 O320E2A 41508EA SNSNCH74DM M74DM EA TRAILING EDGE FLCORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH AND RH FLAP NOSE RIBS SEVERELY CORRODED. SUSPECT CAUSED BY DISSIMILAR METAL CONTACT BETWEEN RIBS AND HINGE BRACKETS. CORROSION WAS ALSO FOUND ON THE LOWER RUDDER RIB WHERE IT CONTACTED THE CONTROL HORN (DISSIMILAR METALS CORROSION). THE LOWER SECTION OF THE FIN AND ON THE TOP FUSELAGE SKIN UNDER THE FIN ALSO CONTAINS CORROSION. THE CORROSION ON THE FUSELAGE SKIN AND IN THE FIN WAS CAUSED PRIMARILY BY THE ACCUMULATION OF DEBRIS IN THE LOWER HALF OF THE FIN (MUD, WASPS NESTS) THAT ALLOWEDPROLONGED MOISTURE CONTACT IN THIS AREA. THE AIRCRAFT IS LOCATEDIN A CORROSIVE SEACOAST ENVIRONMENT. 1L71 3O3 O 2A13 E274 5 NP88614 20020205001862002020500186SO 2002 2 5 AUS20011457 120011219G5711 SPAR PIPER PA28 PA28140 7102802SO LYC O320 O320E2A 41508EA SNSNCH74DM M74DM EA WING SPAR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH AND RH WING REAR SPAR ATTACHMENT POINTS CORRODED AS DESCRIBEDIN AD/PA28/40. INSPECTION WAS CARRIED OUT IAW AD/PA28/40 WHICHWAS NOT DUE FOR ANOTHER TWO YEARS. 1L71 3O3 O 2A13 E274 5 NP88614 20020206000582002020600058SW 2002 2 6 AUS20011458 120011220G2560BL7505 CABLE BELL 407 407 1182206SW ALLSN 250C 250C47B GL RESCUE HOIST FAILED W O OTHER D INFLIGHT SEPARATION HOHOVERING 1 AUS (AUS) RESCUE HOIST CABLE BROKE IN AN AREA APPROXIMATELY 100MM (4IN) ABOVE RESCUE HOOK ATTACHMENT POINT. 1G71 3U3 UO H2SW E1GL 20020205001872002020500187SO 2002 2 5 AUS20011459 220011212G8530 EXHAUST VALVE CONT TSIO520VB CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C505 GL RECIPROCATING ENLEAKING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE EXHAUST VALVE LEAKING DURING COMPRESSION TEST. 1L72 3O3 O A7CE E8CE 5 CP22EA 20020205001882002020500188NE 2002 2 5 AUS20011460 320011202G61102D30 PROPELLER HAMSTD 2D30 SCWZERG164 G164A 3952704EA PWA R985 R985AN1 52008NE HAMSTD2D 2D30 NE PROPELLER ASSEMBFAULTY W K NONE O OTHER ININSP/MAINT 1 AUS 119789 (AUS) THE FOLLOWING DEFECTS WERE FOUND ON THE PROPELLER WHEN RECEIVED FOR OVERHAUL:-1. ZERO BEARING TENSION ON BOTH BLADES2. REAR BARREL HALF HAS BEEN DRILLED, TAPPED AND GREASE NIPPLES FITTED. NO CERTIFICATION COULD BE FOUND TO SUBSTANTIATE THIS MODIFICATION WHICH HAD BEEN CARRIED OUT WHEN THE PROPELLER WASDISMANTLED AS THE BARREL HALF HAD BEEN REPLATED AFTER THE MODIFICATION HAD BEEN CARRIED OUT 3. NON-MATCHING PART NUMBER BLADES FITTED 4. EXCESSIVE WEAR IN CYLINDER COUNTERWEIGHTBUSH BORESPERSONNEL/MAINTENANCE ERROR. UNAPPROVED MODIFICATION. 1Q71 3R3 R 1A16 5E1 5 CP206 20020206000592002020600059 2002 2 6 AUS20011463 420011228G22100119244TF CONTROLLER BNORM BN2 BN2B20 1520302EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL AUTOPILOT SYSTEMFAULTY W O OTHER O OTHER NRNOT REPORTED 1 AUS (AUS) AUTOPILOT CONTROL PROGRAMMER FAULTY. 1H72 3O3 O A17EU 1E4 5 CP920 20010802002722001080200272 2001 8 2 B3OR20010003 420010130G221510150004717 SERVO BEECH 200 C12C CE ELEVATOR BINDING B B3ORA UNSCHED LANDING FE FLT CONT AFFECTED VIBRATION/BUFFET CRCRUISE 1 SW031553 BC30 DURING A FLIGHT, THE PILOT EXPERIENCED SLUGGISH ELEVATOR CONTROL WHEEL MOVEMENT. ELEVATOR CONTROL WOULD MOVE FREELY IN NOSE UP DIRECTION BUT THE MOVEMENT IN THE NOSE DOWN DIRECTION WOULD SOMETIMES BE HARD TO MOVE AND THEN EASY TO MOVE. THIS CAUSED SEVERE PITCH OSCILLATION. PILOT FOUND THAT IF HE MOVED THE CONTROL SLOWLY, ALL WAS OK. AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION FOUND THE ELEVATOR AUTOPILOT SERVO INTERMITENTLY LOCKING UP IN THE THE NOSE DOWN DIRECTION CAUSING THE PILOT TO HAVE TO FIGHT THE SERVO CLUTCH. REPLACED SERVO MOTOR. ALTHOUGH THIS IS A MILITARY AIRCRAFT, THE SAME SERVO IS INSTALLED IN OTHER RAYTHEON A200 AIRCRAFT. 1L72 4T A24CE 20010802002732001080200273EU 2001 8 2 B3OR20010004 120010621G77220301037070 THERMOCOUPLE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ENGINE OUT OF TOLERANCEB B3ORE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW035204X802 20 3099 9570 AIRCRAFT HAD SUFFERED A SERIES OF HUNG STARTS, ENGINE WOULD HANG UP AT 30%. IF THE ENGINE WOULD START, IT WOULD BE A SLOW START. USUALLY, THE PILOT WOULD REACH THE STARTER TIME LIMIT OF 45 SEC'S BEFORE THE ENGINE WOULD START AND BE SELF-SUSTAINING,AND HE WOULD HAVE TO ABORT THE START SEQUENCE. TROUBLE SHOOTING FOUND THE INJECTORS WERE "DRIBBLEING" FUEL INSTEAD OF A SMOOTH,EVEN,FAN PATTERN. CHANGED THE OVERSPEED AND DRAIN VALVE. AFTER HAVING THE SAME RESULTS: SLOW/HUNG STARTS, CALLED A TURBOMECCA TECH REP.HE SUGGESTED THAT WE CHECK THE T4 HARNESS.HARNESS WAS OHMED OUT, ONE PROBE SHOWED AN OPEN PROBE. REPLACED T4 HARNESS, GROUND RUN AIRCRAFT HAD 3 SUCCESSFUL STARTS. OPS CHECK WAS NORMAL. THE SLOW START HUNG START1G71 3U3 U H9EU E19EU 20010802002742001080200274CE 2001 8 2 B3OR20010005 120010629G3260S13771 SWITCH CESSNA210 T210N 2073456CE MLG IMPROPER PART B B3ORK NONE J WARNING INDICATION ININSP/MAINT 1 SW036621A 21063559 DURING INSTALLATION OF MAIN LANDING GEAR ACTUATORS AFTER COMPLIANCE WITH SEB01-2, A MAIN LANDING GEAR DOWN INDICATION SWITCH WAS FOUND DAMAGED. THE SWITCH, P/N S1377-1 FROM THE ILLUSTRATED PARTS MANUL, WAS ORDERED FROM CESSNA. WHAT WAS RECEIVED HAD THE CORRECT P/N ON THE PACKAGING BUT THE P/N ON THE PART WAS P6-340005. CESSNA WAS CONTACTED AND WE WERE INFORMED THAT THIS IS THE REPLACEMENT PART. AN ATTEMPT WAS MADE TO PUT THE PART IN THE AIRCRAFT TO NO AVAIL. THE SHAPE OF THE OLD SWITCH HOUSING IS BASICALLY RECTANGULAR WITH A SHAVED OFF CORNER. THE NEW SWITCH HAD NO SHAVED OFF CORNER. THE NEW SWITCH WOULD CONTACT A FORK ASSEMBLY IN THE GEAR. CESSNA WAS NOTIFIED AND THEY RECALLED THE SWITCHES. AS OF 7-11-2001, CE1H71 3O 3A21 20010802002752001080200275EU 2001 8 2 B3OR20010006 120010709G6730AC67032 SERVO SNIAS 350 AS350B2 8680813EU HYD SYSTEM LEAKING B B3ORK NONE K FLUID LOSS ININSP/MAINT 1 SW035204X808 3099 DURING A PREFLIGHT INSPECTION, HYDRAULIC FLUID WAS FOUND UNDER THE FORWARD PORTION IF THE TAIL BOOM. INVESTIGATION FOUND TAIL ROTOR SERVO LEAKING. AREA WAS CLEANED AND HYDRAULIC POWER UNIT WAS RUN ON AIRCRAFT TO LOCATE LEAK. SERVO WAS LEAKING FROM THE SHAFT TWICE THE ALLOWABLE LEAK RATE AND THE SERVO WAS ALSO LEAKING FROM A NON SERVICABLE PLUG ON THE HOUSING. UNIT WAS REPLACED WITH SERVICABLE UNIT. 1G71 3U H9EU 20011015001092001101500109CE 2001 10 15 B3OR20010009 120011006G2730MS27645A4 BEARING CESSNA500 550 2076604CE ELEVATOR CORRODED B B3ORK NONE O OTHER ININSP/MAINT 1 SW032649 5513 150 5500607 THE ELEVATOR WAS REMOVED TO FACILLITATE OTHER MAINTENANCE. UPON REMOVAL OF THE RIGHT HAND ELEVATOR, THE INBOARD ELEVATOR BEARING, INNER RACE CAME OFF WITH THE INBOARD MOUNT BOLT. DURING THE REMOVAL OF THE ELEVATOR, THE BALL BEARINGS FELL OUT OF THE OUTER RACE. UPON FURTHER INVESTIGATION, THE INNER AND OUTER RACE HAD RUST AND RUST POWDER ON THE INNER AND OUTER SURFACES OF THE RACES. THE INNER RACE WAS NOT "SEIZED" TO THE MOUNT BOLT. SOME OF THE BALL BEARINGS WERE MISSING, WHILE SOME SHOWED SIGNS OF CORROSION AND METAL TO METAL CONTACT, SOME WERE NOT FOUND AT ALL. THE BARING, P/N MS27645-A4, WAS REPLACED WITH A NEW BEARING AND STAKED IN ACCORDANCE WITH CESSNA MAINTENANCE INSTRUCTIONS. 1L72 4F A22CE 20010809002562001080900256GL 2001 8 9 BB1 320010720G6110RB2000 BLADE AMTR PULSARSUPERPULSAR GL CONT O240 IO240B 17063SO AMTRRXBK BK063 GL PROPELLER SEPARATED G A UNSCHED LANDING D INFLIGHT SEPARATION TOTAKEOFF 1 WP23 601 806949 EXPERIMENTAL AMATEUR BUILT AIRCRAFT, INITIAL FLIGHT WITH NEW NON-CERTIFICATED VARIABLE PITCH PROPELLER MANUFACTURED BY AEROTEK AUCKLAND, NEW ZEALAND. BOTH COMPOSITE BLADES SEPARATED SIMULTANEOUSLY ON TAKE OFF AT 500 FT. AGL. INSPECTION REVEALED THAT THE BLADE FAILURE OCCURRED AT THE BOND BETWEEN THE BLADES AND THE RETAINING PLUG, TEARING THROUGH THE DOWEL PIN HOLES. SUSPECT A DESIGN AND/OR MANUFACTURING DEFECT. 1L71 3O3 ONTEXPA1L71E7SO 5 NEXPP5N 20010502000612001050200061CE 2001 5 2 BF8R0320 120010320G32450923150 VALVE BEECH 76 76 1153005CE TUBE VALVE SCORED B K NONE O OTHER ININSP/MAINT 1 WP286627U ME214 DEFECTIVE VALVE CORE MATING SEAL. 1L72 3O A29CE 20010802002862001080200286SO 2001 8 2 BIER0056 120010510G7100LW12892 THRUST PLATE PIPER PA28 PA28236 7102815SO LYC O540 O540* 41532EA ROCKER ARM SHAFTBROKEN B BIEAK NONE O OTHER ININSP/MAINT 1 EA21435951435 400 288411018 L2107240A AT 400 HR VALVE INSPECTION FOUND ROCKER ARM SHAFT THRUST BUTTONS BRITTLE AND CRACKED. SUBMITTER RECOMMENDATION: STRESS THE IMPORTANCE OF THE 400 HR VALVE INSPECTION. 1L71 3O3 O 2A13 E295 20010802002952001080200295EA 2001 8 2 BIER200103057 220010703G7322105217 CARBURETOR GROB G115 G115C 1660303EU LYC O320 O320D1A 41508EA ENGINE LOOSE B BIERK NONE O OTHER ININSP/MAINT 1 EA21331AC400 90 82021C L1803039A FOUND FUEL BOWL ATTACH SCREWS LOOSE WITH SUBSEQUENT FUEL LEAK AT BOWL GASKET, REQUIRED CARBURETOR REPLACEMENT DUE TO SCREW HOLE ELONGATION. SUBMITTER NOTES: LYCOMING SB 366, DATED SEPT 14, 1973 REFERENCES THIS FOR MARVEL-SCHEBLER CARBURETORS, WITH NO MENTION OF FACETS. SUBMITTER RECOMMENDS ANNUAL/250 HR SCREW TORQUE CHECK AS A MINIMUM INSPECTION INTERVAL. 1L71 3O3 ONTA57EU E274 20010320001832001032000183SO 2001 3 20 BJ3RE000007 220010226G8530SA643873 EXHAUST VALVE CONT CESSNA310 310Q 2074242CE CONT O470 IO470VO 17026SO ENGINE WORN B K NONE O OTHER ININSP/MAINT 1 SW996960446 46 310Q0812 14953672V DURING AN IRAN INSPECTION, IT WAS NOTICED THAT THE AMOUNT OF VALVE SHOWING ABOVE THE KEEPER WAS LESS ON ONE CYINDER THAN ON THE OTHERS. UPON DISASSEMBLY IT WAS FOUND THAT #3 CYLINDER EXHAUST VALVE WAS 1/16TH INCH SHORTER THAN THE OTHER VALVES. A SLIGHT MUSHROOMING LIP WAS ABLE TO BE FELT AROUND THE TOP OF THE VALVE. IT APPEARS THAT THIS IS THE SAME TYPE OF WEAR AS INDICATED IN CSB98-1B ON CONTINENTAL VALVES. 1L72 3O3 O 3A10 3E1 20010305000932001030500093NM 2001 3 5 CA010105006 120010103G276165448517 HOUSING BOEING 65448517 BOEING737 737217 1384464NM PWA JT8 JT8D17 52049NE SPOILER ACTUATORBROKEN W K NONE O OTHER ININSP/MAINT 1 CA 3251 (CAN) DURING INSPECTION, 17C CHECK OF NR 4 GROUND SPOILER, SPOILER FOUND TO BE LOOSE. FOUND NR 4 SPOILER ACTUATOR, BODY END THAT ENCLOSED THE BEARING, BROKEN AWAY. ACTUATOR REPLACED AS PER WORK CARD 51160. 2L72 4F4 F A16WE E2EA 20010111000742001011100074EU 2001 1 11 CA010105010 120010103G2621 FIRE BOTTLE AIRBUS310 A310304 EU GE CF6 CF680C2* GL ENGINE DISCHARGED W A UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 CA (CAN) A/C 212, DEC 17/2000, FLT 92577, YQM, LOG SEQUENCE 0292319. DURING CLIMB, MAIN DECK (FWD AND MID) SMOKE WARNING OCCURRED. SMELL AND SMOKE AND MIST WAS DETECTED IN COCKPIT. FIRE BOTTLES WERE DISCHARGED AND AIRCRAFT RETURNED TO YMQ. AFTER CREW DEBRIEF, MIST AND ODOR WAS ATTRIBUTED TO INGESTION OF GLYCOL INTO PNEUMATIC SYSTEM DURING DEICE IN YMQ. FIRE BOTTLES WERE REPLACED AS PER WORK CARDS 26-210-005, AND 26-130-103. AIRCRAFT SERVICEABLE. 2L72 4F4 FRTA35EU E23EA 20010305001072001030500107 2001 3 5 CA010110005 420010110G2562400010 ELT ROBSINR22 R22BETA NM LYC O320 O320B2C 41508EA CABIN FAILED W K NONE L NO TEST ININSP/MAINT 1 CA (CAN) DURING ANNUAL INSPECTION, THIS ELT FAILED BECAUSE OF BORDERLINE OUTPUT POWER AND NO G SWITCH. THE ELT WAS RETURNED TO THE MANUFACTURER FOR REPAIR. 1G71 3O3 O H10WE E274 20010306000282001030600028EU 2001 3 6 CA010111019 120010103G30603E32602 HARNESS BFGOODRICH PILATSPC12 PC1245 EU HARTZLHCE4A HCE4A3D GL ANTI-ICE SYSTEM FAULTY W K NONE L NO TEST ININSP/MAINT 1 CA 1351 (CAN) ONE PROPELLER FOUND NOT TO BE HEATING WHILE PERFORMING SCHEDULED PROPELLER DEICER TEST. TROUBLESHOOTING LEAD US TO FIND AN OPEN WIRE IN THE HARNESS. PART ORDERED. 1L71 3T RTA78EU 5 CP210NE 20010306000462001030600046EA 2001 3 6 CA010116027 120010103G5610 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA 95144H8592 (CAN) IN CRUISE, THE F/OS FRONT WINDSHIELD SHATTERED AT 31,000 FEET.THE MAINTENANCE REPLACED THE WINDSHIELD AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010306000472001030600047EA 2001 3 6 CA010116028 120010101G5610 WINDSHIELD CNDAIRCL600 CL6002B19 EA COCKPIT FAILED W K NONE O OTHER APAPPROACH 1 CA 00231H5852 (CAN) ON APPROACH TO YUL, THE F/OS FRONT WINDSHIELD SHATTERED AT 6,000 FEET.THE MAINTENANCE REPLACED THE WINDSHIELD AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4F RTA21EA 20010330000662001033000066NM 2001 3 30 CA010129018 120010104G275065162266 SWITCH BOEING727 72722 1384002NM PWA JT8 JT8D7B 52053NE KRUGER FLAP FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) AFTER DEPARTER&UPON FLAP RETRACTION, NR 5 LEADING EDGE FLAP IN TRANSIT LIGHT ILLUMINATED. FUEL DUMPED & A/C RETURNED TO AIRPORT OF DEPTR: MAINT CHANGED OUT FLAP SWITCH, P/N 40174 & SYS TESTED & FUNCTIONED NORMALLY. A/C DEPARTED & SAME FAULT RECURRED. MAINT REPL NR 5 LEADING EDGE FLAP ACTUATOR, P/N 65-17818-20 & LEADING EDGE POS CNTL MODEL, P/N 65-60212-11, AS PRECAUTIONARY MEASURE: SYS AGAIN TESTED AS PER THE MM& OPALLY CHECKED SEVERAL TIMES W/O FAULT. A/C RT-SRV. DISCREPANCY RETURNED ON NEXT DEPTR: A/C RETURNED AGAIN FOR MAINT TROUBLESHOOTING. FINAL RPT: L/E FLAP POS SWITCHES SWAPP ED BETWEEN 5 & 3 FLAP. WIRING FROM COCKPIT T 2L73 4F4 F A3WE E2EA 20010330000672001033000067 2001 3 30 CA010130007 420010120G2200065006415 COMPUTER BENDIX 220 PILATSPC12 PC1245 EU AUTOPILOT FAILED W O OTHER J WARNING INDICATION CLCLIMB 1 CA 1964 (CAN) IN THE CLIMB, SHORTLY AFTER ENGAGING AUTOPILOT, AUTOPILOT DISENGAGED FOR NO APPARENT REASON. AFTER A SUCCESSFUL RETEST, REENGAGING IS POSSIBLE WITH NO FURTHER PROBLEMS. THIS PROBLEM HAS OCCURRED IN THE RECENT PAST.THE AUTOFLIGHT COMPUTER WAS REPLACED FOR TROUBLESHOOTING AND ITS PERFORMANCE WILL BE MONITORED. 1L71 3T RTA78EU 20010330000682001033000068EU 2001 3 30 CA010130009 120010103G55109412259360 BUSHING PILATS 5551012036 PILATSPC12 PC1245 EU HORIZONTAL STAB FAILED W K NONE O OTHER ININSP/MAINT 1 CA 1351 1351 272 (CAN) HORIZONTAL STABILIZER HAS MOVEMENT OF .003 AT ATTACHMENT POINTS, WHEN TIP OF STAB IS MOVED IN A UP AND DOWN MOTION. THIS AIRCRAFT HAS BEEN LIKE THIS SINCE NEW. AS PER PILATUS, 0 TOLERANCE ALLOWED AT ATTACHMENT POINT. BUSHINGS WERE REPLACED WITH NO IMPROVEMENT. BOLTS PLACED ON ORDER TO TRY TO ILLIMINATE THE PLAY. 1L71 3T RTA78EU 20010330000692001033000069EA 2001 3 30 CA010130011 220010105G7200 ENGINE DHAV DHC6 DHC6 2802606EA PWA PT6 PT6A27 52043EA RIGHT FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) RT ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE. AFTER REACHING CRUISING ALTERNATE RT ENGINE LOW OIL PRESSURE CAPTION APPEARED. LOW OIL PRESSURE GAUGE INDICATION OBSERVED. PRECAUTIONARY ENGINE SHUT DOWN. DIVERTED BACK TO AIRFIELD. 1H72 3T4 TRTA9EA E4EA 20010330000702001033000070NM 2001 3 30 CA010130012 120010101G304007802 WINDSHIELD DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA 10554 (CAN) LEFT WINDSHIELD SHATTERED INFLIGHT. AIRCRAFT LANDED. WINDSHIELD REPLACED IN ACCORDANCE WITH DHC8 MM 56-10-11. RAN AIRCRAFT OPERATIONS CHECKED, OK. AIRCRAFT RETURNED TO SERVICE. NOTE PCA A0101001 2H72 4T4 TRTA13NM E20NE 20010330000712001033000071GL 2001 3 30 CA010131009 120010101G7160653885 FLANGE DIAMONDA20 DA20C1 2990001GL CONT O240 IO240B 17063SO SNSNCHW69EK W69EK63 EA INTAKE PIPE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 569 (CAN) FLANGE CRACKED. 1L71 3O3 ONTTA4CH E7SO 5 NTA4CH 20010330000722001033000072EA 2001 3 30 CA010131015 120010105G5753F35 SEALANT DHAV DHAV DHC7 DHC7103 2802710EA PWA PT6 PT6A50 52043EA HAMSTD24PF 24PF305 GL UNDER NR 4 FLAP PEELING W K NONE O OTHER ININSP/MAINT 1 CA 10482 (CAN) THE SEALANT USED UNDER THE NR 4 FLAP TRACK AS PER AD CF-87-04, SB 7-57-30 WAS FOUND PEELING OFF. 10481.68 HOURS HAVE ACCUMULATED ON THIS AIRCRAFT AFTER INITIAL APPLICATION BACK IN OCTOBER OF 1987. THIS AIRCRAFT HAS BEEN OPERATING IN ASIA. 2H74 4T4 T A20EA E4EA 6 CP1NE 20010330000732001033000073SO 2001 3 30 CA010131016 120010105G812046C1983985 TURBOCHARGER PIPER PA46 PA46350P SO LYC O540 TIO540AE2A 41532EA ENGINE FAILED W O OTHER O OTHER CRCRUISE 1 CA 159 (CAN) PILOT REPORTED LOSS IN MANIFOLD PRESSURE FOUND TURBOCHARGER TURBINE MISSING A BLADE AND TURBO SEIZED. 1L71 3O3 ORTA25SO E14EA 20010330000742001033000074 2001 3 30 CA010131017 420010104G25620004006A BATTERY LEIGH SHARC7H2184 ELT WRONG PART W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 132428 (CAN) ELT WAS SUBMITTED FOR ANNUAL RECERT. UNAPPROVED BATTERY WAS CERTIFIED WITH ELT NOV.1/2000 - ELT AS SUCH IS NOT TC APPROVED. AND INSTALLED HORIZONTALLY IN AIRCRAFT (CESSNA, AS PER CUSTOMER), AND THE G SWITCH IS INSTALLED FOR A VERTICAL MOUNT INSIDE THE UNIT. ELT RETURNED AS IS, CUSTOMER ADVISED TO FIND ALTERNATE REPLACEMENT. 20010330000752001033000075CE 2001 3 30 CA010131018 120010110G551112326194 RIB CESSNA 183260029 CESSNA210 T210M 2073451CE CONT O520 TSIO520R 17040SO MCAULYD3A34 D3A34C402 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A 50 HOUR INSPECTION OF THE HORIZONTAL STAB, THE 4 RIBS WERE FOUND TO BE LOOSE & CRACKED. THIS IS DONE BY SQUEEZING THE NOSE RIBS (WITH A MODERATE AMOUNT OF PRESSURE) AND LISTEN FOR CLICKING SOUNDS & FEELING OF LOOSE RIVETS. THEREFORE, THE LOWER SKIN WAS PEELED BACK THE 4 RIBS WERE REMOVED AND REPLACED WITH NEW RIBS. THE SKIN WAS RIVETED BACK ON. STAB WAS INSTALLED AND AIRCRAFT WAS RETUNED TO SERVICE. 7 B&C S.D. FOUND DUING 50 HOUR INSPECTION. NO ACTION REQUIED BY FLIGHT CREW. 1H71 3O3 O 3A21 E8CE 5 CP47GL 20010330000852001033000085EA 2001 3 30 CA010202005 120010107G3244256K433 TIRE 60085123 CNDAIRCL601 CL6012A12 1900303EA GE CF34 CF341A NE MLG FAILED W O OTHER O OTHER TOTAKEOFF 1 CA 249 (CAN) ON TAKEOFF CREW HEARD MUFFLED BANG. NO AIRCRAFT CONTROL PROBLEMS NOTED. CONTINUED TO DESTINATION LANDED WITHOUT INCIDENT. DURIG POST FLIGHT FOUND THE NR 3 TIRE HAD LOST ALL TREAD. THE TIRE WAS STILL INFLATED. DAMAGE TO RIGHT INBOARD FLAPS LOWER SURFACE AND THE RIGHT MAIN LANDING GEAR INBOARD WEIGHT ON WHEEL ANTI-SKID HARNESS. 2L72 4F4 FRTA21AE E15NE 20010330000872001033000087EA 2001 3 30 CA010202008 120010103G5610 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) THE CREW REPORTED THAT THE CAPTS FRONT WINDSHIELD SHATTERED IN CRUISE. THE LANDING WAS UNEVENTFUL.THE MAINTENANCE REPLACED THE WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010330000882001033000088EA 2001 3 30 CA010202011 120010103G2752 ACTUATOR CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE RT FLAP FAILED W O OTHER J WARNING INDICATION APAPPROACH 1 CA (CAN) THE CREW REPORTED THE FLAP FAIL CAUTION MESSAGE WHICH APPEARED ON APPROACH (SELECTIION OF 45 DEGREES, STOPPED AT 37). THE MAINTENANCE REPLACED THE RT OUTBOARD FLAP INBOARD ACTUATOR 2L72 4F4 FRTA21EA E15NE 20010330000892001033000089EA 2001 3 30 CA010202013 120010106G261247259701 FIRE DETECTOR CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE NR 1 ENGINE FAILED W O OTHER N FALSE WARNING DEDESCENT 1 CA (CAN) DURING DESCENT INTO MEMPHIS, THE CREW ON AIRCRAFT 7416 SHUT DOWN ENGINE NR 1 PER THE EMERGENCY PROCEDURES DUE TO THE POSTING OF AN INTERMITTENT LT ENGINE FIRE MESSAGE ON THE EICAS. DURING TROUBLESHOOTING THE MECHANICS FOUND THE FIRE DETECTION UNIT UNDER THE LT CONSOLE SHORTED AND CONTAMINATED (COFFEE) WITH LIQUID. A NEW CONTROLLER AND BOTTLE WAS INSTALLED AND THE SYSTEM SUCCESSFULLY TESTED PER THE AMM. 2L72 4F4 FRTA21EA E15NE 20010330000902001033000090NE 2001 3 30 CA010202022 220010107G7210 GEARBOX CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 ENGINE FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION NRNOT REPORTED 1 CA (CAN) NR 2 ENGINE VIBRATION FLUCTUATION INDICATED .4 TO .7 MILS APPROXIMITELY 3 TO 5 MIN. LATER, NR 2 ENGINE SHUT DOWN UNCOMMANDED. PERFORMED QRH PROCEDURE & DIVERTED INTO NEXT AIRPORT (ISO), THE FLIGHT CREW DECLARED EMERGENCY (UNEVENTFUL).FOUND METAL IN CHIP DETECTOR (SUSPECT GEARBOX - INTERNAL) NOT CONFIRMED. REPLACEMENT OF ENGINE S/N 807528 IN PROGRESS. 2L72 4F4 FRTA21EA E15NE 20010330000912001033000091EA 2001 3 30 CA010205006 120010111G3040NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CRCRUISE 1 CA 1566 (CAN) THE CREW REPORTED THAT THE LT WINDSHIELD CORE PLY CRACKED DURING FLIGHT.THE MAINTENANCE REPLACED THE WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010330000922001033000092EA 2001 3 30 CA010205008 120010101G5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CRCRUISE 1 CA (CAN) THE CREW REPORTED THAT THE RT WINDSHIELD CARACKED IN FLIGHT. THE MAINTENANCE REPLACED THE RT WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010402002522001040200252SO 2001 4 2 CA010206004 220010104G8530628309 VALVE GUIDE CESSNA150 150M 2071830CE CONT O200 O200A 17020SO EXHAUST VALVE WORN W ED ENGINE SHUTDOWN RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CA 1439 (CAN) ENGINE RAN VERY ROUGH AT START UP.CYLINDER NR 3 REMOVED DUE TO LOW COMPRESSION. EXHAUST GUID WORN CAUSING CARBON TO JAM VALVE IN OPEN POSITION. CYLINDER RELACED DUE TO ABOVE PROBLEM. 1H71 3O3 O 3A19 E252 20010403001242001040300124EU 2001 4 3 CA010208013 120010123G2431RG390E BATTERY BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE7315R 01518WP MAIN BATTERY OVERHEATED W O OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA 407 (CAN) ENGINE ROTATION TOO SLOW AT START ATTEMPTS FOR SUCCESSFUL ENGINE LIGHT OFF. BATTERY VENTED EXCESSIVE AMOUNTS OF SMOKE AND VAPOR (STEAM AND ACID GAS) DUE TO SEVERAL SUCCESSIVE FAILED ENGINE START ATTEMPTS WITHOUT ALLOWING SUFFICIENT RECHARGING BY AIRCRAFT ELECTRICAL SYSTEM. HOT BATTERIES REMOVED FROM AIRCRAFT. STRUCTURE NEUTRALIZED AND RINSED WITH FRESH WATER. - NEW BATTERIES FITTED. 2L72 4F4 FRTA3EU E6WE 20010403001252001040300125NE 2001 4 3 CA010208014 120010124G62207610308010103 HUB SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 3985 3985 (CAN) DURING THE POST FLIGHT INSPECTION BY AME A FINE LINE WAS NOTICED ON THE UPPER DAMPER ATTACH LUG. THE LUG WAS PAINT STRIPPED AND A DEFINITE CRACK CAN BE SEEN. STARTING NEAR THE BOLT HOLE PROGRESSING INBOARD FOR APPROXIMATELY 1 1/4 INCH. THE MAIN ROTOR HUB WAS REPLACED. 1G72 3U3 U H1NE E1GL 20010403001262001040300126SW 2001 4 3 CA010208016 120010122G6220471202527 GRIP BELL 47 47J2 1181104SW LYC O435 TVO435* 41516EA MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2261 31 (CAN) AIRCRAFT IS BEING IMPORTED INTO CANADA. CRACKS IN ROOT OF THREADS FOUND DURING EDDY CURRENT INSPECTION. 1G71 3O3 O 2H1 1E13 20010403001272001040300127EU 2001 4 3 CA010209002 120010124G2612 FIRE DETECTOR FOKKERF28 F28MK1000 4990808EU NR 2 ENGINE INTERMITTENT W FA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CA (CAN) FLT 8473SHORTLY AFTER DEPARTURE OUT OF KELOWNA (YLW), FLT CREW REPORTED THAT NR 2 ENGINE FIRE WARNING CAME ON. NR 2 ENGINE SHUTDOWN & BOTH FIRE BOTTLES WERE DISCHARGED. PILOTS REPORTED THAT FIRE WARNING LIGHTS REMAINED ON AFTER THE BOTTLES WERE DISCHARGED. A/C ROUTED TO VANCOUVER (YVR) DUE TO WEATHER MINS IN INTERIOR. REMAINDER OF FLT UNEVENTFUL & A/C LANDED IN YVR WITH NO FURTHER INCIDENTS TO REPORT. MAINT INSPECTION AFTER LANDING CONFIRMED FAULTY INDICATOR ONLY. CRA FLEET RELIABILITY DEPT CREATED WORK PACKAGE FOR INDICATION PROBLEM. 2L72 4F RTA20EU 20010403001282001040300128SO 2001 4 3 CA010209003 120010209G6310 ENGINE PIPER PA31 PA31P 7103120SO LYC O541 TIGO541E1A 41539EA NACELLE FAILED W O OTHER J WARNING INDICATION DEDESCENT 1 CA 1231 (CAN) ENGINE LOSSED MANIFOLD PRESSURE FOLLOWED BY LOSS OF OIL PRESSURE. VISUAL INSPECTION REVEALS CRACKED CASE. 1L72 3O3 O A8EA E19EA 20010403001292001040300129WP 2001 4 3 CA010209004 120010112G2435230321183 BELL ASSY LUCAS 23032018 HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL STARTER GEN UNAPPOVED PART W K NONE O OTHER ININSP/MAINT 1 CA 1177 2514 (CAN) STARTER GEN RECEIVED FOR OVERHAUL. FOUND THE ADE (COMM END) END BELL ASSEMBLY TO BE 3, WHICH ACCORDING TO THE OEM IS AN OLD, OBSOLETED PART THAT WAS APPLICABLE ONLY TO THE 23032-005 STARTER-GENERATOR, WHICH IS ITSELF OBSOLETE, UNSUPPORTED AND NOT LISTED IN THE OVERHAUL MANUAL. THE ASSEMBLY IS ALSO CORRODED AND CRACKED AROUND THE MOUNTING HOLES. THE CORRECT ASSY IS P/N 23032-1423. A CORRECT ASSY WAS INSTALLED DURING OVERHAUL, ALONG WITH THE CORRECT BEARING RETAINER AND FAN COVER.THE OFFENDING PARTS ARE BEING TRANSMITTED TO THE AIRCRAFT OPERATOR FOR FOLLOW-UP. 1G71 3U3 U H3WE E4CE 20010403001302001040300130SW 2001 4 3 CA010209006 120010129G2435230791281 BRUSHES LUCAS 230790001 SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP ROTOL R321 R321482F8 GL STARTER GEN UNAPPOVED PART W K NONE O OTHER ININSP/MAINT 1 CA 499 10020 (CAN) DURING SCHEDULED MAINTENANCE, AT BRUSH INSPECTION IT WAS FOUND THAT THE BRUSHES INSTALLED IN THIS STARTER-GENERATOR WERE. THIS BRUSH IS ONLY APPROVED FOR THE STARTER GEN MODELS 23079-009 AND 23079-000-2.THE BRUSHES WERE REMOVED AND REPLACED WITH FAA-PMA LONG LIFE BRUSH PART NO.M23088-1320, WHICH IS APPROVED FOR THIS STARTER-GENERATOR MODEL 23079-000-1 WHEN USED ON THE FAIRCHILD SA227AC AIRCRAFT. THE STARTER GEN WAS RETURNED TO SERVICE. 2L72 4T4 TRTA8SW E4WE 6 CP61GL 20010403001312001040300131EU 2001 4 3 CA010209007 120010131G32409595601511 BRAKE PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL LT MLG FROZEN W O OTHER O OTHER LDLANDING 1 CA (CAN) TAKEOFF IN FT ST. JOHN IN POWDER SNOW MAY HAVE CAUSED MOISTURE TO ENTER LT BRAKE ASSEMBLY. DURING FLIGHT TO FT NELSON, BRAKE FROZE. ON LANDING IN FT. NELSON LT TIRE WOULD NOT ROTATE AND TIRE FLAT SPOTTED AND BLEW. AIRCRAFT WAS STOPPED ON RUNWAY AND MAINTENANCE WAS CALLED. TIRE AND WHEEL ASSEMBLY WAS REPLACED AND GEAR ASSEMBLY INSPECTED FOR DAMAGE. THIS IS THE 3RD SUCH INCIDENT IN THE LAST 12 MONTHS. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010403001322001040300132NE 2001 4 3 CA010209009 220010116G72304036T24P01 BLADE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE ENGINE SEPARATED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 2264 2264 (CAN) AIRCRAFT IN CLIMB FL110, LOUD BANG HEARD, RT FIRE WARNING ACTIVATED. POWER REDUCED, FUEL SHUT OFF, FIRE WARNING DE-ACTIVATED. AIRCRAFT RETURNED TO DEPARTURE AIRPORT AND SINGLE ENGINE LANDING CARRIED OUT WITHOUT FURTHER INCIDENT. GROUND INSPECTION REVEALED THAT FINAL STAGE TURBINE HAD LOST ONE BLADE (CONTAINMENT RING DAMAGED BUT NOT PENETRATED) RESULTANT IMBALANCE CAUSED SEVERE DAMAGE TO REMAINING BLADES AND SHROUD AND CAUSED EXHAUST TAIL PIPE TO SEPARATE AT MOUNTING FLANGE. HOT GASES RELASED INSIDE COWLING CAUSED FIRE WARNING TO ACTIVATE. ENGINE OVERHAUL AGENCY MAY HAVE MORE INFORMATION AFTER THEIR ANALYSIS. 2L72 4J4 J A10CE 1E16 20010403001332001040300133SW 2001 4 3 CA010209015 120010121G5610412669001100 WINDOW BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA COCKPIT FAILED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) WHILE IN STRAIGHT AND LEVEL FLIGHT A LOUD BANG WAS HEARD. IT WAS DISCOVERED THAT THE RT REAR SLIDING DOOR WINDOW HAD SHATTERED. AN UNEVENTFUL LANDING WAS CARRIED OUT. ALLL PIECES WERE RECOVERED. 1G71 4U4 U H4SW E22EA 20010403001342001040300134EU 2001 4 3 CA010209017 120010131G3310MS24149A1 RELAY BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE7313R 01518WP LIGHTING FAILED W O OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN) AFTER TAXI IN AT YVR THE NR 2 AC INVERTER FAIL LIGHT ILLUMINATED AS WELL AS XS2 BUSS FAIL LIGHT ILLUMINATED. RESET THE NR 2 INVERTER SWITCH FAILED TO RESET THE SYSTEM. MAINTENANCE TROUBLESHOOT THE PROBLEM BACK TO A FAULTY RELAY WITHIN THE CABIN LIGHTING SYSTEM. FURTHER INVESTIGATION FOUND THE LIGHTING RELAY CHATTERING, CAUSED A FLUCTUATING VOLTAGE ON THE XS2 BUSS RESULTING IN THE NR 2 INVERTER TRIPPING OFF LINE. AFTER TRACING THE HISTORY OF THIS PROBLEM IT WAS FOUND THAT IN MORE THAN ONE OCCASIION THE CABIN LIGHTING HAS CAUSED A TOTALFAILURE OF THE AIRCRAFTS RIGHT AC BUSS THUS LEAVING CONCERNS AS TO HOW A SECONDARY SYSTEM CAN FAIL A PRIMARY SYSTEM ON THE AIRCRAFT. 2L72 4F4 F A3EU E6WE 20010403001362001040300136CE 2001 4 3 CA010212005 120010123G531224120651 BULKHEAD CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 10545 (CAN) DURING INSPECTION OF AIRCRAFT FOLLOWING A GEAR UP LANDING, THE TWO BULKHEADS RUNNING VERTICALLY IN FRONT OF CABIN DOORS WERE FOUND CRACKED AT FLOOR LEVEL. THE CRACK IS LOCATED AT THE CUT OUT FOR THE HEAT DISCHARGE DUCT. THESE CRACKS WERE NOT CAUSED BY THE GEAR UP LANDING. 1H71 3O3 O 3A17 E286 5 CP7EA 20010403001372001040300137CE 2001 4 3 CA010212006 120010123G531205120122 BULKHEAD CESSNA172 172P 2072436CE LYC O320 O320D2J 41508EA FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 15904 (CAN) DURING ROUTINE CESSNA PROGRESSIVE CARE INSPECTION, THE BULKHEAD AT THE BACK END OF THE BAGGAGE COMPARTMENT STATION 108 WAS FOUND TO BE CRACKED AT BOTH LOWER CORNERS, AND THE UPPER RIGHT CORNER. THE CRACKS ARE APPROXIMATELY 2 INCHES LONG. THIS AIRCRAFT IS USED FOR FLIGHT TRAINING AND ON OCCASION BANNER TOWING. 1H71 3O3 ONT3A12 E274 20010403001382001040300138EA 2001 4 3 CA010212007 120010125G2701C3CF3913 CONTROL COLUMN DHAV DHC3 DHC3 2800202EA PWA PT6 PT6A34 52043EA COCKPIT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE CARRYING OUT AIRWORTHINESS DIRECTIVE CF-82-34 WE FOUND A CRACK IN THE LOWER WELD ASSEMBLY OF THE AILERON CONTROL COLUMN LOCATED AT THE CUT HOLE FOR THE AILERON CHAIN. THE CRACK WAS APPROXIMATELY 1/4 INCH LONG. 1H71 3R4 T A815 E4EA 20010403001392001040300139NE 2001 4 3 CA010212011 220010118G7200 ENGINE BOEING727 727225 1384077NM PWA JT8 JT8D7B 52053NE NR 1 FAILED W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) ENROUTE TO CPH FROM EMA NR 1 ENGINE OIL QUANTITY SLOWLY DECREASED TO 1 GALLON AT WHICH POINT THE INFLIGHT SHUT DOWN WAS PERFORMED. THE A/C LANDED WITHOUT INCIDENT AT CPH. THE ENGINE MAINTAINED POSITIVE OIL PRESSUE FOR THE 20-25 MINUTE PERIOD OF WINDMILL CONDITION. THE ENGINE WAS REMOVED AND IS ENROUTE FOR ASSESSMENT. 2L73 4F4 F A3WE E2EA 20010403000782001040300078 2001 4 3 CA010212033 420010123G2562R889V BATTERY CESSNA150 150L 2071826CE CONT O200 O200A 17020SO ELT UNAPPOVED PART W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ELT SENT IN FOR RECERTIFICATION. WAS EQUIPPED WITH A NON-APPROVED BATTERY PACK ARTEX . ONLY APPROVED BATTERY IS TECHNISONIC. BATTERY REPLACED AND ELT RECERTIFIED. 1H71 3O3 O 3A19 E252 20010403000802001040300080CE 2001 4 3 CA010213003 120010118G7160 HOSE CESSNA150 150 2071802CE CONT O200 O200* 17020SO CARB HEAT CONTAMINATED W C ABORTED TAKEOFF RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET TOTAKEOFF 1 CA (CAN) DURING THE WINTER MONTHS WE ARE RECEIVING COMPLAINTS OF A SERIOUS NATURE. UPON TAKEOFF, USUALLY THE FIRST ONE, THE AIRCRAFT RUNS VERY ROUGH. I HAVE EXPERIENCED THIS PERSONALLY. WE HAVE DETERMINED THAT SNOW COLLECTS IN THE SCAT HOSE THAT PROVIDES AIR FOR CARB HEAT. THIS SNOW MELTS AFTER THE ENGINE HAS WARMED UP AND UPON SELECTION OF CARB HEAT THE ENGINE WANTS TO QUIT. WE HAVE REMEDIED THIS ON SEVERAL AIRCRAFT BYMAKING A SMALL HOLE IN THE LOW SPOT OF THE SUBJECT SCAT HOSE, USING A SOLDERING IRON. 1H71 3O3 ONT3A19 E252 20010403000812001040300081EA 2001 4 3 CA010213004 120010119G33102LFV4090600AA COAX CNDAIRCL600 CL600* EA INSTRUMENT PANELBURNED W HA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) PILOT REPORTED CENTER INSTRUMENT PANEL FLOOD LIGHTING INOPERATIVE WITH BRIGHT/DIM POTENTIOMETER. KNOB SWITCHED OFF AND LIGHTING OPERATED WITH BRIGHT/DIM SWITCH. INVESTIGATION AREVEALED THAT CABLE ASSY, CONNECTOR PIN AT INVERTER END WAS BURNED OFF.CABLE ASSY AND INVERTER/POWER SUPPLY. THE CONNECTOR WAS PROBABLY NOT SEATED CORRECTLY AT ONE TIME, BUT AT TIME OF INVESTIGATION THE CONNECTOR WAS PROPERLY INSTALLED. ARCING AT THE INVERTER CONNECTOR PIN COULD HAVE RESULTED IN AN OVERHEAT AND/OR FIRE CONDITION. 2L72 4F RTA21EA 20010327002042001032700204EA 2001 3 27 CA010213005 120010203G3244256K433 TIRE CNDAIRCL601 CL6012A12 1900303EA SIDEWALL BULGED W O OTHER O OTHER ININSP/MAINT 1 CA 199 93170620 (CAN) BULGE IN TIRE SIDEWALL/TREAD RADIUS EDGE. IT APPEARS THAT AIR IS LEAKING INTO THE RADIUS AND GETTING TRAPPED BETWEEN PLIES. THIS IS THE THIRD TIRE THAT I KNOW OF WITH THIS PROBLEM. 2L72 4F RTA21AE 20010327002052001032700205SO 2001 3 27 CA010213006 220010126G8530 CYLINDER HEAD CONT 642344 CESSNA421 421B 2076014CE CONT O520 GTSIO520H 17032SO MCAULY3AF34C3AF34C92 GL SP PLUG-INJECTR CRACKED W O OTHER O OTHER ININSP/MAINT 1 CA 100 (CAN) AT 100 HOUR INSPECTION IN NOVEMBER 2000, FOUND FOUR CYLINDERS WITH SIMILAR CRACKS. AT NEXT 100 HOUR INSPECTION IN JANUARY 2001 FOUND SIX MORE CYLINDERS WITH CRACKS IN SAME LOCATION (BETWEEN SPARK PLUG HOLE AND INJECTOR HOLE). CYLINDERS REPLACED AFTER DETECTING CRACKS. PAST EXPERIENCE SHOWS THAT CRACKS ARE VERY COMMON IN THIS AREA.2001-02-15 TC: PART #S, TSN, ADDITIONAL CONTRIBUTING FACTORS WERE NOT GIVEN. 1L72 3O3 O A7CE E7CE 5 CP22EA 20010327002062001032700206SO 2001 3 27 CA010213008 120010122G52804752932 HINGE PIPER PA31 PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA IN RADIUS CRACKED W O OTHER O OTHER ININSP/MAINT 1 CA 317712043 (CAN) DURING INSPECTION AS PER AIRWORTHINESS DIRECTIVE 200-25-01,(2)TWO GEAR DOOR HINGES FOUND CRACKED. HINGES REPLACED. 1L72 3O3 O A20SO E14EA 20010327002072001032700207EA 2001 3 27 CA010213009 120010124G2701C2CF834A CONTROL COLUMN DHAV DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE AT WELD CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 15576 497 (CAN) COMPLETED INSPECTION AS PER SB 2/28 AND AD CF-84-01R1, FOUND CRACK IN WELD. 128 HOURS SINCE LAST INSPECTION.SUBMITTER FEELS LACK OF MAINTENANCE MAY BE RESPONSIBLE FOR THIS CRACK BEING NOTED EARLY. 1H71 3R3 R A806 5E1 20010327002092001032700209EA 2001 3 27 CA010213018 120010125G2760 ACTUATOR CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE ACTUATOR LUG BROKEN W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN) ON APPROACH, AT LAST FLP SELECTION, A/C ROLLED TO THE RIGHT FOLLOWED BY FLT SPLR DEPLOY CAUTION MESSAGE.CREW DECLARED EMERGENCY AND LANDED WITHOUT ANY FURTHER EVENT. MAINTENANCE FOUND FLIGHT SPOILER PANEL ACTUATOR LUG BROKEN. PANEL REPLACED. AIRCRAFT RETURNED TO SERVICE. AD IN PROGRESS 2L72 4F4 FRTA21EA E15NE 20010327002102001032700210EA 2001 3 27 CA010213019 120010124G2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 EA GE CF34 CF341A NE LAV SMOKE DETCTRFAULTY W O OTHER N FALSE WARNING APAPPROACH 1 CA (CAN) ON SHORT FINAL, SMOKE TOILET CAUTION MESSAGE CAME ON. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT ANY FURTHER EVENT.LAV SMOKE DETECTOR FOUND FAULTY & REPLACED. 2L72 4F4 FRTA21EA E15NE 20010403000842001040300084EA 2001 4 3 CA010213020 120010124G2740 ACTUATOR CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE HORIZONTAL STAB FAILED W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CA (CAN) DURING TAKEOFF ROLL, CONFIG TRIM AND CONFIG STAB WARNINGS APPEARED. CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS.HSTA AND MCU REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010327002112001032700211EA 2001 3 27 CA010213021 120010124G2740 STABILIZER CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE HORIZ STAB FAILED W O OTHER F FLT CONT AFFECTED CLCLIMB 1 CA (CAN) ON CLIMBOUT, STAB AND MACH TRIM DISENGAGED AT 8.2 UNITS AT NOSE UP TRIM. WOULD NOT RE-ENGAGE. AIRCRAFT PERFORMED A FLAP 20 DEGREES PER QRH WITHOUT ANY FURTHER EVENT. MAINTENANCE REPLACED THE HORIZONTAL STAB TRIM PANEL AND RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010327002122001032700212EA 2001 3 27 CA010213023 120010125G5610 WINDSHIELD CNDAIR CL6002B19 CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE F/O WINDSHIELD CRACKED W A UNSCHED LANDING D INFLIGHT SEPARATION CRCRUISE 1 CA 7037 (CAN) IN CRUISE FLIGHT, F/O WINDSHIELD SHATTERED. NO INFO ON ALTITUDE OR IF EMERGENCY WAS DECLARED. AIRCRAFT RETURNED INTO SERVICE AFTER WINDSHIELD REPLACEMENT. 2L72 4F4 FRTA21EA E15NE 20010327002132001032700213EA 2001 3 27 CA010213024 120010117G5610NP1393219 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE L/H WINDSHIELD CRACKED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA 00201H3495 (CAN) DURING TAXI, CAPTAIN WINDSHIELD CRACKED.AIRCRAFT RETURNED INTO SERVICE AFTER WINDSHIELD REPLACEMENT. 2L72 4F4 FRTA21EA E15NE 20010327002142001032700214EA 2001 3 27 CA010213025 120010113G5610NP1393216 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE R/H WINDSHIELD CRACKED W O OTHER O OTHER CLCLIMB 1 CA 99298H2154 (CAN) CREW RPORTED THAT PASSING FLT 160 AT A DIFFERENTIAL CABIN PRESSURE 6,4, R/H WINDSHIELD CRACKED. NO INFO IF EMERGENCY WAS DECLARED.AIRCRAFT RETURNED INTO SERVICE AFTER WINDSHIELD REPLACEMENT. 2L72 4F4 FRTA21EA E15NE 20010403000852001040300085EA 2001 4 3 CA010213027 120010213G5730 PANEL CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE RT AND LT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE JACKING AIRCRAFT, MAINTENANCE FOUND TWO CRACKS ON AFT SECTION OF LOWER WING PLANK. ONE ON THE LT AND ONE ON THE RT SIDE, AT WS 148, NEAR THE WING JACKING POINTS. REPAIR ACTIVE, AIRCRAFT WILL RETURN INTO SERVICE SOON. 2L72 4F4 FRTA21EA E15NE 20010327002152001032700215EA 2001 3 27 CA010213028 120010130G7800NAS6303U4 BOLT GE CF343B1 CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE DELTA BRCKET POSSHEARED W O OTHER O OTHER ININSP/MAINT 1 CA 3100 (CAN) MAINTENANCE FOUND THE L/H EXHAUST NOZZLE CRACKED DURING A CHECK INSPECTION. DURING REPLACEMENT OF THE EXHAUST NOZZLE, MAINTENANCE FOUND TWO (OUT OF THREE) DELTA BRACKETS ATTACH BOLTS SHEARED, AT 2 AND 10 OCLOCK POSITION.FAULTY PARTS REPLACED PER AMM. 2L72 4F4 FRTA21EA E15NE 20010327002162001032700216EA 2001 3 27 CA010213032 120010129G5610 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE L/H WINDSHIELD CRACKED W O OTHER O OTHER CRCRUISE 1 CA (CAN) DURING CUSTOMER ACCEPTANCE FLIGHT, IN CRUISE, L/H WINDSHIELD CRACKED. L/H WINDSHIELD REMOVED AND REPLACED. 2L72 4F4 FRTA21EA E15NE 20010403000862001040300086EA 2001 4 3 CA010214004 120010201G5210601R31765303 STRUCTURE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE PAX DOOR LATCH CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A ROUTINE E3 (1200 HOURS) INSPECTION WHEN REMOVING THE PASSENGER DOOR SIDE PANELS A CRACK WAS FOUND IN THE PASSENGER DOOR LATCH BOX ASSEMBLY 601R31765-3/03. THE AIRCRAFT REMAINED GROUNDED UNTIL A NEW LATCH BOX WAS INSTALLED. FOLLOWING THE REPLACEMENT OF THE FAULTY COMPONENT, THE AIRCRAFT WAS THEN RELEASED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010403000872001040300087EA 2001 4 3 CA010214008 220010112G8500 ENGINE PIPER PA28 PA28R200 7102811SO LYC O360 IO360C1C 41514EA ENGINE BAY FAILED W A UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 CA 687 (CAN) ENGINE HAD STOPPED / SEIZED AFTER THE ENGINE HEATER PLATE WHICH HAD BEEN INSTALLED THE DAY BEFORE THE FLIGHT WAS DISLODGED WHEN THE NOSE LANDING GEAR DRAG LINK CONTACTED WITH THE PLATE IN GEAR UP POSITION. THE PLANE LANDED THE PILOT DIDNT NOTICE ANYTHING. ON THE SECOND FLIGHT WHEN SELECTING GEAR UP THE PLATE WAS PUSHED ON THE QUICK DRAIN BY THE LANDING GEAR AND ALLOWED THE ENGINE OIL TO DRAIN COMPLETELY. ENGINE STOPPED THE PILOT HAD TO MAKE A FORCED LANDING IN A FIELD. ONLY MINOR DAMAGES WERE MADE TO THE PLANE. 1L71 3O3 O 2A13 1E10 20010403000892001040300089SW 2001 4 3 CA010214011 120010119G2510502565213 SHOULDER BELT HUGHES269 269C1 8059504SW LYC O360 HO360C1A 41514EA COCKPIT FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) MAIN STRAP SHREADED.REPLACED SHOULDER STRAP. 1G71 3O3 OO 4H12 E286 20010403000912001040300091CE 2001 4 3 CA010214027 120010125G57530621229 HINGE CESSNA305 305A 2074002CE CONT O470 O47011 17026SO LT WING TE FLAPSCRACKED W K NONE O OTHER ININSP/MAINT 1 CA 3667 (CAN) WING FLAP HINGE INBOARD FOUND CRACKED AT BOTH LOWER FLANGES THAT ATTACH TO THE SPAR. PART REPLACED WITH NEW. 1H71 3O3 O 5A5 E269 20010404000142001040400014CE 2001 4 4 CA010219009 120010129G275005235372 ROD CESSNA172 172N 2072434CE LYC O320 O320D2J 41508EA TE FLAPS BENT W K NONE O OTHER ININSP/MAINT 1 CA 9627 (CAN) FLAP ROD BENT. 1H71 3O3 ONT3A12 E274 20010404000172001040400017EU 2001 4 4 CA010219018 120010201G261172111211000 SMOKE DETECTOR BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP ROTOL R333 R333482F12 GL CARGO POD FAILED W A UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CA (CAN) JUST AFTER TAKEOFF OUT OF LA RONGE HEADING NORTH APPROXIMATELY 80 MILES, THE BAGGAGE POD SMOKE ALARM WENT OFF. THE AIRSCREW TURNED AROUND, & DECLARED AN EMERGENCY TO LANDED BACK IN YVC. MAINTENANCE FOUND NO SMOKE OR FIRE IN THE POD. THE SMOKE DETECTOR WAS REMOVED, THE LENSE WAS CLEANED, DETECTOR REINSTALLED AND TESTED S. THIS IS AN ONGOING PROBLEM WITH THIS UNIT IN THAT IF THE LENSE (SENSOR) GET A LITTLE DUSTY, IT WILL GIVE FALSE INDICATION. AIRCRAFT WAS REKEASED FOR SERVICES. 2L72 4T4 TRTA21EU E4WE 6 CP61GL 20010404000192001040400019EA 2001 4 4 CA010219021 220010205G8500 ENGINE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA RIGHT FAILED W A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CA 821 (CAN) AFTER TAKEOFF OUT OF URANIUM CITY PILOT HAD TO RETURN TO AIRPORT AFTER EXPERIENCING LOSS OF POWER ON RT ENGINE. MAINTENANCE INVESTIGATED AND FOUND THAT THE ACCESSORY CASE COMPONENT DRIVE GEARS WOULD NOT TURN. ALSO FOUND OIL FILTER FULL OF METAL. MATINTENANCE SUSPECTS THAT ONE OF THE DRIVE GEARS IN THE ACCESSORY CASE HAS LET GO. ENGINE IS BEING SENT TO PRO AERO ENGINES FOR STRIP DOWN AND REPAIR. FURTHER REPORT TO FOLLOW. 1L72 3O3 O A20SO E14EA 20010404000232001040400023NM 2001 4 4 CA010222010 120010205G272082700544001 CONTROL CABLE DHAV DHC8 DHC8* NM PWA 120 PW120 NE RUDDER BROKEN W D RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 CA (CAN) AFTER ENGINE STARTING, BEFORE TAXIING OUT FOR TAKEOFF, CREW CHECKED CNTLS FOR FREEDOM OF MOVEMENT. AT THAT TIME, PILOT FOUND THAT RUDDER PEDALS WERE NOT HAVING ANY RESISTANCE WHEN MOVED&WITH BOTH ENGINES RUNNING HE COULD NO T SEE ANY RUDDER MOVEMENT ON AFCS IND. AT TIME HE CALLED OFF FLT, SHUTDOWN ENGINES&CALLED MAINT. MAINTENACE CREW ARRIVED ATTHE SCENE FOUND RUDDER CABLE ASSY BROKEN. DETAILED INSP IN THE AREA REVEALED RUDDER CABLE ASSY NEXT TO 1ST ONE - DAMAGED, CORRODED, WITH 30 PERCENT OF DIAMETER, WIRES BROKEN. LOOKING TO GET ACCESS TO ALL INVOLVED AREA, THOROUGH INSP REVEALED PORT SIDE ELEV CABLE ASSY 2H72 4T4 TRTA13NM E20NE 20010404000242001040400024NM 2001 4 4 CA010222011 120010206G49408Z7591125 BRACKET DHAV DHC8 DHC8* NM PWC 150 PW150A EA APU DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING TROUBLESHOOTING FOR APU FAILED START, THE GROUND CABLE FROM APU SHUNT WAS FOUND SEPARATED FROM 4900-GS10 (STN X792) ON BRACKET. THE ATTACHMENT BRACKET WAS FOUND BURNT AS WELL AS THE CABLE CONNECTION. SYD WAS ISSUED AND THE CABLE WAS REPAIRED AND INSTALLED. BASED ON THE INFORMATION PROVIDED BY THE OPERATOR, IT IS BELIEVED THAT THE MOST PROBABLE CAUSE OF DAMAGE WAS IMPROPER INSTALLATION TORQUING OF THE GROUND STUD AND ATTACHING HARDWARE. 2H72 4T4 TRTA13NM E00062EN 20010404000252001040400025CE 2001 4 4 CA010222015 120010212G2752D14500462 TRANSMISSION CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL TE FLAPS FAILED W D RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 CA (CAN) AFTER LANDING THE PILOTS SELECTED FLAPS TO THE UP POSITION AND THE FLAP CIRCUIT BREAKER POPPED. THE FLAP CIRCUIT BREAKER WAS RESET AND THE FLAPS WERE SELECTED UP NORMALLY. WHEN THE FLAPS WERE RESELECTED TO THE DOWN POSITION THE CIRCUIT BREAKER POPPED AGAIN. THE FLAP TRANSMISSION AND MOTOR ASSEMBLY WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 5 CP60GL 20010404000262001040400026CE 2001 4 4 CA010222016 120010212G7160NAS561C410 ROLL PIN CESSNA 26520251 CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL BELLCRANK BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING THE ROUTINE 100 HOUR INSPECTION THE AIRCRAFT ENGINEER FOUND THAT THE ROLL PINS, QUANTITY 4, SECURING THE BELL CRANK TO THE AIR BYPASS DUCT FOR THE ENGINE, WERE LOOSE. UPON RMEOVAL WE FOUND THAT ALL FOUR PINS WERE BROKEN. PIN REPLACED WITH NEW. 1H71 3T3 T A37CE E4EA 5 CP60GL 20010404000282001040400028CE 2001 4 4 CA010223002 120010206G6100 BLADE MCAULY 1C172MDM CESSNA172 172 2072402CE CONT O300 O300A 17022SO MCAULY1C172 1C172MDM GL PROPELLER CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 765 633 71581 (CAN) EXTRA WORK REQUIRED TO REMOVE CORROSION FROM BLADE FACE (CAMBER FACE) IN ACCORDANCE WITH MCCAULEY MANUAL 730720. 1H71 3O3 ONT3A12 E253 5 NP910 20010404000322001040400032NM 2001 4 4 CA010223007 120010131G243523088002B STARTER GEN DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE NR 2 ENGINE DISINTEGRATED W D RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 CA 15963773 611A (CAN) A VIBRATION WAS FELT DURING START-UP ON NR 2 ENGINE AND THEN DURING TAXI THE NR 2 D.C. GENERATOR LIGHT CAME ON. THE CREW WERE UNABLE TO SUCCESSFULLY RESET THE NR 2 GENERATOR AND RETURNED TO THE GATE. INVESTIGATION REVEALED THE NR 2 GENERATOR FAN END BEARING HAD FAILED. STARTER GENERATOR REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010404000332001040400033NM 2001 4 4 CA010223008 120010120G291082970010391 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYDRAULIC SYS LEAKING W O OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CA 31326 (CAN) UPON ARRIVAL AT THE GATE HYDRAULIC FLUID WAS NOTICED TO BE LEAKING FROM THE LT WHEEL WELL AREA. INVESTIGATION REVEALED THAT THE AFT NR 1 DOOR CLOSE LINE WAS LEAKING.LINE REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010404000342001040400034NM 2001 4 4 CA010223010 120010120G291082950010277 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYDRAULIC SYS LEAKING W K NONE O OTHER ININSP/MAINT 1 CA 25366 (CAN) A PUDDLE OF HYDRAULIC FLUID WAS NOTICED AROUND THE LT MAIN WHEEL AREA. INVESTIGATION REVEALED THAT THE LEAK WAS COMING FROM THE LT OUTBOARD ROLL SPOILER LIFT DUMP LINE.LINE REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010404000382001040400038CE 2001 4 4 CA010226002 120010215G2431A876K TERMINAL CESSNA560 560XL CE PWA 545 PW545A NE BATTERY FAILED W K NONE O OTHER ININSP/MAINT 1 CA 474 (CAN) AIRCRAFT ARRIVED AT ST. HUBERT (YHU) PILOTS SHUT DOWN ENGINES AND APU, HAD NO POWER ON AIRCRAFT WITH BATTERY SWITCH ON BATTERY. PILOT TOOK SWITCH AND TOGGLED IT TO OFF AND THEN TO EMERGENCY POWER AND STILL NO POWER ON AIRCRAFT. UNABLE TO PUT BATTERY ON LINE. 2L72 4F4 FRTA22CE E00059EN 20010404000392001040400039EA 2001 4 4 CA010226005 120010203G4990 APU CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE APU BAY LEAKING W O OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 CA (CAN) THE CREW REPORTED THE SMOKE TOILET CAUTION MESSAGE AT 9000 FEET. SMOKE WAS VISIBLE WHEN BLEED WAS TRANSFERRED IN CABIN AND COCKPIT WHEN BLEEDS WERE TRANSFERRED TO APU. AIRCRAFT DID AN EMERGENCY LANDING.THE MAINTENANCE FOUND OIL COMING FROM COMPRESSOR DRAIN OF THE APU. APU WAS DEFERRED TO BE REPLACED LATER. 2L72 4F4 FRTA21EA E15NE 20010404000402001040400040EA 2001 4 4 CA010226008 120010206G5610601R3303312 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA (CAN) THE RT WINDSHIELD SHATTERED IN CRUISE DURING THE FLIGHT NR 5.THE MAINTENANCE REPLACED THE WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010404000412001040400041EA 2001 4 4 CA010226009 120010206G5610601R330339 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER CLCLIMB 1 CA (CAN) THE LT WINDSHIELD SHATTERED IN CRUISE AT 35,000 DURING THE FLIGHT NR 5.THE MAINTENANCE REPLACED THE WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010404000422001040400042EA 2001 4 4 CA010226010 120010202G5610NP1393222 WINDOW CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE COCKPIT CRACKED W O OTHER O OTHER CRCRUISE 1 CA (CAN) THE RT WINDOW CRACKED IN CRUISE. THE MAINTENANCE REPLACED THE WINDOW. 2L72 4F4 FRTA21EA E15NE 20010404000432001040400043EA 2001 4 4 CA010226011 220010205G74144347 MAGNETO HUGHES269 269C1 8059504SW LYC O360 HO360C1A 41514EA ENGINE FAILED W O OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 CA 576 (CAN) AIRCRAFT HARD TO START. RETARD LOW INTENSITY SPARK. REPLACED MAGNETO. 1G71 3O3 OO 4H12 E286 20010404000442001040400044SW 2001 4 4 CA010226012 120010125G8011SAZ4401 RELAY HUGHES269 269C1 8059504SW LYC O360 HO360C1A 41514EA STARTER FAILED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) ENGAGEMENT INTERMITTENT DUE TO VIBRATION. REPLACED STARTER RELAY. 1G71 3O3 OO 4H12 E286 20010404000462001040400046EA 2001 4 4 CA010226018 220010101G74144250R MAGNETO CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160DTM GL ENGINE FAILED W O OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CA 525 (CAN) ENGINE STARTING RUNNING ROUGH IN CRUISE FLIGHT PILOT RETURNED TO STATION. GROUND RUN INDICATED EXCESSIVE RPM LOSS ON RT MAGNETO. MAGNETO REPLACED AND FOLLOW UP GROUND RUN CARRIED OUT RESULTING IN NORMAL RPM (STATIC) AND RT RPM DROP WITHIN LIMITS. NO APPARENT EXTERNAL PROBLEMS WITH MAGNETO COULD BE IDENTIFIED. AN SC REPORT MAY FOLLOW SHOULD WE CHOOSE TO HAVE THE MAGNETO OVERHAULED. 1H71 3O3 ONT3A12 E274 5 NP910 20010404000472001040400047WP 2001 4 4 CA010226020 220010201G7412103784005C EXCITER GULSTM690TP 690D 3970405SW GARRTTTPE331TPE331* 01514WP ROTOL R306 R306382F7 GL LT ENGINE SHORTED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA 5 (CAN) LT ENGINE WOULD NOT START. NO IGNITION. IGNITION SYSTEM CHECKED AND THE EXCITER WAS FOUND TO BE AT FAULT. 1H72 3T3 T 2A4 E2WE 6 CP8EU 20010404000482001040400048NM 2001 4 4 CA010228008 120010206G6320A0061 GEARBOX ROBSINR22 R22BETA NM LYC O360 O360J2A 41514EA MAIN ROTOR FAILED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA 1747 (CAN) MAIN ROTOR GEARBOX CHIP DETECTOR LIGHT ACTIVATED IN FLIGHT. PILOT LANDED ON GROUND LIGHT WENT OUT. CHIP DETECTOR REMOVED AT MAINTENANCE FACILITY. FUZZ PARTICULATE FOUND, DETECTOR CLEANED, INSPECTED, REINSTALLED. HELICOPTER GROUND RUN ON GROUND FOR 30 MINUTES WITH NO LIGHT INDICATION. GEARBOX OIL REPLACED AT CUSTOMER REQUEST. 1G71 3O3 O H10WE E286 20010404000492001040400049EU 2001 4 4 CA010228009 120010227G5302 SKIN SNIAS 350 AS350BA 8680817EU TAILBOOM WRONG PART W O OTHER W INADEQUATE Q C LDLANDING 1 CA 14116 (CAN) - TAILBOOM COLLAPSED AFTER LANDING. - TAIL ROTOR DRIVE DISCONNECTED, FAILING DAMAGE.- LOWER FORWARD SKIN BUCKLED AND FRACTURED BETWEEN NR 3 AND 4 BEARING. - FAILURE ANALYSIS FOUND WRONG SKIN THICKNESS.- MEASURES 0.0325 INCH, SHOULD BE 1.0MM (0.03937 INCH). - OPERATOR INSPECTED FLEET OF 6 OTHERS AND FOUND AIRCRAFT S/N 2495 ALSO HAS INCORRECT SKIN. - BOOMS ARE FACTORY ORIGINAL - NO REPAIR HISTORY. - EUROCOPTER USA ADN HAWAII FAA NOTIFIED. 1G71 3U NCH9EU 20010404000502001040400050NE 2001 4 4 CA010301002 220010103G7310226311001 LINE HONEYWELL BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE ENGINE FUEL MISREPAIRED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) DURING RECEIPT OF A LOANER ENGINE, IT WAS NOTED THAT ONE OF THE INSTALLED LINES FROM THE FLOW DIVIDER TO THE FUEL MANIFOLD HAD AN UNAPPROVED WELD REPAIR ACCOMPLISHED ON IT. THE LINE WAS REPLACED. 2H74 4F4 FRTA49EU E6NE 20010404000512001040400051NM 2001 4 4 CA010301004 120010127G291082950010175 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) DURING ROUTINE INSPECTION, HYDRAULIC FLUID WAS FOUND LEAKING FROM THE LT WING INBOARD FLAP CANOE. INVESTIGAITON RESULTED IN REPLACEMENT OF A LEAKING FLIGHT SPOILER UNLOAD LINE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010404000522001040400052EA 2001 4 4 CA010301005 120010209G7112311269001 ADAPTER DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE VENTURI CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING SCHEDULED INSPECTION OF THE R/H ENGINE, THE ENGINE BLEED AIR VENTURI ADAPTER WAS FOUND TO HAVE A V SHAPED CRACKED ON THE OUTSIDE OF THE 90 DEGREE BEND OF THE VENTURI. THE VEE HAD OPENED UP, ALLOWING BLEED AIR TO BE DUMPED INTO THE ENGINE COMPARTMENT. THE ADAPTER WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (THIS AREA OF THE ADAPTER IS COVERED WITH A SHROUD, MAKING INSPECITON A DELIBERATE ACTION.) 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010404001962001040400196NE 2001 4 4 CA010301017 220010117G7200 ENGINE BOEING767 7673S1 1385211NM GE CF6 CF680C2B2 30025NE RIGHT FAILED W E ENGINE SHUTDOWN Y ENGINE STOPPAGE LDLANDING 1 CA 3233832338 720611 (CAN) ON FINAL INTO YYZ, RIGHT ENGINE SHUTDOWN, 4 MINUTES TO LANDING. ENGINE SHUTDOWN CHECKLIST COMPLETED. LANDED WITHOUT INCIDENT. ON INSPECTION OF RT ENGINE METAL FOUND IN TAILPIPE. RT ENGINE REPLACED. OFF PART NUMBER 6-7200-9-0002, SERIAL NUMBER 2611.2001-03-06 TC: EXPECT OPERATOR TO FOLLOW-UP WHEN TEAR DOWN AVAILABLE. 2L72 4F4 FRTA1NM E13NE 20010404001992001040400199NE 2001 4 4 CA010301029 120010216G6210S611520107 BLADE SKRSKYS61 S61N 8142104NE GE CT58 CT581401 30011NE MAIN ROTOR DEBONDED W K NONE O OTHER ININSP/MAINT 1 CA 8770 (CAN) AIRCRAFT LANDED TO REFUEL. IT WAS NOTED THAT DURING A WALKAROUND THAT, A ROTOR BLADE POCKET HAD BECOME DEBONDED. A TEMPORARY REPAIR WAS MADE AND THE AIRCRAFT WAS FLOWN BACK TO BASE. 2G72 4U4 U 1H15 1E3 20010404002002001040400200EA 2001 4 4 CA010301030 120010301G275072740196011 TUBE DHAV DHC7 DHC7103 2802710EA PWA PT6 PT6A50 52043EA HAMSTD24PF 24PF305 GL FLAP DRIVE WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING INSPECTION, SEVERE WEARING WAS NOTED ON OUTBOARD FLAP DRIVE SECONDARY DRIVE TUBE P/N 72740196-011 BY THE STEADY BEARINGS. UNABLE TO DETECT WEAR PROPERLY UNLESS STEADY BEARING REMOVED. WEAR WAS FOUND ON BOTH SIDES OF FLAP DRIVE SYSTEM. MAXIMUM WEAR FOUND 0.0265 INCH. TUBE THICKNESS APPROXIMATELY 0.040. BOTH WORN TUBES REPLACED WITH SERVICEABLE UNITS. 2H74 4T4 T A20EA E4EA 6 CP1NE 20010404002012001040400201NE 2001 4 4 CA010301031 120010209G29103935 SHUTOFF VALVE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ACTUATOR LEAKING W ED ENGINE SHUTDOWN RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CA 162 (CAN) ON START UP THE NR 1 SERVO JAM WARNING LIGHT WOULD NOT EXTINGUISH WHEN NORMAL HYDRAULIC PRESSURE WAS REACHED. THE FLIGHT CREW SHUT DOWN AND UPON EXITING THE AIRCRAFT SAW HYDRAULIC FLUID UNDER THE AIRCRAFT. THE ENGINEER FOUND THE NR 1 HYDRAULIC SYSTEM FLUID LOW WHICH CAUSED THE NR 1 SERVO JAM LIGHT TO STAY ON. FURTHER INVESTIGATION FOUND THE TAIL SERVO SHUT OFF VALVE LEAKING FROM THE ELECTRICAL ACTUATOR BODY. THE VALVE WAS REPLACED, NR 1 HYDRAULIC SYSTEM REPLENISHED AND BLED. THE AIRCRAFT WAS TEST FLOWN AND THEN RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20010404002022001040400202EA 2001 4 4 CA010301032 120010213G3246901230602 FITTING DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE LT FLOAT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CORROSION AND STRESS CRACK DEVELOPED ON THE TAPER HOLE OF THE SPREADER BAR ATTACH FITTING LT FLOAT AFT SPREADER ATTACH P/N 901-23060-2 WAS REMOVED AND QUARANTINED. REPLACEMENT P/N S1901-23060-2 INSTALLED AS PER STC SF-92-7. 1H71 3R3 R A806 5E1 20010404002032001040400203EA 2001 4 4 CA010301033 120010213G3246901230602 FITTING DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE LT FLOAT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CORROSION AND STRESS CRACK DEVELOPED ON THE TAPER HOLE OF THE SPREADER BAR ATTACH FITTING RT FLOAT FORWARD SPREADER ATTACH WAS REMOVED AND QUARANTINED. REPLACEMENT P/N S1901-23060-2 INSTALLED AS PER STC SF-92-7. 1H71 3R3 R A806 5E1 20010404002042001040400204EA 2001 4 4 CA010301035 220010216G8540LW10292 IDLER GEAR PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA ENGINE WORN W K NONE O OTHER ININSP/MAINT 1 CA 820 (CAN) THE IDLER GEAR BETWEEN THE CRANKSHAFT AND THE CAMSHAFT GEAR DISENGAGED DUE TO FRACTURING OF THE CRANKCASE AND ACCESSORY CASE. THESE FRACTURES ARE DIRECTLY OPPOSITE THE CRAN GEAR AND WOULD INDICATE THAT A SOLID OBJECT WENT IN BETWEEN THE CRANK GEAR AND IDLER GEAR. THE UPPER ROW OF TEETH ON THE IDLER, DRIVES THE MAGNETO AND THERE IS ONE TOOTH MISSING. THIS MISSING TOOTH IS PROBABLY WHAT WENT IN BETWEEN THE GEARS. 1L72 3O3 O A20SO E14EA 20010404002052001040400205EA 2001 4 4 CA010301036 220010212G72503027102 TURBINE BLADES PWA PT6T PT6T3 52045EA ENGINE WRONG PART W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 3000 (CAN) POWER TURBINE SECTION DISASSEMBLED FOR EVALUATION. POWER TURBINE BLADES SHOWED A DIFFERENT CONFIG THAN P/N 3027102 POWER TURBINE BLA DES NORMALLY FOUND ON THIS MODEL ENGINE. ALSO PART NO (P/N 3013102) STAMPED ON BLADES WAS CROSSED OUT & P/N 3027102 WAS ENGRAVED. P&W WAS NOTIFIED & RESPONDED THAT SUBJECT BLADES WERE APPLICABLE TO A PT6A ENGINE & NOT PT6T. THEY ALSO STATED THAT THERE IS NO APPRD MODS THAT WOULD ALLOW 3013102 BLADES TO BE REIDENTIFIED. P&WSTATES BLADES MUST BE REMVD FROM SERVICE. 2001-03-05 TC: FORWAEDED TO MAINT & MFG S.U.P. 4 U E22EA 20010404002292001040400229CE 2001 4 4 CA010302006 120010214G531207126161 BULKHEAD CESSNA182 182H 2072718CE CONT O470 O470R 17026SO MCAULY2A34C 2A34C50 GL VERTICAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 4269 (CAN) CRACK ABOVE LT RUDDER STOP BOLT LOCATION ON (BULKHEAD) FLANGE BEND RADIUS DIRECTLY ABOVE BOLT. A/C HANGARED FOR LAST 15 YRS & NOT SUBJECTED TO WIND. REMOVAL & INSP SHOWS POOR STANDARD PRACTISE OF DRIVING 90 DEGS STIFFENER INTO BEND RADIUS OF FLANGE (ASSY IS SANDWICH OF STIFFENERS). THUS WHEN RUDDER STOP BOLT JAM NUT IS TIGHTENED, STIFFENER CUTS INTO BEND RADIUS. REPL PART WORSE&REJECTED (NEW). NEW BULKHEAD STIFFENER PLAC ED SO AS TO RIDE UP BEND RADIUS ENOUGH TO FIT 0.015 FEELER GAUGE. ASSY MANUFACTURED & RIVETED WITH GAP. FEW STROKES WITH FILE WOULD MATCH BEND RADIUS & NOT CAUSE PROBLEM DURING MANUFACTURE: SK210-161-1 WILL BE INST (SEB99-12R1). 1H71 3O3 ONT3A13 E273 5 CP3EA 20010404002072001040400207EU 2001 4 4 CA010302007 120010214G2912583400 FILTER 704A44633025SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE HYD SYSTEM CLOGGED W A UNSCHED LANDING F FLT CONT AFFECTED HOHOVERING 1 CA 257 (CAN) - UPON HOVERING IN AERIAL LONG LINE WORK. THE PILOT NOTICED SOME FEEDBACK IN CYCLIC CONTROLS WHEN INPUTING AGGRESSIVE MOVEMENTS (I.E. WINDY CONDITIONS). HE IMMEDIATELY ABORTED THE TASK AT HAND AND LANDED.- ON INSPECTION OF HYDRAULIC FILTER FOUND A BLACK DEPOSIT IN FILTER MEDIA.- THIS IS ABNORMAL CONSIDERING THE 500 HR FILTER LIFE, AND TAFT OF 257.2 HOURS. - POSSIBLE CAUSE: DEPOSITS INSIDE HYDRAULIC LINES AND COMPONENTS AT TIME OF MANUFACTURE AND HIGH DETERGENT ATTRIBUTES OF AEROSHELL FLUID 41). 1G71 3U3 U H9EU E19EU 20010404002102001040400210CE 2001 4 4 CA010302010 120010131G3230ALM50 CURRENT LIMITER BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA HARTZLHCD4N3HCD4N3A GL MLG FAILED W O OTHER J WARNING INDICATION APAPPROACH 1 CA (CAN) AIR NUNAVUT KING AIR WAS ON APPROACH TO IGALUIT AT NIGHT. FLIGHT CREW SELECTED GEAR, THEY RECEIVED AN UNSAFE GEAR INDICATION AND HAD TO USE GEAR EMERGENCY EXTENSION METHOD, AFTER WHICH GAVE 3 GREEN GEAR DOWN AND LOCKED INDICATION. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AN INSPECTION OF LANDING GEAR SYSTEM WAS ACCOMPLISHED. IT WAS DISCOVERED THAT R/H GENERATOR BUS POWER LIMITER HAD FAILED. MAINTENANCE WAS UNSUCCESSFUL AT FINDING A CAUSE FOR LIMITER FAILURE. NEW POWER LIMITER INSTALLED. GEAR SWINGS ACCOMPLISHED AS PER AVIA DESIGNS MAINTENANCE MANUAL. AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A24CE E4EA 5 CSTC 20010404002112001040400211EU 2001 4 4 CA010302012 120010302G62401179405303 INDICATOR BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE TRIPLE TACH FAULTY W A UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CA 12 468 (CAN) NR (ROTOR RPM) NEEDLE STARTED TO READ LOW. PILOTS RECOGNIZED THIS AS AN INDICATION PROBLEM. PILOTS LANDED AT BASE WITHOUT INCIDENT. PROBLEM WAS CORRECTED BY INSTALLING A SERVICEABLE TACHOMETER. 1G72 3U3 U H13EU E5NE 20010404002132001040400213CE 2001 4 4 CA010302014 120010209G304010138402522 WINDSHIELD BEECH B300 B300 1159232CE PWA PT6 PT6A60A 52043NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA 1205 98108H3288 (CAN) WHILE IN CRUISE FLIGHT AT FL310 AND OAT -46 DEGREES C, A LOUD BANG WAS HEARD AND THE RT WINDSHIELD CRACKED. (WINDSHIELD HEAT HAD BEEN ON FOR THE ENTIRE FLIGHT (1 HOUR PLUS)). FLIGHT CREW REFERENCED ABNORMAL OCCURRENCE IN POH AND MADE AN UNSCHEDULED, UNEVENTFUL LANDING IN YYC. AIRCRAFT GROUNDED FOR WINDSHIELD REPLACEMENT. NOTE: SIMILAR OCCURRENCE TO LT WINDSHIELD FAILURE IN OCTOBER 1999. 2L72 4T4 TRTA24CE E4EA 20010404002212001040400221NM 2001 4 4 CA010306015 120010128G2120 UNKNOWN DHAV DHC8 DHC8* NM PWC 150 PW150A EA CABIN ODOR W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CA (CAN) DURING A TAKEOFF A SMELL WAS NOTED AND INCREASE DRAMATICALLY DURING THE CLIMB. CREW NOTED THAT THERE WAS NO VISIBLE SIGN OF SMOKE. CREW RETURNED TO BASE FOR INVESTIGATION. MAINTENANCE CARRIED OUT AN APU START, BLEED ON, SMELL PRESENT FOR 2 MIN. THEN DISAPPEARED. ENGINE RUN PERFORMED NO SMELL. DC CONTACTOR BOXES CHECKED, NO FAULT. AREA AROUND WATER BOILER INSPECTED, NO FAULT. EPCU CHECKED FOR FAULT CODES, NO FAULT. CDS CHECKED, NO FAULT. ENGINE RUN PERFORMED AGAIN, NO FAULT. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20010405000662001040500066CE 2001 4 5 CA010307004 120010220G3246C1630030201 WHEEL MCAULY CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA NLG DAMAGED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA (CAN) REPORTED TO MAINTENANCE OF CLICKING NOISE FROM FRONT AREA DURING TAXI. INSPECTION REVEALED THREE (3) THRU BOLTS MISSING ON WHEEL RIM RESULTING IN DAMAGE TO NOSE FORK. TWO OF THREE REMAINING BOLTS FOUND LOOSE. SUSPECT INCORRECT TORQUE ON WHEEL BOLTS. 1H71 3O3 ONT3A12 E274 20010405000672001040500067SW 2001 4 5 CA010307007 120010214G6230206010332121 BEARING BELL 206040002007BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL MAST CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 4456 1461 NOF4734 (CAN) SEVERE PITTING OF LOWER BEARING JOURNAL INNER RACE AT LOWER PORTION OF MAST ASSEMBLY. 1G71 3U3 U H2SW E4CE 20010405000722001040500072SW 2001 4 5 CA010307013 120010109G6510206040102103 COVER BELL 206 206L 1181522SW ALLSN 250C 250C20B 03013GL T/R COUPLING GROOVED W K NONE O OTHER ININSP/MAINT 1 CA 15 (CAN)WHEN REINSTALLING A MAIN DRIVESHAFT AFTER A INPUT TRANSMISSION SEAL REPLACEMENT, FOUND THAT THE TRANSMISSION END OF THE SHAFT COULD NOT MOVE. OPENED THE COUPLING END FOUND THAT SPRINGS WAS NOT INSTALLED PROPERLY. THE COVER WAS GROOVED. INSPECTED THE INNER AND OUTER COUPLING ON BOTH END OF DRIVESHAFT ASSEMBLY. NO MORE DAMAGE FOUND 15.0 HOUR SINCE LAST INSPECTION. COMPLETED THE SHAFT INSPECTION AFTER REPLACING THE COVER AND THE SPRING THAT WERE DAMAGED BY NEW PARTS. A/C WAS RETURNED TO SERVICE. 1G71 3U3 U H2SW E4CE 20010405000742001040500074WP 2001 4 5 CA010307015 120010225G6310 ENGINE LKHEED1011 1011385114 WP RROYCERB211 RB21122B02 54555NE ENGINE FAILED W A UNSCHED LANDING O OTHER CLCLIMB 1 CA 47592 (CAN) AFTER TAKEOFF ENGINE NR 3 VIBS INCREASED TO 2.5 UNITS, THROTTLE RETARDED TO KEEP BELOW LIMITS. AIRCRAFT RETURNED TO MAINTENANCE BASE YMX. TROUBLESHOOTING CARRIED OUT AS PER MM 79-00-00 PAGE 121, ENGINE RUNS CARRIED OUT AS PER TEST NR 21 VIBRATIONS WITHIN LIMITS, AIRCRAFT RETURNED TO SERVICE.SUSPECT OIL FINDING. 2L73 4F4 F A23WE E12EU 20010405000762001040500076NE 2001 4 5 CA010307017 220010218G7200 ENGINE LKHEED1011 1011385115 5265015WP RROYCERB211 RB21122B02 54555NE NR 2 VIBRATION W K NONE O OTHER ININSP/MAINT 1 CA 44530 (CAN) AFTER TAKEOFF (DURING FIRST STAGES OF CLIMB) THE NR 2 ENGINE VIBRATION INCREASED, FLIGHT CREW SHUTDOWN ENGINE IN ACCORDANCE WITH OPERATING PROCEDURE AND RTURNED TO BASE. MAINTENANCE PERFORMED TEST 21 IN ACCORDANCE WITH ROLLS ROYCE PROCEDURES, ENGINE VIBRATIONS RETURNED TO NORMAL, AIRCRAFT RETURNED TO SERVICE. NO FURTHER REPORTED INCIDENTS.MAINTENANCE SUSPECT OIL HIDING AS CAUSE OF ENGINE VIBRATION . 2L73 4F4 F A23WE E12EU 20010405000772001040500077EA 2001 4 5 CA010307018 120010220G3232 BRACE CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF343B1 NE MLG DOOR SHEARED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AIRCRAFT 604-54F05 WITH TSN OF 611.3 HOURS AND 304 CYCLES HAS BEEN FOUND TO HAVE A BROKEN TRUNNION PIN AT L/H MLG SIDE BRACE ACTUATOR INBOARD END.THIS WAS FOUND AS THE AIRCRAFT WAS ON JACKS AND A TECHNICIAN NOTICED THAT THE GEAR MOVED. THE FORWARD ATTACH NUT WAS SHEARED OFF AND LAYING ON TOP OF THE WING. THIS ALLOWED THE PIN TO MIGRATE APPROXIMATELY 0.3 INCHES AFT, ALLOWING THE GEAR TO MOVE. PART REPLACED. BROKEN PART RETURNED TO BOMBARDIER FOR ANALYSIS.UNDER INVESTIGATION 2L72 4F4 FRTA21EA E15NE 20010405000782001040500078EA 2001 4 5 CA010307021 120010219G5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING THE PRE-FLIGHT INSPECTION, IT WAS NOTICED THAT THE CAPTAINS WINDSHIELD WAS CRACKED. THE AIRCRAFT RETURNED TO SERVICE AFTER REPLACEMENT OF THE WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010405000792001040500079NE 2001 4 5 CA010307024 220010219G7200 ENGINE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 FAILED W O OTHER J WARNING INDICATION DEDESCENT 1 CA (CAN) PILOT REPORT IN DESCENT: AUDIT ENGINE OIL AND MASTER WARNING. ENGINE NR 2 OIL PRESSURE RAPIDLY DROPPED TO 0 PSI. CREW INITATED AN IN-FLIGHT SHUTDOWN PROCEDURE, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PARTICLE ON NR 2 CHIP DETECTOR. AT THE TIME OF WRITING THE CAUSE FOR THE LOSS OIL PRESSURE HAS NOT BEEN DETERMINDED. THE CUSTOMER AND THE MANUFACTURER WILL CONTINUE THE INVESTIGATION. 2L72 4F4 FRTA21EA E15NE 20010405000802001040500080EA 2001 4 5 CA010307026 120010219G5730601R10046 PANEL CNDAIRCL600 CL6002B19 EA GE CF34 CF34* NE LT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 18652 (CAN) DURING A SERVICE CHECK, THE MECHANIC FOUND A SUSPECTED CRACK N THE LT WING LOWER SKIN AT WING STATION WS 148.019. THE CRACK WAS CONFIRMED WITH LPI AND EDDY CURENT NDT. THE REPAIR WAS CARRIED OUT PER REPAIR ENGINEERING ORDER 601R-57-21-130. THE AIRCRAFT SUBSEQUENTLY RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010405000812001040500081EA 2001 4 5 CA010307027 120010219G5730601R10046 PANEL CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 13895 (CAN) DURING A C CHECK INSPECTION, A CRACK WAS FOUND IN THE LOWER WING PLANK AT WING STATION WS 148.019.AT THE TIME OF REPORT, THE AIRCRAFT WAS STILL IN C CHECK. REPAIR ENGINEERING ORDER (REO) 601R-57-21-130 WILL BE APPLIED PRIOR TO RETURNING THE AIRCRAFT INTO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010405000822001040500082EA 2001 4 5 CA010307028 120010219G5600NP1393215 WINDOW CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA (CAN) WHILE MANOEUVRING ON THE GROUND, THE LT SIDE WINDOW WAS FOUND CRACKED. THE WINDOW WAS REPLACED AND THE AIRCRAFT RETURNED INTO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010405000832001040500083NE 2001 4 5 CA010307030 220010221G7200 ENGINE CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE LEFT FAILED W A UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 CA (CAN) ENGINE VIBRATION DURING CLIMB OUT AND LEVEL FLIGHT (FL230). MAXIMUM VALUE WAS 3.3 MILS. LATER FLUCTUATION BETWEEN 2.3 AND 3.3 MILS. ENGINE SHUT DOWN IN FLIGHT. SINGLE ENGINE OPERATION AS PER QRH. CHANGE LEFT ENGINE. REASON: HIGH N1 VIBRATION. 2L72 4F4 FRTA21EA E15NE 20010405000842001040500084EA 2001 4 5 CA010307033 120010222G5270601R317001 SENSOR CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE PASSENGER DOOR OUT OF ADJ W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CA (CAN) DURING CLIMB CREW RECD PASSENGER ENTRANCE DOOR WARNING MESSAGE PAX DR LATCH (AMBER) & PASSENGER DOOR (WARNING) EICAS MESSAGES. A/C RETURNED TO DEPTR AIRPORT&LANDED W/O INCID.&LATER FERRIED TO MAINT BA SE. MAINT FINDINGS: 1. PSEU FAULT LOG 2 RECORDED S47 & S46;2. FLT CREW RPT EICAS MESSAGES EXTINGUISHED BELOW 7000 ASI; 3. GREEN ALIGNMENT MARKS ON CAM LATCHES NOT WITHIN RANGE WHEN INNER DOORHANDLE IS SLOWLY ENGAGED; 4. PROX SENSOR PSSMB GAP .068 INCH, .018 INCH BEYOND LIMITS;5. A/C RECORDS SHOWN HAVE BEEN NO ADJUSTMENT MADE TO PSSMB SENSOR OR DOOR MECHANISM WITHIN PAST 30 DAYS. RECTIFICATION 1. PROX SENSOR PSSMB GAP ADJUSTED WITHIN LIMITS;2. INNER DOOR HANDLE STOP ADJUSTED;3. DOOR MECHANISM LUBRICATED A 2L72 4F4 FRTA21EA E15NE 20010405000902001040500090EA 2001 4 5 CA010308007 120010202G492049100011 APU CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE APU BAY DAMAGED W K NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CA (CAN) SMELL OF FUEL AND SMOKE IN AIRCRAFT AFTER APU STARTED ON DESCENT. EMERGENCY RESPONSE CALLED. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. APU REPLACED OPERATION AND LEAK CHECK CARRIED OUT AND SYSTEM CHECKED SERVICEABLE. 2L72 4F4 FRTA21EA E15NE 20010405000912001040500091EA 2001 4 5 CA010308010 120010212G2910AE3660010K0270 LINE CNDAIRCL600 CL6002B16 1900305EA HYDRAULIC SYSTEMCHAFED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A 60 MONTH/2400 HOUR INSPECTION, THE FLEXIBLE HYDRAULIC LINE (SUCTION TO THE ENGINE DRIVEN PUMP) OF THE NR 1 SYSTEM WAS FOUND TO HAVE CHAFED A HOLE THROUGH FUEL SHROUD SUPPLY LINE TO THE EDP.HYDRAULIC LINE P/N: AE3660010K0270FUEL SHROUD P/N: 601R62701-45 ACTT: 2261.5TOTAL LANDINGS: 1082 2L72 4F RTA21EA 20010405000922001040500092NM 2001 4 5 CA010308011 120010208G2497 WIRE BOEING737 7372Q9 138448MNM PWA JT8 JT8D9A 52048NE FIREWALL CHAFED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WIRE W200-453-06 CHAFED THROUGH INSULATION AND WIRE. LENGTH & WIDTH OF CHAFE IS 3/8 INCH, DEPTH 1/8 INCH. APPEARS TO HAVE RUBBED AGAINST COWLING AT SOME TIME. HOWEVER, AT TIME OF DISCOVERY, IT WAS NOT APPARENT WHAT THE WIRE HAD CHAFED. THERE HAD BEEN NO REPORTED ELECTRICAL POWER DEFECT. THE HARNESS HAS BEEN REPLACED WITH PARTICULAR EMPHASIS TO CORRECT ROUTING AND CLAMPING. 2L72 4F4 F A16WE E2EA 20010405000932001040500093NM 2001 4 5 CA010308012 120010219G2761654456113 ACTUATOR BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE SPOILER LEAKING W O OTHER K FLUID LOSS DEDESCENT 1 CA (CAN) AT APPROXIMATELY 20 MINUTES OUT, THE A SYSTEM HYDRAULIC LIGHT ILLUMINATED. THE HYDRAULIC FLUID GAUGE WAS CHECKED AND FOUND TO BE EMPTY. THE USE OF ALTERNATE FLAP AND GEAR EXTENSION WAS REQUIRED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE FIRE DEPARTMENT WAS ALERTED AND STANDING BY AS A PRECAUTION MEASURE. MAINTENANCE FOUND THE LEFT INBOARD FLIGHT SPOILER ACTUATOR LEAKING. 2L72 4F4 F A16WE E2EA 20010405000942001040500094CE 2001 4 5 CA010308013 120010212G551010138000110 BOOT BEECH B300 BEECH B300 B300 1159232CE PWA PT6 PT6A60A 52043NE HORIZ STAB DEICEDETACHED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 3880 FL26 (CAN) AIRCRAFT WAS IN CLIMBOUT FROM ST.JOHNS AIRPORT, AT 22,000 FEET, AIRSPEED 140 KNOTS, RATE OF CLIMB 1,800 F.P.M., PILOT EXPERIENCED SEVERE BUFFETING TO THE POINT THAT A/C WAS ABOUT TO STALL. STALL WARNING DID NOT ACTIVATE, A/C WAS PLACED IN LEVEL FLIGHT AND BUFFETING STOPPED. A/C RETURNED TO ST. JOHNS FOR MAINTENANCE. UPON INSPECTION MAINTENANCE DISCOVERED THAT THE RIGHT DE-ICER BOOT HAD DETACHED FROM THE HORIZONTAL STABILIZER ON THE OUTBOARD END. NEW DE-ICER BOOTS WRE INSTALLED ON THE LEFT AND RIGHT SIDE, A/C WAS TEST FLOWN ALL FLIGHT CHARACTERISTICS NORMAL. 2L72 4T4 TRTA24CE E4EA 20010405000952001040500095 2001 4 5 CA010313009 420010226G8300BP252 GEARBOX KAMOV KA32 KA32A1 SW ACCESSORY MAKING METAL W A UNSCHED LANDING J WARNING INDICATION HOHOVERING 1 CA 148 L20011007K (CAN) CAUTION SYSTEM - GEARBOX CHIP LIGHT, SMALL FLAT FLAKES FOUND IN OIL. 1G72 4U NC 20010405000962001040500096SW 2001 4 5 CA010313014 120010228G6220471401241 TUBE BELL 47 47G2 1181008SW LYC O435 VO435A1F 41516EA MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 79 (CAN) DURING DAILY INSPECTION ON MAIN CONTROL STABILIZER BAR AS PER AD 74-08-02. PILOT FOUND STABILIZER BAR TUBE WAS CRACKED. 1G71 3O3 O H1 E279 20010405000972001040500097NM 2001 4 5 CA010313015 120010304G2913570347 PUMP DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYD SYSTEM FAILED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA 137703804 MX452601C (CAN) HYDRAULIC PUMP FAILED CAUSING FAILURE OF NR 1 HYDRAULIC SYSTEM. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010405000982001040500098CE 2001 4 5 CA010313016 120010209G2435SBC9401 RELAY PRESTOLITE MHB4016 BEECH 76 76 1153005CE LT STARTER FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 10775 30000047 (CAN) LT ENGINE STARTER REMAINED ON AFTER SWITCHING STARTER OFF. STARTER RELAY HAD STUCK ON DUE TO ERRODED CONTACTS. STARTER SUBSEQUENTLY OVERHEATED AND FUSED ITSELF. THIS CONDITION CAUSED ALL ELECTRICAL POWER AVAILABLE FROM THE AIRCRAFT CHARGING SYSTEM AND BATTERY TO GO TO THE STARTER AS A DEAD SHORT, THEREFORE ALL ELECTRICAL SYSTEMS WENT COMPLETELY DEAD IN APPROXIMATELY 30 SECONDS. 1L72 3O A29CE 20010405000992001040500099CE 2001 4 5 CA010313017 120010215G7721RHM38E SPARK PLUG BEECH 76 76 1153005CE LYC O360 O360A1G6D EA ENGINE DAMAGED W A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 CA 300 (CAN) IN CRUISE PILOT REPORT RT ENGINE SURGING, THEN COMPLETELY ROUGH RUNNING. ENGINE SHUTDOWN, AIRCRAFT LANDED SAFELY. COMPRESSION TEST REVEALED ONE WEAK CYLINDER 50/80 PSI. BOTH SPARK PLUGS IN THAT CYLINDER SHORTED DUE TO BEING PEENED OVER BY FOREIGN OBJECT BOUNCING BACK AND FORTH IN CYLINDER. SUSPECT CERAMIC PIECE FROM A PLUG CAME OFF AND DID DAMAGE, HOWEVER PIECE NOT FOUND, NEW CYLINER ASSEMBLY INSTALLED, SPARK PLUGS ARE RECONDITIONED IN HOUSE USING CHAMPION PLUG CLEANER/TESTER. 1L72 3O3 O A29CE E286 20010405001492001040500149EA 2001 4 5 CA010313019 220010228G741410382681 CAPACITOR BENDIX D6LH3200 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA MAGNETO FAILED W K NONE R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 CA 124 (CAN) AIRCRAFT HAD FLOWN 2-3 HOURS ENGINE SHUT DOWN TO UNLOAD PASSENGERS. PILOT STARTED 1 ENGINE BUT 2ND WOULD NOT START. PROBLEM WAS INVESTIGATED AND CAPACITOR FOUND U/S. CAPACITOR REPLACED AND ENGINE STARTED. WE HAVE HAD 3 SUCH CASES IN THE LAST MONTH. WE HAE TESTED THE U/S CAPACITORS AS PER MANUFACTURERS INSTRUCTIONS AND CAPACITORS CHECK OUT SERVICEABLE. WE HAVE ALSO NOTICED THAT POINTS ARE NOT LASTING AS LONG IN THE MAGS. ALL CAPACITORS WERE REPLACED AS PER TELEDYNE CSB 662A. 1L72 3O3 O A20SO E14EA 20010405001542001040500154CE 2001 4 5 CA010313024 120010309G2431 BATTERY CESSNA172 172L 2072432CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160CTM GL MAIN BATTERY FAILED W A UNSCHED LANDING HGJELECT. POWER LOSS-50 PC MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 CA (CAN) PILOT ENCOUNTERED COMPLETE (GREATER THAN 50 PERCENT) ELECT. FAILURE IN FLT. AFTER ATTEMPTING TO GET A/C RADIOS TO TRANSMIT/RECEIVE, PILOT SQUAKED RADIO FAILURE CODE. FURTHER ATTEMTPS AT GETTING OTHER ELECT. SYSS TO FUNCTION, PILOT FOUND THAT ALL ELECT. SYS WAS UNSERVICEABLE. A/C RETURNED TO POINT OF DEPTR & THEN CONTACTED TOWER ON LAND LINE.AFTER BRIEF INSP , FOUND THAT A/C BATTERY COMPLETELY DISCHARGED. BATTERY (NEW & INST NOV.2000) ELECTROLYTE LEVEL INSP OK, BATTERY CHARGED OVERNIGHT. AFTER BATTERY CHARGED, GROUND RUN/FUNCTION CHECKED. NOTED WITH CHARGING SYS COMPLETELY LOADED UP, CHARGE IND. WEAK. SUSPECT BATTERY VOLTAGE INITY LOW & CHARGING SYS UNABLE TO KEEP UP WITH DE 1H71 3O3 ONT3A12 E274 5 NP910 20010405001552001040500155EU 2001 4 5 CA010313025 120010226G53023160S451010060 GUARD AEROSPSA316 SA315B 8680615EU TMECA ARTST3ARTOUSTE3B 60003EU TAIL ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2714 (CAN) WHILE CLEANING AIRCRAFT, AME FOUND CRACK COMING FROM UNDER BOTTOM CLAMP.NEW TAIL ROTOR GUARD WAS INSTALLED. 1G71 4U3 U H1IN E11N 20010405001592001040500159CE 2001 4 5 CA010314003 120010226G561010138402522 WINDSHIELD BEECH B300 B300 1159232CE PWA PT6 PT6A60A 52043NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA 5 (CAN) WHILE IN CRUISE FLIGHT AT FL310 AND OAT -50 DEGREES C, FLIGHT CREW OBSERVED RT WINDSHIELD OUTER PANE CRACK DEVELOP. CRACK WAS DIAGONAL IN LOWER INBOARD CORNER (APPROXIMATELY 6 INCHES). POH ABNORMAL CHECKLIST FOLLOWED AND FLIGHT RETURNED TO POINT OF DEPARTURE. 2L72 4T4 TRTA24CE E4EA 20010405001612001040500161WP 2001 4 5 CA010314007 220010312G723031037081 BEARING MTSBSIMU2 MU2B60 5780460CE GARRTTTPE331TPE33110 01514WP COMPRESSOR WRONG PART W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) GARRETT SB 72-0634 DATED AUG 17 1989 (OPTIONAL COMPLIANCE) LISTED COMPRESSOR BEARING P/N 3103708-1 AS REPL FOR P/N 3101405-1. BULLETIN APPLICABLE TO ALL MODELS OF TPE 331 ENGINE WHICH PREV HAD P/N 3101405-1 BEARING. SUBSEQUENT REVISION NR 1 TO SB DATED APR 27, 1990 DELETED SOME ENGINE MODELS FROM EFFECTIVITY LIST. ENGINE MODEL DELETED FROM LIST, HOWEVER IT NOT RECOMMENDED TO REMOVE ANY P/N 3103708-1 BEARINGS INST IN COMPLIANCE WITH T HE 1ST ISSUE OF SB- IN NOV 1998 P/N 3103708-1 BEARING INST INTO ENGINE. SUBSEQUENET REVIEW OF LIFE LIMITED COMPONENTS IN ENGINE, AGAINST REQMTS OF SB 72-0180 TBO REQMTS, INDICATED PART NO LONGER LISTED ON APPLICABLE LIFE LIMIT TABLES. 1H72 3T4 TRTA10SW E4WE 20010405001622001040500162NE 2001 4 5 CA010314009 320010218G61147827015 HUB DHAV DHC8 DHC8101 2809002NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE LT PROPELLER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9085 (CAN) DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT PROPELLER ASSEMBLY HAD EVIDENCE OF OIL LEAK. UPON FURTHER INVESTIGATION LEAK WAS FOUND TO BE COMING FROM NR 4 BLADE. AFTER REMOVING THE LEFT NR 4 BLADE THE OUTER BEARING RACE WITHIN THE PROPELLER HUB WAS FOUND TO BE CRACKED AND GALLED.LEFT PROPELLER HUB, PROPELLER ACTUATOR, AND 3 BLADES WERE REPLACED DUE TO OIL CONTAMINATION AND AN ADDITIONAL BEARING RACE FOUND GALLED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010405001672001040500167SO 2001 4 5 CA010314023 120010223G562045099013 WINDOW PIPER PA31T PA31T2 7103127SO PWA PT6 PT6A135 52043NE FUSELAGE BROKEN W A UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 CA 12355 (CAN) - THE AIRCRAFT WAS CLIMBING THROUGH 16,000 FEET WHEN THE CABIN PRESSURIZATION WAS LOST. - THE PILOTS INITIATED EMERGENCY DESCENT TO 10,000 FEET AND DECLARED EMERGENCY. - THE CAUSE FOR DEPRESSURIZATION WAS FOUND TO BE A BROKEN WINDOW IN THE CABIN AREA (3RD WINDOW ON LT SIDE).- AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. 1L72 3T4 TRTA8EA E4EA 20010405001682001040500168EA 2001 4 5 CA010314024 120010121G273022D1174A CONTROL CABLE SCWZERSG2 SGS233A 8051606EA ELEVATOR FRAYED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) BEARING ASSEMBLY AFT END OF TORQUE TUBE ASSEMBLY, LT MOUNT NUTCONTACTING CABLE. SUSPECT ANGLE BLOCK (FAIRLEAD) AFT END OF TORQUE TUBE ASSEMBLY AMPLIFIED DAMAGE TO CAUSE CABLE WEAR IN EXCESS OF 50 PERCENT. FURTHER INVESTIGATION ONGOING BY SCHWEIZER. 1K00 G2EA 20010405001692001040500169EU 2001 4 5 CA010314026 120010227G21339599091131 REGULATOR PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL CABIN PRESSURE CONTAMINATED W K NONE O OTHER ININSP/MAINT 1 CA 2649 (CAN) SAFETY VALVE FAILED TON OPEN WHEN CARRYING OUT 1500 HOUR PRESSURIZATION CHECK. FAILED SAFETY VALVE WAS REMOVED AND VALVE AND SENSE LINE WERE FOUND CONTAMINATED WITH JET FUEL. FUEL APPEARED TO HAVE COME FROM A PREVIOUSLY SEEPING FUEL FILTER BOWL SEAL AND HAD ENETRED THE OUTFLOW VALVE WHERE THE AMBIENT PRESSURE SENSE LINE PROTRUDES THROUGH THE PRESSURE BULKHEAD (APPROX 12 -14 INCHES AFT OF THE FUEL BOWL). 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010405001702001040500170SW 2001 4 5 CA010314027 120010223G3222 STRUT GULSTM112 112 0144701SW LYC O360 IO360C1D6 41514EA HARTZLHCE2Y HCE2YR1BF GL NLG CONTAMINATED W O OTHER J WARNING INDICATION LDLANDING 1 CA 1711 1711 (CAN) A/C HAD UNCOMMANDED NOSE GEAR RETRACTION UPON LDG. IT NOTICED DURING POWER PACK PRESSURE TEST THAT 700PSI ON UP SIDE WHEN GEAR EXTENDING & THAT PRESSURE WOULD NOT DECREASE BELOW 50-100 PSI WHEN GEAR WAS FULLY EXTENDED.RESIDUAL PRESSURE PREVENTING DETENT PINS FROM ENGAGING. HYDRAULIC POWER PACK REMOVED & DISASSEMBLED. FOUND ONE 8 OF INCH OF BLACK SLUDGE & 1 X 5 INCH PIECE OF PAPER IN RESERVOIR.VALVE BODY ALSO DISSASSEMBLED. FOUND GEAR UP CHECK VALVE O-RING HARD & BRITTLE & SEATS OF MOST OF VALVES COVERED WITH SLIMY GOO. NOSE GEAR ACTUATOR DISASSEMBLED. MAIN PRESSURE O-RING MS28775-117 NOTICED TO BE ROLLED. 1L71 3O3 O A12SO 1E10 5 CP9EA 20010405002212001040500221EA 2001 4 5 CA010320010 120010308G5610NP1393212 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) RT WINDSHIELD INNER PLY FOUND CRACKED, UNIT REPLACED AND AIRCRAFT BACK IN SERVICE. 2L72 4F4 FRTA21EA E15NE 20010405002222001040500222EA 2001 4 5 CA010320013 120010308G3234 HANDLE CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE MLG SELECTOR FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) DURING CLIMBOUT LANDING GEAR WOULD NOT RETRACT, ANTI-SKID FAIL MESSAGE SHOW ON EICAS. MAINTENANCE REPLACED LANDING GEAR HANDLE AND AIRCRAFT BACK IN SERVICE. 2L72 4F4 FRTA21EA E15NE 20010405002232001040500223 2001 4 5 CA010320014 420010308G34178220371140 ADC CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE E/E BAY FAILED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) DURING CRUISE STABILIZER TRIM CH2 AND MACH TRIM FAILED. MAINTENANCE REPLACED ADC AND AIRCRAFT BACK IN SERVICE. 2L72 4F4 FRTA21EA E15NE 20010405002242001040500224CE 2001 4 5 CA010320018 120010228G2820120010679 LINE CESSNA206 U206G 2073356CE CONT O550 IO550F 17042SO FUEL DISTRIBUT CHAFED W K NONE O OTHER ININSP/MAINT 1 CA 1970 (CAN) LINE ASSEMBLY - FUEL, STRAINER TO ELBOW FOUND CHAFING AGAINST RT NOSE GEAR STEERING BOOT.1.50 INCH X 0/032 INCH TUBING FOUND WORN BY 0/018 INCH ON ONE SIDE. PART HAS BEEN REPLACED WITH A NEW LINE ASSEMBLY - FUEL AND PROTECTED WITH NYLON SPIRAL WRAP. 1H71 3O3 O A4CE E3SO 20010405002272001040500227EU 2001 4 5 CA010320021 120010214G2910 LINE AIRBUS310 A310304 EU GE CF6 CF680C2A5 NE HYDRAULIC SYS LOOSE W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) PILOT OBSERVED GREEN SYSTEM HYDRAULICS WAS LOOSING FLUID. AIRCRAFT DIVERTED TO YYT. HYDRAULIC LINE IN NR 1 ENGINE PYLONFOUND LOOSE. LINE TIGHTENED AND LEAK CHECK CARRIED OUT SERVICEABLE. 2L72 4F4 FRTA35EU E13NE 20010405002332001040500233SO 2001 4 5 CA010322002 120010208G3242 LINER PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360EB 17025SO BRAKES DESTROYED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 43 (CAN) WHILE CONDUCTING A GENERAL WALK AROUND FOR A PRE-PURCHASE, THE INBOARD PRESSURE PLATE SIDE OF THE BRAKE CALIPERS, THE BRAKE LINERS WERE TOTALLY DESTROYED, RESULTING IN THE STEEL PRESSURE PLATE TO COME IN FULL CONTACT WITH THE BRAKE DISC WHICH CREATED DEEP GROOVES AND SIGNIFICANT AMOUNT OF HEAT TO DISCOLOR THE PRESSURE PLATES AND DISCS. 1L72 3O3 O A7SO E9CE 20010405002392001040500239NM 2001 4 5 CA010322012 120010317G4920 COMPRESSOR BOEING737 737281 138448PNM PWA JT8 JT8D17 52049NE APU MAKING METAL W K NONE O OTHER ININSP/MAINT 1 CA 41944881 (CAN) THE AIRCRAFT WAS CLIMBING OUT OF VANCOUVER WHEN THE APU DID AN AUTO SHUT DOWN AND THE APU FIRE HANDLE ILLUMINATED. THE FIRE HANDLE WAS PULLED BUT THE BOTTLE WAS NOT DISCHARGED DUE TO THE FIRE INDICATION GOING OUT. THE AIRCRAFT RETURNED TO VANCOUVER WHERE THE APU AREA WAS INSPECTED AND NO EVIDENCE OF A FIRE WAS DISCOVERED. THE APU WAS PLACED ON MEL AND THE AIRCRAFT WAS RELEASED TO SERVICE. FURTHER INVESTIGATION LATER IN THE DAY FOUND THAT THERE WAS METAL FRAGMENTS FOUND IN THE INTAKE OF THE APU AND THE APU WAS REMOVED FROMTHE AIRCRAFT. IT WILL BE RETURNED TO THE OVERHAUL FACILITY FOR DISASSEMBLY AND REPAIR. 2L72 4F4 F A16WE E2EA 20010405002402001040500240EU 2001 4 5 CA010323002 120010217G2701AS2219 CONTROL CABLE SIREN S1609 SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE CARGO HOOK BROKEN W O OTHER O OTHER CLCLIMB 1 CA 876 (CAN) MANUAL / EMERGENCY RELEASE CABLE SHEATH BROKEN AWAY FROM FERRULE / SLEEVE WHERE CABLE ASSEMBLY ATTACHES TO THE CARGO HOOK.THE CARGO SUSPENSION SYSTEM (SWING) ALLOWS FOR A LOT OF MOVEMENT OF THE CARGO HOOK. THERE APPEARS TO BE A LOT OF FLEXING OF THE CABLE ASSY WHERE IT ATTACHES TO THE CARGO HOOK LEADING TO FAILURE OF THE CABLE SHEATH.THIS FAILURE RESULTED IN AN UNCOMMANDED LOAD RELEASE. 1G71 3U3 U H9EU E19EU 20010405002412001040500241NE 2001 4 5 CA010323003 220010309G75302496722 WASHER BENDIX 153212A DHAV DHC8 DHC8* NM PWA 120 PW120 NE VALVE SEALS CRACKED W K NONE O OTHER ININSP/MAINT 1 CA RF4252 (CAN) COMPRESSION WASHER CRACKED AND JAMMED BETWEEN THE VALVE SEAL AND SEALING SURFACE PREVENTING THE A SIDE FROM COLOSING. 2H72 4T4 TRTA13NM E20NE 20010405002432001040500243EA 2001 4 5 CA010323005 120010314G5530C6TFM102529 ADAPTER DHAV DHC6 DHC6 2802606EA VERTICAL STAB FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) LOWER LT MOUNTING / MATING SURFACE INCORRECTLY MACHINED. SURFACE WAS MACHINED CYLINDRICALLY INSTEAD OF SPHERICAL CONVEX. IF INSTALLED THE MATING SURFACES WOULD NOT MATCH CAUSING STRESS AND POSSIBLE FAILURE OF THE MOUNT. CONCERNED THAT MORE WERE PRODUCED AND INSTALLED FROM THE SAME BATCH. 1H72 3T RTA9EA 20010405002442001040500244SO 2001 4 5 CA010323006 120010307G7721LW16740 EXHAUST VALVE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA NR 5 CYLINDER BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 1724 (CAN) PILOT REPORTED HIGH OIL TEMP VERNATHERN REPLACED AND ON GROUND RUN ENGINE RAN ROUGH. LARGE AMOUNT OF OIL NOTED COMING FROM SNIFFLE VALVE MIXED WITH FUEL. SPARK PLUGS REMOVED AND FOUND THOSE REMOVED FROM NR 5 CYLINDER WERE DAMAGED. REMOVED CYLINDER AND FOUND 1/3 OF VALVE FACE (EXHAUST) MISSING. REPLACED CYLINDER AND CHECKED ALL SCREENS AND FILTERS. 1L72 3O3 O A20SO E14EA 20010405002462001040500246CE 2001 4 5 CA010323008 120010302G5751991300003 SKIN BEECH 100 100BEECH 1152916CE PWA PT6 PT6A28 EA RT AILERON CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 13438 (CAN) WHEN CHECKING SB 57-3148 IT WAS NOTICED THAT THIS AILERON WAS ALSO CRACKED AS PER SB 57-3148. KIT 109-4011-1 INSTALLED. 1L72 3T4 T A14CE E4EA 20010405002492001040500249CE 2001 4 5 CA010323011 120010313G561011450431S WINDSHIELD BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE COCKPIT CRACKED W O OTHER O OTHER DEDESCENT 1 CA 7057 (CAN) ON DESCENT IN YWG PILOT HEARD SNAPING AND CRACKING AS THE OUTER LAYER OF LT WINDSHIELD SHATTERED. THEY DESCENDED TO YWG ASKING FOR PRIORITY LANDING WITHOUT INCIDENT. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20010405002502001040500250CE 2001 4 5 CA010323013 120010315G7603S351 CLAMP CESSNA CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA THROTTLE CABLE LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THROTTLE SHEAF HAD VIBRATED LOOSE FROM CONNECTING CLAMP WHICH LEFT NO CONTROL FOR THROTTLE ADJUSTMENT. THROTTLE CABLE WAS RE-POSITIONED IN THE SHEAF AND NEW HARDWARE WAS INSTALLED.AIRCRAFT WAS GROUND UN AND ALL PARAMETERS NORMAL. 1H71 3O3 ONT3A12 E274 20010416004582001041600458SO 2001 4 16 CA010402004 120010306G78105005500 EXHAUST STACK PIPER PA31T PA31T 7103124SO PWA PT6 PT6A28 EA ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AFTER A FLIGHT, THE PILOTS REPORTED A CRACK AT THE INNER WELD SEAM OF THE LE OUTBOARD EXHAUST STACK. 1L72 3T4 T A8EA E4EA 20010416004592001041600459CE 2001 4 16 CA010402005 120010310G531005121871 DOOR FRAME CESSNA172 172M 2072418CE LYC O320 O320E3D 41508EA FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 8970 (CAN) LOWER AFT DOOR POSTS INSPECTED PER SEB 97-1 AND FOUND LT CRACKED. INSTALLED SERVICE KITS SK172-149-1 AND -2 TO CORRECT. 1H71 3O3 ONT3A12 E274 20010416004602001041600460NM 2001 4 16 CA010402006 120010309G572082710038101 FITTING DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE RUDDER PEDAL CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 28935 (CAN) THE PART WAS CRACKED TWO-THIRDS OF THE CIRCUMFERENCE AROUND THE RAISED BOSS (CASTING) NEAR THE RADIUS. THE TOP END FITTING WAS REPLACED IN ACCORDANCE WITH THE MAINTENANCE MANUAL AND CHECKED - SERVICEABLE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010416004662001041600466EA 2001 4 16 CA010403003 120010313G5340601350061 BEAM 60135006 CNDAIRCL600 CL6002B19 EA GE CF34 CF341A NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING C-CHECK A CRACK WAS FOUND IN THE ENGINE SUPPORT BEAM LOWER WEB BETWEEN FS 625.30 AND FS 640.00 NEAR LBL 36.20. THE CRACK WAS LOCATED IN THE CORNER OF ACCESS PANEL (P/N 601-35006-39) LANDING AND ENDED NEAR THE PANEL EDGE. 2L72 4F4 FRTA21EA E15NE 20010416004672001041600467EA 2001 4 16 CA010403004 120010313G5610601R330339 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER DEDESCENT 1 CA (CAN) PILOT REPORT LT WINDSHIELD INNER PLY BOTTOM LOWER CORNER CRACKED. WINDSHIELD REMOVED AND REPLACED. 2L72 4F4 FRTA21EA E15NE 20010416004682001041600468EA 2001 4 16 CA010403006 120010314G4920 APU CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE APU BAY FIRE W F ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 CA (CAN) APU CAUGHT FIRE ON THE GROUND AFTER LANDING.FIRE WAS EXTINGUISHED BUT RELIT. FIRE DEPARTMENT EXTINGUISHED IT FOR GOOD. APU WAS REPLACED. 2L72 4F4 FRTA21EA E15NE 20010416004692001041600469EA 2001 4 16 CA010403007 120010314G5730 PANEL CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE LT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) LT WING PLANK CRACKED AT WS 148.019 FOR ABOUT 1.2 INCHES LONG. THE RT HAS NO CRACK. THEY WILL PERFORM THE REO 601R-57-21-130. 2L72 4F4 FRTA21EA E15NE 20010417000982001041700098EA 2001 4 17 CA010403011 120010306G7603C3CE12 CABLE DHAV DHC3 DHC3 2800202EA PWA R1340 R1340* 52016NE THROTTLE BROKEN W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) DURING THE PRE-FLIGHT RUN-UP, THE THROTTLE CONTROL WAS NOT RESPONDING PROPERLY. INVESTIGATION FOUND THAT THE FLEX CABLE WAS BROKEN INSIDE THE TUBING. 1H71 3R3 R A815 5E2 20010417000992001041700099EA 2001 4 17 CA010403012 120010305G7721357285 CYLINDER DHAV DHC3 DHC3 2800202EA PWA R1340 S3H1G 52016NE NR 3 CRACKED W O OTHER E VIBRATION/BUFFET CRCRUISE 1 CA 1184 (CAN) DURING A FLIGHT THE PILOT WAS FEELING AN ENGINE VIBRATION. HE REDUCED POWER AND CONTINUED HIS FLIGHT. ON MAINTENANCE THE NR 3 CYLINDER WAS FOUND CRACK FROM FRONT SPARK PLUG HOLE TO THE REAR. 1H71 3R3 R A815 E142 20010417001302001041700130NE 2001 4 17 CA010403013 220010312G8530357285 HOUSING DHAV DHC3 DHC3 2800202EA PWA R1340 S3H1G 52016NE ROCKER BROKEN W A UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 CA 1199 (CAN) DURING A FLIGHT, THE PILOT FELT AN ENGINE VIBRATION AND POWER REDUCTION. HE LANDED ON A LAKE. MAINTENANCE FOUND A CYLINDER WITH ROCKER HOUSING BROKEN. 1H71 3R3 R A815 E142 20010417001312001041700131CE 2001 4 17 CA010403014 120010312G552050350055 FITTING CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO LT ELEVATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 12195 (CAN) - LEFT ELEVATOR FITTING FOUND CRACKED AT UPPER HOLE. NEW FITTING P/N 5035005-3 INSTALLED. 1L72 3O3 O A7CE E8CE 20010417001322001041700132SO 2001 4 17 CA010403015 120010219G3242492152 VALVE PIPER PA44 PA44180 7104402SO PARKING BRAKE BENT W O OTHER O OTHER APAPPROACH 1 CA 3818 (CAN) PILOT REPORTED PARK BRAKE APPLYING ITSELF. NOTICED ONCE ON TAKEOFF ONCE ON LANDING. CONFIRMED BY APPLYING SLIGHT PRESSURE TO PARK BRAKE SELECTOR TO THE OFF POSITION. UNIT REPLACED WITH SERVICEABLE UNIT, WHICH WAS SERVICED WITH NEW O-RINGS AND SYSTEM BLED GROUND CHECKED OK. 1L72 3O A19S0 20010417001332001041700133EA 2001 4 17 CA010404002 120010305G323183231014003 ROD DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE LT MLG DOOR BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 22260 (CAN) ON WALKAROUND INSPECTION, THE LT AFT OUTBOARD MLG DOOR ACTUATING ROD WAS FOUND TO BE BROKEN. THE DOOR OPENING ASSIST SPRING PN 83231020-003VP WAS ALSO FOUND BROKEN. THE SPRING HAD FRACTURED IN THE MID COIL AREA AND SPECULATION IS THAT THE BROKEN SPRING FOULED THE DOOR ACTUATING ROD DURING THE LAST LANDING GEAR EXTENSION, KINKING AND BREAKING THE ROD. ROD AND SPRING WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010417001342001041700134EA 2001 4 17 CA010404003 120010308G2820DSC33810D FITTING DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE FUEL SYSTEM LEAKING W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) THE FLIGHT CREW REPORTED THE NR 1 -FUEL LOW PRESS- CAUTION LIGHT WOULD ILLUMINATE AS SOON AS THE AUXILIARY FUEL PUMP WAS SELECTED OFF, BUT THE LIGHT WOULD GO OUT AT LOW POWER SETTINGS. MAINTENANCE INVESTIGATION REVEALED THAT A FITTING ON THE MOTIVE FLOW LINE INSIDE THE FUEL TANK COLLECTOR BAY WAS LEAKING AND LIMITING THE OUTPUT FROM THE EJECTOR PUMPS IN THE FUEL TANK. THE O-RINGS INSIDE THE FITTING WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. TTAF 22,271 TCAF 32,957. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010417001362001041700136EA 2001 4 17 CA010404005 120010313G21307G959 PRESSURE SWITCH DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE NR 1 ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE FLIGHT CREW REPORTED THAT THEY HAD NO HIGH BLEED ON EITHER ENGINE. MAINTENANCE INVESTIGATION REVEALED THAT THE NR 1 ENGINE HIGH PRESSURE >65 PSI SWITCH WAS OUT OF TOLERANCE AND REPLACED IT. THE AIRCRAFT WAS RETURNED TO SERVICE. THE NR 1 & 2 ENGINE HIGH BLEED SWITCHES OPERATE IN SERIES THROUGH A COMMON DELAY RELAY, THUS FAILURE OF ONE SWITCH WILL INHIBIT SWITCHING ON BOTH ENGINES. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010417001372001041700137NM 2001 4 17 CA010404006 120010319G323183232086001 ROD END DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE MLG DOOR BROKEN W O OTHER O OTHER CLCLIMB 1 CA (CAN) THE FLIGHT CREW REPORTED AN AIRFRAME HOWL AFTER TAKEOFF AND LANDING GEAR RETRACTION. MAINTENANCE INVESTIGATION REVEALED A BROKEN ACTUATING ROD FOR THE RT AFT NOSE LANDING GEAR DOOR. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010417001382001041700138NE 2001 4 17 CA010404007 220010312G7200 ENGINE BOEING737 737217 1384464NM PWA JT8 JT8D17A 52049NE NR 2 VIBRATION W A UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 CA 47894930 (CAN) A/C 722, MAR 12/2001, YQX, LOG SEQUENCE 0295200. TOP OF DESCENT WHEN THRUST LEVERS RETARDED, NR 2 ENGINE VIBRATION WAS INDICATING 2 MILS ON INLET AND 3.5 ON TURBINE. NR 2 START LEVER WAS VIBRATING. TRIED ENGINE ANTI-ICE AND THROTTLE MOVEMENT, WITH NO CHANGE IN VIBRATIONS. ENGINE NR 2 THRUST LEVER RETARDED AND VIBS THEN REDUCED, BUT REMAINED RUMBLING UNTIL ENGINE WAS SHUTDOWN. AIRCRAFT DIVERTED TO GANDER. NR 2 ENGINE WAS REPLACED AS PER WORK CARD 1125-2. 2L72 4F4 F A16WE E2EA 20010417001432001041700143WP 2001 4 17 CA010405002 120010328G6210369D21100523 BLADE HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2269 (CAN) UPPER AND LOWER SKIN CRACKED AT STN 36.5. CRACKED FROM TRAILING EDGE TOWARDS LEADING EDGE 4.25 INCHES. 1G71 3U3 U H3WE E4CE 20010417000242001041700024CE 2001 4 17 CA010405005 120010302G30001143800465 HOSE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT BRAKE ASSY BLOWN W O OTHER J WARNING INDICATION CRCRUISE 1 CA (CAN) PILOT REPORTED LT BRAKE DEICE FAIL LIGHT CAME ON IN FLIGHT. DEICE SYSTEM WAS TURNED OFF AND AIRCRAFT CONTINUED TO DESTINATION. UPON MAINTENANCE INVESTIGATION, THE FLEXIBLE BLEED AIR HOSE ASSY CARRYING HOT AIR TO BRAKE ASSY WAS FOUND BLOWN. THE LINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA24CE E4EA 20010417000292001041700029SO 2001 4 17 CA010406008 220010321G8500 ENGINE CESSNA421 421C 2076016CE CONT O520 GTSIO520M 17032SO RIGHT FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CA 95 (CAN) PILOT/OWNER REPORTED NORMAL PRE-TAKEOFF START/RUN-UP PROCEDURES. NORMAL TAKEOFF WABASCA, ALBERTA, IN ROUTE, EXPERIENCED A SURGE (OVERBOOST) RT ENGINE. ADJUSTED POWER BACK TO CRUISE, LT AND RT. WHILE ADJUSTING MIXTURE - RIGHT ENGINE ''THE ENGINE BLEW UP''. ENGINE SHUT DOWN AND PROPELLER FEATHERING PROCEDURES CARRIED OUT. PILOT ELECTED TO CONTINUE FLIGHT TO CYEG. ENGINE TO BE REMOVED AND SENT FOR INVESTIGATION/REPAIR - FURTHER REPORT PENDING. 1L72 3O3 O A7CE E7CE 20010417000312001041700031EA 2001 4 17 CA010406010 220010316G852011F20022D3 CRANKCASE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA RT ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 4946 1340 (CAN) DURING ROUTINE 50 HR INSP, BROKEN CYLINDER HOLD DOWN STUD FOUND SITTING IN BOTTOM OF ENGINE COWLING. LATER INVEST., BROKEN STUDS ORIG LOCATION LOCATED ON FRONT INNER CYLINDER OF RT ENGINE. UPON CONSULTATION WITH AERO RECIP ENGINES OF WINNIPEG, MANBITOBA, REMOVAL OF CYLINDER COMPLETED FOR FURTHER INVEST. ONCE REMOVED, IT FOUND THAT BROKEN STUD NOT THROUGH BOLT BUT NORMAL SHORT STUD. ANY FURTHER DISCUSSION ABAUG FURTHER REPAIRS OF HOLD DOWN STUD HALTED ONCE LARGE CRACK OF AT LEAST 6 IN FOUND AHEAD OF AFFECTED CYLINDER ON CRANK CASE. CRACK WOULD POSSIBLY NOT HAVE BEEN DETECTED AS IT NOT AL ALL CLEARLY VISIBLE UNTIL REMOVAL OF CYLINDER. 1L72 3O3 O A20SO E14EA 20010417000322001041700032CE 2001 4 17 CA010406011 120010316G243523085001 STARTER GEN BEECH B300 B300 1159232CE PWA PT6 PT6A60A 52043NE RIGHT FAILED W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 CA 288 2518 (CAN) WHILE IN CRUISE FLIGHT THE RT GENERATOR FELL OFF LINE AND WOULD NOT RESET. AIRCRAFT CONTINUED TO FUEL STOP AIRPORT. MAINTENANCE DISCOVERED FAULTY STARTER/GENERATOR WITH OBVIOUS DAMAGE TO FORWARD (DRIVE SPLINE END) BEARING. GENERATOR SENT FOR OVERHAUL WITH REQUEST FOR BEARING EVALUATION. 2L72 4T4 TRTA24CE E4EA 20010417000442001041700044SO 2001 4 17 CA010409010 220010329G731464621011A3 PUMP CESSNA340 340A 2076405CE CONT O520 TSIO520NB 17040SO LT ENGINE FUEL FAILED W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CA 445 (CAN) LT ENGINE WOULD NOT RUN WITHOUT AUXILIARY ELECTRIC FUEL PUMP ON HIGH. FUEL PUMP AT DRIVE REPLACED, GROUND CHECKED OK. 1L72 3O3 O 3A25 E8CE 20010417000452001041700045CE 2001 4 17 CA010409017 120010227G3240AE2463509GO150 HOSE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE MLG BRAKES LEAKING W O OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 CA 1214 (CAN) FLIGHT CREW REPORTED RT BRAKE SOFT, AND BRAKE PRESSURE LOW WARNING ON, CREW LANDED AIRCRAFT NORMALLY USING THRUST REV. AND BRAKES. MAINTENANCE FOUND LEAKING BRAKE HOSE, HOSE REPLACED, BRAKE SYSTEM BLEED.HOSE DATE: AEROQUIP TELFLON HOSE (FOR SKYDROL BRAKE FLUID) A/PT 04-98, 3000 PSI. 2L72 4F4 FRTA22CE E25EA 20010417000462001041700046CE 2001 4 17 CA010409018 120010326G551004320049 BRACKET CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9135 (CAN) FOUND DURING INSPECTION FOR 80-11-04 NUTPLATES FOR CRACKS, ALSO TRANSPORT CANADA SDA AV-2000-06. 1H71 3O3 ONT3A19 E223 20010417000472001041700047CE 2001 4 17 CA010409019 120010321G551004320041 BRACKET CESSNA150 150F 2071814CE CONT O200 O200A 17020SO HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 5116 (CAN) FOUND DURING INSPECTION FOR 80-11-04 NUTPLATES FOR CRACKS. ALSO SDA AV-2000-06. AFFTER REMOVAL OF BRACKET ALSO FOUND REAR SPAR REINFORCEMENT P/N 0432001-15 CRACKED (HOLES ARE ALSO ELONGATED) ALONG TOPSIDE, AFTER REMOVAL OF REAR SPAR. REINFORCEMENT BOTH L/H AND R/H SPARS P/N 0432001-56. 1H71 3O3 O 3A19 E252 20010417000482001041700048CE 2001 4 17 CA010409020 120010326G551004320049 BRACKET CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA MCAULY1A103 1A103TCM GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 13221 (CAN) FOUND DURING INSPECTION FOR 80-11-04 NUTPLATES FOR CRACKS, ALSO TRANSPORT CANADA SDA AV-2000-06. 1H71 3O3 ONT3A19 E223 5 NP50GL 20010417000492001041700049 2001 4 17 CA010410006 420010322G3418 COMPUTER CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE STALL WARNING FAILED W O OTHER J WARNING INDICATION CLCLIMB 1 CA (CAN) STALL FAIL MESSAGE AFTER GEAR UP. MAINTENANCE CARRY LRU DIAGNOSTICS AND OPERATIONAL CHECK, NO FAULT FOUND AT THIS TIME AND AIRCRAFT BACK IN SERVICE. 2L72 4F4 FRTA21EA E15NE 20010417000502001041700050EA 2001 4 17 CA010410008 120010322G5610 WINDOW CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA (CAN) DURING CRUISE SIDE WINDOW SHATTERED, CREW DIVERTED AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED SIDE WINDOW. 2L72 4F4 FRTA21EA E15NE 20010417000512001041700051EA 2001 4 17 CA010410009 120010322G4920 APU CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE APU BAY FAILED W F ACTIVATE FIRE EXT. A FLAME/FIRE ININSP/MAINT 1 CA (CAN) APU SELECTED DURING DESCENT, FIRST TIME DID NOT START, PILOT RESELECT APU START. SECOND TIME APU START WITHOUT ANY INCIDENT. AIRCRAFT PULLED UP TO THE GATE, MAINTENANCE MET PILOT AT THE AIRCRAFT, ENGINE HAD BEEN SHUTDOWN WITH THE APU RUNNING. MAINTENANCE FOUND FIRE COMING OUT OF THE EXHAUST, PILOT EXECUTED THE FIRE EMERGENCY MEMORY ITEMS AND CONTACTED THE FIRE DEPARTMENT. FIRE DEPARTMENT SHOWED UP AND SPRAYED THE APU COMPARTMENT WITH EXTINGUISHANT.APU AND APU FIRE SYSTEM DEFERRED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010417000522001041700052EA 2001 4 17 CA010410010 120010322G3040601R330339 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA 1353 (CAN) AFTER LANDING CREW REPORT LT WINDSHIELD SHATTERED. MAINTENANCE REMOVED AND REPLACED WINDSHIELD AND AIRCRAFT BACK IN SERVICE. 2L72 4F4 FRTA21EA E15NE 20010417000532001041700053EA 2001 4 17 CA010410012 120010322G2421755469B IDG CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE NR 1 DAMAGED W EA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA 1323313233 (CAN) DURING CRUISE, CREW NOTED AN IDG NR 1 FAULT MESSAGE, FOLLOWED BY OIL PRESSURE FLUCTUATIONS, OIL PRESSURE WARNING. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT MADE AN UNEVENTFUL SINGLE ENGINE LANDING. MAINTENANCE INVSTIGATION SUGGEST THAT IDG DISCONNECT DID NOT ACTIVE. IDG, ACCESSARY GEAR BOX AND LUBE/SCAVENGE PUMP WERE REMOVED AND REPLACED. OIL FILTER AND OIL SAMPLE WERE SENT FOR ANALYSIS.AIRCRAFT HAS RETURNED IN SERVICE. 2L72 4F4 FRTA21EA E15NE 20010417000542001041700054EA 2001 4 17 CA010410014 120010324G5610NP1393216 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA 2877 (CAN) ENROUTE ATLANTA TO COLUMBIA SC, FIRST OFFICERS WINDSHIELD SHATTERED. CREW LANDED UNEVENTFULLY IN COLUMBIA.THE DAMAGE TO THE WINDSHIELD IS ON THE INNER SURFACE AND GLASS FRAGMENTS WERE FOUND ON THE GLARESHIELD BY MAINTENANCE. WINDSHIELD WAS REPLACED AND TESTED I.A.W. AMM. 2L72 4F4 FRTA21EA E15NE 20010417000552001041700055EA 2001 4 17 CA010410023 120010330G5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER DEDESCENT 1 CA 40 (CAN) ON DESCENT INTO WICHITA THE LT WINDSHIELD CRACKED. AIRCRAFT WAS FERRIED TO MEMPHIS AND THE WINDSHIELD WAS REPLACED. 2L72 4F4 FRTA21EA E15NE 20010417000562001041700056EA 2001 4 17 CA010410025 120010402G5610NP1393212 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) THE RT WINDSHIELD MIDDLE PLY WAS FOUND CARACKED AIRCRAFT ON PARKING. THE AIRCRAFT DID A FERRY FLIGHT TO MORLAIX. THE WINDSHIELD WAS REPLACED AT THE MAINTENANCE BASE AS PER AMM 56-11-01. 2L72 4F4 FRTA21EA E15NE 20010417000572001041700057EA 2001 4 17 CA010410027 120010402G5210601R3189233 ROD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE PAX DOOR FAILED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) IN PITT DURING TURN AROUND, FLT ATTENDANT & CREW WERE UNABLE TO CLOSE MAIN PASSENGER DOOR. AFTER MULTIPLE ATTEMPTS CREW WERE ABLE TO CLOSE DOOR BUT WERE UNABLE TO RE-OPEN FROM INSIDE. NORTHWEST AIRLINK MAINT, ENGINEERING & BOMBARDIER FSR WERE SENT TO PITT TO VERIFY REPORTED EVENT. IT NOTICED THAT WHEN ATTEMPTING TO SLOWLY CLOSE DOOR FROM INSIDE HANDLE WOULD JAM HALF WAY. WHILE HAVING HANDLE HALF WAY, TORQUE TUBES GREEN LINES WERE ALIGNED, WITH SECONDARY LOCK ALIGNMENT LINE OFF BY APPROX 3/4 OF AN INCH. FLAPPER DOOR ALSO NOT FULLY CLOSED. LATCH BOX ASSY & ACTUATING RODS HAD NO VISUAL DEFECTS.THE RIG PINS WERE INST PER AMM. THE CNTL ROD ASSY 2L72 4F4 FRTA21EA E15NE 20010417000582001041700058EA 2001 4 17 CA010410030 120010403G5610601R2303310 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER DEDESCENT 1 CA (CAN) THE RT WINDSHIELD INNER PLY CRACKED WHILE THE AIRCRAFT WAS IN DESCENT. THE WINDSHIELD WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010417000592001041700059SO 2001 4 17 CA010411003 120010315G53414A0021001 TAPER PIN EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA WING CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AIRCRAFT TT: 18965.4 HRS CYC: 24946 PART TT: APP. 7200 HRS. IF REPLACED AT LAST C12 INSP. TAPER PIN CONE BUSHINGS ALSO AFFECTED. PIN DID NOT COME OUT WITH MANUFACTURERS SPECIAL TOOL PRESS. NEW PINS AND CONES REQUIRED. PIN HAD TO BE DRILLED AND CUT BY MACHINIST.IT APPEARS ITL P/N 1027251T2, MASTINOK 6856K JOINTING COMPOUND MADE BY PRC PESOTO INTERNATIONAL HAS NOT BEEN UTILIZED AT INSTALLATION AS SPECIFIED. 1L72 4T4 T A21SO E4EA 20010417000602001041700060EA 2001 4 17 CA010411004 120010312G5300 SKIN FRCHLDF27 F27F 3373008EA RROYCEDART DART5297E 54507EU FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 36671 (CAN) CRACK FOUND AT TOP REAR CORNER OF FRONT CARGO DOOR FRAME (FUSELAGE). THE PROBLEM IS ONE BAD FLUSH RIVET CRACK FROM RIVET TO SKIN EDGE. CRACK FOUND ON DAILY INSPECTION.REPAIR DONE AT STATION 181.102 AND 14 INCH ABOVE W.L. 0 LINE. 2H72 4T4 T 7A1 E297 20010417000612001041700061CE 2001 4 17 CA010411008 120010316G2822RG34720A PUMP BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA FUEL BOOST LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA 853 (CAN) CARRYING OUT A DAILY INSPECTION ON MARCH 16, AFTER RETURNING FROM A TRAINING FLIGHT. FOUND THAT THE ENGINE DRIVEN FUEL BOOST PUMP P/N 91-38003 THAT IS MOUNTED ON THE REAR OF ENGINE S/N PCE-81053 WAS LEAKING FUEL AROUND THE BASE OF THE VALVE THAT IS INSTALLED ON THE FUEL BOOST PUMP.ORDERED A NEW FUEL PUMP FROM TC STORES IN OTTAWA INSTALLED ON AIRCRAFT AND FOUND IT TO BE SERVICEABLE FOR FLIGHT, NO LEAK FOUND. 1L72 4T4 T A24CE E4EA 20010417000622001041700062EA 2001 4 17 CA010411011 220010326G7230 COMPRESSOR PWA PT6 PT6A28 EA ENGINE FAILED W K NONE C F.O.D. ININSP/MAINT 1 CA (CAN) THE COMPRESSOR HAD SUSTAINED FOD. AFTER REPAIR, PT AND CT VANE AREA ADJUSTMENT, THE ENGINE WAS RELEASED WITH SIMILAR TO NEW PERFORMANCE. 4 T E4EA 20010507003562001050700356NE 2001 5 7 CA010411013 220010316G7260311196801 TOWERSHAFT PWA 120 PW120A NE SPIRAL GEAR FRACTURED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE CAUSE OF THE IN FLIGHT SHUTDOWN WAS A FRACTURED TOWERSHAFT, RESULTING IN A LOSS OF DRIVE TO THE FUEL AND OIL PUMPS. FAILURE ANALYSIS OF THE TOWERSHAFT INDICATES THAT THE FRACTURE RESULTED FROM FATIGUE AT THE OUTER SURFACE, LEADING TO A TWISTED DUCTILE FRACTURE WITH THE CENTRE OF THE SHAFT FAILING IN TENSILE MODE.THERE WERE NO IDENTIFIED WORKMANSHIP ERRORS RELATED TO THE FAILURE OF THE TOWERSHAFT. 2001-04-12 TC: NO DEFINITE RESULT OF FAILURE WAS DETERMINED. 4 T E20NE 20010507003602001050700360SW 2001 5 7 CA010423005 120010328G6420 BEARING 212010704107BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA TRUNNION FAILED W K NONE S AFFECT SYSTEMS ININSP/MAINT 1 CA 185 AFS3682FM (CAN) BAD BRINNELLING, TEFLON WORN AWAY.(FLAPPING BEARINGS) 1G71 4U4 U H4SW E22EA 20010507003612001050700361SW 2001 5 7 CA010423006 120010406G6220206010189001 BEARING BELL 206011100021BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL MAIN ROTOR FAILED W K NONE O OTHER ININSP/MAINT 1 CA 980 JILM11164 (CAN) FAILURE OF ROLLER BEARING CAGE CAUSED ROLLERS TO BUNCH UP AND MISALIGN WITH RACES, SCORING RACES, ROLLERS AND HUB.FAILURE WAS DETECTED BY AN ENGINEER OBSERVING PIECES OF METAL IN THE PURGED GREASE. PRIOR TO DISASSEMBLY NO RESTRICTED MOTION WAS DETECTED, HOWEVER, PIECES OF FAILED CAGE SHOWED EVIDENCE OF BEING SQUASHED BETWEEN ROLLERS AND RACES. THIS COULD POTENTIALLY CAUSE A SEIZURE OF THE GRIP FEATHERING MOTION. 1G71 3U3 U H2SW E4CE 20010507003622001050700362CE 2001 5 7 CA010423007 120010315G561010138402521 WINDSHIELD BEECH B300 B300 1159232CE PWA PT6 PT6* 52043EA COCKPIT BROKEN W O OTHER O OTHER CRCRUISE 1 CA (CAN) AIRCRAFT IN CRUISE FLIGHT 29,000 FEET ALTITUTE OAT 45 WEATHER CLEAR NO TURBULENCE. SIMULTANEOUS LOUD BANG AND LT (PILOTS) WINDSHIELD (INNER PANE)INSTANT SPIDER WEB CRACKS. 2L72 4T3 TRTA24CE E2NE 20010507003632001050700363WP 2001 5 7 CA010423009 120010316G6320269D2512311 GEAR DOUG 369D25100505HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL M/R TRANSMISSIONBROKEN W K NONE J WARNING INDICATION ININSP/MAINT 1 CA 2214 U0312 (CAN) MAIN ROTOR TRANSMISSION REMOVED FOR MAKING METAL. UPON DISASSEMBLY IT WAS DISCOVERED THAT ON INPUT GEAR TOOTH HAD BROKEN OFF. THE TOOTH WAS FOUND IN THE SCAVENGE PUMP INTAKE.REMNANTS OF THE TOOTH WERE FOUND IN THE SCAVANGE SPRAY TUBE. 1G71 3U3 U H3WE E4CE 20010507003642001050700364NM 2001 5 7 CA010423011 120010322G6210A1561 BOOT ROBSIN A0052 ROBSINR22 R22BETA NM LYC O320 O320B2C 41508EA MAIN ROTOR BLADELEAKING W K NONE O OTHER ININSP/MAINT 1 CA 393 (CAN) AIRCRAFT PARKED OVERNIGHT WITH COVERS AND HEATERS ON THE ENGINE. OVERNIGHT TEMP -35C. PILOT HAD LEFT PRINCE GEORGE, B.C., THE PREVIOUS DAY AND TEMP WAS ABOUT +5C AT CYXS. PILOT NOTED NO DEFECTS THE MORNING OF DEPARTURE ON HIS PRE-FLIGHT AND AS HE REMOVED THE COVERS AND HEATERS. HE NOTED THAT OAT GAUGE READ -27 WHEN HE STARTED THE AIRCRAFT ON A WALK AROUND AFTER ARRIVING BACK TO PRINCE GEORGE, HE NOTED OIL ON THE ROTOR HEAD AND THE PYLON. REMOVED THE ROTOR BLADES AND FOUND THE INNER CLAMPS FOR THE BOOT LOOSE, TIGHTENED THEM AND REPLACED THE OIL. SUSPECT THAT WITH THE COLD WEATHER, THE BOOTS GOT STIFF AND THEN SLIPPED ON THE SPINDLE. AIRCRAFT HAD BEEN OPERATED OUT OF WARM HANGAR PRIOR. 1G71 3O3 O H10WE E274 20010507003652001050700365EU 2001 5 7 CA010423012 120010329G29103408360821 HARNESS BAG JETSTMJETSTM4112 EU GARRTTTPE331TPE33110 01514WP ROTOL R333 R333482F12 GL OVERRIDE SWITCH BROKEN W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CA (CAN) DURING CLIMB, THE FLAPS WOULD NOT OPERATE WITH THE CONTROL SWITCH. THE HYDRAULIC OVERRIDE HANDLE HAD TO BE USED TO FUNCTION THE FLAPS UP AND DOWN.THE OVERRIDE SWITCH WIRING HARNESS (P/N 340-4263110) WAS FOUND TO BE AT FAULT, ONE WIRE WAS BROKEN, THE RECOIL SPRING WAS BROKEN WHICH PROBABLY CAUSED THE WIRE TO BREAK DUE TO A LACK OF SUPPORT FROM THE SPRING. 1L72 4T4 TRTA196 E4WE 6 CP61GL 20010507003672001050700367WP 2001 5 7 CA010423018 120010401G6210500P2100101 BLADE HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL MAIN ROTOR FAILED W K NONE O OTHER ININSP/MAINT 1 CA 1711 A393 (CAN) BOND VOIDS BEYOND LIMITS LOW SIDE OF BLADE. LETTER SENT TO FAA DATED 24 APR 01 EXPRESSING TRANSPORT CANADA CONCERNS.(CADIS PROJECT REPORT 20010079. (CROSS REFER TO SDR 20010423019) 1G71 3U3 U H3WE E4CE 20010507003682001050700368WP 2001 5 7 CA010423019 120010409G6210500P2100101 BLADE HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL MAIN ROTOR FAILED W K NONE O OTHER ININSP/MAINT 1 CA 2120 A048 (CAN) BOND VOIDS BEYOND LIMITS LOW SIDE OF BLADE. LETTER SENT FAA DATED 24 APR 01 EXPRESSING TC CONCERNS. (CADIS PROJECT REPORT20010079). CROSS REFER TO SDR 20010423018. 1G71 3U3 U H3WE E4CE 20010507003692001050700369EA 2001 5 7 CA010424002 220010316G7314 SHAFT SUNDSTRANDAI02527730007 BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA FUEL PUMP FAILED W O OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 CA 4463 PE3224 (CAN) THE NR 2 ENGINE FLAMED OUT. AFTER THE PILOT LANDED THE AIRCRAFT SUCCESSFULLY, REMOVE THE AFCU, MFCU AND ENGINE DRIVEN FUEL PUMP. I FOUND THE FUEL PUMP SPLINES WITH NO LUBRICATION AND WORN WELL BEYOND LIMITS. (NOTE: THE SPLINED ADAPTER WAS SPINNING FREELY ON PUMP INPUT SPLINES.) 1G71 4U4 U H4SW E22EA 20010507003702001050700370CE 2001 5 7 CA010424003 120010409G5510043200146 RIB CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA STABILIZER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING INSPECTION STABILIZER RIB 0432001-46 LT, CRACKED. 1H71 3O3 ONT3A19 E223 20010507003722001050700372SW 2001 5 7 CA010425004 120010405G2435230321380 BRUSHES LEARSIEGLER 23032018 BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL STARTER GEN BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 324 4666 (CAN) STARTER-GENERATOR WAS INSPECTED BECAUSE OF PREVIOUS HISTORY OF PROBLEMS IN THIS AR4A. UPON INSPECTION FOUND 3 BRUSH LEADS BROKEN OFF BRUSHES AND 3 SPRINGS BROKEN. THE STARTER GENERATOR HAS BEEN REMOVED FOR OVERHAUL. STARTER-GENERATOR LAST OVERHAULED AT CANADIAN AERO ACCESS, CALGARY AND INSTALLED ON AIRCRAFT AT 12445.8 BRUSHES HAD BEEN REPLACED AT 12653.3STARTER-GENERATOR REMOVED AT 12769.8 1G71 3U3 U H2SW E4CE 20010507003742001050700374EU 2001 5 7 CA010426002 120010327G2750B001 SHAFT PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL TE FLAPS SHEARED W CB ABORTED TAKEOFF EMER. DESCENT BA SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE APAPPROACH 1 CA 1898 (CAN) ON SELECTION OF FLAPS DOWN, FLAPS CAUTION ON C.A.W.S. PANEL CAME ON. FLAPS WERE RESET & TRIED AGAIN. FLAPS CAUTION CAME ON AGAIN. A/C LANDED W/O FLAP. MULTIPLE RESETS WERE THEN TRIED ON GROUND WHICH WOULD CAUSE F LAP CCT BREAKER ON BATTERY BUS TO POP. TROUBLE SHOOTING REVEALED 2 INIT E203 CODES (MORE THAT 20 TURNS DIFFERENCE BETWEEN L/H & R/H ROTATION SENSORS, THEN MULTIPLE E208 CODES (OVERLOAD CB POPPED), & E203 CODES AGAIN. AS AIRCRAF T WASHED SHORTLY BEFORE DEPTR, IT IS FELT THAT R/H FLAP FROZE IN FLT CAUSING INIT E203 CODE. SUBSEQUENT RESETS CAUSED R/H INBOARD FLEX SHAFT TO SWELL & JAM IN ITS HOUSING CAUSING E208 CODES. DURING TROUBLE SHOOTING AFTER MORE RESETS, FLEX SHAFT EVENTUALLY BROKE CAU 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010507003752001050700375EU 2001 5 7 CA010426003 120010328G32525322012262 STRAP PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL NLG BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 495 (CAN) NOSE GEAR BONDING STRAP P/N 532.20.12.262 WAS WRAPPED AROUND SHOCK STRUT P/N 571.10.12.353 AND HAD BENT THE STRUT SOME 70 DEGREES UP FROM ITS NORMAL POSITION. THE STRUT COULD NO LONGER OPEN AND CLOSE THE OIL COOLER DOOR UPON GEAR RETRACTION. BONDING STRAP REQUIRED REPLACEMENT AS WELL AS THE STRUT. BONDING STRAP APPEARS TO BE A BIT LONGER THAN REQUIRED TO ALLOW FOR THE NOSE WHEEL ASSEMBLE TO TURN, THEREFORE CAUTION IS ADVISED WHEN INSTALLING BONDING STRAP TO ENSURE THAT THE BONDING STRAP WILL NOT SAG ONTO THE SHCOK STRUT ASSEMBLE. FIVE GEAR CYCLES COMPLETED AND AIRCRAFT WAS RETURNED TO SERVICE. NO FURTHER ACTION WAS REQUIRED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010507003782001050700378NM 2001 5 7 CA010426010 120010303G523085230480104 SUPPORT DHAV DHC8 DHC8103 1386005NM PWA 120 PW120 NE HAMSTD14SF 14SF7 NE COUNTER BALANCE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WE HAD AN INSPECTION OF THE BAGGAGE DOOR ON ONE OF OUR DASH 8S, S/N 357, PER TASK 5230/51 AND DURING THAT INSPECTION, WE FOUND THE AFT COUNTER BALANCE SUPPORT P/N 85230480-104 WAS CRACKED. I AM SUBMITING A STRUCTURAL DEFECT REPORT FOR S/N 257. AIRCRAFT S/N 357 WAS DONE ON 3-3-01 AND HAD A TAT 16.286.6 AND TCY 26, 179. PART REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010507003792001050700379NM 2001 5 7 CA010426019 120010403G325189923 LINK 8900115 DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE STEERING ACTU SPLIT W K NONE O OTHER ININSP/MAINT 1 CA 220971081 DCL2388900 (CAN) DURING AN INSPECTION, THE NOSEWHEEL STEERING ACTUATOR TELESCOPING ADJUSTABLE LINK WAS FOUND SPLIT (PULLED APART) AND THE ATTACH LOCKING BOLT FOR THE LINK WAS MISSING (P/N NAS 1304-7D).THE STEERING ACTUATOR ASSEMBLY WAS REPLACED AND ALL FURTHER CHECKS COMPLETED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010507003802001050700380EA 2001 5 7 CA010426025 220010320G8520LW16812 LIFTER PIPER PA44 PA44180 7104402SO LYC O360 O360* 41514EA ENGINE WORN W K NONE O OTHER ININSP/MAINT 1 CA 651 (CAN) PILOT REPORTED VIBRATION ON LT & RT ENGINE ON RUN-UP. INSPECTED BOTH ENGINES, FOUND GOOD COMPRESSION, NO BROKEN ENGINE MOUNT (COMMON ON THIS AIRCRAFT). REMOVED LIFTERS FOUND BADLY DAMAGED, DAMAGE ON CAMSHAFT AS WELL. FRONT SURFACE MISSING PIECES ON LIFTERS. BOTH ENGINES REMOVED (& PROP FOR FLUSHING) SEND TO LEAVENS AVIATION FOR REPAIR. NOTE: LIFTERS INSPECTED ON 500 HOUR SINCE OVERHAUL, NO DAMAGE AT THAT TIME. DAMAGE OCCUR WITHIN 150 HR SINCE THAT INSPECTION. 1L72 3O3 O A19S0 E286 20010507003812001050700381EA 2001 5 7 CA010426026 120010403G32440276970 TIRE CNDAIRCL604 CL604 EA MLG FAILED W K NONE O OTHER ININSP/MAINT 1 CA 534 9181P00282 (CAN) A/C DEPARTED TOLUCA, MENCO & LANDED AT TORONTO. UPON ARRIVAL IT NOTED THAT NR 3 MAIN WHEEL TIRE MISSING ITS TREAD. GTAA OPS STAFF RPTED NO DEBRIS ON LDG RWY. THEREFORE SEPARATION, MOST LIKELY OCCURRED ON TAKEOFF FROM TOLUCA. BASED ON ATMOSPHERIC CONDITION AT TIME OF DEPTR, IT CALCULATED THAT ACTUAL SPEED SEEN BY WHEELS 162 KNOTS. IS WELL BELOW RATED SPEED FOR TIRE: TIRE SHOWED NO SIGNS OF DAMAGE THAT WOULD HAVE LED TO SEPARATION. ALSO, TIRES ARE REGULARLY CHECKED FOR CORRECT TIRE PXS. AS RESULT OF SEPARATION, INBOARD RT FLAP INBD RT FLAP VANE&LOWER FWD SECTION OF RT PYLON, SUFFERED MINOR DENTS. ALSO RT MLG W.O.W. HARNESS BRACKET THAT AFFIXES TO CEILING OF GEAR BAY BECAME DISBONDED AS RESULT OF IMPACT. 2L72 4F RTA21EA 20010507003822001050700382WP 2001 5 7 CA010426031 220010330G7412103784005 EXCITER CESSNA441 441 2076020CE GARRTTTPE331TPE33110 01514WP IGNITION SYS FAILED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA 893 (CAN) ENGINE WOULD NOT START. FOUND IGNITION EXCITER UNSERVICEABLE. REPLACED UNIT. 1L72 3T4 TRTA28CE E4WE 20010507003852001050700385NE 2001 5 7 CA010430008 220010307G7200 ENGINE AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE RIGHT FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) RT ENGINE HAD A RUMBLE SOUND AND WAS THROWING FLAMES OUT THE EXHAUST. CREW REPORTED COMPRESSOR STALL.ENGINE REMOVED FOR INVESTIGATION. REPLACED ENGINE. 2L72 4F4 FRTA28NM E29NE 20010507003892001050700389NE 2001 5 7 CA010430016 220010407G7200 ENGINE LKHEED1011 1011385114 WP RROYCERB211 RB21122B02 54555NE NR 1 FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 CA 49254 (CAN) DRUING FLIGHT ENGINE NR 1 EXPERIENCED A SUDDEN VIBS INCREASE TO 3.5 UNITS ON BOTH CHANNELS A & B, WARNING LIGHTS CAME ON, ENGINE SHUT DOWN WAS ACCOMPLISHED.MCD CHECKS WAS C/O NOT DAMAGED, ENGINE BORESCOPE WAS C/O NO DAMAGE FOUND. FAN BLADES REMOVED CLEANED AND RE-INSTALLED, FAN CLAPPERS LUB.FAN TRIM BALANCE TO BE ACCOMPLISHED. 2L73 4F4 F A23WE E12EU 20010507003912001050700391WP 2001 5 7 CA010430018 120010321G52301586301113 HANDLE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE CARGO DOOR OUT OF ADJ W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CA (CAN) AT 9,000 FEET, DURING CLIMB, ON F/E ANNUNICATOR PANEL CARGO DOOR LIGHTS ILLUMINATE, AIRCRAFT RETURNED TO MAIN BASE. FOUND T HANDLE ADJUSTMENT OUT OF RIG, ADJUSTED IN ACCORDANCE WITH MAINTENANCE MANUAL 52-35-01 AND PROXIMITY SENSOR IN ACCORDANCE WITH 52-71-03. 2L73 4F4 F A23WE E12EU 20010507003922001050700392EA 2001 5 7 CA010430022 120010406G5210 LOCK CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE PAX DOOR OUT OF ADJ W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA (CAN) FLIGHT ATTENDANT REPORTED THAT SHE WAS UNABLE TO CLOSE AND LOCK THE PASSENGER DOOR. MAINTENANCE FOUND THE SECONDARY LOCK PAWL TO BE FOULING AGAINST THE TORQUE TUBE, TORQUE TUBE AND SECONDARY LOCK PAWL OUT OF ADJUSTMENT. THEY DID A PASSENGER DOOR ADJUSTMENT PER THE AMM. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010507003932001050700393EA 2001 5 7 CA010430024 120010407G5210 HANDLE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE PAX DOOR JAMMED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA (CAN) WHILE AT THE GATE, AFTER BOARDING, THE FLIGHT ATTENDANT REPORTED THAT SHE WAS UNABLE TO CLOSE THE PASSENGER DOOR. THE FLIGHT ATTENDANT REPORTED THAT THE HANDLE WOULD JAM HALF WAY WHEN CLOSING.THE AIRCRAFT WAS BROUGHT TO THE HANGAR AND MAINTENANCE WERE UNABLE TO INSTALL THE RIG PINS. THE DOOR WAS RIGGED PER THE AMM AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010507003942001050700394EA 2001 5 7 CA010430025 120010407G5610601R3303310 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER DEDESCENT 1 CA 00165H9933 (CAN) FIRST OFFICERS WINDSHIELD SHATTERED. CABIN DIFFERENTIAL PRESSURE 7.3. NO PRESSURE LOSS. REPLACED WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010507003952001050700395EA 2001 5 7 CA010501002 120010412G5210 BUSHING CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE PAX DOOR FAILED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA (CAN) WHEN THE AIRCRAFT ARRIVED IN THE HANGAR THE MECHANICS WERE UNABLE TO OPEN THE PASSENGER DOOR. THE BUSHING FROM THE CASTING FOR THE TORQUE TUBE WERE FOUND TO BE MIGRATED. THE BUSHING WERE RE-INSTALLED AND THE DOOR RIGGING C/OUT. 2L72 4F4 FRTA21EA E15NE 20010507003962001050700396EA 2001 5 7 CA010501005 120010412G5610NP1393216 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA (CAN) FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT, NO CABIN PRESSURIZATION LOSS.WINDSHIELD REPLACED. 2L72 4F4 FRTA21EA E15NE 20010507003972001050700397NE 2001 5 7 CA010501006 220010412G72004121T03G01 ENGINE CNDAIRCL600 CL6002B19 EA GE CF34 CF34* NE NR 2 FAILED W D RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN) ON TAXI WITH THE THROTTLE ON IDLE POSITION THE ITT ON ENGINE NR 2 INCREASED SUDDENLY UP TO 1093 CELSIUS. THE ENGINE SHUT DOWN BY ITSELF.BASE ON THE INSPECTION RESULTS GE RECOMMANDS TO REPLACE THE FMU AND ENGINE RUN IN ORDER TO CONTINUE TO OPERATE THE ENGINE. 2L72 4F4 FRTA21EA E15NE 20010507003982001050700398EA 2001 5 7 CA010501008 120010416G5610 WINDSHIELD CNDAIRCL600 CL6002A12 1900304EA COCKPIT CRACKED W O OTHER O OTHER APAPPROACH 1 CA (CAN) R/H WINDSHIELD CRACKED WHILE ON APPROACH. MAINTENANCE REMOVED AND REPLACED RT WINDSHIELD WITH NEW UNIT. AIRCRFT BACK IN SERVICE. 2L72 4F RTA21EA 20010507003992001050700399EA 2001 5 7 CA010501015 120010417G5610601R330339 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER LDLANDING 1 CA (CAN) UPON TOUCH DOWN, CAPTAINS WINDSHIELD INNER PLY CRACKED. WINDSHIELD REPLACED. 2L72 4F4 FRTA21EA E15NE 20010510000672001051000067EA 2001 5 10 CA010501017 120010129G5610601R330339 WINDSHIELD CNDAIRCL600 CL6002B19 EA COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA 11 (CAN) AT 17,000 FEET, 280 KTS - LT WINDSHIELD STARTED TO CRACK AND THEN SHATTERED. 2L72 4F RTA21EA 20010510000682001051000068EA 2001 5 10 CA010501021 120010205G5610601R330339 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER CLCLIMB 1 CA 7 (CAN) CLIMBING THROUGH 31,000 FEET - 7 MACH, 8.2 P.S.I. LT WINDSHIELD SHATTERED. 2L72 4F4 FRTA21EA E15NE 20010515003342001051500334NM 2001 5 15 CA010502004 120010405G2750655280726 MODULE BOEING737 737296 1384486NM PWA JT8 JT8D9A 52048NE TE FLAPS DEFECTIVE W D RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CA 1264 (CAN) AS THE POWER LEVERS WERE ADVANCED FOR TAKEOFF AT 1.2 EPR A WARNING HORN SOUNDED. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT PROCEEDED BACK TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP/SLAT POSITION ACCESSORY UNIT P/N 65-52807-26 S/N D00235. 2L72 4F4 FRTA16WE E2EA 20010515003442001051500344CE 2001 5 15 CA010503011 120010427G2810 FUEL CELL BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RT WING LEAKING W O OTHER K FLUID LOSS CLCLIMB 1 CA 17749 (CAN) A/C DEPARTED SMITHERS, BC ENROUTE TO VANCOUVER. AT APPROX 15 MIN. OUT A PASSENGER NOTED TO CREW THAT RT WING HAD A SMALL LEAK OF FUEL COMING FROM A RIVET HEAD JUST O/B OF ENGINE NACELLE. THE CREW HAD NO IND.S OUT OF ORDINARY BUT AFTER CONFERRING WITH MAINT OVER RADIO THEY ELECTED TO RETURN TO SMITHERS AS A PRECAUTIOINARY MEASURE: EMERG SRVCS WHERE STANDING BY & THE A/C MADE AN UNEVENTFUL LDG. LEAK WAS ONLY EVIDENT BY SOME WEEPING ON R/H WING & MUST HAVE BEEN GREATER WITH WING LOADING & AIRPRESSURES IN FLT.MAINT DEFUELED A/C ANDINVESTIGATED INTERNAL AREAS OF WING. SOME RIVETS WHERE SEALED IN AREA OF WEEPING & A LEAK CHECK CARRIED OUT. 2L72 4T4 TRTA24CE E4EA 20010515003452001051500345CE 2001 5 15 CA010503012 120010416G322212434262 TORQUE LINK CESSNA210 210L 2073448CE CONT O520 IO520L 17032SO NOSE GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) UPPER NOSE GEAR TORQUE LINK FOUND CRACKED HALF WAY UP PART AS SHOW. CRACK WAS IN TWO LOCATIONS ABOUT 1/4 INCH LONG. PART HAD NOT FAILED.THIS IS THE SECOND PART FOUND CRACKED ON CESSNA 210 AIRCRAFT, BOTH IN THE SAME LOCATION. 1H71 3O3 O 3A21 E5CE 20010515003462001051500346CE 2001 5 15 CA010503013 120010418G322212434262 TORQUE LINK CESSNA210 T210K 2073447CE CONT O520 TSIO520H 17040SO MCAULY3A32C D3A32C88 GL NOSE GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) UPPER NOSE GEAR TORQUE LINK FOUND CRACKED AS SHOWN. CRACK WAS IN TWO LOCATIONS ABOUT 1/8 INCH LONG. PART HAD NOT FAILED.THIS IS THE SECOND PART FOUND CRACKED ON CESSNA 210 AIRCRAFT, BOTH IN THE SAME LOCATION. 1H71 3O3 O 3A21 E8CE 5 CP21EA 20010515003472001051500347NE 2001 5 15 CA010503015 120010323G242131176002 SHAFT SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL2B NE GENERATOR WORN W K NONE O OTHER ININSP/MAINT 1 CA 237 (CAN) AIRCRAFT GENERATOR TURNS AT 12,000 RPM IS DRIVEN BY THE MAIN TRANSMISSION OF HELICOPTER & FAN CAME LOOSE ON SHAFT, RETENTION NUT MS21042-4 HAD SELF LOCKING FRICTION STILL WITHIN LIMITS. FAN IS A FIT ON SHAFT BY NUT TORQUE ONLY, NUT MUST NOT HAVE BEEN ON TIGHT ENOUGH, EVEN THOUGH NUT FRICTION WAS WITHIN LIMITS. FAN BEGAN TO VIBRATE AND A HIGH FREQUENCY VIBRATION WAS FELT. FAN COST IS US$4,900.00 FOR A SIMPLE FAN BLADE WITH REQUIRED AN EXCHANGE GENERATOR COST US$13,000. 1G72 3U3 UNCH1NE E00054EN 20010515003482001051500348NM 2001 5 15 CA010503016 120010414G2920231840 POWER UNIT DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYD SYSTEM FAILED W K NONE O OTHER ININSP/MAINT 1 CA MX467234 (CAN) WHILE USING STANDBY POWER UNIT DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT UNIT WAS NOT PRODUCING PRESSURE. UNIT REPLACED WITH SERVICEABLE AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010515003492001051500349NE 2001 5 15 CA010503017 120010418G6320SB3151A1 BEARING SKRSKYS61 S61N 8142104NE GE CT58 CT581401 30011NE MAIN ROTOR GB FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) INPUT BEARING FAILED DURING THE INITIAL RUN IN PROCEDURE. INVESTIGATION SHOWED THAT BEARING PUSHER TOOL WAS IMPROPERLY USED CAUSING DEFORMATION OF BEARING CAGE AT OVERHAUL. TOOL WAS REMOVED FROM SHOP TO PREVENT POSSIBLE REOCCURRENCE. 2G72 4U4 U 1H15 1E3 20010515003502001051500350EA 2001 5 15 CA010504002 320010411G6110 PROPELLER PIPER PA22 PA22135 7102206SO LYC O320 O320B2A 41508EA SNSNCH74DM M74DM EA ENGINE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 2480 336 (CAN) HEAVY CORROSION THRU-OUT INTER PROPELLER, .040TH OFF MATERIAL. REMOVED TO REMOVE CORROSION. 1H71 3O3 O 1A6 E274 5 NP88614 20010515003512001051500351EU 2001 5 15 CA010504004 120010419G6520369D25434 SHAFT 369D25400 HUGHES369 369FF EU ALLSN 250C 250C30 03013GL T/R GEARBOX BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 2673 1076 (CAN) - METAL GENERATION, SCHEDULED 100 HOUR INSPECTION.- GEARBOX REMOVED AND SENT FOR REPAIR. - TEARDOWN INSPECTION FOUND THAT THE INPUT GEARSHAFT HAD FAILED INBOARD OF THE INPUT GEAR.- THIS GEARBOX HAD BEEN REPAIRED ON 3 PREVIOUS OCCASIONS FOR CLOUDY OIL/SLUDGE IN OIL.- THE FAILED SHAFT HAS BEEN SENT FOR METALLURGICAL INSPECTIONS. 1G71 3U3 U H3WE E1GL 20010604000012001060400001EU 2001 6 4 CA010504007 120010323G5530SD3316384XAA FITTING STBROS SD360 STBROSSD3 SD360 8100606EU PWA PT6 PT6A65R 52043EA VERTCAL STAB CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 28800 SH3633 (CAN) DURING MID-LIFE STRUCTURAL INSPECTION THE ABOVE CLEAT WAS FOUND TO BE EXFOLIATED IN VARIOUS SPOTS BETWEEN THE WEBS. IT IS LIKELY THAT STANDING WATER COULD SIT IN THE WEB AREAS AND SPEED UP THE CORROSION PROCESS. THE VERTICAL STAB WAS REMOVED TO OBTAIN ACCESS TO THE CLEAT. THE CLEAT WAS REPLACED AND THE VERTICAL STAB REINSTALLED. 2H72 4T4 T A41EU E4EA 20010515003552001051500355CE 2001 5 15 CA010504009 120010405G5552MS20253P25120 PIN CESSNA 550 CESSNA500 550 2076604CE LT ELEVATOR HINGMISMANUFACTURED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 2339 2339 5500807 (CAN) FOUND ELEVATOR TRIM TAB HING PIN SHORT IN LENGTH ON LEFT SIDE ELEVATOR. 1L72 4F A22CE 20010515003562001051500356CE 2001 5 15 CA010504010 120010408G272003101965 SPRING CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160DTM GL RUDDER DISCONNECTED W A UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 CA (CAN) LT RUDDER AND BRAKE PEDAL RETURN SPRING P/N 0310196-5 BECAME DISLODGED FROM FRONT ANCHOR POINT BRACKET P/N 510128 IN FORWARD CENTRE TUNNEL ASSEMBLY P/N 0591301-11.THIS ALLOWED THE LEFT BRAKE & RUDDER PEDAL TO MOVE FULL FWD. THE PEDALS WOULD NOT RETURN TO NEUTRAL POSITION. ALSO NO LEFT BRAKE WAS AVAILABLE DUE TO ANGLE OF PEDALS.BY ROLLING THE SPRING P/N 0310196-5, ONE EIGHTY DEGREES & HOOKING IT OUT THROUGH BRACKET P/N 0510128 INSTEAD OF IN THROUGH THE BRACKET WOULD PREVENT THE SPRINGS P/N 0310196-3 L/H AND P/N 0310196-12 FROM BECOMING DISLODGED. BY DOING THIS THE GEOMENTRY OF THE SPRINGS ARE NOT ALTERED.NO EVIDENCE OF WEAR WAS VISIBLE ON ANY OF THE ABOVE MENTIONED PARTS. 1H71 3O3 ONT3A12 E274 5 NP910 20010515003572001051500357EU 2001 5 15 CA010504012 120010420G2550AS2219 CABLE SNIAS 350 AS350B2 8680813EU CARGO HOOK BROKEN W K NONE P NO WARNING INDICATION ININSP/MAINT 1 CA (CAN) THE METAL SHEATH THAT FORMS THE OUTER COVER OF THE MANUAL EMERGENCY RELEASE CABLE FOUND BROKEN. THE SHEATH WAS BROKEN WHERE THE RELEASE CABLE ATTACHES TO THE CARGO HOOK. THIS IS A CARGO SWING INSTALLATIION WHERE THE CARGO HOOK IS ATTACHED TO A FRAME THAT IS SUSPENDED FROM THE HELICOPTER BY FOUR CABLES. THERE IS A SUBSTANTIAL AMOUNT OF MOTION/MOVEMENT OF THE CARGO HOOK RELATIVE TO THE HELICOPTER. THE RELEASE CABLE UNDERGOES A LOT OF FLEXING, LEADING TO FATIGUE FAILURE AT CABLE ATTACHMENT. 1G71 3U H9EU 20010515003612001051500361EU 2001 5 15 CA010504018 120010409G6510BB1B649781A BEARING 11731521 BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE TAIL ROTOR DRIVEROUGH W K NONE O OTHER ININSP/MAINT 1 CA 4574 443 (CAN) HEARD CLICKING NOISE DURING DAILY INSPECTION WHILE TURNING MAIN ROTOR.DISCOVERED ROUGH NR 3 TAIL ROTOR DRIVESHAFT BEARING, BEARING CAUSED RUBBER SLEEVE ON SHAFT TO SPIN. DAMAGE TO SHAFT BEYONG LIMITS. SUSPECT INTERNAL CORROSION DUE TO HISTORY OF THIS PART SITTING IN STORAGE FOR A LONG TIME. 1G72 3U3 U H13EU E5NE 20010515003622001051500362EU 2001 5 15 CA010504020 120010415G6510350A236534451 BRACKET SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE T/R BEARING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 4216 (CAN) UPON INSPECTION, THE EIGINEER NOTICED A CRACK ON THE NR 5 T/R HANGAR BEARING SUPPORT BRACKET. 1G71 3U3 U H9EU E19EU 20010515003632001051500363EU 2001 5 15 CA010504021 120010415G2913350A35107000 BRACKET SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE HYD PUMP MOUNT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 4216 (CAN) UPON INSPECTION THE ENGINEER NOTICED A CRACK ON THE HYDRAULIC PUMP MOUNTING BRACKET. THE CRACK SEEMS TO ORIGINATE FROM TOOL MARKS CAUSED BY MAINTENANCE. 1G71 3U3 U H9EU E19EU 20010515003702001051500370SO 2001 5 15 CA010507006 120010213G3245600X6 TUBE MICHEL 6006 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA NLG TIRE FAILED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA 68 (CAN) NOSE TIRE DEFLATED. TUBE FOUND DEFECTIVE WITH HOLE IN SIDEWALL. MANUFACTURE NOTIFIED. 1L72 3O3 O A20SO E14EA 20010515003712001051500371SO 2001 5 15 CA010507007 120010227G3245600X6 TUBE MCCREARY 6006 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA NLG TIRE FAILED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA 20 (CAN) NOSE WHEEL DEFLATED.TUBE WAS FOUND DEFECTIVE WITH PIN HOLE IN SIDEWALL. MANUFACTURE NTIFIED. 1L72 3O3 O A20SO E14EA 20010515003722001051500372SW 2001 5 15 CA010507008 120010409G6320F506A OIL CAP BELL F506A BELL 206 206L 1181522SW ALLSN 25OC 250C20R GL LOCKING PINS LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) LOCKING PINS IN TRANSMISSION OIL FILTER CAP ASSEMBLY CAME LOOSE AND FELL OUT OF TRANSMISSION OIL FILLER CAP ASSEMBLY. REPLACED WITH NEW OIL FILTER CAP ASSEMBLY 1G71 3U3 U H2SW E4CE 20010515003772001051500377EA 2001 5 15 CA010507015 120010507G2731M3414 ROD END DHAV DHC3 DHC3 2800202EA PWA PT6 PT6A135 52043NE BEARING WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FOUND ROD END WORN EXCESSIVELY ON INSPECTION 200 HOURS AFTER STC SA99-219/ST01243NY WAS INSTALLED. 1H71 3R4 T A815 E4EA 20010515003882001051500388CE 2001 5 15 CA010508007 120010418G2612302157 FIRE DETECTOR BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA NR 1 ENGINE SHORTED W O OTHER N FALSE WARNING DEDESCENT 1 CA 69428 (CAN) DURING DESCENT NR 1 ENG FIRE INDICATION ILLUMINATED. ENGINE WAS SHUT DOWN. INSPECTION DETERMINED NO ACTUAL FIRE. THE ERRONEOUS FIRE INDICATION COULD NOT BE DUPLICATED ON GROUND. BASED ON PREVIOUS TROUBLE SHOOTING ALL THE WIRING FOR THE FIRE DETECTIONS WAS SPRAYED WITH WATER. WHEN THE WIRING WAS MOVED, OR THE WIRE BUNDLE SQUEEZED, THE FIRE INDICATION ILLUMINATED. INVESTIGATION REVEALED THAT THE WIRING FOR THESE DETECTIONS ARE SUSCEPTABLE TO MOISTURE AND SUBSEQUENTLY WILL SHORT OUT BRINGING ON THE FALSE INDICATION. 1L72 3T4 T A14CE E4EA 20010515003892001051500389SO 2001 5 15 CA010508008 120010405G573062061804 SKIN PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) UPON INSPECTION ON SCHEDULED #50, FOUND REAR WALK SKIN FLEX TOO MUCH ON ONE SPOT. OPEN INSPECTION PANEL, FOUND CRACK DOUBLER, ON ENFORCED SKIN (THAT IS SANDWICH SKIN). CRACK LENGTH 5 INCHES.SKIN ORDERED, TO BE REPLACE. 1L71 3O3 O 2A13 E274 20010515003902001051500390 2001 5 15 CA010508009 420010424G2562E0109 BRACKET CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA ELT LOOSE W K NONE O OTHER ININSP/MAINT 1 CA 401 029168 (CAN) MOUNTING BRACKET FOR PORTABLE ANTENNA HAS LOOSE FIT AND ALLOWS ANTENNA TO FALL OUT. MS 28775-009 O-RING USED TO RETAIN ANTENNA. 1H71 3O3 ONT3A19 E223 20010515003922001051500392NM 2001 5 15 CA010508011 120010420G5730 SKIN BOEING727 72725C 138400HNM PWA JT8 JT8D7B 52053NE WINGLET DELAMINATED W K NONE O OTHER ININSP/MAINT 1 CA 3840 3840 (CAN) DURING ROUTING C CHECK INSPECTION , FOUND EVIDENCE OF DELAMINATION AT UPPER CHORD, 8 INCHES LONG, 6 1/2 INCHES FORWARD OF AFT MOUNT FITTING. WINGLET REMOVED AND RETURNED TO WINGLET SYSTEM FOR EVALUATION AND POSSIBLE RECTIFICATION. WINGLET SYSTEMS PROVIDED REPLACEMENT WINGLET FOR INSTALLATIOIN TO AIRCRAFT. 2L73 4F4 F A3WE E2EA 20010515003932001051500393EA 2001 5 15 CA010508013 120010212G7120C2EM4A MOUNT DHAV DHC2 DHC2* 2800108EA PWA R985 R985AN14B 52008NE ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 8689 (CAN) THE ENGINE WAS CHANGED IN THE AIRCRAFT. UPON INSPECTION, THE ENGINE MOUNT WAS FOUND TO BE CRACKED AROUND THE LORD MOUNT PADS. THE MOUNT ASSEMBLY P/N C2EM4-A WAS REPLACED WITH A REPAIRED PART. 1H71 3R3 R A806 5E1 20010515003942001051500394EA 2001 5 15 CA010508014 120010508G5312C2FS533 FORMER DHAV DHC2 DHC2* 2800108EA PWA R985 R985AN14B 52008NE BULKHEAD CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9689 (CAN) THE INSPECTION REQUIRED BY CF-98-38 BULKHEAD CRACKS STA. 288 WAS CARRIED OUT ON THE AIRCRAFT. THE BULKHEAD AND THE CHANNEL ASSEMBLY WERE FOUND TO BE CRACKED. P/N C2FS533 FORMER WAS REPLACED WITH A NEW PART. P/N C2FS4045A CHANNEL ASSEMBLY WAS REPLACED WITH A NEW PART. 1H71 3R3 R A806 5E1 20010515003962001051500396EA 2001 5 15 CA010509002 120010423G571175710099 SPAR CAP DHAV DHAV DHC7 DHC7102 2802708EA PWA PT6 PT6A50 52043EA HAMSTD24PF 24PF305 GL LT & RT WING CHAFED W K NONE O OTHER ININSP/MAINT 1 CA 24387 (CAN) WE HAVE FOUND CHAFING AT YW279 LT & RT ON THE WING REAR SPAR CAP, BEHIND THE NR 1 AND NR 4 NACELLES. THIS CHAFING IS CAUSED BY A WIRE BUNDLE IN BOTH LOCATIONS. WE HAVE SEEN THIS DAMAGE IN THEE EARLIER MAINTENANCE PROJECTS, ON THE FOLLOWING AIRCRAFT: (1) DHC-7 S/N 037 (GFOF) TSN: 30142.1 CSN: 42908(2) DHC-7 S/N 63 (GCEV) TSN: 33390.4 CSN: 32682(3) DHC-7 S/N 81 (KWZV) TSN: 32198.4 CSN: 30818IN ALL CASES, THE DAMAGE WAS ADDRESSED WITH A REPAIR SCHEME PROVIDED BY DEHAVILLAND. 2H74 4T4 T A20EA E4EA 6 CP1NE 20010515003972001051500397EA 2001 5 15 CA010509003 120010423G571175710099 SPAR CAP DHAV DHAV DHC7 DHC7102 2802708EA PWA PT6 PT6A50 52043EA HAMSTD24PF 24PF305 GL LT & RT WING CHAFED W K NONE O OTHER ININSP/MAINT 1 CA 30142 (CAN) WE HAVE FOUND CHAFING AT YW279 LT & RT ON THE WING REAR SPAR CAP, BEHIND THE NR 1 AND NR 4 NACELLES. THIS CHAFING IS CAUSED BY A WIRE BUNDLE IN BOTH LOCATIONS. WE HAVE SEEN THIS DAMAGE IN THREE EARLIER MAINTENANCE PROJECTS, ON THE FOLLOWING AIRCRAFT:(1) DHC-7 S/N 036 (GJPI) TSN: 24386.6 CSN: 43093(2) DHC-7 S/N 63 (GCEV) TSN: 33390.4 CSN: 32682(3) DHC-7 S/N 81 (KWZV) TSN: 32198.4 CSN: 30818IN ALL CASES, THE DAMAGE WAS ADDRESSED WITH A REPAIR SCHEME PROVIDED BY DEHAVILLAND. 2H74 4T4 T A20EA E4EA 6 CP1NE 20010515003982001051500398EA 2001 5 15 CA010509004 120010423G571175710099 SPAR CAP DHAV DHAV DHC7 DHC7103 2802710EA PWA PT6 PT6A50 52043EA HAMSTD24PF 24PF305 GL LT & RT WING CHAFED W K NONE O OTHER ININSP/MAINT 1 CA 33390 (CAN) WE HAVE FOUND CHAFING AT YW279 LT & RT ON THE WING REAR SPAR CAP, BEHIND THE NR 1 AND NR 4 NACELLES. THIS CHAFING IS CAUSED BY A WIRE BUNDLE IN BOTH LOCATIONS. WE HAVE SEEN THIS DAMAGE IN THREE EARLIER MAINTENANCE PROJECTS, ON THE FOLLOWING AIRCRAFT:(1) DHC-7 S/N 036 (GJPI) TSN: 24386.6 CSN: 43093 (2) DHC-7 S/N 037 (GFOF) TSN: 30142.1 CSN: 42908 (3) DHC-7 S/N 81 (KWZV) TSN: 32198.4 CSN: 30818 IN ALL CASES, THE DAMAGE WAS ADDRESSED WITH A REPAIR SCHEME PROVIDED BY DEHAVILLAND. 2H74 4T4 T A20EA E4EA 6 CP1NE 20010515003992001051500399EA 2001 5 15 CA010509005 120010423G571175710099 SPAR CAP DHAV DHAV DHC7 DHC7103 2802710EA PWA PT6 PT6A50 52043EA HAMSTD24PF 24PF305 GL LT & RT WING CHAFED W K NONE O OTHER ININSP/MAINT 1 CA 32198 (CAN) WE HAVE FOUND CHAFING AT YW279 LT & RT ON THE WING REAR SPAR CAP, BEHIND THE NR 1 AND NR 4 NACELLES. THIS CHAFING IS CAUSED BY A WIRE BUNDLE IN BOTH LOCATIONS. WE HAVE SEEN THIS DAMAGE IN THREE EARLIER MAINTENANCE PROJECTS, ON THE FOLLOWING AIRCRAFT:(1) DHC-7 S/N 036 (GJPI) TSN: 24486.6 CSN: 43093(2) DHC-7 S/N 037 (GFOF) TSN: 30142.1 CSN: 42908(3) DHC-7 S/N 63 (GCEV) TSN: 33390.4 CSN: 32682IN ALL CASES, THE DAMAGE WAS ADDRESSED WITH A REPAIR SCHEME PROVIDED BY DEHAVILLAND. 2H74 4T4 T A20EA E4EA 6 CP1NE 20010515004052001051500405CE 2001 5 15 CA010509015 120010417G272004115261 TORQUE TUBE CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA CABLE ARM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9133 (CAN) CRACK FOUND IN WELD FROM TORQUE TUBE TO CABLE ARM. THE CRACK WAS APPROXIMATELY 1/8 INCH LONG AT THE END OF THE WELD. 1H71 3O3 ONT3A19 E223 20010515004072001051500407SW 2001 5 15 CA010510003 120010403G6710206010355003 TUBE 206010355001BELL 206 206L 1181522SW ALLSN 25OC 250C20R GL PITCH LINK ASSY CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 14068 DI035 (CAN) CRACK WAS VISIBLE TO NAKED EYE EMINATING FROM LOWER INSERT FAYING SURFACE AND EXTENDING VERTICALLY UPWARD 0.4 INCHES. SOME CORROSION PRESENT. REPLACED BOTH PITCH LINK ASSEMBLY WITH LINK ASSY P/N 206-010-360-005. SUSPECT THEY ARE ORIGINAL WHICH MEANS 14,068 HOURS. 1G71 3U3 U H2SW E4CE 20010515004082001051500408CE 2001 5 15 CA010510004 120010417G24002050421 CONNECTOR CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL ELECTRICAL CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 193 (CAN) THIS CONNECTOR HAS BEEN FOUND TO BE EASILY DAMAGED WHEN IT IS REQUIRED TO REMOVE OR INSERT A CONTACT IN IT. NEW REPLACEMENT PARTS OFTEN ARRIVE DAMAGED AS WELL. WHILE NOT A PROBLEM IN TYPICAL OPERATION IT DOES ALLOW FOR THE POSSIBILITY AT THE TERMINAL BEING HELD IN PLACE ONLY BY THE SEALING COMPOUND. THERE IS A SPECIFIC TOOL FOR INSERTING THESE CONTACTS BUT EVEN WITH EXTREME CARE, IT IS VERY EASY TO DAMAGE THE CONNECTOR. CONNECTOR P/N 205042-1, 205043-1 1H71 3T3 T A37CE E4EA 5 CP60GL 20010515004092001051500409EA 2001 5 15 CA010510005 120010420G531560035031159 FLOORBEAM CNDAIRCL601 CL6012A12 1900303EA GE CF34 CF34* NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 5393 (CAN) DURING A CORROSION INSPECTION EXCESSIVE CORROSION AND EXFOLIATION WAS FOUND ON THE TOP SURFACE OF TWO FLOOR BEAMS IN THE AREA UNDER THE LAVATORY AND WATER SYSTEMS FILL CANISTERS. FS 559 TO FS 621. 2L72 4F4 FRTA21AE E15NE 20010515004112001051500411EU 2001 5 15 CA010510007 120010412G78309055M20P272 CLAMP 9118M85G02 AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE THRUST REVERSER BROKEN W C ABORTED TAKEOFF M OVER TEMP TOTAKEOFF 1 CA (CAN) - ON TAKEOFF REW NOTICED 3/4 KNOB THROTTLE STAGGER. - DURING CLIMB NR 2 ENGINE LOOP B LIGHT ON. - IN CRUISE NOTICED NACELLE TEMP RISING.- UPON LANDING FOUND NR 2 ENGINE T/R BLOW OUT PANEL HANGING DOWN. - NR 2 CORE COWLS OPENED, FOUND REMAINS OF CLAMP IN T/R RT COWL. - CLAMP REPLACED WITHOUT FURTHER INCIDENT. 2L72 4F4 FRTA35EU E23EA 20010515004122001051500412CE 2001 5 15 CA010510008 120010417G554104330106 SPAR CESSNA 04330101 CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA RUDDER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9133 (CAN) 4 CRACKS WERE FOUND ORIGINATING FROM A 1.0 INCH DIA. LIGHTENING HOLE, 1.50 INCH BELOW UPPER RUDDER HINGE BRACKET. NOTE: REPLACEMENT SPAR WITH THE SAME P/N FROM CESSNA DOES NOT HAVE THIS LIGHTENING HOLE. 1H71 3O3 ONT3A19 E223 20010515004132001051500413CE 2001 5 15 CA010510009 120010416G551004320049 BRACKET CESSNA 043200159 CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9133 (CAN) 2 CRACKS FOUND AT WELDED EDGE.2 CRACKS FOUND AT ANCHOR NUT HOLE.1 CRACK WELD CRACKED. 1 CORNER NOT WELDED. 1H71 3O3 ONT3A19 E223 20010515004142001051500414CE 2001 5 15 CA010510010 120010417G272004115261 TORQUE TUBE CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA MCAULY1A103 1A103TCM GL CABLE ARM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACK FOUND IN WELD FROM TORQUE TUBE TO CABLE ARM. CRACK WAS APPROXIMATELY 0.125 INCH LONG AT THE END OF WELD. 1H71 3O3 ONT3A19 E223 5 NP50GL 20010515004222001051500422NE 2001 5 15 CA010511002 220010330G73216078T55P18 FUEL CONTROL WOODWARD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE RT ENGINE FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CA 485 WYG99820 (CAN) CREW REPORTED THAT THEY HAD 3 UNCOMMANDED OVERSPEEDS OF RIGHT ENGINE N1 DURING FLT. 1ST 104.5 PERCENT N1 FOR 5.7 SEC ICAS N1 ICON TURNED RED. PILOT PULLED THROTTLE BACK & ENGINE DID NOT COME BACK FOR 3 TO 4 SEC. PILOT ADVANCED THROTTLE BACK TO CRUISE POWER & 2ND OVERSPEED HAPPENED. IT 103.3 PERCENT N1 FOR 6.1 SEC N1 ICON TURNED RED. THROTTLE PULLED BACK & WITH 2 TO 3 2ND DELAY BEFORE ENGINE CAME BACK IN SPEED. N1 SPEED SWITCH TURNED OFF&ENGINE SPEED ADVANCED BACK TO CRUISE POWER. 3RD OVERSPEED THEN HAPPENED AT 99.1 PERCENT FOR 0.7 SEC. PILOT REDUCED THROTTLE & TURNED A/C BACK TO DEPTR AIRPORT.MAIN FUEL CNTL REPLACED & A/C RT-SRV.2001-05-11 TC: INVESTIGATING 2L72 4F4 FRTA21EA E15NE 20010515004232001051500423EA 2001 5 15 CA010511005 120010419G5400A33721 ROD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE NACELLE DOOR LOOSE W A UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 CA (CAN) AIRCRAFT ENROUTE TO MONTERREY, THE CREW WERE UNABLE TO RETARD THE LEFT HAND THROTTLE LOWER THAN 95 PERCENT. THE CREW RETURNED TO MEMPHIS AND CARRIED OUT QRH ABNORMAL 1-14. MECHANICS FOUND THE HOLD OPEN STRUT OF THE LT ENGINES UPPER CORE COWL JAMMED BETWEEN THE FUEL CONTROL UNIT INPUT SHAFT AND THE COWLING. THE STRUT WAS REMOVED (DMI) AND THE AIRCRAFT RETURNED TO SERVICE.DURING THE PRELIMINARY INVESTIGATION THE BALL WITHIN THE PIN BLC38C11SL5C4 WAS FOUND TO BE MISSING. THE STRUT STOWING END, BRACKET 228-50182-585 AND THE CLIP 228-50583-101 WILL BE VERIFIED UPON INSTALLATION OF NEW ROD TO CONCLUDE THE INVESTIGATION. 2L72 4F4 FRTA21EA E15NE 20010515004242001051500424EA 2001 5 15 CA010511008 120010419G2910AE2460010H0264 LINE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE HYD SYSTEM CHAFED W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CA (CAN) UPON CLIMBING, CREW RECEIVED A HYDRAULIC NR 1 LOW PRESSURE MESSAGE, ASSOCIATED WITH A NR 1 SYSTEM, QUANTITY INDICATING ZERO PERCENT. AIRCRAFT DIVERTED TO BIRMINGHAM. MAINTENANCE FOUND A CHAFED STEEL BRAIDE HYDRAULIC LINE IN AFT FUSE. THE LINE IS THE PESSURE LINE AT THE BULKHEAD. THE RUBBER HAD WORN OFF CLAMP P/N M85052-2-8. LINE REPLACE, ADP NR 1 REPLACED, OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010515004252001051500425NE 2001 5 15 CA010511012 220010425G7260 GEAR CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 ENGINE FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) NR 2 ENGINE OIL PRESSURE DROPPED TO APPROXIMATELY 18 PSI WITH LOW OIL PRESSURE WARNING. ENGINE SHUTDOWN PER QRH. NR 2 ENGINE REPLACED DUE TO GEAR MATERIAL ON THE CHIP DETECTOR. 2L72 4F4 FRTA21EA E15NE 20010515004262001051500426EA 2001 5 15 CA010511014 120010426G5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER APAPPROACH 1 CA (CAN) LT WINDSHIELD CRACKED DURING THE APPROACH. WINDSHIELD REPLACED AND RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010515004272001051500427EA 2001 5 15 CA010511016 120010426G5610NP1393219 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FRACTURED W O OTHER O OTHER DEDESCENT 1 CA (CAN) CAPTAINS WINDSHIELD EXPERIENCED A PLY FRACTURE DURING DESCENT. WINDSHIELD REPLACE, AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010515004282001051500428EA 2001 5 15 CA010511018 120010429G7120 BEAM CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE ENGINE SUPPORT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING C-CHECK SEVEN CRACKS WERE FOUND IN THE ENGINE SUPPORT BEAM. TWO CRACKS WERE LOCATED ON THE LOWER WEB AT FS 640.0 NAR LBL9.0. FIVE CRACKS WERE LOCATED ON THE UPPER WEB AT FS640.0 BETWEEN LBL9.0 AND RB122.0.REPAIR ONGOING IAW REO 601R-53-61-340. 2L72 4F4 FRTA21EA E15NE 20010515004292001051500429EA 2001 5 15 CA010511019 120010429G5610NP1393226 WINDOW CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE COCKPIT CRACKED W O OTHER O OTHER LDLANDING 1 CA (CAN) ON LANDING COPILOTS SIDE WINDOW CRACKED.REPLACED COPILOTS SIDE WINDOW. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010515004302001051500430EA 2001 5 15 CA010511020 120010429G76032100140007 GEARBOX CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE ENGINE CONTROLS FAILED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA 3961 3217 (CAN) RIGHT ENGINE WILL NOT SHUT DOWN USING POWER LEVER.REPLACED THE THROTTLE CONTROL GEAR BOX ASSEMBLY. ENGINE RUNS CARRIED OUT, NO FAULTS FOUND.AIRCRAFT RETURNED TO SERVICE. 2001-05-11 TC: REQUESTING DETAILED INFORMATION FROM ORIGINATOR. 2L72 4F4 FRTA21EA E15NE 20010515004312001051500431EA 2001 5 15 CA010511021 120010429G77206030T40P01 HARNESS CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE ITT INDICATOR INOPERATIVE W C ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CA (CAN) CREW ABORTED TAKEOFF DUE TO NR 2 ENGINE OVER TEMPERATURE. MAINTENANCE FOUND ITT THERMOCOUPLE HARNESS PARTIALLY INOPERATIVE. REPLACED HARNESS. NO FURTHER FAULTS FOUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010515004322001051500432NE 2001 5 15 CA010511023 220010416G7230BRR17740 BLADE RROYCE M33119 BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE HP COMPRESSOR BROKEN W A UNSCHED LANDING EYJVIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 CA 2821 1797 (CAN) AIRTRAN A/C 702, NR 1 ENGINE S/N 13121 EXPERIENCED SHUTDOWN ON CLIMB OUT OF RALIEGH DURHAM AT 9,000 FT. ENGINE RPTEDLY MADE RMBLING NOISE&LOST POWER & RAN DOWN, ENGINE SUB-IDLE BEFORE SHUTDOWN, VIBRATION HIGH BUT NOT AMBER, SURGE LIGHT CAME ON. GROUND INSP REVEALED NO METAL IN TAIL PIPE&NO EVIDENCE OF EXTERNAL DAMAGE OR BIRDSTRIKE. WEATHER AT TIME OF EVENT CLEAR&SUNNY. ON GROUND, PRELIM GROUND-RUN PERFORMED&EVM ROSE TO 4.0 UNITS N2 BY 72% N2. PHYSICAL VIBRATION FELT,&RUN STOPPED. BORESCOPE PERFORMED&HP1 COMPRESSOR BLADE FOUND BROKEN OFF MID SPAN, PLUS EXCESSIVE HP1 COMPRESSOR DAMAGE. ENGINE CHANGE HAS BEEN CALLED FOR. DETAILS OF TROUBLE SHOOTING:ENGINE BORESCOPE PERFORMED IN RALIEGH DURHAM ON 16/04 2L72 4F4 FTRA6WE E00061EN 20010614000022001061400002SO 2001 6 14 CA010511025 120010402G5712 SUPPORT PIPER PA28 PA28140 7102802SO LYC O320 O320E2A 41508EA BOLT ATTACHMENT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE CRACK IS CAUSED BY THE ATTACHMENT OF THE SUPPORT ON THE EDGE WITH AN AN3-4A BOLT. 1L71 3O3 O 2A13 E274 20010614000032001061400003EA 2001 6 14 CA010511026 120010421G7500 ACTUATOR CNDAIRCL604 CL604 EA GE CF34 CF343B1 NE BLEED AIR SYSTEMFAILED W K NONE MJ OVER TEMP WARNING INDICATION ININSP/MAINT 1 CA 2683 (CAN) OVERHEAT OF THE ACCUMULATOR, THE ELECTRIC WIING, LOWER ENGINE FAIRING AND THE LOWER CENTRAL PART OF THE NACELLE DUE TO DE-COUPLING OF THE COMPRESSED AIR INTAKE AND THE 10TH STAGE HOT AIR PORTION. THIS COUPLING IS IN A HARD TO READ AREA AND IS HARD TO TIGHT AND HAS NO RETAINING WIRE. THIS IS THE 3RD INCIDENT THAT I NOTICE OF THIS SORT. 2L72 4F4 FRTA21EA E15NE 20010614000042001061400004SW 2001 6 14 CA010511027 120010115G6220 HUB BELL 64A BELL 47 47G4A 1181031SW LYC O540 VO540B1B3 41532EA MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 1543 192 CH116 (CAN) FOUND CRACKED IN THREADED AREA AFTER EDDY CURRENT INSPECTION WHILE CARRYING OUT AD, CF-1988-08R1. 1G71 3O3 O 2H3 E304 20010614000102001061400010NM 2001 6 14 CA010515004 120010420G3240 ISOLATION VALVE BOEING737 7372Q9 138448MNM PWA JT8 JT8D9A 52048NE MLG LEAKING W D RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 CA 1731 0575 (CAN) AIRCRAFT LOST A SYSTEM HYDRAULIC FLUID UPON TAXIING TO THE TERMINAL. CREW HAD TO USE DIFFERENTIAL BRAKING TO GET TO GATE. AFTER INVESTIGATION IT WAS DETERMINED THAT THE MAIN GEAR ISOLATION VALVE P/N 65-44581-6, S/N 0575 WAS LEAKING. 2L72 4F4 F A16WE E2EA 20010614000112001061400011EA 2001 6 14 CA010515005 120010410G3510 RHEOSTAT DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA COCKPIT OVERHEATED W HA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA 9250 9250 (CAN) OXYGEN REGULATOR IN COPILOT POSITION WAS REPLACED WITH OVERHAULED UNIT. INTERNAL LIGHTING WIRES FOR THIS UNIT WERE CONNECTED IMPROPERLY (POLARITY REVERSED).AS A RESULT THE RHEOSTAT WHICH CONTROLS LIGHT INTENSITY FOR THE COPILOTS INSTRUMENT LIGHTING WAS SHORTED TO GROUND. THE 5 AMP CIRCUIT BREAKER THAT PROTECTS THIS LIGHTING RHEOSTAT DID NOT POP AND CAUSED THIS RHEOSTAT (RATED AT 2.7 AMPS MAX .7 MIN.) TO OVERHEAT AND CAUSE SOME SMOKE IN THE COCKPIT AREA. 1H72 3T4 TRTA9EA E4EA 20010614000122001061400012EU 2001 6 14 CA010515008 120010419G2910 SOLENOID VALVE BOLKMS105 BO105C 5626005EU ALLSN 250C 250C20B 03013GL HYD SYSTEM FAILED W K NONE J WARNING INDICATION ININSP/MAINT 1 CA (CAN) HYD BLOCK LIGHT CAME ON IN FLIGHT. PILOT RETURNED TO BASE AND CALLED OUT RESCUE CREW. LANDED WITHOUT DIFFICULTY. SOLENOID VALVE REPLACED AND AIRCRAFT RETURNED TO SERVICE ON APRIL 20. AIRCRAFT TEST FLOWN FOR 30 MINUTES AND NO FURTHER LIGHT REPORTS. 1G72 3U3 U H3EU E4CE 20010614000132001061400013SW 2001 6 14 CA010515009 120010327G6700 TUBE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL TRANSMISSION CHAFED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) TUBE ASSY (XMSN) FOUND CHAFED IN VERTICAL TUNNEL. ONE OF THE CONTROL TUBES CHAFED THE TUBE WITH EVERY CONTROLLED INPUT. TUBE ASSY REPLACED. 1G71 3U3 U H2SW E4CE 20010614000142001061400014SW 2001 6 14 CA010515010 120010327G6510 BEARING BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL T/R DRIVESHAFT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) 2 TAIL ROTOR DRIVESHAFT BEARINGS HAVE GREASE HOUSINGS CRACKED. BOTH BEARINGS ROUGH, EXCESSIVE GREASE SQUEEZE OUT. BOTH BEARINGS REPLACED. 1G71 3U3 U H2SW E4CE 20010614000152001061400015EU 2001 6 14 CA010515011 120010413G6310 ENGINE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE NACELLE FAILED W K NONE O OTHER ININSP/MAINT 1 CA 6349 1876 878 (CAN) AIRCRAFT LANDED AND SHUTDOWN. AFTER APPROXIMATELY 10 MIN WHEN ATTEMPTING A RESTART AT APPROXIMATELY 15 PERCENT NG AND T4 -400 DEGREES C A LOUD RINGING NOISE WAS HEARD FROM THE ENGINE COMPARTMENT AND START STALLED - START WAS ABORTED. AFTER SOME TROUBLESHOOTING THE ENGINE WAS REMOVED AND RETURNED TO THE MANUFACTURER FOR FURTHER EVALUATION. 1G71 3U3 UNCH9EU E19EU 20010614000162001061400016 2001 6 14 CA010515013 420010412G2312 POWERPACK NARCO 661 GRUMAVTBM TBM3EAIRTRD 3950310EA WRIGHTR2600 R260020 67050EA HAMSTD23E 23E50 NE VHF COMM BURNED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) SHORTLY AFTER TAKEOFF THE PILOT DETECTED THE SMELL OF SMOKE IN THE COCKPIT. HE ELECTED TO RETURN TO Fredericton AIRPORT AND DID A NORDO APPROACH AND LANDED SAFELY. MAINTENANCE FOUND THAT THE POWERPACK RESISTOR HAD BURNED AND THEREBY CUTOUT NR 1 RADIO. THE BURNED MP-10 POWER PACK RESISTOR WAS CAUSED BY A FAILED VOLTAGE REGULATOR (BENDIX P/N TYPE 1589) WHICH RESULTED IN AN UNCONTROLLED VOLTAGE SITUATION. 1L71 4R4 R L82 TC176 6 CP603 20010614000172001061400017CE 2001 6 14 CA010515014 120010404G6310 ENGINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA R GEARBOX FAILED W K NONE O OTHER ININSP/MAINT 1 CA 251531475 (CAN) ENGINE SPOOL DOWN NOTED TO BE VERY SHORT HIGH RESISTANCE TO TURNING REDUCTION GEAR BOX THROUGH PROP BLADES AND INTERNAL RUBBING DETECTED INDICATING INTERNAL PROBLEMS. - CAUSE TO BE DETERMINED UPON ENGINE TEAR DOWN. - ENGINE WAS INVOLVED IN A PROP STRIKE 10 DAYS (64 FLIGHT HOURS) EARLIER AND HAD JUST BEEN RETURNED TO REGULAR MAINTENANCE INTERVALS AFTER COMPLETING THE REQUIRED INCREASED INSPECTIONS REQUIRED BY THE ENGINE MANUFACTURER. - ENGINE TEAR DOWN SHOULD INDICATE THAT THE PROP STRIKE WAS THE CAUSE. 2L72 4T4 TRTA24CE E4EA 20010614000182001061400018EU 2001 6 14 CA010518002 120010126G6210 BLADE SNIAS 350 AS350B2 8680813EU MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2100 (CAN) DURING ROUTINE DAILY INSPECTION, MAIN ROTOR BLADE WAS FOUND TO HAVE TWO CRACKS ON THE UPPER SKIN AT STA 1177 AND STA 1182, RUNNING IN A CORD WISE DIRECTION. UPON REMOVED OF PART AND FURTHER INSPECTION, IT WAS DETERMINED THAT BLADE WAS NOT REPAIRABLE AS PER EUROCOPTER INSTRUCTION. 1G71 3U H9EU 20010614000202001061400020EU 2001 6 14 CA010518003 120010430G2822 PUMP SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE FUEL BOOST FAILED W K NONE O OTHER ININSP/MAINT 1 CA 216 23455 (CAN) NR 2 FUEL BOOST PUMP WAS FOUND TO BE EXCESSIVELY NOISY DURING POST FLIGHT INSPECTION. PUMP WAS REMOVED FOR REPAIR AS THIS NOISE IS A SIGN OF IMPENDING FAILURE. REPLACEMENT PUMP INSTALLED. 1G71 3U3 U H9EU E19EU 20010614000272001061400027EU 2001 6 14 CA010518009 120010326G2822 PUMP SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE FUEL BOOST INTERMITTENT W O OTHER J WARNING INDICATION APAPPROACH 1 CA 670 (CAN) PILOT NOTED FUEL PRESSURE INTERMITTENT/FLUCTUATING, NORMAL LANDING WAS CARRIED OUT. FUEL PUMP WAS REPLACED TO CORRECT PROBLEM. 1G71 3U3 UNCH9EU E19EU 20010730000062001073000006 2001 7 30 CA010518010 420010503G6113 PLATE MOONEY SA8659SW MOONEYM20 M20F 5870214SW LYC O360 IO360A1A 41514EA HARTZLHCC2Y HCC2YK1 GL SPINNER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 100 (CAN) CRACK & FAILURE OF FLANGE OF BACKING PLATE THAT HAS BLADE ROOT CLOSING FAIRING ATTACHED.A PORTION OF FAIRING REMAINED ATTACHED TO SPINNER WHICH SEVERELY DAMAGED NOSE BOWL FAIING LEAVING BACKING PLATE&FAIRING DEBRIS INSIDE ENGINE COWL.THERE WAS SOME MINOR DAMAGE TO PROP BLADES ABOUT FOOT FROM ROOT. SPINNER REMAINED ATTACHED&SECURE: CRACK APPEARED TO BEGIN NEAR FWD EDGE OF FLANGE OF BOTH BACKING PLATE&FAIRING ATTACHMENT. PERHAPS ABOUT 1/2 INCH&REST OF FAILURE APPEARED TO HAVE BEEN EXTREMELY RAPID. 1L71 3O3 O 2A3 1E10 5 CP920 20010614000332001061400033 2001 6 14 CA010522010 420010427G2213 CONTROL CABLE DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE AILERON FRAYED W K NONE O OTHER ININSP/MAINT 1 CA 22429 (CAN) THE FLIGHT CREW REPORTED THAT THE ROLL CONTROL FELT HEAVIER THAN STANDARD FOR TYPE. MAINTENANCE INVESTIGATION REVEALED THAT THE R/H UPPER AILERON CONTROL CABLE WAS FRAYED AT THE STEEL PULLEY, WING STATION YW 256.0, JUST OUTBOARD OF THE ENGINE NACELLE. THE CABLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. TTAF 22,429 HOURS, TCAF 33,043. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010614000342001061400034EU 2001 6 14 CA010522011 120010429G3200 PROXIMITY SENSOR BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE MLG FAILED W O OTHER N FALSE WARNING TXTAXI/GRND HDL 1 CA 1523913602 (CAN) THE FLIGHT CREW REPORTED THE L/H RED "GEAR UNSAFE" LIGHT ILLUMINATED ACCOMPANIED BY GEAR HORN, STICK SHAKER, AND MANUAL SPOILER FAULT WHILE AT THE GATE AFTER SWITCHING FROM GROUND POWER TO APU. MAINTENANCE INVESTIGATION REVEALED AN OPEN CIRCUIT IN THE L/H MAIN GEAR SIDESTAY PROXIMITY SENSOR. THE SIDESTAY ASSEMBLY WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H74 4F4 FRTA49EU E6NE 20010614000352001061400035NM 2001 6 14 CA010522013 120010506G2420 CONNECTOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE NR 2 GENERATOR LEAKING W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CA 6070 161 (CAN) THE FLIGHT CREW REPORTED ILLUMINATION OF THE NR 2 A/C. GENERATOR LIGHT ON TAKEOFF. AN UNSCHEDULED LANDING WAS ACCOMPLISHED AND THE GENERATOR WAS REPLACED. OIL WAS FOUND IN THE MAIN ELECTRICAL CONNECTOR OF THE UNSERVICEABLE GENERATOR. THIS UNIT HAD BEEN REPAIRED 161 HOURS PREVIOUS TO THIS OCCURRENCE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010614000362001061400036NE 2001 6 14 CA010522016 120010501G6220 PLATE SKRSKY S61102000304SKRSKYS61 S61N 8142104NE GE CT58 CT581401 30011NE MAIN ROTOR HEAD CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 141001508 A9835 (CAN) ON POST FLIGHT INSPECTION A CRACK WAS FOUND EXTENDING UPWARD FROM BIFILAR ATTACH BOLT HOLE ON MAIN ROTOR HUB UPPER PLATE. MAIN ROTOR HEAD REMOVED FROM SERVICE. ON DISASSEMBLY, SHIM CHECK WAS CARRIED AS PER SB 61B10-46, AND FOUND TO BE WITHIN ACCEPTABLE TOLERANCE. NO NOTABLE CORROSION WAS FOUND IN THE PLATE BOLT. SIKORSKY HAS BEEN NOTIFIED. 2G72 4U4 U 1H15 1E3 20010614000382001061400038CE 2001 6 14 CA010522019 120010508G7721 CYLINDER CESSNA172 172 2072402CE CONT O300 O300B 17022SO NR 1 SEPARATED W O OTHER O OTHER APAPPROACH 1 CA 2103 (CAN) NR 1 CYLINDER BARREL BROKE LEAVING CYLINDER BAS ATTACHED TO CRANKCASE AND CYLINDER ATACHED BY EXHAUST AND INTAKE. APPROXIMATELY 1" OF CYLINDER IS STILL ATTACHED TO CRANKCASE. PISTON AND CONNECTING ROD ARE DESTROYED. BOTH CASE HAVES AND REAR CASE IS DESTROYED. A SUCCESSFUL FORCED LANDING WAS MADE AT PRINCE GEORGE AIRPORT. 1H71 3O3 ONT3A12 E253 20010614000402001061400040SW 2001 6 14 CA010522025 120010501G3210 CROSSTUBE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA MLG BROKEN W O OTHER O OTHER LDLANDING 1 CA (CAN) HELICOPTER WAS ON A HELI SKIING JOB. THE JOB DESCRIPTION IS LOW HOURS BUT LOTS OF LANDINGS IN SNOW. THE PILOT HAD A RATHER ABRUPT LANDING ON ONE OF THE LANDING SITES (NOT HARD BUT NOT SMOOTH). AT THE NEXT LANDING THE PILOT HEARD A LOUD BANG AND IT WAS NOTED THAT THE SKID TUBE ON THE LEFT SIDE OF THE AIRCRAFT WAS NO LONGER PARALLEL WITH THE AIRCRAFT, THE SKID TUBE WAS DETACHED FROM THE REAR CROSS TUBE BUT STILL ATTACHED TO THE FRONT CROSS TUBE, A CRIB OR SUPPORT WAS BUILT TO ALLOW THE AIRCRAFT TO LAND AND SHUT DOWN WITH NO INCIDENT. THE HELICOPTER HAD BROKEN THE LOW AFT CROSS TUBE NEAR THE SKID TUBE ATTACHMENT SADDLE ON THE LEFT SIDE. 1G71 4U4 U H4SW E22EA 20010614000422001061400042SW 2001 6 14 CA010523004 120010410G3040 WINDSHIELD FRCHLDSA227 SA227DC 3377521SW GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C652 NE COCKPIT CRACKED W O OTHER O OTHER CRCRUISE 1 CA 1790 (CAN) DURING CRUISE FLIGHT AT 24,000 FEET, WITH CABIN PRESSURE APPROXIMATELY 6 PSI, THE LT WINDSHIELD OUTER PANEL CRACKED. THE CREW ELECTED TO DIVERT TO THE NEAREST AIRFIELD, REDUCE ALTITUDE TO 10,000 FEET, AND DEPRESSURIZE THE CABIN AS A PRECAUTION.IT WAS NOTED THAT THE FAIRCHILD 227 FLIGHT MANUAL DOES NOT GIVE ANY DIRECTIVES FOR ACTION IN THE CASE OF A CRACKED WINDSHIELD, THEREFORE THE CREW TOOK ACTION BASED ON EXPERIENCE ON OTHER SIMILAR TYPES OF AIRCRAFT.FAIRCHILD WILL BE CONTACTED TO REQUEST AN AMENDMENT TO THE FLIGHT MANUAL PROCEEDURES SECTION TO COVER THIS SITUATION. 2L72 4T4 TRTA18SW E4WE 6 C3PNE 20010614000432001061400043CE 2001 6 14 CA010523006 120010514G1100 PLACARD CESSNA206 U206F 2073333CE CONT O520 IO520F 17032SO COCKPIT REVERSED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE DECAL ON THE ELEVATOR TRIM WHEEL APPEARS TO HAVE BEEN FABRICATED. WHEN IT WAS INSTALLED, THE "NOSE UP" AND "NOSE DOWN" DECALS WERE REVERSED. WHEN THE PILOT THOUGHT HE WAS TRIMMING THE NOSE DOWN, HE WAS ACTUALLY TRIMMING IT UP. THE LOCATION OF THE DECALS WAS CORRECTED. 1H71 3O3 O A4CE E5CE 20010726000232001072600023EU 2001 7 26 CA010523010 120010502G2913704A33690004 BELT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE HYD PUMP FAILED W A UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 CA 190 (CAN) WHILE IN CRUISE FLIGHT THE PILOT LOST HYDRAULIC PRESSURE. SLOWED THE A/C AND LANDED. HYDRAULIC PUMP BELT BROKEN. 1G71 3U3 UNCH9EU E19EU 20010730000072001073000007EU 2001 7 30 CA010523011 120010430G63201171206301 BEVEL GEAR KAWSKI 1171201001 BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE TRANSMISSION MAKING METAL W K NONE J WARNING INDICATION ININSP/MAINT 1 CA 3733 KA0225 (CAN) MINOR "PEPPER" METAL, SHINY, WITHIN OPERATIONAL LIMITS WOULD OCCASIONALLY ACTIVATE OR FLICKER CAUTION LIGHT."PEPPER" FOUND IN BOTH FILTERS, MAINLY NR 1 SIDE. REMOVAL OF INSPECTION COVER REVEALED DEGENERATION OF SURACE OF BEVEL GEAR. 1G72 3U3 U H13EU E5NE10 20010730000082001073000008SO 2001 7 30 CA010523012 120010420G53201712124 CHANNEL PIPER PA23 PA23 7102302SO FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 4221 (CAN) DURING ANNUAL 100 HOUR INSPECTION OF THE TAIL AREA, NOTICED THAT THE CHANNEL THAT SUPPORTS THE LOWER RUDDER SUPPORT AND RUDDER STOP BRACKET WAS CRACKED. THIS WAS THE RESULT OF THE RUDDER BEING FORCED HARD AGAINST THE RUDDER STOPS BY WIND. 1L72 3O 1A10 20010730000092001073000009SO 2001 7 30 CA010523013 120010420G32201904600 DRAG LINK PIPER PA23 PA23 7102302SO NLG BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING ANNUAL 100 HOUR INSPECTION FOUND NOSE GEAR LOWER DRAG LINK BROKEN IN THE DOWN LOCK AREA. 1L72 3O 1A10 20010726000242001072600024WP 2001 7 26 CA010523015 120010426G6210369D21100517 BLADE HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL MAIN ROTOR DAMAGED W O OTHER O OTHER ININSP/MAINT 1 CA 2111 (CAN) DURING HIS DI, THE PILOT NOTICED ADHESIVE MISSING FROM ONE MAIN ROTOR BLADE ROOT FITTING. MAINTENANCE WAS ADVISED. THE BLADE WAS REMOVED AND CHECKED AS PER DN188. THE ROOT FITTING FAILED THAT INSPECTION. THE REST OF THE BLADES WERE ALSO INSPECTED AND FOUND SERVICEABLE. THE BLADE WAS RETURNED TO THE MANUFACTURER. A SERVICEABLE BLADE WAS INSTALLED AND THE AIRCRAFT RETURNED TO SERVICE. 1G71 3U3 U H3WE E4CE 20010730000112001073000011SO 2001 7 30 CA010523017 120010427G3230455180 RELEASE CABLE PIPER PA30 PA30 7103002SO LYC O320 IO320B1A 41508EA MLG STIFF W O OTHER J WARNING INDICATION CLCLIMB 1 CA (CAN) - LANDING GEAR FAILED TO RETRACT ON CLIMB OUT & BREAKERS POPPED.- GEAR FAILED TO EXTEND WHEN BREAKER RESET & SELECTED DOWN, NO GREEN LIGHT TO INDICATE GEAR DOWN AND LOCKED.- PILOT COULD NOT RELEASE EMERGENCY GEAR EXTENSION HANDLE.- RT GEAR COLLAPSED ON ROLL OUT. - TELEFLEX CABLES FOUND TO BE VERY STIFF IN CONDUIT/SLEEVE, LUBRICATION FREED UP ACTION CONSIDERABLY. 1L72 3O3 O A1EA 1E12 20010726000262001072600026GL 2001 7 26 CA010523019 220010329G72306890550 COMPRESSOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE FAILED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) THE COMPRESSOR WAS FRESHLY OVERHAUL WITH A TSO OF 1.1, CSO .3 AIRCRAFT FAILED TO START. PROBLEM FOUND TO BE COMPRESSOR LOCKED UP. MANUFACTURE CALLED AND INDICATED PROBLEM TO BE POSSIBLE REAR BEARING DIFFUSOR DUE TO THE TIGHT TOLERANCES. 1G71 3U3 U H2SW E4CE 20010726000302001072600030WP 2001 7 26 CA010523020 120010424G5511369D23623 SPAR HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 5657 (CAN) UPON SHOP REPAIR OF THIS STABILIZER FOR SKIN CRACKS, DOUBLER CRACKS AND LOOSE RIVETS. IT WAS OBSERVED, THAT THE AFT SPAR IS CRACKED ALMOST ALL THE WAY THROUGH, 2.5 INCHES FROM THE INBOARD END. WE ALSO SUSPECT ANOTHER CRACK AT ANOTHER LOCATION ON THE SAME SPAR, BUT HAVE NOT CONFIRMED IT. THESE STABILIZERS HAVE JUST HAD THEIR RETIREMENT LIFE EXTENDED. THIS STABILIZER HAS BEEN REMOVED FROM SERVICE. 1G71 3U3 U H3WE E4CE 20010730000122001073000012EA 2001 7 30 CA010523024 220010427G741466M19385 CLAMP BENDIX 1068291018 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA MAGNETO WORN W K NONE O OTHER ININSP/MAINT 1 CA 207 825199 (CAN) DURING A ROUTINE INSPECTION, IT WAS NOTED THAT EXCESSIVE OIL WAS LEAKING AROUND THE MAGNETO GASKET. UPON REMOVAL OF THE MAGNETO, IT WAS NOTED THAT THE MAGNETO HAD ABNORMAL AMOUNT OF WEAR IN THE MAGNETO CLAMP AREA. FURTHER INVESTIGATION REVEALED ONE OF THE HOLD DOWN CLAMPS WAS GROUND AWAY IN THE FACE CONTACT AREA, RESULTING IN THE MAGNETO HANGING ON THE CASE BY ONE CLAMP. BOTH THE MAGNETO AND CLAMPS WERE REMOVED AND SENT TO THE OVERHAUL FACILITY FOR REPLACEMENT. 1L72 3O3 O A20SO E14EA 20010730000132001073000013EA 2001 7 30 CA010523030 120010425G27603310961 BELLCRANK SCWZERSG2 SGS233A 8051606EA DRAG CONTROL CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 4155 (CAN) AN INSPECTION WAS CALLED FOR AS INSRUCTED IN A SPECIAL INSPECTION DND C-12-382-000/NS-016. UPON INSPECTION OF SUBJECT PART, IT WAS DETERMINED THAT THE PART HAD REJECTABLE INDICATIONS. SUBJECT PART WAS SENT FOR REPAIRS AND RETURNED TO SERVICE. FURTHER INSTRUCTION PENDING QUALITY ENGINEERING TEST ESTABLISHMENT FINDINGS. 1K00 G2EA 20010730000142001073000014EA 2001 7 30 CA010523031 120010425G27603313661 BELLCRANK SCWZERSG2 SGS233A 8051606EA DRAG CONTROL CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2897 (CAN) AN INSPECTION WAS CALLED FOR AS INSTRUCTED IN A SPECIAL INSPECTION DND C-12-382-000/NS-016. UPON INSPECTION OF SUBJECT PART, IT WAS DETERMINED THAT THE PART HAD REJECTABLE INDICATIONS. SUBJECT PART WAS SENT FOR REPAIRS AND ETURNED TO SERVICE. FURTHER INSTRUCTION PENDING QUALITY ENGINEERING TEST ESTABLISHMENT FINDINGS. 1K00 G2EA 20010730000152001073000015EA 2001 7 30 CA010523032 120010425G27603310961 BELLCRANK SCWZERSG2 SGS233A 8051606EA DRAG CONTROL CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 3142 (CAN) AN INSPECTION WAS CALLED FOR AS INSTRUCTED IN A SPECIAL INSPECTION DND C-12-382-000/NS-016. UPON INSPECTION OF SUBJECT PART, IT WAS DETERMINED THAT THE PART HAD REJECTABLE INDICATIONS. SUBJECT PART WAS SENT FOR REPAIRS AND RETURNED TO SERVICE. FURTHER INSTRUCTION PENDING QUALITY ENGINEERING TEST ESTABLISHMENT FINDINGS. 1K00 G2EA 20010730000192001073000019EA 2001 7 30 CA010529003 120010505G2910C3CF6139 LINE DHAV DHC3 DHC3 2800202EA PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL HYD SYSTEM BROKEN W O OTHER K FLUID LOSS LDLANDING 1 CA (CAN) ON LANDING THE PILOT PUMPED THE FLAPS DOWN, WHEN THE FLAPS REACHED THE DOWN POSITION THE HYDRAULIC LINE TO THE FLAP SELECTOR BROKE, LEAKING HYDRAULIC FLUID ON TO THE FLOOR. THE PILOT LANDED THE AIRCRAFT WITHOUT INCIDENT. UPON INVESTIGATION THE AME FOUND THAT THE HYDRAULIC LINE FROM THE HYDRAULIC FILTER TO THE FLAP SELECTOR HAD BROKEN OFF AT THE SELECTOR. SUSPECT THAT THE PROBLEM WAS THAT THE HYDR AULIC LINE NUT WAS OVERTORQUED AT ONE TIME WHICH CAUSED THE FLAIR TO EVENTFULLY BREAK OFF. THE LINE WAS REPAIRED AND THE AIRCRAFT RETURNED TO SERVICE.. . 1H71 3R4 T A815 E4EA 6 CP15EA 20010730000202001073000020EU 2001 7 30 CA010529004 120010507G2822MS345613273P CONNECTOR BRAERO748 HS7482A 4231001EU RROYCEDART DART5342 EU ROTOL R4304 R2124304 EU FUEL PRESS SYS SHORTED W O OTHER J WARNING INDICATION CRCRUISE 1 CA 664 (CAN) THE PORT FUEL PRESSURE WARNING LIGHT WAS INITY RPTED FLICKERING IN FLT, LATER CAME ON STEADY. LIGHT REMAINED ON WHEN CREW SELECTED POWER OFF DURING POST FLT SHUTDOWN ON RAMP.INVEST. REVEALED THAT PORT FWD WING ROOT BREAK CONNECTOR PL3 HAD DEVELOPED AN INTERNAL SHORT BETWEEN PINS 4, 5 & 24 (NOTE: THIS A/C HAS AERO CONSULTING SRVCS "CONNECTOR MOD" NOC38 550 INCORPORATED). THIS ALLOWED 24 VDC PORT BATTERY BUS BAR C/B 5 (5 AMP) THROUGH PIN 24 TO FEED PINS 4 & 5 (PORT FUEL LOW PRESSURE SWITCH/WARNING LIGHT CCT) PIN 5 BEING F103 (3 AMP) CENTRE BUSS BAR NORMAL FEED TO PORT FUEL LOW PRESSURE SWITCH & PIN 4 BIENG LOAD SIDE OF PORT FUEL LOW PRESSURE SWITCH ALSO CONNECTED TO PORT LOW FUEL PRESSURE IND. LIGHT. PL3 W 2L72 3T4 T A24EU A196 6 CP899 20010705000052001070500005EU 2001 7 5 CA010529005 120010429G2421740119G IDG AIRBUS320 A320212 EU CFMINTCFM56 CFM565A3 NE IDG OVERSERVICED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 CA 1970 (CAN) 35,000 CLIMBING - LOSS GEN #2 LOSS GEN #2 AND AC #2 RETURNED TO AIRPORT FOUND IDG (INTERGRATED DRIVE GENERATOR) #2 OVERSERVICED.IDG #2 REPLACED. . LEAK CHECKED AND OPS CHECKED SERVICEABLE. ALL BUS TRANSFERS NORMAL, SERVICEABLE.. .. . . . 2L72 4F4 FRTA28NM E29NE 20010730000212001073000021EU 2001 7 30 CA010529006 120010426G2910S43500272 MANIFOLD AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE HYD SYSTEM LEAKING W H DEACTIVATE SYST/CIRCUITS K FLUID LOSS DEDESCENT 1 CA 23300 1588 (CAN) YELLOW SYSTEM LOW LEVEL ECAM ON DESCENT INTO YYC - MAJOR HYDRAULIC LEAK EVIDENT AT BLOCK IN ON RAMP. FOUND YELLOW LEAK MEASUREMENT MANIFOLD LEAKING. REPLACED HYDRAULIC LEAK MEASUREMENT MANIFOLD. SYSTEM CHECKS SERVICEABLE IAW 29-19-41-401.. . . . 2L72 4F4 FRTA28NM E40NE 20010730000362001073000036NE 2001 7 30 CA010529007 220010327G855012345 TUBE NAMER T6 HARVARDMK4 1922828GL PWA R1340 S3H1 52016NE HAMSTD12D 12D40 NE OIL TRANSFER BENT W K NONE O OTHER ININSP/MAINT 1 CA 378 (CAN) ENGINE SUMP WAS REQD TO BE REMVD FROM ENGINE TO FACILITATE CYLINDER REMOVAL. UPON REMOVAL OF SUMP, IT WAS DISCOVERED THAT DAMAGE HAD OCCURRED TO OIL TRANSFER TUBES FROM SUMP TO CRANKCASE. THIS HAD BEEN CAUSED BY IMPROPER ASSY OF ENGINE AT AN EARLIER REPAIR. 1L71 3R3 R EXPA1L71E143 5 CP257 20010730000382001073000038GL 2001 7 30 CA010529009 120010327G5741 ATTACH FITTING NAMER T6 HARVARDMK4 1922828GL WING IMPROPER PART W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 8496 (CAN) OUTER WING ATTACHMENT HARDWARE CONSISTS OF 224 NUTS AND BOLTS FOR BOTH WINGS. APPROXIMATELY 40% OF THE NUTS USEDWERE OF A TYPE USED IN SHEAR APPLICATIONS (NAS679). CORRECT HARDWARE SHOULD HAVE BEEN AN365-428 AND AN365-524 NUTS AS CALLED FOR IN THE HARVARD PART LIST. HARDWARE WAS REPLACED AS REQUIRED. 1L71 3R EXPA1L71 20010730000412001073000041GL 2001 7 30 CA010529010 120010327G5522662200110 SKIN NAMER T6 HARVARDMK4 1922828GL ELEVATOR MISREPAIRED W K NONE O OTHER ININSP/MAINT 1 CA 84960 (CAN) ELEVATOR COVERING WAS OBSERVED DURING NORMAL INSPECTION TO HAVE CRACKING OF THE DOPE FINISH. FURTHER INVESTIGATION DISCOVERED BODY FILLER BETWEEN TWO SEPARATE DOPING AND PAINTING PROCESSES. UPON REMOVAL OF ELEVATOR, THE BALANCE CHECK CONFIRMED AN EXTREME TAIL HEAVINESS (IN EXCESS OF TWO POUNDS BEYOND ALLOWABLE LIMITS) OF BOTH ELEVATORS. ELEVATORS WERE REPLACED WITH SERVICEABLE SPARES. . . 1L71 3R EXPA1L71 20010730000452001073000045EU 2001 7 30 CA010529013 120010515G5532202473 SKIN PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL VERTICAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 4528 4528 (CAN) SMOKING WAS NOTICED AT THE ETOP R/H VERTICAL STAB SKIN. FURTHER INSPECTION REVEALED THAT THE REPAIR PATCH PREVIOUSLY INSTALLED IAW PILATUS TECH MEMO EC-12-TM-540 WAS CRACKED AT APPROXIMATELY THE SAME LOCATION AS THE ORIGINAL SKIN CRACKED. THE FIRST REPAIR WAS CARRIED OUT AT 880.8 HOURS AND 1103 CYCLES. THE SECOND REPAIR CARRIED OUT AT 4528.4 HOURS AND 5315 CYCLES UNDER TECH MEMO EC-12TM-939.. . 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010730000482001073000048GL 2001 7 30 CA010529015 320010515G61147724981 PLATE DHAV DHC7 DHC7102 2802708EA PWA PT6 PT6A50 52043EA HAMSTD24PF 24PF305 GL PROPELLER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 5000 (CAN) DURING LPI OF BARREL PLATE IT FOUND TO HAVE A CRACK THAT GOES ACROSS PACKING GROOVE FOR PACKING THAT SEALS BARREL PLATE TO BARREL. THIS PACKING SEALS BARREL LUBRICATING OIL INTO BARREL.THE BARREL PLATE IS ITEM #682.IPL FIGURE #1A, CMM 61-13-01,REVISION 10.AFTER WE FOUND THIS BARREL PLATE CRACKED WE EXAMINED ANOTHER PROP FROM A DIFFERENT OPERATOR THAT & IT WAS ALSO FOUNDWITH A CRACKED BARREL PLATE.WE THEN CHECKED A 2ND BARREL PLATE FROM 2ND OPERATOR & IT ALSO HAD A VERY SMALL CRACK STARTING.THE 1ST OPERATOR THEN SENT 2 MORE BARREL ASSY TO TRY & SALVAGE THE BARREL PLATES FROM THEM & BARREL PLATES WERE ALSO FOUND CRACKED.THE 2ND REPL BARREL ASSY WAS REMVD FROM SERVICE WITH TIME SINCE LAST MAJOR INSP OF 6,32 2H74 4T4 T A20EA E4EA 6 CP1NE 20010730000512001073000051SO 2001 7 30 CA010529016 120010427G7120V961312 ISOLATOR PIPER 1607305 PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA HARTZLHCE2Y HCE2YR2 GL ENGINE MOUNT LOOSE W K NONE O OTHER ININSP/MAINT 1 CA 665 274721 (CAN) TO KEEP FRONT OF ENGINE FROM CONTACTING COWL, ADDITIONAL P/N 85012-101 WASHERS WERE FOUND UNDER LOWER CORD MOUNTS TO RAISE FRONT OF ENGINE. . . . 1L72 3O3 O 1A10 1E4 5 CP9EA 20010730000532001073000053SW 2001 7 30 CA010529017 120010427G1100 PLACARD RKWELL700 700 7630520SW LYC O540 TIO540R2AD 41532EA HARTZLHCE3Y HCE3YR2A GL ENGINE OIL DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHEN ADDING OIL TO ENGINE WE NOTICED THAT EXTERNAL MARKING ON LITRE CONTAINER SAID "EXXON AVIATION OIL 100". WE CHECKED THE CARTON CONTAINING 12 LITRES AND IT READ "EXXON AVIATION OIL EE100". ONE INDICATED ASHLESS DISPERSANT OIL AND ONE INDICATED STRAIGHT MINERAL OIL. DISTRIBUTOR FOR OIL CONFIRMED PROBLEM AND TOOK BACK ALL PRODUCT IN QUESTION. . . . . 1L72 3O3 O A12SW E14EA 5 CP33EA 20010730000562001073000056EU 2001 7 30 CA010529020 120010430G2550S160919 SPACER SIREN S16096 SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE CARGO HOOK CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 843 843 898 (CAN) WHEN THE HOOK ARRIVED AT E.C.L., THE SCREW AND NUT WHICH TIGHTEN THE SPACER (P/N S1609-19) HAD BEEN LOOSENED. IT WAS TIGHTENED TO PERFORM INCOMING TESTS. THE CAM WHICH RELEASES THE LOAD BEAM WOULD NOT FUNCTION UNDER LIGHT LOAD (12 LBS). AS THE LOAD WAS INCAREASED THE CAM WOULD BE PUSHED OUT OF THE PATH OF THE LOAD BEAM, BUT THE CAM WOULD NOT RETURN. WHEN THIS OCCURES THE HOOK WILL NO LONGER HOLD A LOAD.. 1G71 3U3 U H9EU E19EU 20010730000582001073000058NM 2001 7 30 CA010529021 120010415G3320BA080061 BALLAST DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE LIGHTS FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA 3403 (CAN) WHEN THE FLIGHT CREW ARRIVED AT THE AIRCRAFT (ON GATE WITH EXTERNAL POWER ON) THEY REPORTED A BURNING SMELL IN THE CABIN. THEY IMMEDIATELY TURNED OFF THE AIRCRAFT POWER. MAINTENANCE FOUND THE OVERHEADLIGHTING BALLAST FOR ROW 1 - R/H, HAD OVERHEATED AND BURNED OUT. THE BALLAST AND BULB WERE REPLACED AND CHECKED - SERVICEABLE. . .. . 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010730000602001073000060NM 2001 7 30 CA010529022 120010423G291082950010271 TUBE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYD SYSTEM LEAKING W O OTHER K FLUID LOSS TXTAXI/GRND HDL 1 CA 25945 (CAN) DURING A WALK-AROUND, THE FLIGHT CREW NOTED FLUID LEAKING FROM THE R/H WING. MAINTENANCE FOUND THE HYDRAULIC TUBE (PRESSURE) TO THE R/H INBOARD ROLL SPOILER ACTUATOR LEAKING (PIN HOLE). THE HYDRAULIC TUBE WAS REPLACED AND ALL CHECKS COMPLETED. . . . . 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010730000612001073000061SO 2001 7 30 CA010529023 220010425G8530646605 NUT CONT 646742 CESSNA337 337G 2075730CE CONT O360 IO360D 17025SO MCAULY2AF34CD2AF34C306 GL CYLINDER SECTIONDAMAGED W E ENGINE SHUTDOWN DR INFLIGHT SEPARATION PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 CA 1432 (CAN) AFTER LANDING PILOT WAS TAXIING FOR SHUTDOWN WHEN HE HEARD A BANKING NOISE AND REAR ENGINE ROUGHNESS. INSPECTION REVEALED A DENT IN VALVE COVER. COVER REMOVED AND FOUND BOTH ROCKER SHAFT HOLD DOWN STUDS SHEARED. IT HAS BEEN NOTED BEFORE ON OTHER AIRCRAFT THAT ROCKER SHAFT HOLD DOWN NUTS HAVE BEEN STRIPING EASILY EVEN WITH TELEDYNE CONTINENTAL NEW ROCKER SHAFT HOLD DOWN NUTS TORQUE VALVES. . . 1H72 3O3 O A6CE E1CE 5 CP5EA 20010730000732001073000073SW 2001 7 30 CA010530009 120010510G25509307U BEARING 52800200 BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA CARGO HOOK SEIZED W K NONE O OTHER ININSP/MAINT 1 CA CAL909 (CAN) DURING AN OPS CHECK IT WAS DISCOVERED THAT THE UPPER HOUSING NR 76 TO LOWER HOUSING NR 100, LOCK NR 79 WAS DISLODGED. FURTHER INVESTIGATION FOUND THAT THE BEARING NR 98 (WHICH ALLOWS THE CARGO HOOK TO ROTATE UNDER LOAD) WAS SEIZED DUE TO CORROSION. THERE ARE SEVERAL POSSIBLE AREAS THAT MOISTURE COULD ENTER THIS AREA. ONE WAS THE MANUAL RELEASE CABLE AND THE SEALANT AROUND IT WAS IN POOR CONDITION. THIS HOLE THROUGH THE UPPER HOUSING IN DETAILED IN THE PICTURE PROVIDED. THE HOOK ASSEMBLY IS BIENG REPLACED. TSO OF HOOK ASSY IS 9 MONTHS.. 1G71 4U4 U H4SW E22EA 20010730000812001073000081EA 2001 7 30 CA010531003 120010422G2750865D1007 DRIVE UNIT CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE TE FLAPS FAULTY W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FLAP FAIL CAUTION MESSAGE DISPLAY ON EICAS (ENGINE INDICATIONS AND CREW AL ERT SYSTEM), QRH PERFORM WITH A NORMAL LANDING. RESET DONE AND FOUND SERVICEABLE BUT DEFECT RE-OCCURRED. FECU (FLAP ELECTRONIC CONTROL UNIT) CHANGED AS A PREVENTIVE MEASURE WITHOUT ANY SUCCESS, THE DEFECT RE-OCCURRED, AFTER FURTHER INVESTIGATION, MAINTENANCE FOUND TO BE THE PDU (POWER DRIVE UNIT) TO BE AT FAULT. REPLACED POWER DRIVE UNIT AND ALSO ADJUSTED #6 & 7 POTENTIOMETERS FECU AND PDU WIRING CHECK (NIL FAULT DETECTED). FLAP RIGGED AND OPERATIONAL CHECK CARRIED OUT... 2L72 4F4 FRTA21EA E15NE 20010705000062001070500006EU 2001 7 5 CA010531004 120010428G5210D5311253800000 BEARING AIRBUS AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE DOOR HINGE SEIZED W K NONE O OTHER DEDESCENT 1 CA (CAN) PASSENGER DOOR L1 NOISEY DURING DECENT, WHEN DOOR OPENED ON ARRIVAL, , DOOR JAMMED. FOUND DOOR HINGE BEARING TO FRAM, SEIZING. REPLD UPP ER & LOWER HINGE BEARINGS, OP CHECKED NORMAL.. . . . . . 2L72 4F4 FRTA28NM E29NE 20010730000832001073000083NM 2001 7 30 CA010531005 120010414G2150EO390DD03S2B11B RECEPTACLE AIRBUSA319 A319114 NM FUSLEAGE FAULTY W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) FORWARD CABIN CONDITION TRIM AIR VALVE SYSTEM AT FAULT, ECAM MESSAGE, LONG HISTORY, MINIMUM EQUIPMENT LIST 21-63-02 APPLIED. ON TROUBLESHOOTING, FOUND TRIM AIR VALVE CONNECTOR 1941VC RECEPTACLE & 1941VCA PLUG FOR ZONE CONTROLLER DAMAGED, BURNT PINS. ON TROUBLESHOOTING FOUND SHORT BETWEEN PIN 11A OF CONNECTOR AB AN PIN 5A OF AA CONNECTOR OF 8HK ZONE TEMPERATURE CONTROLLER. PULLING ON CONNECTOR 1941VC CAUSED ARCING AND DAMAGE TO CONNECTOR 1941VC AND VCA. THE FAULTY RECEPTACLE AND PLUG IS LOCATED BELOW CABIN FLOOR AT STATION 1290. REPLACED CONNECTOR 1941VC AND 1941 VCA, FORWARD CABIN CONDITION TRIM AIR SYSTEM TESTED, OPERATION NORMAL. 2L72 4F RTA28NM 20010730000842001073000084WP 2001 7 30 CA010531006 120010428G3320 TERMINAL BLOCK LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE ROW 23 OVERHEATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA (CAN) ON ARRIVAL CREW REPORTE SMOKE AT ROW 23 LT CEILING. FOUND LUMINARE TERMINAL BLOCK OVERHEATED. LUMINARE ASSY REPLACED AND TERMINAL BLOCK REPLACED AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A23WE E12EU 20010730000862001073000086WP 2001 7 30 CA010531007 120010508G490074275 FUEL BOWL PWC ST6 LKHEED1011 1011385114 WP RROYCERB211 RB21122B02 54555NE FUEL FILTER CRACKED W D RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CA 74275 (CAN) DURING THE TAXI IN THE AIRCRAFT LOST APPROXIMATELY 600 LBS OF FUEL. MAINTENANCE FOUND FUELLEAK FROM APU. UPON INSPECTION FOUND THAT THE FUEL WAS COMING FROM THE LOW PRESSURE FUEL FILTER BOWL CRACKED AT MOUNTING FLANGE. BOWL REPLACED AND AIRCRAFT RETURNED TO SERVICE. BOWL MUST HAVE BEEN INSTALLED COCKED EYED AND THE BOLT WAS USED TO OVER TORQUE THE FLANGE TO SEAT THE BOWL PROPERLY. . . . . 2L73 4F4 F A23WE E12EU 20010705000072001070500007WP 2001 7 5 CA010531008 120010428G24002621TB9 TERMINAL BLOCK LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE 317 BB FAILED W K NONE P NO WARNING INDICATION ININSP/MAINT 1 CA (CAN) FOLLOWING APU WARNING HORN RCCB TRIPPED OFF FOUND 5 WIRES WHERE THE INSULATION WAS BROKEN AND RELATED TERMINAL BUS CHEMICALLY DESTROYED BY SKYDROLL. APU FIRE-EX BOTTLE SQUIB WS INTERMITTENT DUE TO DAMAGE. REPLACED TERMINAL BLOCK AND REPAIRED WIRING AND AREA CLEAN FROM SKYDROLL AND INSPECTED FOR LEAKS. NO LEAKS WERE NOTED, AIRCRAFT RETURNED TO SERVICE. . . . . 2L73 4F4 F A23WE E12EU 20010730000882001073000088CE 2001 7 30 CA010621003 120010524G24217565T ALTERNATOR CESSNA305 305A 2074002CE CONT O470 O47011 17026SO MCAULY1A200 1A200FM GL ENGINE FAILED W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 CA 6 (CAN) ALTERNATOR WS REMOVE TO CHECK FOR INSTALLATION OF NUT AND SPLINE DRIVE. COTTER PINE WAS BROKEN AND NUT WAS BACKED OFF ON SPLINE. BOTH THE NUT AND COTTER PIN WS FOUND INSIDE THE ENGINE SPLINE GEAR. ALTERNATOR WAS SENT TO MANUFACTURER FOR OBSERVATIONS. 1H71 3O3 O 5A5 E269 5 NP874 20010730000892001073000089CE 2001 7 30 CA010621004 120010518G24217565T ALTERNATOR CESSNA305 305A 2074002CE CONT O470 O47011 17026SO MCAULY1A200 1A200FM GL ENGINE FAILED W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 CA 32 (CAN) ALTERNATOR WENT OFF LINE AND WOULD NO LONGER SUPPLY POWER. THE ALTERNATOR WAS REMOVED FOR REPLACEMENT. THE ALTERNATOR WAS RETURNED TO THE MANUFACTURER FOR WARRANTY CONDSIDERATION. THE MANUFACTURER 9SKYTRONICS) CONTACTED ME AND INFORMED ME THAT THE ROTORS AND STATORS WERE FRIED. THE REASON WAS UNKNOWN. RAM AIR WAS CONNECTED AND FUNCTIONING. 1H71 3O3 O 5A5 E269 5 NP874 20010730000912001073000091CE 2001 7 30 CA010621005 120010420G24217565T ALTERNATOR CESSNA305 305A 2074002CE CONT O470 O47011 17026SO MCAULY1A200 1A200FM GL ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 CA 32 (CAN) ALTERNATOR WAS REMOVED TO CHECK FOR INSTALLATION OF NUT ON SPLINE DRIVE. COTTOR PIN WAS BROKEN AND NUT WAS BACKED OFF THE SPLINE. BOTH THE NUT AND COTTER PIN WAS FOUND INSIDE THE ENGINE SPLINE GEAR. ALTERNATOR WAS SENT TO MANUFACTURER FOR OBSERVATIONS. 1H71 3O3 O 5A5 E269 5 NP874 20010730000932001073000093CE 2001 7 30 CA010621006 120010425G24217565T ALTERNATOR CESSNA305 305A 2074002CE CONT O470 O47011 17026SO MCAULY1A200 1A200FM GL ENGINE FAILED W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 CA 4 (CAN) ALTERNATOR WENT OFF LINE AND WOULD NO LONGER SUPPLY POWER. THE ALTERNATOR WAS REMOVED FOR REPLACEMENT. IT WAS NOTED THAT THE ALTERATOR DID HAVE A NUT INSTALLED ON THE SPLINE DRIVE. THE SPLINE DRIVE WAS NOTED TO BE SHEARED. THE ALTERNATOR WAS RETURNED TO THE MANUFACTURER FOR WARRANTY CONSIDERATION. 1H71 3O3 O 5A5 E269 5 NP874 20010730000942001073000094CE 2001 7 30 CA010621007 120010419G24217565T ALTERNATOR CESSNA305 305A 2074002CE CONT O470 O47011 17026SO MCAULY1A200 1A200FM GL DRIVE GEAR FAILED W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 CA 295 (CAN) ALTERNATOR WENT OFF LINE AND WOULD NO LONGER SUPPLY POWER. THE ALTERNATOR WS REMOVED FOR REPLACEMENT. IT WAS NOTED THAT THE ALTERNATOR DID NOT HAVE A NUT INSTALLED ON SPLINE DRIVE. THE SPLINE DRIVE WAS NOTED TO BE SHEARED. THE ALTERNATOR WAS RETURNED TO THE MANUFACTURER FOR WARRANTY CONSIDERATIONS. 1H71 3O3 O 5A5 E269 5 NP874 20010730001102001073000110EA 2001 7 30 CA010621016 120010601G76033011094 PIN DHAV DHC3 DHC3 2800202EA PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL POWER LEVER MAKING METAL W O OTHER E VIBRATION/BUFFET TOTAKEOFF 1 CA 16 16 (CAN) AT T/O POWER LEVER GOT NOTICIABLY DIFFICULT TO MOVE, EVENTUALLY SEIZING COMPLETELY AT LANDING. APPEARS TO BE MATERIAL FAILURE OF PIN 1H71 3R4 T A815 E4EA 6 CP15EA 20010730001192001073000119CE 2001 7 30 CA010621018 120010515G32421338932 STATOR BFGOODRICH 215286 CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE RT BRAKE BROKEN W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA 637 0534 (CAN) WHEN AIRCRAFT WAS TAXING FOR TAKE-OFF PILOTS REPORTED A LOUD NOISE AND THE AIRCRAFT BECAME DIFFICULT TO TAXI. THE PILOTS MADE AN ATTEMPT TO RETURN TO THE HANGAR BUT WERE UNABLE TO DO SO. MAINTENANCE PERSONNEL WERE CALLED, ANDUPON INSPECTION OF THE R/H BRAKE, DISCOVERED THAT A STATOR DISC HAD FAILED AND JAMMED THE MAIN WHEEL. THE BROKEN STATOR WAS REMOVED AND THE AIRCRAFT WAS TOWED BACK TO THE HANGAR AND REPAIRED AS REQUIRED. 1L72 4F4 F A22CE E1NE 20010730001202001073000120EA 2001 7 30 CA010621020 120010515G324631279 WHEEL CNDAIRCL215 CL2151A10 EA NLG GOUGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) UPON DISASSEMBLY OF NOSE WHEELS A SHARP DEEP GOUGE WAS FOUND IN THE VICINITY OF THE ONE WHEEL HALF. AFTER BLENDING THE DAMAGE WAS BEYOND THE LIMITS STATED IN THE B.F.G MANUAL. THE GAUGE APPEARED TO HAVE BEEN MADE DURING THE PREVIOUS DISASSEMBLY SUBSEQUENTLY FOUR OTHER WHEELS HAVE BEEN FOUND WITH THE SAME DAMAGE. THE WHEELS WERE REPLACED WITH SERVICEABLE UNITS. 2H72 4R A14EA 20010730001222001073000122SO 2001 7 30 CA010621024 120010508G32421107252132 HOSE EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL BRACK ASSY BLOCKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) BRAKES ON 4TH SIDE WERE REPORTED GRABBING AND OCCASSIONALLY NOT RELEASING PROPERLY. BRAKE UNIT, SHUTTLE VALVE AND BRAKE PRESSURE REDUCER WERE ALL REPLACED WITH NO SUCCESSFUL RESULT. IT WAS DISCOVERED THAT THE ABOVE BRAKE HOSE HAD DETERIORATED INSIDE AND A SMALL PIECE OF RUBBER WAS ACTING LIKE A FLAPPER/CHECK VALUVE, RESTRICTING THE PROPER FLOW OF FLUID IN BOTH DIRECTIONS. 4 BRAKES WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A21SO E4EA 6 CP15EA 20010730001232001073000123WP 2001 7 30 CA010621026 120010524G7921369H5656 PULLEY DOUG 369H5656 HUGHES369 369HS 4470728WP ALLSN 250C 250C20 03013GL OIL COOLER FAILED W K NONE O OTHER ININSP/MAINT 1 CA HL9936 (CAN) OIL COOLER PULLEY IS MADE UP OF A SPLINE BELT PULLEY WITH A METAL RING THAT IS "STAKED" ONTO THE PULLEY. THE RING WAS FOUND AROUND THE ENGINE OUTPUT DRIVE SHAFT AFTER GROUND RUNNING THE A/C. A NEW PART WAS USED TO COMPARE THE STAKING MARKS ON THE OLD PULLEY. THE NEW PULLEY HAS 4 LARGE STAKE MARKS COMPARED TO 8 SMALLER STAKE MARKS ON THE OLD PULLEY. 1G71 3U3 U H3WE E4CE 20010730001252001073000125CE 2001 7 30 CA010621027 120010526G32421338932 STATOR BFGOODRICH 215286 CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE BRAKE ASSY CRACKED W O OTHER D INFLIGHT SEPARATION LDLANDING 1 CA 670 2164 (CAN) UPON LANDING IN QUESNEL B.C, WHEN THE PILOT APPLIED BRAKE HE FELT THE AIRCRAFT VIBRATE AND SHUTTER WHEN LH BRAKE APPLIED. THEY TAXIED TO THE RAMP AND NOTIFIED MAINTENANCE AFTER SHUTDOWN. INVESTIGATIONBY MAINTENANCE FOUND THAT THE BRAKE WEAR PINS STILL INDICATED THERE WAS LIFE REMAINING ON THE BRAKES, HOWEVER THE BRAKE WAS WORN TO THE LIMITS AND THE INBD STATOR WAS CRACKED THROUGH. THE BRAKE ASSEMBLY WAS REPLACED WITH AN OVERHAUL UNIT AND THE A IRCRAFT WAS RETURNED TO SERVICE. 1L72 4F4 F A22CE E1NE 20010730001272001073000127CE 2001 7 30 CA010621028 120010520G32135081032017 AXLE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE MLG CRACKED W O OTHER J WARNING INDICATION LDLANDING 1 CA 1583 1583 (CAN) CREW REPORTED A HARD LANDING ON MAY 20/01 DURING LANDINGT. THE A/C WS INSPECTED WHERE THE MAINTENANCE STAFF NOTED WHAT WERE POSSIBLY CRACKS IN THE MAIN LANDING GEAR AXLE HOUSING. NDT WAS PERFORMED AND CONFIRMED THE PRESENCE OF CRACKS ONBOTH THE LEFT HAND AND RT SIDE. THE LOWER OLD AXLE ASSEMBLIES ARE CURRENTLY BEING REPLACED 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20010730001292001073000129EA 2001 7 30 CA010621034 120010606G79211893013 REGULATOR 21563113805 CNDAIRCL215 CL2151A10 EA OIL COOLER STUCK W E ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CA (CAN) #2 ENGINE SHUT DOWN IN FLIGHT DUE TO HIGH OIL TEMPERATURE AND DECREASING OIL PRESSURE. MAIN OIL SCREEN INSPECTED AND NO CONTAMINATS WERE PRESENT. THE OIL COOLER REGULATOR WAS STUCK IN THE CLOSED POISITION. THE OIL COOLER REGULATOR WAS REPLACED, AIRCRAFT WAS GROUND RUN AND LEAK CHECKED SERVICEABLE. AIRCRAFT RETURNED TO SERVICE. 2H72 4R A14EA 20010730001472001073000147CE 2001 7 30 CA010622003 120010529G3240114800851143880 BRAKE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE MLG MALFUNCTIONED W O OTHER J WARNING INDICATION LDLANDING 1 CA (CAN) PILOT DEPARTED CALGARY ON ROUTE TO PENTICTON. AT SOME POIN WHILE AIRBOURNE THE PARKING BRAKE WAS ENGAGED. DURING TOUCHDOWN IN PENTICTON NR 2,3,& 4 MAIN TIRES BLEW. THE A/C VEERED TO THE RIGHT, THE PILOTS MAINTAINED CONTROL AND THE A/C STOPPED AT SOME POINT ON THE RUNWAY. AS A RESULT OF THE TIRES BLOWING NR 3 & 4 MAIN WHEELS AND BRAKES WERE DAMAGED BEYOND REPAIR. A MAINTENANCE CREW WAS FLOWN TO PENTICTON WHERE THE A/C WA JACKED UP, TIRES AND BRAKES REMOVED, NR 1 & 2 BRAKE ASSEWMBLIES WERE FOUND SERVICABLE. NR 3 & 4 BRAKE ASSEMBLIES WERE REPLACED. ALL FOUR MAIN WHEEL ASSY'S WERE REPLACED. THE A/C WAS THEN RETURNED TO SERVICE. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20010730001482001073000148EA 2001 7 30 CA010622004 220010531G7261 GARLOCK SEAL BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HARTZLHCB4M HCB4MP3 GL LT ENGINE FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CLCLIMB 1 CA (CAN) LT ENGINE LOST OIL PRESSURE DURING CLIMB OUT OF AFTER APPROX. 20 MINUTES. PILOT SECURED ENGINE WHEN OIL PRESSURE WAS IN YELLOW ARC OF OIL GAUGE. AIRCRAFT LANDED UNEVENTUALLY ATER RETURNING TO YUR. MAINTENANCE FOUND THAT MOST OF THE OIL HAD BEEN EJECTED OVERBOARD THROUGH THE FUEL PUMP CASE DRAIN. GARLOCK SEAL AND CARRIER SEAL WERE REPLACED TWICE WITHOUT RESULTS. IVESTIGATION STILL IN PROGRESS. LT ENGINE POWER SECTION AND OIL COOLER WERE REPLACED THE 2 DAYS BEFORE. OIL LEAK WAS ALSO REPORTED 1 DAY BEFORE AND THE THRMAL BYPASS VALCE WAS REPLACED. GROUND RUS CHECKED SERVICEABLE. 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20010730001772001073000177SW 2001 7 30 CA010622018 120010528G331060647 POTENTIOMETER AIRTRCAT802 AT802 0390305SW PWA PT6 PT6A67A 52043NE HARTZLHCB5M HCB5MP3 GL COCKPIT SPARKS W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA 545 (CAN) IN FLT, A/C EXPERIENCED "SHOWER OF SPARKS" EMINATING FROM L OWER INSTRUMENT LIGHTING DIMMER POTENTIMETER. DURING APPROACH PILOT TRIED TO ADJUST THELOWER INSTRUMENT DIMMER THESPAR KS FLEW UPON LDG.THE INST WAS INSP/IT WAS NOTED THAT SOLDERED CONNECTION OF BOTH UPPER & LOWER INSTRUMENT DIMMER POTTS WERE CONTACTING EACHOTHER. SINC E THERE IS NO POSITIVE ENGAGEMENT OF POTENTIOMETER TO INSTRUMNET PANEL. IF ATTACH NUT ON POTENTIOMETER BECOMES SLIGHT LOOSE, POT ROTATE & CONTACT ADJACENT POT. BOTH POTENTIOMETERS WERE RE-SECURED IN ASAFE POS AND CHECKED FOR CORRECT OP/OTHER DAMAGE TO SYS. FLEET CHECK. ONLY ONE OTHER A/C HAD A LOOSE POTENTIOMETER. 1L71 3T4 TNCA19SW E26NE 6 CP44GL 20010730001792001073000179EA 2001 7 30 CA010622019 120010522G2752MS28775142 SEAL 215750108 CNDAIRCL215 CL2151A10 EA FLAP ACTUATOR LEAKING W O OTHER K FLUID LOSS ININSP/MAINT 1 CA H358 (CAN) A/C HAD BEEN ON GROUND 45 MINS WIHT NO SIGN OF FLUID LEAK. SUDDEN HYDRAULIC FLUID STARTED TO LEAK FROM R/H FLAP ACTUATOR & FLAPS DROOPED TO APPROX. 10 DEGS. FLUID WAS COMING F ROM LOWER END SEAL. ACTUATOR WAS CLEANED & FLAPS WERE CYCLED 20 TIMES WITH NO FURTHER SIGNS OF LEAKAGE. A/C WAS RT-SRV. A/C WAS PARKED FOR NIGHT WITH NO S IGNS O F LEAKS. UPON DAILY INSPS NEXT MORNING FLAPS WERE FOUND SAGGED TO APPROX. 10 DEGS/ PUDDLE OF HYD. FLUID FOUND BELOW R/H FLAP ACTUATOR. FLAPS WERE CYCLED WITH THEAUX FLUID PU MP/ A STREAM OF FLUID EMITTED FROM LOWER END OF ACTUATOR ON 1ST CYCLE ONLY.NO SIGNS OF LEAKAGE FOLLOWING 10 CYCLES. 2H72 4R A14EA 20010730001812001073000181CE 2001 7 30 CA010622021 120010608G534750150193 CHANNEL CESSNA 501509797 CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C87 GL SEAT SUPPORT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 5890 5890 (CAN) BROUGHT THE A/C IN TO ADJUST THE LOW FUEL PRESS ON THE AUX FUEL PUMP. TO D0SO YOU MUST REMOVE THE PILOT SEAT & ADJUST A RESISTOR UNDER THE PILOT SEAT SUPPORT ASSY. THAT IS WHEN NOTICED THE CRACKIN THE LOWER R/H SEAT SUPPORT ASSY BOTTOM CHANNEL 1L72 3O3 O A7CE E8CE 5 CP22EA 20010730001832001073000183EA 2001 7 30 CA010622024 220010421G853075838 VALVE GUIDE LYC LW12966 PIPER PA31 PA31 7103102SO LYC O540 TIO540J2BD 41532EA HARTZLHCC4Y HCC4YR2 GL CYLINDER WORN W K NONE O OTHER ININSP/MAINT 1 CA 41 (CAN) ON THE 1ST EVENT INSPECTION AFTER ENGINE WAS INSTALLED FOUND NR 5 CYLINDER FAILED COMPRESSION CHECK WITH 15/80. PROGRESSIVE AIR IN KAMLOOPS SUSPECTS GUIDE WORN. RETURNED CYLIDER TO THEM FOR WARRANTY CONSIDERATION. 1L72 3O3 O A20SO E14EA 5 CP52GL 20010730001852001073000185CE 2001 7 30 CA010622025 120010605G3213504100036 ATTACH FITTING CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING AN INSPECTION, THE LOWER SCISSOR ATTACH LUG WAS FOUND CRACKED. THE CRACK WAS FOUNDONLY AROUND THE SMALLER LUG. THE RT LANDING GEAR AXLE ASSE MBLY WAS REPLACED. 1L72 3O3 O A7CE E8CE 20010730001882001073000188CE 2001 7 30 CA010622028 120010605G574352920048 DOUBLER CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE COMPLETING AN INSPECTION A CRACK WAS FOUND ON THE RT MAIN LANDING GEAR DOUBLER. A WING RIB IMPROVEMENT KIT (SK414-8E) WAS PREVIOUSLY INSTALLED. DOUBLER P/N 5292004-8 WAS PART OF THE KIT. IT WAS THIS DOUBLER THAT WAS AGA IN FOUND CRACKED. THE DOUBLER WAS REPLACED. 1L72 3O3 O A7CE E8CE 20010730001962001073000196EA 2001 7 30 CA010622029 120010512G7810311178001 EXHAUST STACK DHAV DHC3 DHC3 2800202EA PWA PT6 PT6A34 52043EA LT ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 870 870 (CAN) ON A 100 HOUR INSPECTION A CRACK WAS FOUND ON THE LT EXHAUST STACK MOUNTI NG FLANG OF THE TURBINE_EXHAUST DUCT. DUE TO THE FACT THAT THERE WAS SO LITTLE TIME ON THE ENGINE I CALLED P&W AND THEY SENT A REP. & A NEW PART FOR OUR AIRCRAFT. THE REP DID NOT KNOW WAY OUR EXHAUST WOULD CRACK. WE ARE NOW LOOKING AT THE EXHAUST AT 50 HOURS INTERVALS FOR THE NEXT LITLE WHILE TO SEE IF WE GET ANY MORE CRACKS. 1H71 3R4 T A815 E4EA 20010730001982001073000198EU 2001 7 30 CA010622032 120010530G2560AFG0314294 SEAT BELT SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE COCKPIT DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) INERTIA REELS, EACH 2 WERE RE-WEBBED BY AN UNAUTHORIZED REPAIR FACILITY IN CANADA. IT IS UNKNOWN IF WEBBING / THREAD MEETS REQUIRMENT SPECIFICATIONS / IF THE HARNESS ASSY WOULD TENSUKE TEST TO PROPER FOR MATERIAL / STITCH PATTERN. PARTS WERE RE-WEBBED AND CERTIFIED WITH PROPER MATERIALS AND TC24-0045 CONFORMITY CERTIFICATIONS ISSUED PARTS RETURNED TO SERVICE. 1G71 3U3 U H9EU E19EU 20010730001992001073000199SO 2001 7 30 CA010622033 220010604G73146462121 PUMP CESSNA185 A185E 2072818CE CONT O520 IO520D 17032SO MCAULYD3A34 D3A34C403 GL FUEL SYSTEM LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA 570 (CAN) THE PILOT NOTED FUEL DRIPPING FROM THE OVERBOARD DRAIN TUBE. MAINTENANCE DISCOVERED FUEL COMING FROM THE FUEL PUMP SEAL DRAIN. THERE IS A CRITICAL SERVICE BULLETIN C53 01-01. ALTHOUGH THE PART NUMBER DID NOT MATCH THE BASIC FUEL PUMP WAS IDENTIFIED BY THE PRESENCE OF TWO ROUND BOSSES LOCATED ON OPPOSITE SIDES OF THE FUEL PUMP HOUSING OWNER /AME SHOULD BE ALERT TO ANY FUEL LEAKAGE IN THIS AREA. 1H71 3O3 O 3A24 E5CE 5 CP47GL 20010730002002001073000200EA 2001 7 30 CA010622034 120010515G2510FDC2700 SEAT BELT DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA HARTZLHCB3T HCB3TN3 GL COCKPIT DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) 10 PAX LAP BELT ASSY'S WERE REPAIRED AND CERTIFIED BY UNAUTHORIZED REPAIR FACILITY. UNKNOWN IF WEBBING MATERIAL AND THREAD MEETS SPECIFICATION. UNKNOWN IF STITCH PATTERN WILL TENSILE TEST TO REQUIRED LIMIT. LAP BELTS WERE RE-WEBBED TO PROPER 1500 LB CINFIGURATION WITH CERTIFIED MATERIALS. TENSILE TEST TO 1500 LSB CARRIED OUT. PROPER TAGS WERE INSTALLED ON BELTS AND 24-0045 CONFORMITY CERTIFICATIONISSUED. PARTS RETURNED TO SERVICE. 1H72 3T4 TRTA9EA E4EA 6 CP15EA 20010730002012001073000201EU 2001 7 30 CA010622035 120010606G5280137414B416 DOOR BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP MCAULY4HFR344HFR34C652 NE MLG BENT W O OTHER O OTHER LDLANDING 1 CA (CAN) THE GEAR WAS SELECTED DOWN FOR LANDING. A VIBRATION WAS FELT AND THE AIRCRAFT DELVELOPED A SLIGHT YAW TO THE RIGHT. THE YAW WAS TRIMMED OUTAND THE LA NDING CONTINUED. AFTER LANDING IT WAS DISCOVERED THAT THE RT GEAR DOOR WAS HANGING LOOSE. ON INSPECTION IT WAS FOUND THAT THE ROD CONNECTINGTHE DOOR TO THE GEAR HAD FAILED IN COMPRESSION AND THE AFT HINGE WAS BROKEN. THE DOOR WAS BENT OUTWARD FROM A POINT ABOUT 7 INCHES INBOARD OF THE HINGE LINE. IT APPEARS THAT THE DOOR HUNG UP ON THE EDGE OF THE LANDING GEAR BAY. THE ACTION OF THE GEAR LOWERING PUSHED DOWN ON THE DOOR CAUSING IT TO BEND OUTWARDS AND EVENTUALLY BREAK THE OPERATING ROD. 2L72 4T4 TRTA21EU E4WE 6 C3PNE 20010730002022001073000202SO 2001 7 30 CA010622036 220010507G85206419311075 BOLT CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C505 GL LT ENGINE BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 973 (CAN) UPON INSPECTION (EVENT 1 & 2), TAKING THE COWLING OFF ON LEFT ENGINE, A NUT WITH PART OF THE THRU BOLT HIT THE FLOOR, FURTHER INSPECTION FOUND THE LEFT THRU BOLT HAS SNAPPED. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010730002032001073000203SO 2001 7 30 CA010622037 120010705G332010002719 LIGHT EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL CABIN SPARKS W K NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CA (CAN) CUSTOMER REPORTED SPARKS FROM LOOSE OVERHEAD LIGHT IN 7TH ROW, LEFT SIDE. 1L72 4T4 T A21SO E4EA 6 CP15EA 20010730002042001073000204EU 2001 7 30 CA010625001 120010613G3210200877664 PIN BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE MLG DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA 280207342 (CAN) LARGE SECTION OF CHROME MISSING FROM DIAMETER "A" PIN (PARENT METAL CORRODED UNDER AREA OF MISSING CHROME) DEFECT FOUND REMOVAL OF PIN WHEN RETRACTION ACTUATOR REPLACEMENT WAS REQUIRED. PIN REPLACED. ADDITIONAL INFORMATION & PICTURES E-MAILED TO STEVE DUDKA AT TRANSPORT CANADA. 2H74 4F4 FRTA49EU E6NE 20010730002062001073000206NM 2001 7 30 CA010625002 120010611G5330 SKIN BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 51026 (CAN) CRACKED FUSELAGE SKIN LEFT SIDE, BETWEEN FUSELAGE STATIONS 747 ABD 767, STRINGER 17L. REPAIRED AS PER SRM 53-30-3, TABLE 1, METHOD 1 PAGES 87,88 & 88A. 2L72 4F4 F A16WE E2EA 20010730002082001073000208NM 2001 7 30 CA010625004 120010611G5330 SKIN BOEING737 737296 1384486NM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 52471 (CAN) CRACK IN FUSELAGE SKIN LEFT SIDE, BETWEEN FUSELAGE STATIONS 747 AND 767, STRINGER 17L. REPAIRED AS PER SRM 53-30-3, TABLE 1, METHOD 1, PAGES 87,88 & 88A. 2L72 4F4 FRTA16WE E2EA 20010730002282001073000228CE 2001 7 30 CA010625005 120010616G612011538900215 CONTROL CABLE HARTZL HCB3TN3G BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA HARTZLHCB3T HCB3TN3 GL RT ENGINE BROKEN W O OTHER E VIBRATION/BUFFET CRCRUISE 1 CA BUA20464 (CAN) WHILE OPERATING IN CRUISE FLIGHT, A SELECTION OF THE PROPELLOR LEVER CONTROL FOR THE RIGHT ENGINE WAS MADE WITH NO CHANGE IN PROP RPM. ANOTHER SETTING WAS TRIED WITH NO RESPONSE. THE RPM REAMINED AT 1900. THE FLIGHT ROUTIG WAS CANCELLED AND TH AIRCRAFT RETURNED FOR MAINTENANCE INSPECTION. MAI NTENANCE DETERMINED THAT THE PROPELLER CONTROL PUSH/PULL CABLE ASSEMBLY HAD BROKEN ABOUT 3 INCHES INSIDE OF THE HOUSING AT THE COCKPIT LEVER END. THERE WERE NO PREVIOUS INDICATIONS OR REPORTS OF A STIFF OR ROUGH PROP LEVER CONTROL. THE BROKEN CABLE ASSY WAS REMOVED FOR REPLACEMENT WITH A NEW ASSEMBLY. 1L72 4T4 T A24CE E4EA 6 CP15EA 20010730002772001073000277CE 2001 7 30 CA010625010 120010531G561010138402522 WINDSHIELD BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE HARTZLHCB4M HCB4MP3 GL COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA 1241 (CAN) A/C WAS ENROUTE AT FL. 310, WINDHIELD ANTI-ICE WAS SE LECTED ON.SUDDENLY A LOUD CRACK WAS HEARD AND THE CO-PILOTS WINDHIELD SHATTERED AND THE INNER PANE INTO MANY SMALL PIECES. CR EW FOLOWED CHECKLIST FOR CRAKED WIND AND A/C DESENDED TO 12,000 FT ASL AND LANDED. CO-PILOTS WINDSHIELD ASSYWAS REPALACED AND IT WAS CONFIRM ED THAT THE H.P AND L.P HEAT ELEMENTS AND CONTROL SENSOR ON THE FAILED WINDSHIELD PANEL WERE SERVICEABLE. LATEST WINDSHIELD AVAILABLE P/N 101-384025-2 4 INCORPORATING NEW INTERLAYER MATERIAL (PPG-12) INSTALLED, TO REPLACE FAILED WINDSHIELD. 2L72 4T4 T A24CE E4EA 6 CP56GL 20010730002782001073000278SW 2001 7 30 CA010625011 120010516G5311 FRAME AIRTRCAT802 AT802 0390305SW FUSELAGE WORN W K NONE O OTHER ININSP/MAINT 1 CA 50 (CAN) ON INSPECTION THE RUDDER CABLE AND RUDER TRIM CABLE WERE FOUND TO BE RUBBING ON THE CUT-OUT IN THE BULKHEAD AT THE FS 180. 1L71 3T NCA19SW 20010730003062001073000306SO 2001 7 30 CA010625013 120010605G57516237601 DOUBLER PIPER PA28 PA28140 7102802SO LYC O320 O320E2A 41508EA SNSNCH74D 74DM EA AILERON CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING ANNUAL INSPECTION CRACKS WERE NOTED ALONG THE BEND RADIUS OF PARTS (REFER PHOTOS ATTACHED). SUSPECT DAMAGE WAS CAUSED FROM CONTROLS NOT BEING PROPERLY SECURED ALLOWING AILERONS TO WORK UP ANDDOWN DURING WINDY CONDITION S._P/N'S 66767-00 & 66767-01. 1L71 3O3 O 2A13 E274 5 NP88614 20010730003072001073000307SW 2001 7 30 CA010625014 120010607G324640279 WHEEL AIRTRCAT802 AT802 0390305SW MLG CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 25 (CAN) UPON DISASSEMBLY OF WHEEL MAINTENANCE DISCOVERED SERIOUS CORROSION AT THE TOP AND BOTTOM OF THE OUTER BEARING RACE. 1L71 3T NCA19SW 20010730003082001073000308SO 2001 7 30 CA010625015 120010525G2140 COMBUSTION LINERJANITROL 90D381 PIPER PA44 PA44180 7104402SO LYC O360 O360E1A6 41514EA HARTZLHCC2Y HCC2YR2 GL HEATER CRACKED W BA EMER. DESCENT UNSCHED LANDING O OTHER CLCLIMB 1 CA 283 4791851 (CAN) PILOT SMELLED A STRANGE BURING SMELL IN COCKPIT WHICH LAST APPROX. 30 SEC AND DISAPPEARED. SHORTLY FOLLOWING SHE STARTED FEELING A FLOATING SENSATION /TRANSFERRED CONTROL TO STUDENT/WITHIN 30 SEC THE STUDENT FEELING SAME EFFECTS.THE PILOT THAN DECLARED EMERGENCY AND REGAINED CONTROL FLIGHT WAS IMC. WE OPENED THE STORM WINDOW SHUT OFF HEATER/CHECKED THE CO DETECTIR WHICH INDICATED NORMAL. WITHIN 30SEC WE FELT BETTER WITH THE FRESH AIR AND LANDED WIT HOUT INCIDENT. INSPECTION SHOWED AIRCRAFT HEATING SYSTEM REVEALED A 2.5-3 INCH CRACK IN THE COMBUSTION HEATER CAN, IN THE AFT WELDED LID. HEATER W AS REPLACED. NEXT DUE FOR PRESSURE DECAY TEST AT 500HR. HEATER HOBBS TIME. 1L72 3O3 O A19S0 E286 5 CP920 20010730003092001073000309CE 2001 7 30 CA010625016 120010530G575150130016 HINGE BRACKET BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA HARTZLHCD4N3HCD4N3A GL RT AILERON MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) PILOT FOUND AILERON SECURED ONLY BY OUTBOARD HINGE AND PUSHROD DURING WALK AROUND INSPECTION. THE SCREWS FOR THE INBOARD AND MIDDLE HINGE BRACKETS WERE IN PLACE, BUT NOT THROUGH THE BRACKETS. THE AILERON WAS REMOVED IN NOV 98 FOR PAINT. THE A/C WENT THROUGH A FULL PHASE 1-4 INSPECTION IN OCT. 99. THE A/C WENT THROUGH ANOTHER FULLPHASE 1-4 INSPECTION IN FEB 2001 WHO ALSO CONDUCTED THE EXPORT C OFA.CANADIAN APPROVAL WAS THEN CARRIED OUT IN TORONTO. P/N'S 50-130016 & 50-130021. 1L72 3T4 TRT3A20 E4EA 5 CSTC 20010730003102001073000310SO 2001 7 30 CA010625017 120010605G574062102000 BRACKET PIPER PA28 PA28140 7102802SO LYC O320 O320E2A 41508EA SNSNCH74D 74DM EA WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AILERON SUPPORT BRACKET AT BOLT HOLE WERE FOUND CRACKED WITH THE RIGHT HAN D PART COMPLETLY BROKEN AS PER PHOTO. SUSPECT CAUSE-CONTROLS NOT SECURED BUT ALLOWED TOFLOP AROUND DURING WINDY CONDITIONS, PROBABLY OVER A PERIOD OF TIME._P/N'S 62102-000(LEFT) 62102-001(RIGHT) 1L71 3O3 O 2A13 E274 5 NP88614 20010730003112001073000311NE 2001 7 30 CA010625019 320010509G611478230101 BEARING 14SF7 DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE PROP HUB GOUGED W K NONE O OTHER ININSP/MAINT 1 CA 10500 8992 (CAN) SUSPECT ELECTRICAL ARCING OR DELAMINATION OF CHROME COATING FROM SUB SURFACE STRUCTURE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010730003122001073000312EA 2001 7 30 CA010625024 220010509G7200PT6A41 ENGINE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA HARTZLHCB3T HCB3TN3 GL RIGHT FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CA 8808 980 (CAN) ABOUT 1 HR INTO FLT CREW NOTED A SLIGHT FLUNCTUATION IN RT ENGINE TORQUE ALONG WITH A REDUCTION IN ENGINE NG SPEED. ITT ALSO INCREASED 50 DEGS HIGHER THAN NORMAL FOR CRUISE POWER.THE CREW MONITORE ENGINE PARAMETERS & NOTED A FURTHER DECREASE IN NG TO BELOW NORMAL OP LIMITS WITH INCREASES IN ITT. REW ELECTED TO SHUTDOWN ENGINE IN ACCORD WITH AFM AND SOP'S & RETURNED TO MAIN BASE FOR FURTHER INVEST.. A/C LANDED W/O FURTHER INCID..MAINT INSP OF ENGINE REVEALED THAT ACCESSORY SECTION /GAS GEN GROUP HAVE SIGNS OF INTERNAL DAMAGED AS INDICATED BY INABILITY TO ROTATE SEVERAL OF DRIVES. NO FURTHER TEAR DOWN OF ENGINE WILL TAKE 1L72 4T4 T A24CE E4EA 6 CP15EA 20010730003132001073000313SW 2001 7 30 CA010625025 120010430G2150 BEARING SWRNGNSA227 SA227AC 8780603SW ROTOL R321 R321482F8 GL COOLING TURBINE SEIZED W ED ENGINE SHUTDOWN RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA (CAN) AFTER LDG /DURING TAXI TO TERMINAL BLDG CREW NOTICED A SMOKY HAZE IN FWD CABIN& COCKPIT AREA. THEY IMMEDIATELY TURNED OFF LEFT & RIGHT BLEED AIR SWITCHES & THEN ELECTED TO SHUTDOWN ENGINES WHEN THEY DIDN'T SEE ANY NOTICEABLE CHANGE WITH SWITCHES SELECTED OFF.THE CREW & PASSENGERS DEPLANED A/C W/O FURTHER INCID.. MAINT RETURNED A/C TO TH HANGAR & BEGAN AN INSP INTO CAUES OF INCID.. IT WAS DETERMINED THAT LEFT AIR-COND, COOLING TURBINE WAS INOPERATIVE & HAD SEIZED. IT APPEARS THAT BEARING IN THEUNIT IS AT FAULT, RESULTING IN AN IMBALANCE IN ROTATING IMPELLER. THIS RESULTED IN IMPELLER RUBBING ON SHROUD CAUSING IT TO FAIL 2L72 4T RTA8SW 6 CP61GL 20010730003142001073000314CE 2001 7 30 CA010625026 120010529G7120 MOUNT CESSNA180 180A 2072604CE CONT O470 O470K 17026SO MCAULY2A34C 2A34C66 GL LT ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 3199 (CAN) ENG MOUNT FOUND CRACKED ON UPPER LT STRUT. 1H71 3O3 O 5A6 E273 5 CP3EA 20010730003152001073000315NM 2001 7 30 CA010625028 120010614G3241 CONNECTOR BOEING737 737281 138448PNM PWA JT8 JT8D17 52049NE MLG BRAKE MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 187 (CAN) IN TROUBLE SHOOTING A HISTORY OF INTERMITTENT ANTI-SKID PROBLEMS IT WAS DISCOVERED THAT THE HYDRAULIC BRAKE PRESSURE LINES FROM THE AIRFRAME TO THE TOP OF THE R.H LANDING GEAR SWIVELS THE CONNECTORSTOTHE WHEEL SPEED TRANSDUCERS WERE SWAPPED TO THE OPPOSITE WHEEL. THE A/C WAS RESTORED TO NORMAL. NO FURTHER PROBLEMS OCCURRED. THE FAULT HISTORY INDICATED ON GEAR INSTALLATION AT T THIRD PARTY A.M.O.THE OVER HAULER WAS ADVISED AND IS IMPLEMENTING CHANGES IN THEIR PROCEDURES. 2L72 4F4 F A16WE E2EA 20010730003162001073000316EU 2001 7 30 CA010625029 120010613G71105711012367 HINGE PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL ENGINE COWL CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 6560 (CAN) DURING AN INSPECTION OF THE FLAP ASSY FOR THE OIL COOLER DOR A 1" CRACK WASFOUND DBETWEEN THE MOUNTING HOLES AND THE HINGE. NEW PART WAS INSTALLED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010730003182001073000318GL 2001 7 30 CA010625031 220010606G72306890550 BEARING BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE FAILED W A UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 CA 6228 2980 (CAN) PILOT FELT ENGINE VIBRATION, 30 MINUTES INTO THE FLIGHT, WITH CLIMB OF T.O.O. TURN BACK FOR LANDING. ENGINE OIL PRESS FLACTUATE. 6FT ABOVE GROUND THE ENGINE QUIT. THE PILOT DID LOWER AUTOROTATION, NO DAMAGE TO AIRCRAFT AND NO ONE GOT INJURED. INITIAL INSPECTATION WAS DONE AND FOUND THAT COMPRESSOR BLADES WERE DAMAGED AND NR 1 BEARING AND SEAT FAILED. ENGINE ASSY REMOVE /REPLACED /SENT FOR EVALUATION. 1G71 3U3 U H2SW E4CE 20010730003192001073000319CE 2001 7 30 CA010625033 120010518G3234998100753 BRACKET 11581102011 BEECH 90 F90 1152909CE PWA PT6 PT6A135 52043NE SWITCH MOUNT MISMANUFACTURED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) SWITCH MOUNT FLANGE NOT BENT PROPERLY PER DRAWING TO OBTAIN 90 DEGREE RELATIONSHIP WITH PIVOT POINT. THIS RESULTS IN A SMALLER RANGE OF ADJUSTMENT. SWITCH P/N 622EN51 (HONEYWELL) INTERNAL SPRING IS SOSTIFF(3-6LBS) THE BRACKET FLEXES EXCESSIVELY AS THE SWITCH IS BEING ACTIVATED. THIS ALSO RESULTS IN REDUCING RANGE OF ADJUSTMENT. HAVE TALKED TO RAYTHEON TECH SUPPORT. 1L72 4T4 T A31CE E4EA 20010730003202001073000320EA 2001 7 30 CA010625034 220010518G741410682056 DISTRIBUTOR BLK BENDIX D6LN3200 PIPER PA31 PA31 7103102SO LYC O540 TIO540J2BD 41532EA HARTZLHCC4Y HCC4YR2 GL DUAL MAGNETO WORN W A UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 CA 1335 4072013 (CAN) PILOT EXPERIENCED ROUGH RUNNING ENGINE SHORTLY AFTER TAKEOFF. INSPECTION OF THE MAGNETO REVEALED A SEVERLY WORN BRONZE BUSHING ON THE DISTRIBUTOR BLOCK. ROUGH RUNNING WAS ATTRIBUTED TO INTERNAL CONTAMINATION OF THE MAGNETO WITH FINE BRONZE FILINGS, PARTIALLY SHORTING THE CONTACTS. 1L72 3O3 O A20SO E14EA 5 CP52GL 20010730003212001073000321NM 2001 7 30 CA010625035 120010625G32462601450 WHEEL BOEING737 737200 1384453NM MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 467 (CAN) DURING TEAR DOWN FOR OVERHAUL CRACK WERE DISCOVERED EMANTAING FROM THE BEARING CUP BORE AND EXTENDING INTO THE SPOKE WEBS ABD REACHING TO WITHIN 1" OF SPLITTING THE HUB. THE PART WAS BER'D THE LAST OVERHAUL INCLUDED LIQUID PENETRANT INSPECTION AND HIGH FREQUENCY EDDY CURRENT INSPECTION AT WHICH TIMENO ANOMALIES WERE INDICATED. 2L72 4F A16WE 20010730003222001073000322CE 2001 7 30 CA010625037 120010514G321314504A20100J WASHER CESSNA 208B CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL TRUNNION BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 2255 26410081 (CAN) DURING INSPECTION, MAINTENANCE FOUND THE PIN SECURING THE MAIN LANDING GEAR SPRING (LEG) HAD MOVED AFT APPROXIMATELY 3/4 OF AN INCH.MAINTENANCE CONCLUDED WASHER (ITEM 28-FORWARD) WAS DISHED AND FRACTUR ED DUE TO OVERTORQUING OF BOLT (ITEM 30) AND NUT.T HE TWO WASHERS (ITEM28) ARE FOR THE PURPOSE OF RETAINING PIN (ITEM 27) WITHIN ITS BORE. REF:FIGURE 01,32-10-00 OF THE 208 IPC 1H71 3T3 T A37CE E4EA 5 CP60GL 20010730003232001073000323CE 2001 7 30 CA010625038 120010522G5521115610010169 RIB BEECH 115610010347BEECH 100 100BEECH 1152916CE PWA PT6 PT6A28 EA ELEVATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 8742 (CAN) WHEN REMOVING RH ELEVATOR FOR INSTALLATION OF UPDATE KIT # 100-4005-1SWAS FOUND INBOARD RIB CRACKED TWO PLACES AT FORWARD END. RIB REPLACED WITH FACTORY NEW. 1L72 3T4 T A14CE E4EA 20010730003242001073000324CE 2001 7 30 CA010625039 120010606G275012602442 TUBE CESSNA 12602441 CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL TE FLAP BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 6441 (CAN) FOUND DURING A SCHEDULED 200 HOUR INSPECTATION. TUBE ASSY BROKE AT A POINT OF APPROX. 3/8" OUTBOARD OF THE INBOARD ROD END. (AT THE BASE OF THE THREADS). TUBE THEN RESTED ON TOP OF THE FLAP MOTOR AND BELLCRANK. 1H71 3O3 O A4CE E5CE 5 CP47GL 20010730003252001073000325EA 2001 7 30 CA010625043 220010515G853016T19468 EXHAUST VALVE LW12966 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA ENGINE DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA J3151 (CAN) ON GROUND RUN PILOT REPORTED R/H ENGINE RUNNING ROUGH. MAINTENANCE FOUND #2CYLINDER, EXHAUST VALVE SEAT DISLODGED, DAMAGING THE PISTON. ENGINE HAD METAL CONTAMINATION. ENGINE FIREWALL FORWARD REPLACEDWITH O/H UNIT AND COMPONENTS AND HOSES. CYLINDER ASSY HAD 596.4 HOURS SINCE REPAIR. 1L72 3O3 O A20SO E14EA 20010730003262001073000326EA 2001 7 30 CA010625044 220010611G8520T10540J2BD CONNECTING ROD CONT TIO540J2BD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA ENGINE FAILED W C ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 CA 2418 L798161A (CAN) ON TAKEOFF FROM YVG (VERMILION) THE PILOT NOTICED THE LH ENGINE STARTED TO RUN ROUGH AND LOSE POWER. THE ENGINE THEN STARTED TO VIBRATE BADLY AT WHICH POINT THE PILOT STOPPED AND FEATHERED THE # 1 ENGINE. THE AIRCRAFT RETURNED TO VERMILION WHERE MAINTENANCE CHANGED THE #1 ENGINE. UPON INSPECTION, MAINTENANCE FOUND THE # 6 CYLINDER CONNECTING ROD DETATCHED FROM PISTON. SUBSEQUENT ROTATION OF ENGINEAND CONNECTING ROD CAUSED SEVERE DAMAGE TO CRANKCASE AND CAMSHAFT VISIBLE THROUGH HOLE IN CRANKCASE ABOVE # 5 CYLINDER CASUING ENGINE STOPPAGE. THE ABOVE ENGINE WAS RUNNING ON CONDITION. WE ARE PRESENTLY REVIEWING OUR ON CONDITION PROCEDURES. 1L72 3O3 O A20SO E14EA 20010730003272001073000327NM 2001 7 30 CA010625046 120010530G2612 FIRE DETECTOR BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE APU SHORTED W F ACTIVATE FIRE EXT. J WARNING INDICATION CRCRUISE 1 CA (CAN) IN CRUISE 15 MIN AFTER APU SHUT DOWN. APU FIRE WARNING OCCURED. FIRE HANDLED PULLED AND BOTTLE DISCHARED. FIRE INDICATION TERMINATED. AFTER APPROX. 30 SEC. FIRE TEST CARRIED OUT, ALL INDICATIONS NORMAL. FLIGHT CONTINUED NO FURTHER PROBLEM. INVESTIGATION ON GROUND FOUND NO EVIDENCE OF FIRE OR OVER HEATING DAMAGE TROUBLE SHOOTING OF LOOPS AND WIRING FOUND NO FAULTS. A/C DISPATCH WITH MEL ON DISCHARGED BOTTLE AND MEL ON FIRE DETECTION SYSTEM.. 2L72 4F4 F A16WE E2EA 20010730003282001073000328SW 2001 7 30 CA010625047 120010525G5302205030899009 SKIN BELL BELL 204 204B 1181404SW LYC T53 T5313B 41549NE TAIL BOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACK IN SKIN DUE TO BROKEN STIFFENER INSIDE FIN. APPROX LOCATION IS FSTA 444.75, WATERINE 85 RIGHT BUTTLINE 3.0. STIFFENER P/N 205-030-899-036 ALSO RIB P/N 204-030-827-015 WAS DAMAGED BY BROKEN STIFFENER. 1G71 4U4 U H1SW E17EA 20010730003302001073000330NE 2001 7 30 CA010625051 220010622G73234301121204 GOVERNOR BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE POWER TURBINE FAILED W K NONE O OTHER ININSP/MAINT 1 CA 1005 (CAN) TORQUE SPLITS COULD NOT BE BROUGHT INTO SPLE WITH ALLOWABLE AIRFRAME ADJUSTMENTS AND PERCENTAGE OF SPLITTING WOULD VARY AT EACH CYCLE. 1G72 3U3 U H13EU E5NE 20010730003312001073000331CE 2001 7 30 CA010625052 120010614G271035524238124 RETAINER BEECH 55 95A55 1152704CE CONT O470 IO470L 17026SO MCAULY2AF36C2AF36C39 GL AILERON MISSING W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING SCHEDULED MAINTENANCE IT WAS FOUND THAT THE LOWER CONTROL ARM RETAINER WAS MISSING. UPON FURTHER INVESTIGATION, IT WAS FOUND LYING IN THE BELLY OF THE AIRPLANE. IT WAS ALSO NOTED THAT THE UPPERCONTROL ARM RETAINER WAS ATTACHED WITH ONLY ONE OF TWO SCREWS WAS THE INCORRECT STYLE. 1L72 3O3 O 3A16 3E1 5 CP911 20010730003352001073000335CE 2001 7 30 CA010626006 120010524G32125801 SWITCH CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULY2A34C D2A34C58 GL FLOAT FAILED W O OTHER J WARNING INDICATION APAPPROACH 1 CA (CAN) ON GEAR EXTENSIONFOR LANDING IN PRINCE ALBERT SASK. THE RH MAIN GEAR DOWN INDICATOR LIGHT DID NOT ILLUMINATE. AFTER TESTING THE SYSTEM AND HAVING THE SAME RESULTS, THE PILOT ELECTED TO LAND AND DID SOWITHOUT INCIDENT. ON THE GROUND, TESTING REVEALED THAT THE PROXIMITY SWITCH FOR THE RH MAIN GEAR WOULD FAIL INTERMITTANTLY. AS A PRECAUTION THE OTHER SWITCHES WERE ALSO TESTED AND THE LH NOSE WHEEL A LSO FAILEDINTERMITTANTLY. NEW SWITCHES HAVE BEEN ORDERED TO REPLACE THE FAULTY ONES. BOTH SWITCHES ARE THE SAME PART NUMBER. AS A MATTER OF INTEREST THE LANDING GEAR HAD BEEN SWUNG AS MANY AS THIRTY TIMES THAT DAY BEFORE WITHOUT FAILURE WHILE TROUBLE SHOOTING A DIFFERENT DISCREPENCY. 1H71 3O3 O 3A24 E5CE 5 CP3EA 20010730003362001073000336NM 2001 7 30 CA010626007 120010527G6210369D21102523 BLADE DOUG 600N 600N 3027377NM ALLSN 250C 250C47M 03013GL MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 642 (CAN) A/C STOPPED FOR REFUELING, DUE TO THE TQ EVENTS THAT HAD BEEN ACCUMULATED, (160) THE PILOTS CARRIED OUT A BLADE TORQUE EVENT INSPECTION I.A.W. SB600N-031. THEY FOUND THE WHITE BLADE TO BE CRACKED, BOTTOM SIDE, 12.5" O/B OF THE LAST BOLT ON THE BLADE GRIP, 2.25" I/B OF THE SERIAL # DATA PLATE, MID WAY IN THE BLADE, CRACK WAS MEASURED TO BE .75" LONG, BUT THE PILOTS CONFIRMED THAT THE CRACK WAS LONGER WITH THE BLADE SUPPORTED OFF THE DROOP STOP RING, AND WAS SAID TO RUN TO .25" FROM THE TRAILING EDGE, ESTIMATING THE CRACK TO BE 2.5" TO 3.0" LONG IN LENGTH. 1G71 3U3 UNCH3WE E1GL 20010730003372001073000337NM 2001 7 30 CA010626008 120010612G25202A0590174 TUBE BOEING757 757236 NM RROYCERB211 RB211535E43754555NE SEAT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) TORQUE TUBE CRACKED WHERE THE CUTOUT HAS BEEN MADE FOR THE WIRING TO GO THROUGHT. THIS IS THE SECOND SEAT WE FIND WITH THE SAME PROBLEM. 2L72 4F4 FRTA2NM E12EU 20010731000402001073100040EA 2001 7 31 CA010626019 120010530G3610320207231 CHECK VALVE CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF343B1 NE APU FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) DURING APU BLEED TRANSITION TO ENGINES THE APU LCV FAIL LIGHT CAME ON AND OPEN LIGHT REMAINED ON. ABOUT 15 SECONDS THE RT FIRE INDICATION APPEARED, CREW THROTTLED BACK JUST BELOW 70 PERCENT N1 AND THE FIRE WENT OUT. CREW SHUTDOWN ENGINE AND DECLARED EMERGENCY AND LANDED UNEVENTUALLY AT LAX. FOLLOW UP: FOUND LCV AND FIRE LOOP BAD. ALSO FOUND THE FLAPPERS FOR THE CHECK VALVE ABOVE THE LCV MISSING. FOUND BOTH FLAPPERS OF CHECK VALVE, ALSO FOUND RT STATER DAMAGE POSSIBLE FROM CHECK VALVE PIECES. PARTS REPLACED AND RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010731000412001073100041EA 2001 7 31 CA010626020 120010417G7110 ACCESS DOOR CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE NOSE COWL MISSING W O OTHER D INFLIGHT SEPARATION LDLANDING 1 CA (CAN) AFTER AIRCRAFT LANDED AT CHICAGO O'HARE, IT WAS NOTICED T HAT THE NOSE COWL LOWER ACCESS PANEL (228-50081-142) WAS ON THE RUNWAY. OTHER DAMAGED PARTS WERE NOSE COWL UPPER ACCESS PANEL 228-50080-158 AND COVER ASSEMBLY 228-50793-120. PRIOR TO THIS EVENT THE AIRCRAFT WAS DOWN FOR ROUTINE MAINTENANCEAN D WORK WAS PERFORMED ON THE THRUST REVERSER SYST EM DUE TO A MMEL. 2L72 4F4 FRTA21EA E15NE 20010731000432001073100043EA 2001 7 31 CA010626022 120010528G2421 GENERATOR DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE NR 1 FAILED W A UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 CA 9014 (CAN) SHORTLY AFTER TAKEOFF, NR 1 AC GENERATOR FAILURE WARNING CAME UP. THE GENERATOR SYSTEM WAS RESETED IAW THE FMP, WITHOUT SUCCESS. THE GENERATOR WAS THEN DEACTIVATED AND ISOLATED IAW THE FMP.THE GENERATOR WS REPALCED AN THE AIRCRAFT WS RELEASED FOR SERVICE WITHOUT FURTHER INCIDENTS. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010705000132001070500013NM 2001 7 5 CA010626024 120010430G7830312N53217 DUCT BOEING LJ76579 BOEING757 757236 NM RROYCERB211 RB211535E43754555NE JOINT SLEEVE LEAKING W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION NRNOT REPORTED 1 CA (CAN) #1 ENG THRUST REVERSER DEACTIVATED AS PER MEL. INVESTIGATION FOUND THE PYLON MOUNTED FAN THRUSR REVERSER ELECTRICAL HARNESS PN LJ6579 AND LJ 76580 MELTED AND HEAVELY DAMAGED. HOT AIR LEAK FROM HP2 ANDHP7 BLEED AIR DUCT PN 312N5321-7 AND 312N5306-1 ALSO CAUSED LH THRUST REVERSER HYD LINES AND PROTECTION SLEEVE TO OVERHEAT. #1 THRUST REVERSER UPPER FEEDBACK CABLE FOUND DAMAGED AND SEIZED AND FAILED THE STIFFNESS CHECK, PARTS REPLACED. 2L72 4F4 FRTA2NM E12EU 20010731000442001073100044CE 2001 7 31 CA010626026 120010502G2823M83248110111 O-RING CESSNA206 T206H CE LYC O540 TIO540AJ1A EA FUEL SELECTOR LEAKING W O OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CA 104 (CAN) DURING APPROACH AND LANDING A FUEL ODOR WAS APPARENT. INVESTIGATION OF THE REPORTED SNAG REVEALED THAT THE FUEL SELECTOR WAS LEAKING AND SOME FUEL HAD ACCUMULATED IN THE FUSELAGE, UNDER THE CABIN F LOOR. 1H71 3O3 O A4CE E14EA 20010731000452001073100045NM 2001 7 31 CA010626027 120010607G2400FCC4008 RELAY BOEING737 7372E1 138448FNM PWA JT8 JT8D9A 52048NE COCKPIT FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) DURING CLIMB OUT, ALL LIGHTS ON FORWARD PANEL, AND GLARESHIELD ILLUMINATED. AIRCRAFT RETURNED WITHOUT INCIDENT. WHILE TROUBLE SHOOTING THE R33 RELAY WAS INTERCHARGED WITH THE R41 AND THIS SOLVED THEUNSERVICEABILITY. A NE W R33 RELAY WAS INSTALLED AND SYSTEM WAS TESTED SERVICEABLE. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2L72 4F4 F A16WE E2EA 20010731000462001073100046EA 2001 7 31 CA010626028 120010612G3244 TIRE CNDAIRCL601 CL6012A12 1900303EA GE CF34 CF343A 30015NE MLG FAILED W C ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CA (CAN) THREAD SEPARATION ON TAKEOFF WHICH INDUCED DAMAGE TO WHEEL WELL AREA. 2L72 4F4 FRTA21AE E15NE 20010731000472001073100047EA 2001 7 31 CA010626029 120010613G5246215310326 WEB CNDAIRCL215 CL2151A10 EA PWA R2800 CA3 52026NE WATER DOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FOLLOWING THE INCIDENT REPORTED ON A/C CL215-1A10 S/N 1076 (SDR DATED 00-08-24) BOMBARDIER AMO 35-95 DECIDED TO CARRY OUT A SPECIAL INSPECTION ON HIS FLEET. THE WEB P/N 215-31032-6 HAS BEEN FOUND CRACKED BEHIND RH AND LH UPLOCK SPIGOTS AND WATER DOOR ACTUATOR SPIGOTS IN WATER SYSTEM APPROX. FS368.5 ON VARIOUS A/C AND VARIOUS DEGREE. BOMBARDIER ENGINEERING HAS PRODUCED DIFFERNET REPAIR ENGINEERING ORDERS AND TWO GENERAL REAPIR APPLICABLE TO ALL CL215. REO 215-53-10-75 (WATER DOOR ACTUATOR MOUNTING LUGS) AND 215-53-10-093 (UPLOCK ACTUATOR MOUNTING LUGS. THE FOLLOWING A/C HAVE BEEN INSPECTED AND REPAIRED 2H72 4R4 R A14EA E231 20010731000562001073100056NE 2001 7 31 CA010626043 220010520G7261 SUMP CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE ENGINE COKED W E ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION APAPPROACH 1 CA (CAN). NR 2 ENGINE SHUT WITHOUT PILOT'S INPUT DURING THE APPROACH PHASE OF THE FLIGHT, APPROX 3500 FEET. UPON INSPECTION, MAINTNANCE NOTED: OIL DETECTED IN THE TAILPIPE, ENGINE QUANTITY CHECKED AND FOUND DEPLETED, AND SUMP B SCREEN COKED UP. ENGINE REPLACED AND A/C RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010731000572001073100057NM 2001 7 31 CA010626044 120010617G3260 DOWNLOCK SENSOR BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NLG FAILED W A UNSCHED LANDING N FALSE WARNING APAPPROACH 1 CA (CAN) NOSE GEAR TRANSIT LIGHT ILLUMINATED WHEN GEAR SELECTED DOWN. CREW CYCLED GEAR A COUPLE OF TIMES WITH NO RESULTS. A VISUAL CHECK THROUGH FLOOR HOLE VIEWER ATTEMPTED. NOSE GEAR VIEWER HARD TO DETERMINE VISUAL ON RED LINES FOR A LOCKED CONDITION.THE CREW OPTED TO RETURN TO STATION OF ORIGIN WITH AN UNEVENTFUL LANDING. THE A/C WAS FERRIED TO THE MAIN BASE FOR MAINTENANCE. MAINTTENANCE TESTED AND CONSEQUENTLY REPLACED THE NLG DOWN LOCK SENSOR. AS A PRECAUTION THE NLG VIEWER WAS CLEANED AND THE DOWNLOCK INDICATOR ARROWS WERE REPAINTED. 2L72 4F4 F A16WE E2EA 20010731000582001073100058EA 2001 7 31 CA010626045 120010619G3244299K631 TIRE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE MLG FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) AFTER TAKE OFF AT GEAR RETRACTION, THE CREW NOTED A LEFT MAIN LANDING GEAR DISAGREEMENT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL INSPECTED ANDFOUND THAT THE TREADHAD SEPARATED FROM THE LEFT INBOARD MAIN GEAR TIRE DURING THE TAKE OFF ROLL. COLLATERAL DAMAGE TO THE LEFT INBOARD FLAP AND MAIN GEAR DOOR BELL CRANK WERE ALSO OTED. THE FLAP ASSEMBLY P/N 601R14002-1 AND THE LEFT MAIN GEAR DOOR BELL CRANK P/N 601R31185-15 WERE ALSO REPLACED. 2L72 4F4 FRTA21EA E15NE 20010705000142001070500014EA 2001 7 5 CA010626046 120010619G5610 WINDSHIELD PPG NP1393219 CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE WINDSHIELD CRACKED W A UNSCHED LANDING O OTHER CLCLIMB 1 CA 5572 98343H4828 (CAN) PASSING THROUGH 8,000 FT. THE WINDSHIELD DEVELOPED A CRACK AND SHATTERED. AFTER THE EVENT THE AIRCRAFTIMMEDIATELY RETURNED FORA WINDSHIELD REMOVAL AND REPLACEMENT. 2L72 4F4 FRTA21EA E15NE 20010731000602001073100060EA 2001 7 31 CA010626049 120010524G5720 STRUCTURE CNDAIRCL600 CL6002B19 EA GE CF34 CF34* NE RT WING DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING PREFLIGHT INSPECTION MECHANIC OBSERVED THAT THE RT WING TIP HAD BEEN DAMAGED BY CONTACT WITH A HARD OBJECT 9LIKE A RUNWAY) THE WINGTIP FAIRING HAD BEEN GROUND DOWN TO THE UNDERLYING STRUCTURE AND ALSO DAMAGE THE WING EXTENSION LOWER SKIN. WING EXTENSION LOWER SKIN AND WING TIP FAIRING REPLACED WITH NEW PARTS. SKIN DOUBLER REPAIRED PER REO 601R-57-31-279. 2L72 4F4 FRTA21EA E15NE 20010731000612001073100061EA 2001 7 31 CA010626050 120010524G2751 TRANSMITTER CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE TE FLAP FAILED W O OTHER N FALSE WARNING APAPPROACH 1 CA (CAN) ON APPROACH AFTER SELECTING FLAP DOWN, CREW NOTICED THAT THE FLAP INDICATION WAS DIFFERENT FROM LEFT TO RIGHT. MAINTENANCE INSPECTED FLAP SYSTEM AMD FOUND FUNCTIONING NORMALLY. RT FLAP POSITION TRANSMITTER WAS DEFERRED PER MEL. 2L72 4F4 FRTA21EA E15NE 20010731000632001073100063 2001 7 31 CA010627008 420010612G3416215T5100876 NIPPLE BOMBDR CNDAIRCL215 CL2156B11215 EA STATIC PORT WRONG PART W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) A NIPPLE FITTING INSTALLED AT THE STATIC PORT OF THE ALTIMETER WAS FOUND TO BE THE WRONG TYPE HAVING AN OPENING OF .032 INCH INSTEAD OF THE RECOMMENDED .008 INCH. THIS COULD HAVE CAUSED PROBLEMS IN CALIBRATING THE ALTIMETER ABD FURTHER MORE , SHOULD FITTINGS DIFFER FROM PILOT TO CO-PILOT SIDE, THE INDICATIONS WILL LAG IN CLIMB ABD DESCENT BUT WILL BE CORRECT AT LEVEL FLIGHT. A BOMBARDIER SERVICE PROBLEM 34-12-00-001 WAS OPENED UP IN ORDER TO CORRECT THIS DISCREPENCY. 2H72 4T RTA14EA 20010731000662001073100066NM 2001 7 31 CA010627010 120010527G2612 CONNECTOR BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE NR 2 ENGINE DIRTY W O OTHER N FALSE WARNING CRCRUISE 1 CA (CAN) WHIE ENROUTE TO YYC, NR 2 ENGINE FIRE WARNING LIGHT AND BELL CAME ON. NO EVERHEAT LIGHT CAME ON. ENGINE SECURED AND AIRCRAFT LANDED IN YYC WITHOUT INCIDENT. ALL CONNECTOR PLUGS CHECKED AND CLEANED. MEL 26-2 RAISED. DMI 29776. FIRE BOTTLES REPLACED IAW MM 26-21-11. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2L72 4F4 F A16WE E2EA 20010731000682001073100068NM 2001 7 31 CA010627011 120010507G5242 SWITCH BOEING737 7372E1 138448FNM PWA JT8 JT8D9A 52048NE E/E BAY DOOR OBSTRUCTED W O OTHER D INFLIGHT SEPARATION DEDESCENT 1 CA (CAN) DURING FLIGHT, E& E BAY DOOR OPENED AND AIRCRAFT LANDED WITHOUT INCIDENT. E& E BAY DOOR SWITCH STICKER WAS JAMMING THE SWITCH IN THE DEPRESSED MODE. THE OBSTRUCTION WAS REMOVED AND THE DOOR CLOSED. INDICATION TESTED IAW MM 2-71-00 AND CHECKED SERVICEABLE. NO FURTHER INCIDENT SUBSEQUENT FLIGHT. 2L72 4F4 F A16WE E2EA 20010731000692001073100069NM 2001 7 31 CA010627012 120010515G5414 PANEL BOEING737 7372E1 138448FNM PWA JT8 JT8D9A 52048NE RT NACELLE MISSING W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A MAINTENANCE CHECK, IT WAS OBSERVED THAT THE RT AFT NACELLE PANEL WAS MISSING. SERVICEABLE PANEL WAS INSTALLED. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2L72 4F4 F A16WE E2EA 20010731000702001073100070 2001 7 31 CA010627013 420010501G2312 STATIC WICK BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE COMM SYSTEM WORN W O OTHER O OTHER DEDESCENT 1 CA (CAN) DURING DECEND AND FLYING THROUGH PRECIPITATION, BOTH VHF RADIOS HAD HEAVY STATIC. AIRCRAFT LANDED WITHOUT INCIDENT. 5 STATIC DISCHARGERS WERE FOUND OUT OF LIMITS. ALL REPLACED IAW MM 23-61-00. NO FU RTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2L72 4F4 F A16WE E2EA 20010705000152001070500015NM 2001 7 5 CA010627014 120010509G3700BACH30BC060332 LINE BOEING737 7372A9C 1384495NM PWA JT8 JT8D9A 52048NE RH PITOT STATIC WORN W K NONE O OTHER CRCRUISE 1 CA (CAN) AT CRUISE, FIRST OFFIER'S AIRSPEED INDICATION WASERRATIC, AIRCRAFT LANDED WITHOUT INCIDENT. FOUND PITOT STATIC LINES WORN. LINES REPLACED AND TESTED SERICEABLE IAW MM34-11-0. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2L72 4F4 F A16WE E2EA 20010731000712001073100071WP 2001 7 31 CA010627015 120010528G5610 WINDSHIELD HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL COCKIT CRACKED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) DURING FLIGHT F5890 FROM MADRID TO LYON, INCRUISE CO-PILOT WINDSHIELD INNER PLY CRACKED, UNSCHEDULED LANDING IN BIARRITZ. RT WINDSHIELD REPLACED. A/C RETURNED TO SERVICE. 1G71 3U3 U H3WE E4CE 20010731000732001073100073EA 2001 7 31 CA010627021 120010529G7120 WEB BOMBDR 60135006 CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE ENGINE SUPPORT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 19301 (CAN) DURING "C" CHECK, SIX CRACKS WERE FOUND INTHE ENGINE SUPPORT BEAM. TWO CRACKS WERE LOCATED ON THE LOWER WEB AT FS 640.0 BETWEEN LBL 9.5 AND RBL 9.5. FOUR CRACKS WERE LOCATED ON THE UPPER WEB AT FS 640 BETWEEN LBL 9.5 REPAIR PERFORMED PER REO 601R-53-61-345. 2L72 4F4 FRTA21EA E15NE 20010731000752001073100075NE 2001 7 31 CA010627025 220010612G7261 PUMP CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE ENGINE OIL FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CA (CAN) NR 2 ENGINE OIL PRESSRE BEGAN TO FLUCTATE DURING CRUISE. THE PRESSURE DROP FOLLOWED BY AN INCFREASE IN OIL TEMP. THE PILOT INITIATED AN IN FLIGHT SHUTDOWN. ENGINE OIL PUMP REPLACED. 2L72 4F4 FRTA21EA E15NE 20010731000772001073100077NE 2001 7 31 CA010627032 220010517G7261 ENGINE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE OIL SYSTEM MALFUNCTIONED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) DURING CRUISE FLIGHT CREW REPORTED LOW OIL PRESSURE AND ASSOCIATED WITH HIGH OIL TEMPERATURE. ENGINE REPLACED AND A/C RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010731000782001073100078NE 2001 7 31 CA010627034 220010619G7261 OIL SYSTEM CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE ENGINE FLUCTUATES W EA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) A/C IN CRUISE AT FL.310, CREW NOTICED FLUCTATION IN OIL PRESSURE WITH A LOSS OF OIL PRESSURE. ENGINE SHUT DOWN BY THE FLIGHT CREW AND LANDED IN PHOENIX. INVESTIGATING AT THIS POINT SHOWS OIL TANK AS GOOD. OIL LEVEL IN GEARBOX IS GOOD. GE ON WING SUPPORT IS ON SITE TO HELP WITH INVESTIGATION. FSR HAS REQUESTED THAT THE MDC BE DOWNLOADED AND THE DFDR BE DOWNLOADED. 2L72 4F4 FRTA21EA E15NE 20010731000802001073100080SW 2001 7 31 CA010627040 120010627G5302206031418005 SUPPORT BRACKET BELL 206031004 BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL TAIL BOOM BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE FLANGE FOR THE VERTICAL FIN UPPER ATTACHMENT BOLT IS SEPARATED FROM SUPPORT DUE TO CRACK. 1G71 3U3 U H2SW E4CE 20010731000822001073100082CE 2001 7 31 CA010627042 120010622G24347565T1 ALTERNATOR CESSNA305 305A 2074002CE CONT O470 O47011B 17026SO ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 CA 6 (CAN) ALTERNATOR REMOVED FROM AIRCRAFT AFTER PILOT REPORTED NO INDICATION OF CHARGE AFTER HIS LAST LANDING. AFTER MAKING A FEW TEST, IT WAS DETERINED THAT THE ALTERNATOR WAS FAULTY. THIS NEW ALTERNATOR WAS INSTALLED ON THE AIRCRAFT AS A REPLACEMENT FOR THE PREVIOUS DEFECTIVE ALTERNATOR. UPON REMOVAL OF THE DEFECTIVE ASSEMBLY NO EXTERIOR DAMAGES WAS FOUND THAT COULD HAVE LEAD TO THE FAILURE. SOMETHING INSIDE THE ALTERNATOR HAD FAILED BUT SINCE THE ALTERNATOR IS PARTIALLY SEALED AND IS ON WARRANTY COVERAGE NO FURTHER ACTION WAS TAKEN TO INVESTIGATE TH FAILED ASSEMBLY. 1H71 3O3 O 5A5 E269 20010731000842001073100084CE 2001 7 31 CA010627043 120010621G24347565T1 ALTERNATOR CESSNA305 305C 2074014CE CONT O470 O47011B 17026SO ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 CA 1 (CAN) ALTERNATOR REMOVED FROM AIRCRAFT AFTER PILOT REPORTED NO INDICATION OF CHARGE AFTER HIS LAST LANDING. AFTER MAKING A FEW TEST, IT WAS DETERMINED THAT THE ALTERNATOR WAS FAULTY. THIS NEW ALTERNATOR WAS INSTALLED ON THE AIRCRAFT AS A REPLACEMENT FOR THE PREVIOUS DEFECTIVE ALTERNATOR. UPON REMOVAL OF THE DEFECTIVE ASSEMBLY, A SMALL PIECE FELL OFF BY VENT DUCT OF THE SHROUD OF THE ALTERNATOR. LOOKING CLOSELY AT THE PIECE IT WAS DETERMINED THAT THIS SMALL PIECE WAS A DIODE. THE DIODE SEEMED NOT DAMAGED OTHER THAN BEING UNSOLDERED FROM THE INTERNAL PART OF THE ALTERNATOR. IT WAS CERTAINLY NOT SOLDERED PROPERLY AND FAILED WITH THE VIBRATIONS OF THE AIRCRAFT. THE P/N OF THE DIODE COULD BE SEEN EASILY.PN. MR2504W01H71 3O3 O 5A5 E269 20010731000992001073100099CE 2001 7 31 CA010627044 120010622G24347565T1 ALTERNATOR CESSNA305 305A 2074002CE CONT O470 O47011 17026SO ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 CA 4 (CAN) ALTERNATOR REMOVED FROM AIRCRAFT AFTER PILOT REPORTED NO INDICATION OF CHARGE AFTER HIS LAT LANDING. AFTER MAKING A FEW TESTS, IT WAS DETERMINED THAT THE ALTERNATOR WAS FAULTY. THIS OVERHAULED ALTERNATOR WS INSTALLED ON THE AIRCRAFT AS A REPLACEMENT FOR THE PREVIOUS DEFECTIVE ALTERNATOR. UPON REMOVAL OF THE DEFECTIVE ASSEMBLY, SMALL PIECES COULD BE HEARD MOVING INSIDE THE ALTERNATOR. THE ALTERNATOR WAS SHAKEN TO TRY AND REMOVE THESE PIECES BY THE SHROUD AIR VENT BUT NONE FELL OUT. SINCE THE ALTERNATOR IS PARTIALLY SEALED AND IS ON WARRANTY COVERAGE NO FURTHER ACTION WAS TAKEN TO INVESTIGATE THE FAILED PIECES. 1H71 3O3 O 5A5 E269 20010731001012001073100101EA 2001 7 31 CA010627046 120010626G7120 SUPPORT BRACKET GE CF343A1 CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 00 (CAN) BOMBARDIER AEROSPACE HAS JUST RECEIVED A REPORTALE SDR EVENT WHICH WE ARE REQUIRED TO REPORT ON. DURING INSPECTION OF ENGINE SUPPORT BEAM IAW SB A601R-53-059, MAINTENANCE FOUND CRACKS. REPAIR ENGINEERING ORDER PROGRESS, SHOULD BE PROVIDED TO THE OPERATOR SOON. 2L72 4F4 FRTA21EA E15NE 20010731001022001073100102EA 2001 7 31 CA010627047 120010622G7120 SUPPORT BRACKET GE CF343A1 CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 00 (CAN) DURING INSPECTION OF ENGINE SUPPORT BEA IAW SB A601R-53-059, MAINTENANCE FOUND CRACKS. REPAIR ENGINEERING ORDER PROVIDED, REPAIR IN PROGRESS. 2L72 4F4 FRTA21EA E15NE 20010731001032001073100103EA 2001 7 31 CA010627048 120010622G7120 SUPPORT BRACKET GE CF343A1 CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 00 (CAN) DURING INSPECTION OF ENGINE SUPPORT BEAM IAW SB A601R-53-059, MAINTENANCE FOUND CRACKS. REPAIR ENGINEERING ORDER PROVIDED, REPAIR IN PROGRESS. 2L72 4F4 FRTA21EA E15NE 20010731001052001073100105SW 2001 7 31 CA010627051 120010627G212121036012 BLOWER GULSTM690TP 690 0141720SW GARRTTTPE331TPE3315251K NM HARTZLHCB3T HCB3TN5 GL AIR DISTRIBUTIONSEIZED W O OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 CA 40 (CAN) SMOKE ENTERED COCKPIT AFTER ORBITING FIRE FOR 20 MINUTES. GROUND BLOWER RESET CIRCUIT BREAKER TRIPPED OFF. COCKPIT CHECKED FOR DAMAGED WIRING. ENGINE BLEED AIR SUPPLY WAS INSPECTED FOR OIL CONTAMINATION NO DEFECTS NOTED. GROUND BLOWER INTAKE WAS INSPECTED NO OBSTRUCTION WAS NOTED. GROUND BLOWER UNIT REPLACED FUNCTION TESTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 1H72 3T4 T 2A4 E2WE 6 CP15EA 20010731001072001073100107SW 2001 7 31 CA010627052 120010519G6320212040233001 TUBE BELL 212 212 1181420SW PWA PT6 PT6A34 52043EA TRANSMISSION OILCRACKED W EA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) DURING CRUISE 300 FT AGL, MAIN TRANSMISSION OIL PRESS WAS NOTICED FLUCTUATING. AN IMMEDIATE PRECAUTIONARY LANDING WAS CARRIED OUT. A/C WAS INTERMEDIATELY SHUT DOWN. UPON INVESTIGATION TUBE ASSY P/N 212-040-233-001 IN HELL HOLE WAS FOUND LEAKING. TUBE REPLACED TRANSMISSION FILTER WAS INSPECTED NO CONTAMINATION WAS FOUND. 6 LITRES OF OIL WAS ADDED. (12 L MAX CAPACITY) AIRCRAFT GROUND RUN & RETURNED TO SERVICE. 1G71 4U4 T H4SW E4EA 20010731001092001073100109CE 2001 7 31 CA010627053 120010625G5720MS2001426 BOLT BEECH 55 95A55 1152704CE CONT O470 IO470L 17026SO MCAULY2AF36C2AF36C39 GL WING FAILED W K NONE O OTHER ININSP/MAINT 1 CA 630 (CAN) UPON MPI IT WAS FOUND THAT 2 OF 4 WING BOLTS FAILED INSPECTION. IT WAS THANDETERMINED TO CHANGE ALL THE BOLTS. LOG ENTRY INDICATES BOLTS WERE LAST CHANGED IN 1992. THER IS NO RECORD OF BOLT INSPECTION SINCE THAT TIME ALTHOUGH INSPECTION IS CALLED FOR AFTER 5 YEARS. 1L72 3O3 O 3A16 3E1 5 CP911 20010731001102001073100110SO 2001 7 31 CA010627054 120010608G32226705403 TRUNNION PIPER PA28 PA28RT201T 7102817SO CONT O360 TSIO360FB 17025SO HARTZLHCC3Y PHCC3YF1 GL NLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2474 (CAN) WHILE INSPECTING SHIMMEY DAMPENER AS PART OF 100 HOUR INSPECTION. IT WAS DISCOVERED THAT THE NLG TRUNNION ASSEMBLY WAS CRACKED AT SHIMMEY DAMPENE R ATTACH POINT. 1L71 3O3 O 2A13 E9CE 5 CP25EA 20010731001112001073100111CE 2001 7 31 CA010627055 120010615G32341013841379 SWITCH BEECH 200 B200 1152922CE PWA PT6 PT6A42 52043NE HARTZLHCB3T HCB3TN3 GL COCKPIT INTERMITTENT W O OTHER J WARNING INDICATION CLCLIMB 1 CA 6147 (CAN) WHEN LANDING GEAR SELECTED UP AFTER TAKE OFF, GEAR DID NOT RETRACT. GEAR SELECTED BACK DOWN WITH NORMAL DOWN AND LOCKED INDICATION ON ALL GEAR. NORMAL LANDING CARRIED OUT WITHOUT INCIDENT. TROUBLESHOOTING FOUND INTERMITTENT MIRCOSWITCH CONTACTS IN LANDING GEAR SELECTOR SWITCH ASSEMBLY WHEN HANDLE SELECTED UP. ASSEMBLY REPLACED AND GEAR SWINGS COMPLETED. NO FURTHER FAULTS. 1L72 4T4 T A24CE E4EA 6 CP15EA 20010731001122001073100112CE 2001 7 31 CA010627056 120010626G561010138402515 WINDSHIELD BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA HARTZLHCB3T HCB3TN3 GL COCKPIT FAILED W B EMER. DESCENT O OTHER CRCRUISE 1 CA 3218 (CAN) AIRCRAFT WAS IN LEVEL FLIGHT AT 24000 FEET ON AUTOPILOT WHEN LT WINDSHIELD SHATTERED. FLIGHT CREW DEPRESSURIZED AND DESCENDED. AIRCRAFT RETURNED WITHOUR FURTHER INCIDENT. 1L72 4T4 T A24CE E4EA 6 CP15EA 20010731001142001073100114CE 2001 7 31 CA010627057 120010529G55102332051 GUSSET LEAR 263200032 LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE73122B 01518WP HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 14818 35002 (CAN) WHILE CARRYING OUT A ROUTINE INSPECTION (PHASE C6-1200HRS) ON THE HORIZONTAL STABILIZER "GUSSET" A CRACK WAS DISCOVERED IN THE GUSSET ERNINATING FROM THE EDGE OF THE LIGHTENING HOLE. THE INSPECTION SPECIFIES SCRUTINY OF THESEGUSSETS FOR CRACKS ON AIRCRAFT THAT DID NOT INCORPORATE AN EXTRA DOUBLER INSTALLED PER SSK 954. THIS AIRCRAFT DID NOT INCORPORATE THE DOUBLER. THE CRACK IS SMALL (.141 INCH LONG AND DIFFICULT TO SEE. IT WAS CONFIRMED USING HIGH FREQUENCY EDDY CURRENT. THERE IS A SMALL SCRATCH ON THE WEB OF THE GUSSET AT THE CRACK SITE. THE STABILIZER WAS REMOVED TO INSTALL LEAR SPECIAL SERVICES KIT 954 IN PLACE OF THE CRACKED GUSSET. 2L72 4F4 F A10CE E6WE 20010731001162001073100116NM 2001 7 31 CA010627059 120010627G3213 STABILIZER DHAV DHC8 DHC8101 2809002NM PWA 120 PW120 NE HAMSTD14SF 14SF7 NE MLG BROKEN W O OTHER O OTHER APAPPROACH 1 CA (CAN) PORT MAIN LANDING GEAR FAILED TO LOCK DOWN WHEN SELECTED DOWN FOR LANDING. GEAR WAS CYCLED AND LOCKED DOWN ON SECOND ATTEMPT. ON INSPECTION, THE LEFT SPRING ON THE PORT MLG STABILIZER STRUT WAS FOUND BROKEN. AS THIS IS NOT AN LRU, PERMISSION WAS OBTAINED TO FERRY AIRCRAFT TO MAIN BASE WITH GEAR LOCKED DOWN. AIRCRAFT FERRIED TO BASE FOR REPAIRS. PORT MAIN LANDING GEAR STABILIZER ASSY CHANGED IAW 32-10-26 GEAR RETRACTION CHECK CARRIED OUT SATISFACTORY. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010731001172001073100117CE 2001 7 31 CA010627060 120010615G7120075100125 MOUNT CESSNA180 180C 2072608CE CONT O470 O470L 17026SO MCAULY2A34C 2A34C66 GL ENGINE CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA 6950 (CAN) UPPER LT VERTICAL TUBING CRACKED AT LOWER GUSSET 1H71 3O3 O 5A6 E273 5 CP3EA 20010731001202001073100120CE 2001 7 31 CA010627061 120010614G32601303640489 CIRCUIT BOARD BEECH B300 B300 1159232CE PWA PT6 PT6A60A 52043NE HARTZLHCB4M HCB4MP3 GL MLG INDICATOR FAILED W L ABORTED APPROACH N FALSE WARNING LDLANDING 1 CA 5106 (CAN) ON APPROACH AIRCRAFT LOSS ALL GREEN ADVISORY LIGHTS AIRCRAFT MADE 3 FLY BY'S TO VERIFY GEAR DOWN & LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. THE LANDING GEAR LIGHTS ARE DIMMED THROUGH THE ABOVE P.C. BOARD. 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20010705000162001070500016SO 2001 7 5 CA010627062 220010618G8530648049 PISTON CONT I0360 CESSNA337 337G 2075730CE CONT O360 IO360G 17025SO MCAULY2AF34CD2AF34C306 GL PISTON BROKEN W O OTHER R PARTIAL RPM/PWR LOSS ININSP/MAINT 1 CA 1350 352436 (CAN) ON A GROUND RUN-UP PRIOR TO A SCHEDULED INSPECTION A PARTIAL POWER LOSS WAS DETECTED. A MOTO-STAT WAS CARRIED OUT AND #6 CYL. HAD VERY LOW COMPRESSION. A FILTER CHECK WAS CARRIED OUT AND SUBSTANIAL METAL PARTS, ALM, CHROME AND STEEL WERE FOUND THAT ARE CONSISTANT WITH A PISTON FAILURE. THE ENGINE HAS BEEN REMOVED FROM SERVICE. STRIP REPORT TO FOLLOW. 1H72 3O3 O A6CE E1CE 5 CP5EA 20010731001212001073100121EA 2001 7 31 CA010627063 220010621G731076778 MANIFOLD PIPER PA31 PA31 7103102SO LYC O540 TIO540A2B 41532EA HARTZLHCE3Y HCE3YR2A GL FUEL SYSTEM CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA 2407 (CAN) ON INSPECTION OF AD 93-02-05 FUEL INJECTOR LINES AND CLAMPS IT WAS NOTED THAT FUEL WAS LEAKING WITH BASE OF FITTING IN MANIFOLD. UPON REMOVAL OF MANIFOLD IT WAS TOWED TO BE CRACKED BETWEEN BOTH LT & TOP FITTING. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010731001222001073100122CE 2001 7 31 CA010628002 120010614G2510041405410 RELEASE SYSTEM CESSNA 04140711 CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA MCAULY1A103 1A103TCM GL SEAT SHEARED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA 11600 80173 (CAN) 3 OF 4 LATCH PINS CONTROLLING SEAT NIGHT FOUND SHEARED AT ENGAGEMENT HOLE ALLOWING SEAT TO DROP AND TILT. 1H71 3O3 ONT3A19 E223 5 NP50GL 20010731001352001073100135EA 2001 7 31 CA010628012 120010511G612012350 TUBE DHAV DHC3 DHC3 2800202EA PWA R1340 R1340* 52016NE HAMSTD23D 23D40 NE PROPELLER OIL BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 274 (CAN) COULD NOT CYCLE PROPELLER. FOUND OIL TRANSFER TUBE IN NOSE CASE BROKEN AT ATTACH POINT IN CENTRE OF TUBE. ONE TUBE REPLACED AT 274 HOURS SINCE OVERHAUL AND ANOTHER TUBE WAS REPLACED WITH 243 HOURS SINCE REPLACEMENT. THESE ARE 2 SEPARATE OCCURANCES. 1H71 3R3 R A815 5E2 6 CP719 20010731001382001073100138SO 2001 7 31 CA010628014 120010522G3097 WIRE PIPER PA31T PA31T 7103124SO PWA PT6 PT6A28 EA HARTZLHCB3T HCB3TN3 GL COCKPIT MELTED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA 9259 (CAN) DURING CRUISE, WITH ENGINE AND WINDSHIELD HEAT SELECTED. SMOKE WAS OBSERVED COMING FROM THE RIGHT FORWARD CIRCUIT BREAKER PANEL. AT THIS POINT THE RIGHT ENGINE AND WINDSHIELD DEICE SYSTEMS WERE TURNED OFF AND THE SMOKE DISSAPPEARED. THE AIRCRAFT LANDED SAFELY AT ITS DESTINATION. MAINTENANCE THEN DISCOVERED THAT 2 WIRES, BEHIND THE CIRCUIT BREAKER PANEL WERE MELTED : ONE BEING RIGHT INLET DEICE ANDTHE OTHER RIGHT WINDSHIELD HEAT. CORROSION WAS FOUND AT THE SPLICES, WHICH CAUSED EXCESSIVE HEAT. 1L72 3T4 T A8EA E4EA 6 CP15EA 20010731001392001073100139SW 2001 7 31 CA010628016 120010606G275012395 PULLEY BBAVIA8 8GCBC 1220803SW LYC O360 O360C2E 41514EA MCAULY1A200 1A200* GL FLAP SYSTEM SEIZED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) LT AND RT PULLEYS FOUND SEIZED AT WING ROOT(100 HOUR INSP.) BOTH CABLES FREYED AND UNSERVICEABLE. (LT/RT) AT POSITION OF PULLEY.SOLID ALUMINUM PULLEYS, NO BEARING , DIFFICULT TO KEEP LUBRICATED. HIGH POTENTIAL FOR INFLIGHT FLAP CABLE FAILURE. 1H71 3O3 O A21CE E286 5 NP874 20010731001442001073100144CE 2001 7 31 CA010628023 120010524G28231013890253 SHUTOFF VALVE BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA HARTZLHCB3T HCB3TN3 GL FUEL SYSTEM FAILED W D RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 CA (CAN) FAILED.PILOTS CHECK FOR LEAKING SHUTOFF VALVE AS PER FLT. MANUAL PROCEDURES. NEW VALVE INSTALLED CHECKED OK. 1L72 3T4 TRT3A20 E4EA 6 CP15EA 20010731001812001073100181CE 2001 7 31 CA010628029 120010511G551107321014 SPAR CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULY2A34C D2A34C58 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2572 (CAN) DURING ANNUAL INSPECTION FOUND PLAY IN HORIZONTAL STABILIZER TO ELINMINATE PLAY REPLACE ALL HARDWARE AND BUSHING IN ASS. DURING LUBRICATING OF ELEVATOR HINGES DISCOVERED CRACK ON STABILIZER HINGE REINFORCEMENT. THIS REINFORCEMENT IS RIVETED ON MAIN SPARE. STABILIZER HINGE IS BOLTED THROUGH MAIN SPARE AND REINFORCEMENT. A/C CONFIGURATION: SEAPLANE STRAIGHT FLOATS 1H71 3O3 O 3A24 E5CE 5 CP3EA 20010731001842001073100184SO 2001 7 31 CA010628037 120010525G324616205700 WHEEL PIPER PA44 PA44180 7104402SO LYC O360 O360E1A6 41514EA HARTZLHCC2Y HCC2YR2 GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 5266 (CAN) FLANGE OF OUTER WHEEL HALFFOUND CRACKED (4 INCHES) ALONG FLANGE WHERE TIRE BEAD SEATS. 1L72 3O3 O A19S0 E286 5 CP920 20010731002052001073100205EU 2001 7 31 CA010628038 120010520G26126493950730 FIRE LOOP AIRBUS320 A320212 EU CFMINTCFM56 CFM565A3 NE NR 2 ENGINE DAMAGED W K NONE N FALSE WARNING ININSP/MAINT 1 CA (CAN) PRF MESSAGE CHECK ENGINE NR 2 FIRE LOOP "B". THIS DEFECT WAS UNDER INVESTIGATION BY MAINTENANCE PERSONNEL AND ALSO DEFFERED UNDER MEL 26-12-01 CATEGORY "C" AS A RESULT OF THIS PFR MESSAGE. FIRE LOOP "B" REPLACEMENT WAS SCHEDULED WHILE OPERATING THE "C" DUCT FOR LOOP REPLACEMENT IT WAS NOTICED FOR DAMAGE TO THE NR 2 ENGINE RT "C" DUCT HEAT SHIELD. THE DAMAGE HAS BEEN CAUSE BY A MISSING "PISTON RING" (P/N336-510-710-0 OR 649-395-073-0 POST SB).MAINTENANCE PERSONNEL INSTALLED NEW PISTON RING, BUT AIRCRAFT WAS GROUNDED DUE TO THE EXTENSIVE DAMAGE TO THE 32 ENGINE RT "C" DUCT HEAT SHIELD. A TEMPORARY RE PAIR HAS BEEN ACCOMPLISHED TO THE HEAT SHIELD WITH A REPETITIVE INSPECTION EVERY "A" CHECK GRANTED BY BF GOO2L72 4F4 FRTA28NM E29NE 20010731002132001073100213EA 2001 7 31 CA010628039 220010628G8530LW19340 CAMSHAFT GULSTM500 500S 0141107SW LYC O540 IO540E1B5 41532EA HARTZLHCA3V HCA3VK2 GL ENGINE WORN W K NONE E VIBRATION/BUFFET CRCRUISE 1 CA 1440 (CAN) ENGINE HAD BEEN HARD TO START, LOW STATIC RPM AND HIGH MANIFOLD PRESSURE. ENGINE INSP. REVEALED THAT THE CAMSHAFT LOBE THAT DRIVES NR 5&6 CYL INTAKE VALVES WERE WORN. FURTHER TEAR DOWN OF ENGINE REVEALED NO FURTHER ABNORMAL WEAR OR CORROSION. 1H72 3O3 O 6A1 1E4 5 CP6EA 20010731002152001073100215SO 2001 7 31 CA010628042 120010527G29103036 HOSE PIPER PA31 PA31 7103102SO LYC O540 TIO540A2B 41532EA HARTZLHCE3Y HCE3YR2A GL HYD SYSTEM RUPTURED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) HYDRAULIC HOSE RUPTURE AT FITTING P/N MS24590-4. FITTING M524590-4 HAD WORN INTERNAL THREADS WHEN HOSE WAS MANUFACTURED. HOSE AND FITTING SEPARATED ON GEAR CYCLE. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010731002172001073100217SW 2001 7 31 CA010628043 120010520G5711 SPAR BBAVIA7 7CCM 21101MWSW CONT C90 C9012F 17009SO SNSNCH76AK M76AK EA WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) TO CARRY OUT AD 2000-25-02, ADDITIONAL HOLES WERE CUT IN EACH LOWER WING PANEL. NO PROBLEMS WERE FOUND. REMOVED WING ROOT FAIRINGS AND FABRIC ON TOP OF BOTH WINGS JUST TO BE SURE IN WING ROOT AREA. FOUND BOTH FWD SPAR ROOT ATTACH POINTS CRACKED AT THE ENDS. ALSO ONE LONG CRACK APPROX. 1 INCH DOWN FROM TOP TO BOTTOM OF SPAR APPROX. 4 FT LONG BETWEEN ROOT /STRUT WHICH WAS NOT SEEN UNTIL FABRIC WAS COMPLETELY REMOVED. THE OTTAWA AIRWORTHINESS OFFICE WAS CONTACTED. 1H71 3O3 O A759 E252 5 N1P210 20010731002202001073100220SO 2001 7 31 CA010628045 120010520G76032489403 CONTROL CABLE PIPER PA30 PA30 7103002SO LYC O320 IO320B1A 41508EA HARTZLHCE2Y HCE2YL2 GL THROTTLE FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CA 5141 5141 (CAN) THROTTLE CONTROL CABLE BROKE AT ENGINE END RESULTING IN LOSS OF ENGINE POWER SELECTION CAPABILITY. SUBSEQUENTLY, ALL ENGINE CONTROL /CABLES ON BOTH ENGINES WERE REPLACED. 1L72 3O3 O A1EA 1E12 5 CP9EA 20010731002442001073100244NM 2001 7 31 CA010628062 120010528G3260189915 UPLOCK SENSOR BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE MLG FAILED W O OTHER N FALSE WARNING CRCRUISE 1 CA (CAN) RED LEFT GEAR ANNUNCIATOR ON FORWARD PANEL ILLUMINATED IN FLIGHT WITH LANDING GEAR SELECTOR UP AND OFF. ALL OTHER LANDING GEAR ANNUNICATION (INCLUDING DOOR ANNUNICATORS) EXTINGUISHED. RED LEFT GEAR ANNUNICATOR EXTINGUISHED WITH ILLUMINATION OF GREEN LEFT GEAR LIGHT WHEN LANDING GEAR SELECTED DOWN. LEFT MAIN LANDING GEAR UP-LOCK SENSOR REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL AND TESTED SERVICEABLE. NO FURTHER DEFECTS NOTED IN THE LAST TWO FLIGHT LEGS. 2L73 4F4 F A3WE E2EA 20010705000202001070500020NM 2001 7 5 CA010628064 120010322G3040 WINDSHIELD TRIPLEX 0780306 DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE HAMSTD14SF 14SF7 NE WINDSHIELD CRACKED W O OTHER O OTHER CRCRUISE 1 CA 13748 TH2078 (CAN) BOMBARDIER AEROSPACE REGIONAL AIRCRAFT HAS JUST RECEIVED A REPORTABLE SDR EVENT WHICH WE ARE REQUIRED TO REPORT ON MARCH 22/01. IN CRUISE FLIGHT AT 15,000FT. THE FIRST OFFICERS WINDSCREEN CRACKED AND BECAME TOTALLY DISTORTED. EMERGENCY DECLARED AND FLIGHT DIVERTED TO BASE LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FIRST OFFICERS WINDSHIELD IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL OPERATIONAL CHECK OF WINDSHIELD GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010731002492001073100249EU 2001 7 31 CA010629006 320010514G6110697071003 BLADE ROTOL 697071003 DHAV DHC8 DHC8* NM PWC 150 PW150A EA ROTOL R4304 R4304* EU PROPELLER BURNED W O OTHER C F.O.D. APAPPROACH 1 CA (CAN) BOMBARDIER AEROSPACE REGIONAL AIRCRAFT HAS JUST RECEIVED A REPORTABLE SDR WEVENT WHICH WE ARE REQUIRED TO REPORT ON MAY 5/01. DURING APPROACH, THE PILOT REPORTED THAT THE R/H PROPELLER SUSTAINED A LIGHTENING STRIKE. INSPECTION OF THE PROPELLER UPON LANDING SHOWED A BURN MARK ON ONE BLADE APPROX 3MM IN WIDTH FROM TIP, CENTRE OF BLADE. IAW THE AMM THE PROPELLER ASSY, HUB ANDBETA TUBE HAVE TO BE REMOVED AND SENT TO DOWTY FOR INVESTIGATION. NEW ASSY, INSTALLED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN6 CP890 20010731002512001073100251EA 2001 7 31 CA010629009 120010522G2710 SERVO COLLINS 6222366001 DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6* 52043EA AILERON FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 CA (CAN) DURING FLIGHT, AILERON CONTROL LOST DUE TO AILERON SERVO SERVO PRIMARY JAMMED. AIRCRAFT RETURNED TO BASE. SERVO WAS REPLACED. AIRCRAFT RETURNED TO SERVICE. 1H72 3T3 TRTA9EA E2NE 20010731002542001073100254 2001 7 31 CA010629017 420010323G3417 ADC DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD14SF 14SF23 NE E/E BAY FAILED W A UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 CA (CAN) DURING CLIMB, AT APPROX. 6000FT, RDADC FAIL. BOTH ADVISORY DISPLAYS RESE T LIGHT WAS ON. SAT 2 WAS SHOWING DASHES. ALTITUDE SELECT BLANK. BASIC PITCH MESSAGE ON. VSI 2 SHOWED 0. ALT PRESELECT BLANK. YAW DAMPER FAIL. AP DISCONNECTED EGPWS FAIL. RNAV MESSAGE "ADC FAIL" TRUE AIRSPEED INOP. ON ECP, "NR 2 ENG ECU FLAGGED. NO CHANGE WHEN L DADC WAS MADE MASTER. FLT ABORTED. A/C RETURNED TO BASE.ON GROUND: NO FAULT CODES IN FLT FAULT SUMMARY. UNABLE TO DUPLICATE THEFAULT ON GROU ND #2 AIR DATA COMPUTER REPLD. CHECKED WATER DRAINS..OK PITOT/STATIC LEAK TESTOK/PURGED PITOT/STATIS LINES...OK A/C RETURN TO SERVI 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010731002562001073100256EA 2001 7 31 CA010629019 220010426G732125244405 FUEL CONTROL BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA HARTZLHCD4N3HCD4N3A GL ENGINE FAILED W O OTHER O OTHER APAPPROACH 1 CA 3514 (CAN) RT POWER LEVER IS VERY DIFFICULT TO SCHEDULE SUBTLE POWER CHANGES. IE. WHEN ATTEPTING TO SELECT A CHANGE OF 100 FT/LBS RESULTING TORQUE CHANGE COULD BE AS MUCH AS 400FT/LBS. THIS RESULTS IN AN OSCILLATION OF POWER LEVER MOVEMENT TO GET DESIRED POWER OUTPUT. THIS IS ESPECIALLY APPARENT WHEN LANDING WITH GUSTING WINDS. R/H FUEL CONTROL UNIT REPLACED. S/N OFF A7414.S/N ON A7968. TEARDOWN REPORT INDICATED GOVERNOR HYSTERESIS WAS 180 RPM. MAX ALLOWABLE IS 50 RPM. DRIVE BODY ALSO FOUND TO BE DIRTY/SOOTY. THIS WOULD CAUSE FCU TO RESPOND SLOWLY AND INTERMITTENTLY. 1L72 3T4 T A14CE E4EA 5 CSTC 20010731002592001073100259EA 2001 7 31 CA010629020 220010604G7230 SEAL SOCATATBM TBM700 8682000EU PWA PT6 PT6A6A 52043EA HARTZLHCE4N HCE4N3 NE ACTUATOR MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 CA 29 (CAN) INERTIA ACTUATOR MOTOR P/N 200N6071017220 WAS REPLD 29.9 HRS PRIOR TO FAILURE . NEW ACTUATOR WAS BEING INST WHEN NOTICES INERTIA APOATOR DEFLECTOR BEING CUT WHILE MANU MOVING. UNIT WAS REMOVED FROM HC & WHILE INVESTIGATING NOTICED SEAL THAT HAD UNEVEN MASHINGS FROM WEAR. WHEN DISLOCATED CREATED SAME PROBLEM OF DEFLECTOR BEING CAUGHT & REQ A LOT OF FORCE TO MOVE. THAT COND ITION TOOK OUT NEW MOTOR. EMPIRE PERFORMANCE DROPPED IN FLT & A/C ALTITUDE LIMITED. INCORRECT INST OF INERTIA SEPARATOR SEAL DISCLOSED CAUSING PROC FAILURE OF MOTOR DUE TO EXCESSIVE PRESSURE SUGGESTED CONNECTIVE ACTION-AFTER REMOVAL & REINSTATIN OF INERTIA SEPARATOR DISCONNECT WATER FROM ASSY & MANU CHECK. 1L71 3T3 TRTA60EU E4EA 5 CP10NE 20010731002612001073100261EU 2001 7 31 CA010629023 120010511G2434HED60CR132200 BRUSHES BOSCH 5243212158 PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL GENERATOR WORN W O OTHER J WARNING INDICATION CRCRUISE 1 CA 222 100037 (CAN) THE NR 2 GENERATOR CAUTION LIGHT ILLUMINATED ON THE CAWS PANEL. THE PILOT NOTED THAT THE NR 2 GENERATOR OUTPUT WAS FLUCTUATING BETWEEN A 60AMP DISCHARGE AND A 20 AMP POSITIVE CHARGE. HE TURNED THE GENERATOR OFF, THEN RE-SELECTED IT TO THE ON POSITION.THE RESET WAS SCESSFUL FOR APPROX. 20 MINUTES AT WHICH TIME FOR APPROX 20 MINUTES, THE PROBLEM REOCCURRED. MAINTENANCE FOUND THAT THE BRUSHES WERE WORN WELL BEYOND A SERVICEABLE LIMIT. A NEW SET OF BRUSHES WAS INSTALED AND THE AIRCRAFT GROUND RUN. NO FURTHER PROBLEMS NOTED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010731002632001073100263EU 2001 7 31 CA010629024 120010518G2434HED60CR132200 BRUSHES BOSCH 5243212158 PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL GENERATOR WORN W O OTHER J WARNING INDICATION CRCRUISE 1 CA 12 100037 (CAN) THE NR 2 GEN CAUTION LIGHT ILLUMINATED ON CAWS PANEL. PILOT ALSO NOTED THAT A VERY LOUD SQUEALING SOUND COULD BE HEARD IN HEADSET. CAUTION LIGHT THEN ILLUMINATED & PILOT THEN SELECTED NR 2 GEN SWITCH TO OFF POS. GEN WAS THEN RE-SELECTED TO ON POS, WITH SAME RESULT AS NOTED ABOVE. GEN #2 WAS THEN SELECTED TO OFF POS, & THEAIRCRA FT RETURNED TO BASE. ONCE AGAIN MAINTENACE FOUND THAT POST SB- "24-016" BRUSHES HAD FAILED WELL BEFORE THEIR LIFE LIMIT WAS REACHED. A EW SET OF POST S/B BRUSHES WAS INSTAND AIRCRAFT GROUND RUN, WITH NO FURTHER DEFECTS BEING NOTED. AS MENTION IN OUR PREVIOUS SDR 11-05-2001. MAINT HAS INSTITUED A VOLUNTARY 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010731002642001073100264NE 2001 7 31 CA010629025 220010522G73218063041 FUEL CONTROL PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL ENGINE FAILED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA 1215 (CAN) WHEN TRYING TO START ENGINE, THE ENGINE WOULD NOT ACCELERATE ABOVE APPROXIMATELY 35-39 PERCENT THE FUEL CONTROL UNIT WAS REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010731002652001073100265EU 2001 7 31 CA010629026 120010528G24349789601090 BRUSHES 5243212158 PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL GENERATOR WORN W K NONE O OTHER ININSP/MAINT 1 CA 94 100318 (CAN) DURING A 100 HOUR INSPECTION, THE BRUSH ASSEMBLY WAS REMOVED TO VERIFY THE CONDITION. THE BRUSH ASSEMBLY WAS WORN EXCESSIVELY AND HAS BEEN REPLACED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010731002672001073100267EU 2001 7 31 CA010629027 120010518G52709733024202 ARM PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL DOOR SWITCH BROKEN W D RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CA 1572 (CAN) ON CLOSING THE CARGO DOOR THE UNLOCKED WARNING LIGHT IN THE COCKPIT FAILED TO EXTINGUISH. ON INVESTIGATION THE ROLLER SPRING ON THE MICRO SWITCH WAS BROKEN. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010731002682001073100268EU 2001 7 31 CA010629029 120010518G24349789601090 BRUSHES 5243212158 PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL GENERATOR WORN W O OTHER J WARNING INDICATION APAPPROACH 1 CA 370 100092 (CAN) #2 GENERATOR FAIL LIGHT CAME ON DURING FLIGHT. AN INSPECTION OF THE BRUSHES SHOWED ONE TO HAVE SUFFERED SIGNS OF ARCING. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010731002712001073100271EU 2001 7 31 CA010629032 120010514G27105271012115 CONTROL CABLE PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL AILERON DEFECTIVE W K NONE O OTHER ININSP/MAINT 1 CA 1993 (CAN) WHEN INSPECTING CONTROL CABLES AS PER 2000HR/5YR. INSPECTION REQUIREMENT, SOME ABNORMALITIES WERE NOTED ON THE 2 FORWARD AILERON CONTROL CABLES. ON ONE OF THE BUNDLES OF STRANDS IT APPEARED AS IF 2 OR 3 OF THE INDIVIDAL STRANDS WERE SEPARATED FROM EACHOTHER WITH A SLIGHT KINK. THIS PATTERN REPEATED ITSELF EVERY 4 OR 5 INCHES. THIS ABNORMALITY IS ONLY A FEW MILLIMETERS IN LENGTH. THE 115 CABLE HASSEVERVAL OF THESE SUSPICIOUS SPOTS AND THE 116 HAS ONLY A FEW. THE CABLES HAVE BEEN REPLACED WITH NEW PILATUS PARTS AND THE SUSPECT CABLES HAVE BEEN FORWARDED TO OUR REGIONAL SUPERVISOR FOR FURTHER EVALUATION. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010731002722001073100272 2001 7 31 CA010629033 420010514G3425071014393100 CONTROL PANEL PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL COCKPIT MALFUNCTIONED W O OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 CA 1993 (CAN) HDG CONTROL KNOB FEELS SCRATCHY, CAUSING INTERMITTENT RED FLAG ON HDG SYMBOL ON EFIS.PANEL REPLACED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010731002742001073100274 2001 7 31 CA010629036 420010530G2210 SERVO HONEYWELL 7002260922 DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD14SF 14SF23 NE AUTOPILOT FAILED W C ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 CA 00105873 (CAN) ELEVATOR HEAVY OPERATION AFTER TAKE OFF. FLIGHT WAS ABORTED. LANDING WAS UNEVENTFUL. MAINTENANCE TESTS REVEALED THAT THE AUTO PILOT ELEVATOR SERVO MOTOR'S CLUTCH WAS STILL ENGAGED. ELEVATOR ACTUATOR SERVO MOTOR IS BEING REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010731002772001073100277NE 2001 7 31 CA010629038 220010517G72613033990 LINE DHAV DHC8 DHC8101 2809002NM PWA 120 PW120 NE HAMSTD14SF 14SF7 NE OIL SUPPLY FRACTURED W FA ACTIVATE FIRE EXT. UNSCHED LANDING AJ FLAME/FIRE WARNING INDICATION CRCRUISE 1 CA (CAN) AN INCID. OCCURRED ON CLIMB OUT. PILOTS RPT THAT NR 1 ENGINE TRQ DROPPED TO 30 PERCENT, PILOTS PULLED & RESET CCT BREAKER. 30 2NDS AFTER TRQ DROP WAS NOTICED NR 1 OIL PX DROPPED TO 0 PSI & FIRE IND. FOR NR 1 ENG. ILLUMINATED. PILOTS BLEW 1 FIRE BOTTLE AFTER ENGINE SHUTDO WN 28 SEC LATER FIRE IND. EXTINGUISHED A/C RETURNED TO BASE W/O INCID.. NR 1 ENGINE IS SEIZED WITH PROP UNFEATHERED. UPON INSP OF ENGINE, OIL SUPPLY LINE TO NR 6 BEARI NG FOUND FRACTURED. FIRE WAS CONTAINED WITHIN NACELLE FIREWALL, HOWEVER THERE HAS BEEN HEAT DAMAGE TO STRUCTURE: 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010731002792001073100279EU 2001 7 31 CA010629039 120010629G2913501310000 PRESSURE SWITCH VICKERS 887673 AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE HYD PUMP FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 528 528 MX632028 (CAN) DEPARTED YUL FOR KEF. WHILE IN CLIMB THE ENGINE NR 2 YELLOW HYDRAULIC PUMP FAULT LIGHT ILLUMINATED. THE PUMP WAS DE-ACTIVATED AND THE AIRCRAFT DIVERTED TO YHZ. MAINTENANCE TROUBLESHOOTING LOCATED A HYDRAULIC LEAK FROM THE HYDRAULIC PUMP NR 2 PRESSURE SWITCH. THE SWITCH ASSY WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA28NM E40NE 20010731002812001073100281WP 2001 7 31 CA010629040 120010608G323128B4028 TORQUE TUBE CVAC PBY5 PBY5A 2421208WP PWA R1830 R183092 52020NE MLG DOOR CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 6960 (CAN) NOSE GEAR DOOR TORQUE TUBES REMOVED FOR INSPECTION DUE TO THE PROMPTING OF A SERVICE DIFFICULTY ADVISORY. THE CONDITION PREDICTED IN THE ADVISORY (CORROSION) WAS FOUND TO EXIST IN A FAIRLY ADVANCED STAGE, PARTICULARLY AROUND THE TAPER PINS AND HOLES. THESE TUBES HAVE BEEN MODIFIED WITH GREASE FITTINGS TO FACILITATE FILLING THE TUBES WITH GREASE, HOWEVER, AN INCOMPLETE FIL HAD IN FACT MADE THE PROBLEM WORSE. THE PLUGS OF GREASE HAD IN FACT CREATED POCKETS WHERE MOSITURE WAS TRAPPED, WORSENING THE PROBLEM. NEW TUBES WERE FABRICATED AND INSTALLED WITH NEW HARDWARE. AS THE ADVISORY POINTS OUT, FAILURE DURING WATER LANDING COULD HAVE FATAL CONSEQUENCES IF THE DOOR COLLAPSE. 2H72 4R4 R 2548 5E4 20010731002822001073100282NE 2001 7 31 CA010629043 220010317G7321324485318 FUEL CONTROL DHAV DHC8 DHC8201 2809001NM PWA PW120 PW123 NE HAMSTD14SF 14SF23 NE RT ENGINE FAILED W A UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 CA 30 (CAN) THE NR 2 ENGINE POWER COULD NOT BE ADJUSTED AFTER TAKEOFF TO SET POWER. THEAIRCRAFT EXPERIENCED MODERATE TURBULENCE BETWEEN 20 TO 21 THOUSAND FEET. THE ENGINE WAS STUCK AT ABOUT 88 PERCENT TORQUE AND FUEL FLOW WAS ABOUT 610 TO 640 LBS PER HOUR. AT ENGINE SHUTDOWN AN OVER TORQUE WA S NOTED BUT IT IS NOT KNOWN HOW MUCH OVER. WITH THE POWER LEVER AT FLIGHT IDLE THE FUEL FLOW WAS STILL NOTED TO BE 610 TO 640LB 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010731002852001073100285NM 2001 7 31 CA010703002 120010611G5330 SKIN BOEING737 737296 1384486NM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 52471 (CAN) CRACK IN FUSELAGE SKIN LEFT SIDE BETWEEN FUSELAGE STATIONS 747 AND 767, STRINGER 17L REPAIRED AS PER SRM 53-30-3, TABLE 1, METHOD 1, PAGES 87,88 & 88A. 2L72 4F4 FRTA16WE E2EA 20010731003022001073100302NM 2001 7 31 CA010703007 120010612G5610 WINDSHIELD DHAV DHC8 DHC8* NM PWC 150 PW150A EA COCKPIT CRACKED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) CO-PILOTS WINDSHIELD CRACKED IN CRUISE. A/C THEN DESCENDED, SLOWED AND REDUCED PRESSURIZATION. A/C LANDED UNEVENTFUL. WINDSHIELD REPLACED. 2H72 4T4 TRTA13NM E00062EN 20010731003082001073100308EU 2001 7 31 CA010703013 120010614G6410355A12005004 BLADE SNIAS 355A12005004SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE TAIL ROTOR FAILED W A UNSCHED LANDING C F.O.D. CLCLIMB 1 CA 1528 6964 (CAN) T/R BLADES WERE SUBJECTED TO A MINOR CONTACT ON THE OUTBOARD SKIN AREA WITH A PINE BOUGHT IN SLOW FORWARD FLIGHT, A/C THEN LANDED TO INSPECT THE BLADES. BLADES WERE REMOVED TO HAVE CRACKS IN THE FILLER AROUND THE EDGE OF THE TABS REPAIRED ( WARRANTY WORK) AND ALSO TO FURTHER INSPECT AND REPAIR MINOR BLADE DAMAGE. 1G71 3U3 U H9EU E00054EN 20010731003092001073100309EU 2001 7 31 CA010703015 120010628G2560504202201 BUCKLE AMSAFTYEQUIP504202403 PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL SEAT BELT BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 1240 AFG0598790 (CAN) CO-PILOTS SEAT BELT BUCKLE WOULD NOT UNLATCH WHEN OPERATED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010731003192001073100319SO 2001 7 31 CA010703026 120010614G273071056003 SPRING PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA ELEVATOR BROKEN W D RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 CA 632 (CAN) AFTER LANDING, THE PILOT NOTED UNUSUALY LIGHT ELEVATOR.UPON SHUTDOWN, THE ELEVATOR WAS INSPECTED AND IT WAS NOTED THAT THE SPRING WAS BROKEN. UPON INSPECTION OF RECORDS, THE PART WAS FOUND TO HAVE 632HOURS SINCE REPLACEMENT AS PER AWD 98-08-18. THE PART HAS BEEN RETAINED IF FUTURE INSPECTION IS REQUIRED. 1L72 3O3 O A20SO E14EA 20010731003252001073100325CE 2001 7 31 CA010703032 120010622G8011654472 BUSHING CESSNA421 421C 2076016CE CONT O520 GTSIO520L 17032SO MCAULY3FF32 3FF32C501 GL STARTER SHAFT WORN W K NONE O OTHER ININSP/MAINT 1 CA 375 (CAN) DURING SCHEDULED COMPLIANCE WITH CSB-94-4C THE STARTER SHAFT BUSHING WAS FOUND TO BE LOOSE IN THE ENGINE CASE. 1L72 3O3 O A7CE E7CE 5 CP45GL 20010705000212001070500021NE 2001 7 5 CA010703034 220010617G7210130000405 BEARING HONEYWELL T5313B BELL 205 205A1 1181414SW LYC T53 T5313B 41549NE BEARING BROKEN W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA 1413 LE07592 (CAN) ENGINE CHIP LT CAME ON. METAL CHIPS WERE FOUND IN CHIP PLUG & FILTER. REPLACED ENGINE. INVESTIGATION SHOWS BEARING P/N 1-300-004-05 CAGE WAS BROKEN & INNER/ OUTER RACE BEARING SURFACE HAD FLAKE DAMAGE. 1G71 4U4 U H1SW E17EA 20010731003272001073100327CE 2001 7 31 CA010703035 120010615G24346682 RETAINER SKYTRONICS 7565T1 CESSNA305 305C 2074014CE CONT O470 O47011 17026SO ALTERNATOR BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 113 0201123 (CAN) ALTERNATOR REMOVED FROM A/C ENGINE FOR INVEST. & TO SEE IF RETAINER CUP WS DAMAGED. SMALL PIECES OF METAL & RUBBER FELL OFF ACCESSORIES CASE UPON REMOVAL OF ALTNR. LOOKING AT ALTERNATOR SPLINE GEAR & DRIVE SHAFT, EVIDENCE OF DAMAGES WERE FOUND. RETAINING CUP WAS SHREDDED IN PIECES & ONLY ONE RUBBER BUSHING LEFT IN PLACE. AT TIME OF REMOVAL ALTNR WAS CHARGING PRO PERLY INDICATING THAT SHAFT OF ROTOR WAS STILL TURNING. RETAINING CUP & RUBBER BUSHINGS ARE MOUNTED BETWEEN SPLINE GEAR DRIVING SHAFT & ROTOR SHAFT OF ALTNR. THIS INSTATION IS DESIGNED TO SHEAR OFF & PREVENT DAMAGES TO ENGINE IN CASE WHERE AN ALTNR. THIS INST IS DESIGNED TO SHEAR OFF 1H71 3O3 O 5A5 E269 20010731003282001073100328CE 2001 7 31 CA010703036 120010615G24346682 RETAINER SKYTRONICS 7564T1 CESSNA305 305C 2074014CE CONT O470 O47011B 17026SO ALTERNATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 44 0201124 (CAN) ALTERNATOR REMOVED FROM AIRCRAFT ENGINE FOR INVESTIGATION AND TO SEE F RETAINER CUP WAS DAMAGED. LOOKING AT THE ALTERNATOR SPLINE EAR AMD DRIVE SHAFT, EVIDENCE OF DAMAGES WERE FOUND. THE RETAINING CUPWAS CRACKED WHERE THE RUBBER BUSHINGS ARE SEATED. THE RETAINING CUP AND RUBBER BUSHINGS ARE MOUNTED BETWEEN THE SPLINE GEAR DRIVING SHAFT AND THE ROTOR SHAFT OF THE ALTERNATOR. THE INSTALLATION IS DE SIGNED TO SHEAR OFF AND PREVENT DAMAGES TO THE ENGINE IN THE CASE WHERE AN ALTERNATOR SHAFT WOULD SEIZE UP. IN THIS CASE, A FE WMORE HOUR FLIGHT WOULD HAD CERTAINLY CAUSED THE TOTAL BREAK OF THE CRACKED RETAINER CUP AND FAILURE OF THE ALTERNATOR. 1H71 3O3 O 5A5 E269 20010731003302001073100330CE 2001 7 31 CA010703037 120010615G24346682 RETAINER SKYTRONICS 7565T1 CESSNA305 305A 2074002CE CONT O470 O47011 17026SO ALTERNATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 50 0201120 (CAN) ALTERNATOR REMOVED FROM A/C ENGINE FOR INVESTIGATION AND TO SEE IF RETAINER CUP WAS DAMAGED. LOOKING AT THE ALTERNATOR SPLINE GEAR AND DRIVE SHAFT, EVIDENCE OF DAMAGES WERE FOUND. THE RETAINING CUP WAS CRACKED WHERE THE RUBBER BUSHINGS ARE SEATED. THE RETAINING CUP AND RUBBER BUSHINGS ARE MOUNTED BETWEEN THE SPLINE GEAR DRIVING SHAFT AND THE ROTOR SHAFT OF THE ALTERNATOR. THE INSTALLATION IS DESIGNED TO SHEAR OFF AND PREVENT DAMAGES TO THE ENGINE IN THE CASE WHERE AN ALTERNATOR SHAFT WOULD SEIZE UP. IN THIS CASE, A FEW MORE HOU OF FLIGHT WOULD HAD CERTAINLY CAUSED THE TOTAL BREAK OF THE CRACKED RETAINER CUP AND THE FAILURE OF THE ALTERNATOR. 1H71 3O3 O 5A5 E269 20010731003362001073100336CE 2001 7 31 CA010703038 120010614G24346682 RETAINER SKYTRONICS 7565T1 CESSNA305 305A 2074002CE CONT O470 O47011B 17026SO ALTERNATOR FAILED W K NONE O OTHER ININSP/MAINT 1 CA 76 0201121 (CAN) ALTERNATOR REMOVED FROM A/C ENGINE FOR INST ON A NEW ENGINE FOR THIS A/C. NO PILOT RPTED LOSS OF CHARGE BEFORE ENGINE WAS STOPPED FOR HIS TBO. SMALL PIECES OF METAL & RUBBER FELL OFF THE ACCESSORIES CASE UPON REMOVAL OF ALTNR. LOOKING CLOSELY TO ALTNR SPLINE GEAR & DRIVE SHAFT, EVIDENCE OF DAMAGES WERE FOUND. RETAINING CUP & RUBBER BUSHINGS WERE COMPLETELY SHREDED. SPLINE GEAR LUGS WERE ALSO BROKEN OFF & THIS PARTICULAR ALTNR, ROTOR SHAFT SHEARED. RETAINING CUP & RUBBER BUSHINGS ARE MOUNTED BETWEEN SPLINE GEAR DRIING SHAFT & THEROTOR SHAFTOF ALTERNATOR. THIS INST IS DESIGNED TO SHEAR OFF & PREVENT DAMAGES TO ENGINE IN CASE WHERE AN ALTNR SHAFT 1H71 3O3 O 5A5 E269 20010731003372001073100337CE 2001 7 31 CA010703039 120010613G24346682 RETAINER CUP SKYTRONICS 7565T1 CESSNA305 305A 2074002CE CONT O470 O47011B 17026SO ALTERNATOR FAILED W K NONE O OTHER ININSP/MAINT 1 CA 73 0201126 (CAN) ALTERNATOR REMOVED FROM A/C AFTER PILOT REPORTED NO INDICATION OF CHARGE AFTER HIS LAST LANDING. SMALL PIECES OF METAL AND RUBBER FELL OFF THE ACCESSORIES CASE UPON REMOVAL OF ALTERNATOR. LOOKING CLOSELY TO THE ALTERNATOR SPLINE GEAR AND DRIVE SHAFT, EVIDENCE OF DAMAGES WERE FOUND. THE RETAINING CUP AND TH RUBBER BUSHINGS WERE COMPLETLY SHREDDED. THE SPLINE GEAR LUGS WERE ALSO BROKEN.THE RETAININGCUP AND RUBBER BUSHINGS ARE MOUNTED BETWEEN THE SPLINE GEAR DRIVING SHAFT AND THE ROTOR SHAFT OF THE ALTERNATOR. THIS INSTALLATION IS DESIGNED TO SHEAR OFF AND PREVENT DAMAGES TO THE ENGINE IN THE CA S WHERE AN ALTERNAOTR SHAFT WOULD SEIZE UP. IN THIS CASE, THE ALTERNATOR SHAFT COULD BE TURNED FREEY 1H71 3O3 O 5A5 E269 20010731003402001073100340EA 2001 7 31 CA010704011 120010627G7120 BEAM GE CF343B1 CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE ENGINE SUPPORT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACKS WERE FOUND DURING ENGINE SUPPORT BEAM INSPECTION, AS PER SB601R-53-059. 2L72 4F4 FRTA21EA E15NE 20010705000222001070500022NE 2001 7 5 CA010704015 220010627G7200 CARBON SEAL GE CF343B1 CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE CARBON SEAL FAILED W G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) BOMBARDIER AEEROSPACE HAS JUST RECEIVED A REPORTABLE SDR EVENT WHICH WE ARE REQUIRED TO REPORT ON. WHILE IN CRUISE FLIGHT THE CREW COULD SMELL AND SEE SMOKE.OXYGEN MASKS WERE DONNED BY THE CREW ANDTHEPAX MASKS WERE DEPLOYED. FLIGHT WAS DIVERTED. UPON INVESTIGATION THE ENGINE #1 CARBON SEAL WAS FOUND TO HAVE COME APART. 2L72 4F4 FRTA21EA E15NE 20010731003452001073100345EA 2001 7 31 CA010704024 120010629G5320 PLATE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING C CHECK, MAINTENANCE FOUND A CRACK LOCATED IN THE PLATE ASSY. RBL 45.00 AT THE JOINT WITH THE FLOOR BEAM SUPPORT ANGLE AT PRESSURE BULKHEAD FS 621.00 THE CRACK WAS CONFIRMED USING NDT INSPECTION. 2L72 4F4 FRTA21EA E15NE 20010731003482001073100348 2001 7 31 CA010704028 420010629G3160 CONTROL UNIT CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 FAILED W A UNSCHED LANDING O OTHER CLCLIMB 1 CA (CAN) DURING CLIMB PILOT REPORTED EICAS MESSAGE DCU NR 2 AUR AL FAIL, APR FAIL AND FLUCTATION OF ENGINE PARAMET ERS 9N1,N2 & ITT) ON BOTH ENGINES. THEY SELECTED THE APR SWITCH OFF AND THE FLUCTUATIONS WENT AWAY, FLIGHT CONTINUED TO NICE. IT CAME BACK AT 40 NM OF MONTPELLIER. BASED ON MDC CODES MAINTENANCE FOUN DCU NR 2 DEFECTIVE. REPLACED DCU NR 2, AIRCRAFT BACK IN SERVICE. 2L72 4F4 FRTA21EA E15NE 20010725005552001072500555WP 2001 7 25 CA010706004 120010429G32001523153115 SWITCH LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE SWITCH FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) AFTER DEPARTURE FROM YMX, THE TRUCK LIGHT CAME ON, NORMAL PROCEDURES WHERE NOT TO RETRACT THE GEAR, CREW DUMPED FUEL AND RETURNED TO BASE. FOUND TRUCK SWITCH AT FAULT, COMPLETE ACTUATOR REP LACED AND AIRCRAFT RELEASED FOR A FLIGHT TEST, SYSTEM CHECKED SERVICEABLE AND AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A23WE E12EU 20010731003522001073100352WP 2001 7 31 CA010706006 120010428G49702621TB9 TERMINAL BLOCK LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE APU DESTROYED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FOLLOWING APU WARNING HORN RCCB TRIPPED OFF FOUND 5 WIRES WHEE THE INSOLATION WAS BROKEN AND RELATED TERMINAL BUS CHEMICALLY DESTROYED BY SKYDROLL. APU FIRE-EX BOTTLE SQUIB WAS INTERMITTENT DUE TO DAMAGE. REPLACED TB AND REPAIRED WIRING AND AREA CLEAN FROM SKYDROL AND INSPECTED FOR LEAKS. NO LEAKS WERE NOTED, AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A23WE E12EU 20010725005562001072500556WP 2001 7 25 CA010706007 120010428G3320 TERMINAL BLOCK LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE ROW 23 L/H CEILIOVERHEATED W K NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA (CAN) ON ARRIVAL CREW REPORTED SMOKE AT ROW 23 L/H CEILING. FOUND LUMINARE TERMINAL BLOCK OVERHEATED. LUMINARE ASSEMBLY REPLACED AND TERMINAL BLOCK REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A23WE E12EU 20010731003532001073100353EU 2001 7 31 CA010706008 120010508G7120S5411020001000 MOUNT AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE HAMSTD14SF 14SF5 NE LT ENGINE WORN W K NONE O OTHER ININSP/MAINT 1 CA 18491 (CAN) LEFT ATACHMENT FOR LOWER NACELLE IS WORN AND HOLE ARE ELONGATED. ENGINE MOUNT TO BE REPLACED BEFORE FURTHER FLIGHT. 2H72 4T4 TRTA53EU E20NE 6 CP7NE 20010731003542001073100354CE 2001 7 31 CA010706009 120010505G531050430043865 DOOR FRAME BEECH 100 B100 1152919CE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DOOR FRAME AFT FOUND CRACKED AROUND REAR BAYONET. 1L72 4T A14CE 20010731003552001073100355SW 2001 7 31 CA010706014 120010430G6410206011809109 PITCH HORN BELL 206 206L 1181522SW ALLSN 250C 250C20B 03013GL TAIL ROTOR LOOSE W K NONE O OTHER ININSP/MAINT 1 CA 730 (CAN) DURING A DAILY INSPECTION, WE DISCOVERED THAT THE TORQUE OF THE BOLTS HOLDING THE PITCH HORN TO THE TAIL ROTOR BLADE WAS LOOSE. THE LOCKWIRE WAS STILLIN PLACE BUT THE 2 BOLTS WERE NO LONGER TORQUED.DURING THE DISMANTLING NO OTHER ANORMALITIES. THE PITCH HORN AND THE TAIL ROTOR BLADE WERE DISMANTLED, CLEANED, CHECKED AND REASSEMBLED IN ACCORDANCE TO THE (BELL HELICOPTER T EXTRON) COMPONENT REPAIR& OVERHAUL MANUAL CHAPTER 4. IF THIS DISCREPANCY HAD NOT BEEN FOUND, IT MIGHT HAVE RESULTED IN A TAIL ROTOR CONTROL LOSS. 1G71 3U3 U H2SW E4CE 20010731003562001073100356EA 2001 7 31 CA010706015 120010305G2910 LINE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE HYD SYSTEM LEAKING W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) PILOT REPORT: HYDRAULIC SYSTEM NR 2 LOW PRESSURE MESSAGE DURING CRUISE. FOUND HYDRAULIC SYSTEM NR 2 EMPTY OF FLUID. MAINTENANCE FINDING: FOUND FITTING OF FILL LINE LEAKING (REF IPC 29-11-00-5-270). FOUND FITTING ADAPTER WRONG INSTALLED ON FILL LINE. INSTALLED SWAGE ADAPTER. REFILLED HYDRAULIC AND REPLACED UNSERVICEABLE EDP. 2L72 4F4 FRTA21EA E15NE 20010731003572001073100357EA 2001 7 31 CA010706016 120010505G5610 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FOUND THE CAPTAIN WINDSHIELD INNER PLY CRACKED ON AN UNSCHEDULED MAINTENANCE INSPECTION. WINDSHIELD REPLACED, AIRCRAFT BACK IN SERVICE. 2L72 4F4 FRTA21EA E15NE 20010725005572001072500557EA 2001 7 25 CA010706017 120010513G7732 ENGINE GE CF343B1 CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE R/H ENGINE FAILED W A UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 CA EBU7114 (CAN) ON TAKEOFF R/H ENGINE N2 VIBRATION EXCEEDED LIMITS, IN FLIGH T ENGINE SHUT DOWN CARRIED OUT AND AIRCRAFT RETURNED FOR TROUBLSHOOTING 2L72 4F4 FRTA21EA E15NE 20010725005582001072500558EA 2001 7 25 CA010706018 120010513G5610601R330333 WINDSHIELD CNDAIR CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE L/H WINDSHIELD CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 95039H2892 (CAN) LEFT WINDSHIELD CRACKED. WINDSHIELD REPLACED. 2L72 4F4 FRTA21EA E15NE 20010731003582001073100358EA 2001 7 31 CA010706019 120010513G5610601R33033 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA (CAN) AT FL330 THE CAPTAIN'S WINDSHIELD SHATTERED. NO CONFIRMATION IF PIECES OF WINDOW DEPARTED AIRCRAFT. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IN ACCORDANCE WITH AMM 54-11-01. 2L72 4F4 FRTA21EA E15NE 20010731003602001073100360EA 2001 7 31 CA010706020 120010326G2460M81381 HARNESS CNDAIRCL601 CL6012A12 1900303EA ELECTRICAL CHAFED W K NONE O OTHER ININSP/MAINT 1 CA 7194 (CAN) A TECHNICIAN WAS WORKING IN AFT FUSELAGE SECTION,PAINTING AROUND APU EXHAUST OUTLET WHEN HE 1ST SMELLED SMOKE.HE THEN SAW A WIRE BUNDLE ERUPTING INTO SPARKS & FIRE EVEN THOUGH THERE WAS NO CONTACT WITH WIRE BUNDLE WHEN EVENT OCCURRED.THE BATTERY WAS CONNECTED BUT A/C POWER WAS OFF.IT IS ASSUMED THAT THERE WAS AN EXISTING CHAFING CONDITION & THAT WIRE BUNDLE HAD BEEN DISTURBEDDURING APU EXHAUST REMOVAL.ONE CCT BREAKER POPPED ON JB-4 & IT WAS NOT NOTED BY TECH.17 WIRES HAVE BEEN DAMAGED WHERE SOME WERE POWERED BY BATTERY DIRECT BUS.SOME OTHER A/C INSP FOR CHAF ING CONDITIO N & A/C 3025 WIRING WAS ROUTED SLIGHTLY DIFFERENT.THE CUSTOMER MADE SOME TEMP SPLICES & WILL REPL ALL DAMAGED WIRES SHORTLY. 2L72 4F RTA21AE 20010731003622001073100362SW 2001 7 31 CA010711002 120010625G623020601033217 MAST BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL MAIN ROTOR DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA 9863 2715 (CAN) WHEN REASSEMBLED 1/2 OF THE SPLIT CONE ASSEMBLY HAD NOT SEATED PROPERLY IN THE GROVE IN THE MAST. MAIN ROTOR MAST NUT TORQUE CHECK WAS CARRIED OUT AFTER 1.3 HOURS OF OPERATION AND TORQUE LOSS WAS NOTED. WHEN DISASSEMBLED AGAIN DAMAGE TO THE SPLINE WAS FOUND. MAIN ROTOR MAST AND SPLIT CONES WERE REPLACED. 1G71 3U3 U H2SW E4CE 20010731003652001073100365EU 2001 7 31 CA010711008 120010627G2910HTE400005 CHECK VALVE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP ROTOL R333 R333482F12 GL HYD SYSTEM CRACKED W O OTHER K FLUID LOSS APAPPROACH 1 CA (CAN) PILOTS WERE NOT ABLE TO EXTEND LANDING GEAR. GEAR WAS PUMPED DOWN (EMERGENCY EXTENSION). AIRCRAFT LANDED WITHOUT INCIDENT. CHECK VALVE WAS FOUND CRACKED, ALLOWING FLUID TO EXCAPE SYSTEM. NO PHYSICAL DAMAGE THAT COULD CAUSE CRACK WAS EVIDENT. PART REPLACED. SYSTEM CHECKED AND SERVICED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA21EU E4WE 6 CP61GL 20010801000312001080100031NM 2001 8 1 CA010711014 120010622G531085310776111 WINDOW POST DHAV DHC8 DHC8103 1386005NM COCKPIT CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 25978 (CAN) L/H AND R/H FLIGHT COMPARTMENT WINDSHIELD FRAMS P/N 85310776-111 AND P/N 85310776-112 ARE CORRODED AT THE BOTTM OF THE FRAMES. THIS CORROSION WAS FOUND DURING THE SCHEDULED MAINTENANCE GROUND RUNS, PRESSURIZATION LEAK CHECK. A STREAM OF WATER SPOUTED FROM THE L/H WINDSHIELD CORNER. WINDSHIELDS WERE REMOVED AND DURING FURTHER CLEANING AND INSPECTION CORROSION WAS FOUND ON THE LOWER PORTION OF THE FRAMES. 2H72 4T RTA13NM 20010801000622001080100062EA 2001 8 1 CA010711015 120010628G2460CE934641 TERMINAL BLOCK DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE ELECTRICAL OVERHEATED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) TERMINAL BLOCK 2449-TB3 SHOWS SIGN OF OVERHEATING DUE TO CORROSION ON AFT SIDE OF REAR PRESSURE BULKHEAD. THE OVERHEATING OF THE TERMINAL BLOCK RESULTED IN IGNITION OF THE INSULATION ON THE TERMINAL LUG OF FEEDER CABLE 2449-37A0-1. THE OVERHEATING AND CORROSION WERE FOUND WHEN COMPLYNG WITH DASH 8 SERVICE BULLETIN 8-24-48. 2H72 4T4 TRTA13NM E20NE 20010801000652001080100065EA 2001 8 1 CA010713003 120010629G8011 NUT DHAV DHC7 DHC7102 2802708EA PWA PT6 PT6A50 52043EA HAMSTD24PF 24PF305 GL STARTER GEN SHEARED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING SCHEDULED MAINTENANCE, FOUND THAT THE NR 4 STARTER/GENERATOR COULD ROTATE 1/4 TURN ON IT'S MOUNT. THE SELF LOCKING NUT ON THE CLAMP HAD NO FRICTION AND BACKED OFF. THE CLAMP WAS LOOSE. THE STARTER HAD SHEARED THE ALIGNMENT PIN. WE REPLACED THE NUT, THE STARTER/GENERATOR AND THE MOUNT. 2H74 4T4 T A20EA E4EA 6 CP1NE 20010801000672001080100067 2001 8 1 CA010713011 420010704G2562MX1300 BATTERY DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN1 52008NE ELT WRONG PART W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING BATTERY DUE DATE INSPECTION IT WAS FOUND THAT THE ELT HAD INCORRECT BATTERIES INSTALLED. INSTALLED CORRECT BATTERIES. 1H71 3R3 R A806 5E1 20010801000772001080100077EU 2001 8 1 CA010723001 120010621G302021175789 COMPUTER HONEYWELL BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE ENGINE ANTI-ICE MALFUNCTIONED W O OTHER JW WARNING INDICATION INADEQUATE Q C ININSP/MAINT 1 CA 22539 45209 (CAN) DURING A MAINTENANCE ENGINE RUN, THE NR 1 ANTI-ICE VALVE CIRCUIT BREAKER POPPED AND WOULD NOT RESET. MAINTENANCE REPLACED THE JUST INSTALLED THRUST MODULATION SYSTEM (TMS) COMPUTER, AND THE PROBLEM WENT AWAY. APPARENTLY, A FAULT IN THE TMS COMPUTER BLEW THE CIRCUIT BREAKER IN THE OTHER SYSTEM. 2H74 4F4 FRTA49EU E6NE 20010725005602001072500560NM 2001 7 25 CA010723003 120010626G2910AN937D6 FITTING BOMBDR AN937D6 DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE FITTING CRACKED W O OTHER K FLUID LOSS ININSP/MAINT 1 CA (CAN) THE FLIGHT CREW REPORTED A FLUID LEAK FROM THE R/H WING ROOT DURING WALKAROUND. MAINTENANCE INVESTIGATION REVEALED A CRACKED HYDRAULIC "CROSS" FITTING, P/N AN 937 D6. THE FITTING WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010801000802001080100080NM 2001 8 1 CA010723004 120010704G2910DSX252B4012 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) THE FLIGHT CREW REPORTED FLUID LEAKING FROM THE NOSEGEAR AREA DURING WALK AROUND. MAINTENANCE INVESTIGATION REVEALED THAT THE HYDRAULIC FLEX LINE FOR THE NLG DRAG LINK ACTUATOR "UP" SELECTION WAS LEAKING AT THE AREA OF MAXIMUM FLEX, ADJUCENT TO THE FITTING. THE LINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010801000822001080100082NE 2001 8 1 CA010723041 220010714G7200 ENGINE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE NR 1 DAMAGED W E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DEDESCENT 1 CA (CAN) NR 1 ENGINE STALLED ON TOP OF DESCENT INTO YYZ DURING DECELERATION, ENGINE WAS SHUT DOWN. STALL INSPECTION, ENGINE BOROSCOPE DISCOVERED THAT 1 HP COMPRESSOR BLADE BROKEN OFF AND DAMAGED REMAINING HP COMPRESSOR. 2L73 4F4 F A23WE E12EU 20010801001102001080100110EU 2001 8 1 CA010723043 120010716G2824 VALVE AIRBUS310 A310 EU GE CF6 CF680C2A5 NE FUEL TRANSFER FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ETOP REQUIRED REPORTING. AIRCRAFT COULD NOT TRANSFER ALL THE FUEL FROM CENTER TANK. FQIS RESET AND BITE CHECKED SERVICEABLE. THIS IS A RECURRING DEFECT WHERE THE FQIS IS REST AND THE DEFECT RETURND A COUPLE OF FLIGHTS LATER ADDITIONAL TROUBLE SHOOTING REQUIRED. 2L72 4F4 FRTA35EU E13NE 20010809001012001080900101NE 2001 8 9 CA010724004 220010708G72604002TO2P03 BEARING SKRSKYS61 S61N 8142104NE GE CT58 CT581401 30011NE ACCESSORY DRIVE MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 265 (CAN) INVESTIGATION OF A CHIP LIGHT ON FORWARD CHIP PLUG SHOULD A BUILD UP OF BLACK FUZZY PASTE WITH SOME INDICATION OF FERROUS MATERIAL. ENGINE WAS REMOVED AND DISASSEMBLED. SUBSTANCIAL WEAR WAS FOUND ON ACCESSORY DRIVE GEAR BOX IMPUT PISTON BEARINGS. PARTS WERE ROUTED TO LAB FOR FURTHER INVESTIGATION. 2G72 4U4 U 1H15 1E3 20010809001032001080900103NE 2001 8 9 CA010724008 220010705G7210214040214001 LINER BELL 212040005005BELL 214 214B1 1182105SW LYC T55 T5508D 41555NE GEARBOX UNSERVICEABLE W A UNSCHED LANDING J WARNING INDICATION HOHOVERING 1 CA 7151 1476 AMG28031 (CAN) AFTER RECEIVING CHIP IND. FROM REDUCTION GEARBOX FILTER REMVD FOR INSP. OIL IN FILTER & BOWL FOUND TO BE BLACK WITH FERROUS MATERIAL PRESENT. REDUCTION GEARBOX THEN REMOVED & INIT INSP REVEALED THAT GEARBOX INPUT GEAR NUT P/N 214-040-236-001 HAD LOST TORQUE & BACKED OFF OF IMPUT GEAR&INTO SIX ENGINE OUTPUT SHAFT SEAL HOUSING BOLTS P/N MS9566-12. BOTH INPUT GEAR NUT & SIX SEAL HOUSING BOLTS WERE FOUND TO BE SCRAP. IT WAS NOTED THAT APPROX ONE HR EARLIER REDUCTION GEARBOX REMVD TO FACILITATE REPL OF ENGINE OUTPUT SHAFT SEAL HOUSING RE-SHIMMED TO ACCOMMODATE NEW OUTPUT SHAFT (PART OF TORQUE KIT). 2G71 4U4 U H6SW E4NE 20010809001092001080900109NE 2001 8 9 CA010724009 220010716G8530399356 ROCKER BOSS AIRTRCAT400 AT401B 0370207SW PWA R1340 R1340AN1 52016NE HAMSTD23D 23D40 NE EXHAUST VALVE CRACKED W A UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 CA 538 (CAN) THE EXHAUST VALVE ROCKER ARM BOSS CRACKED THROUGH THE PIVOT BOLT HOLES WHICH ALLOWED THE ROCKER ARM TO MOVE WITHOUT OPENING THE EXHAUST VALVE, SEVERLY REDUCING ENGINE POWER. FROM DISCUSSIONS WITH SEVERAL AME'S THE CONSENSUS IS THAT OVERTORQUING OF THE PIVOT BOLT, AT SOME TIME IN THE PAST, COULD CAUSE FATIQUE IN THIS AREA. THIS CYLINDER HAS HAD NO REPAIRS SINCE LAST OVERHAUL. 1L71 3R3 RNCA17SW 5E2 6 CP719 20010809001112001080900111 2001 8 9 CA010724011 420010710G611305503671 SPINNER CESSNA172 172L 2072432CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160DTM GL PROPELLER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9127 (CAN) CRACK IN PROPELLER CUTOUT OPENING IN SPINNER NOTED DURING PREFLIGHT INSPECTION. AIRCRAFT WAS GROUNED FOR REPAIRS. 1H71 3O3 ONT3A12 E274 5 NP910 20010809001122001080900112SW 2001 8 9 CA010724012 120010712G5320206031200118 STRAP BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE INSTALLING ELECTRICAL EQUIPMENT, A CRACK WAS FOUND ON THE AFT OUTBOARD RADIUS, STATION 100.8. THE CRACK STARTED FROM THE EDGE OF THE STRAP AT A TOOLING MARK MADE EITHER DURING MANUFACTURE OR PREVIOUS INSTALLATION. THE CRACK IS APPROXIMATELY 2 1/2 INCHS LONG, MOVING FORWARD AND OUTBOARD. THE STRAP WAS REPLACED. 1G71 3U3 U H2SW E4CE 20010809001142001080900114SW 2001 8 9 CA010724015 120010708G6220 BEARING BELL 205 205A1 1181414SW LYC T53 T5313B 41549NE M/R ROD END WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE PERFORMING REGULAR MAINTENANCE (DAILY INSPECTION) EXCESSIVE PLAY WAS OBSERVED IN THE M/R DAMPER RODEND ON ONE OF THE DAMPER ASSEBLIES. FURTHER INVESTIGATION REVEALED THAT THE TEFLON LINER (APPROX. 50%) WAS EXTRUDING FROM THE BEARING. THE BEARING WAS REPLACED AND THE A/C RETURNED TO SERVICE. 1G71 4U4 U H1SW E17EA 20010809001162001080900116CE 2001 8 9 CA010724023 120010710G2720 ARM CESSNA188 A188 2073004CE CONT O520 IO520D 17032SO MCAULY2A34C D2A34C98 GL RUDDER BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 4200 (CAN) RUDDER PEDAL PEDASTAL BROKEN ON LANDING. FOUND THE PEDAL ARM BROKEN DUE TO CORROSION 1L71 3O3 O A9CE E5CE 5 CP3EA 20010809001182001080900118NM 2001 8 9 CA010724026 120010714G324626045641 WHEEL BOEING727 727260 NM PWA JT8 JT8D17 52049NE MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 59 (CAN) DURING SERVICE CHECK, NR 1 MAIN WHEEL TIRE PRESSURE FOUND TO BE 40 PSI PRESSURE DETECTED TO BE LEAKING AT WHEEL HUB. NR 1 AND 2 MAIN WHEEL ASSEMBLIES REPLACED, NO FURTHER FAULTS AFTER 8 FLIGHT SEGMENTS. 2L73 4F4 FRTA3WE E2EA 20010809001202001080900120NM 2001 8 9 CA010724027 120010718G324426045611 TIRE BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE MAIN WHEEL ASSY FLAT W K NONE O OTHER ININSP/MAINT 1 CA 366 (CAN) NR 3 MAIN WHEEL TIRE FOUND FLAT ON WALKAROUND INSPECTION. MAIN WHEEL REPLACED. NO FURTHER FAULTS ON NEXT FIVE FLIGHT SEGMENTS. 2L73 4F4 F A3WE E2EA 20010809001212001080900121SW 2001 8 9 CA010724031 120010607G5302206032400027 BULKHEAD BELL 206031004FM BELL 206 206L 1181522SW ALLSN 25OC 250C20R GL TAIL BOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 13108 AOKP00649 (CAN) THE TAIL BOOM WAS REMOVED FOR 1200 HOUR INSPECTION. CRACKS WERE FOUND AROUND THE TOP LEFT ATTACH BOLT HOLE SHIM PART 206-032-400-117, WHEN THE BULK HEAD WAS REMOVED CRACKS WERE FOUND ALONG THE TOP EDGE OF THE MATING SURFACE OF THE BULK HEAD AND BOLT ATTACH FITTING PART 206-032-409-001 AND THE RADIUS WHERE THE BULK HEAD ATTACHED TO THE SKIN. THE BULK HEAD WAS REPLACED WITH NEW BELL HELICOPTER PART AS PER THE STRUCTURAL REPAIR MANUAL. 1G71 3U3 U H2SW E4CE 20010809001232001080900123SW 2001 8 9 CA010724032 120010607G5340206030111003 FITTING BELL 206 206L 1181522SW ALLSN 25OC 250C20R GL FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 13109 (CAN) THE FITTING WAS FOUND CORRODED ON 1200 HOUR INSPECTION AND NEW PART 206-033-173-001 WAS INSTALLED. THE ORIGINAL PART IS MANUFACTURED FROM MAGNESIUM WHERE THE NEW PART IS ALUMINUM SO AFTER 13109 OF FLYING ON A AIRCRAFT MANUFACTURED IN 1978 THIS WOULD NOT BE UNUSUAL. WE SHOULD GET MUCH BETTER SERVICE FROM THE ALUMINUM FITTING. 1G71 3U3 U H2SW E4CE 20010809001252001080900125SW 2001 8 9 CA010724033 120010523G214046D36 SWITCH BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL HEATER CONTROL MISSING W O OTHER O OTHER CRCRUISE 1 CA (CAN) WHILE IN CRUISE FLIGHT ALL EXPERIENCED A NO HEAT CONDITION. ON INSPECTION, FOR SWITCH WAS REMOVED AND RUDDER PAD ON THE END OF THE PLUNGER WAS FANNED DEBONDED & LODGED IN ORIFICE CAUSING HEATER NOT TO WORK. 1G71 3U3 U H2SW E1GL 20010809001262001080900126WP 2001 8 9 CA010724034 120010710G6410269A603523 BLADE HUGHES269 269C 4470504WP LYC O360 HIO360D1A 41514EA TAIL ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 3380 (CAN) ON DAILY INSPECTION OUTBOARD PART OF BLADE SKIN WAS FOUND TO BE CRACKED. CRACK IS FORMED AROUND TIP BLOCK ON BLADE. THE CRACK IS APPROX. 3 INCHES LONG, STARTING FROM BEHIND ABRASION STRIP TO ABOUT MIDDLE OF BLADE. 1G71 3O3 O 4H12 1E10 20010809001272001080900127WP 2001 8 9 CA010724035 120010710G6410269A603523 BLADE HUGHES269 269C 4470504WP LYC O360 HIO360D1A 41514EA TAIL ROTOR DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA 2890 (CAN) ON INSPECTION OF OPPOSITE TAIL ROTOR BLADE, THIS TAIL ROTOR BLADE WAS FOUND TO HAVE NO ABRAISON STRIP ON LEADING EDGE OF BLADE. FURTHER INSPECTION REVEALED THAT FILLER WAS USED UNDER PAINT TO BUILD UP EDGE. BOTH BLADES WERE REMOVED AND SENT TO SCHWEIZER A/C CORP FOR FURTHER INVESTIGATION. 1G71 3O3 O 4H12 1E10 20010809001292001080900129SW 2001 8 9 CA010724036 120010709G6510206040272101 SEAL BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL T/R DRIVE SHAFT DAMAGED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) ON PRE-FLIGHT INSPECTION, GREASE LEAKAGE ON FORWARD COUPLING ON INPUT DRIVESHAFT WAS NOTED. FURTHER INSPECTION REVEALED THATTHE FORWARD SEAL ASSY HAD FAILED AND ALL THE GREASE IN THE FORWARD COUPLING WAS THROWN OUT WHICH CAUSED AN OVERHEAT CONDITION. A MORE DETAILED PRE-FLIGHT INSPECTION OF FORWARD AND AFT SEAL ASSEMBLIES FOR RIPS, TEARS AND GREASE LEAKAGE WILL HELP PREVENT AN OVERHEAT CONDITION OR TOTAL DRIVESHAFT FAILURE 1G71 3U3 U H2SW E4CE 20010809001302001080900130CE 2001 8 9 CA010725005 120010705G554004331401 RUDDER HORN CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA MCAULY1A103 1A103TCM GL VERITICAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) UPON COMPLYING WITH AD CF-2000-20 RE. RUDDER INSPECTION, FOUND LOWER RIB P/N 0431004-24 CRACKED. LEVER RUDDER FAIRING HAD TO BE REMOVED IN ORDER TO REPAIR RIB. UPON FAIRING REMOVAL, FOUND RUDDER HORN CRACKED IN TWO PLACES AT RADIUS. I FEEL THIS DAMAGE WAS CAUSED FRIN WIND DAMAGE AND NO RUDDER LOCK INSTALLED. 1H71 3O3 ONT3A19 E223 5 NP50GL 20010809001372001080900137SW 2001 8 9 CA010725006 120010621G30208943822 TUBE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP MCAULY4HFR344HFR34C652 NE ANTI-ICE SYS CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING ENGINE CHANGE EGT AND FF WERE HIGH AND RIGGING WAS DIFFICULT. BLEED AIR LEAK WAS FOUND AND THE LINE REPLACED. ENGINE PARAMETERS WERE NOW NORMAL AND RIGGING WAS ACCOMPLISHED. THE CRACKED TUBE ALSO CAUSED THE ENGINE COWL TO HEAT UP, POSSIBLE FIRE CONSIDERATION. 2L72 4T4 TRTA8SW E4WE 6 C3PNE 20010809001382001080900138NE 2001 8 9 CA010725007 320010710G611178030S0CN8173881SEAL CNDAIRCL215 CL2156B11415 EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE PROP SEAL BROKEN W K NONE K FLUID LOSS ININSP/MAINT 1 CA 4 4 (CAN) THE PROPELLER BLADE SEAL HAD SPRING INSIDE OF IT AND THE TWO ENDS ARE WELDED TOGETHER BY THE MANUFACTURE. THE SPRING BROKE AT THE WELDED JOINT CAUSING OIL TO LEAK OUT OF THE HUB AT THE BLADE ROOT. IT WAS NOTICED DURING A D.I AFTER THE FLIGHT. THE SEAL AND SPRING ASSY WAS REPLACED AND THE A/C RETURNED TO SERVICE. 2H72 4T4 TRTA14EA E20NE 6 CP7NE 20010809001622001080900162EU 2001 8 9 CA010725008 120010717G29109603001261 SELECTOR VALVE PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL HYD SYSTEM LEAKING W O OTHER J WARNING INDICATION LDLANDING 1 CA 1713 HG40288 (CAN) PILOTS REPORTED A INTERMITTENT PROBLEM WITH THE HYDRAULIC LIGHT COMING ON WHEN LANDING. THIS INDICATES THE HYDRAULIC PUMP CYCLED 6 TIMES IN 1 HOUR. AFTER SERVICING THE SYSTEM THE PROBLEM WOULD STILL OCCUR. IT WAS DECIDED TO CHANGE THE HYDRAULIC SERVICE SELECTOR VALVE. THE PROBLEM DID NOT RETURN AFTER THIS. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010809001642001080900164EU 2001 8 9 CA010725010 120010719G28229688411404 PUMP PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL FUEL BOOST UNSERVICEABLE W O OTHER J WARNING INDICATION DEDESCENT 1 CA 1458 1458 (CAN) BOOST PUMP FAILED CAUSING FUEL IMBALANCE. AIRCRAFT LANDED AND PUMP REPLACED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010809001702001080900170EU 2001 8 9 CA010725013 120010710G27529787320001 DRIVE GEAR PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA 2126 (CAN) PILOTS REPORTED FLAP SYSTEM 1 AMP CIRCUIT BREAKER ON BATTERY BUS TRIPPED WHEN FLAP SELECTED DOWN. THE SYSTEM WOULD FUNCTION NORMAL IF THEY KEPT THE AIR SPEED BELOW 140 KNOTS. THE FAILURE COULD NOT BE DUPLICATED ON THE GROUND. THE FLAP POWER DRIVE UNIT WAS REPLACED. THE AIRCRAFT WAS FLOWN AND FLAPS EXTENDED AT MAX EXTENSION SPEED AND SYSTEM FUNTIONED NORMAL. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010809001712001080900171EU 2001 8 9 CA010725014 120010710G25109593001216 SEAT BACK PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL COCKPIT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2135 (CAN) THE SEAT WAS REMOVED TO REPAIR BROKEN UP/DOWN ADJUSTMENT AND THE SEAT BACK WAS FOUND CRACKED. THE CRACKS WERE FOUND TO BE ONLY IN THE PLASTIC PART OF THE ALUMINUM STRAPS WERE NOT CRACKED, THE PART WAS REPLACED WITH A NEW UNIT. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010809001722001080900172EA 2001 8 9 CA010725019 120010705G7120 MOUNT CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING SUPPORT BEAM INSPECTION, AS PER SB601R-53-059, CRACKS WERE FOUND AT BL0 AND LBL36. 2L72 4F4 FRTA21EA E15NE 20010809001732001080900173EU 2001 8 9 CA010725020 120010704G6720 LINER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE T/R BEARING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE BEARING LINER WAS FOUND CRACKED IN BOTH TAIL ROTOR PITCH LINKS. THE SAME PROBLEM HAS BEEN REPORTED IN THE PAST. 1G71 3U3 UNCH9EU E19EU 20010809001752001080900175SW 2001 8 9 CA010725021 120010703G2550204075157001 SLIP RING BELL 212 212 1181420SW PWA PT6T PT6T3B 52045NE CARGO HOOK DEBONDED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) PILOT REPORTED PROBLEMS WITH ELECTRICAL RELEASE ON CARGO HOOK ASSEMBLY. SUSPENSION ASSEMBLY LATER DISASSEMBLED AND FOUND THAT INNER RING ON SLIP RING ASSEMBLY HAD DISBONDED PREVENTING PROPER CONTACT. THE SLIP RING ASSEMBLY WAS REPLACED WITH NEW PART AND UNIT REASSEMBLED. THE SUSPENSION ASSEMBLY WAS REINSTALLED IN THE AIRCRAFT AND SYSTEMCHECKED SERVICEABLE. THE SLIP RING ASSEMBLY ( THAT IS; DEBONDING AND PITTING) IS A COMMON SOURCE OF PROBLEMS WITH THE SUSPENSION ASSEMBLY. 1G71 4U4 U H4SW E22EA 20010809001782001080900178SW 2001 8 9 CA010725022 120010703G7500 ARM BELL 206 206L 1181522SW ALLSN 250C 250C20R2 GL ACTUATOR DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FOUND NUT OF ACTUATOR ARM LOOSE IN ARM. UNIT REPLACED AND AIRCRAFT RETURNED TO SERVICE AFTER ADJUSTMENTS. 1G71 3U3 U H2SW E4CE 20010809001792001080900179SW 2001 8 9 CA010725023 120010703G5302206031329003 FITTING BELL 206 206L 1181522SW ALLSN 250C 250C20R2 GL TAIL BOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE FITTING HAD TO BE REPLACED DUE TO CRACK. IT APPEARS TO HAVE CRACKED DUE TO INCORRECT INSTALLATION. THERE WAS A 100 INCH GAP BETWEEN THE LONGERON AND THE FITTING AND THIS PLACED THE FITTING UNDER STRESS. THE FITTING WAS REPLACED BY A NEW PART WITH CARE TAKEN TO ENSURE NO GAP WAS PRESENT ON THE NEW PART INSTALLATION. 1G71 3U3 U H2SW E4CE 20010809001812001080900181EU 2001 8 9 CA010725024 120010704G6710350A371508 ROD END SNIAS 350 AS350D 8680803EU LYC LTS101LTS101600A2 41560NE MAIN ROTOR SEPARATED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING POST FLIGHT INSPECTION OF AIRCRAFT IT WAS NOTICED THAT THE MAIN ROTOR PITCH LINK ROD AND RETAINER HAD SEPARATED FROM ROD END. PILOT CONFIRMED THAT ON PREVIOUS FLIGHT HE HAD STARTED TO EXPERIENCE A MAIN ROTOR VIBRATION. MAIN ROTOR AND SWASHPLATE ASSEMBLIES INSPECTED BY MAINTENANCE. NO OTHER DAMAGE FOUND. THE MAIN AIRCRAFT WAS FLIGHT TESTED AND RETURNED TO SERVICE. 1G71 3U3 U H9EU E5NE 20010809001832001080900183NE 2001 8 9 CA010725026 220010626G851016475 CASE DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE ENGINE LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA 562 (CAN) SMALL OIL LEAK ON NOSE SECTION. REMOVED NOSE SECTION AND DISCOVERED CRACK RADIATING FROM BOLT HOLE IN BEARING BORE OF FRONT ENGINE CASE. REMOVED ENGINE FOR REPLACEMENT. 1H71 3R3 R A806 5E1 20010809001842001080900184SW 2001 8 9 CA010725031 120010703G2810206063688001 HOSE 206063600 BELL 206 206L 1181522SW ALLSN 250C 250C20R2 GL FUEL SYSTEM LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) DURING REFUELING OPERATION, FUEL WAS OBSERVED LEAKING FROM TANK VENT HOSE ASSEMBLY WHEN TANK WAS FILLED TO CAPACITY. HOSE APPEARS TO HAVE DETERIORATED WITH AGE ALLOWING FUEL TO LEAK. DUE TO THIS DEFECT ANOTHER AIRCRAFT WAS VERIFIED BY PRESSURE TESTING THE VENT HOSE ASSEMBLY. IT WAS ALSO FOUND TO BE LEAKING. BOTH AIRCRAFT HOSES WERE REPLACED AND SYSTEMS CHECKED SERVICEABLE. MANUFACTURER OF AIRCRAFT CURRENTLY DOES NOT HAVE A RETIREMENT OR TEST SCHEDULE FOR THESE FLEXIBLE HOSES. 1G71 3U3 U H2SW E4CE 20010809001912001080900191NE 2001 8 9 CA010725032 120010705G32317625100702043 LINK SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MLG DOOR SHEARED W O OTHER J WARNING INDICATION LDLANDING 1 CA 1882 (CAN) DURING MAIN LANDING GEAR RETRACTION AND EXTENSION PILOTS NOTED A SLIGHT YAW. THEY ASSUMED IT TO BE CASUED BY DIFFERNECE IN RETRACTION RATES OF LANDING GEAR. UPON LANDING AT BASE, THE ENGINEER NOTED THAT THE GEAR DOOR WAS LOWER THAN THE RIGHT. INVESTIGATION REVEALED THAT THE LANDING GEAR DOOR LINK WAS REPLACED WITH A NEW ONE AND THE SYSTEM WAS FUNCTION CHECKED SERVICEABLE. AIRCRAFT RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20010809001962001080900196NE 2001 8 9 CA010725033 120010705G29107665103004041 TUBE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL HYD SYSTEM LEAKING W H DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) APPROX. 10 MINS AFTER TAKEOFF UNUSUAL LOW WHISTLING SOUND NOTICED BY ONE OF PILOTS, FOLLOWED SHORTLY THEREAFTER BY NR 2 SERVO WARMING LIGHT ILLUMINATING & NR 2 HYDRAULIC PRESSURE CYCLING BETWEEN 1000 & 3000PSI. SWITCHED OFF #2 SERVO SWITCH AT WHICH TIME HYDRAULIC PRESSURE IND. RETURNED TO NORMAL (INDICATIVE OF LEAK AFT OF SERVO SHUTOFF VALVE. EMERG CHECKLIST FOR "LOSS OF HYD. PRESSURE" PREFORMED. PILOTS REVERSED COURSE&CARRIED OUT PRECAUTIONARY LDG W/O INCID.. POST FLT INSP REVEALED FLUID LEAKING OUT OF BELLY AREA AFT OF BAGGAGE COMPT & NR 2 HYDRAULIC RESERVOIR BELOW MIN.LEVEL. MAINT INVEST. FOUND FLUID LEAK FROM PINHOLE IN NR 2 TAIL ROTORPRESSURE TUBE. TUBE REPL ALONG WITH HYDRAULIC PUMP DUE TO 1G72 3U3 U H1NE E1GL 20010809001992001080900199EA 2001 8 9 CA010726001 120010715G712060135006 MOUNT CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE ENGINE CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA 19370 (CAN) DURING AN OPPORTUNITY INSPECTION OF THE ENGINE BEAM, CRACKS WERE FOUND ON THE CENTER SECTION. (REF ASB 601R-53-069.) 2L72 4F4 FRTA21EA E15NE 20010809002002001080900200EA 2001 8 9 CA010726006 120010705G7120 MOUNT CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING AN OPPORTUNITY INSPECTION OF THE ENGINE SUPPORT BEAM, CRACKS WERE FOUND ON THE CENTER SECTION. SEE ASB 2L72 4F4 FRTA21EA E15NE 20010809002062001080900206EU 2001 8 9 CA010726008 120010703G6220350A37116200 YOKE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE MAIN ROTOR BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ONE OF THE THREE DROOP RESTRAINT STOP YOKES WERE FOUND BROKEN IN TWO PIECES. MAIN ROTOR HEAD AND BLADES INSPECTED AND NO ADDITIONAL DAMAGE FOUND. YOKE REPLACED. 1G71 3U3 UNCH9EU E19EU 20010809002072001080900207NE 2001 8 9 CA010726012 120010705G32007655200904046 HARNESS SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MLG BROKEN W O OTHER D INFLIGHT SEPARATION CRCRUISE 1 CA (CAN) DURING CRUISE, RED LANDING GEAR UNSAFE LIGHT FLICKERING INTERNITTENTLY WITH A CORRESPONDING "CLUNKING" IN THE AIRFRAME FELT THROUGH THE COLLECTIVE STICK. UPON RETURN FROM FLIGHT MAINTENACE PUT AIRCRAFT ON JACKS AND THE LANDING GEARWAS OPERATED TO SIMULATE THE CONDITION. THE FAULT WAS TRACED TO THE LEFT MAIN DOWN LOCK WIRING HARNESS. THE HARNESS WAS REPLACED WITH A NEW ONE. THE SYSTEM WAS FUNCTION TESTED SERVICEABLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20010809002132001080900213CE 2001 8 9 CA010726014 120010620G7603K30B22HT WIRE GARRTT TFE73122B LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE73122B 01518WP ENGINE FAILED W C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 CA P74114C (CAN) ON TAKE OFF ROLL, ENGINE SLUGGISH, R/H FUEL COMPUTER LIGHT ON (COMPUTER KICKED OFF), ABORT TAKEOFF, CAME BACK TO MAINTENACE HANGAR (MAIN BASE). N2 MONOPOLE FAULT APPEARS, CODE 14 ON DITAL ENGINE COMPUTER DOWNLOAD. WIRE K30B22HT SUSPECTED TO CAUSE THE FAULT BETWEEN CONNECTORS P360 & P358. WIRE REPLACED WITH NEW ONE. GROUND RUN CARRIED OUT. HIGH SPEED TAXIING CARRIED OUT. NO MORE FAULT FOUND. A/C RETURNED TO SERVICE. 2L72 4F4 F A10CE E6WE 20010809002172001080900217WP 2001 8 9 CA010726024 120010606G6310369D25351 SPRAG CLUTCH HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL TRANSMISSION BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 392 (CAN) O/R CLUTCH ASSY WAS REMOVED FOR O/H. UPON O/H INSPECTION IT WAS FOUND THAT THE SPRAG ASSY HAD ONE BROKENSPRAG. THE BROKEN PIECE WAS RECOVERED FROM INSIDE THE ASSEMBLY. 1G71 3U3 U H3WE E4CE 20010809002182001080900218 2001 8 9 CA010726025 420010726G3457114DD26 RELAY CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL GPS UNSERVICEABLE W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 CA (CAN) HSI LT/RT DEVIATION REAMINS CENTERED WHEN GPS IS SELECTED WITH NO FAILURE WARNING/INDICATION GPS LAMP REMAINED ON, GPS & TO FROM FLAGS REMAINED VALID). RELAY K2 IN AVIONICS J-BOX #1 FAILED TO ENERGIZE WHEN GPS WAS SELECTED. REPLACED K2. NOTE: TC ENGINEERING REQUIRES THAT THE GPS LAMP BE INTERLOCKED THROUGH ALL RELAYS. IF A SINGLE RELAY WERE TO FAIL, THE GPS LAMP WOULD EXTINGUISH. TH 208/B SWITCHING SYSTEM WAS APPROVED IN THE USA WITHOUT SUCH INTERLOCKS. HSI (GS) VERTICAL DEVIATION POINTER IS DRIVEN DURING GPS SELF TEST. FOUND GPS VERTICAL DEVIATION WIRES CONNECTED TO CESSNA J-BOX. CAPPED AND STOWED GPS VERTICAL DEVIATION WIRES AT AVIONICS J-BOX #2. 1H71 3T3 T A37CE E4EA 5 CP60GL 20010809002192001080900219EU 2001 8 9 CA010726026 120010724G34110851HL PROBE AIRBUS330 A330322 3930325EU PWA 4168 PW4168 NE PITOT SYSTEM BLOCKED W C ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CA (CAN) A/C ARRIVED WITH CAPTS. AIRSPEED READING INCORRECTLY. MTCE SWAPPED ADIRU #1 INTO #3 POSITION TO DEFER WITH LEAST AMOUNT OF IMPACT. A/C DEPARTED AND REJECTED T/O. ADM WAS OBTAINED FROM AIR CANADA AND INSTALLED IN A/C SSV. AVIONICS WAS CALLED IN TO C/O PITOT STATIC CHECK. FAULT STILL PRESENT. PITOT LINE REMOVED BETWEEN CAPT. PITOT PROBES AND ADM AND FOUND BLOCKED. DEBRIS REMOVED FROM LINE AND PROBE SYST. TESTED SERVICEABLE WITH PITOT STATIC TEST SET. A/C DECLARED SERVICEABLE 7:30 HOURS. 2L72 4F4 FRTA46NM E36NE 20010809002212001080900221SW 2001 8 9 CA010726027 120010726G6510407340339103 BEARING 4070403031 BELL 407 407 SW ALLSN 250C 250C47B GL FAN SHAFT NOISY W K NONE O OTHER ININSP/MAINT 1 CA 1256 (CAN) AFTER NORMAL UNEVENTFUL FLT, PILOT SHUTDOWN A/C&NOTICED NOISE COMING FROM TAIL ROTOR DRIVE TRAINN DURING COAST DOWN. SUBSEQUENT INSP REVEALED THATT HE GREASE EMANATING FROM AFT FAN SHAFT BEARING BLACK WITH METALLICPARTICLES, BEARING ROUGH WHEN ROTATED USING DRIVE TRAIN BY HAND&MORE PLAY IN BEARING THAN IS NORMALLY FELT WHEN LOADED IN LATERAL&FORE&AFT DIRECTION BY HAND. NO ANCILLARY DAMAGE. BEARING WS REPL WITH NEW BEFOREFURTHER FLT. HAVE BEEN OTHER FAILURES OF TYPE ON BELL 407 RESULTING IN TC AD CF-2000-02 REQ 25 HR INSP&LUBE OF THESE BEARINGS. PLEASE NOTE THAT BEARING FAILED 13.7 HRS AFTER SUCH INSP.THE INSP AT THAT TIME DID NOT REVEAL ANY PAR 1G71 3U3 UO H2SW E1GL 20010809002222001080900222SW 2001 8 9 CA010726028 120010724G6510407340339103 BEARING 407040303101BELL 407 407 SW ALLSN 250C 250C47B GL FAN SHAFT DISINTEGRATED W A UNSCHED LANDING O OTHER CLCLIMB 1 CA 1233 (CAN) SHORTLY AFTER TAKEOFF, ABOUT 400 FT ABOVE GROUND, A/C SOUND & VIBRATION LEVELS SUDDENLY CHANGED FROM NORMAL TO HEAVY VIBRATION THROUGHOUT WHOLE A/C WITH OSCILLATING, DRONING NOSIE. AS WELL, PILOT NOTICED PULSING FEEDBACK SE NSATION FROM ANTITORQUE PEDALS. PILOT IMMEDIATELY ABORTED CLIMB&CARRIED OUT PRECAUTIONARY DESCENT&NORMAL LDG W/O INCID.. TAIL ROTOR CNTL AUTH NEVER LOST. AFTER ENGINE SHUTDOWN, INSP REVEALED COMPLETELY FAILED FWD FAN SHAFT BEARING WITH DISINTIGRATED BEARING CAGES & BALLS EJECTED INTO IMPELLER. ANCILLARY DAMAGE TO IMPELLER, SHAFT&OIL COOLER BLOWER HOUSING. THER HAVE BEEN OTHER FAILURES OF TYPE ON BELL 407 RES ULTING IN TC AD CF-2000-02 REQ 1G71 3U3 UO H2SW E1GL 20010809002232001080900223EU 2001 8 9 CA010726034 120010725G6520350A33212900 PLATE 350A33200403SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR WORN W K NONE O OTHER ININSP/MAINT 1 CA 428 V231292 (CAN) BLACK PAINT INDEX MARKS MISALIGNED AND OUTBAOARD SPACER FREE TO ROTAT. UNIT IS POST MOD 07-6554 PART 2.B.3 AND POST MOD 07-6551. RECEIVED IN SHOP, DOUBLE LOCKING OF NUT VERIFIED ALL VISIBLE ELEMENTS INBOARD OF BEARING FELT TIGHT AND SECURE, NUT UNLOCKED AND TORQUE APPLIED. NUT ROTATED 30 DEGREES PRIOR TO ACHIEVING MINIMUM TORQUE LOAD. UNIT DISASSEMBLED, ALL SPACERS AND BEARING INNER RACE EXHIBITED SIGNS OF ROTATION. BEARING INNER RACE HAS WORN THROUGH THE D148 VARISH AND INTO PARENT MATERIAL OF ROTATING PLATE (350A33-2129-00). 1G71 3U3 UNCH9EU E19EU 20010809002242001080900224EU 2001 8 9 CA010726035 120010725G2400350A61131201 CIRCUIT BOARD SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BUCKET RELEASE CORRODED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) UNABLE TO PERFORM WATER BUCKET OPERATIONS (FIRE SUPPRESSION) DUE TO ELECTRICAL DEFECT. TROUBLESHOOTING CARRIED OUT ON SYSTEM AND PRINTED CIRCUIT BOARD 25 IDENTIFIED AS CAUSE DUE TO HAEAVY CORROSION ON CONTACT POINTS OF BOARD. BOARD WAS REPLACED WITH NEW UNIT AND SYSTEM CHECKED SERVICEABLE. THIS BOARD ALSO CONTROLS OTHER AIRCRAFT SYSTEMS SUCH AS COMMUNICATIONS, CARGO HOOK OPERATIONS, ETC. IT IS CURRENTLY NOT PART OF THE MANUFACTURE'S INSPECTION PROGRAM AS A POINT OF INSPECTION. 1G71 3U3 UNCH9EU E19EU 20010809002262001080900226NM 2001 8 9 CA010726036 120010716G2720401602728A COMPUTER BOEING727 727172C 1384058NM PWA JT8 JT8D7B 52053NE FEEL SYSTEM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) POST INSTALLATION DURING FUNCTIONAL TEST THE UNIT DISCOVERED TO BE LEAKING. AFTER REMOVAL OF THE FEEL COMPUTER IT WAS NOTICED THAT A CRACK APPROX. 3 INCHES IN LENGTH WAS WMITTING FROM THE ACTUATOR MOUNTING COVER. THE CRACK ITSELF IS LOCATED ON THE CHAMBER. THIS UNIT WAS RECENTLY OVERHAULED BY AVBORNE ACCESSORY GROUP INC. 2L73 4F4 F A3WE E2EA 20010809002272001080900227WP 2001 8 9 CA010726038 120010630G79206843698 INSULATOR ALLSN 501D13D CVAC 440 440 2422902WP ALLSN 501D 501D13D 03004GL INSULATOR DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA 705276 (CAN) FOUND INSULATOR MISSING ON SERVICE CHECK NEW PART INSTALLED. NO OTHER PROBLEM FOUND AND A/C RETURNED TO SERVICE. LT ENGINE REAR SCAVENGE PUMP INSULATOR WAS MISSING IT HAD BEEN REPORTED BY GROUND PEOPLE THAT A PART FALL FROM AIRCRAFT ON APPRAOCH TO LAND IN WINNIPEG. NORMAL INSPECTION CALL TO VERIFY PRESENCE OF INSULATOR. 2L72 4R4 T 6A6 E282 20010809002282001080900228SW 2001 8 9 CA010727001 120010704G6510R34665 TURBINE 2040625401 BELL 205 205A1 1181414SW LYC T53 T5313B 41549NE COOLER BLOWER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9209 322 417 (CAN) VIBRATION ON BLOWER ASSY. EXAMINE BLOWER ASSY & FOUND TWO CRACKS ON THE ROOT OF TWO BLADE. 1G71 4U4 U H1SW E17EA 20010809002292001080900229EA 2001 8 9 CA010727008 120010607G6310269A55593 SHAFT 259A55593 SCWZER269 269D 8059501EA LYC O360 HIO360D1A 41514EA ENGINE ADAPTER BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 4138 5424 (CAN) BROKEN TEETH ON SHAFT ON ENGINE ADAPTER SIDE. REPLACE SHAFT. 1G71 3U3 O0 4H12 1E10 20010809002302001080900230EA 2001 8 9 CA010727009 120010707G6320CR3687 SEAL SCWZER269 269D 8059501EA LYC O360 HIO360D1A 41514EA MAIN ROTOR LEAKING W K NONE O OTHER ININSP/MAINT 1 CA (CAN) OIL SEAL LEAKING IN RPM CABLE. REPLACE OIL SEAL PN CR 3687. 1G71 3U3 O0 4H12 1E10 20010809002332001080900233EA 2001 8 9 CA010727010 120010607G6220269A1227817 BEARING SCWZER269 269D 8059501EA LYC O360 HIO360D1A 41514EA MAIN ROTOR WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) BEARING WORN INSIDE. REPLACE ALL 3 GRIP BEAR IN SET. 1G71 3U3 O0 4H12 1E10 20010809002342001080900234EA 2001 8 9 CA010727011 120010707G6220269A1231 BEARING 269A12215 SCWZER269 269D 8059501EA LYC O360 HIO360D1A 41514EA MAIN ROTOR RATCHETING W K NONE O OTHER ININSP/MAINT 1 CA (CAN) BEARING RACHET WHEN INSPECTION. REPLACE BEARING. 1G71 3U3 O0 4H12 1E10 20010809002352001080900235EA 2001 8 9 CA010727014 120010707G2140269A4799003 BRACKET 269A4799001 SCWZER269 269D 8059501EA LYC O360 HIO360D1A 41514EA HEATER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) BRACKET CRACK . REPLACE BRACKET. 1G71 3U3 O0 4H12 1E10 20010809002392001080900239SW 2001 8 9 CA010727015 120010607G5302206032400027 BULKHEAD 206032400177BELL 206 206L 1181522SW ALLSN 25OC 250C20R GL TAIL BOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 13108 AOKP00649 (CAN) THE TAIL BOOM WAS REMOVED FOR 1200 HOUR INSPECTION. CRACKS WERE FOUND AROUND THE TOP LEFT ATTACH BOLT HOLE SHIM PART # 206-032-400-117. WHEN THE BULKHEAD WAS REMOVED, CRACKS WERE FOUND ALONG THE TOP EDGE OF THE MATING SURFACE OF THE BULKHEAD AND BOLT ATTACHMENT FITTING #206-032-409-001, AND THE RADIUS WHERE THE BULKHEAD ATTACHES TO THE SKIN. THE BULKHEAD WAS REPLACED WITH NEW BHTC PART AS PER THE SRM. 1G71 3U3 U H2SW E4CE 20010809002412001080900241NM 2001 8 9 CA010727016 120010718G3244 TIRE BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE MLG FAILED W O OTHER O OTHER LDLANDING 1 CA (CAN) THE NR 1 TIRE THREAS SEPARATED FROM THE CARCASS DURING T/O ROTATION. DAMAGE ON EXTERIOR OF THE WING DOOR. THE NR 2 TIRE FAILED ON TAXI INTO RAMP IN YYC. 2L73 4F4 F A3WE E2EA 20010809002422001080900242GL 2001 8 9 CA010727017 220010720G7210 GEARBOX CVAC 340 340CVAC 242270AWP ALLSN 501D 501D22 03005GL ENGINE LEAKING W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CA (CAN) DURING CLIMB THROUGH FL170 AFTER DEPARTURE NOTICED NR 2 GEAR BOX OIL PRESSURE FLICKERING. OIL PRESSURE WAS STILL IN THE GREEN RANGE AND THE POWER SECTION OIL PRESSURE WAS NORMAL. ENGINE SHUT DOWN AND AIRCRAFT DIVERTED INTO YYZ. 2L72 4R4 T 6A6 E282 20010807002232001080700223NM 2001 8 7 CA010727020 120010718G2910271N61191 HYDRAULIC LINE 273N20025 BOEING757 75723A 1384967NM RROYCERB211 RB211535E43754555NE RUPTURED @ MIDPTLEAKING W D RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 CA (CAN) AIRCRAAFT RETURNED TO THE GATE, AFTER PUSH BACK, DUE TO A HYDRAULIC LEAK AT THE L/H MAIN LANDING GEAR DOWNLOCK ACTUATOR SUPPLY FLEX LINE. LINE WAS FOUND RUPTURED AT MID POINT. LINE WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA2NM E12EU 20010809002432001080900243NM 2001 8 9 CA010727023 120010727G2730 BUSHING 2827001011 BOEING767 767233 NM PWA JT9 JT9D7R4D 52054NE ACTUATOR LOOSE W O OTHER O OTHER CRCRUISE 1 CA (CAN) BUFFETING FELT THROUGH THE FLIGHT AND INCREASE IN FREQUENCY DURING CLIMB OUT. THE LEFT ELEVATOR WAS INDICATING LOWER THAN THE RIGHT AND WOULD FLUCTUATE UPWARD. INVESTIGATION REVEALED LEFT END OUTBOARD POWER ACTUATOR (P.C.A.) EYE END BUSHING LOOSE AND SUPPORT TRUNNION LOOSE. REPLACED ACTUATOR AND TRUNNION. 2L72 4F4 FRTA1NM E3NE 20010807002242001080700224WP 2001 8 7 CA010727026 120010711G27510070J TRANSMITTER DOUG DC9 DC932 3022066WP PWA JT8 JT8D7 52053NE TRANSMITTER FAILED W O OTHER O OTHER APAPPROACH 1 CA (CAN) STALL WARNING OCCURRED SEVERAL TIMES DURING APPROACH WITH SPEED ABOVE 220 KTS. REPLACED FLAP POSITION TRANSMITTER. 2L72 4F4 F A6WE E2EA 20010807002252001080700225NM 2001 8 7 CA010727027 120010705G29122705579 CLAMP BOEING737 737296 1384486NM PWA JT8 JT8D9A 52048NE CLAMP W D RETURN TO BLOCK K FLUID LOSS TOTAKEOFF 1 CA (CAN) HYDRAULIC LOSS OF SYSTEM A AFTER TAKE OFF, AIRCRAFT RETURNED. BROKEN CLAMP ON THE RETURN FILTER BOWL. NEW CLAMP INSTALLED, AND FILTER ELEMENT CHANGED. 2L72 4F4 FRTA16WE E2EA 20010807002262001080700226NM 2001 8 7 CA010727029 120010704G4910732138701 ACTUATOR 732138701 BOEING767 767233 NM PWA JT9 JT9D7R4D 52054NE ACTUATOR W K NONE O OTHER CRCRUISE 1 CA (CAN) BUFFETING FELT THROUGH THE FLIGHT AND INCREASED IN FREQUENCY DURING CLIMB OUT. FOUND TO BE THE APU DOOR ACTUATOR AT FAULT. HALF INCH PLAY IN ACTUATOR BEARING AND SEAL DAMAGE. REPLACED THE APU DOOR ACTUATOR. 2L72 4F4 FRTA1NM E3NE 20010809002442001080900244CE 2001 8 9 CA010727034 120010719G3310041312610 RHEOSTAT CESSNA172 172D 2072410CE CONT O300 O300D 17022SO COCKPIT FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CA (CAN) WHILE PERFORMING THE ANNUAL INSPECTION OF THE ELCTRICAL SYSTEM THE RHEOSTAT BEGAN SMOKING. 1H71 3O3 ONT3A12 E253 20010809002452001080900245NE 2001 8 9 CA010727035 220010727G7532 SWITCH 3192100 SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLEED VALVE FAILED W K NONE L NO TEST ININSP/MAINT 1 CA 2831 283 670 (CAN) LOST SIGNAL FROM BLEED VALVE WHICH WORKS CORRECTLY. FOUND SWITCH LEAF AND ROLLER WAS BROKEN. 1G71 3U3 UNCH9EU E19EU 20010809002462001080900246CE 2001 8 9 CA010727036 120010723G3230244110010 PIVOT CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 6300 (CAN) DURING INSPECTION CARRIED OUT IAW AD 2001-06-06, BOTH PIVOT ASSMEBLIES WERE FOUND CRACKED 1H71 3O3 O 3A17 E286 5 CP7EA 20010809002472001080900247CE 2001 8 9 CA010730001 120010723G323398820152 ACTUATOR CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL LANDING GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 6300 (CAN) DURING INSPECTION REQUIRED BY CESSNA SEB 01-2 BOTH ACTUATORS WERE FOUND CRACKED 1H71 3O3 O 3A17 E286 5 CP7EA 20010809002492001080900249CE 2001 8 9 CA010730002 120010723G323399820152 ACTUATOR CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL LANDING GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 8600 (CAN) DURING INSPECTION CARRIED OUT IAW CESSNA SEB01-2, BOTH LANDING GEAR ACTUATORS WERE FOUND CRACKED. 1H71 3O3 O 3A17 E286 5 CP7EA 20010823000872001082300087CE 2001 8 23 CA010808002 120010729G6310105199 CARBURETOR CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA ENGINE MALFUNCTIONED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA 650 (CAN) ENGINE STARTED LOSING POWER WHILE IN CRUISE AT 2500 FT & 30 SEC LATER QUIT RUNNING. PILOT INSTRUCTOR MADE A FORCED LANDING IN HAY FIELD. ENGINE WOULD NOT START AGAIN. CARBURATOR WAS REPLACED AND ENGINE STARTED TO RUN NORMALLY AND AIRCRAFT WAS FLOWN OFF FIELD. NOTE: LAST SUMMER A SIMILAR INCIDENT OCCURRED ON ANOTHER OF OUR C-152'S EXCEPT THAT THE ENGINE DID NOT QUIT COMPLETELY AND HE LANDED AT ON AIRPORT. 1H71 3O3 ONT3A19 E223 20010823000932001082300093SW 2001 8 23 CA010808003 120010706G63202060400321 BEARING 20604000005 BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL TRANSMISSION SPALLED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW99 7617 2233 B12150 (CAN) TRANSMISSON REMOVED FROM A/C DUE TO METAL CONTAMINATION AND EXCESSIVE NOISE. ON DISASSEMBLY, MAIN INPUT GEAR SHAFT P/N 206040040003 WAS FOUND TO HAVE VERTICAL PLAY. AFTER REMOVING THE SHAFT AND THE DUPLEX THRUST BEARING P/N 2060400321 THE TOP BEARING OF THE THRUST BEARING WAS FOUND TO BE BADLY SPALLED ON ALL THE BALLS. THE VERTICAL MOVEMENT OF THE SHAFT AND RING GEAR ALSO CAUSED EXCESSIVE WEAR OF THE PINON AND RING GEAR. 1G71 3U3 U H2SW E4CE 20010823000952001082300095NM 2001 8 23 CA010808032 120010726G5246LJ76872 DOOR BOEING757 757236 NM RROYCERB211 RB211535E43754555NE ENGINE OIL MISSING W K NONE D INFLIGHT SEPARATION ININSP/MAINT 1 CA (CAN) AIRCRAFT ARRIVED ON STATION WITH NR 2 ENGINE OIL SERVICING DOOR MISSING. ROLLS ROYCE SERVICE BULLETIN RB 211-71-B592 WAS INCORPORATED ON THE DOOR. A NEW ACCESS DOOR WAS INSTALLED. NEW SPRING CLIP FROM GOODRICH WILL BE INSTALL WHEN MODIFICATION BECOME AVAILABLE AS PER FIELD TECHNICAL STATUS ISSUE 12. 2L72 4F4 FRTA2NM E12EU 20010823001002001082300100WP 2001 8 23 CA010808060 120010801G52801512449107 ROD LKHEED1011 1011385114 WP RROYCERB211 RB21122B02 54555NE MLG DOOR STIFF W A UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SW99 (CAN) AFTER TAKE OFF, LEFT HAND NOSE GEAR DOOR WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE STATION. FOUND THE LEFT HAND GEAR DOOR ROD ACTUATOR VERY STIFF. UNIT WAS SERVICED AS PER MAINTENANCE MANUAL AND CHECKED SERVICEABLE AS PER OVERHAUL MANUAL. SYSTEM WAS VERIFIED AND FOUND SERVICEABLE DURING TEST FLIGHT. 2L73 4F4 F A23WE E12EU 20010823001012001082300101GL 2001 8 23 CA010809001 220010725G723023033721 COMPRESSOR WHEEL C20B6890550 BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE DAMAGED W K NONE O OTHER ININSP/MAINT 1 SW99 5069 1695 CAC35783 (CAN) DURING AN SCHEDULED INSP THE 1ST STAGE COMPRESSOR WAS NOTED TO HAVE F.O.D. AFTER REMOVING THE CASE HAVLES FOR FURTHER INSPECTION. IT WAS FOUND NO DAMAGE WENT FURTHER DOWN THAN THE 1ST STAGE. THE DAMAGE WAS INSPECTED AND BLENDED OUT IAW MAINTENANCE MANUAL. THIS F.O.D. WAS UNDETERMINED ON WHAT AND HOW, SINCE THERE WAS A PART SEP. INSTALLED. 1G71 3U3 U H2SW E4CE 20010823001032001082300103GL 2001 8 23 CA010809002 220010724G73231056058312 SPRING BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NR 2 ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A POWER ASSURANCE CHECK NR 2 ENGINE HAD TOT AND TORQUE FLUCTUATIONS. ENGINE POWER RETURNED TO OPERATIVE LIMITS AND A/C LANDED AT MAINTENACE FACILITY. DURING POST FLIGHT INSPECTION, SPRING WAS FOUND TO BE CRACKED OFF FROM GOVERNOR ARM. NEW ONE INSTALLED. 1G72 3U3 U H3EU E4CE 20010823001042001082300104CE 2001 8 23 CA010809003 120010725G21501155550259 SHAFT BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA A/C PACK SHEARED W K NONE O OTHER ININSP/MAINT 1 CA 593 (CAN) QUILL SHAFT IN AIR CONDITIONING COMPRESSOR DRIVE SHEARED AT SHEAR POINT BEHIND SPLINE. SHAFT REPLACED & AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA24CE E4EA 20010823001052001082300105GL 2001 8 23 CA010809005 220010718G725023065833 TURBINE BLADES ALLSN 250C 250C20B 03013GL ENGINE SEPARATED W EA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 CA 373 373 (CAN) AFTER AN INFLIGHT SHUTDOWN, THE ENGINE WAS DISMANTLED AT THE VANCOUVER SERVICE CENTRE OF STANDARD AERO. THE LOCAL TSB, ROLLS ROYCE AND CUSTOMER WERE ALL PRESENT DURING THE TEARDOWN INVESTIGATION. IN THE DISMANTLING OF THE TURBINE ASSEMBLY, THE 3RD STAGE TURBINE WHEEL WAS MISSING ONE ENTIRE BLADE. THE BLADE HAD SEPARATED AND CAUSED SIGNIFICANT DOWNSTREAM DAMAGE. THE EXACT CAUSE OF THE FAILURE IS CONSIDERED UNKNOWN. IN CONJUNCTION WITH THE TSB IN VANCOUVER, THE FAILED PARTS WILL BE FORWARDED TO ROLL ROYCE IN INDIANAPOLIS FOR A FULL METALURGICAL INVESTIGATION. 3 U E4CE 20010823001072001082300107WP 2001 8 23 CA010809006 120010725G2913EA501828 PUMP CVAC 440 440 2422902WP ALLSN 501D 501D13 03004GL HYD SYSTEM FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 CA 1297 (CAN) EMERGENCY LANDING WITH SMOKE IN COCKPIT. FOUND ELECTRIC HYDRAULIC PUMP BYPASSING THRU CASE DRAIN AND PUMP DEVELOPING 2,700 PSI ONLY. AFTER INSPECTION AIRCRAFT WAS FERRIED TO MAINTENANCE BASE WITH GEAR DOWN AND PUMP OFF. AC PUMP REPLACED. MULTIPLE GEAR RETRACTION C/O AND FLAP MOVEMENT USING AC HYDRAULIC PUMP. PRESSURE AND TEMPERATURE WITHIN LIMIT. AIRCRAFT RETURN TO SERVICE. 2L72 4R4 T 6A6 E282 20010823001082001082300108SW 2001 8 23 CA010809007 120010724G6310206040272101 SEAL 206040015103BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL DRIVESHAFT DETERIORATED W O OTHER D INFLIGHT SEPARATION LDLANDING 1 CA A2001964 (CAN) ON LANDING AN ABNORMAL NOISE WAS HEARD FROM ENGINE COMPARTMENT. ENGINE WAS SHUT DOWN AND IT WAS DISCOVER THAT THE FORWARD COUPLER OF THE ENGINE -TRANSMISSION X HAD HEATED UP. THE SEAL HAD RUPTURED ALLOWING THE GREASE TO EXIT HEAT UP THE COUPLER AND FURTHER MELT THE SEAL. ALL 4 TEMPLATES ON THE COUPLER HAD TURNED BLACK INDICATING AN OVERTEMP CONDITION. AT THE DAILY INSPECTION/PREFLIGHT THERE WERE NO SIGNS OF GREASE LACKING FROM THE COUPLER AND ALL 4 TEMPLATES WERE NORMAL. THIS VISUAL INSPECTION WAS CARRIED OUT BY THE PILOT 1.6FLT LVS PRIOR TO DISCOVERY OF THE FAULT. 1G71 3U3 U H2SW E4CE 20010823001092001082300109WP 2001 8 23 CA010809008 120010724G7921A1855 BRACKET ROBSIN C2361 ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA SCROLL ASSY BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 841 (CAN) UPON REMOVING THE SCROLL TO CORRECT A CLUTCH ACTUATOR SWITCH THAT WAS NOT FUNCTIONING, THE BROKEN A185-5 BRACKET WAS DISCOVERED. SUSPECT FAN IMBALANCE TO BE THE CAUSE OF THIS DEFECT. 1G71 3O3 O H11NM E295 20010823001102001082300110WP 2001 8 23 CA010809009 120010724G6200V31001 SWITCH ROBSIN C0511 ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA ACTUATOR WORN W K NONE O OTHER ININSP/MAINT 1 CA 841 0312 (CAN) AT 100 HR INSPECTION, TEST OF ACTUATOR SWITCHES-ONE SWITCH FAILED THE TEST. INSPECTION OF THE SWITCH REVEALED THAT THE ACTUATOR BUTTON ON THE SWITCH WAS WORN TO ABOUT 1/2 OF IT'S ORIGINAL HEIGHT. INSTALLED A NEW SWITCH. SUSPECT FAN IMBALANCE TO BE THE CAUSE OF THIS WEAR. 1G71 3O3 O H11NM E295 20010823001112001082300111NM 2001 8 23 CA010809014 120010710G3211NAS679A5 NUT BOEING B273201602 BOEING727 72722 1384002NM PWA JT8 JT8D7B 52053NE SUPPORT ASSY SPLIT W K NONE O OTHER ININSP/MAINT 1 CA 2031 (CAN) UPON SCHEDULED MLG REMOVAL FOUND NUT P/N NAS679A5 ON RT SUPPORT ASSY TRUNNION SPLIT ON ONE SIDE. 2L73 4F4 F A3WE E2EA 20010823001372001082300137GL 2001 8 23 CA010809016 220010722G7230 CASE 6890550 BELL 206 206L 1181522SW ALLSN 250C 250C20J 03013GL ENGINE DAMAGED W O OTHER DR INFLIGHT SEPARATION PARTIAL RPM/PWR LOSS ININSP/MAINT 1 CA 4168 982 CAC41685 (CAN) ON WINDUP FROM GROUND IDLE TO FLIGHT IDLE, THE PILOT HEARD A POPPING NOISE AND A STEADY SOUND OF RUSHING AIR. THE TURBINE OUTLET TEMPERATURE (TOT) HAD CLIMBED INTO THE YELLOW ARC. DURING TROUBLLE SHOOTING THE COMPRESSOR CASE HALF WAS MISSING AND STATOR (NEXT TO THE SPLIT LINE) AT THE 4TH STAGE STATION LINE. THIS STATOR WENT BACK AND DAMAGED THE REMAINING STATORS AND WHEELS. COMPRESSOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1G71 3U3 U H2SW E4CE 20010920000472001092000047SO 2001 9 20 CA010809018 120010726G21331036383 OUTFLOW VALVE PIPER PA42 PA42 7104202SO PWA PT6 PT6A41 52043EA CABIN PRESSURE DIRTY W B EMER. DESCENT W INADEQUATE Q C CRCRUISE 1 CA 310 (CAN) AT FLIGHT LEVEL 22000, CABIN LOST PRESSURE. AN EMERGENCY DESCENT WAS CARRIED OUT AND THE REMAINDER OF THE FLIGHT WAS NORMAL. UPON INSPECTION THE OUTFLOW VALVE WAS FOUND TO BE LOOSE AND DIRTY. THE VALVE WAS CLEANED & TIGHTENED, THEN A SATISFACTORY TEST FLIGHT WAS CARRIED OUT. 1L72 4T4 T A23SO E4EA 20010814000132001081400013NE 2001 8 14 CA010810001 120010422G5320 BULKHEAD SKRSKY SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S1 60030NE L/H SIDE ST.215 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 11668 (CAN) CRACKED FOUND AT ST.215 L/H SIDE BULKHEAD 7.5 INCHES BELOW WATERLINE 121. EXTENDING FROM M6B SUPPORT TO MAIN BULKHEAD ELECTRICAL PLUG. 1G72 3U3 U H1NE E19EU 20010920000482001092000048SW 2001 9 20 CA010810005 120010723G6410206016201133 BLADE BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL TAIL ROTOR DENTED W K NONE O OTHER ININSP/MAINT 1 CA 106 (CAN) DURING A DAILY INSPECTION THE PILOT NOTICED A DENT ON THE LEADING EDGE OF THE NOTED T/R BLADE. UPON INSPECTION THE DAMAGE WAS MEASURED AND FOUND TO BE IN LIMITS. FURTHER TO THE INVESTIGATION IT WAS FOUND THAT A SCREW HAD COME LOOSE FROM THE GEARBOX FAIRING INTO THE T/R BLADE PATH. NO OTHER DAMAGE WAS NOTED. 1G71 3U3 U H2SW E4CE 20010920000492001092000049WP 2001 9 20 CA010810006 120010801G3246C2411 CROSSTUBE ROBSIN C0148 ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA MLG CHAFED W K NONE O OTHER ININSP/MAINT 1 CA 1355 (CAN) 2 CHAFED MARKS APPROX 1/16" DEEP, 3/8" APART & 1/2" LONG, MADE BY THE WIRES OF THE SEAT HOSE THAT IS ATTACHED TO THE CABIN HEATER SHROUD ON THE OUTLET SIDE. HEATER SHROUD IS NOT A TIGHT FIT TO THE MUFFLER & I HAVE IN THE PAST NOTED WEAR ON THE MUFFLER SUPPORT RINGS FOR THE SHROUD. THERE IS ROOM FOR THE SHROUD TO ROTATE UNTIL THE SEAT HOSE & CLAMP TOUCHES & WEARS THE AFT CROSS TUBE. AFT CROSS TUBE REPLACED. 1G71 3O3 O H11NM E295 20010920000502001092000050CE 2001 9 20 CA010810007 120010518G2612302158 FIRE DETECTOR BEECH 99 99 1154002CE PWA PT6 PT6A20 52043EA LT ENGINE INTERMITTENT W E ENGINE SHUTDOWN N FALSE WARNING APAPPROACH 1 CA (CAN) ON SHORT FINAL, THE FIRE DETECTION SYSTEM ON THE LEFT ENG ACTIVATED. THE PILOT ELECTED TO SHUTDOWN THE ENG & CONTINUED WITH THE LANDING. NO OTHER INDICATIONS, SUCH AS SMOKE OR FLAMES, WERE NOTICED. ON INSPECTION THE LOWER AFT FIRE DETECTOR (NR 3) WAS FOUND TO BE INTERMITTENTLY INDICATING A FIRE WHEN THERE WAS NO FIRE. THE DETECTOR WAS REPLACED WITH A SERVICEABLE UNIT & THE A/C WAS RETURNED TO SERVICE. THERE IS AN AD ON THIS UNIT, PYROTECTOR 78-14-09, WHICH INCLUDES TESTING THE SYSTEM EVERY 100 HOURS. THIS AD HAD BEEN CARRIED OUT ABOUT 25 HOURS AGO WITH NO INDICATION OF ANY PROBLEMS. THIS IS THE FIRST TIME WE HAVE HAD A FALSE FIRE INDICATION FROM ONE OF THESE UNITS. 1L72 3T3 T A14CE E4EA 20010920000532001092000053SW 2001 9 20 CA010810013 120010625G5711 SPAR BBAVIA7 7ECA 21101NNSW AMTR CUSHMNO200 05645GL MCAULY1A100 1A100ACM GL WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) BOTH WINGS WERE STRIPPED OF FABRIC & L/E MATERIAL REMVD DURING INSP. BOTH WING TIPS WERE REMVD ALONG WITH FUEL TANKS & AILERON BELLCRANKS. SPARS WERE BLOWN WITH COMPRESSED AIR THEN WASHED DOWN WITH MILD SOAP & WARM WATER. THE INSP THEN PROCEEDED USING HIGH INTENSITY LAMP & LARGE MAGNIFYING GLASS. AFTER REMOVING VARNISH IN LIFT STRUT ATTACHMENT POINT, I COULD IDENTIFY VERY SMALL CRACK IN GLUE JOINT ON REAR FACE OF RIGHT REAR WING SPAR. USING LIGHT & MAGNIFYING GLASS, I DETECTED ON UPPER EDGE OF RIGHT REAR SPAR, TOTAL OF 5 COMPRESSION TYPE CRACKS WHICH UNDER NORMAL LIGHTING CONDITIONS COULD NOT BE SEEN. 2 ACTUAL SPLITS WERE REVEALED STARTING AT REINFORCING PLYWOOD PLATE. THESE SPLITS FOLLOWED EDGE GRAIN OF 1H71 3O3 O A759 EXPA3O 5 NP918 20010920000552001092000055EU 2001 9 20 CA010813003 120010731G243123491 BATTERY BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE731* 01518WP NR 2 OVERHEATED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA 35 (CAN) DURING CRUISE NR 2 BATTERY OVERHEAT INDICATED IN COCKPIT, CREW DIVERTED TO CYXU, BATTERY WAS REPLACED WITH SERVICABLE UNIT AND AIRCRAFT PROCEEDED WITH NO ADDITIONAL FAULTS. FAULTY BATTERY WAS FORWARDED FOR REPAIR/DEEP CYCLE. 2L72 4F4 FRTA3EU E6WE 20010920000572001092000057EA 2001 9 20 CA010813005 220010703G7230 BLADE BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA HARTZLHCB4T HCB4TN3 GL COMPRESSOR SEPARATED W C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 CA (CAN) ON TAKEOFF PARTIAL LOSS OF POWER EXPERIENCED ON RT ENGINE. TAKEOFF ABORTED. UPON SUBSEQENT TEAR DOWN WITH A PRATT & WHITNEY REPRESENTATIVE PRESENT, IT HAS BEEN DETERMINED THAT A COMPRESSOR TURBINE BLADE SEPARATED AND DAMAGED COMPONENTS DOWNSTREAM IN ENGINE. 1L72 3T4 T A14CE E4EA 6 CP40EA 20010920000592001092000059CE 2001 9 20 CA010813009 120010630G531050430043867 DOOR FRAME BEECH 100 100BEECH 1152916CE PWA PT6 PT6A28 EA HARTZLHCD4N3HCD4N3A GL FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 21552 (CAN) DOOR FRAME FORWARD 50-430043-867 CRACKED ON LOWER BAYONNET HOLE TO SCREW HOLE AND 1/2" BEYOND. OTHER SCREW HOLE TO BAYONNET HOLE. DOOR FRAME AFT 50-430043-865 CRACKED ON UPPER BAYONNET HOLE TO SCREW HOLE ONE ONLY. 1L72 3T4 T A14CE E4EA 5 CSTC 20010920000612001092000061EU 2001 9 20 CA010813011 120010716G2750ONL3120146X77 BOLT Z4243430000 ZLIN 242 Z242L 9970204EU LYC O360 AEIO360A1B6 41514EA FLAP CONTROL BENT W K NONE O OTHER ININSP/MAINT 1 CA 3046 (CAN) DURING A 100/500 HOUR INSPECTION THE LT FLAP BELLCRANK BOLT WAS FOUND TO BE BENT. THE BOLT WAS REPLACED WITH A NEW ONE. IT IS SUSPECTED THAT A STUDENT PILOT EXTENDED THE FLAPS ABOVE THE MAXIMUM SPEED ALLOWED FOR FLAP EXTENSION. THE MAINTENANCE SCHEDULE ALREADY HAS AN ADDITIONAL INSPECTION ON THE FLAP BOLTS AND THE INSTRUCTORS AND STUDENTS WERE AGAIN REMINDED OF THE PROPER PROCEDURE USING THE FLAPS. 1L71 3O3 O0 A76EU 1E10 20010920000682001092000068NM 2001 9 20 CA010813012 120010721G5310 DOOR FRAME BOEING727 72722 1384002NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FWD FRAME OF AFT CARGO DOOR CRACKED AT BS1057, STR.24. CRACK MEASURED 1.5 INCHES. 2L73 4F4 F A3WE E2EA 20010920000732001092000073CE 2001 9 20 CA010813013 120010720G280057181061 HARNESS CESSNA441 441 2076020CE FUEL SYSTEM CHAFED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA (CAN) DURING INVESTIGATION OF INTERMITTENT BOOST PUMP FOUND CHAFED SPOT ON WIRE HARNESS INSIDE FUEL TANK. MAGNIFIED VIEW SHOWED EVIDENCE OF ELECTRICAL CONTACT BETWEEN WIRE AND STRUCTURE OF FUEL TANK. 1L72 3T RTA28CE 20010920000752001092000075SO 2001 9 20 CA010813014 120010720G324410320400 BOLT CLEVELAND 40106 PIPER PA31T PA31T 7103124SO PWA PT6 PT6A28 EA WHEEL CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 795 795 (CAN) ON AN EVENT NR 2 INSPECTION IT WAS FOUND THAT THE RIGHT MAIN WHEEL P/N 40-106 WAS MISSING 1 THROUGH BOLT ((P/N 103.20400 (AN5-35A))AND ANOTHER BESIDE THE MISSING BOLT BROKEN IN TWO AND PROTRUDING FORWARD THE BRAKE CALIPER. THE ROTATION OF THE WHEEL CAUSED THE HEAD OF THE BOLT TO CAUSE CONSIDERABLE DAMAGE TO THE TORQUE PLATE. (P/N 075-12800). 1L72 3T4 T A8EA E4EA 20010920000762001092000076 2001 9 20 CA010813016 420010715G34201242102011 INDICATOR PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL AHRU FAILED W O OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 CA 462 1545 (CAN) DURING STRAIGHT AND LEVEL FLIGHT THE PILOTS AHRU DISPLAY WENT BLANK. THE PILOT CYCLED THE CIRCUIT BREAKERS, AND THE UNIT CAME BACK ON. THE UNIT HAS BEEN REPLACED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010920000792001092000079 2001 9 20 CA010813017 420010724G34201242102011 INDICATOR PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL AHRU FAILED W O OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 CA 476 (CAN) DURING STRAIGHT AND LEVEL FLIGHT THE CO-PILOTS AHRU DISPLAY WENT BLANK. THE PILOT CYCLED THE AVIONICS POWER, AND THE UNIT CAME BACK ON. THE UNIT HAS BEEN REPLACED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010920000812001092000081EU 2001 9 20 CA010813018 120010724G24349789601090 BRUSH HOLDER BOSCH 5243212158 PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL GENERATOR WORN W K NONE O OTHER ININSP/MAINT 1 CA 102 100318 (CAN) DURING A 100 HOUR INSPECTION, THE BRUSH ASSEMBLY WAS REMOVED TO VERIFY THE CONDITION. THE BRUSH ASSEMBLY WAS WORN EXCESSIVELY, AND HAS BEEN REPLACED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010920000862001092000086SW 2001 9 20 CA010813021 120010725G281071493 STRUCTURE BBAVIA8 8GCBC 1220803SW LYC O360 O360C2E 41514EA FUEL CELL CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) - FUEL TANK CRACKING. - POSSIBLY DUE TO TOO LIGHT GUAGE OF MATERIAL & NO INTERNAL BAFFLES INTANK. CRACKS USUALLY OCCUR AT END OF STIFFENER INDENTS. - WE AVERAGE 2-3 FUEL TANK FAILURE DUE TO CRACKING PER FLYING SEASON. 1H71 3O3 O A21CE E286 20010920000872001092000087SW 2001 9 20 CA010813022 120010801G2823110660 SHUTOFF VALVE BBAVIA8 8GCBC 1220803SW LYC O360 O360C2E 41514EA FUEL SYSTEM FAILED W D RETURN TO BLOCK Y ENGINE STOPPAGE TXTAXI/GRND HDL 1 CA (CAN) - THREADED COLLAR THAT SECURES VALVE SHAFT IN BODY CAME LOOSE AND DETACHED ITSELF FROM SHUTOFF BALL INSIDE VALVE. FOR SOME REASON THE VALVE WAS OR WENT INTO THE CLOSED POSITION & STARVED THE ENGINE FOR FUEL DURING TAXI OUT FOR DEPARTURE. - THERE IS NOTHING PROVIDED TO SECURE THE COLLAR SO THAT IT WILL NOT LOOSEN. 1H71 3O3 O A21CE E286 20010920000912001092000091CE 2001 9 20 CA010813024 120010809G3220030A39313 BOLT MTSBSIMU2 MU2B36A 5780413CE GARRTTTPE331TPE3315 01514WP NLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE NOSE LANDING GEAR DRAG STRUT ATTACH BOLT WAS FOUND CRACKED AT SCHEDULED NDT INSPECTION OF BOLT. THIS BOLT HAD BEEN MAGNETIC PARTICAL INSPECTED EVERY 2000 HOURS. 1H72 3T4 T A10SW E4WE 20010920000932001092000093NM 2001 9 20 CA010814003 120010726G2900TC125UK00ZY1 INDICATOR BOEING767 767333 NM PWA 4060 PW4060 52119NE HYD PRESSURE LEAKING W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) ENROUTE FROM TEL AVIV TO TORONTO AFTER THE LT SYSTEM WAS TOPPED OFF (IN TLV) LOSS OF HYDRAULIC FLUID OF THE L/H SYSTEM, THE A/C RE-ROUTED AND ASK FOR AN EMERGENCY LANDING. A/C LANDED SAFELY WITHOUT FURTHER INCIDENT. FOUND TO BE A LEAK AT THE DIFFERENTIAL INDICATOR PRESSURE DRAIN CASE MODULE FILTER (AROUND THE POP OUT). REPLACED THE PRESSURE CASE DRAIN FILTER MODULE DIFFERENTIAL PRESSURE INDICATOR. 2L72 4F4 FRTA1NM E24NE 20010920000942001092000094EU 2001 9 20 CA010814005 120010718G274047147400 ACTUATOR AIRBUSA340 A340313 EU CFMINTCFM56 CFM565C4 13802NE HORIZONTAL STAB FAILED W K NONE F FLT CONT AFFECTED ININSP/MAINT 1 CA (CAN) ON MAINTENANCE CHECK FOUND TRIM HORIZONTAL STABILIZER ACTUATOR BALLNUT TRANSFER TUBE DISCONNECTED FROM BALLNUT. REPLACED TRIM HORIZONTAL STABILIZER ACTUATOR AND SYSTEM TESTED. 2L74 4F4 FRTA197 E37NE 20010920000962001092000096EU 2001 9 20 CA010814006 120010718G3244 TIRE AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE MLG SEPARATED W A UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 CA (CAN) #3 MAIN WHEEL TIRE CAP SEPARATION ON TAKEOFF. AIR TURN BACK TO AIRPORT. AIRCRAFT SUSTAINED DAMAGE TO #2 ENGINE FAN BLADES, ENGINE INTAKE ACOUSTIC PANELS, R/H INBOARD TRAILING EDGE FLAP. ONE LINE OF THE YELLOW HYDRAULIC SYSTEM BROKE IN AREA OF R/H MAIN LANDING GEAR AREA. THE R/H HORIZONTAL STABILIZER DENTED AND HOLE ON THE UPPER SURFACE OF THE R/H WING ABOVE THE MAIN LANDING GEAR (R/H).REPAIRS WILL BE ACCOMPLISHED AFTER ENGINEERING EVALUATION.FINAL REEPORT FOR FIXES WILL BE PRODUCED AT A LATER DATE. 2L72 4F4 FRTA28NM E29NE 20010828000722001082800072CE 2001 8 28 CA010814020 120010615G213113035616 CONTROLLER 13035616 CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE INTERNAL W BG EMER. DESCENT O2 MASK DEPLOYED W INADEQUATE Q C DEDESCENT 1 CA 207 79327 (CAN) PRESSURIZATION PROBLEMS OCCURRED SHORTLY AFTER TAKEOFF BACK TO OTTAWA (CONTROL). ON DESCENT THROUGH 23,000 FEET. CREW EXPERIENCED RAPID DEPRESSURIZATION. MASKS WERE DONNED AND DESCENT ACCELERATED TO BELOW 10,000 FT. MAINTENANCE DETERMINED THE CAUSE TO BE THE PRESSURIZATION CONTROLLER, CONTROLLER REPLACED. NO FURTHER ACTION REQUIRED. 1L72 4F4 F A22CE E1NE 20010920000982001092000098CE 2001 9 20 CA010814021 120010807G213041EN496 SQUAT SWITCH CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE CABIN PRESSURE WORN W BG EMER. DESCENT O2 MASK DEPLOYED W INADEQUATE Q C DEDESCENT 1 CA (CAN) WHILE IN DESCENT FROM FL330, AND DESCENDING THROUGH 15,000 FT CABIN ALTITUDE STARTED TO INCREASE RAPIDLY. AIRCRAFT DIVERTED TO CYQM FOR MAINTENANCE. WHILE AT 10,000 FT CABIN ALTITUDE RECOVERED. WHEN THROTTLES REDUCED FROM 88 TO 70 PERCENT N1, CABIN PRESSURIZATION WAS LOST AGAIN. MAINTENANCE DETERMINED THAT THE L/H SQUAT SWITCH WAS AT FAULT UNIT REPLACED, NO FURTHER ACTION. 1L72 4F4 F A22CE E1NE 20010920001002001092000100CE 2001 9 20 CA010814022 120010802G27100510105217 CONTROL CABLE CESSNA CESSNA172 172I 2072426CE LYC O320 O320E2D 41508EA MCAULY1C172 1C172MTM GL AILERON CONTROL FRAYED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AIRCRAFT DAMAGE ON LANDING AT PICTOU ISLAND. AIRCRAFT BEING STRIPPED FOR REPAIR WHEN THE CABLE, ABOVE WAS FOUND FRAYED WHERE IT PASSES OVER THE PULLEY. LT SIDE TOP OF FUSELAGE. 1H71 3O3 ONT3A12 E274 5 NP910 20010920001042001092000104NM 2001 9 20 CA010815001 120010709G24332299 TRANSFORMER BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE E&E BAY FAULTY W O OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 CA (CAN) AT CRUISE, A SNAPPING NOISE WAS HEARD. NR 1 TR CB POPPED. NR 1 MAIN FUEL TANK AFT FUEL BOOST PUMP CB POPPED ALONG WITH NUMEROUS C/P LIGHTS. #1 ENGINE OIL TEMP INDICATOR, CAPT'S AUX. PITOT STATIC AND NO SMOKING & FASTEN SEAT BELT SIGNS ALL NOT OPERATING. AS A PRECAUTION, ATC NOTIFIED FOR DIRECT DESTINATION IN CASE OF FURTHER ELECTICAL PROBLEMS. ON INITIAL DESCENT, THE TR BUS SUDDENLY POWERED BACK UP AGAIN & AIRCRAFT LANDED WITHOUT INCIDENT #1 TR REPLACED IAW MM 24-21-0 AND CHECKED SERVICEABLE. NO FURTHER PROBLEM DURING SUBSEQUENT FLIGHT. 2L72 4F4 F A16WE E2EA 20010920001052001092000105NM 2001 9 20 CA010815002 120010716G28222580003 PUMP BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE FUEL BOOST FAILED W O OTHER O OTHER CRCRUISE 1 CA (CAN) 1. EXTENGUISHED. NR 1 115 VAC TR BUS INOP. AIRCRAFT LANDED WITHOUT INCIDENT. MAIN FUEL TANK, AFT FUEL BOOST PUMP UNSERVICEABLE. BOOST PUMP CHANGED IAW MM 28-22-41. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2L72 4F4 F A16WE E2EA 20010920001062001092000106EU 2001 9 20 CA010815003 120010713G5240A5247514700800 DOOR AIRBUS310 A310304 EU GE CF6 CF680C2A5 NE LAV SERVICE MISSING W K NONE O OTHER ININSP/MAINT 1 CA (CAN) 1. DURING THE TURNAROUND IT WAS OBSERVED THAT THE MID LAV SERVICING PANEL DOOR WAS MISSING. 2. DMI 35881 WAS RAISED UNDER CDL 52-4. AIRCRAFRT RELEASED FOR FLIGHT.3. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT. 2L72 4F4 FRTA35EU E13NE 20010920001072001092000107EU 2001 9 20 CA010815004 120010720G5270 WARNING SYSTEM AIRBUS310 A310304 EU GE CF6 CF680C2B2 30025NE CARGO DOOR FALSE ACTIVATIONW O OTHER N FALSE WARNING CLCLIMB 1 CA (CAN) 1. DURING TAKEOFF, ECAM WARNING FOR BULK CARGO DOOR INDICATION. AIRCRAFT RETURNED TO GATE. SYSTEM CHECKED AND MEL 52-7-0 APPLIED. AIRCRAFT RELEASED FOR FLIGHT. 2. NO PROBLEM DURING SUBSEQUENT FLIGHT. 3. UPON ARRIVAL TO HOME BASE, BULK CARGO DOOR INDICATION CHECKED SERVICEABLE AND MEL 52-7-0 CLEARED.4. NO FURTHER PROBLEM DURING SUBSEQUENT FLIGHT. 2L72 4F4 FRTA35EU E13NE 20010920001082001092000108EU 2001 9 20 CA010815005 120010620G315020662155 CONTROLLER AIRBUS310 A310304 EU GE CF6 CF680C2B2 30025NE ECAM FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA 1893 (CAN) 1. AT CRUISE, ECAM CONTROLLER SHOWED SIGNS OF BEING ERRATIC, FLASHING THEN TURNED BLACK. SMOKE STARTED FOR 10 SECONDS WITH ELECTRICAL SMELL. CB POPPED AND SMOKE STOPPED. NOT ENOUGH SMOKE TO DON O2 MASKS. 2. PHONE PATCH MADE TO DISPATCH REGARDING PROBLEM. AIRCRAFT CONTINUED WITH FLIGHT WHILE MONITORING SITUATION. 3. ON ARRIVAL, #1 ECAM CONTROLLER REPLACED AND CHECKED SERVICEABLE IAW MM 31-51-00. 4. NO FURTHER PROBLEM DURING SUBSEQUENT FLIGHT. 2L72 4F4 FRTA35EU E13NE 20010920001102001092000110CE 2001 9 20 CA010815012 120010801G55401156400006 HINGE BEECH 99 99 1154002CE PWA PT6 PT6A28 EA HARTZLHCB3T HCB3TN3 GL RUDDER LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) UPPER RUDDER HINGE BRACKET RIVETS LOOSE DUE TO FLIGHT CONTROL FLUTTER.SCREWS WERE LOOSE IN THE CENTER HINGE ALSO. PC/TSO/TSN ARE UNKNOWN, NOT 0.0. 1L72 3T4 T A14CE E4EA 6 CP15EA 20010920001122001092000112CE 2001 9 20 CA010817002 120010814G571010140243S BOLT BEECH 99 99 1154002CE PWA PT6 PT6A28 EA WING DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA 1118111181 (CAN) BOLT FOUND WITH MECHANICAL THREAD DAMAGE UPON INSPECTION 1L72 3T4 T A14CE E4EA 20010920001132001092000113SO 2001 9 20 CA010817003 120010626G3260 INDICATOR PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA MLG FAILED W L ABORTED APPROACH N FALSE WARNING APAPPROACH 1 CA (CAN) WHILE LANDING THE LT WHEEL LIGHT DID NOT COME ON. AFTER VERIFICATION WITH THE MIRABLE TOWER WHO CONFIRMED 3 WHEELS OUT. THE AIRCRAFT RETURNED TO ST-HUBERT WITH THE LANDING GEAR DOWN. THE LIGHT CAME ON WHILE ONROUTE TO ST-HUBERT. 2 ELECTRICAL TERMINALS WERE REPLACED AND THE GROUND WAS CLEANED FOLLOWED BY MANY RETRACTIONS AND THE SYSTEM WAS CHECKED SERVICEABLE. 1L72 3O3 O 1A10 1E4 20010920001142001092000114NE 2001 9 20 CA010820009 220010619G8500114651 CYLINDER HEAD CVAC PBY5 PBY5A 2421208WP PWA R1830 R183092 52020NE ENGINE CRACKED W A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CA 248 (CAN) NO. 11 CYLINDER HEAD CRACKED CYLINDER REPLACED. A/C RETURNED TO SERVICE. ON A TRAINING FLIGHT FLIGHT, ONE WATER PICK UP WAS CARRIED OUT, LOAD WAS DROPPED ON TARGET, WHILE GOING BACK FOR A SECOND LOAD, THE MAP SHOWED A SUBSTANTIAL SPEED. VISUAL CHECKS OF THE ENGINES WAS DONE AND A SUBSTANTAIL OIL LEAK ON THE RIGHT ENGINE WAS FOUND. ENGINE WAS SHUT DOWN, SOON AS POSSIBLE. 2H72 4R4 R 2548 5E4 20010920001152001092000115CE 2001 9 20 CA010820010 120010807G2841774000419 TRANSMITTER CESSNA150 150J 2071820CE FUEL QTY STUCK W D RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TXTAXI/GRND HDL 1 CA 116 (CAN) TRANSMITTER LEVER PIVOT HAS BECOME SOMEWHAT STIFF, RESULTING IN INACCURATE FUEL LEVEL INDICATIONS. PART WAS REPLACED. THIS PART IS PART OF CESSNA SERVICE KIT SK-150-65. THE KIT WAS MADE NECESSARY BY THE UNAVAILABILITY OF THE ORIGINAL STEWART- WARNER SYSTEM PARTS. THIS UNIT IS MADE BY ROCHESTER. HOLDING PARTS FOR 21 DAYS. AFTER WHICH IT WILL BE RETURNED FOR WARRANTY. 1H71 3O 3A19 20010920001162001092000116SO 2001 9 20 CA010820012 120010726G3297 WIRE PIPER PA44 PA44180 7104402SO MLG BROKEN W O OTHER P NO WARNING INDICATION APAPPROACH 1 CA (CAN) AS PILOT SELECTED GEAR DOWN ON APPROACH "GEAR WARNING" CCT BREAKER TRIPPED&UNSAFE LIGHT DID NOT ILLUMINATE DURING GEAR EXTENSION. PILOT NOTICED THAT HE HAD 3 GREEN LIGHTS INDICATING GEAR DOWN&LOCKED. AIRCRAFT LANDED W/O INCID.. MANTENANCE FOUND L.H. DOWNLOCK SWITCH WITH WIRES PULLED OUT OF SWITCH BODY. DOWNLOCK SWITCHES TURN OFF GEAR WARNING SYS WHEN ALL 3 SWITCHES ARE ENGAGED. PULLED WIRES WERE SHORTING OUT&WHEN TH E GEAR SELECTED DOWN BREAKER WOULD TRIP.WHEN LDG GEAR RETRACTS WIRES RUB ON GEAR LEG,&IF SWITCH IS INST W/O ANY SLACK IN WIRES THEY CAN BE PULLED OUT OF SWITCH. WIRES WERE WRAPPED WITH SPIRAL WRAPAND SWITCH INST WITH ENOUGH SLACK IN THE 1L72 3O A19S0 20010920001172001092000117SO 2001 9 20 CA010820014 120010727G27404296102 SCREW PIPER 4269200 PIPER PA18 PA18 7101802SO LYC O320 O320A2B 41508EA STABILIZER BROKEN W K NONE F FLT CONT AFFECTED TXTAXI/GRND HDL 1 CA 2725 (CAN) STABILIZER TRIM FOUND NOT WORKING ON PILOT'S WALK AROUND. DISASSEMBLE AND FOUND SCREW BROKEN IN HALF, JAMMED IN THE YOKE HOUSING. 1H71 3O3 O 1A2 E274 20010920001182001092000118EU 2001 9 20 CA010821003 120010807G30103D248526 TIMER PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL AIRFOIL DEICER MALFUNCTIONED W K NONE L NO TEST ININSP/MAINT 1 CA 471 (CAN) ON THE SCHEDULED AIRFOIL DEICER SYSTEM INSPECTION, IT WAS DISCOVERED THAT THE NORMAL INFLATION SEQUENCE WOULD WORK PROPERLY ONLY 1 TIME OUT OF THREE. IT WAS DETERMINED THAT THE TIMER WAS FUNCTIONING IN AN INTERMITTENT MANNER. DEICER CAUTION LIGHT WOULD COME ON INDICATING SEQUENCE MALFUNCTION. THE TIMER WAS REPLACED WITH A SERVICEABLE UNIT. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010920001192001092000119CE 2001 9 20 CA010821005 120010811G24347565T1 ALTERNATOR CESSNA305 305A 2074002CE CONT O470 O47011 17026SO ENGINE FAILED W O OTHER N FALSE WARNING CRCRUISE 1 CA 446 151 (CAN) ALTERNATOR WENT OFF LINE. UPON REMOVAL OF THE ALTERNATOR WAS NOTICED THAT THE SPLINE GEAR WAS SHEARED. THE DRIVE SHAFT WAS ALSO SHEARED IN THE THREADED PORTION, JUST BELOW THE CASTLE NUT. THE CASTLE NUT WAS STILL INTACT ON THE TIP OF THE THREADED SHAFT WITH THE COTTER PIN INTACT. THIS PARTICULAR UNIT HAS BEEN SENT TO DND TEST FACILITIES TO DETERMINE THE EXACT CAUSE OF FAILURE. 1H71 3O3 O 5A5 E269 20010920001202001092000120CE 2001 9 20 CA010821010 120010808G3221NA5130514DH BOLT CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL NLG BROKEN W EC ENGINE SHUTDOWN ABORTED TAKEOFF DR INFLIGHT SEPARATION PARTIAL RPM/PWR LOSS TOTAKEOFF 1 CA 4347 (CAN) ON TAKE OFF PILOT BEARD A BANG. THIS WAS FOLLOWED BY A NOTICEABLE LOSS OF NOSE WHEEL CONTROL (STREERING). TAKE OFF WAS ABORTED, INSPECTION REVEALED ONE OF THE NOSE GEAR FORK ATTACH BOLTS WAS BROKEN. 1H71 3T3 T A37CE E4EA 5 CP60GL 20010920001212001092000121CE 2001 9 20 CA010821011 120010813G27200411307 ARM CESSNA206 U206G 2073356CE CONT O550 IO550F 17042SO RUDDER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2965 (CAN) DURING A 200 HOUR ANNUAL INSPECTION, THE PILOT R/H RUDDER PEDAL ARM FOUND LOOSE. THE ARM WAS CRACKED IN TWO PLACES: FROM EACH OF THE ATTACH BOLT HOLES TO THE BOTTOM OF THE TUBE. 1H71 3O3 O A4CE E3SO 20010921000082001092100008WP 2001 9 21 CA010822013 220010730G7250TPE33110UG514H ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP ROTOL R333 R333482F12 GL NACELLE DAMAGED W E ENGINE SHUTDOWN X ENGINE FLAMEOUT LDLANDING 1 CA 3319 (CAN) ON LANDING IN FORT MCMURRAY ON THE MORNING OF 30 JULY, 01 AN UNCOMMANDED ENGINE SHUTDOWN OCCURRED. THE PILOT REPORTED THAT THE ENGINE SHUT DOWN WHEN THE WHEEL TOUCHED THE GROUND, OR SHORTLY THEREAFTER. HE PULLED THE STOP FEATHER LEVER FOR THAT ENGINE AND CONTINUED THE LANDING. ON INVESTIGATION OF THE ENGINE, WE COULD NOT FIND ANYTHING WRONG EXTERNALLY, BUT THE ENGINE WOULD NOT START. WE REMOVED THE ENGINE FROM THE AIRCRAFT AND FOUND EVIDENCE THAT INTERNAL DAMAGE HAD OCCURRED. THE THIRD STAGE APPEARS TO HAVE BEEN RUBBING. 2L72 4T4 TRTA21EU E4WE 6 CP61GL 20010921000112001092100011WP 2001 9 21 CA010823003 120010727G2120LS11088B614 DUCT LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE CABIN AIR SPLIT W C ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CA (CAN) AIRCRAFT REJECTED TAKE OFF AT 80 KTS DUE A LOUD NOISE IN COCKPIT. FOUND THE #2 ZONE TRIP MANIFOLD DUCT HOSE COUPLING SPLIT. THE COUPLING WAS REPAIRED AS PER MAINTENANCE MANUAL AND SUBSEQUENTELY THE HOSE COUPLING WAS REPLACED AT THE NIGHT LAYOVER. 2L73 4F4 F A23WE E12EU 20010921000162001092100016GL 2001 9 21 CA010823015 320010815G6110A4643 SPACER TMPSONNAVIONNAVIONA 6150104SW MCAULY2A34C D2A34C98 GL PROPELLER CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 43 (CAN) PART CORRODED AND INSTALLED UPSIDE DOWN. 1L71 3O A782 5 CP3EA 20010921000172001092100017SO 2001 9 21 CA010827004 220010809G7414M3820 DISTRIBUTOR BLK SLICK 6310 CESSNA206 TU206G 2073357CE CONT O520 TSIO520M 17040SO MCAULY2AF34CD2AF34C* GL MAGNETO BURNED W K NONE O OTHER ININSP/MAINT 1 CA 106 01012755 (CAN) BOTH MAGNETOS WERE REMOVED IN ERROR FOR 500 HR INSP ONLY LH WAS DUE WHEN RH MAGNETO WAS DISASSEMBLIED BY LEGGAT AVIATION. THE BEARING BAR P/N M3004 WAS BURNED THROUGH AT HIGH TENSION BRUSH AREA OF DISTRIBUTER BLOCK NO PROBLEM WAS EVER FOUND ON MAGNETO CHECK. 1H71 3O3 O A4CE E8CE 5 CP5EA 20010921000182001092100018EU 2001 9 21 CA010827008 120010812G79301D1 CHIP DETECTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ENGINE ACTIVATED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) ENGINE CHIP LIGHT IN FLIGHT. CHIPS FOUND ON UPPER ELECTRICAL CHIP PLUG, MO5 AND ENGINE OIL TANK PLUGS. ENGINE REMOVED FOR EVALUATION. 1G71 3U3 U H9EU E19EU 20010921000192001092100019SW 2001 9 21 CA010827009 120010814G6410 BLADE BELL 206011810013BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL TAIL ROTOR TORN W A UNSCHED LANDING FD FLT CONT AFFECTED INFLIGHT SEPARATION NRNOT REPORTED 1 CA 2585 MOT3141 (CAN) WHILE IN FLIGHT THE T/R COULING FILLER COVER DEPARTED AND STRUCK THE TAIL ROTOR BLADE CAUSING A 2 CM TEAR OR HOLE IN ONE BLADE ABOUT 2/3 OF THE WAY DOWN. JUST AFT OF THE LEADING EDGE. THE A/C LANDED SAFELY. NO OTHER DAMAGES WAS FOUND. NEW COVER TO T/R ASSY INSTALLED A/C RETURNED TO SERVICE. 1G71 3U3 U H2SW E1GL 20010921000252001092100025NE 2001 9 21 CA010828021 120010827G651076361040078101 COUPLER SKRSKY 763610520104SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL TAIL ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 171 (CAN) DURING INSP OF TAIL ROTOR DRIVESHAFT ASSY IT NOTED THAT FLEX COUPLING BETWEEN INTERMEDIATE GEARBOX & NR 5 TAIL ROTOR DRIVESHAFT HAD CRACKED LAMINATE. COUPLING REMOVED & INSP. IT HAD ONE CRACKED LAMINATE (OUTTER LAMINATE OF PACK) & CRACK LOCATED BETWEEN 2 OF FLANGE ATTACHEMNT BOLT HOLES. CRACK RUNS COMPLETLELY THROUGH LAMINATE IN STRAIGHT LINE FROM OUTTER EDGE TO INNER EDGE. IS NO APPARENT SURFACE DEFECT THAT WOULD APPEAR SURFACE DEFECT THAT WOULD APPEAR TO BE CAUSE IF CRACK. PART HAS BEEN SENT TO SIKORSKY A/C PRODUCT SAFETY DEPARTMENT FOR EVALUATION. SIKORSKY A/C FIELD SERVICE REPRESENTATIVE STATED THAT HAS BEEN PREVIOUS CASES OF THESE COUPLINGS CRACKING. 1G72 3U3 U H1NE E1GL 20010921000332001092100033CE 2001 9 21 CA010828023 120010814G2730 TORQUE TUBE BEECH 1156100103 BEECH 99 99 1154002CE PWA PT6 PT6A28 EA HARTZLHCB3T HCB3TN3 GL ELEVATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA NA (CAN) UPON PERFORMING THE SB2145 ON THE COMPONENT.FIRST INSPECTION FROM FACTORY, WE DO IT UPON ARRIVAL FOR QUALITY REASONS. A CRACK WAS FOUND DURING THE LPI PROCESS.THE CRACK TRAVELS FROM INSIDE THE HOLE TO APROX. 4MM OUTSIDE THE HOLE RUNNING AXIAL ALONG THE TUBE. TUBE WAS REJECTED. 1L72 3T4 T A14CE E4EA 6 CP15EA 20010921000352001092100035CE 2001 9 21 CA010829009 120010819G2810052600750 FUEL TANK CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA MCAULY1C160 1C160DTM GL FUSELAGE CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA 4055 (CAN) TANK WOULD ALWAYS POP OR OIL CAN AS IT WAS FILLED, LEAK WOULD ONLY OCCUR WHEN TANK WAS FUELLED RIGHT TO THE TOP. IT IS BELIEVED THAT THE REPETITIVE OIL CANNING OF THE TANK CAUSED A FATIQUE CRACK TO START. THE TANK WAS REPAIRED AND THE UPPER SURFACE WAS CONTOURED BACK TO ITS ORIGINAL SHAPE SO IT WILL NOT OIL CAN ANY LONGER. 1H71 3O3 ONT3A12 E274 5 NP910 20010921000472001092100047CE 2001 9 21 CA010830007 120010823G243523079004 STARTER GEN CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL RT ENGINE FAILED W EH ENGINE SHUTDOWN DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 CA 84 (CAN) PILOT WAS TAXING WHEN HE LOST TOTAL POWER TO NO. 2 BUS. INVESTIGATION FOUND THAT THE R/H GENERATOR COOLING FAN BLADES TOTALLY CRACKED OFF AND FLEW INTO THE GENERATOR WINDINGS, DESTROYING ALL WORKING CAPABLITY OF STARTER GENERATOR. THIS CAUSED A GCU FAILURE AND A NO. 2 BUS CURRENT LIMITER TO BLOW AS WELL. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20010921000482001092100048EU 2001 9 21 CA010830009 120010823G21609599020135 CONTROL VALVE PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL TEMP CONTROL SEIZED W D RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CA 3783 3783 (CAN) AFTER STARTUP THE PILOT SELECTED COOL SETTING ON THE ENVIRONMENTAL CONTROL SYSTEM (ECS). THE SYSTEM BLEW COOL AIR FOR APPROX 25 SECONDS, THEN BLEW HOT AIR. AFTER APPROX 1 MINUTE THE SYSTEM SHUTDOWN AND AN AMBER LIGHT INDICATING ECS FAILURE APPEARED ON THE CAWS DISPLAY. THE SYSTEM AND DETERMINED THAT THE TEMP CONTROL VALVE WAS NOT FUNCTIONING. AFTER REPLACEMENT OF THE PART AND RUNUP, THE SYSTEM WORKED NORMALLY. AIRCRAFT WAS RETURNED TO SERVICE. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010921000492001092100049EU 2001 9 21 CA010830017 120010713G3246AHA1489 WHEEL BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 3234 699 (CAN) THE WHEEL HAD BEEN REMOVED DUE TO THE TIRE BEING WORN TO LIMITS. DURING THE CLEANING PROCESS, TWO CRACKS WERE DISCOVERED VISUALLY. THEY RAN FROM THE LIGHTENING HOLES TO UNDER THE WHEEL BEARING OUTTER RACE. PICTURES ARE AVAILABLE. THE WHEEL HALF HAD BEEN N.D.T. INSPECTED AT LAST TIRE REPLACEMENT MAR 28/01. 2H74 4F4 FRTA49EU E6NE 20010921000552001092100055GL 2001 9 21 CA010830020 220010828G73132306045 NOZZLE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE WARPED W K NONE O OTHER ININSP/MAINT 1 CA 535 (CAN) THERE WERE INTERMITTENT START DELAYS ON A/C AT VARIOUS TIMES DURING OPAL SORTIES. IT DETERMINED THAT POOR FITTING 1ST STAGE NOZZLE CAUSED START DELAY. TURBINE REPD WITH INST OF NEW 1ST STAGE NOZZLE P/N 23062753 S/N KD258711; NEW NOZZLE SHIELD P/N 23073533&2 NEW POSING PLUGS P/N 23009573. NOZZLE TBO 535.6 HRS, NOZZLE SHIELD TBO U/K 535.6 HRS SINCE INSP. POS PLUG TSN U/K TBO U/K TIME SINCE INSP 535.6 HRS. FINDINGS PRIOR TO THE REPLACED OF AFOREMENTIONED PARTS; 1ST STAGE NOZZLE P/N 23060450, NOZZLE SHIELD P/N 6890040 APPEARED TO BE WARPED WHEN PLACED ON LEVELING PLATE THAT MAY HAVE CONTRIBUTED TO POOR FIT OF BOTH ENGINE COMPONENTS. ONE ADDITIONAL OBSERVATIO N MODS TO LOWER POSING PL 1G71 3U3 U H2SW E4CE 20010921000592001092100059SO 2001 9 21 CA010831004 120010821G71203743701 FASTENER PIPER PA34 PA34220T 7103420SO CONT O360 TSIO360KB 17025SO MCAULY3AF32C3AF32C508 GL FITTING MISSING W K NONE O OTHER ININSP/MAINT 1 CA (CAN) 1. FITTING, ASSY OUTBOARD LOWER ENGINE MOUNT. ONE MISSING FASTENER ON OUTBOARD LOWER SIDE FITTING (P/N: 37437-01).2. FITTING, ASSY INBOARD LOWER ENGINE MOUNT. ONE MISSING FASTENER ON INBOARD LOWER SIDE OF FITTING (P/N: 37442-01) 1L72 3O3 O A7SO E9CE 5 CP22EA 20010921000622001092100062EA 2001 9 21 CA010831005 220010815G7210 GEARBOX BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA MAIN ROTOR DAMAGED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) ON RAMP AFTER M/R HEAD CHANGE MASTER CAUTION LIGHT ACTIVATED&ENGINE CHIP LIGHT ACTIVATED. ENGINEER FOUND ON REAR CHIP DETECTOR FOR ENGINE MINOR FUZZ. ENGINER CLEANED CHIP DETECTOR & REINSTALLED ENGINEER INSPECTED FILTERS & FOUND NO DISCREPANCY. A/C GROUND RUN&NO CHIP LIGHTS OCCURRED. AFTER TRACK & BALANCE. COUPLE HRS LATER ANOTHER ENGINE CHIP LIGHT. TIME MASSIVE AMOUNTS OF METAL. A/C SHUTDOWN. METAL GENERATION MAYBE COMING FROM NR 2 POWER SECTION OR COMBINING GEARBOX. ONCE POWER SECTION REMVD BEARING CAGE OF NR 5 DUPLEX BEARING IN TRANSITION AREA OF POWER SECTION&COMBINING GEARBOX. COMBINING GEARBOX REPLACED. TSO OF COMBINING GEARBOX 2126 HRS. 1G71 4U4 U H4SW E22EA 20010921000652001092100065CE 2001 9 21 CA010831006 120010817G2820 TUBE CESSNA206 U206G 2073356CE CONT O550 IO550F 17042SO MCAULYD3A34 D3A34C402 GL FUEL SYSTEM LEAKING W L ABORTED APPROACH KRJFLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) NR 5 CYLINDER FUEL DISTRIBUTION TUBE RUPTURED DURING CRUISE FLIGHT. TUBE BREAK IS AT THE CONNECTION TO FUEL DISTRIBUTOR VALVE. CONNECTION POINT A CYLINDER REMAINED INTACT. FAILURE OCCURRED AT FLANGE END WHERE TUBE FLARE END IS BRAZED TO TUBE ASSY. NO POSITIVE CAUSE IDENTIFIED. VIBRATION AND CYCLES MAY HAVE CONTRIBUTED TO FAILURE. POSSIBLE FLAW WITH BRAZING OF TUBE ASSY. 1H71 3O3 O A4CE E3SO 5 CP47GL 20010921000682001092100068CE 2001 9 21 CA010831007 120010803G7120NAS148A94 BOLT CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL ENGINE MOUNT DAMAGED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 3800 (CAN) ON ENGINE REMOVAL, MAINTENACE FOUND ENGINE MOUNT BOLT PART NO. NAS 148A94 (S3461-64) AT LEFT, LOWER ENGINE MOUNT BRACKET. (ITEM 27)- THREADBOUND DUE TO WASHER PART NO. MS20002C8 NOT INSTALLED AT FACTORY ASSEMBLY. MAINTENACE ALSO FOUND INCORRECT WASHERS PART NO. AN960-616L INSTALLED ON ENGINE MOUNT BOLTS AT RIGHT LOWER BRACKET (ITEM 28) AND TOP CENTER BRACKET (ITEM 26)- INSTEAD OF WASHERS PART NO. MS20002C8. THE THREE REMAINING CESSNA 208B AIRCRAFT IN THE FLEET WERE INSPECTED FOR THE SAME CONDITION WITH NO DISCREPANCIES NOTED. 1H71 3T3 T A37CE E4EA 5 CP60GL 20010917000302001091700030WP 2001 9 17 CA010831010 120010822G6210369D21100523 MAIN ROTOR HUGHES 369D21200503HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL LWR SKIN ROOT CRACKED W O OTHER O OTHER ININSP/MAINT 1 CA 3340 2544 (CAN) 1 1/2"- 2" CHORDWISE CRACKS IN LOWER ROOT DOUBLER ADJACENT TO OUTBOARD END OF ROOT END FITTING. TWO BLADES FROM SAME SET WITH SIMILAR CRACKS S/N'S 009999-K068,-K070. *TORQUE EVENTS CALCULATED BY TSNX20 (REF: BOEING SERVICE BULLETIN SB 369D195R3) 1G71 3U3 U H3WE E4CE 20010921000742001092100074CE 2001 9 21 CA010831012 120010802G2434 BRUSHES CESSNA 991059111 CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA ALTERNATOR FAILED W O OTHER HW ELECT. POWER LOSS-50 PC INADEQUATE Q C TXTAXI/GRND HDL 1 CA 472 A149997 (CAN) - AIRCRAFT ALTERNATOR FAILED. - ALTERNATOR INTERIOR INSPECTION REVEALED A BROKEN BRUSH BLOCK ASSEMBLY CAUSED BY A INCORRECT INSTALLATION. 1H71 3O3 ONT3A12 1E10 20010921000752001092100075CE 2001 9 21 CA010831013 120010816G24349910591111 BRUSHES CESSNA 9910591111 CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA ALTERNATOR BROKEN W K NONE HW ELECT. POWER LOSS-50 PC INADEQUATE Q C TXTAXI/GRND HDL 1 CA 445 A150018 (CAN) - AIRCRAFT ALTERNATOR FAILED. - ALTERNATOR INTERIOR INSPECTION REVEALED A BROKEN BRUSH BLOCK ASSEMBLY CAUSED BY A INCORRECT INSTALLATION 1H71 3O3 ONT3A12 1E10 20010921000762001092100076EU 2001 9 21 CA010831014 120010824G56109598110108 WINDSHIELD PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL COCKPIT FAILED W C ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CA 132 (CAN) ON TAKE-OFF AT FT ST. JOHN, CO-PILOTS WINDSHIELD SHATTERED JUST AT ROTATION, PILOT ABORTED TAKEOFF AND TAXIED BACK TO RAMP. WINDSHIELD WAS REPLACED 132 HRS PRIOR. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010921000772001092100077EU 2001 9 21 CA010831016 120010828G77125771112104 TUBE PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL GEARBOX OIL LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) PART TIME NOT KNOWN. METAL CLAMP ON LINE CHAFED THROUGH OIL LINE.TUBE WAS FOR TORQUE TRANSDUCER. FIG 01, 77-10-00 ITEM 10 MOST OF THESE LINES HAVE CLAMPS WITHOUT RUBBER INSERTS. THEY ARE METAL ON METAL. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010921000792001092100079NE 2001 9 21 CA010831018 220010831G7314RG9570R1M COVER PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL FUEL PUMP LOOSE W K NONE K FLUID LOSS ININSP/MAINT 1 CA 2761 2761 (CAN) COVER SCREWS WERE FOUND WITH INSUFICIENT TORQUE AS PER FOCA AD HB 2001-500. COVER SCREWS WERE TORQUED TO SPECIFICATIONS AND SAFTIED AS PERSB28-009NO SIGNS OF FUEL LEAKAGE OR EXTRUDED GASKET MATERIAL WAS FOUND. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010921000802001092100080NE 2001 9 21 CA010831019 220010824G7314RG9570R1 PUMP PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL ENGINE LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA 1020 (CAN) INSPECTION OF THE ENGINE DRIVEN FUEL PUMP AS PER PILATUS AWD HB2001-500 AND SB 28-009 REVEALED THAT FUEL PUMP WAS LEAKING AND EXTRUDED GASKET MATERIAL WAS FOUND. THE TORQUE OF THE SCREWS WAS CHECKED. 1/8TH TO 1/4 TURNS WERE NEEDED TO TORQUE THE SCREWS TO THE SPECIFIED TORQUE OF 23 IN LB TO 25 IN LB. THE PUMP WAS REPLACED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010921000822001092100082NM 2001 9 21 CA010905008 120010717G2540214861 SLEEVE BOEING747 747475 NM GE CF6 CF680C2B6F 30025NE DUMP VALVE SHORTED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) A/C 381 M FOUND DURING UNRELATED ROUTINE MAINT IN AREA. EVIDENCE OF FIRE DAMAGE CAUSED BY SHORTED LEAD AT WASTER TANK DUMP VALVE HEATER SLEEVE. FIRE TRACK WAS FOLLOWED FROM SOURCE FWD THROUGH LIGHTNING HOLE OF ADJACENT STRUCTURE, & UPWARD ALONG FRAME TO STRINGER 3 FEET FROM AFT DUMP VALVE LOCATION. INSP OF STRUCTURE CARRIED OUT, NIL DEFECTS TO STRUCTURE FOUND. INSULATION BLANKETS REMVD & REPLD DUE TO BURN DAMAGE OF OUTER LAYER. AREA CLEANED OF DUST. AREA RPTECTED. A/C RELEASED FOR SERVICE. BOEING FIELD REP INFORMED. AIR CANADA ENGINEERING TO INVESTIGATE & LIASE WITH BOEING CUSTOMER REPS FOR SOLUTION & FURTHER INSP REQMTS. FLEET CAMPAIGN TO INSPECT AFFECTED AREA IS UNDER CONSIDERATION. 2L74 4F4 FRTA20WE E13NE 20010921000852001092100085NE 2001 9 21 CA010906006 220010902G7320311989203 FUEL CONTROL PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL ENGINE INTERMITTENT W C ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 CA 2556 2556 (CAN) A/C IN QUESTION IN RED LAKE & ON ITS BACKTRACK.EVERYTHING INDICATING NORMAL.FLT IDLE ASKED FOR & WHEN LEVER SET FOR FLT IDLE IT NOTICED GEN 1 LIGHT CAME ON. ENGINE IN PROCESS OF FLAME OUT & CONTINUED UNTIL STOPPED. MAINT CONTACTED & INSP ENGINE FROM FRONT TO BACK WITH ASSISTANCE OF PRAT REP. BOROSCOPE, CHIP DETECTOR INSP, RUNUPS, NOTHING VIABLE COULD BE FOUND TO EXPLAIN EVENTS EXCEPT THAT IT WAS FCU AS IT CNTLS FUEL. PRATT BACKED UP THINKING & FCU REPL. THE STARTER GEN REPLACED ALSO. ALL GROUND RUNS CHECKED WITHIN MFGS PARAMETERS.A/C FERRIED TO THUNDER BAY & ENGINE REPLACED FOR OTHER REASONS. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010921001032001092100103EU 2001 9 21 CA010906017 120010719G55305357500020000 BOLT AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE VERTICAL STAB LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING H-CHECK AND ACCOMPLISHING AIRCRAFT MAINTENANCE MANUAL TASK 53-51-00-210-009 FOUND THREE BOLTS LOOSE AS WELL AS CORRODED NUT FOR THE TAIL CONE ATTACHMENT.BOLTS RETORQUED AND NUTS REPLACED. 2L72 4F4 FRTA28NM E29NE 20010921001042001092100104NM 2001 9 21 CA010906019 120010729G801297910211 VALVE BOEING737 737275 1384485NM PWA JT8 JT8D17 52049NE STARTER FAILED W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CA (CAN) TWO AIR TURN BACK DUE TO A #1 START VALVE OPEN LIGHT ILLUMINATED DURING FLIGHT. ACCOMPLISHED #1 ENGINE FAILURE SHUTDOWN TWICE.AFTER THE FIRST INCIDENT, THE STARTER, START VALVE AND ACTUATOR PRESSURE SWITCH WERE CHANGED, & THE SECOND TIME THE START VALVE & THE PRESSURE SWITCH WAS REPLACED. IT WAS DETERMINED THAT THE FIRST START VALVE WAS A ROGUE UNIT. THE FINAL FIX WAS THE REPLACEMENT OF THE STARTER VALVE. 2L72 4F4 F A16WE E2EA 20010921001052001092100105NE 2001 9 21 CA010906020 220010807G72301211313010 ACTUATOR AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE ENGINE FAILED W E ENGINE SHUTDOWN DR INFLIGHT SEPARATION PARTIAL RPM/PWR LOSS DEDESCENT 1 CA (CAN) COMPRESSOR STALL 25 MINUTES BEFORE LANDING IN TORONTO, AIRCRAFT DECLARED AN EMERGENCY LANDING, THE CREW RE-STARTED THE ENGINE AND LANDED SAFELY WITH NO INCIDENT. AIRCRAFT REMOVED FROM SERVICE FOR TROUBLESHOOTING AND RECTIFICATION.FOUND TO BE THE VARIABLE STATOR ACTUATOR AT FAULT.REPLACED THE VARIABLE STATOR ACTUATOR. 2L72 4F4 FRTA28NM E29NE 20010921001072001092100107NE 2001 9 21 CA010907001 120010826G6230 LINK SKRSKYS76 S76A 8143006NE MAIN ROTOR WRONG PART W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) DURING A MAIN GEARBOX BUILDUP AND PRIOR TO INSTALLATION OF THE STATIONARY SCISSORS ASSEMBLY, THE ENGINEER NOTICED THE UPPER LINK OF STATIONARY SCISSORS WAS ASSEMBLED 180 DEGREES OUT OF POSITION. THE ENGINEER CORRECTED THIS CONDITION PRIOR TO INSTALLING THE SCISSORS ASSEMBLY ON THE MAIN GEARBOX. UNCORRECTED, THIS WOULD LIMIT THE VERTICALMOVEMENT (DOWN) OF THE SWASHPLATE. 1G72 3U H1NE 20010921001312001092100131WP 2001 9 21 CA010907007 120010823G6210369A10045 PIN HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL M/R BLADE SHEARED W K NONE O OTHER ININSP/MAINT 1 CA 5295 (CAN) WHILE CARRYING OUT HIS DAILY INSPECTION, THE PILOT NOTICED THE NUT LOOSE ON THE BLADE PIN UPON INSPECTION THE THREADED PORTION OF THE BLADE PIN WAS SHEARED. 1G71 3U3 U H3WE E4CE 20010921001342001092100134CE 2001 9 21 CA010907010 120010823G531305131324 STRINGER CESSNA172 172K 2072430CE LYC O320 O320E2D 41508EA MCAULY1A175 1A175* GL FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 13201 (CAN) DURING ROUTINE MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE RIGHT HAND ENGINE RAIL WAS CRACKED. P/N 0513132-4 STRINGER ASSEMBLY IN FUSELAGE FRONT SECTION STRUCTURE ASSEMBLY WAS REPLACED. 1H71 3O3 ONT3A12 E274 5 NP857 20010917000332001091700033CE 2001 9 17 CA010907020 120010719G5230NAS561F824 ROLL PIN CESSNA 208B CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL ROLL PIN BENT W K NONE O OTHER CRCRUISE 1 CA 13231 208B0305 (CAN) IT APPEARS SOMEONE TRIED TO UNLATCH THE UPPER CARGO DOOR WITHOUT PUSHING (ITEM #41) RELEASE KNOB TO RELEASE THE INNER HANDLE FROM THE LOCK PLATE (ITEM #46) EXCESSIVE FORCE WAS APPLIED THUS DAMAGING MECHANISM (ROLL PIN ITEM #2), WITH THIS CONDITION, IF THE INNER HANDLE WAS POSITIONED IN THE LOCK PLATE THEN THE LOCK PINS WOULD BE RETRACTED ALLOWING THE DOOR TO COME OPEN. DOOR WARNING SYSTEM CHECKED AFTER REPAIRS AND FUNCTIONED NORMALLY. PILOT REPORTED THAT DOOR WARNING LIGHT CAME ON JUST PRIOR TO OPENING. 1H71 3T3 T A37CE E4EA 5 CP60GL 20010921001432001092100143EA 2001 9 21 CA010910003 220010822G72303013511 COMPRESSOR WHEEL DHAV DHC6 DHC6100 EA PWA PT6 PT6A20 52043EA ENGINE FAILED W O OTHER MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 CA 3543 (CAN) HOT START LACK OF POWER.HOT SECTION REMOVED FROM POWER OLANT. SERVICEABLE HOT SECTION INSTALLED AIRCRAFT RUN CARRIED OUT. FOUND SATISFACTORY. SHROUD P/N 3020259STATOR ASSY P/N 3018490 1H72 3T3 T A9EA E4EA 20010924000122001092400012NM 2001 9 24 CA010910007 120010624G3220141T991113 SPRING BOEING767 767233 NM PWA JT9 JT9D7R4D 52054NE SPIN BRAKE MISSING W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ON WALK AROUND IN YYZ, FOUND RIGHT HAND NOSE WHEEL SPIN BRAKE SPRING MISSING. INSTALLED SPIN BRAKE SPRING. 2L72 4F4 FRTA1NM E3NE 20010921000212001092100021NM 2001 9 21 CA010910009 120010810G8011449188 SEAL PWA JT8D17A BOEING737 7372T7 1384482NM PWA JT8 JT8D17A 52049NE STARTER LEAKING W O OTHER O OTHER CRCRUISE 1 CA 702788 (CAN) NR 2 LOW OIL PRESSURE FLICKERING FOR THE LAST 4 MINUTES OF FLIGHT WITH THE PRESSURE GAUGE IN AND OUT OF CAUTION RANGE. TEMPERATURE NORMAL, ENGINE OPERATED AT REDUCED THRUST AND SHUTDOWN AFTER LANDING. FOUND TO BE THE STARTER DRIVE PAD CARBON SEAL TO BE LEAKING (AROUND 200 ML/15 MINUTES). REPLACED SEAL. 2L72 4F4 FRTA16WE E2EA 20010924000142001092400014SW 2001 9 24 CA010911002 120010910G6330209040110015 STUD BELL 212040001059BELL 212 212 1181420SW PWA PT6T PT6T3B 52045NE TRANSMISSION MISSING W O OTHER O OTHER NRNOT REPORTED 1 CA ABW50227 (CAN) FOUND BOKEN OFF STUD ON THE LIFT LINK TRANSMISSION MOUNT. ON THE TRANSMISSION THE LEFT REAR STUD HAD BROKEN OFF. THEY FOUND THIS DEFECT WHILE CHANGING A SERVO. 1G71 4U4 U H4SW E22EA 20010924000152001092400015SW 2001 9 24 CA010912003 120010819G5302206031329103S FITTING BELL 206 206L 1181522SW ALLSN 25OC 250C20R GL TAILBOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ROUTINE INSPECTION UPPER LEFT TAIL ATTACH FITTING FOUND CRACKED.REPLACED AS PER BELL STRUCTURAL REPAIR MANUAL 6-214, BUT NUMEROUS REPORTS OF CRACKS IN THIS LH UPPER FITTING AREA OF TAILBOOM/FUSELAGE INTERFACE. 1G71 3U3 U H2SW E4CE 20010924000172001092400017CE 2001 9 24 CA010912007 120010820G531050420013451 CROSSBEAM BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA HARTZLHCB3T HCB3TN3 GL LWR FWD SILL CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2617 2617 (CAN) IT WAS FOUND THAT AN INDIVIDUAL HAD REMOVED MATERIAL FROM THE DOUBLER & CROSS-TIE IN AN EFFORT TO ELIMINATE CONTACT WITH THE EMERGENCY EXCAPE HATCH.CRACKS WERE FOUND PROPAGATING FROM THE SHARP CORNER OF THIS RADIUS. WE ALSO DISCOVERED DURING THE REMOVAL OF THIS PART, THAT IT WAS INSTALLED WITH A PRE LOAD DURING THE RIVETING PROCESS. I AM SURE THIS HELPED THE CRACKS TO FORM.NO REFERENCES OR DATA WAS FOUND TO SUPPORT THE WORK DONE, BUT IT CLEARLY DID NOT FOLLOW STANDARD PRACTICES. 1L72 3T4 TRT3A20 E4EA 6 CP15EA 20010924000262001092400026 2001 9 24 CA010912016 420010912G3425 HARNESS PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL FLIGHT CONTROL CHAFED W K NONE O OTHER ININSP/MAINT 1 CA 3197 3197 (CAN) WHILE MOVING THE ELEVATOR CONTROL, A SLIGHT "CATCH" COULD BE FELT.INVESTIGATION REVEALED THAT WHEN PULLED BACK, THE AILERON CROSSOVER TIE ROD P/N 941.93.43.415 ON THE CONTROL COLUMN, CAME INTO CONTACT WITH THE WIRING HARNESS ON THE BACK OF THE MULTI FUNCTION DISPLAY (MFD). THE SCREWS HOLDING THE MFD CONNECTOR TO THE BACK OF THE MFD TRAY WERE ALSO PULLED OUT. THE WIRING HARNESS OF THE MFD WAS INSPECTED FOR CHAFFING AND REPOSITIONED AND FASTENED. NEW SCREWS WERE INSTALLED TO HOLD THE MFD CONNECTOR TO THE TRAY. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010924000272001092400027CE 2001 9 24 CA010912017 120010904G534204321671 STIFFENER CESSNA150 150J 2071820CE LYC O320 O320E2D 41508EA MCAULY1C172 1C172TM GL STAB ATTACH CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 4671 (CAN) COMMON PROBLEM ON OLDER CESSNA 150 SERIES, MANUFACTURER HAS BEEN REPLACED THIS PART WITH A NEW IMPROVE PART P/N 0432169-1 ALSO INCLUDING NEW IMPROVE BULKHEAD ASSY P/N 0412177-2. 1H71 3O3 O 3A19 E274 5 NP910 20010924000282001092400028WP 2001 9 24 CA010912018 120010905G6520369D25400B GEARBOX HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL TAIL ROTOR MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 13075426 (CAN) DURING A HELICOPTER ENGINE PERFORMANCE CHECK AT 2000 FT CRUISE, THE TAIL ROTOR GEARBOX CHIP LIGHT ILLUMINATED AND STAYED LIT. AFTER LANDING AT BASE, THERE WAS METAL FLAKES PRESENT ON CHIP DETECTOR. T/R GEARBOX WAS FLUSHED, CHIP DETECTOR CLEANED, & RE-INSTALLED. AIRCRAFT WAS GROUND RUN FOR 10 MIN AND SHUTDOWN.T/R GEARBOX CHIP DETECTOR REMOVED AGAIN.METAL WAS FOUND ON DETECTOR - T/R GEARBOX REMOVED FROM AIRCRAFT. 1G71 3U3 U H3WE E4CE 20010924000292001092400029SW 2001 9 24 CA010913001 120010904G6210 TRIM TAB BELL 407015001117BELL 407 407 SW ALLSN 250C 250C47B GL M/R BLADE DEBONDED W K NONE O OTHER ININSP/MAINT 1 CA 400 400 A348 (CAN) DURING SCHEDULED AIRFRAME PERIODIC INSP TRIM TAB ON PARTICULAR MAIN ROTOR BLADE FOUND TO HAVE SEVERE DEBONDING WHICH INITIALLY SHOWED UP AS CRACKS IN FILLER MATERIAL AROUND TRIM TAB EDGES. CLOSER INSP REVEALED SEVERE DEBONDING & COMPROMISE OF TRIM TAB ATTACHMENT SECURITY. MAIN ROTOR BLADE REPLACED WITH NEW FROM BELL HELICOPTER. MAIN ROTOR BLADE S/N A-348 HAD TOTAL TIME SINCE NEW OF 2052.5. IT HAD BEEN INSP & REPLACED AT BELL HELICOPTER AT TOTAL TIME SINCE NEW OF 1652.2 AT WHICH TIME TRIM TAB REPLACED. (TIME SINCE REPAIR & TRIM TAB REPLACED 400.3). IT IS QUITE COMMON TO SEE MINOR CRACKING IN FILLER MATERIAL SURROUNDING TRIM TAB. 1G71 3U3 UO H2SW E1GL 20010924000302001092400030CE 2001 9 24 CA010913004 120010912G324399123057 VALVE CESSNA500 S550 2076607CE PWA JT15 JT15D4 52112NE BRAKE FAILED W O OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 CA 7984 (CAN) FOLLOWING AN UNEVENTFUL LANDING AND WHILE TAXING AFTER THE LANDING ROLL OUT, THE CREW ENCOUNTERED A BRAKE FAILURE AND HAD TO APPLY THE EMERGENCY BRAKE IN ORDER TO STOP THE AIRCRAFT. MAINTENANCE TROUBLESHOOTING AND INSPECTION OF THE SYSTEM DETERMINED THAT THE POWER BRAKE -ANTI SKID VALVE ASSEMBLY HAD FAILED. THE VALVE ASSY WAS REPLACED AND ALL TESTS CONDUCTED IN ACCORDANCE WITH THE MM AND THE AIRCRAFT RELEASED. 1L72 4F4 FRTA22CE E1NE 20010924000312001092400031CE 2001 9 24 CA010914002 120010824G534305411212 CASTING CESSNA182 182A 2072704CE CONT O470 O470L 17026SO MCAULY2A34C 2A34C66 GL REAR GEAR CUTOUTCRACKED W K NONE O OTHER ININSP/MAINT 1 CA 6293 (CAN) SUPPORT CASTING HAD CRACK FROM RADIUS OF CUTOUT FOR GEAR REARWARD. 0541153 U-BOLT WAS ALSO BROKEN AND REPLACED. 1H71 3O3 ONT3A13 E273 5 CP3EA 20010924000422001092400042EU 2001 9 24 CA010914004 120010910G2750ONL312014 BOLT Z4243430000 ZLIN 242 Z242L 9970204EU LYC O360 AEIO360A1B6 41514EA FLAP BELLCRANK BENT W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A 100/500 HOUR INSPECTION THE LT FLAP BELLCRANK BOLT (P/N ONL3120.146X77)WAS FOUND TO BE BENT. THE BOLT WAS REPLACED WITH A NEW ONE. IT IS SUSPECTED THAT A STUDENT PILOT EXTENDED THE FLAPS ABOVE THE MAXIMUM SPEED ALLOWED FOR FLAP EXTENSION. THE MAINTENANCE SCHEDULE ALREADY HAS AN ADDITIONAL INSPECTION ON THE FLAP BOLTS AND THE INSTRUCTORS AND STUDENTS WERE AGAIN REMINDED OF THE PROPER PROCEDURE USING THE FLAPS. 1L71 3O3 O0 A76EU 1E10 20010924000592001092400059EU 2001 9 24 CA010917001 120010913G2434HEDCR132200 BRUSHES BOSCH 5243212158 PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL GENERATOR WORN W K NONE HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 CA 3296 3296 (CAN) THE NR 2 GENERATOR CAUTION LIGHT ILLUMINATED ON CAWS PANEL. EIS INDICATED THAT NR 2 GENERATOR HAD COME OFF LINE.THE PILOT THEN RE-SELECTED GENERATOR SWITCH TO ON POS,&HAD SAME SEQUENCE OF EVENTS OCCUR AGAIN. NR 2 GENERATOR WE AS LEFT OFF LINE FOR REMAINDER OF FLT. GENERATOR BRUSHES WERE REMOVED, & INSPECTED BY MAINTENACE STAFF. BRUSHES WERE FOUND TO HAVE WORN BEYOND SERVICEABLE LIMITS. ONE BRUSH WORN TO POINT WERE CONTACT NOT OCCURRING WITH ARMATURE:THE GENERATOR PREVIOUS INSTALLATION ON A/C REMOVED DUE TO (4) PREMATURE FAILURES OF BRUSH ASSY.THE CURRENT GENERATOR INSTALLED AS "NEW". IS 1ST SET OF BRUSHES TO FAIL ON INSTALLED GENERATOR. MAINTENANCE STAFF HAS NOW IMPLEMENTED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010924000832001092400083EU 2001 9 24 CA010917006 120010917G2434HEDCR132200 BRUSHES 9789601090 PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL GENERATOR WORN W H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CRCRUISE 1 CA 3373 NA (CAN) NR 2 GENERATOR FAILED IN CRUISE FLIGHT. NR 2 GENERATOR WAS TURNED OFF, AND AIRCRAFT RETURNED TO BASE. INVESTIGATION REVEALED NR 2 GENERATOR BRUSHES WORN. NR 2 GENERATOR BRUSH HOLDER ASSEMBLY P/N 978.96.01.090 REPLACED WITH NEW, AIRCRAFT GROUND RUN AND CHECKED SERVICEABLE. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010925000902001092500090SW 2001 9 25 CA010921005 120010902G2910MS28775212 O-RING BELL 212076007003BELL 205 205A1 1181414SW LYC T53 T5313B 41549NE PISTON SPLIT W A UNSCHED LANDING K FLUID LOSS HOHOVERING 1 CA 615 VH9812 (CAN) O-RING ON ACCUMULATOR SPLIT CAUSING HYDRAULIC FLUID LOSS. SUBSEQUENTLY THE PILOT TURNED THE #2 HYDRAULIC SYSTEM OFF AND LANDED THE AIRCRAFT. FURTHER INVESTIGATION REVEALED THAT THE #2 HYDRAULIC RESERVOIR WAS COMPLETELY DRY. THE ACCUMULTOR WAS DISASSEMBLED AND INSPECTED REVEALING THAT THE PISTON O-RING HAD SPLIT THE O-RING WAS REVEALED AND THE REASSEMBLED ACCUMULATOR RETURNED TO SERVICE. 1G71 4U4 U H1SW E17EA 20020114000942002011400094NE 2002 1 14 CA010925001 220010916G7200 ENGINE PWA PT6 PT6A67B 52043NE NACELLE MAKING METAL W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) SILVER PLATLETS WERE FOUND IN AN OIL SAMPLE TAKEN AT THE 100 HOUR MARK OF NEWLY INSTALL ENGINE. ENGINE WAS FLUSHED AND FILTER REPLACED. AFTER ANOTHER 40 HOURS OF SERVICE ON THE ENGINE IT WAS INSPECTED AGAIN AND UPON VISUAL INSPECTION IT WAS FOUND THAT THERE WAS STILL SILVER PLATLETS IN THE OIL FILTER AND WAS NOW GENERATING FERROUS METAL. IT WAS INITIALLY BELIEVED THAT IT WAS JUST JUNK FROM ENGINE ASSEMBLY. THIS CONFIRMED THAT THE ENGINE WAS INDEED GENERATING METAL. ENGINE REMOVED AND SERVICIBLE ENGINE INSTALLED. 4 T E26NE 20020114000952002011400095 2002 1 14 CA010926001 420010924G3421 INDICATOR PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL EADI / EHSI FAILED W O OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 CA (CAN) CREW REPORTED JUST PRIOR TO LEVELING AT FL250, THE NR 1 EADI (UPPER PILOT WAS FLAGGED WITH "ATITUDE FAIL" .SUBSEQUENTLY, THE FLIGHT DIRECTOR AND AUTOPILOT KICKED OFF LINE.CREW SELECTED NR 2 AHRS AND FLIGHT CONTINUED UNEVENTFULLY TO THE NEXT DESTINATION. ON THE SUBSEQUENT START THE NR 1 AHRS WAS RESELECTED WITH NO PROBLEMS. FAILURE COULD NOT BE DUPLICATED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020114001012002011400101EU 2002 1 14 CA010927001 120010926G32305322012072 DRAG LINK PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL NLG BROKEN W O OTHER DJ INFLIGHT SEPARATION WARNING INDICATION DEDESCENT 1 CA (CAN) FAILURE OF PN 532.20.12.072 NOSE GEAR DRAG LINK ON 25TH JUNE 2001. SENT IT OUT FOR INDEPENDENT FAILURE ANALYSIS & CAME BACK WITH CORROSION PITTING AS CAUSE FOR COMPROMISED STRUCTURAL STRENGTH. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020114001052002011400105CE 2002 1 14 CA011001002 120010928G30972601048200 CONNECTOR CESSNA208 208 2073702CE PWA PT6 PT6A114 52043NE MCAULY3AF34C3GFR34C703 GL ELECTRICAL PANELBURNED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING AN INSPECTION OF THE AREA BEHIND THE ELECTRICAL PANEL BY THE PILOTS LEFT FOOT. A WIRE CONNECTOR WAS FOUND BURNED. THE WIRE CONNECTOR BETWEEN THE PROP ANTI-ICE WIRE HA-20 EXITING FROM THE CIRCUIT BREAKER PANEL AND THE WIRE HA-21 GOING TO THE PROP TIMER WAS FOUND BURNED AND DISTORTED FROM HEAT. ON CLOSER EXAMINATION IT WAS FOUND THE TERMINAL ON THE WIRE HAD BEEN CRIMPED IMPROPERLY AND WAS ALLOWED TO MAKE CONTACT WITH THE PLACTIC CONNECTOR HOUSING. THE CONNECTOR WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1H71 3T3 TNTA37CE E4EA 5 CP60GL 20020114001142002011400114GL 2002 1 14 CA011002001 220010924G732123034702 FCU BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE FAILED W A UNSCHED LANDING X ENGINE FLAMEOUT NRNOT REPORTED 1 CA (CAN) FUEL CONTROL WAS REPAIRED. FUEL CONTROL WAS INSTALLED ON BELL 206B DUE TO THE OLD ONE NEARING OVERHAUL. AFTER GROUND RUNS A TEST FLIGHT WAS CARRIED OUT ON AIRCRAFT. AFTER THE TEST FLIGHT THROTTLE WAS DECREASED TO FLIGHT IDLE WHEN THE ENGINE ALMOST FLAMED OUT. ON THE THROTTLE ROLL DOWN THE NG RPM WENT TO 25 PERCENT (NORMAL IDLE SPEED 61PERCENT TO 63 PERCENT NG) NG RPM WOULD NOT RESPOND TO THROTTLE MOVEMENT. INSTALLED ANOTHER FUEL CONTROL AND DEFECT WENT AWAY. 1G71 3U3 U H2SW E4CE 20020114001162002011400116SW 2002 1 14 CA011002002 120010917G77126856362 PISTON RROYCE 6894171 BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL TORQUE METER CLOGGED W K NONE O OTHER ININSP/MAINT 1 CA CAG800082 (CAN) TORQUE INDICATOR ON THE GROUND READ 70 PERCENT TORQUE THEN CLIMBED TO 90 PERCENT TORQUE WITHOUT ADVANCING THE THROTTLE OR INCREASING THE POWER. TORQUE INDICATOR REPLACED, DEFECT DID NOT GO AWAY. REPLACED THE ENGINE GEARBOX. IT WAS NOTED THAT THE BLEED ORFICE WAS PLUGGED WHICH WOULD LEAD TO AN ADVANCE OF TORQUE INDICATION WITH NO INCREASE IN POWER. 1G71 3U3 U H2SW E4CE 20020114001182002011400118SW 2002 1 14 CA011002003 120010915G632023034787 BEARING RROYCE 6886442 BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL M/R GEARBOX FAILED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA CAG34833 (CAN) PILOT REPORTED A CHIP LIGHT & A LOUD GRINDING NOISE COMING FROM THE ENGINE REGION. THE PILOT MADE A PRECAUTIONARY LANDING TO A LANDING SIGHT. THE CHIP PLUGS WERE REMOVED & FOUND LARGE AMOUNT OF FLAKES. ON THE INVESTIGATION FOUND THE TWO AND A HALF BEARING FAILED IN THE ENGINE GEARBOX. THE GEARBOX HAS 12264.1 TSN AND 2675.0 TSO. WHEN THE 2 1/2 BEARING FAILED IT CUT A GROOVE IN THE SPUR ADAPTER GEAR SHAFT RACE. 1G71 3U3 U H2SW E4CE 20020114001212002011400121SO 2002 1 14 CA011002004 120010927G3260 BRACKET PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA RT MLG UPLOCK FAILED W L ABORTED APPROACH J WARNING INDICATION LDLANDING 1 CA 11788 (CAN) RT MAIN GEAR FAILED TO EXTEND. THIS WAS DUE TO RIVETS ATTACHING UPLOCK BRACKETS P/N 40616-01 & 40616-02 SHEARING. THIS MAY HAVE BEEN DUE TO CORROSION. THIS ALLOWED W8 OF LDG GEAR TO PULL RIVETS THROUGH 2 ANGLES P/N 40625-00. AS A RESULT OF THIS, A MISALIGNMENT OF UPLOCK HOOK WITH UPLOCK ROLLER CAUSED UPLOCK HOOK TO JAM. THIS PREVENTED GEAR FROM EXTENDING. PILOT WAS ABLE TO FREE GEAR BY APPLYING POSITIVE & NEGATIVE G LOADS ON GEAR. GEAR THEN EXTENDED NORMALLY. UPLOCK BRACKETS HAD BEEN MODIFIED WHEN BOUNDARY LAYER RESEARCH STC-SA 00202SE SUPER CHIEF II WAS INST & AGAIN WHEN BOUNDARY LAYER RESEARCH SB- BLR 105 WAS COMPLIED WITH. 1L72 3O3 O A20SO E14EA 20020114001222002011400122CE 2002 1 14 CA011002005 120011020G2897 WIRE BEECH 99 99 1154002CE PWA PT6 PT6A27 52043EA COCKPIT PANEL BURNED W C ABORTED TAKEOFF BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TOTAKEOFF 1 CA (CAN) DURING TAKE OFF THE CREW OBSERVED A LOW FUEL PRESSUE LIGHT INDICATION ACCOMPANIED BY THE TRIP OFF OF THE CIRCUIT BREAKER SWITCH FOR THE LT SECONDARY PUMP.SMOKE WAS EMINATING FROM BEHIND THE LOWER LEFT PANEL AT THE SAME TIME. THE TAKE OFF WAS ABORTED AND THE AIRCRAFT WAS SHUTDOWN ON THE RUNWAY. MAINTENANCE FOUND A TERMINAL ON THE CB/SWITCH THAT APPEARED TO BE LOOSE WHICH IS BELIEVED TO GENERATED THE WIRING OVERTEMP. THE DAMAGED WIRE AND CB/SWITCH WERE REPLACED.THE CB WAS EXAMINED AND FOUND TO HAVE NO INTERNAL ANOMOLIES 1L72 3T4 T A14CE E4EA 20020115000012002011500001SW 2002 1 15 CA011002006 120010916G6220D2B20000B LIMITER KAMOV KA32 KA32A1 SW MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACK DISCOVERED DURING POST FLIGHT INSPECTION. FURTHER INVESTIGATION FOUND LEAD AND LAG DRAG HINGE BEARINGS WERE VERY STIFF IN TWO OF THE 3 ROTOR HEAD SLEEVES. 1G72 4U NC 20020114002292002011400229EA 2002 1 14 CA011002007 220010916G75303027249 BLEED VALVE DHAV DHC6 DHC6100 2802610EA PWA PT6 PT6A20 52043EA ENGINE FAILED W D RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CA (CAN) DROP IN ENGINE TORQUE, PROP LEVER PUSHED FORWARD, TEMPED OUT AT 35 LBS TORQUE. 1H72 3T3 TRTA9EA E4EA 20020115000022002011500002SW 2002 1 15 CA011002009 120010727G53022060313291 FITTING BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL TAILBOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 12293 (CAN) TAILBOOM FITTING LT FUSELAGE SIDE FOUND CRACKED VERTICALLY 1 INCH IN LENGTH. NEW PART ORDERED AND INSTALLED. 1G71 3U3 U H2SW E4CE 20020115000032002011500003CE 2002 1 15 CA011002010 120010908G531212128582 BULKHEAD CESSNA206 206CESSNA 2073302CE CONT O520 IO520F 17032SO MCAULY2A34C D2A34C58 GL FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACKS IN AFT FUSELAGE BULKHEAD. 1H71 3O3 O A4CE E5CE 5 CP3EA 20020115000042002011500004SO 2002 1 15 CA011003001 120011002G6120B3807 NUT HARTZL HCE2YR2RBS PIPER PA23 PA23250 7102308SO LYC O540 IO540* 41532EA HARTZLHCE2Y HCE2YR2 GL PROPELLER MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA BP9803B (CAN) THIS IS 2ND OCCURANCE OF PROBLEM. PROP INSTALLED ON OTHER ENGINE HAD SAME PROBLEM. BOTH PROPS WERE NEW WITH ASSY DATES OF 11-13-97&12-18-97, SHIPPED 4/16/98. PROP CHECKED AS PRECAUTIONARY MEASURE: NUT IS SOLID STEEL SELF LOCKING NUT, THAT HOLDS PISTON TO PISTON ROD. IF NUT COMES LOOSE, PISTON COMES OFF OF ROD & PROP HAS UNCOMANDED FEATHER WITH NO WAY TO UNFEATHER PROP. PISTON SEALS PITCH CHANGE OIL ON ROD. OTHER PROP SER BP9804B, NUT HAD COME COMPLETELY LOOSE. PROP REMVD&CHECKED. NUT NOT LOOSE ON PISTON ROD, TORQUE OF NUT CHECKED&NO MOVEMENT FOUND. 1L72 3O3 O 1A10 1E4 5 CP9EA 20020115000052002011500005GL 2002 1 15 CA011003002 220010904G7321 BEARING BELL 47 47G4 1181030SW ALLSN 250C 250C20B 03013GL FCU FAILED W A UNSCHED LANDING J WARNING INDICATION ININSP/MAINT 1 CA 330031 (CAN) INITIAL PROBLEM ENCOUNTERED WAS A CHANGE IN IDLE SPEED. IDLE WAS ADJUSTED, AIRCRAFT WAS TEST FLOWN & NBO PROBLEMS EXISTED.NEXT DAY AIRCRAFT IDLE SPEED HAD CHANGED. IDLE WAS ADJUSTED & RIGGING CHECKED. AIRCRAFT WAS RUN & TEST FLOWN. WHILE AIRCRAFT WAS RETURNING TO SIGHT IT BEGAN N1 FLUCTUATIONS. THE PILOT LANDED & PULLED COLLECTIVE, FLUCTUATION STOPPED. RETURNED A/C TO A MAINTENANCE FACILITY. AT THIS TIME HE HAD TO REDUCE TO THROTTLE TO PREVENT ENGINE OVERSPEED. FUEL CONTROL WAS REMOVED. UPON REMOVAL A LARGE AMOUNT OF METAL FLAKES FELL FROM THE F.C.U. DRIVE BEARING HAD FAILED & THE SHAFT WAS FREE FLOATING. 1G71 3O3 U 2H3 E4CE 20011015000632001101500063WP 2001 10 15 CA011003004 120010921G6310A1902 V-BELT LYC ROBSINR22 R22 7640102WP LYC O320 O320B2C 41508EA FRONT ENGINE TORN W O OTHER D INFLIGHT SEPARATION CRCRUISE 1 CA (CAN) BELTS SENT TO R.H.C. FOR INVESTIGATION. THEIR RESPONSE WAS THAT THE BELTS WERE DRY AND CAUSED SMALL CRACKS IN THE RUBBER WHERE THE BELTS ARE RIDING ON THE SHEAVE. 1G71 3O3 O H10WE E274 20020115000062002011500006EA 2002 1 15 CA011003006 220010924G7313LW18853 INJECTOR PIPER PA31 PA31 7103102SO LYC O540 TIO540J2BD 41532EA HARTZLHCC4Y HCC4YR2 GL RT ENG NR 3 CYL LOOSE W O OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 CA (CAN) PILOT REPORTED INTERMITTENT SLIGHT POWER LOSS & ROUGH RUNNING AT CRUISE POWER, GROUND POWER RUNS SHOWED NORMAL. INSPECTION OF RT ENGINE FOUND NR 3 CYLINDER FUEL INJECTOR "LOOSE" IN CYLINDER HOUSING AND FUEL STAINING AROUND THE AREA. FUEL INJECTOR THREADS & CYLINDER THREADS WERE DAMAGED. IT WAS NOTED THE FUEL INJECTOR LINES WERE PROPERLY CLMAPED AS OUTLINED IN AD 93-02-05 (SB 342). INSPECTION OF THE OTHER INJECTORS FOUND NO PROBLEMS. SUSPECT VIBRATION TO HAVE CAUSED THE INJECTOR TO LOOSEN. NO UNUSUAL VIABRATION REPORTED PREVIOUS TO THIS. 1L72 3O3 O A20SO E14EA 5 CP52GL 20020115000072002011500007SW 2002 1 15 CA011003009 120010917G5320206063107005 LEG ASSY BELL 206 206L 1181522SW ALLSN 25OC 250C20R GL ENGINE BAY CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE CARRYING OUT A 100 HOUR INSPECTION THE ENGINEER NOTICED A HILOCK COLLAR IN THE ENGINE BAY. UPON INVESTIGATION IT WAS NOTED THAT THE HI-LOCK PIN HAD CORRODED THROUGH & THE COLLAR FELL OFF. LEG ASSEMBLY REPLACED WITH NEW. 1G71 3U3 U H2SW E4CE 20020115000082002011500008SW 2002 1 15 CA011003010 120010913G6730412076670101 BEARING BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA UNIVERSAL FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AME WAS COMPLETING A DAILY INSPECTION WHEN HE PULLED THE LT SERVO BRUSH TUBE AND FELT PLAY. UPON INVESTIGATION A BEARING IN THE UNIVERSAL HAD FAILED. 1G71 4U4 U H4SW E22EA 20020115000092002011500009SO 2002 1 15 CA011003013 220010523G8520 CRANKSHAFT CESSNA337 T337H 2075733CE CONT O360 TSIO360H 17025SO MCAULY2AF34CD2AF34C308 GL ENGINE FAILED W A UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 CA (CAN) INFLIGHT CATASTRPHIC FAILURE, CRANKSHAFT, AT LEAST 2 RODS, HOLE IN TOP OF CRANKCASE, CONTINUED FLIGHT ON, REAR ENGINE TO VIKING AIRPORT (ALBERTA). 1H72 3O3 O A6CE E9CE 5 CP5EA 20020115000102002011500010CE 2002 1 15 CA011003014 120010914G27500512128 BRACKET CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULY3A32C D3A32C90 GL TE FLAPS BROKEN W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA 10325 (CAN) FLAPS WOULD NOT EXTEND PROPERLY FOR TAKEOFF. PILOT LEFT FLAPS IN UP POSITION AND RETURNED TO BASE. BRACKET IS MOUNTED TO LOWER BULKHEAD USING 4 SCREWS AND LOCKNUTS ON THE 4 MOUNT TABS. BOTH INBOARD TABS ON BRACKET HAD FAILED AT THE BEND RADIUS, ALLOWING THE BRACKET TO BEND FORWARD AND BIND THE CABLE ON THE COTTER PIN THAT KEEPS THE CABLE IN THE PULLEY GROOVE. NO OTHER DAMAGE WAS DONE TO THE STRUCTURE OR CABLE. 1H71 3O3 O 3A24 E5CE 5 CP21EA 20020115000112002011500011CE 2002 1 15 CA011003015 120010916G712085921701 SPACER J961358 CESSNA401 401B 207590ECE CONT O520 TSIO520EB 17040SO ENGINE MOUNT WRONG PART W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE INSTALLING NEW ENGINE NOTICED THAT ENGINE ATTACH BOLTS WERE TOO SHORT. PART NR OF BOLTS WERE CORRECT. ENGINE MOUNTS WERE FOUND TO BE PROBLEM. SPACERS IN ENGINE MOUNT KITS WERE WRONG LENGTH & WRONG PART NR. 1L72 3O3 O A7CE E8CE 20020115000122002011500012CE 2002 1 15 CA011003016 120010903G213347061 VALVE CESSNA441 441 2076020CE CABIN PRESSURE FAILED W A UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 CA (CAN) DURING AIRCRAFT CLIMB, THE EMERGENCY PRESSURIZATION VALVE OPENED ALLOWING UNCONDITIONAL BLEED AIR INTO THE CABIN. CABIN TEMPERATURE INCREASED AT AN UNCONTROLED RATE. AIRCRAFT RETURNED TO THE AIRPORT FROM WHICH IT DEPARTED. THE EMERGENCY PRESSURIZATION VALVE WAS REPLACED. AIRCRAFT GROUND RUN "S". 1L72 3T RTA28CE 20020115000142002011500014NM 2002 1 15 CA011004001 120010729G29108297000269 LINE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD14SF 14SF23 NE HYD SYSTEM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING 20 FH MAINTENANCE INSPECTION, MAINTENANCE FOUND HYDRAULIC FLUID LEAKING AROUND FS UNLOADING VALVE IN ENGINE NR 2 NACELLE. THE LINE P/N 8297000-269 IS REPORTED TO HAVE A CRACKED CRYOFLARE FITTING. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20020115000162002011500016NM 2002 1 15 CA011004003 120010728G291082970009267 LINE DHAV DHC8 DHC8* NM PWA PW120 PW123 NE HAMSTD14SF 14SF23 NE HYD SYSTEM CHAFED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) DURING 20 FH INSPECTION, MAINTENANCE FOUND EVIDENCE OF HYDRAULIC LEAK IN THE LT ENGINE NACELLE. THE LINE P/N 82970009-267 (FS UNLOADING VALVE TO RETURN MANIFOLD) AND LINE P/N 82970009-157 (RESERVOIR TO HYDRAULIC SOV) CHAFED TOGETHER.THE TWO LINES WERE REPLACED.TSN/CSN 896.05/793 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20020115000172002011500017NE 2002 1 15 CA011004004 220010918G8530ST90P10ER CYLINDER HEAD DHAV DHC2 DHC2* 2800108EA PWA R985 R985AN14B 52008NE ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACK FOUND ON CYLINDER HEAD FROM EXHAUST PORT TO FRONT SPARK PLUG WHILE PERFORMING AD 78-08-07. 1H71 3R3 R A806 5E1 20020207000022002020700002EA 2002 2 7 CA011004005 120010927G5523VALTOCC113618 ATTACH FITTING DHAV C3TE1213 DHAV DHC3 DHC3 2800202EA PWA PT6 PT6A135 52043NE ELEVATOR SERVO CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING INSPECTIONS FOUND THAT ELEVATOR SERVO TAB HAD TWO SHEARED OFF RIVETS UPPER FORWARD ENGINE AT ARM ATTACHMENT BLOCK AND CRACK AT LOWER BETWEEN RIVET HOLES ON ELEVATOR SERVO TAB. 1H71 3R4 T A815 E4EA 20011015000642001101500064CE 2001 10 15 CA011004008 120011003G3610S189148 CLAMP CESSNA CM357024 CESSNA500 500CESSNA 2076602CE PWA JD15 JT15D1A NE CLAMP LOOSE W B EMER. DESCENT O OTHER CLCLIMB 1 CA (CAN) CLIMBING THROUGH FLIGHT LEVEL 290, AIRCRAFT CABIN STARTED TO RAPIDLY CLIMB. FLIGHT CREW INITIATED A RAPID DECENT TO 10,000 FEET. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CLAMP ON CABIN BLEED AIR SUPPLY LINE LOOSE AND THE AIR SUPPLY LINE HAD BECOME DISCONNECTED. THE AIRCRAFT HAD RECENTLY HAD MAINTENANCE PERFORMED ON THE BLEED AIR SYSTEM. ALL OTHER CLAMPS IN THE BLEED AIR SYSTEM WERE CHECKED FOR SECURITY WITH NO FURTHER PROBLEM FOUND. 1L72 4F4 F A22CE E25EA 20020115000202002011500020CE 2002 1 15 CA011004010 120010829G6100CA462220W BOLT MCAULY 1C160DTM755 CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160DTM GL PROPELLER BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 729634 (CAN) ONE OF THE 6 BOLTS ATTACHING THE PROPELLER TO THE ENGINE CRANK SHAFT FLANGE BROKE AT THE TOP OF THE THREADED AERA ON INITIAL TORQUE.THE PROPELLER HAD A PLACARD INDICATING TORQUE SPED FOR 1/2" BOLTS. PROLLER IS ATTACHED WITH 7/16" BOLTS. IT IS SUSPECTED THAT THE BOLTS HAVE BEEN OVER TORQUED ON PREVIOUS INSTALLATIONS. PLACARD WAS REMOVED FROM THE PROPELLER AND BOLTS TORQUED TO THE PROPER TORQUE SPEC FOR 7/16 BOLTS. 1H71 3O3 ONT3A12 E274 5 NP910 20020115000252002011500025SO 2002 1 15 CA011004016 120011004G712012351015 MOUNT PIPER PA18 PA18A150 7101837SO LYC O320 O320A2B 41508EA ENGINE BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ENGINE MOUNT RIGHT DIAGNEL ARM FOUND BROKEN APPROX 2" FROM UPPER RIGHT FIREWALL ATTACH POINT. ENGINE MOUNT REMOVED AND REPLACED WITH NEW 1H71 3O3 O 1A2 E274 20020115000262002011500026CE 2002 1 15 CA011004017 120010918G716004500704 SEAL CESSNA 04500521 CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA AIRBOX TORN W C ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 CA (CAN) - AIRCRAFT ROUGH RUNNING, NOT PRODUCING FULLPOWER. AIR BOX REMOVED AND BUTTERFLY SEAL FOUND UNSERVICEABLE. A SMALL PIECE A SEAL WAS FOUND IN CARB. VENTURI. A NEW AIR DOOR SEAL WAS INSTALLED.- AIRCRAFT GROUND RUN & CHECKED OK. 1H71 3O3 ONT3A19 E223 20020115000282002011500028CE 2002 1 15 CA011005001 120010923G351017201041 REGULATOR SCOTT BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA OXYGEN BOTTLE MISMARKED W O OTHER L NO TEST LDLANDING 1 CA (CAN) CREW REPORTED O2 SYSTEM NOT FUNCTIONING CORRECTLY. ON INVESTIGATION MAINTENANCE DISCOVERED REGULATOR WAS INSTALLED 180 DEGREES OUT OF RIG. ON FURTHER EXAMINATION REGULATOR VALVE WAS FOUND TO ROTATE 360 DEGREES FOR MULTI-POSITION INSTALLATIONS. O2 BOTTLE HAD RECENTLY BEEN INSTALLED & HAD FLOWN ONE FLIGHT BEFORE BEING SNAGGED. THE POTENTIAL FOR SERIOUS INCIDENT AT ALTITUDE COUPLED WITH A DEPRESSURIZATION IS HIGH WITH THIS TYPE OF INSTALLATION. THE VALVE IS NOT "MURPHY PROOF" & REQUIRES EXTREME CARE AND ATTENTION ON INSTALLATION AS THE VALVE ON THE REGULATOR IS ALSO POORLY MARKED FOR ON & OFF POSITION. 1L72 3T4 TRT3A20 E4EA 20020115000292002011500029SW 2002 1 15 CA011005002 120010926G6320204040701103 BEVEL GEAR BELL 212040001123BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA TRANSMISSION BROKEN W K NONE O OTHER ININSP/MAINT 1 CA ABW40395 (CAN) METAL PARTICLES FOUND IN SUMP FILTER AT 50 HOUR INSPECTION. TRANSMISSION REMOVED AND SENT FOR OVERHAUL. WHEN ROTOR BRAKE QUILL WAS REMOVED I NOTICED HEAVY WEAR ON THE TEETH OF THE PINION. INSPECTION OF THE SPIRAL BEVEL GEAR REVEALED TWO BROKEN TEETH AND HEAVY WEAR MARKS ON BACK SIDE OF ALL REMAINING TEETH. 1G71 4U4 U H4SW E22EA 20020116000032002011600003CE 2002 1 16 CA011005003 120010919G2436VR600A VOLT REGULATOR CESSNA150 150M 2071830CE CONT O200 O200A 17020SO MCAULY1A102 1A102OCM GL DC ELECTRICAL INOPERATIVE W O OTHER J WARNING INDICATION CRCRUISE 1 CA (CAN) INCOMPATIBILITY BETWEEN PARTS.IT HAS BEEN DISCOVERED THAT SEVERAL SUPPLIERS HAVE BEEN INFORMED THAT VOLTAGE REGULATORS LAMAR DGR 6 & ELECTROSYS VR600A ARE COMPATIBLE & INTERCHANGEABLE. IN ACTUALFACT LAMAR DGR6 IS INTERCHANGEABLE WITH THE ELECTROSYS VR600. NOTE: VR600 VOLTAGE REGULATORS ARE NO LONGER AVAILABLE. NOTE: ELECTROSYS VR600A HAS BUILT IN OVER-VOLTAGE PROTECTION CCT.WHEN INSTING ELECTROSYS VR600A FOR 1ST TIME, INST INSTRUCTION REQUI RE YOU TO COMPLETELY REMOVE OVER-VOLTAGE SWITCH P/N C593001-010 FROM A/C. 1H71 3O3 O 3A19 E252 5 NP918 20020115000302002011500030CE 2002 1 15 CA011005004 120010921G2710262400724 BELLCRANK CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL AILERON WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING SCHEDULED MAINTENANCE, EXCESSIVE PLAY WAS FOUND BETWEEN THE RT OUTBOARD AILERON BELL CRANK AND THE RESPECTIVE AILERON PUSH / PULL TUBE. FURTHER INVESTIGATION REVEALED THAT THE ATTACH POINT HOLE DIMENSIONS WERE BEOND ACCEPTABLE LIMITS. BELL CRANK WAS REPLACED WITH A NEW ASSEMBLY. 1H71 3T3 T A37CE E4EA 5 CP60GL 20020115000392002011500039SW 2002 1 15 CA011011007 120010831G5302206020123008 STRUCTURE BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL TAILBOOM V FIN VIBRATION W K NONE O OTHER ININSP/MAINT 1 CA (CAN) PART CAUSING HIGH VIBRATION IN T/R SYSTEM. REPLACED VERTICAL FIN. 1G71 3U3 U H2SW E4CE 20020115000402002011500040SW 2002 1 15 CA011011008 120010831G5302206020121006 FITTING BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL TAILBOOM V FIN CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) PART CRACK AT REAR RIVET. REPLACED FITTING. 1G71 3U3 U H2SW E4CE 20020115000412002011500041SW 2002 1 15 CA011011009 120010916G28221C274 PUMP BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL FUEL BOOST FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) PUMP NOT WORKING MOTOR UNSERVICEABLE. REPLACED PUMP ASSEMBLY. 1G71 3U3 U H2SW E4CE 20020115000422002011500042EU 2002 1 15 CA011011010 120010917G2911704A34240015 ACCUMULATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) PART LEAKING. PART REPLACED. 1G71 3U3 UNCH9EU E19EU 20020115000432002011500043GL 2002 1 15 CA011011011 220010918G72104638001001 GEARBOX BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) PIC CALLED IN A MAGNETIC LITE ON. A/C LANDED AT SCHOOL. AME INSPECTED MAG PLUG, 1 SMALL FLAKE AND 1 THIN HAIR. A/C RUN UP CARRIED OUT NO FURTHER INDICATION. A/C FLOWN APPROX 8 MILES TO MIRIMICHI AIRPORT AND HOVERED AROUND RAMP AREA FOR APPROX 80 MINUTES. NO FURTHER INDICATION. AME ELECTED TO CHANGE MGB OIL AND INSPECT MGB FINE OIL FILTER. FILTER FOUND TO CONTAIN NUMEROUS PIECES OF MATERIAL AND DRAINED OIL WAS SHINY. A/C REMOVED FROM SERVICE AND TRANSPORTED BACK TO MAINTENANCE FACILITY. 1G72 3U3 U H3EU E4CE 20020115000442002011500044CE 2002 1 15 CA011011012 120010919G712005510171 MOUNT CESSNA172 172L 2072432CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160CTM GL ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ENGINE MOUNT WAS FOUND CRACKED DURING 50 HOUR INSPECTION. NO CRACKS WERE NOTICED AT THE PREVIOUS INSPECTION AND THE CRACK SHOWED NEW MATERIAL. THIS WOULD INDICATE DETERIORATION DURING THE LAST 50 HOUR. 1H71 3O3 ONT3A12 E274 5 NP910 20020115000472002011500047EU 2002 1 15 CA011011015 120011003G27105271212075 STOP PILATS 5271212003 PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL BELLCRANK MISSING W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE CARRING OUT ANNUAL INSPECTION IT WAS NOTED THAT THIS AILERON BELLCRANK STOP ON THE LEFT HAND WING WAS MISSING. LOOKING AT THE STOP ON THE RIGHT HAND WING IT APPEARS TO BE JUST A PLASTIC STOP PUSHED INTO A HOLE IN THE WING STRUCTURE. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020115000482002011500048EU 2002 1 15 CA011011022 120011002G2897RR53710K WIRE PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL BOOST PUMP PINCHED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ON REMOVAL OF THE BOOSTER PUMP, IT WAS FOUND THAT THE WIRE HARNESS, WHICH IS PART OF THE PUMP HAD APPEARED TO HAVE BEEN TRAPPED BETWEEN THE BOOSTER PUMP MOUNTING PLATE & THE AIRFRAME. THIS HAS CAUSED ONE WIRE OF THE HARNESS TO BE CRIMPED FLAT & THE INTERNAL COPPER CONDUCTOR TO BE EXPOSED.THE BOOSTER PUMP WAS CHANGED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020115000492002011500049SW 2002 1 15 CA011012001 120011002G6410212010750105 BLADE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA TAIL ROTOR DELAMINATED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ON A DAILY INSPECTION THE ENGINEER WAS INSPECTING THE TAIL ROTOR BLADES, ON T/R BLADE S/N A-11101 HE FOUND A DELAMINATION AT THE TIP. A REPLACEMENT T/R HUB ASSEMBLY WAS ORDERED (TSN 729.9 OF S/N A-11101) AT TTSN 413.9 T/R BLADE WAS REMOVED DUE TO DELAMINATION AND TO CARRY OUT SB 212-00-111 REV.A (SB 205-00-80 REV.A) T/R BLADE TIP BLOCK RETENTION MODIFICTION. 1G71 4U4 U H4SW E22EA 20020115000502002011500050CE 2002 1 15 CA011012002 120011011G3210 LANDING GEAR BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA RIGHT FAILED W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CA (CAN) AFTER TAKE-OFF RT GEAR INDICATION INDICATED RT GEAR NOT RETRACTED. GEAR WAS CYCLED DOWN AND THEN INDICATED NOT DOWN AND LOCKED. SUBSEQUENT RE-CYCLE PRODUCED SAME RESULT (NO GREEN FOR RT SIDE AND INTRANSIT LIGHT ON IN GEAR HANDLE). OBSERVATION DURING AIRCRAFT FLY-BY SHOWED GEAR IN DOWN AND LOCKED POSITION. ON THE LANDING ROLL, RT GEAR RETRACTED UNDER THE WEIGHT OF THE AIRCRAFT. INVESTIGATION UNDERWAY. 1L72 3T4 T A14CE E4EA 20020115001692002011500169SW 2002 1 15 CA011012003 120011002G5320205030163095 CAP BELL 205 205A1 1181414SW LYC T53 T5317A 41549NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ON A TURN AROUND CHECK AFTER REFUELING THE AIRCRAFT, AN ENGINEER FOUND A CRACK ON THE EXPOSED SIDE OF THE LEFT BEAM CAP THAT IS LOCATED NEAR THE FORWARD VERTICAL WALL. 1G71 4U4 U H1SW E17EA 20020115000552002011500055NE 2002 1 15 CA011012008 120010529G67101565202535 SERVO VALVE SKRSKYS64 S64E 8142604NE PWA JFTD12JFTD12A4A 52047NE MAIN ROTOR FAILED W HA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 CA (CAN) A/C IN LOGGING OPS NEAR SAYWARD, BC. AS PILOT MADE HIS APPROACH TO LOG LDG& INITIATED FLARE TO SLOW DOWN HIS APPROACH, A/C'S NOSE ABRUPTLY PITCHED UP & CONTINUED TO DO SO EVEN WITH FULL FWD CYCLIC APPLIED. A/C FINALLY LEVELED OFF THEN BEGAN VIOLENTLY PITCHING UP & DOWN. CNTL OF A/C REGAINED BY SHUTTING OFF 1ST STAGE HYDRAULIC SYS. WITH SYS REMAINING TURNED OFF PILOT SET DOWN LOAD OF LOGS & THEN RETURNED TO SERVICE LANDING MAKING UNEVENTFUL LDG. AFTER LDG PILOT CARRIED OUT FULL HYDRAULIC SERVO CHECK & FOUND CYCLIC COULD NOT BE MOVED FWD WITH 1ST STAGE HYDRAULIC SYS ON. MAIN ROTOR TANDEM SERVO INST IN FOR & AFT POS WAS REPL & A/C RT-SRV. 2G72 4U4 U H4EA E15EA 20020115000562002011500056WP 2002 1 15 CA011012009 120010927G6520369D25430 SHAFT 369D25400 HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL T/R GEARBOX BROKEN W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 0298 (CAN) GEARBOX RECEIVED FROM CUSTOMER WITH COMPLAINT OF T/R VIBRATION AND METAL GENERATION. ON STRIP DOWN THE OUTPUT GEARSHAFT WAS REMOVED AND THE OUTPUT JOURNAL AND THE END OF THE OUTPUT GEARSHAFT WERE FOUND INSIDE OF THE ALIGNMENT BEARING.THE OUTPUT GEARSHAFT HAD FAILED.THIS THE SECOND OCCURRENCE OF THIS TYPE, THE FIRST OCCURRED 1997-03-05. 1G71 3U3 U H3WE E4CE 20020115000572002011500057EA 2002 1 15 CA011016001 120011016G2120C6VF11181 SCREEN DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA EXPANSION CHAMB BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING MAINTENACE TO CHANGE A GROUND BLOWER THE EXPANSION CHAMBER WAS REMOVED TO GAIN ACCESS TO THE BLOWER. A RATTLE WAS NOTICED INSIDE THE CHAMBER . INVESTATION REVEALED THE INTERNAL SCREEN HAD SEPERATED FROM THE FILTER SCREEN. THIS CONDITION COULD POSSIBLY LET FOREIGN OBJECTS INTO THE HEATING SYSTEM.THE AFFECTED PART WAS REPLACED WITH A NEW ITEM .THE NEW PART WILL BE INSPECTED PERIODICALLY TO CHECK FOR CONDITION 1H72 3T4 TRTA9EA E4EA 20020115000582002011500058WP 2002 1 15 CA011016002 120011016G6310369D25351 SPRAG CLUTCH HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL CLUTCH ASSY CHIPPED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ON 300 HOUR (SLING TIME OF 221.1 HOURS) INSPECTION THE SPRAG ASSEMBLY WAS FOUND TO HAVE ONE BROKE SPRAG 1G71 3U3 U H3WE E4CE 20020115000592002011500059EU 2002 1 15 CA011017002 120011011G6720350A33105803 BELLCRANK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE T/R GEARBOX WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) TAIL ROTOR PITCH CONTROL PUSH-PULL TUBE ROD END BEARING STAKING SLEEVE WORE A CIRCULAR GROOVE INTO THE EAR / CLEVIS OF THE BELLCRANK THAT IS MOUNTED ON THE T/R GEARBOX. 1G71 3U3 U H9EU E19EU 20020115000602002011500060EA 2002 1 15 CA011017003 220010921G7414 GEAR BENDIX S6LN1208 PIPER PA31 PA31 7103102SO LYC O540 TIO540A2B 41532EA MAGNETO SEIZED W EA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA 8215200 (CAN) RT ENGINE SHUTDOWN IN FLIGHT, AT TOP OF CLIMB AT ABOUT 8,500 FT. PILOT COULD NOT RESTART. INSPECTION ON GROUND THE GEAR TRAIN IN ACCESSORY CASE WAS OBSERVED NOT TO TURN. THE LEFT MAG WAS REMOVED AND FOUND TO BE SEIZED. THE GEAR ON REAR OF CRANKSHAFT HAD TEETH MISSING LOCATING DOWEL SHEARED AND RETAINER BOLT BROKEN. NO DAMAGE TO NEXT GEAR IN TRAIN WAS OBSERSVED. ENGINE SENT FOR REPAIR / OVERHAUL. MAG SUBMITTED TO OAE TO DETERMINE CAUSE OF FAILURE. 1L72 3O3 O A20SO E14EA 20020115000862002011500086SO 2002 1 15 CA011017006 120010504G3230452440 BEARING PIPER PA31 PA31 7103102SO LYC O540 TIO540A2B 41532EA NLG UPLOCK SEIZED W O OTHER J WARNING INDICATION APAPPROACH 1 CA (CAN) - NOSE WHEEL WOULD NOT COME DOWN FOR LANDING, CONFIGURATION. A/C LANDED ON MAINS WITH NOSE WHEEL FULLY RETRACTED. UPON INSPECTION NOSE WHEEL UPLOCK BEARING FOUND SEIZED WHICH RESULTED IN NOSE WHEEL NOT DISENGAGING FROM UPLOCKED POSITION. - BEARING WAS SERVICED AT PREVIOUS 100 HOUR INSPECTION AND A/C DUE FOR ANOTHER 100 HOUR INSPECTION. - SUSPECTED CAUSE: A WET SPRING ALSO, OPERATOR'S FLIGHTS ARE MOSTLY DONE OFF OF GRAVEL STRIPS. THERE WAS A LARGE ACCUMULATION OF SAND & SILT ON LANDING GEAR. OPERATOR REGULARLY PRESSURE WASHED GEAR AND GREASE JOINTS AND HINGES. BUT UPLOCK WAS OVERLOOKED AND NOT CHECKED REGULARLY ON WALK AROUNDS.BEARING ARE NOW INSPECTED ON A/C DAILY PREFLIGHT INSPECTIONS. 1L72 3O3 O A20SO E14EA 20020115000882002011500088SO 2002 1 15 CA011017007 220010922G8530CH71HER VALVE SEAT CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULY2A34C D2A34C58 GL CYLINDER HEAD CRACKED W A UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 CA (CAN) - NR 6 CYLINDER ASSEMBLY CRACKED FROM EXHAUST VALVE SEAT TO INJECTOR PORT TO INTAKE VALVE SEAT. - INJECTOR AND FUEL FLOW AND PRESSURE NORMAL SO CAUSE UNKNOWN.- CYLINDER REPLACED. 1H71 3O3 O 3A24 E5CE 5 CP3EA 20020115000902002011500090CE 2002 1 15 CA011017008 120011001G273126612158 SCREW CESSNA 26612151 CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL TRIM ACTUATOR DAMAGED W O OTHER F FLT CONT AFFECTED DEDESCENT 1 CA (CAN) FLIGHT CREW REPORTED JAMMED ELEVATOR TRIM. INSPECTION REVEALED DAMAGED SCREW THREADS ON THE ELEVATOR TRIM ACTUATOR (PARTS ENCLOSED).SCREW P/N 2661215-8 INTERNAL SCREW P/N 2661215-6 1H71 3T3 T A37CE E4EA 5 CP60GL 20020115001312002011500131NM 2002 1 15 CA011017016 120010627G7930APT761000100DW TRANSMITTER DHAV DHC8 DHC8* NM PWA PW120 PW123 NE HAMSTD14SF 14SF23 NE OIL PRESSURE FAILED W E ENGINE SHUTDOWN O OTHER DEDESCENT 1 CA (CAN) DURING DESCENT CREW REPORTED NR 2 ENGINE OIL PRESSURE DROPPED BELOW 55 PSID. ENGINE POWER WAS REDUCED AND PROP FEATHERED AS PER FM. NH REMAINED ABOVE 75 PERCENT ON FINAL SO ENGINE WAS SHUTDOWN. NO REPORT ON NR 2 ENGINE OIL PRESSURE WARNING LIGHT ON.ON GROUND, MAINTENANCE REPLACED BOTH THE OIL PRESSURE TRANSMITTER AND PRESSURE GAUGE. ENGINE GROUND RUN OK. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20020115001362002011500136CE 2002 1 15 CA011018008 120010721G28231013890253 SHUTOFF VALVE BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA FUEL SHUTOFF STUCK W O OTHER L NO TEST TXTAXI/GRND HDL 1 CA (CAN) DURING PILOT'S PRE-FLIGHT INSPECTION LT FUEL FIREWALL VALVE WOULD NOT CLOSE. 1L72 3T4 TRT3A20 E4EA 20020115001472002011500147CE 2002 1 15 CA011018009 120011011G3260 WIRE BEECH 100 100BEECH 1152916CE PWA PT6 PT6A28 EA LT MLG DOWNLOCK BROKEN W L ABORTED APPROACH N FALSE WARNING APAPPROACH 1 CA (CAN) NO DOWN AND LOCK INDICATION FOR THE RT MAIN LANDING GEAR. FOLLOWING A MANUAL EXTENSION THE AIRCRAFT LANDED WITH OUT INCIDENT. INSPECTION REVEALED A BROKEN WIRE ON THE RT MAIN DOWN AND LOCK SWITCH. REPAIRS CARRIED OUT. LANDING GEAR FUNCTION CHECKED SERVICEABLE 1L72 3T4 T A14CE E4EA 20020115001492002011500149EA 2002 1 15 CA011018011 220011001G7322CF30766 FLOAT MARVELSCHEBX105009 CESSNA172 172 2072402CE LYC O320 O320* 41508EA CARBURETOR WORN W K NONE O OTHER ININSP/MAINT 1 CA BL2213803 (CAN) CARBURETOR WOULD "FLOOD WHILE AT REST", CARBURETOR BULK DISMANTLED, TOP HALF INVERTED, FOUND FLOAT HEIGHT NON EXISTENT, SHOULD BE 7/32. REMOVED FLOAT FOR INSPECTION. FOUND ADJUSTMENT TAB SEVERELY WORN FROM NEEDLE VALVE. REPLACED DEFECTIVE FLOAT WITH NEW PILYMER FLOAT. 1H71 3O3 ONT3A12 E274 20020115001502002011500150CE 2002 1 15 CA011018012 120010928G552012346391 RIB CESSNA 123463324 CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL ELEVATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE INBOARD NUTPLATE WITH PART OF THE RIB HAD COMPLETELY SEPARATED ALLOWING THE COUNTERWEIGHT TO MOVE FREELY FORWARD AND AFT IN ELEVATOR HORN. 1H71 3O3 O A4CE E5CE 5 CP47GL 20020115001512002011500151SO 2002 1 15 CA011018013 120011017G301025S5D508419 BOOT EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA DEICE SYSTEM DAMAGED W O OTHER D INFLIGHT SEPARATION APAPPROACH 1 CA (CAN) ON APPROACH A VIBRATION WAS FELT BY THE FLIGHT CREW. VISUAL INSPECTION BY THE FLIGHT CREW REVEALED THE OB LEFT HAND WING DEICE BOOT WAS RIPPED AND FLAPING AGAINST THE WING. THE AIRCRAFT LANDED WITH OUT INCIDENT, HOWEVER A PORTION OF THE DEICE BOOT SEPERATED FROM THE AIRCRAFT. THERE WAS NO DAMAGE INFLICTED UPON THE AIRCRAFT. 1L72 4T4 T A21SO E4EA 20020115001522002011500152CE 2002 1 15 CA011018014 120010928G27200411307 TUBE CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL RUDDER ARM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) TUBE CRACKED FROM BOLT HOLE TO LOWER EDGE OF TUBE. 1H71 3O3 O A4CE E5CE 5 CP47GL 20020115001532002011500153CE 2002 1 15 CA011018015 120010928G2701126014215 TUBE CESSNA 126014015 CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL CONTROL COLUMN CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ONE OF 3 BOLT HOLES ATTACHING CONTROL WHEEL TO TUBE CRACKED FROM HOLE TO EDGE OF TUBE. 1H71 3O3 O A4CE E5CE 5 CP47GL 20020115001542002011500154NE 2002 1 15 CA011018016 220010920G7220555225056 RIVET CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE INLET LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AIRCRAFT DOWN FOR PHASE 5 INSPECTION. L/H ENGINE - 2 RIVET IN THE 5 O'CLOCK POSITION AND 3 RIVETS AT 7 O'CLOCK POSITION HAD THE HEADS PULLED 1/3 TO 2/3 AROUND THE SHANK DIAMETER.R/H ENGINE 5 TO 6 RIVETS IN THE 3 TO 6 O'CLOCK POSITION HAD THE HEADS PULLED 1/4 TO 2/3 AROUND THE SHANK DIAMETER.ALL BAD RIVETS REPLACED. 1L72 4F4 F A22CE E1NE 20020115001552002011500155CE 2002 1 15 CA011018017 120011005G532050420013451 CROSSTUBE BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) IT WAS FOUND THAT SOME ONE HAD REMOVED MATERIAL FROM THE CROSS TIE MEMBER, PROBABLY TO DEAL WITH SOME FIT AND CLEARANCE PROBLEM. SUBSEQUENT TO THIS WE HAVE FOUND A CRACK PROPAGATING FROM THE RADIUS FORWARD TO THE BULKHEAD. THIS AIRCRAFT WAS BEING INSPECTED IN PREPARATION FOR A C OF A APPLICATION. 1L72 3T4 TRT3A20 E4EA 20020207000442002020700044CE 2002 2 7 CA011018018 120011005G750031A4121 MANIFOLD CESSNA500 550 2076604CE BLEED AIR SYS CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) SEVERAL CRACKS (SEVEN) FOUND AROUND RING WHERE RADIUS MEETS TUBE. 1L72 4F A22CE 20020115001562002011500156CE 2002 1 15 CA011018020 120011001G5330 SKIN CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING SCHEDULED MAINTENANCE CESSNA 550 PHASE "5" AND PHASE "49" INSPECTIONS, OF THE R/H F.S. 287.78 SKIN SEAM, A 1.5" LONG CRACK WAS FOUND CENTERED ABOUT 115.25 (W.L.). - CESSNA INFORMATION: THIS HAVE OCCUR ON SOME AIRCRAFT, FOLLOWING REPAINTING. - OUR AIRCRAFT S/N 550-0702 HAVE ORIGINAL PAINT. 1L72 4F4 F A22CE E1NE 20020115001572002011500157CE 2002 1 15 CA011018021 120011007G2121 WIRE HARNESS CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE VENT BLOWER CHAFED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) LARGE WIRE BUNDLE TOO CLOSE TO VENT BLOWER MOTOR. 1L72 4F4 F A22CE E1NE 20011108000042001110800004CE 2001 11 8 CA011018024 120010920G24223P639CP589BH WIRE CESSNA 3P639CP589BLCESSNA500 500CESSNA 2076602CE PWA JD15 JT15D1A NE SPLICE SHORTED W H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 CA (CAN) DURING A ROUTINE FLIGHT, ON ARRIVAL AT YYZ #2 INVERTER FAILED. SYSTEM WAS CHECKED AND FINDINGS WERE THAT THE 115 VAC OUTPUT FOR THE R/H BUS, RUNNING BETWEEN THE INVERTER AND THE FRONT PRESSURE BULKHEAD THE WIRE WAS FOUND SHORTED. THERE WAS EVIDENCE OF CORROSION AND ARCING ADJACENT TO A CRIMP SPLICE IN WIRE #3P639-CP589BH. (SEE ACCOMPANYING DIAGRAM). IT APPEARS THAT THE INSULATION MAY HAVE BROKEN DOWN ON ONE WIRE ADJACENT TO THE SPLICE, WHICH CAUSED A SHORT CIRCUIT AND ARCING WHICH CONTINUED TO DETERIORATE THE INSULATION, CAUSING FAILURE IN THE CIRCUIT. 1L72 4F4 F A22CE E25EA 20011108000052001110800005CE 2001 11 8 CA011019001 120011018G243651539012N GCU CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL GCU W K NONE J WARNING INDICATION CRCRUISE 1 CA (CAN) DURING CRUISE, PILOT NOTICED STANDBY POWER ON ANNUNCIATOR FLASHING FOLLOWED SHORTLY BY THE STANDBY POWER INOP ANNUNCIATOR ON STEADILY.THIS WAS FOLLOWED BY THE GENERATOR OFF ANNUNCIATOR ILLUMINATING.BOTH GENERATOR POWER AND STANDBY POWER COULD BE RETURNED ON LINE BY CYCLING THE STANDBY POWER SWITCH AND THE GENERATOR RESET SWITCH.SYSTEM WAS TESTED ON THE GROUND WITH A MIN/MAX RECORDING VOLTMETER. EACH ILLUMINATION OF THE ANNUNCIATOR LIGHT CORRESPONDED WITH A VOLTAGE SPIKE TO 34+ VOLTS. GENERATOR CONTROL UNIT WAS REPLACED AND SYSTEM CHECKED NORMALLY. 1H71 3T3 T A37CE E4EA 5 CP60GL 20020115001642002011500164CE 2002 1 15 CA011019013 120011019G5751122005312 BRACKET CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO AILERON CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 1061710617 (CAN) DURING INSPECTION THE RT INBOARD AILERON BRACKET WAS FOUND CRACKED AT BOTH I/B & O/B UPPER ATTACH POINTS. {WHERE THE BRACKET ATTACHES TO THE REAR SPAR} BRACKET REPLACED 1H71 3O3 O A4CE E5CE 20020116000062002011600006NM 2002 1 16 CA011019022 120010521G7930APT761000100DW TRANSMITTER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE ENG OIL PRESSUREFAILED W E ENGINE SHUTDOWN O OTHER CRCRUISE 1 CA (CAN) ENGINE OIL PRESSURE DROPPED TO BETWEEN 44-55 PSI DURING FLIGHT. THE ENGINE POWER WAS REDUCED AND PROPELLER WAS SELECTED TO START FEATHER. OIL PRESSURE TRANSMITTER REPLACED, FUNCTION AND LEAK CHECKED SERVICEABLE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20020116000072002011600007NM 2002 1 16 CA011019023 120010524G80112431K2 CONTACTOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF15 NE STARTER STUCK W EH ENGINE SHUTDOWN DEACTIVATE SYST/CIRCUITS BH SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 CA (CAN) STARTER DID NOT DISENGAGE AFTER ENGINE START, SMOKE WAS NOTICED COMING FROM THE STARBOARD ENGINE. ELECTRICAL POWER WAS REMOVED AND THE ENGINE SHUTDOWN. THE START CONTACTOR WAS STUCK CLOSED. - STARTER GENERATOR REPLACED. - GENERATOR COANTROL UNIT REPLACED. - START CONTACTOR REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20011108000072001110800007EU 2001 11 8 CA011023001 120011016G77009752902015 DISPLAY PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL DISPLAY W K NONE O OTHER LDLANDING 1 CA 062 (CAN) EIS DISPLAY LIGHTING IS VERY DIM, BARELY READABLE.IT WAS ALSO INTERMITTENTLY FLASHING FROM BRIGHT TO DIM. ACQ DISPLAY REPLACED WITH ASERVICEABLE UNIT. A/C TIME SINCE NEW 435.2 CYCLES SINCE NEW 493 THE ACQUISITION DISPLAY HAS 135.3 HOURS. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020116000102002011600010EU 2002 1 16 CA011023002 120011017G77009752902015 DISPLAY PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL COCKPIT FAILED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 CA 018 (CAN) LOWER HALF OF EIS PANEL WOULD GO BLANK INTERMITTENTLY. TORQUE ITT, NG AND FUEL INDICATION TAPES REMAINED NORMAL. ALL OTHER INSTRUMENTS WERE AFFECTED, EITHER FLASHING, DISAPPEARING TOTALLY AND/OR INDICATING ERRONEOUS INFORMATION.YELLOW AND RED CAUTION LIGHTS WOULD INNUMINATE. WHEN "MENU" WAS SELECTED, THE TOP ROW WOULD GO BLANK AS PER NORMAL, BUT THE TRANSFERRED INFORMATION WOULD NOT SHOW UP ON THE ALTERNATE SCREENS.WHEN "TEST" WAS DEPRESSED EVERYTHING TESTED NORMAL. PANEL WOULD RETURN TO NORMAL AFTER SUBSEQUENT POWER UPS. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020116000112002011600011CE 2002 1 16 CA011023003 120011015G323008411102 LINK CESSNA414 414 2075908CE CONT O520 LTSIO520AE 17040SO MLG SHEARED W L ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 CA 10000 (CAN) DURING CROSS WIND LANDING APPEARENT SIDE LOAD ON LT MAIN U/C STRUT CAUSED THE THREADED PORTION OF THE LINK ASSEMBLY TO SHEAR ALLOWING GEAR TO RETRACK. LT PROPELLER BLADES STRUCK GROUND PILOT APPLIED POWER AND ABORTED LANDING. AFTERBURNING OFF FUEL. ATTEMPTED TO RECYCLE GEAR, NOSE AND RT GEAR INDICATED LOCKED LT INDICATED UNLOCKED. WHEN GEAR WAS RECYCLED LT GEAR FREE FELL INTO LOCKED POSITION AND A/C LANDED WITHOUT FURTHER DAMAGE. 1L72 3O3 ORTA7CE E8CE 20020116000132002011600013EA 2002 1 16 CA011025002 120010614G2910DSC152D8025426 HOSE DHAV DHC7 DHC7103 2802710EA PWA PT6 PT6A50 52043EA HAMSTD24PF 24PF305 GL HYD SYSTEM MISMARKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) A HYDRAULIC HOSE, P/N DSC152D8-0254-260 WAS ORDERED FROM THE COMPANIES STORES DEPARTMENT. THE INFORMATION ON THE PACKAGING INDICATED 3000 PSI WORKING PRESSURE.THE INFORMATION BAND CRIMPED AROUND THE HOSE INDICATED 1000 PSI WORKING PRESSURE. THE HOSE, ALONG WITH 3 OTHERS IDENTIFIED THE SAME WAY WERE RETURED TO THE SUPPLIER.THE SUPPLIER NOTIFIED THE HOSE MANUFACTURER, AND CHECKED THIER STOCK FOR LIKE HOSES.THE SUPPLIER INDICATED THAT AFTER A SEARCH, ONLY THE FOUR HOSES IN QUESTION WERE MISLABLED. 2H74 4T4 T A20EA E4EA 6 CP1NE 20020116000152002011600015GL 2002 1 16 CA011026001 120010717G32974533516 WIRE NAMER T6 HARVARDMK4 1922828GL PWA R1340 R1340AN1 52016NE MLG INDICATOR BROKEN W O OTHER J WARNING INDICATION LDLANDING 1 CA (CAN) DURING PRE-LANDING CHECK, THE PILOT NOTICED THAT THE RT LANDING GEAR INDICATOR PIN WAS NOT SHOWING ALL THE WAY DOWN. ALL OTHER GEAR INDICATIONS WERE NORMAL. (GREEN LIGHT AND VISUAL INDICATION). INVESTIGATION REVEALED THAT THE LANDING GEAR INDICATOR CABLE WAS PULLING OUT OF THE TERMINAL END. THIS RESULTED IN A CABLE THAT WAS SLIGHTLY LONGER AND THEREFORE GIVING THE ERRONEOUS INDICATION. A NEW CABLE WAS INSTALLED. 1L71 3R3 R EXPA1L715E2 20020208000012002020800001GL 2002 2 8 CA011026002 120010717G32604533516 CABLE NAMER T6 HARVARDMK4 1922828GL PWA R1340 R1340AN1 52016NE MLG INDICATOR BROKEN W O OTHER N FALSE WARNING LDLANDING 1 CA (CAN) DURING PRE-LANDING CHECK, THE PILOT NOTICED THAT THE RT LANDING GEAR INDICATOR WAS NOT SHOWING ALL THE WAY DOWN. ALL OTHER GEAR INDICATIONS WERE NORMAL. (GREEN LIGHT AND VISUAL INDICATION). INVESTIGATION REVEALED THAT THE LANDING GEAR INDICATOR CABLE WAS PULLING OUT OF THE TERMINAL END. THIS RESULTED IN A CABLE THAT WAS SLIGHTLY LONGER AND THEREFORE GIVING THE ERRONEOUS INDICATION. A NEW CABLE WAS INSTALLED. 1L71 3R3 R EXPA1L715E2 20020208000022002020800002GL 2002 2 8 CA011026003 120010717G32604533516 CABLE NAMER T6 HARVARDMK4 1922828GL PWA R1340 R1340AN1 52016NE MLG INDICATOR BROKEN W O OTHER N FALSE WARNING LDLANDING 1 CA (CAN) DURING PRE-LANDING CHECK, THE PILOT NOTICED THAT THE RT LANDING GEAR INDICATOR WAS NOT SHOWING ALL THE WAY DOWN. ALL OTHER GEAR INDICATIONS WERE NORMAL. (GREEN LIGHT AND VISUAL INDICATION). INVESTIGATION REVEALED THAT THE LANDING GEAR INDICATOR CABLE WAS PULLING OUT OF THE TERMINAL END. THIS RESULTED IN A CABLE THAT WAS SLIGHTLY LONGER AND THEREFORE GIVING THE ERRONEOUS INDICATION. A NEW CABLE WAS INSTALLED. 1L71 3R3 R EXPA1L715E2 20020116000162002011600016 2002 1 16 CA011026004 420010828G3460KFC295 COMPUTER BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO FLIGHT DIRECTOR MALFUNCTIONED W O OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 CA (CAN) PILOT REPORTED THE INABILITY TO CANCEL THE 'FD' FLIGHT DIRECTOR ANNUNCIATOR LIGHT ON THE AUTOPILOT ANNUNCIATOR PANEL. COMMAND BARS ON ADI WOULD NOT DROP OUT OF VIEW. FLIGHT DIRECTOR COMPUTER REMOVED AND REPAIR. 1L72 3O3 ORT3A16 3E1 20020116000172002011600017SO 2002 1 16 CA011029001 120011014G321014445 BALL JOINT EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA TORQUE LINK DAMAGED W O OTHER D INFLIGHT SEPARATION LDLANDING 1 CA (CAN) ON ROLL OUT FOLLOWING LANDING THE BALL JOIINT ASSEMBLEY PULLED OUT OF THE UPPER TORQUE LINK. THIS CAUSED THE RIGHT MAIN WHEEL TO TURN 180 DEGREES. REPAIRS REQUIRED THE REPLACEMENT OF BOTH THE UPPER TORQUE LINK AND THE BALL JOINT ASSEMBLY 1L72 4T4 T A21SO E4EA 20020116000182002011600018CE 2002 1 16 CA011029003 120010915G551026320273 SUPPORT CESSNA CESSNA208 208 2073702CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL HORIZONTAL STAB CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING AN ANNUAL INSPECTION, WHEN THE HORIZONTAL STABALIZER WAS REMOVED TO CARRY OUT A REPLACEMENT OF A SPAR CAP. CORROSION (PITTING) WAS NOTED IN ONE OF THE FORWARD SUPPORTS AND BOTH OF THE AFT SUPPORTS. NO DAMAGE IS ALLOWED TO CASTINGS OR FITTINGS. 3 OF THE 4 ATTACH SUPPORTS REQUIRED REPLACEMENT AS PER FACTORY RECOMMENDATION. 1H71 3T3 TNTA37CE E4EA 5 CP60GL 20020116000192002011600019CE 2002 1 16 CA011029005 120010915G534326111379 FITTING CESSNA208 208 2073702CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL MLG CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING AN ANNUAL INSPECTION PITTING WAS NOTED ON BOTH OF THE FORWARD AND BOTH OF THE AFT LANDING GEAR ATTACH FITTINGS. WHILE ATTEMPTING TO REMOVE THIS CORROSION THE DAMAGE WAS FOUND TO BE TOO SEVERE TO ATTEMPT. THE LANDING GEAR WAS REMOVED AND MORE CORROSION WAS NOTICED IN THE AREA THAT THE GEAR ATTACHES TO THE FITTING. ALL FOUR MAIN LANDING GEAR FITTINGS WERE REPLACED AS PER VERBAL INSTRUCTIONS FROM FACTORY TECH. REP. 1H71 3T3 TNTA37CE E4EA 5 CP60GL 20020116000202002011600020CE 2002 1 16 CA011029006 120010915G273126612151 ACTUATOR CESSNA208 208 2073702CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL ELEVATOR TRIM CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE PERFORMING AN ANNUAL INSPECTION ON THIS CESSNA CARAVAN THE ELEVATOR TRIM JACKS WAS NOTED TO HAVE SIGNIFICANT CORROSION ON SEVERAL OF THE PARTS. THE FOLLOWING PARTS REQUIRED REPLACEMENT HOUSING P/N 2661215-2/BEARINGS P/N 6361620-6 AND MS27641-66/PINS P/N MS35675-12/ROD ENDS P/N S2629-1. THESE TRIM ACTUATORS HAD BEEN SIGNED AS INSPECTED LESS THAN 100 HOURS PRIOR TO THIS FINDING. 1H71 3T3 TNTA37CE E4EA 5 CP60GL 20020116000212002011600021CE 2002 1 16 CA011029007 120010915G5347261106014 SEAT TRACK CESSNA208 208 2073702CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE PERFORMING AN ANNUAL INSPECTION THE AREA AT THE AFT END OF NR 2 / 3 / 4 SEAT RAIL UNDER THE FLOOR AT FS 283.85 WAS NOTED TO HAVE SEVERE CORROSION ON THE STIFFENER P/N 2611131-3 AND THE DOUBLERS P/N 2611192-4 AS WELL AS THE SEAT RAIL. THE CORROSION WAS CLEANED AS REQUIRED FROM THE STRUCTURE AND SEAT RAILS NR 2 AND NR 4. THE STIFFENER, DOUBLERS AND NR 3 SEAT RAIL, AS WELL AS THE ATTACHING HARDWARE WAS REPLACED. 1H71 3T3 TNTA37CE E4EA 5 CP60GL 20020116000222002011600022CE 2002 1 16 CA011029008 120010915G5550263440221 HINGE CESSNA208 208 2073702CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL EMPENNAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE PERFORMING AN ANNUAL INSPECTION ON THIS AIRCRAFT, EXCESSIVE MOVEMENT WAS NOTED FROM THE OUTBOARD AND CENTRE HINGE BEARINGS FOR THE R/H ELEVATOR. WHEN THE HINGE SUPPORTS WERE DISMANTLED TO REPLACE THE BEARINGS, CORROSION WAS FOUND ON BOTH HALVES OF THE INBOARD AND CENTRE HINGE SUPPORTS. THE HINGE SUPPORTS AS WELL AS THE BEARINGS WERE REPLACED AS PER FACTORY RECOMMENDATION. 1H71 3T3 TNTA37CE E4EA 5 CP60GL 20020116000232002011600023CE 2002 1 16 CA011029009 120010915G53122612591 BULKHEAD CESSNA208 208 2073702CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING AN ANNUAL INSPECTION ON THIS AIRCRAFT AN AREA OF CORROSION WAS FOUND ON THE AFT CANTED BULKHEAD AT STATION 427.88 AFT LEFT WL 1 OR 2 INCHES OFF CENTRE. THE CORRORION WAS REMOVED AND THE DAMAGE WAS FOUND TO BE THROUGH 50 PERCENT OF THE MATERIAL. THE AFT BULKHEAD WASREPLACED PER THE 208 S.R.M. 1H71 3T3 TNTA37CE E4EA 5 CP60GL 20020116000242002011600024CE 2002 1 16 CA011029010 120010915G551126320233 SPAR CAP CESSNA208 208 2073702CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL HORIZONTAL STAB CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING AN ANNUAL INSPECTION OF THIS AIRCRAFT, SEVERE CORROSION WAS NOTED ON THE AFT UPPER TRAILING EDGE SPAR CAP ON THE HORIZONTAL STABILIZER AT APPROXIMATELY SS 80.60 LEFT HAND AND ARIGHT HAND SIDES. THE CORROSION HAS GONE THROUGH THE SPAR CAP BUT HAD NOT YET DAMAGED THE WEB. THIS CORROSION WAS NOT INITIALLY NOTICED DUE TO THE FACT THE CORROSION HAD BEEN PAINTED OVER THE ENTIRE SPAR CAP WAS REPLACED. 1H71 3T3 TNTA37CE E4EA 5 CP60GL 20020116000252002011600025EU 2002 1 16 CA011029011 120011015G6520770441 CARBON SEAL SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR GB CRACKED W E ENGINE SHUTDOWN K FLUID LOSS TXTAXI/GRND HDL 1 CA (CAN) DURING A GROUND RUN ON OIL LEAK WAS DETECTED FROM THE TAIL ROTOR GEAR BOX. AIRCRAFT WAS SHUT DOWN LEAK INVESTIGATED. OIL LEAK FROM INPUT MAG SEAL. SEAL AND HOUSING REMOVED. THE STATIONARY PORTION OF SEAL FOUND TO HAVE MULTIPLE CRACKS. MAG SEAL WAS PREVIOUSLY REMOVED DUE TO SMALL LEAK. SEAL WAS "RE-SEATED" AND REINSTALLED. POSSIBLE CAUSE WAS INCORRECT INSTALLATION OF SEAL.A NEW CARBON MAG SEAL WAS INSTALLED. AIRCRAFT WAS GROUND RUN AND NO FURTHER LEAK PRESENT. 1G71 3U3 U H9EU E19EU 20020116000262002011600026CE 2002 1 16 CA011029012 120010802G555007321008 HINGE CESSNA 07326004 CESSNA180 180J 2072622CE CONT O470 O470S 17026SO HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING 100 HOUR INSPECTION FOUND LT OUTBOARD ELEVATOR BEARING LOOSE. REMOVED LT ELEVATOR TO CHANGE BEARING. WITH ELEVATOR REMOVED, FOUND LT OUTBOARD HINGE ASSEMBLY TO BE CORRODED AND CRACKED WHERE BEARING IS INSTALLED. 1H71 3O3 O 5A6 E273 20020116000272002011600027EA 2002 1 16 CA011029013 120011012G2560 RING 4494701 DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE SEAT BELT CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CORROSION LOCATED UNDER THE ('D' RING) WHERE SEAT BELT WEBBING CONTACTS ALUMINIUM D-RING. 1H71 3R3 R A806 5E1 20020116000282002011600028NE 2002 1 16 CA011029014 220011009G8520128511 CONNECTING ROD DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE HARTZLHCB3R HCB3R304 GL ENGINE BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE IN CRUISE AT 2,000 FEET A LOUD REPORT WAS HEARD FROM THE ENGINE. FOLLOWED WAS EXTREME ENGINE VIBRATION. POWER WAS REDUCED TO IDLE. THE AIRCRAFT WAS LANDED. UPON INVESTIGATION IT WAS DETERMINED THAT NR 5 AND NR 1 CONNECTING RODS WERE BROKEN. ENGINE CHANGED. 1H71 3R3 R A806 5E1 5 CP28EA 20020116000292002011600029NE 2002 1 16 CA011029015 220011003G8530 CYLINDER HEAD DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN1 52008NE ENGINE CRACKED W A UNSCHED LANDING RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CRCRUISE 1 CA (CAN) CYLINDER HEAD CRACKED. 1H71 3R3 R A806 5E1 20020116000302002011600030EU 2002 1 16 CA011029016 120011005G5302350A23002021 SKIN SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAILBOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) A 6 INCH LONG CRACK FOUND ON TAILBOOM FWD UPPER SKIN UNDER N5 BEARING MOUNT SUPPORT AT BOOM STA A868. TAILBOOM INST IN EUROCOPTER APPRD AS350/355 TAILBOM REPAIR FIXTURE FOR REPL OF UPPER SKIN&FOUND N5SUPPORT HAD BADLY MISALIGN TO FIXTURE: N5 BEARING MOUNT SUPPORT HAD BEEN PREV REPL IN FIELD BY OPERATOR PER EUROCOPTER AS350 REPAIR MANUAL CHAPT 53.10.40.773.A 2ND TAILBOOMN FOUND WITH SIMILAR DEFECT, ALSO N 5 BEARING MOUNT SUPPORT HAD BADLY MISALIGN TO FIXTURE: N5 BEARING MOUNT SUPPORT HAD BEEN PREV REPL IN FIELD.WE FEEL THAT MAIN REASON SKIN CRACKED MISALIGNMENT OF #5 BEARING MOUNT WHICH REPL IN FIELD W/O USE OF FIXTURE: 1G71 3U3 UNCH9EU E19EU 20020116000312002011600031EU 2002 1 16 CA011029017 120011025G6520350A33105803 LEVER SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE TAIL ROTOR CONTROL LEVER MAYBE THE SAME AIRFRAME TIME BUT WE ARE NOT 100 PERCENT SURE. THE TAILROTOR CONTROL LEVER HAD A DEFECT OF WEAR ON INSIDE EAR. UPON REMOVAL MAINTENANCE ENGINEER FOUND CRACKS IN THE WEBBING, TOP SIDE AT T/R SPIDER ATTACHMENT POINT. 1G71 3U3 U H9EU E19EU 20020116000342002011600034EU 2002 1 16 CA011029020 120010514G6410355A12004008 SKIN SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE T/R BLADE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) 131 MM CRACK ORIGINATING FROM THE RIVET HOLE FOR THE TRAILING EDGE TAB ON BOTH THE UPPER AND LOWER SURFACE.SDR NO. 20010112018 AND 2019 ADDRESSES THIS SAME DEFECT.SINCE DISCOVERY OF THIS DEFECT EUROCOPTER FRANCE HAS ISSUED INFO TELEX 00000035 REQUIRING A BEFORE FLIGHT/BETWEEN FLIGHT /AFTER FLIGHT AN 500 HOUR/24 MONTH INSPECTION OF THIS AREA FOR CRACKING. 1G71 3U3 UNCH9EU E19EU 20020116000352002011600035SO 2002 1 16 CA011030001 120011004G57136208603 STRINGER PIPER PA28 PA28140 7102802SO LYC O320 O320E3D 41508EA WING BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FLANGES AT END OF STRINGER ARE CRACKING. EVENTUALLY THE ENTIRE END OF STRINGER WILL SEPARATE. EACH WING HAS TWO STRINGERS ON INBOARD BOTTOM SKIN. BOTH ARE BROKEN ON THE RIGHT WING. LEFT WING IS OKAY. IT IS VERY DIFFICULT TO INSPECT THIS AREA ON NEWER PA28'S. IT IS TOTALLY IMPOSSIBLE ON OLDER PA28'S DUE TO LACK OF INSPECTION PANEL.I HAVE SEEN THIS BEFORE, ABOUT TWO YEARS AGO. BUT, IT WAS ON A PA34-200 TWIN. IT LOOKED LIKE AN ONE TIME EVENT, PECULIAR TO THAT AIRCRAFT. NOW I SEE IT AGAIN ON A SIMILAR WING BUT, IT HAS CROSSED MODEL LINES.#11 PART AVAILABLE. "NO", BUT PICTURES WERE TAKEN WITH A DIGITAL CAMERA. THEY ARE IN MY COMPUTER AND CAN BE E-MAILED IF YOU WISH. 1L71 3O3 O 2A13 E274 20020116000362002011600036EA 2002 1 16 CA011030002 120011016G5311C6FSM142236 FRAME DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACK FOUND IN SIDE FRAME AT RT. STATION 218.125 RUNNING ON AN ANGLE FROM TOP OF FRAME. NOTE PART IS POST MOD 6/1462 AS DIRECTED BY CF-78-17R1. DHC SB 6/371 REV.B.PLEASE SEE PHOTOS. 1H72 3T4 TRTA9EA E4EA 20020116000372002011600037SO 2002 1 16 CA011030003 120011015G2912AN62341 FILTER HOUSING PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA RT ENG FIRE WALLCRACKED W O OTHER K FLUID LOSS DEDESCENT 1 CA (CAN) THE PILOT REPORTED THAT THE LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. THE EMERGENCY HAND PUMP SUCCESSFULLY EXTENDED THE GEAR TO INDICATE 3 GREEN. LOW HYDRAULIC FLUID LEVEL WAS FOUND TO BE THE CAUSE OF THE PROBLEM DUE TO A CRACK IN THE THREADS OF THE RT HYDRAULIC FILTER BOWL. THE CRACK IS MOST LIKELY CAUSED BY OVER TIGHTENING THE BOWL, ALTHOUGH IT HAD BEEN IN PLACE 32.5 HOURS BEFORE THE GEAR PROBELM OCCURRED. 1L72 3O3 O A20SO E14EA 20020116000382002011600038SO 2002 1 16 CA011030004 120011015G2140A07D32 SWITCH JANITROL B4050 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HEATER OVERHEATED W FA ACTIVATE FIRE EXT. UNSCHED LANDING BI SMOKE/FUMES/ODORS/SPARKS FLT. ATTITUDE INST. CRCRUISE 1 CA 4B11145 (CAN) THE AIRCRAFT WAS IN LEVEL FLIGHT. THE AFT HEATER WAS BROUGHT ON LINE. A SHORT TIME LATER, THE PASSENGERS NOTED SMOKE AND SPARK'S COMING FROM THE OUTLET. THE HEATER WAS SHUT DOWN AND THE CABIN FIRE EXTINGUISHER WAS DISCHARGED INTO THE INLET. THE AIRCRAFT LANDED AND MAINTENANCE DISCOVERED THE CYCLE SWITCH HAD MALFUNCTION. 1L72 3O3 O A20SO E14EA 20020116000392002011600039CE 2002 1 16 CA011030005 120011009G5743082210045 BRACKET CESSNA CESSNA401 401B 207590ECE CONT O520 TSIO520EB 17040SO MLG CRACKED W A UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 CA (CAN) DURING RETRACTION OF GEAR AFTER TAKEOFF PILOT HEARD A BANG. UPON LANDING AT BASE THE AIRCRAFT WAS INSPECTED AND THE RT FORWARD GEAR DOOR HINGE BRACKET WAS FOUND TO BE CRACKED. 1L72 3O3 O A7CE E8CE 20020116000412002011600041GL 2002 1 16 CA011030007 220011009G7250A23037403 SHAFT ALLSN 250C 250C20B 03013GL ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THIS TURBINE WAS RECD FOR ROUTINE SCHED MAINT. THERE WAS NO SERVICE COMPLAINT. ON DISASSY, TURBINE PT ROTOR NUT FOUND UNTHREADED FROM PT INNER SHAFT. SCORING EVIDENCE ON THE PT INNER SHAFT INDICATES NUT UNTHREADED DURING OP. NUT HAD BEEN STAKED AT 2 PLACES DURING ASSY. LOCKING DIMPLES ON PMA PT INNER SHAFT APPEAR UNDERSIZED WHICH PREVENTS PROPER LOCKING OF NUT ASSY. WHEN NUT UNTHREADED, CLAMPING LOAD BETWEEN NR 3 & NR 4 TURBINE WHEELS WAS COMPROMISED. AS A ARESULT, CURVIC COUPLES ON TURBINE WHEELS SHOW EVIDENCE OF MOVEMENT & FRETTING. TIME ON TURBINE IS AS FOLLOWS:TSN: 10494.0 HRS, TSO: 3476.2 HRS NOTE: PT INNER SHAFT IS A PMA PART. 3 U E4CE 20020116000422002011600042EU 2002 1 16 CA011031001 120011030G3397 WIRE PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL LT WING STROBE CHAFED W H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CRCRUISE 1 CA (CAN) DURING CRUISE, THE STROBE LIGHT CIRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS NOT RESET IN FLIGHT. INVESTIGATION REVEALED A CHAFED WIRE (P/N L08E20) IN THE LEFT HAND WING. THE WIRE WAS REPAIRED AND THE AIRCRAFT RETURNED TO SERVICE. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020116000452002011600045EU 2002 1 16 CA011031005 220011019G8520861115 DIAPHRAGM DIAMONDA20 DA20A1 2990000GL ROTAX 912 ROTAX912 55555EU CYLINDER SWOLLEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING 200 HR INSP OIL FOUND BETWEEN NR 1 & 3 CYLINDERS. COMPRESSION CHECK CARRIED OUT TO DETERMINE CYLINDER THAT PRODUCING OIL. BOTH CYLINDERS PRODUCED NORMAL COMPRESSION READINGS. WHEN BOTTOM SPARK PLUGS WERE REMVD ONE FROM CYLINDER NR 3 FOUND TO HAVE EVIDENCE ON BURNED OIL. NR 3 CYLINDER ASSY & PISTON REMVD. PISTON HEAD COVERED IN BURNED OIL RESIDUE. PISTON HEAD HAD ALSO HAD SMALL PORTIONS OF ITS SURFACE CHIPPED AWAY. DURING THE PREVIOUS INSP (50 HR) NR 1 CYLINDER ASSY & PISTON WERE REPL. IT BELIEVED THAT FAILURE OF NR 1 PISTON RESULTED FROM FAILURE OF PISTON RING. 1L71 3O3 INTTA4CH EXPE3I 20020116000652002011600065SW 2002 1 16 CA011031012 120011018G275012395 PULLEY BBAVIA8 8GCBC 1220803SW LYC O360 O360C2E 41514EA FLAP SYSTEM WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) - LT & RT PULLEYS INBOARD & OUTBOARD ALL FOUND WORN.- LT & RT CABLES FRAYED UNSERVICEABLE AND REPLACED. - CABLES FRAYED AT PULLEYS ON OUTBOARD POSITION.- SOLID ALUMINUM PULLEYS WITH SMALL RADIUS AND SEIZE EASILY CAUSING EXCESSIVE CABLE WEAR. 1H71 3O3 O A21CE E286 20020116000662002011600066SO 2002 1 16 CA011031013 120011004G32134033600 LINK PIPER PA31T PA31T 7103124SO PWA PT6 PT6A28 EA NLG DRAG BRACE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) UPON INSPECTION, A CRACK WAS FOUND AT NOSE GEAR LINK ATTACH POINT. 1L72 3T4 T A8EA E4EA 20020116000672002011600067SO 2002 1 16 CA011031014 120011006G71204000707 MOUNT PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA HARTZLHCE3Y HCE3YR2A GL LT & RT ENGINE WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING INSPECTION OF THE ENGINE MOUNT FOUND CUT MARKS ON LOWER TRUSS MEMBERS OF THE MOUNT. AFTER SOME INVESTIGATION FOUND THAT THE CUTS WERE MADE BY COWL FLAPS OF RESPECTIVE ENGINES. NO EVIDENCE OF COWL FLAP MISRIGGING OR DAMAGE ON COWL FLAPS. THE WEAR MARKS FOUND WERE ABOUT 1/2 THE WALL THICKNESS OF TUBES. TUBES WERE REPAIRED IAW AC43-13 AND AIRCRAFT RETURNED TO SERVICE. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020116000822002011600082SO 2002 1 16 CA011031015 120011006G54144166300 SKIN PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA HARTZLHCE3Y HCE3YR2A GL ENG NACELLES CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING INSPECTION NOTICED SMOKING & LOOSE RIVETS AROUND INBOARD SIDE OF LT AND RT ENGINE NACELLE JUST AFT OF FIREWALL. REMOVED LOWER ACCESS PANEL AND FOUND THAT BOTH LT & RT INBOARD NACELLE PLATES P/N 41663-00 (LT) AND 41663-01 (RT) WERE CRACKED FROM L/E OF PLATE TO AFT END. THIS PLATE CREATE A WRAP AROUND L/E SKIN AND ATTACHES NACELLE STRUCTURE TO SKIN. PART REQUIRED TO BE REPLACED SINCE THERE IS NOT MUCH ROOM TO BE REPAIRED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020116000852002011600085CE 2002 1 16 CA011031016 120011011G28231013890255 SHUTOFF VALVE BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA BOOST PUMP STUCK W D RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 CA (CAN) PILOT CLOSED THE VALVE, BOOST PUMP ON, LOW FUEL PRESSURE LIGHT WENT OFF, MEANING THE FUEL IS LEAKING BY THE VALVE. 1L72 3T4 TRT3A20 E4EA 20020116000862002011600086GL 2002 1 16 CA011031017 120011005G652028135255R GEARBOX ENSTRMF28 280 3300502GL LYC O360 HIO360C1A 41514EA TAIL ROTOR DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING ROUTINE 100 HOUR INSPECTION OIL DRAINED FROM T/R GEARBOX, FOUND EXCESSIVE SLUG & METAL PARTICLES ON CHIP DRAIN PLUG. FLUSHED GEARBOX. ADDED FRESH OIL. DISCONNECT INPUT SHAFT & ROTATED INPUT GEAR WITH T/R ATTACHED TO OUTPUT SIDE. NOISE NOTED FROM INPUT SIDE OF GEAR. ASSEMBLY REMOVED FROM SERVICE AND RETURNED TO ENSTROM FOR WARRANTY AND EVALUATION. REPORT OF FINDINGS REQUESTED. 1G71 3O3 O H1CE 1E10 20020116000872002011600087CE 2002 1 16 CA011031018 120010928G2842 TRANSMITTER CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL FUEL INDICATOR CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) BOTH LT AND RT SENDING UNITS FOUND SEVERELY CORRODED WITH CORROSION DEBRIS IN TANKS. ALUMINUM 3/8 INCH FUEL LINES FROM TANKS TO TRANSFER PUMPS WRE ALSO FOUND CORRODED. 1H71 3O3 O A4CE E5CE 5 CP47GL 20020116000882002011600088CE 2002 1 16 CA011031019 120010928G5751122008516 SKIN CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO MCAULYD3A34 D3A34C404 GL LT AILERON CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) 7 OUT OF 11 SCREW HOLES FOR MOUNTING BALANCE WEIGHT FOUND CRACKED. LT AILERON INSPECTED AND ONE CRACK FOUND. 1H71 3O3 O A4CE E5CE 5 CP47GL 20020116000892002011600089NE 2002 1 16 CA011031021 120011031G5551 ATTACH FITTING CONAERLA4 LA4200 5110310NE LYC O360 IO360A1B 41514EA HORIZONTAL STAB MISMANUFACTURED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AD 98-10-12, HORIZONTAL STAB ATTACHMENT FITTING NO OF NEW CUSTOMERS A/C HAVE BEEN INSPECTED AT COMPANY & ARE NOT IN COMPLIANCE WITH AD, ALTHOUGH ITS BEEN PREVIOUSLY SIGNED OFF. MOST INSPECTIONS REVEAL THAT CLEARANCE I S LESS THAN THE REQUIRED 5/32 INCH. OTHER A/C HAVE HAD FITTING RADIUS REWORKED INSTEAD OF DOUBLER FLANGE.COMPLIANCE IS ALSO BEING ACCOMPLISHED W/O REMOVAL OF STAB FOR FITTING INSP, AS EVIDENT IN REWORK WHICH I S CAUSING GOUGING & MORE DAMAGE TO SPAR DOUBLER&FITTING RADIUS. VISUAL & L. P. INSPECTIONS ARE ALSO NOT COMPLETED ON FITTING RADIUS TO DOUBLER MATING SURFACES. MANY A/C ARE STILL CONSIDERED AIRWORTHY & ARE NOT IN COMPLIANCE. 1H71 3O3 O 1A13 1E10 20020116000902002011600090SO 2002 1 16 CA011031024 120011005G302086245834 HEATER PIPER PA44 PA44180 7104402SO LYC O360 O360A1H 41514EA CARBURETOR BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A ROUTINE ENGINE INSPECTION OF THE LT ENGINE, THE CARB AIR BOX WAS FOUND BROKEN AT THE HEATED AIR INTAKE PIPE. THE COMPLETE CIRCUMFERENCE OF THE WELD ON THE RT END OF THE BOX HAD BROKEN. THE ONLY REASON THE PART STAYED WITH THE AIRCRAFT WAS THE CLAMP ON THE HOSE CONNECTING IT TO THE HEAT INTAKE SHROUD. THE PART WAS REMOVED FOR REPAIR. A SECOND AIRCRAFT WAS FOUND TO HAVE THE SAME PROBLEM. THE PILOT'S WHO FLY THE AIRCRAFT WERE INFORMED THAT IF THEY DO NOT GET A DROP IN RPM WHEN SELECTING CARB HEAT DURING THEIR RUN-UP NOTIFY MAINTENANCE AND A CHECK OF THE CARB HEAT SYSTEM WILL BE CARRIED OUT. 1L72 3O3 O A19S0 E286 20020116000912002011600091EU 2002 1 16 CA011031025 120011005G7120L24263100000 MOUNT ZLIN 242 Z242L 9970204EU LYC O360 AEIO360A1B6 41514EA RT ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A 100 HOUR INSPECTION A CRACK WAS FOUND ON THE UPPER RT MOUNT WEB. THE MOUNT WAS REMOVED FOR FURTHER INSPECTION AND IT WAS NOTICED THAT THE CRACK WAS ABOUT 1 INCH IN LENGTH. MAINTENANCE HAS BEEN INSTRUCTED TO PAY SPECIAL ATTENTION TO THIS AREA DURING 50 AND 100 HOUR INSPECTIONS FOR ANY SIGN OF STRESS OR TINY CRACKS.NOTE: ILLUSTRATION ATTACHED. 1L71 3O3 O0 A76EU 1E10 20020116000922002011600092SW 2002 1 16 CA011031026 120010928G5302205032821023 BULKHEAD BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA TAILBOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A SCHEDULED MAINTENANCE INSPECTION THE CRACK WAS DISCOVERED. HEADQUARTERS HAS RECEIVED THE PARTICULARS AND IS PREPARING A REPAIR SCHEME. 1G71 4U4 U H4SW E22EA 20020116000932002011600093CE 2002 1 16 CA011031027 120011031G324616218000 WHEEL BEECH 99 99 1154002CE PWA PT6 PT6A28 EA MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHEEL HALF WAS REMOVED DUE TO CUTS IN THE RUBBER. UNIT DISASSENBLED AND DYE PEN INSPECTED. CRACK INDICATIONS WERE FOUND ON THE INSIDE OF THE OUTER WHEEL HALF. UNIT SCRAPPED OUT PART TIME AND CYCLES ARE UNKNOWN. 1L72 3T4 T A14CE E4EA 20020116001272002011600127EA 2002 1 16 CA011101011 120011015G5410601350061 WEB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SUPPORT BEAM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM AT THE LOWER WEB FS 630, LBL 36, RBL 36 WHILE PERFORMING SB A601R-53-059. AREA TO BE REPAIRED IAW REO 601R-53-61-361. 2L72 4F4 FRTA21EA E15NE 20020116001282002011600128CE 2002 1 16 CA011101012 120011031G3260903610373 DOWNLOCK SWITCH BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA MLG FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) HIGH RESISTANCE (2.9 OHM) ENCOUNTERED ON CONTACTS AT CONNECTOR A210 PI PINS D TO E WHILE DOING PHASE 1 INSPECTION DUES ITEM CAMP CARD 321171 (CONTINUITY CHECK R/H DOWNLOCK MICRO SW) MICRO SW REPLACED AND RETRACTION TEST CARRIED OUT. 1L72 3T4 TRT3A20 E4EA 20020117000012002011700001SO 2002 1 17 CA011102002 120011018G55539556300 SPAR PIPER PA34 PA34200 7103405SO LYC O360 IO360C1E6 41514EA VERICAL STAB FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FAILURE OF RIVETS SECURING LOWER 4 INCHES OF SPAR FLANGES TO FITTING P/N 63501-00. FOUR RIVETS HAD FAILED ON LT SIDE AND ONE RIVET FAILED ON RT SIDE. 1L72 3O3 O A7SO 1E10 20020117000022002011700002EU 2002 1 17 CA011102003 120011017G6220350A37124520 SCREW AEROSP 355A31000109SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE STARFLEX BROKEN W K NONE O OTHER ININSP/MAINT 1 CA M1429 (CAN) DURING REPLACEMENT OF STARFLEX, DISCOVERY OF ONE OF TWELVE BOLT FOUND BROKEN. PRESENCE OF RUST ON THE BROKEN SECTION, SHOWS THAT THE DEFECT OCCURRED A LONG PERIOD BEFORE DISCOVERY.BECAUSE OFTHE DESIGN OF THE HEAD, THERE WAS NO POSSIBLE WAY TO LOSE ANY PART. NOTE THAT RETIREMENT OF STARFLEX AND BROKEN SCREW IS 2200 HOURS.ATTACHMENT SCREW P/N 350A37-1245-20, S/N 28998 1G71 3U3 UNCH9EU E19EU 20020117000032002011700003WP 2002 1 17 CA011102005 120010815G7921C1861 HUB ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA COOLER FAN CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) PART C186-1 FOUND CRACKED WHILE REPLACING MICROSWITCH V3-1001. THE FAN WAS REMOVED AND THE HUB WAS FOUND CRACKED. THE FAN SHAFT ASSEMBLY C007-5 WAS CORRODED. THE FAN TORQUE WAS FOUND ACCEPTABLE (450-550 FT LBS).\PIECE C186-1 WAS REPLACED AND THE FAN SHAFT C007-5 WAS RETURNED TO ROBINSON FOR OVERHAUL. THE SECOND PROBLEM WAS REPORTED ON 3 OTHER HELICOPTERS IN THE LAST 2/3 YEARS. THE THIRD ONE WAS FOUND CRACK FREE BUT CORRODED. 1G71 3O3 O H11NM E295 20020117000042002011700004EA 2002 1 17 CA011102006 220010506G8530 SPRING CESSNA182 R182 2072734CE LYC O540 O540J3C5 41532EA MCAULY2D34C B2D34C218 GL INTAKE VALVE BROKEN W A UNSCHED LANDING ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) ENGINE VIBRATION WHILE IN FLIGHT. AFTER INSPECTION, THE NR 2 ENGINE CYLINDER WAS FOUND WITHOUT COMPRESSION. THE ADMISSION VALVE WAS FOUND INOPERATIVE. A NEW CYLINDER WAS INSTALLED AND SUCCESSFUL ENGINE TESTS WERE CARRIED OUT. THE CYLINDER WAS SENT TO A REPAIR SHOP FOR INSPECTION AND REPAIR (INTAKE VALVE SPRING BROKEN). 1H71 3O3 ORT3A13 E295 5 CP7EA 20020117000052002011700005CE 2002 1 17 CA011102007 120010731G2720031019613 SPRING CESSNA150 150M 2071830CE CONT O200 O200A 17020SO RUDDER CONTROL BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A PRE-FLIGHT INSPECTION, THE PILOT SAW THE RUDDER TURNED WHILE THE FRONT WHEEL WAS STRAIGHT AND THE PEDALS WERE OFF-CENTERED. AN INSPECTION DETERMINED THE RIGHT SPRING WAS MISSING AND FOUND BELOW IN THE FUSELAGE. 1H71 3O3 O 3A19 E252 20020117000062002011700006EA 2002 1 17 CA011102008 220010802G8510LW14675 CRANKCASE CESSNA182 R182 2072734CE LYC O540 O540J3C5 41532EA MCAULY2D34C B2D34C214 GL ENGINE CRACKED W BA EMER. DESCENT UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) THE PILOT NOTICED AFTER AN HOUR OF FLIGHT THAT THE OIL PRESSURE WAS DROPPING. HE PERFORMED A PRECAUTIONARY LANDING ON THE ROAD WITHOUT ANY PROBLEM. AFTER INSPECTION OF THE ENGINE, A CRACK WAS FOUND ON THE ENGINE BLOCK BETWEEN NR 1 AND 3 CYLINDERS. THE ENGINE WAS REMOVED AND SENT TO A REPAIR SHOP. 1H71 3O3 ORT3A13 E295 5 CP7EA 20020208000062002020800006CE 2002 2 8 CA011102009 120011031G2720031019613 SPRING CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA RUDDER BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THIS IS SECOND OCCURANCE OF SAME DEFECT IN 1205 HRS/18 MONTHS. HAS ALSO OCCURED ON OTHER 152 IN OUR FLEET. OBSERVED DURING WALK-AROUND BY NEXT PILOT (RUDDER SWINGS FREELY WITHOUT NORMAL RESISTENCE). OUR AMO SAYS THAT BROKEN SPRING COULD INTERFERE WITH FLIGHT CONTROLS DURING FLIGHT. 1H71 3O3 ONT3A19 E223 20020117000072002011700007CE 2002 1 17 CA011105001 120011031G7810265400610 FLANGE CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL EXHAUST SYSTEM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE EXHAUST FLANGE WAS FOUND CRACKED AT THE FORWARD RADIUS IN 3 SPOTS. THERE IS A HOLE IN THE FLANGE THAT LINES UP WITH THE THREADS OF A BOLT FROM THE OIL COOLER. THIS HOLE DID NOT LINE UP WITH THE BOLT AND PRODUCED STRESS ON THE FLANGE RESULTING IN THE CRACKS. THE FLANGE WAS REPLACED AND THE BOLT FROM THE OIL COOLER WAS SHORTENED SO IT DOES NOT INTERFERE WITH THE FLANGE. 1H71 3T3 T A37CE E4EA 5 CP60GL 20020117000082002011700008SW 2002 1 17 CA011105002 120010925G6320206040526001 TUBE BELL 206040004101BELL 206 206L 1181522SW ALLSN 25OC 250C20R GL TRANSMISSION CORRODED W K NONE O OTHER ININSP/MAINT 1 CA BMC45132 (CAN) DURING TRANSMISSION 1500 HOUR INSPECTION CORROSION AND PITTING FOUND ON THE FLARE OF THE TUBE ASSEMBLY. 1G71 3U3 U H2SW E4CE 20020117000092002011700009SW 2002 1 17 CA011105003 120010921G291070012J220W234 LINE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA HYD SYSTEM LEAKING W D RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 CA (CAN) DURING RUN UP THE SUBJECT LINE STARTED LEAKING, THIS WAS REPORTED BY PASSENGERS IN AIRCRAFT WHO NOTICED HYDRULIC FLUID LEAKING INTO CABIN FROM OVERHEAD.AIRCRAFT WAS SHUT DOWN AND THE AME LOCATED THE LEAKING LINE ON NR 2 HYDRAULIC SYSTEM. THIS LINE WAS LAST PRESSURE TESTED 10/98. NEW LINE WILL BE INSTALLED PRIOR TO AIRCRAFT RETURN TO SERVICE. 1G71 4U4 U H4SW E22EA 20020117000102002011700010CE 2002 1 17 CA011105004 120011104G275299105863RX ACTUATOR CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE TE FLAPS STUCK W A UNSCHED LANDING F FLT CONT AFFECTED DEDESCENT 1 CA (CAN) PILOT REPORTED IN FLIGHT FAILURE OF FLAP SYSTEM LOCKED IN ONE POSITION. RETURNED TO MAINTENANCE BASE AND REPLACED FLAP ACTUATOR. AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 20020117000112002011700011NE 2002 1 17 CA011105005 220010526G7261 LABYRINTH SEAL SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S 60030NE ENGINE FAILED W E ENGINE SHUTDOWN BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN) TEARDOWN REPORTS - SEVERE FAILURE OF LABYRINTH SEAL. SMALL DIAMETER ROTATING LABYRINTH SEAL ALMOST COMPLETELY DISINTEGRATED. SMALL PIECES RECOVERED. OUTER TWO ROTAING SEALS SEPERATED FROM LABYRINTH SHAFT. ACRO AEROSPACE W/O 21-8077PARTS SHIPPED TO TURBOMECA FRANCE FOR ANALYSIS. 1G72 3U3 U H1NE E19EU 20020117000122002011700012SO 2002 1 17 CA011105006 220011001G7321632558 LINK ROD CONT IO470VO CESSNA310 310Q 2074242CE CONT O470 IO470VO 17026SO MCAULY3AF32C3AF32C87 GL FCU DISCONNECTED W O OTHER EJ VIBRATION/BUFFET WARNING INDICATION APAPPROACH 1 CA 170718R (CAN) ON APPROACH PILOT NOTICED ROUGHNESS FROM LEFT ENGINE AND UPON LANDING REPORTED THAT THE LEFT ENGINE WOULD NOT IDLE UNLESS MIXTURE PULLED BACK HALFWAY. INSPECTION REVEALED THAT THE COTTER PIN WHICH HOLD THE MIXTURE INTERCONNECT ROD TO THE THROTTLE VALVE HAD BROKEN AND THE ARM FELL OFF ALLOWING NO MIXTURE ADJUSTMENT WITH THROTTLE MOVEMENT AS REQUIRED. NEW COTTER PIN INSTALLED, AIRCRAFT GROUND RUN AND CHECKED SERVICEABLE. ADDITIONAL CHECK CARRIED OUT TO ALL CYLINDERS, COMPRESSION AND BORESCOPE REVEALED NO APPARENT DAMAGE CAUSED AIRCRAFT RETURNED TO SERVICE. 1L72 3O3 O 3A10 3E1 5 CP22EA 20020117000132002011700013CE 2002 1 17 CA011105014 120010731G325007430118 ARM CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA NLG STEERING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THIS PROBLEM WAS DISCOVERED DURING THE AIRCRAFTS ANNUAL INSPECTION. THE CRACK IS ALL OF THE WAY THROUGH THE FORWARD SIDE OF THE ARM, VERTICALLY ORIENTED AND PASSES THROUGH THE GREASE FITTING HOLE.IT APPEARS TO HAVE ORIGINATED AT THE FILLET FORMED BY THE RIGHT SIDE OF THE STEERING STOP LUG, AND THE UPPER MACHINED SURFACE OF THE ARM. ALL RELEVANT STEERING PARTS ARE SERVICEABLE AND THERE IS NO APPARENT CAUSE FOR THE CRACK. 1H71 3O3 ONT3A12 E274 20020117000142002011700014EA 2002 1 17 CA011105015 220011015G8500 CASE CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA ENGINE CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) CRACK FOUND IN CASE AROUND FORWARD UPPER THROUGH BOLT. 1H71 3O3 ONT3A12 E274 20020117000152002011700015EU 2002 1 17 CA011105016 120011005G63204638001009 GEARBOX BOLKMS105 BO105C 5626005EU ALLSN 250C 250C20B 03013GL MAIN ROTOR MAKING METAL W E ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN) ON ENGINE START UP - PILOT REPORTED MGB CHIP LIGHT ON, PULSED OFF AND 4 SECONDS LATER LIGHT BACK ON. ENGINE SHUT DOWN, MAG PLUG PULLED 2 SMALL FLAKED AND SOME FUZE ON PLUG. FINE OIL FILTER REMOVED AND FOUND TO BE CONTAMINATED WITH NUMEROUS, VARIOUS SIZED PARTICLES. AIRCRAFT REMOVED FROM SERVICE PENDING MGB CHANGE. 1G72 3U3 U H3EU E4CE 20011108000082001110800008EU 2001 11 8 CA011105017 120011015G291362052RSIMT47CR BEARING AEROSP 350A35013004SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE INTERNAL BROKEN W AL UNSCHED LANDING ABORTED APPROACH FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 CA (CAN) DURING TAKEOFF/CLIMB OUT OF A WOODED AREA, THE PILOT GOT A HYDRAULIC LIGHT INDICATION. HE LATER REPORTED THAT THE AIRCRAFT HAD A COMPLETE HYDRAULIC FAILURE. THE CAUSE OF THE FAILURE WAS DUE TO A BEARING FAILURE IN THE HYDRAULIC DIVE PULLEY, THE CAGE OR THE BEARING HAD BROKEN APART CAUSING THE PULLEY ASSEMBLY TO SEIZE AND THE HYDRAULIC BELT TO BREAK. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. 1G71 3U3 U H9EU E19EU 20020117000162002011700016SO 2002 1 17 CA011105018 120010816G3230455180 STRUCTURE PIPER PA30 PA30 7103002SO LYC O320 IO320B1A 41508EA MLG GALLED W O OTHER R PARTIAL RPM/PWR LOSS LDLANDING 1 CA (CAN) IT WOULD APPEAR, UPON INVESTIGATION THAT A PIECE OF MATERIAL FROM THE INNER ATTACHMENT (TELEFLEX) BROKE AND BECAME LODGED BETWEEN IT AND THE OUTER PORTION (SLIDE) AND CAUSED GALLING/SCORING WHICH JAMMED THE U/C AND WOULD NOT ALLOW GEAR TO EXTEND. AFTER MUCH EFFORT THE GEAR WAS EXTENDED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. 1L72 3O3 O A1EA 1E12 20020208000552002020800055NE 2002 2 8 CA011107001 120011004G32465003450 WHEEL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHEEL SUBASSEMBLY FOUND CRAKED WHILE INVESTIGATING SLOW LEAK. 1G72 3U3 U H1NE E1GL 20020117000172002011700017EU 2002 1 17 CA011108001 120011029G6210350A11001007 BLADE SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING INSPECTION A CRACK WAS FOUND ON THE LOWER SURFACE OF THE BLADE AT STN. 1003. CRACK LENGTH WAS APPROXIMATELY 155.52 MM STARTING 111.46 FROM THE LEADING EDGE TRAVELLING CORDWISE TO 33.02 MM FROM THE TRAILING EDGE. 1G71 3U3 U H9EU E19EU 20020117000182002011700018NE 2002 1 17 CA011108002 220011023G853071166 EXHAUST VALVE BEECH 18 TC45G 1151016CE PWA R985 R985AN14B 52008NE ENGINE FAILED W O OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION LDLANDING 1 CA (CAN) NR 1 EXHAUST VALVE HEAD BROKE OFF CONTACTING PISTON AND BENDING CONNECTING ROD. 1L72 3R3 R A765 5E1 20020117000192002011700019CE 2002 1 17 CA011108003 120011106G2730505244325 BRACKET BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA ELEVATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 1532015320 (CAN) WHILE CONDUCTING THE INSPECTION OF THE ELEVATOR PULLEY BRACKETS IAW BEECH SB 2150 ELEVATOR PULLEY BRACKET PART NR 50-524432-5 AND 50-524432-7 WERE FOUND CRACKED. SERVICE KIT NR 90-4098-1 S INSTALLED IN ACCORDANCE WITH BEECH SB 2150 REVLL 1L72 3T4 T A14CE E4EA 20020117000212002011700021NM 2002 1 17 CA011108007 120011029G7602600035549 CONTROL CABLE PIPER PA60 PA60600 7106001NM LYC O540 IO540K1J5 41532EA MIXTURE CONTROL SEPARATED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING ANNUAL INSPECTION THE ENGINES WERE BEING REMOVED FOR REPLACEMENT. DURING INSPECTION OF THE ENGINE CONTROLS, BOTH THE LT MIXTURE CONTROL CABLE P/N 600035-549 AND RIGHT HAND MIXTURE CONTROL CABLE P/N 600035-547 WERE FOUND TO BE SEPARATED AT THE SWAGED END. THE LT CABLE HAD A TIME OF 2125.8 HOURS SINCE NEW. TIME ON R/H CABLE UNKNOWN. THE CABLES WERE REPLACED WITH SERVICEABLE UNITS. 1M72 3O3 ORTA17WE 1E4 20020117000272002011700027EA 2002 1 17 CA011108011 220011029G74141038291018 MAGNETO PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA RT ENGINE DAMAGED W EA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) DURING CRUISE FLIGHT THE RT ENGINE SURGED ONCE AND THEN FAILED. CREW BELIEVE RPM REMAINED NORMAL BUT MANIFOLD PRESSURE DROPPED TO 20 INCH HG THEN BACK UP AND AGAIN DOWN TO 20 INCH. ELECTRIC FUEL PUMP WERE TRIED BUT DID NOT HELP SO ENGINE WAS SHUT DOWN AND NORMAL LANDING CARRIED OUT ON ONE ENGINE. 1L72 3O3 O A20SO E14EA 20020208000572002020800057EA 2002 2 8 CA011108012 220011031G8520STD1065 DOWEL PIN BNORM BN2 BN2A 1520204EU LYC O540 O540E4C5 41532EA CRANKSHAFT SHEARED W E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 CA (CAN) DURING CRUISE JUST PRIOR TO LANDING IN YVR, LT ENGINE BEGAN TO RUN VERY ROUGH WITH MOST OR ALL POWER LOSS. PILOT SHUT ENGINE DOWN AND LANDED NORMALLY IN YVR. PRELIMINARY INVESTIGATION FOUND BOTH VALVE AND MAG TIMING TO HAVE ALTERED SIGNIFCANTLY. 1H72 3O3 O A17EU E295 20020117000282002011700028EU 2002 1 17 CA011108013 120011107G30973E23602 WIRE PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL DEICE HARNESS BROKEN W K NONE L NO TEST ININSP/MAINT 1 CA (CAN) PILOT REPORTED PROP DE-ICE SYSTEM OPERATING INTERMITTENTLY. INVESTIGATION REVEALED THAT THE GROUND WIRE IN THE HARNESS BETWEEN THE BACKING PLATE TERMINAL BLOCK AND THE BLADE DE-ICER BOOT WAS BROKEN INTERNALLY. WITH FEATHERING AND UNFEATHERING OF THE PROPELLOR THE HARNESS IS CONSTANTLY BENDING THE WIRES CAUSING THE BREAKAGE. THE WIRE APPEARS TO HAVE MADE CONTACT WITH THE TWO BROKEN ENDS CAUSING THE WIRE ENDS TO ARC TOGETHER THUS GIVING THE INTERMITTENT OPERATION OF THE SYSTEM. THE HARNESS WAS REPLACED WITH NEW AND SYSTEM FUNCTIONED NORMALLY. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020117000292002011700029EU 2002 1 17 CA011109002 120010808G3240NB73A4354 LINE BNORM BN2 BN2A27 1520227EU LYC O540 O540E4C5 41532EA RT MLG BRAKE CHAFED W D RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CA 17401 (CAN) ONE OF THE TWO BRAKE LINES THAT RUN DOWN THE LEG CHAFED THROUGH AT THE TOP CLAMP. BRAKES WERE SOFT ON THAT SIDE. 1H72 3O3 O A17EU E295 20020117000302002011700030SO 2002 1 17 CA011109003 120011109G32304204200 LINK PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA MLG BROKEN W O OTHER D INFLIGHT SEPARATION LDLANDING 1 CA (CAN) LINK FAILED AFTER TAKEOFF AND GEAR WOULD NOT COME UP. FORTUNATELY IT WENT BACK DOWN AND AIRCRAFT LANDED NORMALLY. IT COULD HAVE BEEN WORSE VERY EASILY. I WAS ALSO INFORMED BY OPERATOR THAT THIS IS THE SECOND TIME THAT THIS HAS HAPPENED. 1L72 3O3 O A20SO E14EA 20020117000362002011700036SO 2002 1 17 CA011109004 120010917G3242753407 BOLT CLEVELAND 3095A PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA BRAKE ASSY BROKEN W O OTHER D INFLIGHT SEPARATION LDLANDING 1 CA (CAN) UPPER TORQUE PIN (ANCHOR PIN) FAILED ALLOWING BRAKE TO ROTATE INTO BACK OF MAIN LANDING GEAR STRUT. ALSO INSIDE SURFACE OF MAIN WHEEL SCORED. PIPER ANCHOR BOLT P/N 753-407 CLEVELAND ANCHOR BOLT P/N 69-4 1L72 3O3 O A20SO E14EA 20020117000372002011700037CE 2002 1 17 CA011109006 120011023G533097400021101 SKIN BEECH 100 100BEECH 1152916CE PWA PT6 PT6A28 EA FUSELAGE CHAFED W K NONE O OTHER ININSP/MAINT 1 CA 10337 (CAN) DUE TO THE ANGLE OF CONTACT BETWEEN THE WING CENTRE SECTION TO FUSELAGE FILLET P/N 50-420023-37 AND -38 AND THE FUSELAGE SKIN P/N 97-400021-101 AND -102 WHEN THE RIVETS WORK LOOSE IN THE FILLET IT IS ALLOWED TO CHAFE INTO THE FUSELAGE SKIN. THIS SKIN IS A PRESSURE SKIN AND REQUIRES ENGINEERING APPROVED FOR REPAIRS.TO REDUCE RECURRENCE OF THIS PROBLEM THERE SHOULD BE AN ANTI-CHAFE MEDIUM BETWEEN FILLET AND SKIN, I.E. PRC 1422-B 1/2 AND RIVETS SHOULD BE KEPT IN TOP CONDITION, FIXING ANY DEFECTS AS THEY OCCUR. 1L72 3T4 T A14CE E4EA 20020117000392002011700039SW 2002 1 17 CA011109007 120011024G6520204001739003 SEGMENT BELL 204 204B 1181404SW LYC T53 T5311B 41549NE T/R G/B CHAIN MISSING W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) UPON INSTALLATION OF THE NEW CHAIN, THE ENGINEER NOTICED A SPACE BETWEEN SOME CHAIN LINKS. CHAIN IS MISSING A SEGMENT. 1G71 4U4 U H1SW E1EA 20020117000402002011700040EU 2002 1 17 CA011109008 120011009G6710350A2705510602 FRICTION RING SNIAS 350 AS350D 8680803EU LYC LTS101LTS101600A2 41560NE MAIN ROTOR FAILED W O OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 CA (CAN) LOCK PIN NR 10 EITHER NOT PROPERLY INSTALLED OR CAME LOOSE ALLOWING NUT NR 9 TO VIBRATE LOOSE FROM LOWER THREAD PORTION OF COLLAR NR 8, THIS ALLOWED THE ENTIRE FRICTION ASSY TO BE LIFTED BY HAND. THIS COULD EASILY THEN CAUSE BINDING OR LIMIT CYCLIC MOVEMENT. COLLAR NR 8 IS DRILLED TO ACCEPT THE LOCK RING. ALL PARTS EXAMINED AND REINSTALLED TO ENSURE PROPER LOCKING EFFECTIVENESS. 1G71 3U3 U H9EU E5NE 20020117000412002011700041WP 2002 1 17 CA011109010 220011009G72618971973 DRIVE SHAFT GARRTTTPE331TPE33110UA 01514WP SCAVE PUMP DAMAGED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) ON INSPECTION OF PARTS REMOVED FROM P-63110 AT TIME OF OVERHAUL IT WAS NOTED THAT THE FRONT SCAVENGE PUMP DRIVE SHAFT SAFTY COLLER IS 0.210 SMALLER THAN THE REPLACEMENT PART THIS CAN ALLOW THE SHAFT TO ENTER THE PUMP TO FAR AND ALLOW THE FUEL DRIVE SYSTEM TO UNCOUPPLE. ON SDR 20001206012 THE SAME PROBLEM WAS NOTED ON ENGINE S/N P-63111. 4 T E4WE 20020117000422002011700042SO 2002 1 17 CA011109014 120011013G5710 FASTENER EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA LT MLG SHEARED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A 12C INSPECTION (7200 HOUR) MAINTENANCE PERSONNEL FOUND SEVERAL SHEARED HILOCKS ON THE LEFT HAND WING AT RIB NR 6.THE LEFT HAND LANDING GEAR WAS REMOVED AND AREA INSPECTED, NO STRUCTURAL DAMAGE WAS FOUND. 22 HILOCKS WERE REPLACED AND GEAR REINSTALLED. THE SAME INSPECTION WAS COMPLETED ON THE RIGHT HAND SIDE AND NO DEFECTS WERE NOTED. A GEAR SWING WAS COMPLETED AND AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4T4 T A21SO E4EA 20020117000522002011700052EU 2002 1 17 CA011113007 120011113G30603E23602 WIRE PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL DEICE HARNESS BROKEN W O OTHER J WARNING INDICATION CRCRUISE 1 CA (CAN) DURING PROP DEICE OPERATION THE SYSTEM INDICATED A FAILURE.UPON INVESTIGATION / TROUBLESHOOT IT WAS FOUND THE HARNESS P/N 3E23060-2 HAD AN INTERNAL BREAK WITH LITTLE OR NO CONTINUITY WHILE MOVING THE HARNESS AS INSTALLED.PART WAS REMOVED NEW ONE INSTALLED SYSTEM TESTED SERVICEABLE. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020208000592002020800059EA 2002 2 8 CA011113017 120010111G541060135006 SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE PUMP CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 12120 (CAN) FOUND THREE CRACKS DURING CHECKS. CRACKED AT FS 630 & 640, LT & RT BL 36 & 00. 2L72 4F4 FRTA21EA E15NE 20011212000112001121200011EU 2001 12 12 CA011114001 120011001G5230D2586 LATCH DART D350600042 SNIAS 350 AS350D 8680803EU LYC LTS101LTS101600A3 41560NE LATCH FAILED W B EMER. DESCENT DD INFLIGHT SEPARATION INFLIGHT SEPARATION CRCRUISE 1 CA (CAN) PRIOR TO COMMENCING HIS FLT PILOT HAD REMVD SEAT CUSHIONS&STOWED THESE IN SIDE CARGO COMPT POD. DURING FLT POD "DOOR OPEN" LIGHT ILLUMINATED WHICH FOLLOWED BY LOUD BANG&SEVERE VIBRATIONS. PILOT IMMEDIATELY LANDED&FOUND THAT R/H POD DOOR HAD OPENED&SEAT CUSHION HAD FALLEN OUT STRIKING TAILBOOM&TAIL ROTOR WHILE IN FLT. REAR LATCH INSIDE LOCK BROKEN&SUBSTANTIAL DAMAGE TO A/C. FWD LATCH APPEARED UNDAMAGED BUT NOT POSITIVELY LATCHED. IT APPEARS THAT FWD LATCH MAY HAVE ALLOWED FRONT EDGE OF POD DOOR TO OPEN IN FLT AFTER WHICH PRESSURE FROM SLIPSTREAM PROBABLY BROKE REAR LATCH DUE TO EXCESSIVE PRESSURE B EING EXERTED ON DOOR. ALLOWED DOOR T 1G71 3U3 U H9EU E5NE 20020117000722002011700072CE 2002 1 17 CA011114014 120011011G7120045111432 MOUNT CESSNA150 150M 2071830CE CONT O200 O200A 17020SO ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A 50 HOUR INSPECTION THE ENGINE MOUNT WAS FOUND CRACKED. THE SUPPORT WAS REPLACED. 1H71 3O3 O 3A19 E252 20020117000732002011700073SO 2002 1 17 CA011114015 120011024G57516210500 HINGE PIPER PA32 PA32300 7103212SO LYC O540 IO540K1A5 41532EA LT AILERON CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING AN INSPECTION AN ONE AND A HALF INCH CRACK WAS DETECTED ON THE DOUBLER HINGE OUTSIDE OF THE LEFT AILERON. 1L71 3O3 O A3SO 1E4 20020211000052002021100005EU 2002 2 11 CA011114016 120011102G63204619302046 BEARING BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL M/R GEARBOX PEELING W O OTHER J WARNING INDICATION NRNOT REPORTED 1 CA (CAN) CHIP LIGHT INDICATION.GEARBOX DISASSEMBLED FOR INVESTIGATION.BEARING PLATING FOUND PEELING.REPLACED WITH NEW 1G72 3U3 UNCH3EU E4CE 20020205001222002020500122EU 2002 2 5 CA011114017 120011114G63204619310072 BEARING BOLKMS 4619002003 BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL INPUT DEFECTIVE W O OTHER J WARNING INDICATION ININSP/MAINT 1 CA 1112 (CAN) BOTH INNER AND OUTER RACE OF BEARING DISPLAYED MODERATE PITTING AND PEELING 1G72 3U3 UNCH3EU E4CE 20020117000762002011700076NE 2002 1 17 CA011114018 120011030G77129609000254 BEARING SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S1 60030NE TORQUEMETER FAILED W L ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 CA (CAN) SUBJECT: ESN 15051- PARTICLES ANALYSIS. WE HAVE RECEIVED THE ANALYSIS RESULTS OF THE PARTICLES FOUND ON THE MODULE 05 S/N¦ 03199¦ MAGNETIC PLUG . THE PARTICLES¦ ARE 100 C6 MATERIAL AND HAVE AS THE ORIGIN ONE OF THE HYDRAULIC TORQUEMETER BEARINGS ("TRIPLEX") . 1G72 3U3 U H1NE E19EU 20020117000782002011700078SW 2002 1 17 CA011116001 120011107G521090000949722 PUSHROD GULSTM690TP 690A 0141722SW GARRTTTPE331TPE3315251K NM PAX DOOR BENT W O OTHER O OTHER CLCLIMB 1 CA (CAN) DURING CLIMBOUT THE AIRCRAFT PRESSURIZATION REDUCED FROM 4.8 PSI TO 3.5 PSI. UPON INVESTIGATION IT WAS NOTED THAT THE LOWER AFT ENTRANCE DOOR BAYONET WAS NOT EXTENDING INTO THE AIRFRAME. THE TWO PUSHRODS P/N'S 900009-49-7.22 AND 900009-49-9.70 WERE FOUND BENT WHICH CAUSED THE BAYONET NOT TO EXTEND INTO THE AIRFRAME. THE PUSHRODS WERE REPLACED AND THE CABIN DOOR MECHANISM WAS RE-RIGGED. DOOR OPERATIION WAS CHECKED, THE DOOR SEAL WAS INSPECTED AND A PRESSURIZATION CHECK WAS COMPLETED AND CHECKED SERVICEABLE. THE AIRCRAFT WAS RETURNED TO SERVICE. 1H72 3T4 T 2A4 E2WE 20020211000062002021100006 2002 2 11 CA011116002 420011107G6122A20609 CONTROL ARM MCAULY C290D3RT9 CESSNA185 A185E 2072818CE CONT O520 IO520D 17032SO MCAULY2A34C D2A34C58 GL PROP GOVERNOR MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 CA 010596 (CAN) GOVERNOR WOULD NOT CYCLE PROP BELOW 1500 RPM. CONTROL ARM INSTALLED IN THE INCORRECT POSITION ON CONTROL SHAFT. 1H71 3O3 O 3A24 E5CE 5 CP3EA 20020117000802002011700080SW 2002 1 17 CA011116003 120011023G6230269A21725 SUPPORT HUGHES269 269C1 8059504SW LYC O360 HO360C1A 41514EA M/R MAST CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AFT MAIN ROTOR MAST SUPPORT (TAILBOOM TO M/R GEARBOX MAST). 1G71 3O3 OO 4H12 E286 20020117000822002011700082SW 2002 1 17 CA011116004 120011107G6230269A21725 SUPPORT HUGHES269 269C1 8059504SW LYC O360 HO360C1A 41514EA M/R MAST CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AFT MAIN ROTOR MAST SUPPORT (TAILBOOM TO MAIN ROTOR GEARBOX MAST) 1G71 3O3 OO 4H12 E286 20020117000902002011700090EA 2002 1 17 CA011116005 120011023G7714659450105 INDICATOR DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE ENG TRIPLE GAUGEEXPLODED W O OTHER O OTHER LDLANDING 1 CA (CAN) ENGINE TRIPLE GAUGE EXPLODED: - CASE SPLIT (TOTAL CIRCUMFERENCE). - 1 LARGE PORTION OF CASE BROKEN OFF. - FRONT GLASS FACE PLATE SHATTERED OUTWARD SLIGHTLY INJURING PASSENGER IN CO-PILOT SEAT. 1H71 3R3 R A806 5E1 20020117000912002011700091NE 2002 1 17 CA011116006 120011029G62207610308010049 HUB SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL2B NE M/R DAMPER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) A CRACK APPROXIMATELY 2.5 CM, EXTENDING INBOARD FROM BUSHING BORE ON UPPER LUG OF RED MAIN ROTOR DAMPER SUPPORT. 1G72 3U3 UNCH1NE E00054EN 20020117000922002011700092SW 2002 1 17 CA011116007 120010908G3212108839 REGULATOR BELL 222 222U 1182140SW LYC LTS101LTS101750C1 41560NE MLG FLOAT LEAKING W K NONE L NO TEST ININSP/MAINT 1 CA (CAN) AIRCRAFT BELL 222U POP-OUT FLOAT SYSTEM CHARGED TO 3000 PSI AFTER CHANGING FLOAT BOTTLE. SYSTEM LEAKED APPROXIMATELY 200 PSI OVER A 12 HOUR PERIOD. BY REMOVING THE LINES TO AIR BAG IT WAS CONFIRMED THAT AIR WAS LEAKING THROUGH SHEAR HEAD BY SMALL CRACKS. THE SHEAR HEAD IS TO MAINTAIN 3000 PSI IN THE FLOAT BOTTLE TILL FLOATS ARE DEPLOYED. 1G72 3U3 U H9SW E5NE 20020117000932002011700093EU 2002 1 17 CA011116009 120010711G6220704A33633160 BUSHING AEROSP 350A31190701SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE M/R SPIDER DEBONDED W K NONE O OTHER ININSP/MAINT 1 CA M1012 (CAN) BOLT P/N 22208BC10001GL BACKED OUT ALLOWING DEBONDED BUSHING P/N 704A33-633-160 TO MOVE OUTWARD APPROXIMATELY 1/4 INCH ON THE OUTBOARD END OF THE RED ARM. DAMAGE WAS DISCOVERED ON A DAILY INSPECTION. PILOT HAD COMPLAINED OF VIBRATION ON GROUND WHILE RUNNING.ON REPLACEMENT OF THE STAR, BEARING P/N 11-7775P IN THE FREQUENCY ADAPTER WAS FOUND WITH EXCESSIVE PLAY ON THE SAME ARM. 1G71 3U3 U H9EU E19EU 20020117000942002011700094EU 2002 1 17 CA011116010 120011109G6720350A33105803 BELLCRANK AEROSP 350A33105803SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE T/R CONTROL CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AS PER A COMPANY MEMO TO CHECK THIS LEVER/BELLCRANK FOUND ANOTHER ONE CRACKED IN THE SAME REGION (SEE ATTACHED DOCUMENT). NOTE: THE FIRST SDR SUBMITTED THE ARROWS WERE POINTING IN THE WRONG REGION. THE ARROWS SHOULD BE MORE OUTBOARD FROM WHERE THEY WERE POINTING. THIS WAS C-FSPR DATED 01/10/25 CONTROL NUMBER UNKNOWN.SDR CONTROL #20011029017 (C-FSPR) 1G71 3U3 U H9EU E19EU 20020211000072002021100007 2002 2 11 CA011116011 420011029G3422200DC GYRO HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL COCKPIT SHORTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 CA 2909 (CAN) ON FINAL FOR LANDING, PILOT AND PASSENGERS NOTICED AN ELECTRICAL SMELL, SECONDS LATER WHITE SMOKE FILLED THE CABIN COMING FROM BEHIND INSTRUMENT PANEL. ALL CIRCUIT BREAKERS WERE PULLED AND AIRCRAFT SHUT DOWN. INSPECTION REVEALED DIRECTIONAL GYRO HAD SHORTED INTERNALLY AND MELTED DOWN. 1G71 3U3 U H3WE E4CE 20020117000952002011700095NM 2002 1 17 CA011116012 120011115G291082970010249 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYD SYSTEM LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA 30700 (CAN) THE FLIGHT CREW NOTICED FLUID LEAKING FROM THE LEFT NACELLE DURING THEIR WALK-AROUND INSPECTION.MAINTENANCE FOUND THE "MLG DOWN PRESSURE" HYDRAULIC TUBE LEAKING FROM A PIN HOLE UNDER THE EXHAUST SHROUD. THE RIGID TUBE WAS TEMPORARILY REPLACED WITH TWO FLEXIBLE HOSES AS PER AMM 20-50-52. THE SYSTEM WAS TOPPED UP AND LEAK CHECKED PRIOR TO RETURNING THE AIRCRAFT TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20020117000962002011700096CE 2002 1 17 CA011116013 120011105G2752C145350 ACTUATOR CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL TE FLAPS SEIZED W O OTHER O OTHER DEDESCENT 1 CA (CAN) ON APPROACH FLAPS SELECTED FROM 10 TO 20 AS FLAPS TRAVELLED THROUGH APPROXIMATELY 15 DEGREES THE FORWARD FLAP MOTOR FAILED AND BROKE FREE OF THE TRANSMISSION/JACKSCREW ASSY. THIS CAUSED THE FLAP ACTUATOR ASSEMBLY TO BRAKE FREE OF THE ATTACHING STRUCTURE, THUS CAUSING THE FLAP TO RAPIDLY RETRACT TO THE STOWED POSITION. 1H71 3T3 T A37CE E4EA 5 CP60GL 20020117000972002011700097SO 2002 1 17 CA011116014 220011106G73146462121 PUMP CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULY2A34C D2A34C58 GL FUEL FAILED W A UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 CA (CAN) DURING CLIMB AFTER TAKEOFF FROM RUNWAY 16 AT YYC WHEN THE PILOT ADJUSTED THROTTLE AND MIXTURE THE ENGINE STOPPED PRODUCING POWER. AN EMERGENCY LANDING WAS CARRIED OUT ON THE END OF RUNWAY 16. 1H71 3O3 O 3A24 E5CE 5 CP3EA 20020205001232002020500123SW 2002 2 5 CA011116015 120011101G6320204040135001 BEARING BELL 212040001123BELL 212 212 1181420SW PWA PT6T PT6T3B 52045NE BEARING FAILED W A UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 CA ABW40334 (CAN) WHILE IN DESCENT TO THE LANDING AREA THE MAIN ROTOR TRANSMISSION CHIP LIGHT ILLUMINATED. THE PILOT MAINTAINED ITS APPROACH AND LANDED. UPON INSPECTION ON THE CHIP DETECTOR METAL WAS FOUND AND THEN THE WAFFER FILLER WAS CHECKED WHERE MORE METAL WAS FOUND. MAIN ROTOR TRANSMISSION CHANGED. 1G71 4U4 U H4SW E22EA 20020211000082002021100008CE 2002 2 11 CA011116016 120010611G3221 TAIL WHEEL CESSNA180 180H 2072618CE CONT O470 O470* 17026SO MCAULY2A34C 2A34C66 GL MLG SEPARATED W O OTHER WD INADEQUATE Q C INFLIGHT SEPARATION CLCLIMB 1 CA (CAN) AFTER TAKEOFF FROM ROUGH STRIP ON HERSEL ISLAND, PILOT HEARD LOUD BANGING SOUND. HE WAS ABLE TO SEE TAIL WHEEL MISSING. ON LANDING AT AKLAVIK, STEERING CONTROL LOST. MINOR DAMAGE TO TAIL STRINGER. NEW TAIL WHEEL ASSEMBLY INSTALLED WITH PROPER AIRCRAFT BOLTS. THE AIRCRAFT RETURNED TO SERVICE. THE CAUSE WAS FOUND TO BE A NON AIRCRAFT BOLT HOLDING ASSEMBLY ON. 1H71 3O3 O 5A6 E273 5 CP3EA 20020117000982002011700098EA 2002 1 17 CA011116017 220011102G8520LW1594485 CRANKSHAFT CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA ENGINE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CORROSION FOUND UNDERNEATH URETHABOND COATING APPLIED BY FACTORY AT OVERHAUL AS PER SB 505B AND SB 530A AND AD 98-02-08.CRANKSHAFT HAS BEEN RETURNED TO FACTORY FOR WARRANTY CONSIDERATION AND INSPECTION. 1H71 3O3 ONT3A12 E274 20020117000992002011700099CE 2002 1 17 CA011116018 120011108G561010138402521 WINDSHIELD BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA COCKPIT CRACKED W O OTHER O OTHER CRCRUISE 1 CA (CAN) THE AIRCRAFT WAS IN CRUISE AT FLIGHT LEVEL 290, APPROXIMATELY 50 MILES NW OF SUDBURY, ONTARIO, ENROUTE FROM THUNDER BAY TO THETFORD MINES, QUEBEC, WHEN THE LT WINDSHIELD INNER PANE SHATTERED. THE CREW REDUCED PRESSURIZATION TO 4 PSI DIFFERENTIAL PRESSURE AS PER FLIGHT MANUAL PROCEDURES AND DIVERTED TO QUEBEC CITY.THE CREW REPORTED THAT THE WINDSHIELD HEAT WAS IN THE "HIGH" SELECTION AND THAT THE OAT WAS -36 DEGREES C AT THE TIME OF THE OCCURRENCE. 1L72 4T4 T A24CE E4EA 20020117001012002011700101CE 2002 1 17 CA011116020 120011106G5610101384002522 WINDSHIELD BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA HARTZLHCD4N3HCD4N3A GL COCKPIT FAILED W O OTHER O OTHER APAPPROACH 1 CA (CAN) ON APPROACH INTO CIGAR LAKE, SASKATCHEWAN (JWY) THE RIGHT HAND WINDSHIELD INNER PANE SHATTERED IN A LATTICE LIKE MODE. THE NETWORK OF CRACKS EXTENDED OVER THE ENTIRE INNER SURFACE OF THE SHIELD AND AN ORIGINATING POINT OR CAUSE COULD NOT BE DETERMINED. 1L72 4T4 T A24CE E4EA 5 CSTC 20020117001032002011700103SW 2002 1 17 CA011119001 120010914G65102060403255 SHAFT BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL T/R DRIVE GROOVED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ONLY APPLIES TO A/C EQUIPPED WITH CASEY HEATER & ATTACHED DUCTING. DURING GROUND RUN CHECKS AFTER OPS CHECK (600 HR) INBOARD HEATING DUCT CONTACTED SHAFT ASSY P/N 206-040-325-5 & ADAPTER P/N 206-040-328-003 HEATING DUCT (HOSE) WASTORN & WIRE IN HEATER (HOSE) BROKE & CONTACTED THEAFT END OF SHAFT & ADAPTER CAUSING DEEP GROOVES IN BOTH.DURING INSP BOTH SHAFT/COUPLING ADAPTER & BLOWER ASSY WERE REMOVED, & DRIVE SHAFT BEARING WERE REPLACED. DURING THE REMOVAL OR REINSTALLATION OF SHAFT OR BLOWER ASSY HEATER DUCT (HOSE) WHICH HAD BEEN REMVD FOR MAINT ACTION MUST HAVE BEEN SQUEEZED, OR SLIGHTLY DEFORMED,&WHEN REINST, CLEARANCE BETWEEN SHAFT/COUPLING ADAPTER NOT OBTAINED. 1G71 3U3 U H2SW E4CE 20020117001052002011700105CE 2002 1 17 CA011119002 120011029G272003101965 SPRING CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA MCAULY1C160 1C160DTM GL RUDDER BROKEN W A UNSCHED LANDING DF INFLIGHT SEPARATION FLT CONT AFFECTED CRCRUISE 1 CA (CAN) SHORTLY AFTER TAKEOFF & DRING CRUISE EXCESSIVE LT RUDDER WAS AREQD TO KEEP A/C STRAIGHT. PILOT CALLED THUNDER BAY TOWER, & REPORTED RUDDER PROBLEMS & DIFFICULTY CNTLLING AIRCRAFT. PILOT REQED TO LAND WITH EMERG VEHICLES READY. A/C LANDED SAFELY & TAXIED BACK TO COLLEGE HANGAR. ON MECHANICAL INVESTIGATION, IT FOUND THAT LT RUDDER SPRING HAD BROKEN AT TORQUE TUBE END, & WAS HANGING OFF FRONT BRACKET END. (UNDER FLOOR AT PILOTS FEET) THE SPRING WAS CHANGED, RIGGING & RUDDER TRAVEL WERE CHECKED, & A/C WAS RELEASED BACK TO SERVIC E.AGE OF SPRING COULD BE A CONTRIBUTING FACTOR IN THIS CASE AS THERE IS NOT A HIGH STRESS LOAD ON THIS PART. 1H71 3O3 ONT3A12 E274 5 NP910 20020117001072002011700107SW 2002 1 17 CA011119004 120011031G6210407015001107 BLADE BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING AIRFRAME PERIODIC INSP 3.5 INCH DIAGNAL CRACK ON LOWER SKIN OF SUBJECT BLADE FOUND AT BLADE STATION 71.0-73.0.ATTEMPTS TO DRESS OUT CRACK WITH LIGHT SANDING REVEALED SUSPECT LACK OF FIBERGLASS MATTING USED IN CONSTRUCTION OF BLADE TYPE. EVIDENCED BY FURTHER EXPLORATORY SANDING GOING THROUGH GEL ADHESIVE COATING & FILLER MATERIAL & ENDING AT HONEYCOMB CORE W/O 1ST ENCOUNTERING FIBERGLASS CLOTH MATTING. 1G71 3U3 UO H2SW E1GL 20020117001122002011700112EU 2002 1 17 CA011120001 120011111G24349789601090 BRUSH HOLDER PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL GENERATOR WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A 100 HOUR INSPECTION, THE BRUSH ASSEMBLY WAS REMOVED TO VERIFY THE CONDITION. THE BRUSH ASSEMBLY WAS WORN EXCESSIVELY, AND HAS BEEN REPLACED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020211000102002021100010EU 2002 2 11 CA011120002 120011116G27509787320015 FCU PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL TE FLAPS MALFUNCTIONED W D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 CA (CAN) THE PILOT REPORTED AN AMBER FLAPS LIGHT ON THE CAWS PANEL WHEN THE AIRCRAFT POWER WAS TURNED ON. THE AIRCRAFT WAS ON THE GROUND OUTSIDE FOR APPROXIMATELY THREE HOURS, OUTSIDE TEMPERATURE WAS -20C. ONCE TEH AIRCRAFT HAD BEEN WARMED UP IT WAS POSSIBLE TO CARRY OUT A FLAP RESET ON THE FLAP SYSTEM, AND THE SYSTEM FUNCTIONED NORMALLY AFTER THE RESET.THE FLAP CONTROL AND WARNING UNIT WAS REMOVED FROM THE AIRCRAFT AND PLACED IN A FREEZER FOR TWO HOURS, AFTER REMOVING THE UNIT FROM THE FREEZER AND RE-INSTALLING IT IN THE AIRCRAFT IT WAS POSSIBLE TO DUPLICATE THE SAME FAILURE AND RESET SENARIO. THE FCWU HAS BEEN REPLACED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020117001132002011700113SW 2002 1 17 CA011120003 120011002G272012364 CABLE BBAVIA8 8GCBC 1220803SW LYC O360 O360C2E 41514EA RUDDER FRAYED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) BOTH LT AND RT CABLES FRAYED JUST INCHES FWD OF BAGGAGE COMPARTMENT PULLEYS. 1H71 3O3 O A21CE E286 20020117001172002011700117CE 2002 1 17 CA011120009 120010827G712004112816 MOUNT CESSNA170 170A 2072304CE CONT C145 C1452 17012SO LT ENGINE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) LT UPPER ENGINE MOUNT BRACKET AFT OF FIREWALL EXTREME CORROSION (HALF OF BRACKET MISSING) VERY DIFFICULT TO SEE DUE TO INSULATION COVERING ON FIREWALL. 1H71 3O3 O A799 E253 20020117001182002011700118CE 2002 1 17 CA011120010 120011109G56105042006937 WINDSHIELD BEECH 100 B100 1152919CE COCKPIT CRACKED W O OTHER O OTHER CRCRUISE 1 CA (CAN) WHILE AT CRUISE ALTITUDE THE NR 1 (PILOT'S) WINDSHIELD STARTED CRAZING AND CONTINUED PROGRESSIVELY UNTIL OUTWARD VISION WAS SEVERELY IMPAIRED. CABIN PRESSURIZATION WAS LOWERED, WINDSHIELD HEAT WAS DISCONTINUED AND THE AIRCRAFT CONTINUED ON TO DESTINATION. THE UNSERVICEABLE WINDSHIELD WAS REMOVED. A NEW WINDSHIELD WAS INSTALLED. THE AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4T A14CE 20020211000122002021100012CE 2002 2 11 CA011120011 120011115G57535016000310 RIB BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA HARTZLHCB3T HCB3TN3 GL TE FLAP CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 1532315323 (CAN) WHILE CONDUCTING A PREFLIGHT INSPECTION A CRACK IN THE FLAP SKIN WAS DETECTED. THE CRACK WAS LOCATED AROUND THE FLAP ACTUATOR ATTACH BRACKET. FURTHER INVESTIGATION REVEALED THAT BOTH THE FLAP SKIN AND THE NOSE RIB OF THE LT I/B FLAP WERE CRACKED. FURTHER INVESTIGATION REVEALED THAT THE LT O/B FLAP WAS CRACKED IN THE SAME AREA BUT TO A LESSER DEGREE. THE NOSE RIBS IN BOTH THE LT INBOARD AND OUT BOARD ALONG WITH ASSOCIATED FLAP SKINS. 1L72 3T4 T A14CE E4EA 6 CP15EA 20020117001202002011700120EA 2002 1 17 CA011120013 220011108G8520LW1594470 CRANKSHAFT CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA ENGINE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CORROSION FOUND UNDERNEATH PROTECTIVE COATING APPLIED BY FACTORY AT OVERHAUL AS PER LYCOMING SB 505B AND 530A AND AD 98-02-08.CRANKSHAFT HAS BEEN RETURNED TO FACTORY FOR WARRANTY CONSIDERATION AND INSPECTION. 1H71 3O3 ONT3A12 E274 20020117001222002011700122NE 2002 1 17 CA011121001 220011004G8530 STUD AYRES S2 S2RNORMAL 7630202SO PWA R1340 R1340AN1 52016NE ENGINE SHEARED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) NR 1 AND 5 CYLINDERS BASE RETAINING STUDS SHEARED. 1L71 3R3 RNCA3SW 5E2 20020211000152002021100015SO 2002 2 11 CA011121002 220011112G7322S123019 CONTROL CABLE CESSNA150 150J 2071820CE CONT O200 O200A 17020SO CARB HEAT BROKEN W O OTHER E VIBRATION/BUFFET APAPPROACH 1 CA (CAN) PILOT APPLIED CARB HEAT ON DOWNWIND AND KNOB SHAFT ASSEMBLY CAME OUT IN HER HAND. PUSH / PULL WIRE HAD BROKEN ABOUT 3 INCHES PAST THE END OF THE SHAFT. EXAMINATION OF THE BREAK INDICATED A LONG STANDING CRACK ABOUT 2/3 OF THE WAY THROUGH THE WIRE. THERE ARE NO SHARP BENDS AT THIS POINT, THOUGH THE CABLE IS CURVED SOMEWHAT. NO EVIDENCE OF PREVIOUS TRAUMA TO THE WIRE.THE AIRCRAFT WAS LANDED IN NORMAL FASHION AND SHUT DOWN. 1H71 3O3 O 3A19 E252 20020211000162002021100016GL 2002 2 11 CA011121004 220011109G7323252476914 GOVERNOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE FAILED W A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION HOHOVERING 1 CA (CAN) THE HELICOPTER WAS INVOLVED IN FOREST INVENTORY WORK AT LOW ALTITUDE AT NEAR GROSS WEIGHT AT SLOW SPEED WHEN PILOT NOTICED HIS ROTOR RPM DROPING, LOW ROTOR WARNING AND AN INDICATION OF 95 PERCENT. HE MANAGED TO DROP COLLECTIVE AND LAND IN A SMALL CLEARING.THE GOVERNOR WAS REPLACED, AIRCRAFT RUN-UP AND OPERATIONAL CHECKED, OK. 1G71 3U3 U H2SW E4CE 20020117001242002011700124EA 2002 1 17 CA011121005 120011115G5320C2FS3282A STRUT DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE WINDOW FRAME CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 14676 (CAN) THE AIRCRAFT WAS UNDERGOING SCHEDULED MAINTENANCE.THE RIGHT HAND WINDSHIELD WAS BEING REPLACED. THE RIGHT FRONT FUSELAGE STRUT ASSY WAS FOUND CORRODED UNDER THE WINDSHIELD SUPPORT ASSY. THIS STRUT ASSY WAS EXAMINED IN ACCORDANCE WITH CF-98-37R1 IN FEBRUARY OF THIS YEAR. THE AREA CORRODED IS NOT ACCESSIBLE UNLESS THE WINDSHIELD IS REMOVED. 1H71 3R3 R A806 5E1 20020117001292002011700129SO 2002 1 17 CA011121008 120011116G3230401195 BOLT PIPER PA42 PA42720 7104212SO PWA PT6 PT6A61 52043EA MLG BROKEN W O OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION LDLANDING 1 CA (CAN) FLT CREW WERE UNABLE TO EXTEND LT MLG THROUGH NORMAL (HYDRAULIC) OR EMERG (HYDRAULIC/PNEUMATIC) MEANS PRIOR TO LDG. LOSS OF HYDRAULIC FLUID EVIDENT AROUND TRAILING EDGE OF LT WING & FLAP AREAS. NOSE & RT MLG WERE RETRACTED & A/C MADE SUCCESSFUL GEAR UP LDG. INVESTIGATION. DETERMINED LT MLG ACTUATING CYLINDER TOP BOLT HAD BROKEN. ALLOWED CYLINDER TO SLIDE DOWN RAM WHEN GEAR INITIALLY SELECTED DOWN, INSTEAD OF RAM RETRACTING INTO STATIONARY CYLINDER. CYLINDER MOVEMENT BROKE LOWER FITTING THAT IS COMMON TO BOTH HYDRAULIC&PNEUMATIC SYS PRESSURES, RESULTING IN OVERBOARD LOSS OF HYDRAULIC FLUID A ND ANY PENUMATIC PRESSURE: 1L72 4T4 T A23SO E4EA 20020117001302002011700130SO 2002 1 17 CA011121009 120011116G3230668346 WIRE HARNESS PIPER PA42 PA42720 7104212SO PWA PT6 PT6A61 52043EA MLG DISCONNECTED W H DEACTIVATE SYST/CIRCUITS RL PARTIAL RPM/PWR LOSS NO TEST LDLANDING 1 CA (CAN) PILOT ACTIVATED LDG GEAR EMERG BLOWDOWN PNEUMATIC SYS SWITCH DURING LDG GEAR EXTENSION MFLFUNCTION. LATER GROUND INSP DETERMINED THAT PENUMATIC SYS (LT MLG) HAD NOT PROPERLY ACTIVATED. SYS SHOULD HAVE FIRED T HE NITROGEN BOTTLE EXPLOSIVE SQUIB (ON LDG GEAR NOT DOWN & LOCKED) WHEN 28 VOLTS WERE APPLIED BY PUSHING EMERG GEAR EXTENTION SWITCH. VOLTAGE CHECK CONDUCTED AT L/H SQUIB CONNECTOR SHOWED ONLY 0 TO 4 VOLTS WHEN SWITCH ACTIVATED&GEAR UNLOCKED. TROUBLESHOOTING DISCOVERED WIRE LEADING FROM SWITCH TO BE ATTACHED BY ONLY ONE OR 2 STRANDS&PROTECTIVE HEAT SHRINK (VISUALLY NORMAL BUT DISCONNECTED IMMEDIATELY UPON TOUCHING WIRE). 1L72 4T4 T A23SO E4EA 20020117001312002011700131SO 2002 1 17 CA011121013 120011112G32226531904 CYLINDER PIPER PA28 PA28140 7102802SO LYC O320 O320E3D 41508EA TORQUE LINK FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) - UPON INSPECTION OF AIRCRAFT FOR A REPORTED HARD LANDING TORQUE LINK LUGS FOUND TO HAVE FAILED (UPPER).- UPON REMOVAL IT APPEARS OUTBOARD LUG TO HAVE BEEN CRACKED FOR SOMETIME. INBOARD LUG HAD A SMALL CRACK ALSO ABOUT 20 PERCENT OR AREA. - AREA COVERED BY FAIRING, TO INSPECT FAIRING HAS TO BE REMOVED.- S.L. 760 COVERS INSPECTION OF THIS AREA.OLEO CYLINDER P/N 65319-04 HAS BEEN SUPERCEDED BY 65490-00. 1L71 3O3 O 2A13 E274 20020211000282002021100028SO 2002 2 11 CA011121014 120011119G32601459500001 DOWNLOCK SWITCH EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA LT MLG FAILED W O OTHER O OTHER LDLANDING 1 CA (CAN) DURING DESCENT INTO YMO THE CREW SELECTED GEAR DOWN AND DID NOT GET A LT MAIN GEAR DOWN AND LOCKED INDICATION. THE LANDING GEAR WAS CYCLED A FEW TIMES AND GEAR DOWN AND LOCKED WAS CONFIRMED WITH INDICATION OF DOWN AND LOCKED. AS A PRECAUTION THE CREW ELECTED TO RETURN AND DECLARE AN EMERGENCY. THE CREW SUBSEQUENTIALLY PERFORMED AN UNEVENTFUL LANDING. UPON INVESTIGATION BY MAINTENANCE PERSONNEL IT WAS DETERMINED THAT THE LT DOWNLOCK SWITCH PLUNGER HAD FAILED. THE DOWNLOCK WAS REPLACED AND GEAR SWINGS COMPLETED SERVICEABLE. THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 1L72 4T4 T A21SO E4EA 20020117001372002011700137CE 2002 1 17 CA011122006 120011120G326041EN16 SWITCH BEECH 99 99A 1154003CE PWA PT6 PT6A28 EA MLG INTERMITTENT W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CA (CAN) AIRCRAFT DEPARTED AIRPORT AND COULD NOT RETRACT GEAR. AIRCRAFT DEVERTED TO HOME BASE AND LANDED WITHOUT INCIDENT.THE SAFETY SWITCH WAS FOUND INTERMITTTANT ON THE RIGHT HAND GEAR TORQUE KNEES.SWITCH WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. NOTE: PART TIME IS UNKNOWN 1L72 3T4 T A14CE E4EA 20020118000022002011800002 2002 1 18 CA011123001 420011116G6113055032110 PLATE CESSNA 05503671 CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA MCAULY1A170 1A170E GL PROP SPINNER BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE CORNER SECTION OF SPINNER AT LEADING EDGE OF PROPELLER BLADE CUT-OUT BADLY BENT (PEELED BACK) BY CENTRIFUGAL FORCE. THIS WAS CAUSED BY THE ADJACENT CORNER SECTION OF THE BACKPLATE (AROUND ANCHOR NUT) BREAKING OFF DURING OPERATION. CESSNA HAS RECOGNIZED THIS PROBLEM AND ISSUED MOD KIT MK172-61-01 UNDER SB01-61-01. NEW BACKPLATE DESIGN AND P/N INCORPORATED AS PER LISTED KIT AND SB NUMBERS. 1H71 3O3 ONT3A12 1E10 5 NP857 20020211000772002021100077EU 2002 2 11 CA011126001 120011122G63204638302023 BEARING BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL M/R GEARBOX DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) OUTER AND INNER RACE OF BEARING DISPLAY MODERATE PITTING AND PEELING.ONE BALL DISPLAYS HEAVY PITTING 1G72 3U3 UNCH3EU E4CE 20020118000052002011800005GL 2002 1 18 CA011126002 220011123G72506006T87G13 NOZZLE GE CT58 CT58* 30011GL ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE BAFFLE OF THE 3RD STAGE NOZZLE WAS REMOVED TO INVESTIGATE THE CAUSE OF AIR LEAKAGE. VISUAL AND NDT INSPECTION REVEALED CRACKS IN THE SHEET METAL OF THE SUMP ABOVE THE AIR TUBE LOCATION.TELCON WITH GE ON NOV. 21 REGARDING THE CRACKS AND THE LACK OF REPAIRABLE OR SERVICEABLE LIMITS IN THIS AREA. THE PARTS HAVE BEEN FORWARDED TO GE FOR THEIR INVESTIGATION. 4 OF 5 NOZZLES CHECKED HAD SIMILAR CRACKS. 4 U 1E3 20020211000782002021100078CE 2002 2 11 CA011126003 120011010G55521156200219 HINGE BEECH BEECH 99 99 1154002CE PWA PT6 PT6A27 52043EA LT ELEVATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 3910639106 (CAN) DURING ROUTINE INSPECTION, CRACK WAS FOUND ON ELEVATOR HINGE. PART WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.PART AVAILABLE FOR INSPECTION IN QUARANTINE.PART TSO/TSN/CYCLES ARE AIRCRAFT FIGURES. 1L72 3T4 T A14CE E4EA 20020211000822002021100082SW 2002 2 11 CA011127001 120011113G6310CL422501 CLUTCH BELL 20604023013 BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL FREEWHEEL UNIT BROKEN W K NONE K FLUID LOSS ININSP/MAINT 1 CA B12468 (CAN) FREEWHEEL UNIT SENT IN FOR REPAIR OWNER REPORTS: LEAKING AND ROUGH TO TURN ONCE REMOVED. FREEWHEEL DISASSEMBLED AND CLUTCH CAGE FOUND CRACKED AND A PIECE BROKEN OFF. THE INNER RACE AND OUTER RACE BOTH FOUND WORN BEYOND LIMITS. BELL HELICOPTER PRODUCT SUPPORT TECH REP CONTACTED AND HE WILL BE HERE THURSDAY NOVEMBER 15, 2001 TO VIEW THE DAMAGED UNIT. 1G71 3U3 U H2SW E4CE 20020118000062002011800006EA 2002 1 18 CA011127002 220010927G74144771 MAGNETO CESSNA172 172P 2072436CE LYC O320 O320D2J 41508EA MCAULY1C160 1C160DTM GL ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ON LANDING ROLL PILOTS REPORTED A GRINDING NOISE FROM THE ENGINE. - THEY TAXIED OFF THE RUNWAY AND SHUT DOWN. AIRCRAFT PUSHED TO HANGAR.- INITIAL INVESTIGATION SHOWED DEAD LT MAGNETO (TIMING INDICATOR). - MAGNETO REMOVED, SHAFT BENT AND GEAR GROUND BY ENGINE DRIVE GEAR. 1H71 3O3 ONT3A12 E274 5 NP910 20020118000072002011800007GL 2002 1 18 CA011127004 220011115G72506898731 SUPPORT BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE LEAKING W EA ENGINE SHUTDOWN UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 CA (CAN) TURBINE ASSY WAS RECD IN FOR SMOKING ON SHUTDOWN. SMOKING WAS ENCOUNTERED APPROX 7 2NDS AFTER THROTTLE WAS ROLLED TO OFF POS.UPON DISASSY & INSPECTION OF PT SUPPORT IT FOUND THAT INNER DIAMETER (DIA.S) SHOULDER WIDTH WAS INSUFFICIENT FOR PROPER SEALING OF U-RING GASKET. AS A RESULT, THERE WAS A LOSS OF LABYRINTH SEAL PRESSURE & AN INCREASE IN AIR PRESSURE WITHIN POWER TURBINE SUPPORT OIL SUMP, ALLOWING OIL FROM 6 & 7 BEARING AREA TO ENTER GAS PATH. NOTE: SHOULDER WIDTH OF INNER DIAMETER SHOULD BE INSP TO ENSURE SUFFICIENT SURFACEAREA EXISTS FOR PROPER SEALING OF U-RING GASKET (PRINT DIM. FOR SHOULDER WIDTH UNAVAILABLE).P/N 6898731;S/N MK18387 1G71 3U3 U H2SW E4CE 20020212000022002021200002SW 2002 2 12 CA011127005 120011116G2750B10006 COUPLING AIRTRCAT802 AT802 0390305SW FLAP DRIVE SPLIT W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING ANNUAL INSPECTION THE FLAP DRIVE RUBBER COUPLING WAS FOUND TO BE SPLIT, EARLIER IN THE OPERATING SEASON A LOOSE WIRE ON THE FLAPS DOWN SWITCH CAUSED THE FLAPS TO OVERTRAVEL AND BOTTOM OUT THE ACTUATOR. EXPERIENCE HAS SHOWN THAT WHEN THIS SITUATION HAPPENS, THE RUBBER COUPLING IS DAMAGED FROM THE SUDDEN STOPPAGE. THE RUBBER COUPLING SHOULD BE INSPECTED ANY TIME AN OVERTRAVEL IS EXPERIENCED. 1L71 3T NCA19SW 20020212000032002021200003CE 2002 2 12 CA011127006 120011126G5730 SKIN BEECH 90 C90 1152913CE PWA PT6 PT6A21 52043EA LT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ON A RECENT ROUTINE INSPECTION ON LJ886 A CRACK WAS FOUND ON THE LT UPPER WING SKIN AT STA 175 AND WL 81 SEEN FROM THE UNDERSIDE IN THE WHEELWELL. THE AFT NACELLE FAIRING WAS REMOVED AND ANOTHER CRACK WAS FOUND AT STA 182 AND WL70.THE AFT NACELLE FAIRING OF THE RT WING WAS REMOVED AND SUBSEQUENTLY TWO MORE CRACKS IN THE SAME LOCATIONS DESCRIBED ON THE LT WING WERE FOUND. 1L72 3T4 T 3A20 E4EA 20020118000082002011800008EU 2002 1 18 CA011127009 120011022G24345243212137 DRIVE SHAFT PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL NR 2 GENERATOR WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE CARRYING OUT REPLACEMENT OF GEN 2 DRIVE ASSY OUTER BEARING FOR 3000 HR REQUIREMENTS, IT WAS NOTED THAT THE DRIVE SHAFT WAS WORN AT THE BEARING JOURNAL AND THE BEARING WAS LOOSE ON THE SHAFT. THE DRIVE SHAFT HAD TO BE REPLACED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020212000042002021200004EU 2002 2 12 CA011127010 120011120G2497350A311851 STRAP SNIAS 350 AS350B2 8680813EU ELECTRICAL FRAYED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THREE BONDING STRAPS ARE FRAYED HALFWAY THROUGH. 1G71 3U H9EU 20020212000052002021200005CE 2002 2 12 CA011127011 120011120G534336653RH FITTING CESSNA180 180J 2072622CE CONT O470 O470S 17026SO MCAULY2A34C 2A34C203 GL FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) INTERGRANULAR CORROSION ON FUSELAGE FITTING. 1H71 3O3 O 5A6 E273 5 CP3EA 20020212000062002021200006EU 2002 2 12 CA011127012 120011120G27509740338111 CONTACTOR PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL TE FLAP PDU SHORTED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE LOWERING THE FLAPS DURING ROUTINE MAINTENANCE, THE FLAP POWER DRIVE UNIT (PDU )WAS LABOURING. THE FLAP DRIVE SHAFTS WERE DISCONNECTED AT THE PDU, BUT THE PDU WAS STILL LABOURING. THE PDU WAS REPLACED, BUT THE CONDITION STILL PERSISTED. THE K670 CONTACTOR WAS REPLACED AND THE PDU OPERATED NORMALLY. THE SUSPECT K670 CONTACTOR WAS TAKEN APART AND DISCOVERED THAT THE CONTACTS WERE BADLY BURNED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020212000242002021200024EA 2002 2 12 CA011128008 120010722G2432 CELL MARATHON MA300H DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA BATTERY DEFORMED W H DEACTIVATE SYST/CIRCUITS BHMSMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC OVER TEMP TXTAXI/GRND HDL 1 CA 9802292 (CAN) SMOKE WAS VISIBLE IN THE BAGGAGE COMPARTMENT WHEN OPENED ON THE RAMP. ONE CELL WITHIN THE BATTERY WAS FOUND TO BE DEFORMED FROM HEAT. 1H72 3T4 TRTA9EA E4EA 20020212000282002021200028CE 2002 2 12 CA011128016 120011030G541190120003 ANGLE BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA LT & RT NACELLE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) INSIDE LT AND RT MAIN LANDING GEAR WELLS, OUTBOARD SIDE WALL, ANGLE AT CORNER OF SIDE WALL AND FORWARD FACE OF MAIN SPAR WEB, LOWER END OF ANGLE. POSSIBLE NEED TO REMOVE PAINT TO NOTE CRACK. BOTH CRACKS APPROX. .75 INCHES IN LENGTH. 1L72 3T4 TRT3A20 E4EA 20020212000542002021200054CE 2002 2 12 CA011128017 120011114G3500503800573 HOSE BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA OXYGEN SYS BROKEN W B EMER. DESCENT O OTHER CRCRUISE 1 CA (CAN) HOSE BROKE CAUSING LOSS OF PRESSURIZATION, REPLACED HOSE AND FLIGHT TESTED SERVICEABLE. 1L72 3T4 T A14CE E4EA 20020212000552002021200055SO 2002 2 12 CA011128018 120011120G29104083300 LINE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HYD POWERPACK BROKEN W O OTHER J WARNING INDICATION APAPPROACH 1 CA (CAN) ON APPROACH PILOT SELECTED GEAR DOWN WITH NO INDICATION OF ANY MOVEMENT OF THE GEAR. MANUALLY HAND PUMPED GEAR WITH NO SUCCESS. AFTER SEVERAL ATTEMPTS AND BURNING OFF EXCESS FUEL MADE A GEAR UP LANDING WITH NO DIFFICULTY. ON INSPECTION FOUND THE GEAR DOWN LINE AT THE POWER PACK BROKEN AT THE FLARE. REPAIRED LINE INSTALLED AND GEAR FUNCTIONED NORMALLY AFTER FILLING WITH FLUID. 1L72 3O3 O A20SO E14EA 20020212000562002021200056SW 2002 2 12 CA011130001 120011108G275012395 PULLEY BBAVIA8 8GCBC 1220803SW LYC O360 O360C2E 41514EA TE FLAPS SEIZED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) - LT & RT PULLEYS AT WING ROOT FOUND SEIZED AND WORN. - BOTH FLAP CABLES FRAYED AT THAT POSITION. - SMALL ALUMINUM PULLEYS, HARD TO LUBRICATED AND PROVIDE A TIGHT DEFLECTING RADIUS FOR CABLES. 1H71 3O3 O A21CE E286 20020212000572002021200057SW 2002 2 12 CA011130002 120011108G275019023 CONTROL CABLE BBAVIA8 8GCBC 1220803SW LYC O360 O360C2E 41514EA TE FLAPS FRAYED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) - LT & RT UPPER FLAP CABLES FRAYED AT WING ROOT PULLEYS. BOTH LT & RT PULLEYS FOUND SEIZED AND WORN. 1H71 3O3 O A21CE E286 20020212000582002021200058SW 2002 2 12 CA011130003 120011109G275012395 PULLEY BBAVIA8 8GCBC 1220803SW LYC O360 O360C2E 41514EA TE FLAPS SEIZED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) LT & RT PULLEYS AT WING ROOT FOUND SEIZED AND WORN. BOTH FLAP CABLES FRAYED AT SAME LOCATION. 1H71 3O3 O A21CE E286 20020212000592002021200059SW 2002 2 12 CA011130004 120011109G275019023 CONTROL CABLE BBAVIA8 8GCBC 1220803SW LYC O360 O360C2E 41514EA TE FLAPS FRAYED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) - LT & RT UPPER FLAP CABLES FRAYED AT WING ROOT PULLEYS. BOTH LT & RT PULLEYS FOUND SEIZED AND WORN. 1H71 3O3 O A21CE E286 20020212000602002021200060SW 2002 2 12 CA011130005 120011109G2810714941R FUEL TANK BBAVIA8 8GCBC 1220803SW LYC O360 O360C2E 41514EA RT OUTBOARD CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) RT OUTBOARD TANK CRACKED, LOWER SIDE, AT THE END OF REINFORCING INDENT, ON PREVIOUSLY REPAIRED WELD. 1H71 3O3 O A21CE E286 20020212000612002021200061SW 2002 2 12 CA011130006 120011124G6500407340339103 BEARING BELL 407040303101BELL 407 407 1182206SW ALLSN 250C 250C47B GL FAN SHAFT FAILED W A UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 CA (CAN) WHILE ON 5TH SCENIC TOUR OF DAY, AT 2,500 FT ASL IN QUIET MODE CRUISE, A/C SOUND & VIBRATION LEVEL SUDDENLY CHANGED FROM NORMAL TO LOUD WITH HEAVY VIBRATION FROM TAIL ROTOR DRIVE AREA. PILOT IMMEDIATELY RETURNED A/C TO NORMAL MODE CRUISE RPM & EXITED SCENIC ROUTE. HE RETURNED DIRECTLY TO MAIN BASE AT PQ3 WITH PRECAUTIONARY LDG & SHUTDOWN WITHOUT FURTHER INCIDENT. TAIL ROTOR CONTROL AUTHORITY NEVER LOST. AFTER ENGINE SHUTDOWN, INSPECTION REVEALED A COMPLETELY FAILED FWD FAN SHAFT BEARING WITH DISINTEGRATED BEARING CAGE. 1G71 3U3 UO H2SW E1GL 20020212000642002021200064SO 2002 2 12 CA011130012 120011121G3260487312 SPRING PIPER PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA DOWNLOCK BROKEN W L ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 CA (CAN) - RIGHT HAND MAIN LANDING GEAR INDICATION FAILED IN FLIGHT. - PILOT RECYCLED GEAR AND LIGHT APPEARED TO WORK. - INSPECTION REVEALED A BROKEN DOWNLOCK SPRING. 1L72 3O3 O 1A10 1E4 20020212000652002021200065CE 2002 2 12 CA011130014 120011121G782004504004 MUFFLER CESSNA150 150M 2071830CE CONT O200 O200A 17020SO ENG EXHAUST CRACKED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) A NOISE WAS HEARD IN CRUISE. MUFFLER FOUND CRACKED BEFORE RISER. 1H71 3O3 O 3A19 E252 20020212000692002021200069EA 2002 2 12 CA011203001 220011127G74141068291013 CASE BENDIX 1068291013 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA MAGNETO BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 85410122T (CAN) CASE FLANGE BROKEN UNDER UPPER RETAINER. 1L72 3O3 O A20SO E14EA 20020212000722002021200072EU 2002 2 12 CA011203005 120011203G6320461920400146382 BEARING BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL M/R GEAR BOX PEELING W K NONE O OTHER ININSP/MAINT 1 CA (CAN) BOTH THE PLANETARY AXLE AND ROLLER BEARING PLATING PEELING. 1G72 3U3 UNCH3EU E4CE 20020212000742002021200074SW 2002 2 12 CA011205001 120011204G571221588 RIB BBAVIA8 8GCBC 1220803SW LYC O360 O360C2E 41514EA LT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) 3 RIBS RT, 2 RIBS LT WING FOUND CRACKED AT UPPER CORNER OF FLANGE WHERE RIB ATTACHES TO REAR SPAR. ALL RIBS LOCATED CLOSEST INBOARD AT WING ROOT, AND ALL RIBS CRACKED EXACTLY THE SAME. 1H71 3O3 O A21CE E286 20020212001042002021200104CE 2002 2 12 CA011205003 120011204G57440523921 BUSHING CESSNA 0523919 CESSNA180 180J 2072622CE CONT O470 O470S 17026SO TE FLAP SUPPORT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE PREFORMING A FLAP SUPPORT INSPECTION, A CRACK WAS FOUND ON THE FLAP ROLLER BUSHING (LT REAR). THE CYLINDRICAL BUSHING WAS SPLIT IN HALF AND ONLY BECAME APPARENT WHEN THE BUSHING WAS REMOVED FROM THE FLAP ROLLER ASSEMBLY. 1H71 3O3 O 5A6 E273 20020212001052002021200105CE 2002 2 12 CA011205004 120011204G272005121602 BRACKET CESSNA180 180J 2072622CE CONT O470 O470S 17026SO CABLE PULLEY CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A ROUTINE 100 HOUR INSPECTION THE RUDDER CABLE PULLEY BRACKETS THAT ARE LOCATED AT THE BATTERY BOX BULKHEAD, WERE BOTH FOUND TO BE CRACKED AT THE TOP ATTACH POINT (RIVET). BOTH BRACKETS WERE REPLACED. 1H71 3O3 O 5A6 E273 20020212001062002021200106EA 2002 2 12 CA011205005 120011204G3250C2UT473 TORQUE TUBE DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE TAIL WHEEL CRACKED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA (CAN) INVESTIGATION REVEALED A SHEARED TAIL WHEEL STEERING TORQUE TUBE ASSEMBLY (WATER RUDDER). INTERNAL CORROSION WAS PRESENT INSIDE THE TUBE ASSEMBLY. NO ABNORMAL CONDITION PRESENT ON THE EXTERNAL PORTION OF THE TUBE.THE TORQUE TUBE FAILURE TOOK PLACE AT THE WELDED JUNCTION OF THE SPLINE SHAFT AND TUBE ASSEMBLY. 1H71 3R3 R A806 5E1 20020212001072002021200107EA 2002 2 12 CA011205006 120011115G6123 CONTROL UNIT DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE NR 2 ENGINE MALFUNCTIONED W HA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 CA (CAN) PRIOR TO TAKE-OFF, AUTOFEATHER ARMING BAULKED, ACTIVATED ON RE-SELECTION. ON TAKE-OFF, AFTER GEAR UP SELECTION, NR 2 ENGINE INITIATED UNCOMMANDED AUTOFEATHER (TORQUE 125 PERCENT PLUS). CREW DE-SELECTED AUTOFEATHER WITHIN FOUR SECONDS, TORQUE RETURNED TO NORMAL. AIRCRAFT RETURNED TO BASE, AND ENGINE / PROP CHANGE CARRIED OUT. ENGINE TORQUE PROBE, HARNESS AND TSCU SHIPPED TO OEM FOR ANALYSIS, 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20020212001082002021200108EU 2002 2 12 CA011207002 120011207G71706859172 TUBE BOLKMS105 BO105C 5626005EU ALLSN 250C 250C20B 03013GL FUEL DRAIN CHAFED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DRAIN LINE CHAFING ON FUEL CONTROL TO FUEL PUMP BY PASS TUBE IS 99 PERCENT CHAFED. 1G72 3U3 U H3EU E4CE 20020212001142002021200114EU 2002 2 12 CA011207004 120011022G2920MVT1001 SELECTOR VALVE AIRBUS330 A330342 EU RROYCERB211 RB211TRENT77 NE HYD SYSTEM CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) THE AIRCRAFT ARRIVED TO YYZ, WITH THE "YELLOW" HYDRAULIC SYSTEM EMPTY. FOUND RT ELEVATOR, OUTBOARD SERVO (F.I.N.3CS2) SELECTOR VALVE HOUSING CRACKED. 1L72 4F4 FRTA46NM E39NE 20020212001182002021200118EU 2002 2 12 CA011209002 120011129G3251C247820001 SOLENOID VALVE C248560014 AIRBUS330 A330342 EU RROYCERB211 RB211TRENT77 NE NLG STEERING BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING DEACTIVATION OF THE NOSE LANDING GEAR STEERING SYSTEM, THE NOSE WHEELS TURNED 90 DEGREES RIGHT WITHOUT ANY STEERING INPUT WHEN STEERING / ANTI-SKID SWITCH WAS TURNED OFF. AT THAT MOMENT THE THE AIRCRAFT CONDITION WAS:-STEERING BY-PASS PIN INSTALLED IN TOW POSITION.-BOTH ENGINE MASTER SWITCH OFF. -GREEN ELECTRICAL HYDRAULIC PUMP ON.-UPON REMOVING AND OPENING THE SOLENOID VALVE ASSY , WE DISCOVERED THAT THE LINER (MADE OF ALUMINIUM ALLOY) WAS BROKEN (SHEARED). 1L72 4F4 FRTA46NM E39NE 20020212001312002021200131CE 2002 2 12 CA011210009 120011029G7170A1090 DRAIN VALVE BEECH 99 99 1154002CE PWA PT6 PT6A20 52043EA RT ENGINE BROKEN W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) DURING THE LATTER PART OF A FLIGHT THE RT NACELLE WAS SHOWING A DECLINE IN DUEL CAPACITY ABOVE NORMAL. WHEN REACHING THE DESTINATION IT WAS DISCOVERED THAT FUEL WAS ESCAPING FROM THE RT FUEL MANIFOLD DRAIN. UPON FURTHER INVESTIGATION IT WAS FOUND THAT THE CENTRE PORTION OF THE DRAIN VALVE HAD BROKEN OFF AND FALLEN OUT. 1L72 3T3 T A14CE E4EA 20020212001332002021200133GL 2002 2 12 CA011210010 220011130G7323 DRIVE SHAFT ALIDSG 252476914 BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL GOVERNOR DAMAGED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 17611 (CAN) PILOT REPORTED IN NORMAL LEVEL CRUISE FLIGHT AT LOW TO MEDIUM TORQUE SETTING. HE FELT, HEARD AND NOTICED A POWER SURGE AND GAUGE FLUCTUATION APPROX. 2 PERCENT N1. THIS WOULD OCCUR FOR JUST A SECOND AND WOULD ONLY OCCASIONALLY HAPPEN 1 TIME OR SEVEERAL TIMES IN A 1 HOUR PERIOD. THE A/C RETURNED BACK TO BASE AFTER COMPLETING HIS WORK AND WAS DUE FOR 100 HR INSPECTION, THE GOVERNOR WAS REMOVED FOR INSPECTION AND THE DRIVE END AND CIRCLIP WERE FOUND LOOSE AND READY TO FALL OFF. THIS GOVERNOR HAS BEEN REMOVED 3 PREVIOUS TIMES FOR SURGING, DROOPING AND THE LAST TIME FOR THE DRIVESHAFT END FAILURE. 1G71 3U3 U H2SW E4CE 20020212001342002021200134NE 2002 2 12 CA011210012 220011126G8520 CONNECTING ROD DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE ENGINE FAILED W A UNSCHED LANDING EY VIBRATION/BUFFET ENGINE STOPPAGE CRCRUISE 1 CA (CAN) THE A/C WAS ESTABLISHED IN CRUISE WHEN THE PILOT NOTICED ENGINE VIBRATION FOR APPROXIMATELY 5 SECONDS. THIS WAS FOLLOWED BY AN ABRUPT ENGINE STOPPAGE. THE PILOT SAFELY GLIDED TIME A/C TO A NEARBY RIVER. UPON ENGINE TEARDOWN THE NR 1 & 2 CONNECTING RODS WERE BROKEN & THE NR 1 WRIST PIN BENT. 1H71 3R3 R A806 5E1 20020212001362002021200136CE 2002 2 12 CA011210013 120011122G339720GAUGE WIRE CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL EXTERIOR LIGHTS SHORTED W O OTHER H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 CA (CAN) NAV. LIGHT CIRCUIT BREAKER WAS FOUND POPPED THE WIRES TO THE LIGHT IN THE TAIL CONE WERE SHORTED TOGETHER. THESE 2 WIRES SHORTED PORTION WERE REMOVED AND THE WIRES SPLICED TOGETHER. THERE ARE TIE-WRAPS HOLDING THE WIRES TO THE SIDE OF THE TAIL CONE. 1H71 3T3 T A37CE E4EA 5 CP60GL 20020212001462002021200146SW 2002 2 12 CA011210017 120011203G5532410008173 SKIN GULSTM690TP 690A 0141722SW GARRTTTPE331TPE3315251K NM VERTICAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING INSPECTION OF THE AIRCRAFT, CRACKS WERE NOTED ON THE VERTICAL STABILIZER SKIN. THE CRACKS WERE LOCATED AT THE FIRST FASTENER ABOVE THE DOUBLER AT THE CENTRE SPAR. THE LONGEST CRACK MEASURED .75 INCHES IN LENGTH. A X-RAY INSPECTION WAS ACCOMPLISHED IN THE AREA OF THE DOUBLER AND 2 CRACKS WERE NOTED ON THE SKIN AT THE FASTENER THAT WAS UNDERNEATH THE DOUBLER. THE DOUBLER WAS REMOVED FROM THE AIRCRAFT TO INSPECT THE AREA NO FURTHER DAMAGE WAS NOTED. 1H72 3T4 T 2A4 E2WE 20020212001492002021200149SW 2002 2 12 CA011210018 120011203G28105129811 LINE AIRTRCAT802 AT802 0390305SW PWA PT6 PT6A67A 52043NE FUEL SYSTEM CHAFED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING INSPECTION THE AIR CONDITIONER DRIVE ASSY WAS BEING REMOVED FOR LUBRICATION. IT WAS NOTED THAT THE FIRE SLEEVING OF THE FLEX FUEL PRESSURE LINE, HAD BEEN WORN THROUGH. FURTHER INVESTIGATION REVEALED THAT THE STEEL FITTING ATTACHING THE FUEL LINE TO THE FUEL PUMP ASSY. HAD COME LOOSE AND ALLOWED THE FUEL LINE TO CONTACT THE AIR CONDITIONING SYSTEM COMPRESSOR PULLEY. THE OUTER RUBBER OF THE FUEL LINE WAS ALSO DAMAGED. THE LINE WILL BE REPLACED WITH A SERVICEABLE UNIT, AND THE REST OF THE AIRTRACTOR FLEET WILL BE INSPECTED PRIOR TO FURTHER FLIGHT. 1L71 3T4 TNCA19SW E26NE 20020212001552002021200155EU 2002 2 12 CA011210020 120011207G24345243212137 DRIVE SHAFT PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL NR 2 GENERATOR WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) 3000 HR. REPLACEMENT OF OUTER DRIVE SHAFT BEARING WAS CARRIED OUT. ON DISASSEMBLY OF DRIVE HOUSING ASSEMBLY, THE INNER BEARING MOUNTING SURFACE OF DRIVE SHAFT WAS FOUND WORN DUE TO DRIVE SHAFT SPINNING IN THE INNER RACE OF THE BEARING.A NEW DRIVE SHAFT WAS INSTALLED AND AFTER 4 HRS. OF OPERATION, GENERATOR NR 2 FAILED.IT WAS FOUND THAT THE NEW DRIVE SHAFT INSTALLED HAD SHEARED AFTER THE SPLINE DRIVE. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020212001612002021200161GL 2002 2 12 CA011211001 220011207G73216859172 DRAIN LINE BOLKMS105 BO105C 5626005EU ALLSN 250C 250C20B 03013GL FUEL CONTROL CHAFED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) DRAIN LINE CHAFING ON FUEL CONTROL TO FUEL PUMP BYPASS TUBE P/N 6859172 TUBE IS 99 PERCENT CHAFED. 1G72 3U3 U H3EU E4CE 20020212001742002021200174SW 2002 2 12 CA011211002 120011122G6510204040612001 BOLT BELL 212040004003BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA QUILL ASSY BENT W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THIS BOLT HOLDS THE TAIL ROTOR DRIVESHAFT COUPLING TO THE INPUT QUILL OF THE 90 DEGREE GEARBOX. WHEN THE BOLT WAS REMOVED FOR SCHEDULED MAINTENANCE (GREASE REPACKING). IT WAD NOTICED THAT IT WAS NOT THE NORMAL COLOR (BLACK) THAN IT WAS NOTICED THAT IT WAS DISTORTED AROUND THE FLANGE RADIUS. EVEN CLOSER INSPECTION SHOWS THAT THE BOLT DUE TO THE BEND IN THE FLANGE IS NOW LONGER. THE BOLT SHOWS SIGNS OF STRETCHING AND TOOL MARKS MAY INDICATE THAT IT WAS MANUFACTURED BY SOMEONE OTHER THAN THE ORIGINAL MANUFACTURE. THERE IS NO PART NO. WRITTEN ON THIS PART AS THERE IS A NEW ONE. I BELIEVE THIS IS AN UNAPPROVED PART (BOGUS). PART HELD FOR INVESTIGATION. 1G71 4U4 U H4SW E22EA 20020212001762002021200176EA 2002 2 12 CA011211003 120010516G7603C2CE67A CONTROL CABLE DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE FUEL SELECTOR FRAYED W K NONE O OTHER ININSP/MAINT 1 CA 1531515315 (CAN) CABLE FRAYED WHERE IT BENDS AROUND FUEL SELECTORPULLEY. ITEM NOTED DURING ANNUAL INSPECTION. IT IS ADVISEABLE TO HAVE SOMEONE MOVE THE FUEL SELECTOR CONTROL WHILE INSPECTING TO ACCESS AS MUCH OF CABLE AS POSSIBLE AS ITS INSTALLED. 1H71 3R3 R A806 5E1 20020212001792002021200179CE 2002 2 12 CA011211004 120010614G27200510105173 CONTROL CABLE CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULYD3A34 D3A34C403 GL RUDDER FRAYED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FWD (CARRY-THROUGH) CABLE REMOVED TO CARRY OUT AN INSPECTION ON IT'S CONDITION DUE TO THE FACT THAT IT IS IMPOSSIBLE TO FEEL OR SEE MOST OF THE CABLE AS IT'S INSTALLED IN THE A/C. INSPECTION REVEALED FRAYED SECTION WHERE CABLE GOES AROUND THE PULLEY SUGGEST REMOVING ALL SIMILAR CABLE AT TAT 5000HRS TO COMPLETE INSPECTION. 1H71 3O3 O 3A24 E5CE 5 CP47GL 20020212001802002021200180CE 2002 2 12 CA011211005 120010520G551107326032 CHANNEL CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULYD3A34 D3A34C403 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CHANNEL FOUND CRACKED DIRECTLY BEHIND LT STAB HINGE REINFORCEMENT, WHICH WAS ALSO CRACKED. FURTHER INVESTIGATION REVEALED CRACKED SPAR ALSO IN SAME AREA. 1H71 3O3 O 3A24 E5CE 5 CP47GL 20020213000012002021300001GL 2002 2 13 CA011211009 120010516G2720C2CF741AND CONTROL CABLE DHAV DHC1 DHC1B2 2801736GL RUDDER FRAYED W K NONE O OTHER ININSP/MAINT 1 CA 1334513345 (CAN) CONTROL CABLE NOTED TO BE FRAYED AFT OF IT'S ATTACHMENT TO THE LT RUDDER PEDAL. 1L71 3O EXPA1L71 20020213000042002021300004SW 2002 2 13 CA011211013 120011204G3222 STRUT HUGHES500N 500N 3027374SW ALLSN 250C 250C20R2 GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACK FOUND ON UPPER PART OF STRUT AROUND THE BRACE ATTACHMENT HOLE. 1G71 3U3 UNCH3WE E4CE 20020213000052002021300005SW 2002 2 13 CA011211014 120011204G3222 STRUT HUGHES500N 500N 3027374SW ALLSN 25OC 250C20R GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACK FOUND ON UPPER PART OF STRUT AROUND THE BRACE ATTACHMENT HOLE. 1G71 3U3 UNCH3WE E4CE 20020213000062002021300006SW 2002 2 13 CA011211015 120011204G3222 STRUT HUGHES500N 500N 3027374SW ALLSN 25OC 250C20R GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACK FOUND ON UPPER PART OF STRUT AROUND THE BRACE ATTACHMENT HOLE. 1G71 3U3 UNCH3WE E4CE 20020213000072002021300007SW 2002 2 13 CA011211016 120011123G3222 STRUT HUGHES500N 500N 3027374SW ALLSN 25OC 250C20R GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACK FOUND ON UPPER PART OF STRUT AROUND THE BRACE ATTACHMENT HOLE. 1G71 3U3 UNCH3WE E4CE 20020213000082002021300008SW 2002 2 13 CA011211017 120011204G3222 STRUT HUGHES500N 500N 3027374SW ALLSN 25OC 250C20R GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACK FOUND ON UPPER PART OF STRUT AROUND THE BRACE ATTACHMENT HOLE. 1G71 3U3 UNCH3WE E4CE 20020205001282002020500128EA 2002 2 5 CA011211018 220011205G7320A5222690 THROTTLE CABLE BELL A5222640 BELL 47 47G2 1181008SW LYC O435 VO435A1E 41516EA BELOW RH ENGINE FROZEN W B EMER. DESCENT F FLT CONT AFFECTED CRCRUISE 1 CA (CAN) THROTTLE FROZEN AT CRUISE POWER WHEN HELICOPTER CLIMBED THROUGH FREEING LEVEL AT APPROXIMATE 3,000'. THE CABLE BECAME UNSTUCK WHEN THE HELICOPTER RETURNED TO A LOWER LEVEL. BY THIS TIME THE PILOT (FLIGHT INSTRUCTOR) CARRIED OUT AN AUTO ROTATION TO ABBOTSFORD AIRPORT AND HOVER TAXIED BACK TO THE HANGAR. 1G71 3O3 O H1 E279 20020213000092002021300009CE 2002 2 13 CA011211019 120010508G552107346041 RIB CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULYD3A34 D3A34C403 GL LT ELEVATOR CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) LEAD BALANCE WEIGHT ATTACHES TO AFFECTED RIB AND CORROSION FORMED DUE TO DISSIMILAR METAL. AREA IMPOSSIBLE TO INSPECT UNLESS ELEVATOR TIP SKIN IS REMOVED TO ACCESS RIB. UPON REPLACEMENT OF RIB, 1H71 3O3 O 3A24 E5CE 5 CP47GL 20020213000172002021300017EA 2002 2 13 CA011212002 220011203G8530AEL6510241 CYLINDER CESSNA172 172P 2072436CE LYC O320 O320D2J 41508EA ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A REGULAR MAINTENANCE INSPECTION THE CYLINDERS WERE VISUALLY CHECKED USING A BORESCOPE, CRACKS WERE NOTED AT THE SPARK PLUGS PORTS OF NR 1 & 2 CYLINDERS. ALL CYLINDERS WERE REMOVED AND REPLACED. 1H71 3O3 ONT3A12 E274 20020213000182002021300018CE 2002 2 13 CA011212003 120011202G56105042006938 WINDSHIELD BEECH 100 B100 1152919CE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) WINDSHELD CRACKED / CRAZED DURING CRUISE FLIGHT. THE CREW LOWERED CABIN PRESSURE, DISCOUNTINUED HEAT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE INNER LAMINATE LAYER OF THE WINDSHIELD PRC SEALED TO THE WINDOW FRAME STRUCTURE WHICH PREVENTED FREE FLOATING OF THE WINDSHIELD WITHIN THE WINDOW FRAME CREATING STRESS TO THE INNER LAMINATE LAYER WHICH-EVENTUALLY CRACKED. A NEW WINDSHIELD ASSY WAS INSTALLED. 1L72 4T A14CE 20020213000192002021300019CE 2002 2 13 CA011212004 120011211G2140 DIAPHRAGM CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO HEATER FUEL PUMPDAMAGED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) FUEL WAS NOTICED LEAKING FROM THE HEATER FUEL PUMP VENT LINE. THE FUEL PUMP WAS DISMANTLED AND THE DIAPHRAM WAS FOUND TO HAVE FAILED CAUSING FUEL TO LEAK DOWN TO THE BEARING, REMOVING ALL LUBRICATION AN ALSO FALLING. THE FUEL PUMP WAS REPLACED. 1L72 3O3 O A7CE E8CE 20020213000202002021300020CE 2002 2 13 CA011214001 120011214G7931PTI052287579522 OIL FILTER BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA ENGINE OIL DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHEN REPLACING INBD O-RING, FOUND VERY SHARP EDGE IN OIL FILTER BODY DAMAGING O-RING EVERY TIME. 1L72 3T4 TRT3A20 E4EA 20020213000212002021300021CE 2002 2 13 CA011217001 120011011G3233115380103 BEARING BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA MLG ACTUATOR FAILED W O OTHER J WARNING INDICATION CLCLIMB 1 CA (CAN) ON CLIMBOUT RT GEAR DID NOT INDICATE UP & LOCKED & INTRANSIT LIGHT ILLUMINATED. GEAR EXTENDED, THIS TIME GEAR DID NOT INDICATE DOWN & LOCKED & INTRANSIT LIGHT REMAINED ILLUMINATED. UPON LDG RT MAIN GEAR COLLAPSED. LDG GEAR ACTUATOR REMOVED & SENT TO TSB LAB FOR ANALYSIS. IT DETERMINED THAT THRUST BEARING IN ACTUATOR WAS INSTALLED BACKWARDS. RESULTING FAILURE OF THRUST BEARING CAUSED TEETH ON PINION & RING GEAR TO FAIL. 1L72 3T4 T A14CE E4EA 20020213000232002021300023EU 2002 2 13 CA011217004 120011212G24345243212137 DRIVE SHAFT PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL NR 2 GENERATOR WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING ROUTINE 3000 HOUR INSPECTION THE DRIVE SHAFT WAS FOUND TO BE WORN AT THE FWD END OF THE SHAFT. THIS CAUSED THE SHAFT TO WOBBLE EVEN WITH THE NEW BEARING IN PLACE.FWD BEARING WAS NOT SIEZED OR STIFF.NEW SHAFT AND BEARINGS INSTALLED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020213000242002021300024SO 2002 2 13 CA011217005 120011028G371061183 GASKET PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA VACUUM PUMP TORN W EA ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CRCRUISE 1 CA (CAN) PILOT EXPERIENCED OIL PRESSURE LOSS RT ENGINE WHILE INCRUISE. SHUTDOWN AND A/C LANDED WITH NO OTHER INCIDENT. ENGINE WAS REMOVED. INSPECTION FOUND ONE LOOSE VACUUM PUMP RETENSION NUT. WHEN PUMP AND ADAPTOR REMOVED GASKET FOUND TORN AREA NEAR LOOSE NUT. THIS AREA COVERS AN OIL JET WHICH IS NOT USED FOR THIS VACUUM PUMP INSTALLATION. 1L72 3O3 O A20SO E14EA 20020213000292002021300029WP 2002 2 13 CA011217011 220011120G725031081251 BLADE GARRTTTPE331TPE33110UA 01514WP ENGINE ERODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) BORESCOPE INSPECTION REVILED ERODED BLADES AT FUEL NOZZLE CHANGE. 4 T E4WE 20020213000302002021300030EU 2002 2 13 CA011217013 120011212G243523085024 STARTER GEN PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL ENGINE WRONG PART W D RETURN TO BLOCK W INADEQUATE Q C TXTAXI/GRND HDL 1 CA (CAN) STARTER- GEN REMOVED PREMATURELY AT 950 HRS TSO DUE TO UNIT BEING VERY NOISY AT LOWER RPMS. UNIT TAKEN TO AMO FOR OVERHAUL. ON DISASSEMBLY, IT WAS NOTICED THAT UNIT DOES NOT PHYSICALLY CORRESPOND WITH MANUFACTURE`S STARTER-GEN. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020213000322002021300032SO 2002 2 13 CA011217016 120011210G214088D9310 COMBUST CHAMBER JANITROL 90D382 PIPER PA44 PA44180 7104402SO HEATER CRACKED W K NONE L NO TEST ININSP/MAINT 1 CA A95080021 (CAN) THE COMBUSTION TUBE LEAK RATE WAS GREATER THAN ALLOWED AMOUNT. THE HEATER ASSEMBLE WAS REMOVED AND THE COMBUSTION TUBE WAS REMOVED FROM THE HEATER ASSEMBLY. ANOTHER DECAY TEST WAS CARRIED OUT ON THE COMBUSTION TUBE AND WAS FOUND TO HAVE A 1 INCH CRACK ON THE AFT FACE. THE COMBUSTION TUBE WAS SENT OUT FOR REPAIR. IT IS FELT THAT THE HEATER CRACKED DUE TO THE CONSTANT HEATING AND COOLING DURING REGULAR CYCLES OF THE HEATER OPERATIONS. 1L72 3O A19S0 20020213000332002021300033CE 2002 2 13 CA011217017 120011207G321330A04000100 STRUT CESSNA180 180J 2072622CE CONT O470 O470R 17026SO MCAULY2A34C 2A34C201 GL MLG BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) 1/4 INCH RETAINER PIN BROKE AT COTTER PIN HOLE ON RT SHOCK STRUT ASSY. WHEN THE RETAINER PIN FALLS OUT THE LANDING GEAR FALLS DOWN. 1H71 3O3 O 5A6 E273 5 CP3EA 20020213000342002021300034EA 2002 2 13 CA011217018 220011130G8520LW18840 CAMSHAFT ZLIN 242 Z242L 9970204EU LYC O360 AEIO360A1B6 41514EA ENGINE WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING SCHEDULED 50 HOUR INSPECTION THAT CONTAINED TASKS REQUIRED TO COMPLY WITH THE ENGINE ON THE CONDITIONS PROGRAM ESTABLISHED FOR THE ENGINE BEING INSPECTED, A MODERATE AMOUNT OF VERY SMALL METAL PARTICLES WERE FOUND IN THE OIL FILTER ELEMENT DURING INSPECTION. NUMBER ONE CYLINDER WAS REMOVED IN ORDER TO INVESTIGATE THE SOURCE OF THE SOURCE OF THE METAL CONTAMINATION. WITH THE CYLINDER REMOVED IT WAS OBSERVED THAT THE FRONT LOBE OF THE ENGINE CAM SHAFT WAS WORN ABNORMALLY AND THE CAM FOLLOWER WAS VERY BADLY SPALLED. THE ENGINE WAS REMOVED FROM THE AIRCRAFT AND SENT OUT FOR REPAIR. 1L71 3O3 O0 A76EU 1E10 20020213000352002021300035NM 2002 2 13 CA011217019 120011101G6320A0061 GEARBOX ROBSINR22 R22BETA 7640110NM LYC O320 O320B2C 41508EA MAIN ROTOR MAKING METAL W EA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) OCT23 AT 1290 HRS M/R OIL CHANGED (500 HR CHANGE. OCT 30 IN CRUISE FLIGHT MAIN ROTOR CHIP LIGHT -M/R CHIP PLUG REMOVED AND CLEANED OCT 31. OCT 31 MADE ANOTHER FLIGHT 1.1 HRS NO CHIP LIGHT. NOV.1 ON START UP CHIP LIGHT ON M/R AGAIN. SHUT-DOWN AND INSPECTED-FOUND NUMEROUS CHIPS AGAIN. M/R TRANSISSION REMOVED AND SENT TO ROBINSON FOR REPAIR OVERHAUL WAS REQUIRED. NO REPORT ON WHAT PART FAILED. 1G71 3O3 O H10WE E274 20020213000532002021300053EA 2002 2 13 CA011217025 120011217G3411 CONNECTOR KOLLSMAN 518B02 DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE PITOT HEAD FAILED W K NONE L NO TEST ININSP/MAINT 1 CA 21548 3342 (CAN) DURING A ROUTINE INSPECTION , WHEN THE PITOT HEATER SWITCH WAS SELLECTED THE CIRCUIT BREAKER WOULD POP. INVESTIGATION REVEALED THAT THE FEMALE ELECTRICAL CONNECTER TO THE PITOT HEAD HAD FAILED CAUSING A DIRECT SHORT. THE FEMALE PIN CONNECTER WAS REPLACED WITH A NEW UNIT. 1H71 3R3 R A806 5E1 20020213000542002021300054EA 2002 2 13 CA011218002 120011128G7603C6EC12551 THROTTLE CABLE DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A27 52043EA LT ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURIING A ROUTINE EMMA CHECK 46, THE LT ENGINE THROTTLE CABLE TURNBUCKLE END WAS FOUND FRACTURED AND WAS ONLY HELD TOGETHER BY LOCKWIRING. CABLE REPLACED. 1H72 3T4 TRTA9EA E4EA 20020213000652002021300065EA 2002 2 13 CA011218009 120011129G2720VALLT2CF1029R1 CONTROL CABLE DHAV DHC2 DHC2MK1 2800102EA PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL RUDDER FRAYED W A UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 CA (CAN) FOUND THE FORWARD RUDDER CABLE TO BE SHOWING WEAR AT THE LOCATION AT THE FAIRLEAD AT STATION 8.00. THE CABLE WAS REPLACED WITH A NEW UNIT AND THE CABLE RUN WAS CHECKED THROUGH THE FAIRLEAD. 1H71 3R4 T A806 E4EA 6 CP15EA 20020213000682002021300068 2002 2 13 CA011218012 420011217G2562 ELT SAFETY EQUIP FAILED W K NONE L NO TEST ININSP/MAINT 1 CA (CAN) DURING ANNUAL RECERTIFICATION ELT WAS FOUND TO HAVE NO TRANSMIT. UNIT WAS RETURNED TO THE MANUFACTURER FOR REPAIR. 20020213000692002021300069 2002 2 13 CA011218013 420011217G2562 SWITCH POINTER 400010 ELT FAILED W K NONE L NO TEST ININSP/MAINT 1 CA 408494 (CAN) DURING ANNUAL RECERTIFICATION ELT G-SWITCH FAILED TO ACTIVATE UNIT. UNIT WAS RETURNED TO THE MANUFACTURER FOR REPAIR. 20020213000702002021300070SO 2002 2 13 CA011219003 120011130G76032489418 THROTTLE CABLE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA LT ENGINE FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) UPON REACHING CRUISE ALTITUDE, WHILE ATTEMPTING TO SET CRUISE POWER LEFT THROTTLE CABLE JAMMED AT 38 INCHES MANIFOLD PRESSURE. MTCE INSP REVEALED. LE THROTTLE CABLE SEIZED UPON ATTEMPTS TO FREE CABLE, CABLE BROKE APPROX. 1 INCH INSIDE CABLE FROM QUADRANT SWAGE CONNECTION. 1L72 3O3 O A20SO E14EA 20020213000722002021300072CE 2002 2 13 CA011219004 120011205G3220124340215 TRUNNION CESSNA210 P210N 2073454CE CONT O520 TSIO520P 17040SO MCAULYD3A34 D3A34C402 GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) NOSE LANDING GEAR LOWER TRUNNION FOUND CRACKED. 1H71 3O3 O 3A21 E8CE 5 CP47GL 20020213000742002021300074EA 2002 2 13 CA011219005 220011123G73221060301 CARBURETOR HUGHES269 269C1 8059504SW LYC O360 HO360C1A 41514EA ENGINE MALFUNCTIONED W O OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 CA (CAN) ENGINE ROUGH AND SLOW AT RECOVERY FROM AUTOROTATOR. REPLACE CARBURATOR. 1G71 3O3 OO 4H12 E286 20020213000772002021300077CE 2002 2 13 CA011219006 120010520G531207421155 BULKHEAD CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULYD3A34 D3A34C403 GL CARGO BAY CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACK NOTED ON LT BULKHEAD DURING INSPECTION WITH MIRROR. BULHEAD IS LOCATED DIRECTLY ADJACENT TO BAGGAGE DOOR. 1H71 3O3 O 3A24 E5CE 5 CP47GL 20020213000782002021300078CE 2002 2 13 CA011219007 120011212G1100 PLACARD CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL COCKPIT MISSING W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AIRSPEED LIMIT PLACARD NOT INSTALLED ON COMPANY PER T.C. A37CE. 1H71 3T3 T A37CE E4EA 5 CP60GL 20020213000812002021300081CE 2002 2 13 CA011219008 120011203G272005430224 TUBE CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA RUDDER JAMMED W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CA (CAN) A/C HAS 15120.6 T.AT. TIME ON PART UNKNOWN, MAY BE ORIG. UPON TAXI TO HOLD LINE, PILOT TURNED FULL LEFT THEN FULL RIGHT TO CHECK BRAKES & STEERING. PILOT APPLIED FULL POWER AFTER T/O CLEARENCE & HAD TO KEEP GREATER THAN NORMAL RIGHT RUDDER TO KEEP A/C STRAIGHT. WHEELS LEFT GROUND AT 70K A/C IMMEDIATLY YAWED HARD LEFT. PILOT PUT IN FULL RIGHT RUDDER & AILERON TO COMBAT, RUDDER STAYED JAMMED HARD LEFT. A/C LANDED ON GRASS & HIT DITCH CAUSING EXTENSIVE ENGINE, PROP & FUSELAGE DAMAGE. AME & TSB DISCOVERED THAT RT STEERING PUSH-PULL ROD COULD HAVE JAMMED IN SHORTENED POS&AS OLEO EXTENDED, IT PULLED LT RUDDER PEDAL IN, IN TURN DEFLECTING RUDDER FULL LEFT. WASHER THAT USUALLY SLIDES FREELY IN S TEERING TUBE 1H71 3O3 ONT3A19 E223 20020213000822002021300082NE 2002 2 13 CA011219009 120011209G29107665103004073 LINE SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S1 60030NE HYD SYSTEM CHAFED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) DURING POST FLIGHT WALK AROUND FLIGHT CREW NOTICED HYD FLUID LEAKING OUT OF COWLING. COWL WAS REMOVED. HYD RESEVOIR WAS 1/2 FULL AND A/C GROUND RUN A LEAK WAS DETECTED UNDER A CLAMP OF NR 2 SYSTEM PRESSURE LINE. THE LINE WAS REPLACED WITH A NEW PART, NR 2 SYSTEM HYD OIL TOPPED UP TO FULL MARK. A/C GROUND RUN & LEAK CHECKED SERVICEABLE & RETURNED TO SERVICE. 1G72 3U3 U H1NE E19EU 20020213000932002021300093 2002 2 13 CA011220001 420011219G6122 NUT MCAULY C290D4MT4 CESSNA210 210R 2073458CE CONT O520 IO520L 17032SO MCAULYD3A34 D3A34C404 GL RELIEF VALVE LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA 980085 (CAN) DURING ROUTINE GROUND MAINTENCE OIL WAS DISCOVERED EMINATING FROM THE ENGINE COWLING. INVESTIGATION WHICH INCLUDED WASHING DOWN THE AREA AND A RUN UP REVEALED OIL LEAKING FROM THE RELIEF VALVE ADJUSTMENT NUT. REPLACED PROPELLOR GOVERNOR, RAN ENGINE NO LEAKS FOUND.NO PART NUMBER AVAILABLE FOR THE ADJUSTMENT NUT/RELIEF VALVE 1H71 3O3 ORT3A21 E5CE 5 CP47GL 20020213000942002021300094SO 2002 2 13 CA011220002 120011217G3213 HINGE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA LT MAIN GEAR CRACKED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 16538 (CAN) AFTER T/O SELECTED GEAR UP, THE HANDLE RETURNED WITH A RED LIGHT. THE GEAR WAS RECYCLED, WITH NO CHANGE.GEAR SELECTED DOWN AND AIRCAFT LANDED WITHOUT INCIDENT. PART TIMES AND CYCLES FROM AIRCRAFT TIME. 1L72 3O3 O A20SO E14EA 20020213001002002021300100WP 2002 2 13 CA011220003 120011218G6700 BUNGEE CYLINDER ROBSINR44 R44 7640120WP CYCLIC FAILED W O OTHER O OTHER CRCRUISE 1 CA (CAN) PLIOT COMPLAINED OF HEAVY AFT CYCLIC FORCES.INVESTIGATION REVEALED CYCLIC BUNGEE TO BE DISCONNECTED FROM AFT ATTACH POINT ON PUSH ROD P/N C121-9 AT C317-1 BELLCRANK. SUSPECT DISCONNECTION IS DUE TO COLD OPERATING ENVIRONMENT AT THIS TIME. LOCAL TEMERATURES REACHED BELOW -25 DEGREES C.BUNGEE MATERIAL MAY STIFFEN WHEN COLD CAUSING A LOS OF ELASTICITY AND ALLOWING THE DISCONNECTION. THIS AIRCRAFT HAS THE UPDATED STYLE BUNGEE ATTACHMENT CLIP. 1G71 3O H11NM 20020213001012002021300101WP 2002 2 13 CA011220004 120011219G6700 BUNGEE CYLINDER ROBSINR44 R44 7640120WP CYCLIC FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING 100 HOUR INSPECTION, BOTH AFT BUNGEES WERE FOUND TO BE DISCONNECTED AT THE AFT PUSH PULL TUBE C121-9 AT THE C317-1 BELLCRANK.SUSPECT DISCONNECTION IS DUE TO COLD OPERATING ENVIRONMENT AT THIS TIME. LOCAL TEMPERATURES REACHED BELOW -25 DEGREES C. BUNGEE MATERIAL MAY STIFFEN WHEN COLD CAUSING A LOSS OF ELASTICITY AND ALLOWING FOR DISCONNECTION.NOTE THIS AIRCRAFT HAS THE UPDATED STYLE BUNGEE ATTACHMENT CLIP. 1G71 3O H11NM 20020213001032002021300103CE 2002 2 13 CA011221001 120010520G551107321014 BRACKET CESSNA 12320008 CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULYD3A34 D3A34C403 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACK NOTED FROM RETAINER'S EDGE TO INBOARD ATTACHMENT SCREW HOLE AS VIEWED FROM THE LT SIDE OF A/C. ANOTHER CRACK NOTED IN BOTTOM BEND RADIUS OF BRACKET AND EXTENDING ALONG THE BEND FOR APPROX. 1 INCH. PROBABLE CAUSE IS FROM CARRYING EXTERNAL LOADS ON THE SIDE OF THE A/C SUCH AS CANOES, SMALL BOATS ETC. 1H71 3O3 O 3A24 E5CE 5 CP47GL 20020213001072002021300107SW 2002 2 13 CA011221004 120011203G534371470101R TUBE BBAVIA8 8GCBC 1220803SW LYC O360 O360C2E 41514EA MLG BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) TUBE FOUND BROKEN THROUGH APPROXIMATELY AT WELD TO RT FORWARD END OF LDG FITTING. 1H71 3O3 O A21CE E286 20020214000052002021400005CE 2002 2 14 CA011221007 120011205G3222030A39313 BOLT MTSBSIMU2 MU2B36 5780412CE NLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE NOSE LANDING GEAR DRAG STRUT ATTACH BOLT WAS FOUND CRACKED. THIS BOLT HAD BEEN MAGNETIC PARTICAL INSPECTED EVERY 2000 HOURS. 1H72 3T RTA10SW 20020214000062002021400006CE 2002 2 14 CA011221008 120011220G7920017A4710127 LINE MTSBSI MTSBSIMU2 MU2B36 5780412CE OIL COOLER CHAFED W K NONE WK INADEQUATE Q C FLUID LOSS ININSP/MAINT 1 CA (CAN) THE OIL LINE RUNNING FROM THE OIL COOLER WAS FOUND CHAFED BY A SCREW THAT WAS TOO LONG IN A PANEL ON THE SIDE OF THE NACELLE. THE LINE WAS REPLACED AND THE SCREW WAS REPLACED WITH A SHORTER ONE 1H72 3T RTA10SW 20020214000122002021400012CE 2002 2 14 CA011231003 120011224G24605036430821 DIODE BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA BUSS FEEDER BURNED W O OTHER O OTHER APAPPROACH 1 CA (CAN) PILOT HAD MULTIPLE FAILURES WHEN COMING IN TO LAND, SOME EXTERIOR AND INTERIOR LIGHTS WOULD NOT WORK AND THE LANDING GEAR WOULD NOT COME DOWN. THE PILOT EXTENDED THE GEAR MANUALLY AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT NR 1 BUSS FEEDER DIODE BURNT. THE RT NR 1 BUSS FEEDER DIODE WAS REPLACED, NR 2 BUSS FEEDER DIODE WAS REPLACED AND THE RT NR 1 BUSS FEEDER WIRE CONNECTOR PIN WAS ALSO REPLACED AT THE RT CIRCUIT BREAKER PANEL. BEECHCRAFT HAS AN INSPECTION EVERY 800 HOURS THAT WOULD HAVE IDENTIFIED THE PROBLEM DIODE BEFORE THIS HAPPENED, THIS AIRCRAFT WAS 150 HOURS AWAY FROM THAT INSPECTION. I SUBMITTED ANOTHER SDR ON THIS SUBJECT SEE CONTROL NUMBER 19991230038 1L72 3T4 T A14CE E4EA 20020214000142002021400014EU 2002 2 14 CA020102001 120011211G6410 BLADE SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE TAIL ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 6875 (CAN) 35 MM CRACK IN BLADE SKIN ON TAIL ROTOR. 1G71 3U3 U H9EU E00054EN 20020214000162002021400016CE 2002 2 14 CA020102003 120011120G551005320019 SPAR CESSNA 0532001201 CESSNA172 172B 2072406CE CONT O300 O300D 17022SO HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AT ANNUAL INSPECTION THE CENTRE SECTION OF THE STABILIZER SPAR WAS FOUND TO BE BUCKLED AND CRACKED AT THE CENTRE LIGHTENING HOLE, WHERE THE TRIM CABLES RUN THROUGH. THERE WERE TWO CRACKS ABOUT 2 IN. LONG, RUNNING FROM THE BOTTOM RIGHT AND TOP LEFT SIDES OF THE HOLE, WITH CORRESPONDING BUCKLING. THE CRACKS WOULD OPEN AND CLOSE AS PRESSURE WAS APPLIED TO THE TIP OF THE STABILIZER - UP OR DOWN. THE STABILIZER HAD ONLY A SLIGHT LOSS OF STIFFNESS - SO THE PROBLEM WAS ONLY NOTICED BY VISUAL INSPECTION OF THE AFFECTED AREA. THE STABILIZER WAS REMOVED AND REPAIRED. 1H71 3O3 ONT3A12 E253 20020214000172002021400017EU 2002 2 14 CA020103001 120011201G63204638302023 BEARING 4638001010 BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL M/R GEARBOX SPALLED W K NONE O OTHER ININSP/MAINT 1 CA 1159 (CAN) GEARBOX RECEIVED FROM THE USA FOR INVESTIGATION OF METAL CONTAMINATION. UPON DISASSEMBLY THE SUBJECT BEARING SHOWS SIGNS OF EXCESSIVE PEELING ON ONE BALL, 75 PERCENT OF AREA AFFECTED. ANOTHER BALL ALSO STARTING TO PEEL. ONE HALF OF SPLIT INNER RACE HAD SPALLING OVER 10 PERCENT OF BEARING SURFACE. 1G72 3U3 UNCH3EU E4CE 20020214000182002021400018EU 2002 2 14 CA020103003 120011209G2916PPEV3008EA3B POWERPACK PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL HYD SYSTEM CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) DURING A DAILY INSPECTION BY MAINTENANCE STAFF AT THE COMPLETION OF SCHEDULED FLIGHT. HYDRAULIC FLUID WAS FOUND AT LH WING ROOT, BOTTOM OF WING,WHERE ACCESS PANEL IS LOCATED FOR HYDRAULIC POWER PACK. THE AMOUNT OF FLUID LOST DID NOT EFFECT OPERATION OF SYSTEM. THE LEAK WAS DETERMINED TO BE A CRACK IN THE RESEVOIR OF THE HYDRAULIC POWER PACK STARTING AT THE TOP OF RESEVOIR AND TRAVELLING DOWN TO THE BOTTOM OF RESEVOIR WHERE THE ELECTRIC MOTOR IS MOUNTED. HYDRAULIC POWER PACK WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020205001332002020500133EA 2002 2 5 CA020103004 220011211G74141038255514 MAGNETO LYC CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA MCAULY1C160 1C160DTM GL ROTOR & GEAR FAILED W A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 CA (CAN) THE AIRCRAFT ENGINE HAD JUST UNDERGONE AN ON CONDITION INSPECTION AND HAD MET ALL REQUIRED PARAMETERS, INCLUDING FULL POWER CHECK. ONE SIDE OF THE DUAL MAG FAILED ON FIRST FLIGHT POST INSPECTION. UPON DISSASSEMBLY OF DISTRIBUTION BLOCK. SEVERAL ROTOR TEETH WERE FOUND BROKEN OFF. THE ROTOR BEARING WAS FOUND WITH EXCESSIVE WEAR AND THE DISTRIBUTOR CONTACTS APPEAR TO HAVE TOUCHED. 1H71 3O3 ONT3A12 E274 5 NP910 20020214000192002021400019GL 2002 2 14 CA020103005 320011201G6114MS20073XXXX BOLT CESSNA150 150M 2071830CE CONT O200 O200A 17020SO MCAULY1A102 1A102OCM GL PROPELLER WRONG PART W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE REMOVING MCCAULEY PROP FOR 5 YEARS CORRISON INSPECTION IT WAS NOTED THAT PROP BOLTS WERE TO SHORT APPROX 4 THREADS ON ALL BOLTS WERE SECURING THE PROP. NEW BOLT KIT A2513-77 INSTALLED & LOCKED. 1H71 3O3 O 3A19 E252 5 NP918 20020214000202002021400020NE 2002 2 14 CA020103006 220011213G7230350A070867 SEAL SNIAS 350 AS350BA 8680817EU LYC LTS101LTS101600A3 41560NE COMPRESSOR DESTROYED W A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) A/C IN CRUISE. FLYING IN SNOW, VISIBILITY 1 MILE, TEMP -2 DEGS. ON 1ST FLT OF DAY. AFTER 25 MIN FROM TAKEOFF, A/C HAD LIGHT COMPRESSOR STALL. THEN HAS A SERIES OF LARGE ONES. HAD SOME RPM DROP. ON INSPECTION AFTER LDG. FOUND 2 OF INTAKE SEALS INCLUDING RETAINING STRIPS & CLIPS IN INTAKE BOX. ONE RETAINING STRIP & CLIPS & ALSO ONE RUBBER SEAL MISSING. AXIALCOMPRESSOR WHEEL BLADES ARE SEVERELY DAMAGED. ENGINE IS PRESENTLY REMOVED.. 1G71 3U3 UNCH9EU E5NE 20020228000012002022800001EA 2002 2 28 CA020103010 120011220G7921 OIL COOLER GENELC CF343B1 CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT ENGINE LEAKING W K NONE K FLUID LOSS APAPPROACH 1 CA 872259 (CAN) A/C ON APPROACH WHEN CREW NOTED LEFT OIL PRESSURE FLUCTUATING. CREW RPTED PRESSURE FLUCTUATING UP TO 25 PSI&AVERAGING 30 PSI LOWER THAN RIGHT ENGINE. NO MENTION OF WARNINGS OR OTHER ACTION TAKEN. MAINT FOUND LEFT ENGINE TO BE 5 QTS LOW OF OIL. ENGINE SERVICED&RUN WITH AG AXIS LEAK PORTS OPEN. GE REP&FSR WITNESSED MUCH FLUID NOTED FROM J AXIS PORT, CONSIDERABLE STREAM COMING FROM IT&ENGINE SHUTDOWN. THISENGINE OF CONFIG THAT DID NOT HAVE CARBON SEAL&RUNNER ON THAT SHAFT. O RINGS WERE REPL&PUMP REINST ENGINE SERVICED PER GE RECOMMENDATIONS&RUN AGAIN. TIME WHEN OIL TANK CAP REMVD, QUART OR MORE OF OIL CAME OUT OF IT. THROUGH FURTHE 2L72 4F4 FRTA21EA E15NE 20020214000252002021400025SO 2002 2 14 CA020103013 120011030G52804752932 HINGE PIPER 4752932 PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA HARTZLHCE3Y HCE3YR2A GL MLG DOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) MAIN LANDING GEAR DOOR HINGES CRACKED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020214000382002021400038EU 2002 2 14 CA020103017 120011205G3150972813201 DISPLAY PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL COCKPIT MALFUNCTIONED W O OTHER N FALSE WARNING CRCRUISE 1 CA (CAN) MISC. WARNINGS LITES ILLUMINATED ALONG WITH MASTER CAUTION EVEN THOUGH ALL SYSTEMS WERE FUNCTIONING NORMALLY. ALSO CAWS DISPLAY WOULD NOT PASS LITE TEST. CAWS DISPLAY REPLACED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020214000392002021400039EU 2002 2 14 CA020103018 120011224G31509752902014 PANEL PILATSPC12 PC1245 7090551EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL COCKPIT FAILED W O OTHER N FALSE WARNING CRCRUISE 1 CA (CAN) EIS GIVING FALSE READING FOR ITT. EIS PANEL REPLACED. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20020214000402002021400040EA 2002 2 14 CA020104001 120011126G2731AN3C6A BOLT DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE ELEVATOR TRIM SHEARED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING 100 HR INSP REMOVED PUSH/PULL ROD FOR MAINTENANCE. RE-INSTALLED PUSH / PULL ROD AT LATER TIME WITH PREVIOUSLY REMOVED HARDWARE. WORK WAS CHECKED DURING INDEPENDENT INSPECTION. BOLT WAS FOUND SHEARED THE FOLLOWING DAY AFTER SITTING OVERNIGHT IN THE HANGAR, THE BOLT HEAD HAD SHEARED CLEAN OFF AND WAS FOUND ON THE HANGAR FLOOR. PART RETURNED TO SEALAND AVIATION FOR EVALUATION. 1H71 3R3 R A806 5E1 20020214000412002021400041EA 2002 2 14 CA020104002 220011214G7261PT1052287579522 OIL FILTER BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA ENGINE OIL MISMANUFACTURED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) WHEN REPLACING INBD O-RING VERY SHARP EDGE IN OIL FILTER BODY DAMAGING O-RING EVERY TIME. 1L72 3T4 TRT3A20 E4EA 20020214000422002021400042SW 2002 2 14 CA020104003 120011128G793031039721 CHIP DETECTOR GULSTM690TP 690A 0141722SW GARRTTTPE331TPE3315251K NM NR 2 ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) UPON REINSTALLATION OF THE CHIP DETECTOR DRAIN VALVE BODY IN ENGINE NR 1 BEFORE TORQUE VALVE WAS OBTAINED (75 IN LB) , THE NUT PORTION WHICH INCLUDES A RECEPTICLE FOR THE CHIP DETECTOR SEVERED OFF. INSPECTION OF THE PART SHOWED PRESENCE OF PREVIOUS CRACKING AROUND THE RADIUS. THE VALVE BODY WAS REMOVED FROM NR 2 ENGINE AND FOUND IT WAS ALSO CRACKED AROUND THE RADIUS OF THE NUT. THE REMAINING AIRCRAFT IN THE FLEET WILL BE INSPECTED FOR ANY DAMAGE IN THIS AREA. 1H72 3T4 T 2A4 E2WE 20020214000432002021400043EU 2002 2 14 CA020104004 120011211G2432 WIRE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE BATTERY BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CA (CAN) JUST PRIOR TO LDG PILOT SMELLED SOMETHING LIKE PLASTIC OR RATHER BURNING BUT NOT SMOKE. AFTER SHUTTING DOWN, PILOT COULD SEE SMOKE INSIDE TAILBOOM & STRONG SMOKE OF SOMETHING ELECTICAL SMOKING IN MAIN CARGO BAY, PILOT INVESTIGATED FURTHER TO FIND SOURCE & FOUND NOTHING OUT OF ORDINARY. PILOT TRIED START WHEN GUIDE & PASSENGER COULD SEE 3 SPARKS UNDER BELLY OF A/C. FURTHER INVESTIGATION LEAD TO BATTERY BAY. ONE OF WIRE CONNECTORS ON POSITIVE POST OF BATTERY GOT WELDED TO BATTERY CASE. BOTTOM OF BATTERY CASE BURNT&SOURCE TO GROUND TO AIRFRAME. ARE 2 WIRES OR CABLES TO POSITIVE POST OF BATTERY. 1G71 3U3 U H9EU E19EU 20020215000112002021500011 2002 2 15 CA020104012 420011130G3421 GYRO BOEING737 737275 1384485NM PWA JT8 JT8D9A 52048NE COCKPIT FAILED W C ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CA 4932849328 (CAN) ON TAKE OFF FROM EDMONTON, ELECTRICAL SPIKE MOMENTARILY FLAG CAPT.'S ADI AUTOPILOT, WHEN SELECTED ON TRIPPED, TRIED ONE MORE TIME AND WITH LIGHT PRESSURE ON ELEVATOR ON AUTOPILOT TRIPPED AGAIN. NUMBER 1 VERTICAL GYRO AND AIR DATA COMPUTER REPLACED. SYSTEM CHECKED SERVICEABLE. 2L72 4F4 F A16WE E2EA 20020215000272002021500027NE 2002 2 15 CA020104021 220011231G7323LN9367GE12N2 BEARING BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE TURBINE GOVERNORCONTAMINATED W C ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 CA (CAN) LACK OF DROOP COMPENSATION OBSERVED BY PILOTS. ENGINEERING NOTIFIED. ENGINEERING DISCOVERED A BINDING BEARING IN THE N2 CONTROL SYSTEM, LOCATED IN CABIN CEILING. BEARING WAS CLEANED OF DIRT, LUBRICATED AND FUNCTION TESTED SERVICABLE. 1G72 3U3 U H13EU E5NE10 20020215000292002021500029NE 2002 2 15 CA020104022 220011231G7323LN9367GE5DN2 BEARING BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE TURBINE GOVERNORWORN W C ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 CA (CAN) WHEN INSPECTING THE N2 DROOP SNAG(PLEASE SEE PREVIOUS SDR ON SAME DAY), THE BALL WAS DISCOVERED TO BE WORN THROUGH THE SOCKET. THE ARM ASSY WAS REPLACED BY A SERVICABLE UNIT AND THE HELICOPTER WAS RETURNED TO SERVICE. 1G72 3U3 U H13EU E5NE10 20020215000302002021500030SW 2002 2 15 CA020104023 120011227G6230 OIL JET BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA M/R MAST MISLOCATED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) DURING INSTALLATION OF MAIN ROTOR MAST ASSEMBLY IT WAS VISUALLY IDENTIFIED THAT THE OIL JET WAS LOCATED IN THE WRONG POSITION FOR CONNECTION OF OIL SUPPLY LINE. PART WAS REPLACED WITH SERVICEABLE UNIT. 1G71 4U4 U H4SW E22EA 20020215000342002021500034EA 2002 2 15 CA020108002 220011127G8530AEL6510241 CYLINDER CESSNA172 172P 2072436CE LYC O320 O320D2J 41508EA ENGINE CRACKED W A UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 CA (CAN) DURING CLIMB THE PILOT NOTICE A LOSS OF POWER AND ENGINE VIBRATION. RETURNED TO BASE. MAINTENANCE FOUND NR 3 CYLINDER CRACKED AT THE EXHAUST VALVE. THIS IS THE 3RD CYLINDER ON 2 DIFFERENT ENGINES TO CRACK IN THIS PLACE. ALL CYLINDERS REMOVED AND RETURNED TO SUPPLIER. OVERHAULED CYLINDERS INSTALLED AND AIRCRAFT RETURNED TO SERVICE. 1H71 3O3 ONT3A12 E274 20020215000352002021500035EA 2002 2 15 CA020108003 220011214G7314025323300 PUMP PIPER PA42 PA42 7104202SO PWA PT6 PT6A41 52043EA FUEL SYS STRIPPED W A UNSCHED LANDING XYJENGINE FLAMEOUT ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 CA (CAN) ENGINE SHUT DOWN IN CRUISE FLIGHT. AIRCRAFT MADE AN UNSCHEDULED LANDING TROUBLESHOOTING REVEALED NO FUEL FLOW TO DIVIDER. HIGH PRESSURE FUEL PUMP REMOVED. FUEL PUMP SPLINES FUND TO BE STRIPPED. PUMP REPLACED. 1L72 4T4 T A23SO E4EA 20020215000362002021500036EU 2002 2 15 CA020109001 120011203G530211203025221 FLANGE BOLKMS117 BK117A1 5626010EU TAILBOOM CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) TAILBOOM SENT FROM A CUSTOMER IN THE USA FOR REPAIR OF A DAMAGED SKIN. DURING DISASSEMBLY THE TAILBOOM TO FUSELAGE ATTACHMENT RING FOUND CORRODED. AT THE 1:00 AND 11:00 O'CLOCK POSITION DEPTH 1 MM AT THE 2:00 AND 10:00 O'CLOCK POSITION 0.2 MM AT THE 6:00 O'CLOCK POSITION DEPTH OF 0.6MM. 1G72 3U H13EU 20020215000372002021500037EA 2002 2 15 CA020109002 220011102G8520LW1594485 CRANKSHAFT LYC O320 O320H2AD 41508EA MAIN JOURNAL CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CORROSION FOUND UNDER URETHABOND COATING APPLIED BY FACTORY AT OVERHAUL AS PER SB 505B AND SB 530A AND AD 98-02-08.CRANKSHAFT HAS BEEN RETURNED TO FACTORY FOR WARRANTY CONSIDERATION AND INSPECTION. 3 O E274 20020215000392002021500039EA 2002 2 15 CA020109005 220011214G7261PT6A27 ENGINE BEECH 99 99A 1154003CE PWA PT6 PT6A27 52043EA HARTZLHCB3T HCB3TN3 GL NR 2 CONTAMINATED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 14795 (CAN) OIL CONTAMINATION NR 2 LIGHT ILLUMINATED AFTER TAKEOFF, DURING CLIMB OUT. RETUNED FOR LANDING. LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTION REVEALED OIL CONTAMINATED WITH METAL PARTICLES. 1L72 3T4 T A14CE E4EA 6 CP15EA 20020215000412002021500041SO 2002 2 15 CA020109006 120011221G2140 COMBUSTION LINER PIPER PA31 PA31325 7103105SO LYC O540 LTIO540F2BD 41533EA HEATER BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN) PILOT SMELLED FUMES IN THE CABIN. HE SHUT OFF THE JANITROL HEATER. HEATER WAS REMOVED AND INSPECTED FOUND A HOLE BURNED THROUGH COMBUSTION TUBE. INSTALLED NEW OVERHAULED HEATER. 1L72 3O3 O A20SO E14EA 20020228000022002022800002EU 2002 2 28 CA020110003 120011223G2420 IDG HAMSTD AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE IDG OVERHEATED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION APAPPROACH 1 CA (CAN) @1 IDG OIL PRESSURE AND OVERHEAT ON ON DESCENT TO YVR. TEMPERATURE GRADUALLY RISING (PULSATING GREEN) ECAM ACTION CARRIED OUT. IDG DISCONNECTED PRIOR LANDING.IDG FOUND OVERSERVICED. MEL 24-20-01 APPLIED. OIL STILL FLUCTUATING.IDG REPLACED AS PER AMM 24-21-51. 2L72 4F4 FRTA28NM E29NE 20020215000932002021500093SW 2002 2 15 CA020112001 120011203G281071493 FUEL TANK BBAVIA8 8GCBC 1220803SW LYC O360 O360C2A 41514EA LT WING LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) FUEL LEAK DISCOVERED BY VISIAL INSPECTION AT FABRIC DRAIN HOLES IN TE OF WING. INBOARD FUEL TANK OF LEFT WING REMOVED AND PIN HOLE FOUND IN THE WELD WHERE DRAIN BOSS WHERE FUEL HOSE ATTACHES. BOSS REWELDED AND PRESSURE TESTED TANK. NO FURTHER LEAKS FOUND. 1H71 3O3 O A21CE E286 20020215000942002021500094SO 2002 2 15 CA020114001 120010812G8120LW12463 SEAL GARRTT LW12463 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA RT ENGINE LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CA AG020227 (CAN) TURBO OIL SEAL LEAKING (EXHAUST SIDE). ABORT TAKEOFF. LOST POWER ON RT AND SMOKE. 1L72 3O3 O A20SO E14EA 20020215001002002021500100NE 2002 2 15 CA020114008 220011116G7200 ENGINE PWA JD15 JT15D1A NE LT OR RT FAILED W O OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 CA (CAN) ENGINE WAS UNABLE TO ACHIEVE THE RATED POWER WITHIN THE SPECIFIED TEMPERATURE LIMITS. THE OPERATOR DECIDED TO PERFORM AN HSI AND REMOVED THE HOT SECTION COMPONENTS FOR SHIPMENT TO ATLANTIC TURBINES FACILITY IN ATLANTA. AT THIS POINT IT WAS NOTED THAT THE ENGINE HAD SUSTAINED AN HP TURBINE BLADE FAILURE WITH CONSIDERABLE FOD. THE HP & LP TURBINE COMPONENTS WERE FORWARDED TO ATLANTIC TURBINES FOR INVESTIGATION AND RESTORATION TO SERVICEABLE CONDITION. 4 F E25EA 20020215001012002021500101EA 2002 2 15 CA020114009 220011130G7200 ENGINE PWA PT6 PT6A41 52043EA LT OR RT FAILED W OO OTHER OTHER YJ ENGINE STOPPAGE WARNING INDICATION NRNOT REPORTED 1 CA (CAN) ENGINE WAS SENT TO ATI FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED THAT ENGINE HAD BEEN SHUT DOWN IN FLIGHT. THE OPERATOR REPORTED THAT DURING THE APPROACH THE PILOT HAD NOTICED THE TURBINE INTERSTAGE TEMPERATURE HAD INCREASED TO 950 DEGREES C, AND HAD SHUT DOWN THE ENGINE AND LANDED ON THE ONE REMAINING ENGINE. THE OPERATOR HAS SPLIT THE ENGINE, NOTED EXTENSIVE INTERNAL DAMAGE, AND RE-ASSEMBLED THE UNIT PRIOR TO SHIPMENT TO ATI. 4 T E4EA 20020215001022002021500102CE 2002 2 15 CA020116001 120011130G3310A91641 BRACKET CESSNA310 310R 2074245CE CONT O520 IO520MB 17032SO MCAULY3AF32C3AF32C87 GL LIGHT BROKEN W F ACTIVATE FIRE EXT. A FLAME/FIRE APAPPROACH 1 CA (CAN) FIRE IN COCKPIT ON DESCENT FROM FLIGHT TO AIRPORT. SMOKE EMITING FROM RT DASH BY PROP DE-ICE GAUGE. SMOKE TURNED TO FLAME AND EXTINGUISHER EXERCISED. EXAMINATION REVEALED POST LIGHT PLASTIC BROKEN AND FELL DOWN TO METER. LINE POST LIGHT SHORTED ON METER TERMINAL. POST LIGHT SOCKET PLASTIC HEATED UP AND PLASTIC CAUGHT FIRE. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20020215001062002021500106GL 2002 2 15 CA020116007 320011106G6114 PROPELLER MOONEYM20 M20C 5870208SW LYC O360 O360A1D 41514EA HARTZLHCC2Y HCC2YR1 GL FORWARD DAMAGED W K NONE L NO TEST ININSP/MAINT 1 CA (CAN) OWNER DISCOVERED PROP WOULD NOT CYCLE AT PRE-FLIGHT INSPECTION. AIRCRAFT WAS BROUGHT TO THE SHOP AND THE SPINNER WAS REMOVED. GREASE FITTINGS WERE REMOVED AND OIL BEGAN TO RUN OUT. PROP WAS REMOVED AND SENT FOR INSPECTION. 1L71 3O3 O 2A3 E286 5 CP920 20020219000562002021900056SO 2002 2 19 CA020117010 120011120G2460454709 CIRCUIT BREAKER PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA COCKPIT BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AT A ROUTINE 100 HOUR ANNUAL INSPECTION IT WAS DISCOVERED THAT TWO CIRCUIT BREAKERS HAD BROKEN REAR ATTACHMENT LUG AT THE BUS BAR ATTACH POINT. 1L71 3O3 O 2A13 E286 20020219001252002021900125EU 2002 2 19 CA020117017 120011210G5240A2151060200200 DOOR AIRBUS310 A310 EU GE CF6 CF680C2A5 NE FUELING PANEL MISSING W O OTHER D INFLIGHT SEPARATION LDLANDING 1 CA (CAN) FOUND REFUELING PANEL DOOR MISSING ON ARRIVAL TO "VRA". REFUELING DOOR AND AN AIR INLET PANEL WERE REPLACED. 2L72 4F4 FRTA35EU E13NE 20020219001262002021900126WP 2002 2 19 CA020117018 120011204G2780 CONTROL VALVE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE LE FLAPS MALFUNCTIONED W A UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 CA (CAN) ON FERRY FLIGHT TSC 2257 FROM CUN-YMX , DURING TAKE OFF , SLAT SYSTEM LOCKED IN EXTEND POSITION , BUT FLAPS RAISED FULL UP. FLAP RED LIGHT WAS ILLUMINATED ON THE FLAP POSITION INDICATOR (PILOTS CENTER INSTRUMENTS PANEL) AND SLAT MONITOR INDICATED SLATS AT 30 DEGREES.-AIRCRAFT RETURNED TO "CUN".-ON GROUND , POP OUT INDICATOR FOUND OK ON BOTH WING FOR BRAKE INDICATOR. -C/B RESETTED , SYSTEM TEST C/OUT IN ACCORDANCE WITH M.M. 27-81-00. NO FAULTS FOUND.-NO DEFECTS WERE REPORTED AFTER TAKE OFF. 2L73 4F4 F A23WE E12EU 20020219001272002021900127EU 2002 2 19 CA020118001 120011220G27804907905 CONTROL UNIT AIRBUS310 A310300 3930305EU GE CF6 CF680C2A5 NE LE FLAPS MALFUNCTIONED W O OTHER J WARNING INDICATION APAPPROACH 1 CA (CAN) MANY INDICATIONS (DEFECTS REPORTED) OF SLATS / FLAPS SYSTEM NR 1 & 2 FAULTS HAVE BEEN REPORTED ON AIRCRAFT, HAVING SEVERAL MAINTENANCE ACTION C/OUT FROM 2001-11-25 TO 2001-12-20 AND THE FINAL RECTIFICATION BEING THE REPLACEMENT OF THE LAT FLAP CONTROL COMPUTER (SFCC); _DATE 2001-12-20 ; FLAPS SYS NR 2 FAULT WITH SPEED LIMIT ON RT SIDE PFD SLATS AND FLAPS MOVE AT HALF SPEED ALL MTCE ACTIONS C/O AND "O" OPERATION FOR FLIGHT CREW PLACED ON DMI AS PER MEL 27-18 A C T I ON TA KE N SFCC 2 REPLACED IAW 27-51-18 AND BITE TEST PERFORMED.CHECKED SERVICEABLE. 2L72 4F4 FRTA35EU E13NE 20020219001282002021900128SW 2002 2 19 CA020118003 120010725G62302060400365 BEARING BELL 20601033217 BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL MAIN ROTOR MAST SPALLED W K NONE O OTHER ININSP/MAINT 1 CA FAJF56057 (CAN) UPON INSPECTION 3 BALL BEARINGS, FOUND EXCESSIVELY SPALLED AND INNER RACE SHOWED 3 SIGNS OF PITTING IN 3 AREAS. BEARING WAS SCRAPPED. 1G71 3U3 U H2SW E4CE 20020219001292002021900129SW 2002 2 19 CA020118004 120010725G623020601033217 MAST BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL MAIN ROTOR CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) UPON 1500 HOUR INSPECTION OF MAST BEARING RETAINING NUT REMOVAL. PRC SEALANT WAS REMOVED FROM THE LOWER MAST THREADS TO UNCOVER CORROSION PITTING WELL IN EXCESS OF CORROSION TOLERANCES. MAST WAS SCRAPPED. 1G71 3U3 U H2SW E4CE 20020219001302002021900130EU 2002 2 19 CA020118005 120011221G2910AE71112111 LINE AIRBUS330 A330243 3930330EU RROYCERB211 RB211TRENT77 NE HYD SYSTEM MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 41063 (CAN) -DURING CURRENT C03 /A06 HEAVY MAINT VISIT , NR 2 HYDRAULIC PUMP PRESSURE TUBE POSED WITH NO CLEARANCE WITH RESPECT TO THE FUEL / OIL HEAT EXCHANGER HOUSING (ADJACENT TO THE FUEL INLET). AFTER NUMEROUS TIMES OF REPOSING LINE PER AMM GUIDELINES , MIN CLEARANCE OF 0.100 INCH COULD NOT BE ACHIEVED. 2L72 4F4 FRTA46NM E39NE 20020219001322002021900132EU 2002 2 19 CA020118007 120011207G2913974976 PUMP AIRBUS330 A330243 3930330EU RROYCERB211 RB211TRENT77 NE HYD SYSTEM FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) NR 2 ENGINE, YELLOW HYDRAULIC PUMP, SUCTION LINE CONNECTOR LOOSE AT MOUNTING PUMP. THE PUMP WAS REPLACED I.A.W. AMM 29-11-51 2L72 4F4 FRTA46NM E39NE 20020219001392002021900139NM 2002 2 19 CA020121008 120011115G5521657378436 SPAR BOEING737 737217 1384464NM PWA JT8 JT8D17 52049NE RT ELEVATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) RT ELEVATOR REAR SPAR AT TRIM TAB ATTACHMENT POINT FOUND CRACKED. ELEVATOR REMOVED FOR REPAIR, LOCATION OF DAMAGED LOCATED AT STATION 66.54 REPLACED ELEVATOR. DAMAGE REPAIRED AS PER SRM 2L72 4F4 F A16WE E2EA 20020220000022002022000002EU 2002 2 20 CA020121012 120011218G2910AE7111216 LINE AIRBUS330 A330243 3930330EU RROYCERB211 RB211TRENT77 NE HYD SYSTEM WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) - DURING CURRENT C03 /A06 HEAVY MAINTENANCE VISIT, ENGINE NR 2, A HYDRAULIC LINE, WAS FOUND TO BE RUBBING HARD AGAINST THE AIR OIL HEAT EXCHANGER, THE RUBBER PROTECTIVE COATING WAS GOUGED (BUT NOT THROUGH ), STILL WITHIN REPAIRABLE LIMITS. 2L72 4F4 FRTA46NM E39NE 20020220000052002022000005 2002 2 20 CA020122003 420011219G3197 WIRE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE INSTRUMENT PANELBINDING W O OTHER O OTHER DEDESCENT 1 CA (CAN) ON DESCENT INTO ST. JOHN'S, YYT, PILOT NOTICED THAT HE HAD NO AURAL WARNINGS FOR DECISION, H8, ALTITUDE, ALERT, OVERSPEED, GEAR WARNING OR STALL WARNING. MAINT INSPECTED PLUGS FOR AURAL AMPLIFIERS & NOTHING APPEAR TO BE WRONG. WIRING INSP & FOUND 2 WIRES HAD BEEN CHAFED BY LARGE PLASTIC TYWRAPS. ONE WIRE (CODE 24A22) FOR 28VDC INPUT OF AURAL ANNUNCIATOR AMPLIFIER, P/N 207 & AN OTHER WIRE AT PLUG W314P8 FOR CO-PILOTS SPEAKERS. WIRING REPLACED BY MEANS OF BUTTSPLICES. OPAL CHECKS WERE CARRIED OUT FOR APPLICABLE WARNINGS & CHECKED SERVICEABLE. WIRES IN QUESTION WERE TIE WRAPPED AT A POINT WHERE BUNDLE WAS BENDING. IF TIE WRAPS HAD TO BE 1CM ON EITHER SIDE OF BEND THIS WOULD NOT HAVE HAPPENED. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20020205001472002020500147 2002 2 5 CA020122004 420011115G3400ELT1104 ELT ARTEX BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE ELT FAILED W O OTHER O OTHER ININSP/MAINT 1 CA 57781 (CAN) ELT REMOTE SWITCH INDICATOR LIGHT ON IN THE HANGAR WITH NO SIGNAL BEING RECEIVED ON COMM FREQUENCY 121-5. ELT AND WIRING INSPECTED AT ZONE 312, WIRES W3150-12, W3150-13 AND W3150-15 FOUND CHAFED AND GROUNDING OUT. PLASTIC TYWRAP AND PLASTIC CLAMP CUTTING INTO WIRING. WIRING SPLICED AND SPIRAL WRAP INSTALLED AROUND WIRE BUNDLE AND PROTRUDING THROUGH CLAMP TO ENSURE FAULT WOULD NOT RE-OCCUR. ELT UNIT REPLACED AND OPERATIONAL CHECK CARRIED OUT. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20020220000132002022000013CE 2002 2 20 CA020124003 120011212G324230146 HOUSING BEECH 100 100BEECH 1152916CE PWA PT6 PT6A28 EA BRAKE ASSY DAMAGED W O OTHER KR FLUID LOSS PARTIAL RPM/PWR LOSS LDLANDING 1 CA 18687 (CAN) THE PILOT REPORTED WHEN STOPPING AT THE RAMP THE LT BRAKE PEDAL WENT TO THE FLOOR. UPON INSPECTION THE LT FWD CALIPER WAS FOUND DRAGING ON THE GROUND. IT WAS DISCOVERED AFTER THE MISSING PARTS WERE OBTAINED AFT THE TAXI-WAY, THAT THE BOLT HOLDING THE DOWL PIN INTO THE CALIPER HAD WORKED LOOSE, & THE DOWL PIN UNSCREWED OUT OF THE CALIPER DISENGAGING THE CALIPER FROM THE BACK PLATE. (HOWEVER THE BOLT WAS STILL CORRECTLY LOCKWIRED IN POSITION.) THE CALIPER THEN FELL DOWN HITTING THE GROUND AND DISINTEGRATING. INSPECTION OF THE BOLTS ASSEMBLED THERE IS NO INDICATION THAT THE DOWL PIN IS LOOSE OR NOT, MISLEADING THE INSPECTOR TO THINK ALL IS OK. 1L72 3T4 T A14CE E4EA 20020220000612002022000061EU 2002 2 20 CA020129004 120011114G2520NAS110436 BOLT ISRAEL1125 ASTRASPX 4500205EU SEAT BELT FAILED W O OTHER O OTHER DEDESCENT 1 CA (CAN) UPON DEPLANING OF A/C AT DESTINATION, PASSENGER NOTIFIED CAPTAIN THAT OUTBOARD PORTION (LATCH SIDE) OF HIS SEAT BELT HAD BECOME DETACHED FROM HIS SEAT WHEN HE ATTEMPTED TO SECURE IT FOR DESCENT INTO AIRPORT. HE HAD THEN MOVED TO ONE OF UNOCCUPIED SEATS IN PREPARATION FOR LDG. MAINT DISCOVERED THAT NUT & SPACER-BUSHING WERE MISSING FROM SEAT BACK PIVOT / SHACKLE RESTRAINT BOLT, WHICH HAD ALLOWED SEAT BELT SHACKLE TO COME DETACHED FROM SEAT (S/N 15065) 2L72 4F RTA16NM 20020220000652002022000065EA 2002 2 20 CA020130002 120011212G2710 CONTROL CABLE CNDAIRCL215 CL2156B11215 EA AILERONS WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AILERON CABLE WORN BEYOND LIMITS. 2H72 4T RTA14EA 20020220000692002022000069CE 2002 2 20 CA020130006 120011121G2433D2FF10B379AA RECTIFIER FORD POFF10300F CESSNA150 150M 2071830CE CONT O200 O200A 17020SO MCAULY1A102 1A102OCM GL ALTERNATOR WORN W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC APAPPROACH 1 CA A146794 (CAN) ALTERNATOR RECTIFIER FAILED CAUSING ELECTRICAL FAILURE DURING FLIGHT. 1H71 3O3 O 3A19 E252 5 NP918 20020321000922002032100092NM 2002 3 21 CA020131007 120011128G21404100S02801 ADAPTER DHAV DHC8 DHC8* NM PWC 150 PW150A EA ENGINE BURNED W O OTHER J WARNING INDICATION APAPPROACH 1 CA 75 (CAN) DURING THE FINAL APPROACH OF FLIGHT 5632 ON THE 28 NOVEMBER 2001, THE PILOT OF AIRCRAFT DHC8400 S/N 4027, REPORTED THAT THE ENGINE ADAPTER NR 1 CL CAME ON AND THE C/B POPPED. INVESTIGATION FOUND THE NR 1 HEATER INTAKE ADAPTER IN BURNED CONDITION. 2H72 4T4 TRTA13NM E00062EN 20020220000772002022000077NE 2002 2 20 CA020131008 220011209G7314324485317 FUEL CONTROL DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD14SF 14SF23 NE NR 2 ENGINE FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING YEJENGINE STOPPAGE VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 CA (CAN) ON TAKEOFF ROLL NR 2 ENGINE CAUTION LIGHT FLICKERED. WERE NO ABNORMAL IND.S. AFTER TAKEOFF AT 600 FT MSL NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED FOLLOWED BY COMPLETE FAILURE OF NR 2 ENGINE. ENGINE AUTO-FEATHERED, ALL ENGINE PARAMETERS INDICATED ZERO EXCEPT ITT WHICH AT 126. ENGINE FAILURE / FIRE SHUTDOWN DRILL CARRIED OUT. LDG COMPLETED SUCCESSFULLY. ALSO NOTED, THAT DURING TAXI PILOT NOTICED EEC LIGHT ILLUMINATED ACCOMPANIED BY MILT TQ SUR GE&THEN RETURNED TO NROMAL. MAINT FINDINGS: ENGINE EXTERNALLY INSP, PRE-COOLER DISCOVERED CRACKED BUT NOT ENOUGH TO BE CONTRIBUTING FACTOR AS BLEEDS HAD NOT BEEN SELECTED ON. ENGINE OIL FILTERS CHECKED - NO FAULTS FOUND. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20020321000952002032100095NM 2002 3 21 CA020131010 120011205G261310109601 SWITCH DHAV DHC8 DHC8* NM PWC 150 PW150A EA OVERHEAT SENSOR FAILED W EF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 CA (CAN) DURING APPROACH TO BASE AT 2,500 THE NR 1 ENGINE INDICATED A FIRE CONDITION. ONCE ENGINE SECURED, (PER IAC) T-HANDLE INDICATION EXTINGUISHED. CONTINUED WITH CHECK LIST (DID NOT FIRE BOTTLES), FIRE INDICATION REAPPEARED (T-HANDLE LIGHT & BELL). FIRED BOTH BOTTLES ACCOMPLISHED SAFE EMERGENCY LANDING WITHOUT INCIDENT. NO ENGINE INSTRUMENT OR OTHER VISUAL INDICATIONS WERE OBSERVED, BUT DUE TO WEATHER COULD NOT VISUALLY OBSERVE NR 1 ENGINE NACELLE. INVESTIGATION FOUND FAILED CLOSED FIRE/OVERHEAT SENSOR SWITCH, INTERNAL WARNING SWITCH CLOSED AS MEASURED ACROSS PINS A & D.1343.0 HOURS/1841 CYCLES. 2H72 4T4 TRTA13NM E00062EN 20020308000662002030800066SO 2002 3 8 CA020211013 120010709G8011636058 WORM GEAR CONT PIPER PA36 PA36285 7103610SO LYC O540 IO540K1G5 41532EA STARTER CLUTCH BROKEN W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) THE PILOT COULD NOT START THE ENGINE. NOTED THAT ALTHOUGH THE STARTER APPEARED TO SPIN, IT WAS NOT TURNING THE ENGINE. THE AME INVESTIGATED AND DETERMINED THAT THE PROBLEM WAS INTERNAL. THE ENGINE WAS DISMANTLED TO REVEAL THE STARTER WORM GEAR BROKEN IN 3 PLACES. PREVIOUSLY, THE ENGINE HAD BEEN KICKING BACK EXCESSIVELY ON STARTUP. IT WAS FOUND THAT THE MAGNETO SHOWER OF SPARKS WAS WIRED TO THE ADVANCE POINTS RATHER THAN THE RETARD AND THIS COULD HAVE WEAKENED THE WORM GEAR TO THE POINT OF SUBSEQUENT FAILURE. 1L71 3O3 O A10SO 1E4 20020311000042002031100004EA 2002 3 11 CA020219001 220011213G8520LW19340 CAMSHAFT PIPER PA31 PA31350 7103110SO LYC O540 TIO540* 41532EA HARTZLHCE3Y HCE3YR2A GL ENGINE WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) IN THE PROCESS OF PREFORMING A CYLINDER CHANGE, THE MECHANIC WAS UNABLE TO GET THE REQ'D VALVE CLEARANCE WITH THE APPLICABLE PUSHROD LENGHTS. UPON REMOVAL OF THE CYLINDER AND FURTHER INVESTIGATION, IT WAS DETERMINED THAT THE CAM LOBE WAS TOO WORN TO ALLOW THE LONGEST AVAILIABLE PUSHROD TO BRING THE VALVE CLEARANCE INTO LIMITS. THE ENGINE WAS SUBSEQUENTLY REMOVED FROM THE AIRCRAFT AND SENT TO A SERCICE FACILITY FOR REPAIR. 1L72 3O3 O A20SO E14EA 5 CP33EA 20020311000272002031100027SO 2002 3 11 CA020226006 120010608G793177808 SPRING PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA OIL PRESSURE ADJWEAK W K NONE O OTHER ININSP/MAINT 1 CA (CAN) OVERHAULED ENGINE INSTALLED, TEST RUN COMPLETED SATISFACTORY, ON TEST FLIGHT OIL PRESSURE DROPPED TO 65 P.S.I. AIRCRAFT LANDED AND OIL PRESSURE READJUSTED TO 75 P.S.I., BUT WAS AT MAX ADJUSTING LIMITS. REPLACEMENT ADJUSTMENT SPRING INSTALLED AND OIL SCREEN CHECKED AND METAL WAS EVIDENT AT THIS TIME, AFTER A PERIOD OF TIME THE ENGINE WAS REMOVED AND SENT BACK TO OVERHAUL FACILITY FOR REPAIR. NO CAUSE OF CONTAMINATION WAS FOUND. 1L72 3O3 O A20SO E14EA 20020311000282002031100028SO 2002 3 11 CA020226007 120011204G3700442CW6 PUMP PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA VACUUM SYS FAILED W E ENGINE SHUTDOWN K FLUID LOSS TXTAXI/GRND HDL 1 CA (CAN) VACUUM PUMP INSTALLED ON ENGINE, TEST SHOWED EXCESSIVE OIL LEAK AT MOUNT BASE. OIL PRESSURE ON ENGINE WENT TO "0" INDICATED AND ENGINE WAS SHUT DOWN. REPLACEMENT PUMP INSTALLED AND OIL SCREEN DETECTED METAL IN ENGINE. 1L72 3O3 O A20SO E14EA 20020325000152002032500015CE 2002 3 25 CA020227008 120010130G3241 CONNECTOR LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE73122B 01518WP ANTI-SKID SYSTEMDAMAGED W K NONE H ELECT. POWER LOSS-50 PC LDLANDING 1 CA (CAN) ON A BASE INSPECTION IT WAS NOTED THAT THE NR 1 AND NR 2 TIRES HAD FLAT SPOTS FROM SKIDDING. THERE WAS NO REPORTED ANTI-SKID FAILURE LIGHT ILLUMINATION. INVESTIGATION REVEALED THAT THE LT ANTI-SKID CONTROL VALVE WAS NOT RELEASING THE PRESSURE TO THE SKIDDING WHEEL. CONNECTOR PIN "G" ON THE CONTROL VALVE WAS FOUND TO HAVE CORRODED TO THE POINT THAT IT BROKEN OFF INSIDE THE CONNECTOR PLUG. THIS CIRCUIT CONTROLS THE RETURN SHUT-OFF SOLENOID IN THE VALVE. THE FAILURE LOGIC IN THE ANTI-SKID CONTROL BOX CHECKS THE OPERATION OF THE WHEEL TRANSDUCERS BUT DOES NOT INDICATE A FAILURE OF THE VALVE. THE CONTROL VALVE IS LOCATED IN THE WHEEL WELL WHERE IT IS SUBJECT TO WATER CONTAMINATION. 2L72 4F4 F A10CE E6WE 20020325000252002032500025EU 2002 3 25 CA020228011 120011212G5730 PANEL AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE RT WING SEPARATED W O OTHER D INFLIGHT SEPARATION TOTAKEOFF 1 CA (CAN) THIS IS BRIEF DESCRIPTION OF EVENTS LEADING UP TO INCID. OF PANEL 691AT, LOCATED ON RT UPPER WING, EXITING A/C MSN 183 AT TAKEOFF ON 8 DEC 2001.ON 11 NOV 01, PANEL REMOVED TO PERFORM INSP OF LOW SPEED AILERON HINGEBOLTS FOR CORROSION. INSPECTION COMPLETED & PANEL REINSTALLED SAME DAY. 2L72 4F4 FRTA35EU E23EA 20020513000102002051300010WP 2002 5 13 CA020322008 120011207G5540 STRUCTURE NAMER B25 B25J 6400710WP WRIGHTR2600 R260035 67050EA RT RUDDER CONTAMINATED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) RT RUDDER WAS FOUND TO HAVE APROXIMATELY TWO GALLONS OF WATER INSIDE DUE TO A PLUGGED DRAIN GROMMET. FURTHER INSPECTION FOUND DETERIORATED COTTON TAPES FROM AN OLD CECONITE FABRIC RE-COVERING JOB. RUDDER REMOVED AND RECOVERED 2M72 4R4 R AL2 PAGE42 20020411000222002041100022NM 2002 4 11 CA020402006 120010430G21317612608 CONTROLLER BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE CABIN PRESSURE FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) AIRCRAFT CABIN PRESSURIZATION FAILED ON CLIMB. AUTO FAIL WARNING LIGHT ILLUMINATED. CREW TRANSFERED TO STANDBY MODE BUT AIRCRAFT WOULD NOT PRESSURE. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT.MAINTENANCE CHANGED THE CABIN PRESSURE CONTROLLER IAW MM 21-31-21 AND THE SYSTEM FUNCTION CHECKED SERVICEABLE.AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPORT. 2L72 4F4 F A16WE E2EA 20020503000242002050300024EA 2002 5 3 CA020402008 120011213G3246GY22623 BOLT CNDAIRCL604 CL604 1900301EA WHEEL ASSY BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) IN THE PROCESS OF PERFORMING A D.I. THE ENGINEER FOUND A MISSING BOLT ON THE NR 4 MAIN WHEEL ASSY. UPON REMOVAL OF THE WHEEL THE HEAD OF THE BOLT AND HALF OF THE SHANK WHERE STILL IN THE INBOARD WHEEL HALF. THE THREADED END OF THE BOLT AND NUT WERE LATER FOUND BY THE HANGAR WALL. AS A RESULT THE WHEEL ASSY WAS REPLACED WITH A SERVICABLE UNIT AND REPAIRED AS PER M.M. 2L72 4F RTA21EA 20020503000272002050300027CE 2002 5 3 CA020405002 120011115G3213740017 STRUT CESSNA185 185C 2072808CE CONT O470 IO470F 17026SO MLG CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) AS A PRECAUTION DUE TO NOT KNOWING THE HISTORY. THE MAIN LANDING GEAR LEGS WERE SENT FOR MAGNAFLUXING. TWO LONGITUDINAL CRACKS OF ABOUT ONE AND ONE QUARTER INCH LONG WERE DETECTED ON THE LOWER THIRD OF THE LEFT HAND GEAR LEG. NOTE: PART CYCLES, PART TSN AND PART TSO TO BE DESREGARDED. 1H71 3O3 O 3A24 3E1 20020503000292002050300029GL 2002 5 3 CA020405008 220010413G7210 NUT BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL GEARBOX WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) TORQUEMETER GEARSHAFT NUT WORN. 1G71 3U3 U H2SW E4CE 20020503000302002050300030GL 2002 5 3 CA020405009 220010524G73141C2710FR PUMP BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL FUEL BOOST INOPERATIVE W K NONE L NO TEST ININSP/MAINT 1 CA (CAN) AFT BOOST PUMP NOT FUNCTIONAL. 1G71 3U3 U H2SW E4CE 20020503000332002050300033GL 2002 5 3 CA020405013 220011004G72402303910 CASE BELL 206 206L1 1182107SW ALLSN 250C 250C28 03013GL COMBUST CHAMBER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CRACKED ARMPIT ON COMBUSTION CASE. 1G71 3U3 U H2SW E1GL 20020503000342002050300034GL 2002 5 3 CA020405014 220011122G725023008593 NOZZLE BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL TURBINE SECTION BURNED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) HOT END INSPECTION REVEALED THE FIRST STAGE NOZZLE BURNT BEYOND ACCEPTABLE LIMITS. 1G71 3U3 U H2SW E1GL 20020503000352002050300035NM 2002 5 3 CA020405015 120010411G8011MZ4222 STARTER ROBSINR22 R22BETA 7640110NM LYC O320 O320B2C 41508EA ENGINE INOPERATIVE W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) STARTER NOT FUNCTIONAL. 1G71 3O3 O H10WE E274 20020503000362002050300036NM 2002 5 3 CA020405016 120010601G2841 TRANSMITTER ROBSINR22 R22BETA 7640110NM LYC O320 O320B2C 41508EA FUEL QTY IND INOPERATIVE W K NONE L NO TEST ININSP/MAINT 1 CA (CAN) FUEL GAUGE INOPERATIVE REPLACE TRANSMITTER. 1G71 3O3 O H10WE E274 20020503000372002050300037NM 2002 5 3 CA020405017 120010912G7921A30915 PLATE ROBSINR22 R22BETA 7640110NM LYC O320 O320B2C 41508EA OIL COOLER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) OIL COOLER MOUNTING PLATE CRACKED. 1G71 3O3 O H10WE E274 20020503000382002050300038SW 2002 5 3 CA020405018 120010706G282210274 PUMP BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL FUEL BOOST INOPERATIVE W K NONE L NO TEST ININSP/MAINT 1 CA (CAN) FORWARD BOOST PUMP INOPERATIVE. 1G71 3U3 U H2SW E4CE 20020503000392002050300039SW 2002 5 3 CA020405019 120010804G243523032018 STARTER GEN BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE INOPERATIVE W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) STARTER GENERATOR INOPERATIVE. 1G71 3U3 U H2SW E4CE 20020503000402002050300040SW 2002 5 3 CA020405020 120010425G6230204011430001 BEARING BELL 204011400127BELL 212 212 1181420SW PWA PT6T PT6T3B 52045NE SWASHPLATE WORN W K NONE O OTHER ININSP/MAINT 1 CA JI199175 (CAN) SWASHPLATE BEARING WORN BEYOND LIMITS. 1G71 4U4 U H4SW E22EA 20020503000412002050300041NE 2002 5 3 CA020405021 220010728G7310 FLEX LINE BELL 212 212 1181420SW PWA PT6T PT6T3B 52045NE FUEL SYSTEM LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) LEAK AT CROSSOVER FLEX LINE TO AUXILIARY TANK CONNECTION. 1G71 4U4 U H4SW E22EA 20020503000422002050300042SW 2002 5 3 CA020405022 120010503G6210206010152003 BOLT BELL 206010200133BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL M/R BLADE WORN W K NONE O OTHER ININSP/MAINT 1 CA A498 (CAN) EXCESSIVE WEAR ON THE MAIN ROTOR BLADE BOLT SHANK. 1G71 3U3 U H2SW E4CE 20020503000432002050300043GL 2002 5 3 CA020405023 220011119G72506878496 NOZZLE BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL TURBINE SECTION CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FIRST STAGE NOZZLE FOUND CRACKED BEYOND ACCEPTABLE LIMITS. 1G71 3U3 U H2SW E4CE 20020503000442002050300044SW 2002 5 3 CA020405024 120010708G2910206076031013 SERVO BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL HYD SYSTEM INOPERATIVE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) FEEDBACK IN THE FLIGHT CONTROLS. HYDRAULIC SERVO FAILED. 1G71 3U3 U H2SW E4CE 20020426000602002042600060SW 2002 4 26 CA020405025 120011114G5302206030446001F BULKHEAD BELL 206B BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL T/R GEARBOX BAY CRACKED W K NONE O OTHER ININSP/MAINT 1 CA BCJN07389 (CAN) CRACK FOUND DURING INSPECTION IN AFT LT TAIL ROTOR GEARBOX MOUNTING AREA. 1G71 3U3 U H2SW E4CE 20020503000452002050300045GL 2002 5 3 CA020405026 220011128G7323252466714 GOVERNOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE INOPERATIVE W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) GOVERNOR WILL NOT HOLD 100 PERCENT IN FLIGHT. 1G71 3U3 U H2SW E4CE 20020506000122002050600012 2002 5 6 CA020411006 420010816G6113055032110 BULKHEAD CESSNA 055032110 CESSNA172 172P 2072436CE LYC O320 O320D2J 41508EA MCAULY1C160 1C160DTM GL SPINNER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AFT SPINNER BULKHEAD CRACKED AT RADIUS OF PROP CUT OUT. 1H71 3O3 ONT3A12 E274 5 NP910 20020612001052002061200105NM 2002 6 12 CA020508014 120011027G243511521062 STARTER GEN DHAV DHC8 DHC8* NM PWC 150 PW150A EA ENGINE FAILED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) AT FL250 NR 2 STALL SYS & PUSHER SYS CAUTION LTS CAME ON. ACTION ACC QRH. WITHING NEXT 2 MINS SEVERAL OTHER CAUTION ITS CAME ON FOLLOWED BY NR 2 FMS/PFD/MFD MALFS&COMPLETE RT SIDE WITH OUT LIGHTING (COCKPIT & LDG/APPR LTS). ALSO STBY PRESSURE & HYD QTY NR 2 WERE INDICATING ZERO. DECISION TO DIVERT MADE. LDG UNEVENTFUL FOLLOWED BY NORMAL DISEMBARKATION. UPON COMPLETING "AFTER LDG CHECKLIST" RT SIDE LIGHTS CAME ON AGAIN & MOST CAUTION LTS & MESSAGES WENT OUT. AIRCRAFT GROUNDED FOR INSP. NR 2 DC STARTER GEN REPLACED. EPCU READOUT CARRIED OUT - NO FINDINGS, OPS TEST OF MAIN 28V DC GENERATION SYS&DC BUS CONTACTOR K21 CARRIED OUT - WITHOUT FINDINGS. GCU REPLACED. EPCU REPLACED. GCU RETURN ED NFF, EPCU RETURNED 2H72 4T4 TRTA13NM E00062EN 20020807002342002080700234EA 2002 8 7 CA020715006 120010621G5610601R330335 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) CAPTAIN`S WINDSHIELD SHATTERED WHILE IN CRUISE AT 35,000 FEET. PRESSURIZATION WAS NORMAL. FLIGHT DIVERTED TO TXK. 2L72 4F RTA21EA 20020918000472002091800047SO 2002 9 18 CA020905004 120010830G8120 BEARING GARRTT LW12463 PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA TURBOCHARGER STIFF W A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CA LBR0200 (CAN) MANIFOLD PRESSURE FLUCTUATING.TURBOCHARGER TURBINE WHEEL FOUND STIFF TO SPIN. 1L72 3O3 O A20SO E14EA 20021206000232002120600023CE 2002 12 6 CA021101007 120011030G7160109910029115 SKIN BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA AIR INLET CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ENGINE AIR INLET COWLING FOUND CRACKED ALONG STIFFENER RIVET LINE. 1L72 3T4 TRT3A20 E4EA 20021206000512002120600051EA 2002 12 6 CA021108007 220010731G741467542 BEARING PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA LT MAGNETO DESTROYED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) RT ENGINE, LT MAGNETO ENGINE HOURS: 745.2 DAMAGE WAS DISCOVERED DURING ROUTINE SCHEDULED MAGNETO REPLACEMENT. WHEN THE MAGNETO WAS REMOVED THE MAGNETO GEAR RETAINER ASSY AND BEARING PULLED OUT OF THE ENGINE TOGETHER WITH THE DRIVE COUPLING.UPON FURTHER INSPECTION IT WAS DISCOVERED THAT THE GEAR RETAINER ASSY BEARING WAS DESTROYED AND REQUIRED REPLACEMENT. THE BEARING RECESS WAS INSPECTED AND CHECKED O.K. THE BEARING WAS REPLACED WITH NEW AND ASSEMBLY WAS REINSTALLED. NO FURTHER ACTION. 1L72 3O3 O 1A10 1E4 20030718000922003071800092SO 2003 7 18 CA030709005 220010806G8520 BUSHING CESSNA180 180H 2072618CE CONT O470 O470R 17026SO MCAULY2A34C 2A34C203 GL COUNTERWEIGHT WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ENGINE REMOVED FROM VIBRATION. ENGINE COUNTERWEIGHT BUSHINGS WORN OUT. 1H71 3O3 O 5A6 E273 5 CP3EA 20031021000732003102100073EA 2003 10 21 CA030922001 120011016G5610NP1393225 WINDOW CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA (CAN) CAPT'S SIDE WINDOW SHATTERED AT 29000 FT. LANDED AT SCHEDULED DESTINATION. WINDOW REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20040126000982004012600098SW 2004 1 26 CA031117009 120010601G3243206031301025 SUPPORT BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 11430 (CAN) WHILE PERFORMING AN AW CHECK, CRACKS WERE SUSPECTED IN AFT CROSS TUBE SUPPORT AREA. AFTER PAINT STRIPPING CRACKS CONFIRMED AS FOLLOWS. A SMALL HAIRLINE CRACK WAS FOUND ON THE FWD LEG OF THE LT CROSS TUBE SUPPORT. CRACK IS JUST OUTBOARD OF 90 DEGREE ANGLE. CRACK STARTS AT BOTTOM OF SUPPORT & EXTENDS VERTICAL TO FIRST RIVET & THEN VEERS INBOARD & VERTICAL. CRACK IS APPROX. 1 INCH IN LENGTH. A SMALL HAIRLINE CRACK ALSO FOUND JUST BELOW FWD LEG OF THE RT CROSS TUBE SUPPORT. CRACK IS JUST BELOW THIS LEG & RUNS HORIZONTAL & IS ABOUT 1/2 INCH LONG. BELL HELICOPTER IS AWARE OF CRACKS IN THIS AREA & HAS MADE AN UPGRADE TO THESE PARTS. NEW PARTS ARE OF A MUCH THICKER MATERIAL TO PREVENT CRACKING. 1G71 3U3 U H2SW E4CE 20050418000782005041800078NE 2005 4 18 CA041018011 220010813G726101R311159601 TUBE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE GAS GENERATOR CRACKED W ED ENGINE SHUTDOWN RETURN TO BLOCK KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA 35615 120097 (CAN) DURING TAXI OUT TO RUNWAY CREW NOTICED AN ODOR WHICH ALSO SET OFF THE LAVATORY SMOKE DETECTOR. AIRCRAFT RETURNED TO GATE. TROUBLESHOOTING BY MAINTENANCE REVEALED SMOKE WAS ENTERING INTO CABIN WHEN BLEED AIR SELECTED ON, NR 1 ENGINE. ENGINE WAS REPLACED. ENGINEERING REPORT BY FROM ENGINE TEARDOWN INDICATED THAT THE OIL PRESSURE SUPPLY TUBE FOR THE NR 5 BEARING AREA WAS CRACKED AT A WELD SEAM IN THE GASGENERATOR CASE. ENGINE WAS REPAIRED. REPORT AVAILABLE IF REQUIRED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20050503001182005050300118SW 2005 5 3 CA050228010 120010324G6320BP252 GEARBOX KAMOV KA32 KA32A1 SW AMTR VK1A KLIMOVK1A GL MAIN ROTOR MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) GEARBOX CHIP LIGHT, GEARBOX REPLACED. 1G72 4U4 JNC EXPE4J 20050503001162005050300116SW 2005 5 3 CA050228011 120010714G6320BP252 GEARBOX KAMOV KA32 KA32A1 SW MAIN ROTOR MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) GEARBOX CHIP LIGHT, GEARBOX REPLACED. 1G72 4U NC 20010831001892001083100189 2001 8 31 CAXR106173 420010629G34255040122902 INDICATOR UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE INSTRUMENT PNL FAILED C CAXRO OTHER O OTHER NRNOT REPORTED 1 WP15408DC259 1151 ATTITUDE INDICATOR - INSTRUMENT FAILED, INOPERATIVE. RMA NR 031964 1G72 3U3 UNCR0001RD E34NE 20010306000902001030600090NM 2001 3 6 COOSDR000033 120010215G5320 TORQUE BOX BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE NLG WW FATIGUED B EE4YK NONE O OTHER ININSP/MAINT 1 EA258887Z 21856 COOPESA REPORTED THE NOSE WHEEL WELL TORQUE BOX LOWER CHORD LBL 19, WL 148 CHORD WITH CORROSION. REPLACED THE SUBJECT CHORD. PROBABLE CAUSE OF CORROSION WAS FATIGUE. 2L73 4F4 F A3WE E2EA 20010509002882001050900288SO 2001 5 9 CWA1 220010118G7260632617 GEAR CONT CESSNA337 337G 2075730CE CONT O360 IO360GB 17025SO ACCESSORY DRIVE WORN D K NONE L NO TEST ININSP/MAINT 1 GL1372361188 188 33701568 244627R DURING RUN-UP, FOLLOWING ANNUAL INSPECTION, NO VACUUM INDICATION OBSERVED FROM REAR ENGINE. REMOVED PUMP FOR REPLACEMENT AND OBSERVED DRIVE ON ENGINE DID NOT TURN WITH PROPELLER. REMOVED ACCESSORY DRIVE COVER AND FOUND NO TEETH LEFT ON DRIVING BEVEL GEAR. DRIVEN GEAR WAS NOT WORN. 1H72 3O3 O A6CE E1CE 20010307005952001030700595SW 2001 3 7 E27R1730 120010112G53103107041310704 CHANNEL GULSTM690TP 690A 0141722SW WING ROOT CRACKED B E27RK NONE O OTHER ININSP/MAINT 1 WP07921ST10645 11200 DURING PRESSURAZATION LEAK CHECKS, THE CABIN WAS FOUND TO HVE TWO LARGE LEAKS IN LT AND RT WING ROOT AREA. ON EXAM OF THE SUSPECT AREAS IT WAS FOUND THAT THE LT AND RT SUPPORT CHANNELS PN310704-1 AND 310704-2 HAD FAILED FROM FS 144 WL10 TO FS 175 WL 14. THE FAILURE IS IN THE FORM OF A CRACK ON THE VERTICAL OB PORTION OF THE CHANNELS FROM RIVET TO RIVET. THIS FAILURE ALLOWED THE AIRCRAFT SKIN TO PULL AWAY FROM ITS SUPPORTING STRUCTURE ABOVE THE PICTURE WINDOWS IN EXCESS OF .25 IN. 1H72 3T 2A4 20010326004302001032600430SW 2001 3 26 E27R730 120010122G53003107041 CHANNEL GULSTM690TP 690A 0141722SW GARRTTTPE331TPE331* 01514WP LT & RT FAILED B E27RK NONE O OTHER ININSP/MAINT 1 WP07921ST10545 11200 DURING PRESSURIZATION LEAK CHECKS, THE CABIN WAS FOUND TO HAVE TWO LARGE LEAKS IN THE LEFT AND RIGHT WING ROOT AREA. ON EXAMINATION OF THE SUSPECT AREAS IT WAS FOUND THAT THE LEFT AND RIGHT SUPPORT CHANNELS PN 3107041 & 3107042 HAD FAILED FROM FS 144 WL TO FS 175 WL 14, THE FAILURE ALLOWED THE AIRCRAFT SKIN TO PULL AWAY FROM ITS SUPPORTING STRUCTURE ABOVE THE PICTURE WINDOWS IN EXCESS OF .25. 1H72 3T3 T 2A4 E2WE 20010326004312001032600431WP 2001 3 26 E27R7302 220010122G72103103435 GEAR GULSTM690TP 690A 0141722SW GARRTTTPE331TPE33110 01514WP BULL GEAR FAILED B E27RO OTHER O OTHER CRCRUISE 1 WP0748AZ 6991 1612 11307 P79291C BULL GEAR FOUND TO HAVE SHED APPROX 6 IN OF TEETH IN 2 SEGMENTS CAUSING EXTENSIVE DAMAGE TO GEAR BOX COMPONENTS AND CASE. WHICH RESULTED IN AN IN FLIGHT SHUTDOWN. 1H72 3T4 T 2A4 E4WE 20010507003512001050700351SO 2001 5 7 ER00101 120010502G27105540802 CONTROL CABLE PIPER PA31T PA31T1 7103126SO PWA PT6 PT6A11 52043NE FUSELAGE CROSSED W K NONE O OTHER ININSP/MAINT 1 SW992480X2655 200 8104026 DURING SCHEDULED INSPECTION, THE RIGHT HAND AILERON INTERCONNECT CABLE WAS FOUND TO BE CROSSED OVER THE PRIMARY RUDDER CONTROL CABLE (PT NO 46845-0)AT THE UNDERFLOOR SECTION AFT OF THE CABIN DOOR. THERE IS NO WEAR APPARENT AT THIS TIME, THE AIRCRAFT LOG BOOKS ARE BEING INSPECTED IN AN ATTEMPT TO ASCERTAIN WHEN THE SYSTEM WAS LAST DISTURBED. 1L72 3T3 T A8EA E4EA 20010726000652001072600065EU 2001 7 26 ERAA072935 120010420G63104638302093 SHAFT BOLKMS105 BO105S 5626006EU FREEWHEEL LEAKING H ERAAK NONE O OTHER ININSP/MAINT 1 FS01426EH 552 SHAFT HAS 36.9 HRS TSO AND IS CAUSING INPUT SEAL TO LEAK EVEN WITH THE NEW IMPROVED SEAL INSTALLED. 1G72 3U H3EU 20010726000662001072600066NE 2001 7 26 ERAA072936 120010424G800060692032 BLOWER SKRSKYS76 S76A 8143006NE ENGINE INOPERATIVE H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01577EH 760222 PART IS INOPERABLE. MOTOR WON'T START WITH BLOWER ON. HAVE TO TAP ON PLUG CONNECTOR BOX TO START. INSTALLING NEW BLOWER SOLVED PROBLEM. TSO IS ONLY 47.1 HRS. RETURNING TO CORPORATE ROTABLE ON REPAIR ORDER # RW-883735 REQUESTING WARRANTY REPAIR. 1G72 3U H1NE 20010726000672001072600067NE 2001 7 26 ERAA072937 120010501G71200292108940 SUPPORT SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1 60030NE ENGINE BROKEN H ERAAK NONE O OTHER ININSP/MAINT 1 FS01578EH2147 760099 3016 FRONT SUPPORT IS BROKEN IN HALF. PART HAS 2147.0 HRS ON IT. THIS INFORMATION FOR FAA SDR REPLACED WITH NEW SUPPORT. 1G72 3U3 U H1NE E19EU 20010726000682001072600068EU 2001 7 26 ERAA072938 120010501G63204638001007 TRANSMISSION BOLKMS105 BO105A EU M/R GEARBOX MAKING METAL A ERAAK NONE O OTHER ININSP/MAINT 1 AL03290EH12460 S850 TRANSMISSION MAKING METAL. REMOVED SLIP RING CARRIER, FOUND LT BEVEL GEAR BREAKING DOWN. FOUND OIL PUMP DAMAGED FROM METAL CONTAMINATION. PUMP SENT OUT FOR REPAIR. THIS INFORMATION FOR FAA SDR. ACTION TAKEN: REPAIRED TRANSMISSION I/A/W REM 103, INST'D NEW L/H INPUT PINION & BEVEL GEAR, SERVICEABLE OIL PUMP. COMPLIED WITH FREEWHEEL INSPECTION I/A/W REM 103. NEXT INSPECTION DUE IN 600 HRS. ASSEMBLED TRANSMISSION AND ADJUSTED PATTERN AND BACKLASH. 1G72 3U H3EU 20010726000692001072600069EU 2001 7 26 ERAA073270 120010516G2435230321825 STATOR BOLKMS105 BO105S 5626006EU GENERATOR CHAFED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01153EH S572 ARMATURE RUBBING INSIDE STATOR. ISSUED TO AC 153EH BUT COULD NOT BE INSTALLED DUE TO PROBLEM WHEN TRYING TO INSTALL IN GENERATOR. 1G72 3U H3EU 20010726000762001072600076SW 2001 7 26 ERAA073271 120010521G2822 SCREW BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE VALVE STRIPPED H K NONE O OTHER ININSP/MAINT 1 FS01419EH1881 33043 SCREW IS STRIPPED. SCREWS STRIPPED OR BACKING OUT OF VALVE BODY. NOTE: SCREWS WERE LOCK WIRED. T 1G72 4U4 U H4SW E22EA 20010726000772001072600077EU 2001 7 26 ERAA073274 120010531G324610550103 SKID BOLKMS105 BO105S 5626006EU MLG MISOVERHAULED H ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 FS01125EH S562 SKID TUBE ISSUED TO AC 125EH BUT COULD NOT BE INSTALLED. SKID TUBE WAS OVERHAULED AND RETURNED WITH NUT PLATES NOT LINING UP WITH SKID SHOES. 1G72 3U H3EU 20010726000792001072600079EU 2001 7 26 ERAA073275 120010601G324610550103 SKID BOLKMS105 BO105A EU MLG MISOVERHAULED H ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 FS01148EH 703 SKID TUBE ISSUED TO AC 148EH BUT COULD NOT BE INSTALLED. SKID TUBE WAS OVERHAULED AND RETURNED WITH NUT PLATES NOT LINING UP WITH SKID SHOES. 1G72 3U H3EU 20010802003002001080200300SW 2001 8 2 ERAA074613 120010612G24332010001 CONVERTER BELL 412 412 1182202SW ELECTRICAL MALFUNCTIONED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01412EH16 33001 NEW CONVERTER REC'D FROM ANCHORAGE ORDERED FROM BENZ AIRBORNE. UNIT WILL NOT ADJUST LOW ENOUGH. ONLY HAS 15.5 HRS SINCE NEW. RETURNING TO BENZ ON ERA REPAIR ORDER RW-884522 REQUESTING WARRANTY REPAIR. 1G72 4U H4SW 20010802003012001080200301 2001 8 2 ERAA074614 420010612G3444066303102 ALTIMETER SKRSKYS76 S76A 8143006NE RADAR FAILED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01576EH 760212 RADAR ALTIMETER WAS OVERHAULED BY FREESCAN 2 / 2001 AND RET'D TO ERA . INSTALLED ON AIRCRAFT AND HAD TO REMOVE DUE TO BEING TOTALLY INOPERABLE. RETURNING TO FREESCAN ON ERA REPAIR ORDER RW-884523 REQUESTING WARRANTY REPAIR. 1G72 3U H1NE 20010802003062001080200306SW 2001 8 2 ERAA074615 120010612G7714412075010109 INDICATOR BELL 412 412 1182202SW TRIPLE TACH READS HIGH H ERAAK NONE O OTHER ININSP/MAINT 1 FS01418EH TRIPLE TACH REM'D FROM AIRCRAFT AFTER 111.3 HRS AFTER O/H WITH ROTOR NEEDLE READING 5 PERCENT HIGH. 1G72 4U H4SW 20010802003092001080200309EU 2001 8 2 ERAA074616 120010613G63204638001007 TRANSMISSION BOLKMS105 BO105A EU MAIN ROTOR CONTAMINATED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01290EH12460 S850 TRANSMISSION IS CONTAMINATED BY TRASH FROM OIL COOLER. REMOVED ALL OIL JETS TO FLUSH OUT ALL OIL PASSAGES. REMOVED TOP CASE & CENTER HOUSING, CLEANED AND FLUSHED ALL OIL JETS AND OIL PASSAGES, REPAIRED ACCEDSSORY DRIVE, REASSEMBLED TRANSMISSION WITH NEW O-RINGS IAW REM 103. 1G72 3U H3EU 20010802003122001080200312EU 2001 8 2 ERAA074617 120010613G642010531714 HEAD BOLKMS105 BO105S 5626006EU TAIL ROTOR BINDING H ERAAK NONE O OTHER ININSP/MAINT 1 FS01131EH11983 559 T/R ASSY IS BINDING. REPAIRED, PARTIAL DISASSEMBLY, VISUALLY INSPECTED. FOUND NO CAUSE FOR BINDING, INST'D NEW GRIP BUSHINGS AND SEALS. CHECKED FRICTION FORCES 10N AND 17N (MAX 25N) REASSEMBLED T/R ASSY AND MARVEL BALANCED ALL WORK IAW BO105 MM 32, MARVEL MANUAL REM 301. 1G72 3U H3EU 20010802003152001080200315EU 2001 8 2 ERAA074618 120010613G642010531714 HEAD BOLKMS105 BO105S 5626006EU TAIL ROTOR BINDING H ERAAK NONE O OTHER ININSP/MAINT 1 FS01131EH13133 559 THIS INFORMATION FOR FAA SDR. CC: AMERICAN EUROCOPTER CORP. T/R ASSY IS BINDING. ACTION TAKEN: FOUND INNER SLEEVE AND BLADE MOUNTING, FORK BEARING BUSHINGS COATED WITH TEFLON FILM REPAIRED FOR BINDING. DISASSEMBLED, CLEANED, VISUALLY INSPECTED, REASSEMBLED WITH NEW SEALS AND BALANCED. ALL WORK DONE IAW MBB-BO105 REM 301, MM CHAP 34 & 107 & MARVEL BOOK.. 1G72 3U H3EU 20010802003192001080200319GL 2001 8 2 ERAA074619 220010613G73136890040 NOZZLE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL FUEL INJECTION MISREPAIRED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01296EH S849 1ST STAGE NOZZLE SHIELD RET'D FROM OVERHAUL AT DALLAS AIRMOTVE, ISSUED TO AIRCRAFT BUT COULD NOT BE INSTALLED DUE TO NOT BEING WELDED ALL THE WAY AROUND. 1G72 3U3 U H3EU E4CE 20010802003262001080200326 2001 8 2 ERAA074620 420010614G23124120073010 CONTROL HEAD BELL 412 412 1182202SW COCKPIT MISREPAIRED H ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 FS01167EH 33089 CONTROL HEAD MODIFIED INCORRECTLY. WAS MODIFIED TO S INSTEAD OF A. 1G72 4U H4SW 20010803000132001080300013EU 2001 8 3 ERAA074621 120010615G642010531714 HEAD BOLKMS105 BO105S 5626006EU TAIL ROTOR BINDING H ERAAK NONE O OTHER ININSP/MAINT 1 FS01131EH3137 559 T/R ASSY IS BINDING. FOUND NO ABNORMAL WEAR OR DEFECTS. DISASSEMBLED, CLEANED AND INSPECTED BUSHINGS ON INNER SLEEVE. REMOVED AND REPLACED BUSHINGS AND SEAKS IN BLADE MOUNTING FORKS. REASSEMBLED AND BALANCED. ALL WORK DONE IAW MBB BO105 REM 301, MBB-BO105 MM CHAPTERS 34& 107 AND MARVEL BOOK. 1G72 3U H3EU 20010803000722001080300072EU 2001 8 3 ERAA074622 120010615G642010531714 HEAD BOLKMS105 BO105S 5626006EU TAIL ROTOR STIFF H ERAAK NONE O OTHER ININSP/MAINT 1 FS01128EH12475 572 THIS INFORMATION FOR FAA SDR. CC: AMERICAN EUROCOPTER CORP. T/R ASSY HAS STIFF PEDALS. FOUND NO ABNORMAL WEAR OR DEFECTS ACTION TAKEN: DISASSEMBLED, CLEANED AND INSPECTED BUSHINGS ON INNER SLEEVE, REPLACED SEALS AND BUSHIGS IN BLADE MOUNTING FORKS REASSEMBLED AND BALANCED. ALL WORK DONE IAW MBB BO105 REM301, MBB BO105MM CHAPTERS 34 & 107 AND MARVEL BOOK. 1G72 3U H3EU 20010803000732001080300073EU 2001 8 3 ERAA074623 120010615G642010531714 HEAD BOLKMS105 BO105S 5626006EU TAIL ROTOR STIFF H ERAAK NONE O OTHER ININSP/MAINT 1 FS01 13133 THIS INFORMATION FOR FAA SDR. CC: AMERICAN EUROCOPTER CORP. STIFF T/R PEDALS AT 100% FOUND NO CAUSE FOR BINDING. ACTION TAKEN: DISASSEMBLED, CLEANED & VISUALLY INSPECTED. REASSEMBLED USING NEW BUSHINGS & SEALS. C/W FRICTION CHECK (TESTED 3N & 44) & MARVEL BALANCED. ALL WORK IAW BO105 REM 301 & MM CH 33 & 34 & MARVEL BOOK. 1G72 3U H3EU 20010803000752001080300075EU 2001 8 3 ERAA074624 120010618G642010531714 HEAD BOLKMS105 BO105S 5626006EU TAIL ROTOR STIFF H ERAAK NONE O OTHER ININSP/MAINT 1 FS01127EH12841 571 T/R ASSY HAS HEAVY LEFT PEDAL. ACTION TAKEN: REPAIRED, DISASSEMBLED, CLEANED, VISUALLY INSPECTED. INSTALLED NEW GRIP BUSHINGS AND SEALS. INST'D SERVICEABLE CONTROL LEVERS. REASSEMBLED AND BALANCED ALL WORK IAW BO105 REM 301 MM 33,34. 1G72 3U H3EU 20010803000772001080300077SW 2001 8 3 ERAA074626 120010619G6520212040004009 GEARBOX BELL 412 412 1182202SW TAIL ROTOR MAKING METAL H ERAAK NONE O OTHER ININSP/MAINT 1 FS01417EH13445 33031 GEARBOX IS MAKING METAL. BEARINGS BREAKING DOWN. ACTION TAKEN: OVERHAULED, DISASSEMBLED, CLEANED, VISUALLY INSPECTED AND NDT. C/W TB 412-99-157. INSTALLED NEW BEARINGS OP SHAFT, EXCLUDER ASSY AND ALL SEALING ELEMENTS. REASSEMBLED 90 DEGREE GEARBOX AND CHECKED BACKLASH. .009, .009, .009 REPACKED COUPLING WITH GREASE DATED GREASE DATED NOV. 12, 1999. 1G72 4U H4SW 20010803000782001080300078GL 2001 8 3 ERAA074627 220010619G7230250C20B COMPRESSOR BOLKMS105 BO105S 5626006EU ALLSN 250B 250B* GL ENGINE SEIZED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01296EH12458 S849 COMPRESSOR LOCKED UP. PLASTIC ON CASE 1/2 MISSING. ACTION TAKEN: INSTALLED SERVICEABLE CASE. 1G72 3U3 T H3EU E10CE 20010803000792001080300079EA 2001 8 3 ERAA074628 220010621G7230 COMPRESSOR BELL 412 412 1182202SW PWA PT6T PT6T3 52045EA ENGINE FAILED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01421EH13292 33067 AFTER 451.2 HRS T.S.O. C-BOX REMOVED FROM AIRCRAFT DUE TO HIGH OIL PRESSURE. 1G72 4U4 U H4SW E22EA 20010921001552001092100155NE 2001 9 21 ERAA074826 120010718G6730BH185R154 SERVO SKRSKYS61 S61N 8142104NE FLUCTUATES H ERAAK NONE O OTHER ININSP/MAINT 1 FS01563EH 61808 INSTALLED ON A/C AND HAD TO REMOVE DUE TO GAUGE FLUCTUATING. RETURNING ON ERA REPAIR ORDER # RW -885179 REQUESTING WARRANTY REPAIR. 2G72 4U 1H15 20010921001572001092100157EU 2001 9 21 ERAA074827 120010718G63104638302093 SHAFT BOLKMS105 BO105A EU FREEWHEEL UNIT LEAKING H ERAAK NONE O OTHER ININSP/MAINT 1 FS01291EH S842 FREEWHEEL SHAFT IS CAUSING INPUT SEAL TO LEAK. NEEDS SPECIAL COATING REPLACED. WAS PURCHASED NEW 2/14/00. RETURNING ON ERA REPAIR ORDER 885185 REQUESTING WARRANTY EXCHANGE. 1G72 3U H3EU 20010921001612001092100161EU 2001 9 21 ERAA074828 120010720G65204619002003 GEARBOX BOLKMS105 BO105S 5626006EU TAIL ROTOR DAMAGED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01134EH2837 635 BEARINGS SCORED AND INPUT BUSHING FRETTING. DISASSEMBLED, VISUALLY INSPECTED. REPLACED ALL FIVE BEARINGS, INPUT BUSHING, ALL O RINGS, ALL SEALING RINGS, BOTH SEALS, ONE SCREW AND THE LOCKING PLATE. REASSEMBLED, SET GEAR DISTANCE, BACKLASH & PATTERN PRO-SEALED. REPAIRED IAW BO-105 REM-304. COMPLIED WITH ASB BO-105-30-111. COPY SENT TO AMERICAN EUROCOPTER CORP. 1G72 3U H3EU 20010921001622001092100162EU 2001 9 21 ERAA074829 120010723G641010531980 BLADE BOLKMS105 BO105S 5626006EU TAIL ROTOR FLAKING H ERAAK NONE O OTHER ININSP/MAINT 1 FS01152EH2306 S701 SEVERE PAINT AND RUBBER FLAKEING. SENT TO AEC FOR REPAIR AND INSTALLED ON AIRCRAFT 1-22-01. RETURNING ON ERA REPAIR ORDER# RW-885245 REQUESTING WARRANTY REPAIR. 1G72 3U H3EU 20010921001632001092100163EU 2001 9 21 ERAA074830 120010730G3212307561 SQUIB VALVE BOLKMS105 BO105S 5626006EU MLG CORRODED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01133EH881 598 SQUIB VALVE CORRODED. VALVE BODY IS BULGING (OR PERTRUDING) AS INDICATED ON VALVE. CORRECTIVE ACTION: SQUIB VALVE REMOVED FROM AIRCRAFT AND TAGGED AS UNSERVICEABLE. 1G72 3U H3EU 20010921001652001092100165GL 2001 9 21 ERAA074831 220010801G7320252464430N FUEL CONTROL BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MISOVERHAULED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01293EH6921 S844 FUEL CONTROL OVERHAULED BY HONEYWELL 2/23/01. UNIT IS SLOW STARTING AND HANGS AT 55 PERCENT. RETURNING ON ERA REPAIR ORDER RW-885436 REQUESTING WARRANTY REPAIR. 1G72 3U3 U H3EU E4CE 20010921001672001092100167SW 2001 9 21 ERAA074832 120010802G5260LA11A2129 ACTUATOR BELL 412 412 1182202SW STEP FAILED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01SPARE STEP ACTUATOR WAS REPAIRED BY ITT AND RET'D TO ERA 5/30/2001. COULD NOT BE USED ON AIRCRAFT BECAUSE UNIT WOULD NOT RETRACT. RETURNING ON ERA REPAIR ORDER RW-885450 REQUESTING WARRANTY REPAIR. 1G72 4U H4SW 20010921001682001092100168SW 2001 9 21 ERAA075871 120010802G5260LA11A2129 ACTUATOR BELL 412 412 1182202SW STEP FAILED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03SPARE STEP ACTUATOR WAS REPAIRED BY ITT AND RET'D TO ERA 5/30/2001. COULD NOT BE USED ON AIRCRAFT BECAUSE UNIT WOULD NOT RETRACT. RETURNING ON ERA REPAIR ORDER# RW-885450 REQUESTING WARRANTY REPAIR. 1G72 4U H4SW 20010924000932001092400093EU 2001 9 24 ERAA075875 120010809G63104638302093 SHAFT BOLKMS105 BO105S 5626006EU FREEWHEEL UNIT LEAKING H ERAAK NONE K FLUID LOSS ININSP/MAINT 1 FS01294EH615 S675 FREEWHEEL SHAFT LEAKS. WAS SENT TO ZF FOR OVERHAUL 1/26/01 AND WAS INSTALLED ON AIRCRAFT 8/04/01. AFTER 18.2 HRS, UNIT CAUSING INPUT SEAL TO LEAK. SPECIAL COATING WORN. RETURNING TO ZF ON ERA REPAIR ORDER RW-885574 REQUESTING WARRANTY REPAIR. 1G72 3U H3EU 20010924000952001092400095EU 2001 9 24 ERAA075876 120010822G63104638302093 SHAFT BOLKMS105 BO105S 5626006EU FREEWHEEL UNIT LEAKING H ERAAK NONE K FLUID LOSS ININSP/MAINT 1 FS01294EH457 S846 FREEWHEEL SHAFT PREVIOUSLY SENT TO ZF 4/2001 FOR REPAIR FOR SAME PROBLEM, CAUSING LEAKING OF INPUT SEALS. REF MMIR ERAA 0001202. RETURNING ON ERA REPAIR ORDER RW-885812 REQUESTING WARRANTY REPAIR. ALSO RETURNING (2) INPUT SEALS THAT ARE LEAKING WITH THE SAME AMOUNT OF HOURS AS FREEWHEEL SHAFT. ATTN: HERBERT BODENMILLER 1G72 3U H3EU 20011226000012001122600001SW 2001 12 26 ERAA076643 120010921G75003032247 AIR FILTER BELL 412 412 1182202SW ENGINE DEBONDED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01412EH106 33001 PART IS DEBONDED. THIS PARTICULAR AIR FILTER HAD 106.0 HRS BUT HAVE TRIED SEVERAL OTHERS AND IMMEDIATELY AIR FILTERS BEGAN TO BREAK DOWN AND DEBOND. 1G72 4U H4SW 20011226000022001122600002EU 2001 12 26 ERAA076644 120010921G63104638302093 SHAFT BOLKMS105 BO105S 5626006EU FREEWHEEL UNIT LEAKING H ERAAK NONE O OTHER ININSP/MAINT 1 FS01426EH245 552 FREEWHEEL SHAFT CAUSES INPUT SEAL TO LEAK. SPECIAL COATING NEEDS TO BE REPLACED. ONLY HAS 245.1 HRS SINCE LAST RETURNED TO ZF. LAST RETURNED ON WARRANTY CLAIM. 1G72 3U H3EU 20011226000032001122600003SW 2001 12 26 ERAA076647 120010927G75003032247 AIR FILTER BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE DEBONDED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01422EH 33068 CPPS62136 PART IS DEBONDED. FILTER PURCHASED FROM PUR FLOW MFG. IMMEDIATELY COME APART AFTER INSTALLATION. 1G72 4U4 U H4SW E22EA 20011226000042001122600004SW 2001 12 26 ERAA076648 120010927G75003032247 AIR FILTER BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE DEBONDED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01164EH 33004 PART IS DEBONDED. THIS INFORMATION FOR FAA SDR ONLY. PURCHASED FROM PUR FLOW MFG. 1G72 4U4 U H4SW E22EA 20011226000052001122600005SW 2001 12 26 ERAA076649 120010928G75003032247 AIR FILTER BELL 412 412 1182202SW NR 1 & 2 ENGINESDEBONDED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01412EH 33001 PART IS DEBONDED. INSTALLED ON NR 1 AND NR 2 ENGINE BUT BOTH FILTERS DEBONDED AND FELL APART IMMEDIATIATELY. 1G72 4U H4SW 20011226000062001122600006SW 2001 12 26 ERAA076650 120010928G75003032247 AIR FILTER BELL 412 412 1182202SW NR 2 ENGINE DEBONDED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01412EH 33001 PART IS DEBONDED. INSTALLED ON NR 2 ENGINE BUT FILTER FELL APART. THIS INFO FOR FAA SDR. FILTERS PURCHASED FROM PUR-FLOW MFG. 1G72 4U H4SW 20011226000072001122600007NE 2001 12 26 ERAA076652 120011003G304040008330202 INDICATOR SKRSKYS61 S61N 8142104NE RADAR UNIT CONTAMINATED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01561EH135 61471 RADAR INDICATOR HAS WATER DAMAGE. UNIT HAD BLANK SCREEN AND WOULD NOT COME ON.MAJOR WATER DAMAGE WS FOUND IN UNIT. ACTION TAKEN: REMOVED CORROSION, REPAIRED TRACES, ALIGNED AND TESTED. THIS INFORMATION FOR FAA SDR. 2G72 4U 1H15 20011226000082001122600008 2001 12 26 ERAA076653 420011003G344040008330208 INDICATOR SKRSKYS61 S61N 8142104NE RADAR UNIT CONTAMINATED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01561EH1073 61471 RADAR INDICATOR HAS WATER DAMAGE. UNIT WOULD NOT COME ON. FOUND WATER DAMAGE. ACTION TAKEN : REMOVED CORROSION, REPLACED BLOWN RESISTOR AND TESTED UNIT. 2G72 4U 1H15 20011226000092001122600009 2001 12 26 ERAA076654 420011003G344040008330208 INDICATOR SKRSKYS61 S61N 8142104NE RADAR CONTAMINATED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01561EH831 61471 RADAR INDICATOR HAS WATER DAMAGE. INOPERABLE. UNIT HAS WATER DAMAGE ACTION TAKEN: REPLACED BLOWN RESISTOR, REMOVED CORROSION AND TESTED. 2G72 4U 1H15 20011226000242001122600024GL 2001 12 26 ERAA076655 220011003G7320252466715H GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01292EH13707 562 GOVERNOR OCCASIONALLY DROOPS IN FLIGHT. TEST RESULTS CONFIRM SNAG OF DROOP. UNIT WAS DOOPING BY 250 RPM @ T.P. 3.01 ECCENTRIC SHAFT FOUND CORRODED AND WORN BEYOND LIMITS ON LOBES. BEARINGS PN 2520503 AND 2523237 FOUND TO BE ROUGH AND DRY. ACTION TAKEN: ABOVE PARTS REPLACED WITH NEW AND UNIT WAS REPAIRED AND TESTED SERVICEABLE IAW HONEYWELL OH FORM 15-1095A. THIS INFORMATION FOR FAA SDR. 1G72 3U3 U H3EU E4CE 20011226000252001122600025GL 2001 12 26 ERAA076656 220011003G7320252466715H GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01153EH11164 S572 NR 1 GOVERNOR IS SLOW,NR HIGH WITH REDUCED POWER. TEST RESULTS INDICATE GOVERNOR WAS DROOPING OFF SLIGHTLY (100 RPM) SEVERAL INTERNAL BEARINGS PN 2520503 & 2523237 FOUND DRY AND ROUGH. THROTTLE BUSHING WORN ALLOWING SHAFT TO HAVE EXCESSIVE PLAY. ECCENTRIC SHAFT CORRODED AND WORN BEYOND LIMITS. ACTION TAKEN: REPAIRED AND TESTED SERVICEABLE IAW HONEYWELL OHM 15--1095A. ABOVE PARTS REPLACED. CEB A-1353 R1 FOUND N/AB, UNIT S/N, CEB A-1361R1 FOUND C/W. 1G72 3U3 U H3EU E4CE 20011226000262001122600026GL 2001 12 26 ERAA076657 220011003G73202524667 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL WORN H ERAAO OTHER O OTHER NRNOT REPORTED 1 FS01149EH8461 S705 SPLINES ON DRIVESHAFT OF GOVERNOR IS WORN. MAX GOVERING DROOPS OFF 300 RPM TO EARLY. THROTTLE BUSHING VERY SLOPPY WORN SPLINES ON DRIVESHAFT AS WELL AS THE MATING FACE OF THE SPOOL BEARING EXHIBITED HEAVY WEAR FROM THE GOVERNOR WEIGHT FEET. ECCENTRIC SHAFT AND CAM LEVER WERE FOUND SEIZED TOGETHER N THE DRIVE BODY BY CORROSION. AFTER CLEANING THEY WERE BOTH PITTED AND WORN BEYOND LIMITS ACTION TAKEN: OVERHAULED. NOTE: THE CONDITION OF THIS GOVERNOR SEEMS TO INDICATE A VIBRATION PROBLEM ON THE A/C, POTENTIALLY STARTER GENERATOR ON GEARBOX. CEB'S 1347 R1, A-1361R1 AND GT320. C/W CEB A-1353R1 FOUND N/A BY UNIT S/N. THIS INFORMATION FOR FAA SDR 1G72 3U3 U H3EU E4CE 20011226000272001122600027EU 2001 12 26 ERAA076658 120011004G62101051410110 BOLT BOLKMS105 BO105S 5626006EU MAIN ROTOR WORN H ERAAK NONE O OTHER ININSP/MAINT 1 FS01149EH S705 PRIMARY BLADE BOLTS HAS WORN PLATING. ACTION TAKEN : CLEANED & C/W VISUAL & NDT INSPECTION. SCRAPPED 3 BOLTS DUE TO MECHANICAL DAMAGE. THIS INFORMATION FOR FAA SDR. 1G72 3U H3EU 20011226000282001122600028EU 2001 12 26 ERAA076663 120011005G621010515170 BLADE BOLKMS105 BO105A EU MAIN ROTOR DEBONDED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01135EH11317 S675 M/R BLADE IS DEBONDED. LEADING EDGE DEBONDING, POTTING NEEDS CHANGING. ACTION TAKEN: ALL ABRASION STRIPS VOID, HEAVY ERROSION ON ABRASION STRIP, P.U. FILM DETERIORATION, PAINT PEELING, HARDWARE CORRODED SWEEP OUT -13.21MM, NOSE AND NECK SHELLS CRACKED SKIN CRACKED @ NECK SHELL, SKIN DEBONDED @ NECK AREA. REPAIRED. THIS INFORMATION FOR FAA SDR. 1G72 3U H3EU 20011226000292001122600029EU 2001 12 26 ERAA076664 120011009G621010515170 BLADE BOLKMS105 BO105A EU MAIN ROTOR DEBONDED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01135EH11319 S675 BLADE IS DEBONDING ON LEADING EDGE. POTTING NEEDS CHANGING NOSE AND NECK SHELLS CRACKED @ NECK DOWN AREA, SKIN CRACK AND VOIDED @ NECK AREA, TEFLON MISSING FROM MAIN BUSHING, DRAG BUSHING HAS FRAYED AND MISSING TEFLON, DAMPNER WRAP VOID LOWER SURFACE, ALL ABRASION STRIPS VOID @ SCARF JOINTS, HEAVY ERROSION ON OUTBOARD ABRASION STRIP, MINOR CORROSION ON THE TABS. DU DISKS MISSING, MINOR CORROSION ON PENDULUM ARM, SWEEP OUT 10.34MM ACTION TAKEN: REPLACED NR 1 OUTBOARD ABRASION STRIP, REPLACED PT REINSTALLED NR 2,3,4 ABRASION STRIPS, REPLACED DU DISKS REPLACE MAIN BUSHING, REPLACED DRAG BUSHING, REM'D AND TREAT CORROSION OR TRIM TABS, PERFORM SMALL SKIN REPAIR @ NECK, REPLACED NOSE AND NECK SHELLS, REPLACED DAM1G72 3U H3EU 20011226000312001122600031EU 2001 12 26 ERAA076665 120011009G621010515170 BLADE BOLKMS105 BO105A EU MAIN ROTOR DEBONDED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01135EH11428 S675 BLADE IS DEBONDING ON LEADING EDGE. POTTING NEEDS CHANGING. ALL ABRASI9ON STRIPS VOID SCARF JOINT, NR 1 ABRASION STRIP ERROSION NOSE AND NECK SHELL CRACKED AT FITTING, SKIN AT ROOT AREA CRACKED ROVING FILLER SEPERATED, UPPER SURFACE AT TRAILING EDGE, DAMPNER VOID, MINOR ERROSION ON TRIM TABS, TEFLON LINING ON BUSHING FRAYED AND MISSING SWEEP OUT OF TOLERANCE 9.6MM. ACTION TAKEN: REPAIRED AS PER FORM 8130-3 BLOCK, 13 . THIS INFORMATION FOR FAA SDR. 1G72 3U H3EU 20011227000042001122700004 2001 12 27 ERAA076667 420011009G3450D120P2T INDICATOR BELL 412 412 1182202SW COCKPIT CORRODED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01412EH483 33001 PART IS CORRODED. CONNECTOR CORRODED, PIN MISSING, DIRTY INSIDE AND ALSO OUT OF CALIBRATION. ACTION TAKEN: OVERHAULED, REPAIRED LEAKS, TREATED METAL, CALIBRATED AND FUNCTIONALLY TESTED OK TO 20,000 FEET. COMPLIED WITH AIRWORTHINESS DIRECTIVES AS PER MFG PUB 7421 REV A JAN. 1993. 1G72 4U H4SW 20011227000052001122700005 2001 12 27 ERAA076668 420011009G3450D120P2T INDICATOR SKRSKYS61 S61N 8142104NE COCKPIT MISMANUFACTURED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01561EH360 61471 PART MISSING. FILTER MISSING ON PORT; TAKEN FROM STOCK. CONNECTOR PLATE BROKEN, CORROSION ON INSIDE OF BASE AND CASE, UNIT LEAKS, AND NEEDS ADJUSTMENT. ACTION TAKEN: REPAIRED, CLEANED CORROSION, REPLACED CONNECTOR PLATE, FIXED LEAKS, ADJUSTED AND FUNCTRIONALLY TESTED OK TO 20,000 FEET. C/W AIRWORTHINESS DIRECTIVES OR SB'S AS PER TSM 7421 REV A JAN 1993. 2G72 4U 1H15 20011227000062001122700006 2001 12 27 ERAA076669 420011009G3450D120P2T INDICATOR BOLKMS105 BO105A EU COCKPIT CORRODED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01291EH S842 PART IS CORRODED. CONNECTOR INSERTS PULLED OUT . CONNECTOR PLATE BROKEN, CORROSION ON CASE INSIDE AND ON BASE, UNIT LEAKS AND OUT OF ADJUSTMENT. ACTION TAKEN: REPAIRED, CLEANED CORROSION, REPLACED CONNECTOR PLATE, FIXED LEAKS, AND FUNCTIONALLY TESTED OK TO 20,000 FEET. C/W AIRWORTHINESS DIRECTIVES OR SB'S AS PER TSM 7421 REV A JAN 1993. 1G72 3U H3EU 20011227000072001122700007SW 2001 12 27 ERAA076670 120011009G5302 STRUCTURE BELL 412 412 1182202SW TAILBOOM CRACKED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01415EH6871 ADW06067 33009 NO. 2 BULKHEAD CRACKED ABOVE ROOF PANEL. STINGER BULKHEAD UPPER SUPPORT ANGLE CRACKED. STIFFNER P/N 212-030-099-028 CRACKED. ROOF PANEL PN 205-032-815-127 HAS CORROSION & SEPERATED. VERTICAL FIN SUPPORT BULKHEADS PN 212-030-127-029 AND 021 CRACKED. L/H LOWER VERTICAL FIN SKIN CRACKED FWD BULKHEAD PN 212-030-143-009 SEPERATED. ACTION TAKEN: REPLACED STIFFNER PN 212-030-99-028. REPLACED ROOF PANEL & REPLACED FWD BULKHEAD PANEL. REPLACED BOTH VERTICAL FIN SUPPORT BULKHEADS. FABRICATED L/H LOWER VERTICAL FIN SKIN. REPAIRED NO 2 BULKHEAD ABOVE ROOF PANEL. FABRICATED STINGER BULKHEAD SUPPORT ANGLE. C/W AIRWORTHINESS DIRECTIVES OR SB'S AS PER ASB 412-90-49 PART II. THIS INFORMATION FOR FAA SDR. 1G72 4U H4SW 20011227000082001122700008EU 2001 12 27 ERAA076671 120011009G5302 STRUCTURE BOLKMS105 BO105S 5626006EU TAIL BOOM CRACKED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01127EH 571 TAILBOOM IS CRACKED. RT SKIN CRACKED PN 105-30251-56, LT CONTOUR SKIN PN 105-30101-14 CRACKED, SPAR PN 105-30401-16-001 CRACKED, 90 DEGREE GEARBOX FITTING PN 105-30402-12 HAS CORROSION, STRINGER PN 105-30251-25 IS CRACKED, STRINGER PN 105-30251-26 IS CRACKED, FRAME SHEET PN 105-30401-29 IS CRACKED, SPAR PN 105-30412-03 HAS CORROSION. ACTION TAKEN: FAB R/H SKIN AND FAB NEW CONTOUR SKIN, REPLACEC TWO STRINGERS AND CHANGED THE FITTING PN 105-30402-12, REPLACED SPAR PN 105-30401-16-001 AND SPAR PN 105-30412-003 WITH NEW SPECS. REPLACED FRAME SHEET PN 105-30401-29 WITH NEW. 1G72 3U H3EU 20011227000092001122700009GL 2001 12 27 ERAA076672 220011009G7200250C20B ENGINE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL GEARBOX MAKING METAL H ERAAK NONE O OTHER ININSP/MAINT 1 FS01426EH13405 552 ENGINE IS MAKING METAL. G.B. SN CAG-36092 PTO GEAR PITTED. ACTION TAKEN: INSTALLED SERVICEABLE GEAR BOX. 1G72 3U3 U H3EU E4CE 20011227000102001122700010GL 2001 12 27 ERAA076673 220011009G72006898735 ENGINE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NACELLE MALFUNCTIONED H ERAAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 FS01426EH11039 552 TURBINE RUNS HOT, LOW POWER. STRETCHED NR 1 BLADES. ACTION TAKEN: INSTALLED NEW NR 1 & 2 WHEEL & NR 2 NOZZLE. 1G72 3U3 U H3EU E4CE 20011227000112001122700011GL 2001 12 27 ERAA076674 220011009G7200 ENGINE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NACELLE MAKING METAL H ERAAK NONE O OTHER ININSP/MAINT 1 FS01298EH5449 S845 ENGINE IS MAKING METAL. HAS METAL ON MAG PLUGS. 2 1/2 BEARING INNER RFACE HAS METAL. GROOVES ON SEVERAL ROLLERS. ACTION TAKEN: DISASSEMBL3D ENGINE CAE-836436, TURBINE, COMPRESSOR, GEARBOX. CHANGED 11/2 BEARING SN MR55741, INSTALLED MP75985, GEARSHAFT SN 69437 INSTALLED CI21-543. C/W AIRWORTGHINESS DIRECTIVES OR SB'S AS PER CEB-1298. SEAL ON GEARBOX ASSY - PRESSURE OIL FITTINGS. 1G72 3U3 U H3EU E4CE 20011227000122001122700012SW 2001 12 27 ERAA076675 120011009G3213212321103 CROSSTUBE BELL 412 412 1182202SW MLG CORRODED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01 FORWARD CROSSTUBE HAS CORROSION. ACTION TAKEN: CROSSTUBE IS SCRAPPED. 1G72 4U H4SW 20011227000132001122700013SW 2001 12 27 ERAA076676 120011011G6220412010145103 DAMPER BELL 412 412 1182202SW MAIN ROTOR SEPARATED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01168EH4949 33067 SEPERATED, UNABLE TO BALANCE MAIN ROTOR. ACTION TAKEN: RETIRED & SCRAPPED BOTH DAMPER SETS IAW 412 CR&O. 1G72 4U H4SW 20011227000142001122700014SW 2001 12 27 ERAA076677 120011011G6220412010145103 DAMPER BELL 412 412 1182202SW MAIN ROTOR SEPARATED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01168EH225 33067 SEPERATED, UNABLE TO BALANCE MAIN ROTOR. ACTION TAKEN: RETIRED & SCRAPPED BOTN DAMPER SETS IAW 412 CR&O. THIS INFORMATION FOR FAA SDR. 1G72 4U H4SW 20011227000152001122700015SW 2001 12 27 ERAA076678 120011011G6220412010145103 DAMPER BELL 412 412 1182202SW MAIN ROTOR CRACKED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01419EH5488 33043 DAMPER SET IS CRACKED. FOUND SETS WORN & CRACKED ACTION TAKEN: RETIRED & SCRAPPED IAW 412 CR&O, THIS INFORMATION FOR FAA SDR. 1G72 4U H4SW 20011227000162001122700016SW 2001 12 27 ERAA076679 120011011G6220412010145103 DAMPER BELL 412 412 1182202SW MAIN ROTOR CRACKED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01419EH6519 33043 DAMPER SET IS WEAK/ WORN / CRACKED. ACTION TAKEN: DAMPER SET WAS RETIRED & SCRAPPED IAW 412 CR&O. THIS INFORMATION FOR FAA SDR. 1G72 4U H4SW 20011227000172001122700017SW 2001 12 27 ERAA076680 120011011G6410212011701003FM BLADE BELL 412 412 1182202SW TAIL ROTOR DAMAGED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01422EH4048 33068 TAIL ROTOR BLADE A-11090 HAS VOID AT TIP, TRUNNION IS ROUGH. TAIL ROTOR BLADE SENT TO CTI FOR REPAIR. TRUNNION, TRUNNION HOUSING ASSYS SCRAPPED. ACTION TAKEN: INST'D NEW TRUNNION, TRUNNION HOUSINGS, BEARINGS, & SEALS, INSTALLED SERVICEABLE TAIL ROTOR BLADE. ASSEMBLED, BALANCED & LUBED T/R ASSY IAW 412 CR& O & T.B. 412-95-134. C/W AIRWORTHINESS DIRECTIVES OR SB'S AS PER TB 412-95-134. THIS INFORMATION FOR FAA SDR. 1G72 4U H4SW 20011227000182001122700018SW 2001 12 27 ERAA076681 120011011G6320412040002103 TRANSMISSION BELL 412 412 1182202SW MAIN ROTOR CORRODED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01164EH8992 33004 TRANSMISSION DUE 3100 HOUR INSPECTION. LOWER SPIDER BREAKING, UPPER SUN GEAR BREAKING, MAIN INPUT LINER, MAIN CASE HAS EXCESSIVE CORROSION DAMAGE, MAIN INPUT QUILL ALIGNMENT MARKS BEARING PINION OFF, RING GEAR OUTER SURFACE RUSTING, MAIN INPUT BEARING SLEEVE RUSTED. ACTION TAKEN: SENT TO ERA REPAIR STATION ALASKA FOR INSPECTION. THIS INFORMATION FOR FAA SDR. 1G72 4U H4SW 20011227000202001122700020EU 2001 12 27 ERAA076682 120011012G5302 STRUCTURE BOLKMS105 BO105A EU TAILBOOM CRACKED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01290EH5756 S850 TAILBOOM REMOVED FROM AIRCRAFT DUE TO CRACKED SKIN RT SIDE BASE OF VERTICAL FIN. FOUND RUSTED, CORRODED & PITTED TAIL SKID BRACKETS. CORRODED FWD MOUNTING FLANGES. CORROSION & PITTED SPOTS ON 90 DEGREE GEARBOX FITTING BOLT HOLES. ACTION TAKEN: INSTALLED NEW TAILSKID BRACKETS, FWD & AFT, INSTALLED NEW 90 DEGREE GEARBOX FITTING AND REPLACED FWD MOUNT FLANGE. FABRICATED & INSTALLED NEW R/H FWD SKIN, PLUS VALVE MOUNT BRACKETS & DOUBLER AND CLEARED ALL OTHER MAINTENANCE DESCREPANCIES IN BLUE WORK FORMS OF WORK ORDER C298015. THIS INFORMATION IS FOR FAA SDR. 1G72 3U H3EU 20020123000492002012300049SW 2002 1 23 ERAA076683 120011012G3212412050045107 CROSSTUBE BELL 412 412 1182202SW MLG CORRODED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03412EH 33001 AFT CROSSTUBE IS CORRODED. ACTION TAKEN: PART WAS SCRAPPED. 1G72 4U H4SW 20020123000502002012300050SW 2002 1 23 ERAA076684 120011012G5520205030856113 SKIN BELL 412 412 1182202SW RT ELEVATOR CRACKED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01167EH 33089 RT ELEVATOR SKIN CRACKED. FOUND SPAR TO BE UNBONDED AT FLANGE & ROOT RIB TO BE CORRODED BEYOND LIMITS. ACTION TAKEN: RE-MANUFACTURER OUTER SKIN, REPLACED SPAR & ROOT RIBS & REASSEMBLED. C/W AIRWORTHINESS DIRECTIVES OR SB'S AS PER TB-412-83-31. THIS INFORMATION IS FOR FAA SDR. 1G72 4U H4SW 20020123000522002012300052GL 2002 1 23 ERAA077281 120011022G6410332A12005001 BLADE AMTR PURE PUREAIR GL TAIL ROTOR DAMAGED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01170EH286 2016 TAIL ROTOR BLADE HAS AN INTERNAL NOISE AND SUSPECT THAT THERE MAY BE SOMETHING LOOSE INSIDE. 1H71 3O EXPA1H71 20020123000552002012300055EU 2002 1 23 ERAA077284 120011029G6410 PAINT BOLKMS105 BO105S 5626006EU T/R BLADE CRACKED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01293EH1540 587588 559 TAIL ROTOR BLADE PAINT IS CRACKED AND VOIDED ON END CAP. 1G72 3U H3EU 20020123000582002012300058NE 2002 1 23 ERAA077285 120011031G5320 BUSHING SKRSKYS61 S61N 8142104NE BATTERY ABSORBERWORN H ERAAK NONE O OTHER ININSP/MAINT 1 FS01563EH 61808 BUSHINGS WORN. 2G72 4U 1H15 20020123000622002012300062EU 2002 1 23 ERAA077292 120011115G65204619311033 BEARING BOLKMS105 BO105S 5626006EU T/R XMSN FAILED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01133EH 598 BEARING ROLLER FALLS OUT OF CAGE. 1G72 3U H3EU 20020123000742002012300074NE 2002 1 23 ERAA077293 220011115G7311 STRUCTURE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE COOLER BLOWER CORRODED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01417EH8358 5100712 33031 VANE GUIDE ASSY HAS PITTING & CORROSION. COATING ASSY HAS MECHANICAL DAMAGE ON OUTER LIP. SLIGHT CORROSION ON LOCK PLATE. SPACER FAILED DUE TO MECHANICAL DAMAGE. IMPELLAR HAS CRACKED BLADES. ACTION TAKEN: DISASSEMBLED & STRIPPED PAINT. COMPLIED WITH VISUAL & NDT INSPECTIONS. REMOVED & TREATED SLIGHT CORROSION. HAD VARIOUS PARTS PAINTED. REASSEMBLED & OVERHAULED USING NEW COATING ASSY., IMPELLAR, GUIDE VANE ASSY, NEW BEARINGS, PACKING, GASKET, AND HARDWARE AND NEW DECAL IAW 412 CR&O CHAPTER 79 & BHT-ALL-SPM. 1G72 4U4 U H4SW E22EA 20020123000752002012300075GL 2002 1 23 ERAA077294 220011116G7200250C20B ENGINE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENG BAY MAKING METAL H ERAAK NONE O OTHER ININSP/MAINT 1 FS01294EH6308 S675 ENGINE IS MAKING METAL, BOTH PLUGS. FC-OP GEARSHAFT DAMAGED PN 6896437 ACTION TAKEN: INSTALLED NEW GEARSHAFT & COMPLIED WITH CEB-A-1386 TQ METER GEAR INSPECTION . 1G72 3U3 U H3EU E4CE 20020123000762002012300076EU 2002 1 23 ERAA077295 120011116G2435 GEARSHAFT BOLKMS105 BO105S 5626006EU STARTER GEN WORN H ERAAK NONE O OTHER ININSP/MAINT 1 FS01124EH4928 S559 ENGINE IS MAKING METAL. . STARTER GENERATOR GEARSHAFT IS WORN. ACTION TAKEN: INSTALLED NEW GEARSHAFT AND BEARINGS. COMPLIED WITH CEB A-1374 PRESSURE PROBE INSPECTION. 1G72 3U H3EU 20020123000792002012300079SW 2002 1 23 ERAA077296 120011116G6320412040002103 BEARING BELL 412 412 1182202SW TAIL ROTOR MAKING METAL H ERAAK NONE O OTHER ININSP/MAINT 1 FS01418EH7849 TRANSMISSION IS MAKING METAL. TAILROTOR QUILL BEARINGS CAUSE OF METAL CONTAMINATION. SEAL LEAKS. MAIN INPUT R/B QUILL, SYS II HYD QUILL AND AUX JETS ON RING GEAR CASE. ACTION TAKEN: REPAIRED, PARTIALLY DISASSEMBLED, VISUALLY INSPECTED EXPOSED COMP. INSTALLED NEW BEARINGS T/R QUILL AND PACKED WITH GEAR, INSTALLED NEW SEALS, AND GASKET, O RINGS TO REPAIR LEAKS. ALL WORK IAW BHT 412 CR&O. 1G72 4U H4SW 20020123000842002012300084SW 2002 1 23 ERAA077297 120011116G6210 SKIN BELL 412 412 1182202SW M/R BLADE DAMAGED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01168EH8848 33067 REMOVED FOR FLIGHT CHARACTERISTICS BLADE HAS CREASES UPPER AND LOWER, PAINT WORK NEEDED. L/S HAS SKIN DAMAGE WITH VOID AT STA 192-194, T/B AND CTR TRIM TABS HAVE SKIN DAMAGE WITH VOIDS, WATER FOUND IN CORE DURING BOND PREP FOR PATCHES, UPPER SURFACE SKIN DAMAGE AT STA 226- 258 ESTENE DETERIORATED, REFLEX DOUBLER DEBONDED. 1G72 4U H4SW 20020123000862002012300086EU 2002 1 23 ERAA077298 120011116G6410 BLADE BOLKMS105 BO105S 5626006EU TAIL ROTOR DAMAGED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01293EH11985 559 END CAP OF ONE BLADE HAS A SPLIT IN THE PAINT. PITCH MOVEMENT FEELS ROUGH. BLADES DAMAGED, BUSHINGS (TEFLON) DIRTY, SEALS WARPED. ACTION TAKEN: REM'D BLADES AND SENT OUT FOR REPAIR. DISASSEMBLED TO FACILLITATE TEFLON BEARING CLEANING . CLEANED BEARING SURFACES AND REASSEMBLED HUB WITH NEW SEALS & NUTS. INSTALLED SERVICEABLE BLADES AND STATIC BALANCED TAILROTOR ASSY. REPAIRED IAW BO105 REM M/M CHAPTER 34 & 33 AND MARVEL BOOK. 1G72 3U H3EU 20020123000902002012300090GL 2002 1 23 ERAA077515 220011204G7230 PLUG BOLKMS105 BO105A EU ALLSN 250C 250C20B 03013GL COMPRESSOR DISLODGED H ERAAK NONE O OTHER ININSP/MAINT 1 FS01423EH6244 543 ENGINE IS MAKING METAL. RESI-WELD FE 186 SEALANT PLUG DISLODGED FROM COMPRESSOR MOUNT. SEALANT PLUG LODGED IN OIL PUMP SCAVENGE PORT. THIS DID NOT LET THE OIL SCAVENGE, THUS LETTING THE BEARINGS STARVE FOR OIL CAUSING IT TO MAKE METAL. ACTION TAKEN: DISASSEMBLED ENGINE. GEARBOX AND TURBINE WILL NEED OVERHAUL AND COMPLETE INSPECTION OF COMPRESSOR. GEARBOX SN CAG-37622 TT 12330.8 TSO 4694.6 (LAST O/H 3-5-91) 1G72 3U3 U H3EU E4CE 20010502000632001050200063NM 2001 5 2 ERKR200100067 120010326G5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP0712FQ 49766 REPAIRED SKIN PANEL, STATION 560, STRINGER 24R-25R RIGHT. 2L72 4F RTA6WE 20010502000642001050200064NM 2001 5 2 ERKR20010068 120010326G55125922577506 SKIN DOUG MD88 MD88 3023688NM HORIZONTAL STAB CORRODED B ERKRK NONE O OTHER ININSP/MAINT 1 WP0712FQ 49766 RIGHT HORIZONTAL STABILIZER, BARREL NUT HOLES XHS 27.234. THIS DOCUMENT PROVIDES REPAIR INSTRUCTIONS FOR CORROSION FOUND IN THE THREE BARREL NUT HOLE BORES OF THE RIGHT HORIZONTAL STABILIZER LOWER FORWARD AND LOWER CENTER SKIN PANELS. PART NUMBERS 5922576504 AND 5922577506.PER ECRA N12FQ55MD88002EAC. 2L72 4F RTA6WE 20011211000302001121100030SO 2001 12 11 ERY2001F00000 220011115G8520 CRANKCASE BEECH 58 58 1152740CE CONT O550 IO550C SO ENGINE CRACKED F K NONE K FLUID LOSS ININSP/MAINT 1 CE07384P 399 TH1888 684243 ENGINE OIL LEAK, FOUND 3 INCH LONG CRACK IN CRANKCASE ABOVE NR 3 CYLINDER, CRACK SEEMS TO ORIGINATE FROM UPPER CASE LEFT AND EXTEND DOWNWARD. 1L72 3O3 O 3A16 E3SO 20010803000812001080300081CE 2001 8 3 ERYR682D2001 120010511G324250300010121 LINER BEECH 90 E90 1152914CE LT MLG BRAKE BROKEN B ED ENGINE SHUTDOWN RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SO1122TL LW334 OVERHAULED BRAKE ASSEMBLY WAS INSTALLED AND FUNCTIONALLY TESTED BY MAINTENANCE PERSONNEL WITH NO NOTED DEFECTS. DURING TAKEOFF ROLL PILOT NOTICED AIRCRAFT SEEM TO PULL TO ONE SIDE, PILOT ABORTED TAKEOFF AND RETURNED TO CHOCKS. MAINTENANCE PERSONNEL VISUALLY EXAMINED BRAKES AND FOUND NO OBVIOUS DEFECTS. MAINTENANCE AND OPERATOR DECIDED TO PERFORM HIGH SPEED TAXI TO FURTHER TROUBLESHOOT BRAKING SYSTEM. DURING TAXI CHECK LT BRAKE FAILED AND BECAME COMPLETELY INEFFECTIVE. OPERATOR SHUT DOWN ENGINES AND AIRCRAFT WAS TOWED BACK TO MAINTENANCE FOR EVALUATION. MAINTENANCE EVALUATION DISCOVERED APPROXIMATE THREE INCH SECTION OF BRAKE LINING ASSEMBLY HAD BROKEN LOOSE AND ALLOWED LINING TO ROTATE OUT OF KEYWAY SLOTS. 1L72 3T 3A20 20010829002612001082900261SO 2001 8 29 GAC081601 120010816G24321159SCAV5201 CHARGER GULSTMG1159 GIV 3980115SO TAIL FAILED B H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO11426QS359 1426 DURING NORMAL MAINTENANCE WHILE ON THE GROUND THE BATTERY CHARGER BEGAN TO SMOKE AND THE CIRCUIT BREAKER POPPED. REMOVED AND REPLACED BATTERY CHARGER WITH REPAIRED UNIT. 2L72 4F RTA12EA 20010803000832001080300083SW 2001 8 3 GDMA073295 120010612G7910H33C32 BEARING 204062540001BELL 205 205A1 1181414SW ENGINE ROUGH H GDMAK NONE O OTHER ININSP/MAINT 1 FS0197HJ 398 1771292 30173 MEDIUM FREQ VIBRATION IN THE AIRFRAME. REPLACED BEARINGS IN THE FAN 1G71 4U H1SW 20010424003072001042400307CE 2001 4 24 GLBA2001085 120010419G2720 CONTROL UNIT BEECH 1900 1900D 1154162CE RUDDER MALFUNCTIONED A GLBAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CE01257GL UE257 UNCOMMANDED RUDDERR BOOST IN FLIGHT, PENDING CORRECTIVE ACTION 2L72 4T RTA24CE 20010515001322001051500132CE 2001 5 15 GLBA2001094 120010506G5270 HANDLE BEECH 1900 1900D 1154162CE PAX DOOR MALFUNCTIONED A GLBAD RETURN TO BLOCK N FALSE WARNING CLCLIMB 1 CE01257GL UE257 CABIN DOOR ANNUNCIATOR ILLUMINATED ON CLIMB-OUT, INSPECTED RESET CABIN DOOR HANDLE OPS CHECKED GOOD 2L72 4T RTA24CE 20010717000502001071700050CE 2001 7 17 GLBA2001104 120010521G213013037432 CONTROLLER BEECH 1900 1900D 1154162CE ONLY INOPERATIVE A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 CE01257GL138 UE257 CABIN PRESSURIZATION NOT HOLDING, REPLACED CONTROLLER 2L72 4T RTA24CE 20010803000842001080300084CE 2001 8 3 GLBA2001105 120010522G284012281301 METER BEECH 1900 1900D 1154162CE FUEL FLOW FAILED A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE01257GL423 UE257 LEFT AND RIGHT FUEL FLOW GAUGES FLUCTUATED WHEN POWER ADVANCED, REPLACED FLOW METER 2L72 4T RTA24CE 20010803000852001080300085 2001 8 3 GLBA2001111 420010527G34436227337001 RADAR EMB 120 EMB120 3260201SO WX RADAR INOPERATIVE A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 CE0192GL 6786 15 120092 WEATHER RADAR FAILED, INSPECTED FOUND RT UNIT BAD REPLACED OPS CHECKED SYSTEM SATISFACTORY 2L72 4T RTA31SO 20010417001002001041700100NE 2001 4 17 H1IR069Y01 220010305G72303029051 VANE CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE COMPRESSOR CRACKED B H1IRK NONE O OTHER ININSP/MAINT 1 NE0128AN 2221 208B0751 PCEPC0677 COMPRESSOR TURBINE VANE RING OUTER RING ANTI ROTATION LUGS ARE CRACKED OR SEPARATED BEYOND THE MAXIMUM REPAIRABLE LIMIT OF SEVEN. 11 LUGS SEPARATED AND 1 EA CRACKED FROM A TOTAL OF 14. EXPERIENCE INDICATES NORMAL AS REMOVED VANE RINGS WITH THIS TOTAL TIME SHOULD HAVE NO DEFECTS IN THIS AREA. 1H71 3T3 T A37CE E4EA 20010417001012001041700101EA 2001 4 17 H1IR069Y02 220010305G72303032151 VANE PWA PT6 PT6A34 52043EA COMPRESSOR CRACKED B H1IRK NONE O OTHER ININSP/MAINT 1 NE01 9D149 COMPRESSOR TURBINE VANE RING OUTER RING ANTI ROTATION LUGS ARE CRACKED OR SEPARATED BEYOND THE MAXIMUM REPAIRABLE LIMIT OF SEVEN. 9 OF 14 LUGS FOUND SEPARATED. 4 T E4EA 20010910003132001091000313EU 2001 9 10 HCMA075341 120010117G6420350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TAIL ROTOR WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13997BH837 2666 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010910003182001091000318EU 2001 9 10 HCMA075358 120010124G6410355A12004008 BLADE SNIAS 350 AS350B2 8680813EU TAIL ROTOR PEELING E HCMAK NONE O OTHER ININSP/MAINT 1 WP13992BH35 2889 WHITE PAINT IS PEELING OFF BLADE AND IS EXTREMELY HARD TO BALANCE. PLEASE REPAIR UNDER FULL WARRANTY. 1G71 3U H9EU 20010910003212001091000321EU 2001 9 10 HCMA075365 120010522G6420350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TAIL ROTOR WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13992BH805 2889 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010910003232001091000323EU 2001 9 10 HCMA075367 120010706G6420350A33214501 ROD SNIAS 350 AS350BA 8680817EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13642BH606 2495 PART IS WORN BEYOND LIMITS. 1G71 3U NCH9EU 20010910003242001091000324EU 2001 9 10 HCMA075368 120010706G6420350A33214501 ROD SNIAS 350 AS350BA 8680817EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13862BH159 2713 PART IS WORN BEYOND LIMITS. 1G71 3U NCH9EU 20010910003252001091000325EU 2001 9 10 HCMA075369 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU TAIL ROTOR WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13982BH934 2876 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010910003272001091000327EU 2001 9 10 HCMA075370 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13992BH474 2889 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010910003282001091000328EU 2001 9 10 HCMA075371 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13992BH184 2889 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010910003292001091000329EU 2001 9 10 HCMA075372 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13992BH599 2889 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010910003312001091000331EU 2001 9 10 HCMA075373 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13193BH643 2894 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010911000012001091100001EU 2001 9 11 HCMA075374 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13194BH499 2903 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010911000022001091100002EU 2001 9 11 HCMA075375 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13194BH258 2903 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010911000032001091100003EU 2001 9 11 HCMA075376 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13194BH170 2903 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010911000042001091100004EU 2001 9 11 HCMA075377 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13995BH245 2987 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010911000052001091100005EU 2001 9 11 HCMA075378 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13196BH932 3036 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010911000062001091100006EU 2001 9 11 HCMA075379 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13197BH751 2666 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010911000072001091100007EU 2001 9 11 HCMA075380 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13198BH900 3126 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010911000082001091100008EU 2001 9 11 HCMA075381 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13198BH89 3126 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010911000092001091100009EU 2001 9 11 HCMA075382 120010706G6420350A33214501 ROD SNIAS 350 AS350B2 8680813EU PITCH CONTROL WORN E HCMAK NONE O OTHER ININSP/MAINT 1 WP13198BH546 3126 PART IS WORN BEYOND LIMITS. 1G71 3U H9EU 20010911000102001091100010EU 2001 9 11 HCMA075388 120010814G6410355A12004008 BLADE SNIAS 350 AS350B2 8680813EU TAIL ROTOR CRACKED E HCMAK NONE O OTHER ININSP/MAINT 1 WP13992BH874 2889 TAIL ROTOR BLADE CRACKED. 1G71 3U H9EU 20010911000112001091100011EU 2001 9 11 HCMA075391 120010821G5302350A2300000201 TAIL BOOM SNIAS 350 AS350BA 8680817EU TAIL MISMANUFACTURED E HCMAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP13642BH15023 2495 TAILBOOM SKIN NOT PROPER THICKNESS. 1G71 3U NCH9EU 20010419002372001041900237NE 2001 4 19 HEEA071922 120010403G64107610105101041 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW031545X12811 760050 TRAILING EDGE OF PADDLE A IS SPLIT OPEN. THE CENTER PLUG IS ALSO DEBONDED. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20010419002382001041900238NE 2001 4 19 HEEA071923 120010405G62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE MAIN ROTOR BLADECRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0315460 760223 TOP SKIN HAS A CRACK SPANWISE APPROXIMATELY 2 INCHES FROM TRAILING EDGE. THE ABRASION STRIP HAS A CRACK WITH SEPARATION. SENT TO COMPOSITE TECHNICS FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20010419002392001041900239NE 2001 4 19 HEEA071924 120010405G62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE MAIN ROTOR BLADECRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03911UK 760275 TOP INNER AND OUTER DOUBLER SEPARATED BEYOND LIMITS. ABRASION STRIP HAS CRACKS ON BOTH SIDES. SENT TO COMPOSITE TECHNICS FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20010419002402001041900240 2001 4 19 HEEA071925 420010405G2340A3016W CONTROL PANEL SKRSKYS76 S76A 8143006NE INTERPHONE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03761PH 760224 NEEDS EVALUATION. PERFORMED PRELIMINARY INSPECTION AND TESTED. FOUND SWITCHES S1, S4, S5, S8, LIGHT PANEL, VOLUME KNOB AND TRANSMIT KNOB BAD. ALSO LIGHT PANEL LIGHTS BAD FROM STOCK. REPLACED ALL AND RESOLDERED BAD SOLDER CONNECTION ON LIGHT PANEL. REPAIRED. BENCH CHECK GOOD. 1G72 3U H1NE 20010419002412001041900241SW 2001 4 19 HEEA071926 120010402G5302214021211110S PANEL BELL 214 214ST 1182106SW TAILBOOM MISMANUFACTURED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 PANEL RECEIVED PREVIOUSLY TRIMMED ALONG FORWARD END. CANNOT POSITION ON TAILBOOM TO ACHIEVE PROPER EDGE DISTANCE ON ALL FASTENERS. PANEL NEEDS TO BE MOVED FORWARD AND CORE TRANSITION IS ALREADY CONTACTING STRAP AT BOOM STATION 293.50. PANEL IS SHORTER THAN THE PANEL REMOVED FROM THE TAILBOOM SENT TO BELL HELICOPTER TEXTRON FOR CREDIT. 2G72 4U H10SW 20010419002422001041900242SW 2001 4 19 HEEA071927 120010402G6330206033505101 NODAL ARM BELL 206 206L3 1182108SW TRANSMISSION MISMANUFACTURED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 ARM IS NOT MACHINED OUT AT INBOARD RADIUS. 1G71 3U H2SW 20010419002432001041900243SW 2001 4 19 HEEA071928 120010402G5302206033412001A BRACKET BELL 206 206L3 1182108SW TAILBOOM MISMANUFACTURED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 BRACKET HAS PILOT HOLES FROM FACTORY DRILLED OPPOSITE OF REQUIRED LAYOUT. 1G71 3U H2SW 20010419002442001041900244SW 2001 4 19 HEEA071929 120010403G2840473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FUEL INDICATOR INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 FUEL LOW LEVEL LIGHT COMES ON INTERMITTENTLY. 1G72 4U H4SW 20010419002452001041900245SW 2001 4 19 HEEA071930 120010403G261230236ET1 AMPLIFIER BELL 412 412 1182202SW FIRE DETECTOR MALFUNCTIONED E HEEAO OTHER N FALSE WARNING CRCRUISE 1 SW035759N 33002 WHILE IN CRUISE FLIGHT THE BAGGAGE COMPARTMENT FIRE LIGHT ILLUMINATED. NO FIRE OBSERVED. MAINTENANCE REPAIRED CHAFED WIRE AT AMPLIFIER CONTROL CONNECTOR. 1G72 4U H4SW 20010419002462001041900246SW 2001 4 19 HEEA071931 120010403G7600 CONTROL UNIT BELL 214 214ST 1182106SW NR 2 ENGINE MALFUNCTIONED E HEEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW033897N 28106 IN CRUISE FLIGHT, NR 2 ENGINE DROPPED OFF LINE THEN RECOVERED BACK TO 100 PERCENT. PLACED NR 2 ENGINE IN ECU LOCKOUT AND RETURNED TO BASE. 2G72 4U H10SW 20010419002472001041900247SW 2001 4 19 HEEA071932 120010403G2435 BRUSHES BELL 407 407 SW STARTER GEN WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03498PH2544 53399 BRUSHES WORN. 1G71 3U O H2SW 20010419002482001041900248SW 2001 4 19 HEEA071933 120010403G2435 BRUSHES BELL 407 407 SW STARTER GEN WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH1337 53378 BRUSHES WORN. 1G71 3U O H2SW 20010419002492001041900249SW 2001 4 19 HEEA071934 120010403G28221C641 PUMP BELL 412 412 1182202SW FUEL BOOST FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 TRANSFER LIGHT COMING ON ABOVE 1700 LBS. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419002502001041900250SW 2001 4 19 HEEA071935 120010403G6720412010406115 LINK BELL 412 412 1182202SW ROD END WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419002512001041900251SW 2001 4 19 HEEA071936 120010403G6720412010406115 LINK BELL 412 412 1182202SW ROD END WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419002522001041900252SW 2001 4 19 HEEA071937 120010403G6720412010406115 LINK BELL 412 412 1182202SW ROD END WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419002532001041900253SW 2001 4 19 HEEA071938 120010403G6720412010406115 LINK BELL 412 412 1182202SW ROD END WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033911L 33023 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419002542001041900254SW 2001 4 19 HEEA071939 120010403G33407028521 STROBE BELL 412 412 1182202SW EXTERIOR FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033893L 33006 NO OUTPUT. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419002552001041900255SW 2001 4 19 HEEA071940 120010403G3340G62504 LIGHT BELL 412 412 1182202SW EXETERIOR SEARCHFAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 SEARCH LIGHT WILL NOT POINT FORWARD. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419002562001041900256 2001 4 19 HEEA071941 420010403G34165934D3 ALTIMETER BELL 407 407 SW COCKPIT INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW0357416 53070 ALTIMETER IS 120 FEET OFF. 1G71 3U O H2SW 20010419002572001041900257SW 2001 4 19 HEEA071942 120010403G6210206015001107 BLADE BELL 206 206L3 1182108SW MAIN ROTOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036251Y1340 51556 TRAILING SKIN AND SPAR HAS EXCESSIVE CORROSION NEAR THE TIP ON THE LOWER SIDE. 1G71 3U H2SW 20010419002582001041900258SW 2001 4 19 HEEA071943 120010403G243523081018 STARTER GEN BELL 206 206L3 1182108SW ENGINE FAILED E HEEAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW034835 51131 SMOKE AND SPARKS FROM AREA OF TERMINAL BLOCK WHEN MOTORING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010419002592001041900259SW 2001 4 19 HEEA071944 120010403G8011SM20ACD200A21 RELAY BELL 206 206L3 1182108SW STARTER FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW038592X 51508 STUCK IN ENERGIZED POSITION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010419002602001041900260GL 2001 4 19 HEEA071945 220010403G753223005366 BLEED VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036610C2612 51425 HIGH TOT. OVERHAULED AND REPLACED DIAPHRAGMS P/N 6899114. 1G71 3U3 U H2SW E1GL 20010419002612001041900261GL 2001 4 19 HEEA071946 220010403G753223005366 BLEED VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0349EA 2131 51507 ENGINE RUNS HOT. OVERHAULED AND REPLACED DIAPHRAGMS P/N 6899114. 1G71 3U3 U H2SW E1GL 20010419002622001041900262 2001 4 19 HEEA071947 420010403G34161003511326 ALTIMETER BELL 212 212 1181420SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035009N 30936 ALTIMETER WILL NOT ZERO OUT. 1G71 4U H4SW 20010419002632001041900263 2001 4 19 HEEA071948 420010403G3416212070238003 INDICATOR BELL 412 412 1182202SW COCKPIT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 ALTIMETER ADJUSTMENT KNOB DOES NOT TURN. 1G72 4U H4SW 20010419002642001041900264 2001 4 19 HEEA071949 420010403G3416212070238007 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 WHEN BARO KNOB ON ALTIMETER IS TURNED, NEEDLE MOVES INTERMITTENTLY. 1G72 4U H4SW 20010419002652001041900265SW 2001 4 19 HEEA071950 120010403G243230126001 BATTERY BELL 412 412 1182202SW DC SYSTEM DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033893L 33006 BATTERY WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G72 4U H4SW 20010420000862001042000086SW 2001 4 20 HEEA071951 120010403G243230703001 BATTERY BELL 412 412 1182202SW DC SYSTEM DISCHARGED E HEEAK NONE H ELECT. POWER LOSS-50 PC ININSP/MAINT 1 SW03107X 33113 LOST ALL POWER AND WOULD NOT CHARGE. REPLACED WITH SERVICEABLE BATTERY. 1G72 4U H4SW 20010419002662001041900266SW 2001 4 19 HEEA071952 120010403G28222C271 CARTRIDGE BELL 206 206L1 1182107SW BOOST PUMP INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW033178K 45765 BOOST PUMP CARTRIDGE INOPERATIVE. 1G71 3U H2SW 20010419002672001041900267SW 2001 4 19 HEEA071953 120010403G28222C271 CARTRIDGE BELL 206 206L1 1182107SW BOOST PUMP FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033905B 45598 LEFT HAND FUEL BOOST PUMP CARTRIDGE FAILED. 1G71 3U H2SW 20010419002682001041900268SW 2001 4 19 HEEA071954 120010403G28222C271 CARTRIDGE BELL 206 206L3 1182108SW BOOST PUMP INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW033116P 51530 BOOST PUMP CARTRIDGE INOPERATIVE. 1G71 3U H2SW 20010419002692001041900269SW 2001 4 19 HEEA071955 120010403G243232007001 BATTERY BELL 206 206L1 1182107SW DC SYSTEM DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035019F 45244 BATTERY IS TOO WEAK TO REACH PROPER N1 FOR START. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20010419002702001041900270SW 2001 4 19 HEEA071956 120010403G243232007001 BATTERY BELL 206 206L3 1182108SW DC SYSTEM DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW034835 51131 BATTERY WEAK DURING STARTS. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20010419002712001041900271SW 2001 4 19 HEEA071957 120010403G243232007001 BATTERY BELL 206 206L1 1182107SW DC SYSTEM DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033178K 45765 BATTERY DEAD AND WILL NOT HOLD CHARGE. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20010419002722001041900272SW 2001 4 19 HEEA071958 120010403G243232007001 BATTERY BELL 206 206L1 1182107SW DC SYSTEM DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035745S 45491 WEAK STARTING CAPACITY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20010419002732001041900273SW 2001 4 19 HEEA071959 120010403G3300A413AHDACF1428 POWER SUPPLY BELL 206 206L1 1182107SW LIGHTING INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0345RP 45521 POWER SUPPLY HAS NO POWER OUTPUT. 1G71 3U H2SW 20010419002742001041900274SW 2001 4 19 HEEA071960 120010403G3340A490A POWER SUPPLY BELL 206 206L3 1182108SW STROBE INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036160Y 51609 INOPERATIVE - NO FLASH ON STROBE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010419002752001041900275SW 2001 4 19 HEEA071961 120010403G3340A490A POWER SUPPLY BELL 206 206L3 1182108SW STROBE INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036251X 51552 NO POWER TO LIGHT BULB. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010419002762001041900276SW 2001 4 19 HEEA071962 120010403G2432RG222 BATTERY BELL 206 206L1 1182107SW DC SYSTEM DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035014Y 45219 BATTERY TOO WEAK TO START AIRCRAFT. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010419002772001041900277SW 2001 4 19 HEEA071963 120010403G2432A1077 RELAY BELL 206 206L3 1182108SW BATTERY OVERHEATED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW034180F BATTERY RELAY STARTED SMOKING AFTER GENERATOR WAS PLACED ON LINE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010419002782001041900278SW 2001 4 19 HEEA071964 120010403G2430A1077V CONTACTOR BELL 206 206L4 1182110SW DC GENERATOR FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW037074W 52033 CONTACTOR STUCK CLOSED. 1G71 3U NCH2SW 20010419002792001041900279SW 2001 4 19 HEEA071965 120010403G2435SM20ACD200A21 RELAY BELL 206 206L4 1182110SW STARTER GEN FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037074W 52033 WHEN PILOT ENGAGED STARTER DURING ENGINE RINSE THE STARTER WOULD NOT COME OFF LINE UNTIL BATTERY SWITCH WAS TURNED OFF. FOUND STARTER RELAY WAS STUCK CLOSED. SENT TO PRECISION AVIONICS & INSTR. INC. FOR INSPECTION AND REPAIR. 1G71 3U NCH2SW 20010419002802001041900280SW 2001 4 19 HEEA071966 120010403G3260XA7503DC SQUAT SWITCH BELL 206 206L3 1182108SW MLG STUCK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0342EA 51542 STUCK OPEN. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20010419002812001041900281NE 2001 4 19 HEEA071967 220010403G72103024780 GEARBOX BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NR 1 ENGINE MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW032258F 33073 COMBINING GEARBOXMAKING METAL NR 1 SIDE. 1G72 4U4 U H4SW E22EA 20010419002822001041900282SW 2001 4 19 HEEA071968 120010405G243230703001 BATTERY BELL 412 412 1182202SW DC SYSTEM DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032149S 36002 VOLTAGE WAS AT 24 VOLTS AND THEN DROPPED TO 20 WITH ONLY THE BATTERY SWITCHES ON. REPLACED WITH SERVICEABLE BATTERY. 1G72 4U H4SW 20010419002832001041900283SW 2001 4 19 HEEA071969 120010405G6730C42641100 SERVO VALVE 206076031109BELL 206 206L3 1182108SW ACTUATOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03 RH0366 SERVO VALVE IS CAUSING EXCESSIVE INTERNAL LEAKAGE IN NEUTRAL POSITION. SENT TO FORTNER ACCESSORY SERVICE CORP. FOR WARRANTY REPAIR. 1G71 3U H2SW 20010419002842001041900284SW 2001 4 19 HEEA071970 120010405G2432RG222 BATTERY BELL 206 206L1 1182107SW DC SYSTEM DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035007Q 45187 UNABLE TO START AIRCRAFT ON FIRST START ATTEMPT AND WAS WEAK ON THE SECOND START ATTEMPT. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20010419002852001041900285SW 2001 4 19 HEEA071971 120010405G2432RG214 BATTERY BELL 214 214ST 1182106SW DC SYSTEM DAMAGED E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW033897N 28106 WEAK. FOUND DEEP GASH ON LOWER BATTERY CASE. 2G72 4U H10SW 20010419002862001041900286SW 2001 4 19 HEEA071972 120010405G2432RG214 BATTERY BELL 214 214ST 1182106SW DC SYSTEM DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033897N 28106 WILL NOT START AIRCRAFT. REPLACED WITH SERVICEABLE BATTERY. 2G72 4U H10SW 20010419002872001041900287SW 2001 4 19 HEEA071973 120010405G2432RG214 BATTERY BELL 214 214ST 1182106SW DC SYSTEM DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033897N 28106 WILL NOT GO IN A SERIES, WEAK. REPLACED WITH SERVICEABLE BATTERY. 2G72 4U H10SW 20010419002882001041900288 2001 4 19 HEEA071974 420010405G2312064101902 TRANSCEIVER BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0321497 51518 WILL NOT RECEIVE. PERFORMED PRELIMINARY INSPECTION AND TESTED. COULD NOT DUPLICATE PROBLEM. FOUND FREQUENCY SELECTOR INTERMITTENTLY SWITCHING TO MEMORY PRESETS WHEN ADJUSTING FREQUENCY. CLEANED SW102 SWITCH AND SELECTOR CONTACTS. REPAIRED. ADJUSTED SQUELCH AND MIC GAIN. BENCH CHECK GOOD. 1G71 3U H2SW 20010419002892001041900289 2001 4 19 HEEA071975 420010405G2312064102300 TRANSCEIVER BELL 412 412 1182202SW COCKPIT STUCK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03107X 33113 SQUELCH IS STICKING. PERFORMED PRELIMINARY INSPECTION AND TESTED. COULD NOT DUPLICATE PROBLEM. REMOVED CORROSION FROM UNIT. REPLACED BROKEN L505 COIL. ADJUSTED C/N SQUELCH, FREQUENCY, MIC GAIN AND SIDETONE. BENCH CHECK GOOD. 1G72 4U H4SW 20010419002902001041900290 2001 4 19 HEEA071976 420010405G2312064102300 TRANSCEIVER BELL 412 412 1182202SW COCKPIT WEAK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03142PH 33150 TRANSMITS UNREADABLE. PERFORMED PRELIMINARY INSPECTION AND TESTED. FOUND MODULATION VERY WEAK. ADJUSTED MIC GAIN, TRANSMIT POWER, AND SIDETONE. FOUND MODULATION WOULD BECOME DISTORTED AFTER KEYED UP A FEW TIMES. REPLACED Q109 AND Q110 MODULATORS. REPAIRED. REMOVED CORROSION FROM CHASSIS. BENCH CHECK GOOD. 1G72 4U H4SW 20010419002912001041900291 2001 4 19 HEEA071977 420010405G2312064102300 TRANSCEIVER BELL 412 412 1182202SW COCKPIT UNRELIABLE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036559Z 36019 TRANSMITS UNREADABLE. PERFORMED PRELIMINARY INSPECTION AND TESTED. ALIGNED TRANSMITTER. REPAIRED PROBLEM. BENCH CHECK GOOD. 1G72 4U H4SW 20010419002932001041900293 2001 4 19 HEEA071979 420010405G3451066106902 DISPLAY BELL 412 412 1182202SW DME/TACAN UNIT OUT OF TOLERANCEE HEEAK NONE L NO TEST ININSP/MAINT 1 SW03142PH 33150 DME DISPLAY TOO DIM. PERFORMED PRELIMINARY INSPECTION. FOUND PHOTOCELL V901 HAD BROKEN LEG. REPAIRED LEG. REPAIRED UNIT. BENCH CHECK GOOD. 1G72 4U H4SW 20010419002942001041900294 2001 4 19 HEEA071980 420010405G3452066104100 TRANSPONDER BELL 412 412 1182202SW ATC INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032261D 33076 NO TRANSMIT OR RECEIVE. PERFORMED PRELIMINARY INSPECTION, TESTED UNIT, FOUND WOULD NOT POWER UP. FUSE BAD. ALSO TROUBLESHOT UNIT DUE TO FUSE SHORTED AND FOUND TRANSISTOR Q101 BAD. INSTALLED FUSE AND TRANSISTOR Q101. TESTED UNIT AND FOUND SHIELD IN POWER SUPPLY SHORTED. ALIGNED UNIT. BENCH CHECK GOOD. 1G72 4U H4SW 20010419002952001041900295 2001 4 19 HEEA071981 420010405G345713824120234 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036251Y 51556 CONSTANTLY CYCLES. PERFORMED PRELIMINARY INSPECTION. FOUND WPT BUTTON CYCLES THROUGH SEVERAL PAGES WHEN PRESSED. ALSO FOUND MSG, APT/VOR AND NAV BUTTONS INTERMITTENT. SELECTOR SWITCH ALSO INTERMITTENT. REPLACED 4 EACH SWITCHES FOR BUTTONS AND SELECTOR SWITCH. REPAIRED PROBLEM. REPLACED WORN KEY CAPS. BENCH CHECK GOOD. 1G71 3U H2SW 20010419002962001041900296 2001 4 19 HEEA071982 420010405G34211113034 INDICATOR BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033893L 33006 TURN NEEDLE ON ATTITUDE INDICATOR INOPERATIVE. 1G72 4U H4SW 20010419002972001041900297SW 2001 4 19 HEEA071983 120010405G2844124044 INDICATOR BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03 FUEL PRESSURE INDICATOR NEEDLE STAYS ON ZERO. 1G72 4U H4SW 20010419002982001041900298SW 2001 4 19 HEEA071984 120010405G2844124044 INDICATOR BELL 412 412 1182202SW COCKPIT FLUCTUATES E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033893L 33006 FUEL PRESSURE INDICATOR FLUCTUATES 8 TO 10 PSI. 1G72 4U H4SW 20010419002992001041900299SW 2001 4 19 HEEA071985 120010405G280020038000001 TRANSMITTER BELL 412 412 1182202SW FUEL QUANTITY MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03142PH 33150 FUEL LOW LIGHT COMES ON AFTER REFUELING. REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010419003002001041900300SW 2001 4 19 HEEA071986 120010405G3040204070907102 MOTOR BELL 412 412 1182202SW WINDSHIELD WIPERLOOSE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 MOTOR IS LOOSE ON COVERTER. 1G72 4U H4SW 20010419003012001041900301SW 2001 4 19 HEEA071987 120010405G7810212061202010 EXHAUST STACK BELL 412 412 1182202SW ENGINE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03108X 33115 EXHAUST STACK IS CRACKED AT SEAMS OF DUCT HALVES. THE CRACKED AREA EXCEEDS THE LIMITS. 1G72 4U H4SW 20010419003022001041900302SW 2001 4 19 HEEA071988 120010405G2910212076006007 VALVE BELL 412 412 1182202SW NR 2 HYD SYSTEM FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 NR 2 HYDRAULIC SYSTEM VALVE WILL NOT SHUT OFF. 1G72 4U H4SW 20010419003032001041900303SW 2001 4 19 HEEA071989 120010405G2820212076015001 VALVE BELL 412 412 1182202SW FUEL SYSTEM LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW032149S 36002 FUEL VALVE LEAKING THROUGH WEEP HOLE. SENT TO BELL HELICOPTER TEXTRON FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20010419003042001041900304 2001 4 19 HEEA071990 420010405G3424214075244001 GYRO BELL 412 412 1182202SW TURN RATE MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW031202T 33112 RATE OF TURN NEEDLE TRAVELS FULL LEFT AND RIGHT IN HOVER. 1G72 4U H4SW 20010419003052001041900305SW 2001 4 19 HEEA071991 120010405G2611302319 SMOKE DETECTOR BELL 412 412 1182202SW ENGINE MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036559Z 36019 SMOKE DETECTION UNIT WOULD TEST INCONSISTENTLY. 1G72 4U H4SW 20010419003062001041900306SW 2001 4 19 HEEA071992 120010405G771439433339002 INDICATOR BELL 412 412 1182202SW TRIPLE TACH INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033893L 33006 NR 1 NEEDLE ON TRIPLE TACH INOPERATIVE. 1G72 4U H4SW 20010419003072001041900307SW 2001 4 19 HEEA071993 120010405G3213412030437103 CAP BELL 412 412 1182202SW CROSSTUBE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 RUBBER WORN AND DETERIORATED ON CROSSTUBE. 1G72 4U H4SW 20010419003082001041900308SW 2001 4 19 HEEA071994 120010405G3246412050015110 SKID BELL 412 412 1182202SW MLG WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 SADDLE FASTENERS MAKING MUD - SHOWING WEAR. 1G72 4U H4SW 20010419003092001041900309SW 2001 4 19 HEEA071995 120010405G2840473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FUEL INDICATOR MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03142PH 33150 LOW FUEL LIGHT COMING ON AFTER REFUELING AIRCRAFT. 1G72 4U H4SW 20010419003102001041900310SW 2001 4 19 HEEA071996 120010405G2840473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FUEL INDICATOR MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW031202T 33112 TRANSFER LIGHT CAME ON AT 1850 LBS. 1G72 4U H4SW 20010419003112001041900311SW 2001 4 19 HEEA071997 120010405G2840473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FUEL INDICATOR MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW031202T 33112 TRANSFER LIGHT CAME ON AT 1850 LBS. 1G72 4U H4SW 20010419003122001041900312 2001 4 19 HEEA071998 420010405G2340AA34300 INTERPHONE BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03107X 33113 TRANSMITS AND RECEIVES POORLY. SENT TO EDMO DIST. FOR WARRANTY REPAIR. 1G72 4U H4SW 20010419003132001041900313 2001 4 19 HEEA071999 420010405G2561PHI10090 LIFE VEST BELL 412 412 1182202SW CABIN FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032148K 36001 LIFE VEST FAILED 3 MONTH INSPECTION. 1G72 4U H4SW 20010419003142001041900314 2001 4 19 HEEA072000 420010405G3451066106901 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036559Z 36019 DIGITS FLICKERING. REPLACED DISPLAY AND LENS. COOKED UNIT, INSPECTED AND BENCH CHECK GOOD. 1G72 4U H4SW 20010419003152001041900315 2001 4 19 HEEA072001 420010405G3451066106902 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036559Z 36019 SEGMENT VERY DIM IN DAYLIGHT. FOUND PHOTOCELL BAD. INSTALLED NEW PHOTOCELL. ALSO MISSING 2 EACH COVER SCREWS. INSTALLED 2 SCREWS. BENCH CHECK GOOD. 1G72 4U H4SW 20010419003162001041900316 2001 4 19 HEEA072002 420010405G3452066107100 TRANSPONDER BELL 412 412 1182202SW ATC FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW037128R 36007 NO OUTPUT. PERFORMED PRELIMINARY INSPECTION. FOUND MODULATOR WAS LOADING DOWN THE POWER SUPPLY VOLTAGES. REPLACED TWO EACH INSULATORS AND ONE EACH BUSHING FOR TRANSISTORS Q501 AND Q502. CLEANED CORROSION FROM BACKSIDE OF THE TRANSISTORS. REPAIRED. 1G72 4U H4SW 20010419003172001041900317 2001 4 19 HEEA072003 420010405G3452066107100 TRANSPONDER BELL 412 412 1182202SW ATC INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0333008 36004 REPORTED INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. CLEANED EXCESSIVE CORROSION FROM UNIT. FOUND WEAK RECEIVER SENSE AND WEAK TRANSMIT POWER. REPLACED TRANSMITTER BOARD AND ALIGNED TO SPECS. ALIGNED THE RECEIVER. BENCH CHECK GOOD. 1G72 4U H4SW 20010419003182001041900318 2001 4 19 HEEA072004 420010405G3455066107700 RECEIVER BELL 412 412 1182202SW ADF SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032149S 36002 WILL NOT HOME TO STATIONS. PERFORMED PRELIMINARY INSPECTION. FOUND EXCESSIVE CORROSION IN UNIT AND UNDER F.C. I323 AND CAPACITOR C380. REPLACED I323 AND C380 AND CLEANED CORROSION. ALODYNED CHASIS. BENCH CHECK GOOD. 1G72 4U H4SW 20010419003192001041900319 2001 4 19 HEEA072005 420010405G3454071121627 CONTROL UNIT BELL 412 412 1182202SW NAVIGATION SYS MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03142PH 33150 WILL NOT CHANNEL PROPERLY CAUSING VOR NOT TO WORK PROPERLY. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT WILL NOT DISPLAY NAV FREQUENCY ON KTS-143. REPLACED IC I201 AND PHOTOCELL LENS. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20010419003202001041900320SW 2001 4 19 HEEA072006 120010405G5210204031762002 SPRING BELL 412 412 1182202SW BLOCKS BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 DOOR SPRING BROKEN. REPLACED WITH SERVICEABLE SPRING. 1G72 4U H4SW 20010419003212001041900321SW 2001 4 19 HEEA072007 120010405G6320212040233001 LINE BELL 412 412 1182202SW OIL SYSTEM CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 TUBE ASSY WAS FOUND CHAFED. REPLACED WITH SERVICEABLE TUBE. 1G72 4U H4SW 20010419003222001041900322SW 2001 4 19 HEEA072008 120010405G6320212040233001 LINE BELL 412 412 1182202SW OIL SYSTEM CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 TUBE ASSY WAS FOUND CHAFED. REPLACED WITH SERVICEABLE TUBE. 1G72 4U H4SW 20010419003232001041900323SW 2001 4 19 HEEA072009 120010405G6320212040234001 LINE BELL 412 412 1182202SW OIL SYSTEM CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 TUBE ASSY WAS FOUND CHAFED. REPLACED WITH SERVICEABLE TUBE. 1G72 4U H4SW 20010419003242001041900324SW 2001 4 19 HEEA072010 120010405G6320212040234001 LINE BELL 412 412 1182202SW OIL SYSTEM CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 TUBE ASSY WAS FOUND CHAFED. REPLACED WITH SERVICEABLE TUBE. 1G72 4U H4SW 20010419003252001041900325SW 2001 4 19 HEEA072011 120010405G6320212040234001 LINE BELL 412 412 1182202SW OIL SYSTEM CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 TUBE ASSY WAS FOUND CHAFED. REPLACED WITH SERVICEABLE TUBE. 1G72 4U H4SW 20010419003262001041900326SW 2001 4 19 HEEA072012 120010405G2911212076007003 ACCUMULATOR BELL 412 412 1182202SW HYD SYSTEM LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW032149S 36002 ACCUMULATOR LEAKS FROM WEEP HOLE. REPLACED WITH SERVICEABLE ACCUMULATOR. 1G72 4U H4SW 20010419003272001041900327SW 2001 4 19 HEEA072013 120010405G2910212076302001 LINE BELL 412 412 1182202SW HYD SYSTEM CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 CHAFED BEYOND LIMITS. REPLACED WITH SERVICEABLE TUBE. 1G72 4U H4SW 20010419003282001041900328SW 2001 4 19 HEEA072014 120010405G2910212076311001 LINE BELL 412 412 1182202SW HYD SYSTEM CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 CHAFED BEYOND LIMITS. REPLACED WITH SERVICEABLE TUBE. 1G72 4U H4SW 20010419003292001041900329SW 2001 4 19 HEEA072015 120010405G2560214070966107 SEAT BELT BELL 412 412 1182202SW COCKPIT TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 SEAT BELT TORN. REPLACED WITH SERVICEABLE BELT. 1G72 4U H4SW 20010419003302001041900330SW 2001 4 19 HEEA072016 120010405G6710 BEARING BELL 412 412 1182202SW BELLCRANK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 BEARINGS FOUND WORN DURING DAILY CHECK. REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003312001041900331SW 2001 4 19 HEEA072017 120010405G6710412010182101 BEARING BELL 412 412 1182202SW M/R PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 BEARING FOUND WORN. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003322001041900332SW 2001 4 19 HEEA072018 120010405G6710412010182101 BEARING BELL 412 412 1182202SW M/R PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 BEARING FOUND WORN. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003332001041900333SW 2001 4 19 HEEA072019 120010405G6230412010405109 DRIVE LINK BELL 412 412 1182202SW SWASHPLATE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 WORN BEARING. REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003342001041900334SW 2001 4 19 HEEA072020 120010405G6720412010406115 LINK BELL 412 412 1182202SW ROD END WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 WORN BEARING. REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003352001041900335SW 2001 4 19 HEEA072021 120010405G6720412010406115 LINK BELL 412 412 1182202SW ROD END WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 WORN BEARING. REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003362001041900336 2001 4 19 HEEA072022 420010405G2350A3016W AUDIO PANEL BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032149S 36002 TRANSMITS WITH MIC SELECTOR IN FM1 POSITION AND RECEIVES FM1 ON THE FM2 POSITION. PERFORMED PRELIMINARY INSPECTION AND FOUND UNIT TRANSMIT OUTPUT DISTORTED. REPLACED CAPACITOR C30 AND ALSO LIGHT PANEL WORN. REPLACED LIGHT PANEL. BENCH CHECK GOOD. 1G72 4U H4SW 20010419003372001041900337SW 2001 4 19 HEEA072023 120010405G2840APTE1391500SG TRANSDUCER BELL 412 412 1182202SW FUEL SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03142PH 33150 CAUSING INDICATOR TO READ 5 PSI WHEN AIRCRAFT IS SHUTDOWN. REPLACED WITH SERVICEABLE TRANSMITTER. 1G72 4U H4SW 20010419003382001041900338SW 2001 4 19 HEEA072024 120010405G3340G62504 SEARCH LIGHT BELL 412 412 1182202SW EXTERIOR MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03142PH 33150 RETRACTION MOTOR WILL NOT SHUT OFF WHEN FULLY RETRACTED. REPLACED WITH SERVICEABLE LIGHT. 1G72 4U H4SW 20010419003392001041900339SW 2001 4 19 HEEA072025 120010405G6220412010100193FM HUB BELL 412 412 1182202SW MAIN ROTOR VIBRATION E HEEAK NONE E VIBRATION/BUFFET ININSP/MAINT 1 SW036559Z 36019 BLUE SPINDLE CAUSING VIBRATION. REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003402001041900340SW 2001 4 19 HEEA072026 120010405G6710412010182101 BEARING BELL 412 412 1182202SW M/R PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003412001041900341SW 2001 4 19 HEEA072027 120010405G6710412010182101 BEARING BELL 412 412 1182202SW M/R PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003422001041900342SW 2001 4 19 HEEA072028 120010405G6710412010182101 BEARING BELL 412 412 1182202SW M/R PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893N 33010 WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003432001041900343SW 2001 4 19 HEEA072029 120010405G6710412010182101 BEARING BELL 412 412 1182202SW M/R PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893N 33010 WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003442001041900344SW 2001 4 19 HEEA072030 120010405G6710412010182101 BEARING BELL 412 412 1182202SW M/R PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893N 33010 WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003452001041900345SW 2001 4 19 HEEA072031 120010405G6710412010182101 BEARING BELL 412 412 1182202SW M/R PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893N 33010 WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003462001041900346SW 2001 4 19 HEEA072032 120010405G6710412010182101 BEARING BELL 412 412 1182202SW M/R PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003472001041900347SW 2001 4 19 HEEA072033 120010405G6710412010182101 BEARING BELL 412 412 1182202SW M/R PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003482001041900348SW 2001 4 19 HEEA072034 120010405G6710412010182101 BEARING BELL 412 412 1182202SW M/R PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003492001041900349SW 2001 4 19 HEEA072035 120010405G6710412010182101 BEARING BELL 412 412 1182202SW M/R PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003502001041900350SW 2001 4 19 HEEA072036 120010405G6230412010405109 DRIVE LINK BELL 412 412 1182202SW SWASHPLATE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 WORN BEARING. REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003512001041900351SW 2001 4 19 HEEA072037 120010405G6230412010405109 DRIVE LINK BELL 412 412 1182202SW SWASHPLATE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 WORN BEARING. REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003522001041900352SW 2001 4 19 HEEA072038 120010405G6720412010406115 LINK BELL 412 412 1182202SW SWASHPLATE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 MAIN ROTOR VIBRATION. REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010419003532001041900353SW 2001 4 19 HEEA072039 120010405G3212412050013117 FLOAT BELL 412 412 1182202SW MLG LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 LEAKING FROM AROUND FORWARD AIR VALVE. SENT TO OFFSHORE HELICOPTER SUPPORT FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20010419003542001041900354SW 2001 4 19 HEEA072040 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003552001041900355SW 2001 4 19 HEEA072041 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003562001041900356SW 2001 4 19 HEEA072042 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003572001041900357SW 2001 4 19 HEEA072043 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003582001041900358SW 2001 4 19 HEEA072044 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003592001041900359SW 2001 4 19 HEEA072045 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003602001041900360SW 2001 4 19 HEEA072046 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003612001041900361SW 2001 4 19 HEEA072047 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003622001041900362SW 2001 4 19 HEEA072048 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003632001041900363SW 2001 4 19 HEEA072049 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003642001041900364SW 2001 4 19 HEEA072050 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003652001041900365SW 2001 4 19 HEEA072051 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003662001041900366SW 2001 4 19 HEEA072052 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893N 33010 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003672001041900367SW 2001 4 19 HEEA072053 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003682001041900368SW 2001 4 19 HEEA072054 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003692001041900369SW 2001 4 19 HEEA072055 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003702001041900370SW 2001 4 19 HEEA072056 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010419003712001041900371SW 2001 4 19 HEEA072057 120010405G2560501819409 SEAT BELT BELL 412 412 1182202SW COCKPIT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 WORN. 1G72 4U H4SW 20010419003722001041900372SW 2001 4 19 HEEA072058 120010405G2560501836307 SEAT BELT BELL 412 412 1182202SW COCKPIT FRAYED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032298Z 33077 FRAYED. REPLACED WITH SERVICEABLE RESTRAINT. 1G72 4U H4SW 20010419003732001041900373 2001 4 19 HEEA072059 420010405G23709806020023 CVR BELL 412 412 1182202SW COCKPIT WILL NOT TEST E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0330YM 36032 FAILS TO ILLUMINATE TEST LIGHT. 1G72 4U H4SW 20010419003742001041900374 2001 4 19 HEEA072060 420010405G23709806020023 CVR BELL 412 412 1182202SW COCKPIT WILL NOT TEST E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035759N 33002 WILL NOT LIGHT UP TEST LIGHT ON PUSH BUTTON TEST. FOUND UNIT FAILED FSK TEST AND ROTOR SPEED TEST. 1G72 4U H4SW 20010420001862001042000186SW 2001 4 20 HEEA072061 120010405G3212D24911117 FLOAT BELL 412 412 1182202SW MLG LEAKING E HEEAK NONE L NO TEST ININSP/MAINT 1 SW037128R 36007 LEAKING, FAILED 6 MONTH INSPECTION. 1G72 4U H4SW 20010420001872001042000187SW 2001 4 20 HEEA072062 120010405G3212D24921119 FLOAT BELL 412 412 1182202SW MLG FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032014K 33020 AFTER ELECTRICAL INFLATION OF FLOAT SYSTEM, A LEAK AT THE REAR POP OFF VALVE WAS NOTED. VALVE THREADS WERE STRIPPED. VALVE WOULD ONLY ROTATE. 1G72 4U H4SW 20010420001882001042000188SW 2001 4 20 HEEA072063 120010405G3212D24921119 FLOAT BELL 412 412 1182202SW MLG FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW037128R 36007 LEAKING, FAILED 6 MONTH INSPECTION. SENT TO OFFSHORE HELICOPTER SUPPORT FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20010420001892001042000189 2001 4 20 HEEA072064 420010405G2350M880555002 SWITCH BELL 412 412 1182202SW COMM SYSTEM STUCK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW037128R 36007 INTERMITTENT HOT MIKE SWITCH STICKING. REPLACED WITH SERVICEABLE SWITCH. 1G72 4U H4SW 20010420001902001042000190SW 2001 4 20 HEEA072065 120010405G5260PHI101741 STEP BELL 412 412 1182202SW LEFT STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 LEFT HAND STEP STAYING UP. REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010420001912001042000191SW 2001 4 20 HEEA072066 120010405G5260PHI101741 STEP BELL 412 412 1182202SW RIGHT STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 RIGHT HAND STEP WILL NOT GO DOWN. REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010420001922001042000192SW 2001 4 20 HEEA072067 120010405G5260PHI101741 STEP BELL 412 412 1182202SW RIGHT STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R 36007 RIGHT HAND STEP WILL NOT EXTEND. REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010420001932001042000193SW 2001 4 20 HEEA072068 120010405G5260PHI101741 STEP BELL 412 412 1182202SW LEFT STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 WOULD NOT LET LT STEP GO DOWN. REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010420001942001042000194 2001 4 20 HEEA072069 420010405G2312VFS10902 ANTENNA BELL 412 412 1182202SW VHF DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893N 33010 ANTENNA SPLIT. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010420001952001042000195SW 2001 4 20 HEEA072070 120010405G3212412050017133 COVER BELL 412 412 1182202SW FLOAT BAG TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 COVER TORN. SENT TO OFFSHORE HELICOPTER SUPPORT FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20010420001962001042000196SW 2001 4 20 HEEA072071 120010405G2560412070843105 SHOULDER BELT BELL 412 412 1182202SW COCKPIT FRAYED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R 36007 SHOULDER HARNESS WEB FRAYED. REPLACED WITH SERVICEABLE RESTRAINT. 1G72 4U H4SW 20010420001972001042000197SW 2001 4 20 HEEA072072 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 BEARING WORN. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010420001982001042000198SW 2001 4 20 HEEA072073 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 BEARING WORN. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010420001992001042000199SW 2001 4 20 HEEA072074 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 BEARING WORN. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010420002002001042000200SW 2001 4 20 HEEA072075 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 BEARING WORN. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010420002012001042000201SW 2001 4 20 HEEA072076 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 BEARING WORN. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010420002032001042000203SW 2001 4 20 HEEA072077 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 BEARING WORN. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010420002042001042000204SW 2001 4 20 HEEA072078 120010405G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 BEARING WORN. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010420002052001042000205 2001 4 20 HEEA072079 420010405G3452066106200 TRANSPONDER BELL 407 407 SW ATC MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03409PH 53059 LOW POWER AND WIDE PULSE WIDTH. PERFORMED PRELIMINARY INSPECTION AND FOUND F401 FUSE BLOWN AND Q415 BAD. REPLACED F401 FUSE AND Q415 TRANSISTOR. FOUND UNIT WILL NOT RECEIVE. REPLACED V101 CAVITY TUBE AND V301 PHOTOCELL. REPAIRED. BENCH CHECK GOOD. 1G71 3U O H2SW 20010420002062001042000206SW 2001 4 20 HEEA072080 120010405G3212206050248121 FLOAT BELL 206 206L4 1182110SW MLG FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW037074W 52033 L/H AFT FLOAT BAG FAILED 6 MONTH INSPECTION. SENT TO OFFSHORE HELICOPTER SUPPORT FOR WARRANTY REPAIR. 1G71 3U NCH2SW 20010420002072001042000207SW 2001 4 20 HEEA072081 120010405G6730206076062107 ACTUATOR BELL 206 206L3 1182108SW ROTOR SERVO SYS LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW038594X 51531 LEAKING. REPLACED WITH SERVICEABLE FLOAT. 1G71 3U H2SW 20010420002092001042000209 2001 4 20 HEEA072082 420010405G25613500145NL72 LIFE VEST BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 VEST WILL NOT HOLD AIR. SENT TO J.D. MANUFACTURING FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010420002102001042000210SW 2001 4 20 HEEA072083 120010405G6710C4264215 SERVO VALVE 206076062003BELL 206 206L3 1182108SW MAIN ROTOR STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW034282Z RH4128A 51499 SLIDE AND SLEEVE ASSY (SERVO VALVE) HAS STICKY MOVEMENT. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010420002112001042000211SW 2001 4 20 HEEA072084 120010405G712023069751 MOUNT BELL 407 407 SW ENGINE LOOSE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 ENGINE REAR MOUNT BEARING HAS PLAY. REPLACED WITH SERVICEABLE ASSY. 1G71 3U O H2SW 20010420002122001042000212SW 2001 4 20 HEEA072085 120010405G7120206062102013 MOUNT BELL 206 206B3 1181506SW ENGINE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107PH 2789 DAMAGED BEYOND LIMITS. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010420002132001042000213SW 2001 4 20 HEEA072086 120010405G7120206062103017 MOUNT BELL 206 206B3 1181506SW ENGINE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107PH 2789 DAMAGED BEYOND LIMITS. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010420002142001042000214SW 2001 4 20 HEEA072087 120010405G7120206062101101 MOUNT BELL 206 206B3 1181506SW ENGINE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107PH 2789 DAMAGED BEYOND LIMITS. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010420002152001042000215SW 2001 4 20 HEEA072088 120010405G7120206062101102 MOUNT BELL 206 206B3 1181506SW ENGINE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107PH 2789 DAMAGED BEYOND LIMITS. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010420002162001042000216SW 2001 4 20 HEEA072089 120010405G7120206062103018 MOUNT BELL 206 206B3 1181506SW ENGINE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107PH 2789 DAMAGED BEYOND LIMITS. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010420002172001042000217SW 2001 4 20 HEEA072090 120010405G7120206064107101 MOUNT BELL 206 206L1 1182107SW ENGINE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032124Z 45646 WORN BEARING. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010420002182001042000218 2001 4 20 HEEA072091 420010405G2312064101902 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW034835 51131 UNABLE TO TUNE AND TRANSMIT. PERFORMED PRELIMINARY INSPECTION AND TESTED. COULD NOT DUPLICATE PROBLEM. ADJUSTED C/N SQUELCH, CARRIER SQUELCH, MIC GAIN AND SIDETONE. BENCH CHECK GOOD. 1G71 3U H2SW 20010420002192001042000219 2001 4 20 HEEA072092 420010405G2312064101902 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0331077 51520 THE LARGE OUTER CHANNEL CHANGE KNOB INTERMITTENT. PERFORMED PRELIMINARY INSPECTION AND TESTED. REPLACED DISPLAY BOARD ASSY. REPAIRED PROBLEM. ADJUSTED C/N SQUELCH AND BENCH CHECK GOOD. 1G71 3U H2SW 20010420002202001042000220 2001 4 20 HEEA072093 420010405G2312064101905 TRANSCEIVER BELL 206 206L1 1182107SW VHF SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035007Y 45192 WILL NOT CHANGE FROM STANDBY TO IN USE AND VERY HARD TO CHANGE FREQUENCY FOR FIRST 20 TO 30 MINUTES OF FLIGHT. PERFORMED PRELIMINARY INSPECTION AND TESTED. ADJUSTED MIC GAIN AND SIDETONE. BENCH CHECK GOOD. COULD NOT DUPLICATE PROBLEM. 1G71 3U H2SW 20010420002212001042000221 2001 4 20 HEEA072094 420010405G2312064105430 TRANSCEIVER BELL 206 206L4 1182110SW VHF SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW037077F 52038 UNABLE TO CONTROL VOLUME. PERFORMED PRELIMINARY INSPECTION AND TESTED. REPLACED BAD S901. POTENTIOMETER SWITCH VOLUME REPAIRED. BENCH CHECK GOOD. 1G71 3U NCH2SW 20010420002222001042000222SW 2001 4 20 HEEA072095 120010405G7810 SUPPORT BRACKET BELL 412 412 1182202SW EXHAUST STACK CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03108X 33115 SUPPORT BRACKET AND SHROUD CRACKED. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010420002232001042000223SW 2001 4 20 HEEA072096 120010405G7810212061202007 EXHAUST STACK BELL 412 412 1182202SW ENGINE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0322608 33075 EXHAUST STACK IS CRACKED AT SEAMS OF DUCT HALVES. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010420002242001042000224SW 2001 4 20 HEEA072097 120010405G7810212061210001 DUCT BELL 412 412 1182202SW EXHAUST STACK CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 CRACKED. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010420002252001042000225 2001 4 20 HEEA072098 420010405G2312064101902 TRANSCEIVER BELL 206 206L1 1182107SW VHF SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0345RP 45521 DISPLAY INOPERATIVE. PERFORMED PRELIMINARY INSPECTION AND TESTED. FOUND DISPLAY A LITTLE WEAK. REPLACED DS501 DISPLAY. REPAIRED. ADJUSTED MIC GAIN AND SIDETONE. BENCH CHECK GOOD. 1G71 3U H2SW 20010420002262001042000226 2001 4 20 HEEA072099 420010405G2312064101902 TRANSCEIVER BELL 206 206L1 1182107SW VHF SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0345RP 45521 DISPLAY FLICKERS AND MEMORY RESETS. PERFORMED PRELIMINARY INSPECTION AND COULD NOT DUPLICATE PROBLEM. FOUND AUDIO LEVEL TO BE VERY LOW. REPLACED R505 VOLUME CONTROL AND CAPACITOR. ADJUSTED C/N SQUELCH, MODULATION AND SIDETONE. BENCH CHECK GOOD. 1G71 3U H2SW 20010420002272001042000227 2001 4 20 HEEA072100 420010405G2312064101902 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033116L 51529 DISPLAY TOO DIM AND SEVERAL LED DIGITS INOPERATIVE. PERFORMED PRELIMINARY INSPECTION AND FOUND DISPLAY BAD. REPLACED AND ADJUSTED C/N SQUELCH, MIC GAIN AND SIDETONE. BENCH CHECK GOOD. 1G71 3U H2SW 20010420002282001042000228 2001 4 20 HEEA072101 420010405G2312064101902 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0321497 51518 DISPLAY IS UNREADABLE ON HIGH HUMIDITY MORNINGS. REMOVED AND REPLACED DISPLAY. ADJUSTED AND ALIGNED CARRIER NOISE SQUELCH, CARRIER SQUELCH, MODULATION AND SIDETONE. BENCH CHECK GOOD. 1G71 3U H2SW 20010420002302001042000230 2001 4 20 HEEA072102 420010405G2312064101922 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0321497 51518 WILL NOT TRANSMIT OR RECEIVE. PERFORMED PRELIMINARY INSPECTION AND ADJUSTED CARRIER NOISE SQUELCH, CARRIER SQUELCH, AND SIDETONE. BENCH CHECK GOOD. 1G71 3U H2SW 20010420002312001042000231 2001 4 20 HEEA072103 420010405G2312064105430 TRANSCEIVER BELL 206 206B3 1181506SW VHF SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032277A 3630 RADIO TOTALLY INOPERATIVE. WON''''T TURN ON. PERFORMED PRELIMINARY INSPECTION AND TESTED. COULD NOT DUPLICATE PROBLEM. ADJUSTED SIDETONE. REPLACED FADED DISPLAY LENS. BENCH CHECK GOOD. 1G71 3U H2SW 20010420002322001042000232 2001 4 20 HEEA072104 420010405G2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0321497 51518 FLIPPING FROM USE TO STANDBY. PERFORMED PRELIMINARY INSPECTION AND TESTED. COULD NOT DUPLICATE PROBLEM. ADJUSTED FREQUENCY AND SIDETONE. BENCH CHECK GOOD. 1G71 3U H2SW 20010420002342001042000234SW 2001 4 20 HEEA072108 120010406G6220407310100103 DAMPER BELL 407 407 SW MAIN ROTOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 CORROSION IN SHEAR BEARING BORE. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR 715116. LABOR CREDIT ACCOMPLISHED ON J0151671-WA (INVOICE AND DMR NO. 687009. 1G71 3U O H2SW 20010420002352001042000235SW 2001 4 20 HEEA072109 120010406G6220407310101101 BEARING BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 BEARING WORN. SERIAL NUMBERS REMOVED ARE LP6967, LP6611, LP6567 AND LP6625. 1G71 3U O H2SW 20010420002402001042000240SW 2001 4 20 HEEA072112 120010406G6230 SEAL BELL 407 407 SW MAIN ROTOR FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03722PH1687 A874 53288 SWASHPLATE HAS A BLOWN GREASE SEAL. 1G71 3U O H2SW 20010420002412001042000241SW 2001 4 20 HEEA072113 120010406G6720407375024101 CONTROL UNIT BELL 407 407 SW TAIL ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03740PH291 53435 CAUSES PEDAL STOP TO ENGAGE INTERMITTENTLY WITHOUT ELECTRICAL OR MECHANICAL INPUT. 1G71 3U O H2SW 20010420002422001042000242SW 2001 4 20 HEEA072114 120010406G6320407040006107FM TRANSMISSION BELL 407 407 SW MAIN ROTOR MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH3132 53142 CHIP LIGHT HISTORY, POSSIBLY MAKING METAL. 1G71 3U O H2SW 20010420002432001042000243SW 2001 4 20 HEEA072115 120010406G6300407340339103 BEARING PHIPBH40701 BELL 407 407 SW OIL COOLER ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH PHI0002 53199 OIL COOLER BLOWER BEARINGS ARE ROUGH. SERIAL NUMBERS REMOVED ARE E99-0635 AND E99-0696. 1G71 3U O H2SW 20010420002502001042000250SW 2001 4 20 HEEA072116 120010406G6510407340339103 BEARING 407040302107BELL 407 407 SW T/R DRIVESHAFT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH440 A1942 53397 WORN. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR# 71506402. LABOR CREDIT ACCOMPLISHED ON J0147760-WA (INVOICE AND DMR NO. 686974). 1G71 3U O H2SW 20010420002512001042000251SW 2001 4 20 HEEA072117 120010406G6300407340339101 BEARING PHIPBH40701 BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH PHI0014 53397 OIL COOLER BLOWER BEARINGS ARE WORN. SERIAL NUMBERS REMOVED ARE ZV10128 AND ZV10209. 1G71 3U O H2SW 20010420002522001042000252SW 2001 4 20 HEEA072118 120010406G6510407340339101 BEARING 407040302107BELL 407 407 SW T/R DRIVESHAFT OVERHEATED E HEEAK NONE M OVER TEMP ININSP/MAINT 1 SW03495PH A1937 53397 TAIL ROTOR DRIVESHAFT BEARINGS OVERHEATED. 1G71 3U O H2SW 20010420002532001042000253SW 2001 4 20 HEEA072119 120010406G7810407063001101 EXHAUST STACK BELL 407 407 SW ENGINE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH 53400 EXHAUST STACK CRACKED. 1G71 3U O H2SW 20010420002542001042000254SW 2001 4 20 HEEA072120 120010406G6510407340340101 DISC PACK BELL 407 407 SW T/R DRIVE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH 53397 TAIL ROTOR DISC PACK CRACKED. 1G71 3U O H2SW 20010420002552001042000255SW 2001 4 20 HEEA072121 120010406G6300407340339103 BEARING 407040302101BELL 407 407 SW T/R DRIVESHAFT OVERHEATED E HEEAK NONE M OVER TEMP ININSP/MAINT 1 SW03491PH A15 53386 BEARING ON TAIL ROTOR DRIVESHAFT OVERHEATED. 1G71 3U O H2SW 20010420002622001042000262SW 2001 4 20 HEEA072122 120010406G6710406010407101 IDLER LINK BELL 407 407 SW COLLECTIVE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH1913 53207 COLLECTIVE IDLER LINK IS EXCESSIVELY WORN. 1G71 3U O H2SW 20010420002632001042000263SW 2001 4 20 HEEA072123 120010406G6230206010408001 PIN BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 MAIN ROTOR PIVOT PIN IS EXCESSIVELY WORN. 1G71 3U O H2SW 20010420002642001042000264SW 2001 4 20 HEEA072124 120010406G6300406310405101 UNIVERSAL JOINT BELL 407 407 SW MAIN ROTOR DRIVEWORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03417PH2066 53038 UNIVERSAL JOINT ON MAIN ROTOR DRIVE IS EXCESSIVELY WORN. 1G71 3U O H2SW 20010420002652001042000265SW 2001 4 20 HEEA072125 120010406G7400407375038101 GUARD BELL 407 407 SW START SWITCH BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH 53397 START SWITCH GUARD BROKEN. 1G71 3U O H2SW 20010420002662001042000266SW 2001 4 20 HEEA072126 120010406G6320B4749 CHIP DETECTOR BELL 407 407 SW ENGINE GEARBOX LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03402PH 53159 ENGINE GEARBOX CHIP DETECTOR IS LEAKING. 1G71 3U O H2SW 20010420002692001042000269SW 2001 4 20 HEEA072127 120010406G6322206061432121 HOUSING BELL 407 407 SW COOLLER BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH 53159 COOLER BLOWER HOUSING IS CRACKED. 1G71 3U O H2SW 20010420002702001042000270 2001 4 20 HEEA072128 420010406G3120M803B205VBATT CLOCK BELL 407 407 SW COCKPIT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03741PH28 53457 SELECT BUTTON MISSING. 1G71 3U O H2SW 20010420002712001042000271SW 2001 4 20 HEEA072130 120010406G6510407340339101 BEARING PHIPBH40701 BELL 407 407 SW OILCOOLER BLOWEROVERHEATED E HEEAK NONE M OVER TEMP ININSP/MAINT 1 SW03402PH PHI0032 53159 OIL COOLER BLOWER BEARINGS OVERHEATED. 1G71 3U O H2SW 20010420002722001042000272 2001 4 20 HEEA072131 420010406G2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038591X 51495 RADIO FEEDS BACK INTO HEADSET WHEN TRANSMITTING ON OTHER VHF RADIO SYSTEM IN AIRCRAFT. PERFORMED PRELIMINARY INSPECTION. ADJUSTED CARRIER AND CARRIER/NOISE SQUELCH. BENCH CHECK GOOD. 1G71 3U H2SW 20010420002732001042000273 2001 4 20 HEEA072132 420010406G2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 VHF TRANSCEIVER DISPLAY FAILED. 1G71 3U H2SW 20010420000012001042000001 2001 4 20 HEEA072133 420010406G2312064105430 TRANSCEIVER BELL 206 206L1 1182107SW VHF SYSTEM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033904L 45597 VHF TRANSCEIVER BREAKS SQUELCH. 1G71 3U H2SW 20010420000022001042000002 2001 4 20 HEEA072134 420010406G3452066106200 TRANSCEIVER BELL 206 206L1 1182107SW ATC MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035745S 45491 NR F2. PULSE. LOW OUTPUT POWER. LOW RESPONSE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000032001042000003 2001 4 20 HEEA072135 420010406G345713824120234 GPS BELL 206 206L1 1182107SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0345RP 45521 TIME ENROUTE PAGE INOPERATIVE. PERFORMED PRELIMINARY INSPECTION AND TESTED. COULD NOT DUPLICATE PROBLEM BUT FOUND UNIT WOULD FAIL GPS TEST. RESET MEMORY AND REPROGRAMMED. FOUND CRYSTAL OFFSET OUT OF SPECS. ADJUSTED CRYSTAL FREQUENCY TO SPECS. REPAIRED PROBLEM. BENCH CHECK GOOD. 1G71 3U H2SW 20010420000042001042000004 2001 4 20 HEEA072136 420010406G345713824120234 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 DROPS ALL WAYPOINTS. PERFORMED PRELIMINARY INSPECTION AND TESTED. COULD NOT DUPLICATE PROBLEM. REPLACED BAD ENT BUTTON SWITCH AND BAD KEY CAPS. BENCH CHECK GOOD. 1G71 3U H2SW 20010420000052001042000005 2001 4 20 HEEA072137 420010406G345713824120234 GPS BELL 206 206L1 1182107SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032135V 45657 WILL NOT COME ON LINE. PERFORMED PRELIMINARY INSPECTION AND FOUND BATTERY DEAD AGAIN. SENT TO TRIMBLE NAVIGATION FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010420000062001042000006 2001 4 20 HEEA072138 420010406G345713824020109 GPS BELL 206 206L1 1182107SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032124Z 45646 INOPERATIVE WILL NOT PASS CMM5 6-11. SENT TO TRIMBLE NAVIGATION FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010420000072001042000007 2001 4 20 HEEA072139 420010406G345713824120234 GPS BELL 206 206B3 1181506SW COCKPIT DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322751 3627 BATTERY WEAK. SENT TO TRIMBLE NAVIGATION FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010420000082001042000008 2001 4 20 HEEA072140 420010406G345713824120234 GPS BELL 206 206B3 1181506SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032270G 3610 ENTER BUTTON STICKS IN. SENT TO TRIMBLE NAVIGATION FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010420000092001042000009 2001 4 20 HEEA072141 420010406G345713824120234 GPS BELL 206 206B3 1181506SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032270G 3610 MUST INPUT CODE EVERYTIME UNIT IS TURNED ON. UNIT ONLY PICKS UP ONE OR TWO SATELLITES WHEN ANOTHER UNIT WILL PICK UP SEVEN OR EIGHT IN THE SAME AIRCRAFT. UNIT ALSO INTERMITTENTLY RESTARTS, CHANGES MODES WHILE WAITING FOR IT TO PICK UP MORE SATELLITES INTERMITTENTLY. SENT TO TRIMBLE NAVIGATION FOR WARRANTY REPAIR. 1G71 3U H2SW 20010420000102001042000010 2001 4 20 HEEA072142 420010406G345713824120234 GPS BELL 206 206B3 1181506SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032753F 2729 BUTTONS HARD TO PRESS. SENT TO TRIMBLE NAVIGATION FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010420000112001042000011 2001 4 20 HEEA072143 420010406G345713824120234 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03129MR 51129 FLASHES WARNING. SENT TO TRIMBLE NAVIGATION FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010420000122001042000012 2001 4 20 HEEA072144 420010406G345713824120234 GPS BELL 206 206L1 1182107SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035014Y 45219 CANNOT SET TIME. SENT TO TRIMBLE NAVIGATION FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010420000132001042000013 2001 4 20 HEEA072145 420010406G345713824120234 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0332041 51539 WILL NOT HOLD HEADING. SENT TO TRIMBLE NAVIGATION FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010420000142001042000014 2001 4 20 HEEA072146 420010406G345713824120234 GPS BELL 206 206L1 1182107SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032759U 45272 NO MEMORY. SENT TO TRIMBLE NAVIGATION FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010420000152001042000015 2001 4 20 HEEA072147 420010406G345713824120234 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0349EA 1382 51507 WILL NOT LOCATE ITSELF. SENT TO TRIMBLE NAVIGATION FOR WARRANTY REPAIR. 1G71 3U H2SW 20010420000162001042000016SW 2001 4 20 HEEA072148 120010406G6710206001564001 WEB BELL 206 206L3 1182108SW SERVO SUPPORT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341791 51465 OUTBOARD AND INBOARD FORWARD SERVO WEB MOUNT LUGS ARE BEING WORN BY THE SERVO FORWARD ROD END BEARING DUE TO ROCKING MOTION OF THE SERVO. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000172001042000017SW 2001 4 20 HEEA072149 120010406G6710206001564001 WEB BELL 206 206L3 1182108SW SERVO MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206FS 51506 OUTBOARD FORWARD SERVO MOUNT LUGS ARE BEING WORN BY THE SERVO FORWARD ROD END BEARING DUE TO ROCKING MOTION OF THE SERVO. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000182001042000018SW 2001 4 20 HEEA072150 120010406G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0353119 51575 EXHAUST ASSY CRACKED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000192001042000019SW 2001 4 20 HEEA072151 120010406G7120206033201163A MOUNT BELL 206 206L3 1182108SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 CRACKED AT ENGINE MOUNT BOLT HOLE AREA. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000202001042000020SW 2001 4 20 HEEA072152 120010406G7120206064103001 BEARING BELL 206 206L3 1182108SW ENGINE MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0353119 51575 ENGINE MOUNT BEARING WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000212001042000021SW 2001 4 20 HEEA072153 120010406G7120206064105001 MOUNT BELL 206 206L3 1182108SW ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341791 51465 MECHANICAL DAMAGE BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000222001042000022SW 2001 4 20 HEEA072154 120010406G7120206064105002 MOUNT BELL 206 206L3 1182108SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206LS 51070 ENGINE MOUNT CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000232001042000023SW 2001 4 20 HEEA072155 120010406G7120206064105101 MOUNT BELL 407 407 SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03436PH 51436 ENGINE MOUNT TUBE PITTED ON INSIDE. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20010420000242001042000024SW 2001 4 20 HEEA072156 120010406G7120206064105101 MOUNT BELL 206 206L3 1182108SW ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 ENGINE MOUNT HAS MECHANICAL DAMAGE BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000252001042000025SW 2001 4 20 HEEA072157 120010406G7120206064105102 MOUNT BELL 407 407 SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03436PH 51436 ENGINE MOUNT TUBE PITTED ON INSIDE. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20010420000262001042000026SW 2001 4 20 HEEA072158 120010406G7120206064105102 MOUNT BELL 206 206L3 1182108SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 ENGINE MOUNT HAS MECHANICAL AND CORROSION DAMAGE BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000272001042000027SW 2001 4 20 HEEA072159 120010406G7120206064106001 MOUNT BELL 206 206L3 1182108SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206LS 51070 ENGINE MOUNT IS CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000282001042000028SW 2001 4 20 HEEA072160 120010406G7120206064106001 MOUNT BELL 407 407 SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03436PH 51436 ENGINE MOUNT TUBE PITTED ON INSIDE. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20010420000292001042000029SW 2001 4 20 HEEA072161 120010406G7120206064106101 MOUNT BELL 206 206L3 1182108SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 ENGINE MOUNT HAS PITTED CORROSION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000302001042000030SW 2001 4 20 HEEA072162 120010406G7120206064107001 MOUNT BELL 206 206L3 1182108SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206LS 51070 ENGINE MOUNT IS CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000362001042000036SW 2001 4 20 HEEA072163 120010406G7120206064107003 MOUNT BELL 206 206L3 1182108SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206LS 51070 ENGINE MOUNT IS CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000372001042000037SW 2001 4 20 HEEA072164 120010406G7120206064107101 MOUNT BELL 407 407 SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03436PH 51436 ENGINE MOUNT TUBE PITTED ON INSIDE. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20010420000382001042000038SW 2001 4 20 HEEA072165 120010406G7120206064107101 MOUNT BELL 206 206L3 1182108SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341791 51465 ENGINE MOUNT HAS CORROSION DAMAGE BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000392001042000039SW 2001 4 20 HEEA072166 120010406G7120206064107101 MOUNT BELL 206 206L3 1182108SW ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 ENGINE MOUNT HAS MECHANICAL DAMAGE BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000402001042000040SW 2001 4 20 HEEA072167 120010406G7120 BEARING BELL 206 206L3 1182108SW ENGINE MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032619 51375 LEG HAS WORN BEARING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000412001042000041SW 2001 4 20 HEEA072168 120010406G7120206064107103 MOUNT BELL 407 407 SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03436PH 51436 ENGINE MOUNT TUBE PITTED ON INSIDE. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20010420000422001042000042SW 2001 4 20 HEEA072169 120010406G7120206064107103 MOUNT BELL 206 206L3 1182108SW ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 ENGINE MOUNT HAS CORROSION DAMAGE BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000432001042000043SW 2001 4 20 HEEA072170 120010406G7120 BEARING BELL 206 206L3 1182108SW ENGINE MOUNT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032619 51375 LEG HAS WORN BEARING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000442001042000044SW 2001 4 20 HEEA072171 120010406G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 EXHAUST STACK IS CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000452001042000045SW 2001 4 20 HEEA072172 120010406G2560206072841111 SEAT BELT BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 SEAT BELT REEL WILL NOT RETRACT. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000462001042000046SW 2001 4 20 HEEA072173 120010406G2560206072841111 SEAT BELT BELL 206 206L3 1182108SW COCKPIT STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381671 51301 SEAT BELT STICKS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000472001042000047SW 2001 4 20 HEEA072174 120010406G2560206072841115 SEAT BELT BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 SEAT BELT REEL WILL NOT RETRACT. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000482001042000048SW 2001 4 20 HEEA072175 120010406G2560206072841115 SEAT BELT BELL 206 206L3 1182108SW COCKPIT STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0381671 51301 SEAT BELT STICKS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010420000492001042000049EU 2001 4 20 HEEA072176 120010403G2432RG355 BATTERY SNIAS 350 AS350B 8680801EU DC SYSTEM DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03972AE225 3234 ENGINE SLOW TO START. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H9EU 20010420000502001042000050EU 2001 4 20 HEEA072177 120010403G621010581013 BLADE BOLKMS105 BO105S 5626006EU MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724MB3401 S756 NR 1 INBOARD STRIP HAS SEPARATION ON THE OUTBOARD END OF THE ABRASION STRIP. 1G72 3U H3EU 20010420000512001042000051EU 2001 4 20 HEEA072178 120010405G781010560186 EXHAUST PIPE BOLKMS105 BO105S 5626006EU ENGINE CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724MB S756 RUST PITS THROUGH STACK AT MOUNT FLANGE. REPLACED WITH SERVICEABLE PART. 1G72 3U H3EU 20010507005482001050700548NE 2001 5 7 HEEA072350 120010409G2460A1077B RELAY SKRSKYS76 S76A 8143006NE ELECTRICAL SYS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034253S 760035 ESSENTIAL BUSS READS LOW VOLTAGE. 1G72 3U H1NE 20010507005492001050700549NE 2001 5 7 HEEA072351 120010410G71607630207028059 SCREEN SKRSKYS76 S76C 8143008NE ENGINE INTAKE BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03505PH 760505 WIRE MESH HAS WIRE BROKEN. SCRAPPED AND REPLACED WITH SERVICEABLE SCREEN. 1G72 3U NCH1NE 20010507005502001050700550 2001 5 7 HEEA072352 420010411G34578143902240B GPS SKRSKYS76 S76A 8143006NE COCKPIT INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW034253S 760035 GPS INOPERATIVE. FOUND UNIT WOULD INTERMITTENLY TURN OFF BY ITSELF THEN TURN BACK ON AND SELF TEST AGAIN. 1G72 3U H1NE 20010507005512001050700551NE 2001 5 7 HEEA072353 120010411G79217630807901105 OIL COOLER SKRSKYS76 S76A 8143006NE ENGINE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW031546G 760076 OIL COOLER CAUSING HIGH OIL TEMP. 1G72 3U H1NE 20010515001082001051500108 2001 5 15 HEEA072354 420010411G34446223201001 INDICATOR BEECH 200 200BEECH 1152920CE RADIO ALTIMETER INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW0330PH BB635 NO INDICATIONS IN FLIGHT. 1L72 4T A24CE 20010507005902001050700590 2001 5 7 HEEA072355 420010409G3445MI585200 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 BURNED OUT 3 INDICATORS. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT DOES NOT POWER UP. FOUND Q604, Q605 BAD ON POWER SUPPLY. REPLACED Q604, Q605. REPAIRED. ADJUSTED TO SPECS. BENCH CHECK GOOD. 1G72 4U H4SW 20010507005912001050700591 2001 5 7 HEEA072356 420010409G3445MI585200 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 SCREEN ROLLS THEN GOES BLANK. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT DOES NOT POWER UP. REPLACED Q604, Q605. REPAIRED. ADJUSTED TO SPECS. BENCH CHECK GOOD. 1G72 4U H4SW 20010507005922001050700592 2001 5 7 HEEA072357 420010409G3445MI585200 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 INOPERATIVE. NO NOISE BAND DURING TEST. PERFORMED PRELIMINARY INSPECTION. COULD NOT DUPLICATE. ADJUSTED STC AND GAIN VOLTAGE. BENCH CHECK GOOD. 1G72 4U H4SW 20010507005932001050700593 2001 5 7 HEEA072358 420010409G3445MI585200 RADAR BELL 412 412 1182202SW COCKPIT SHORTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 SHORTED INTERNALLY. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT DOES NOT TURN ON. REPLACED Q601, Q602, Q604, Q605 ON POWER SUPPLY. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20010507005942001050700594 2001 5 7 HEEA072359 420010409G3445MI585200 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW033893P 33012 GAPS IN TEST PATTERN. PERFORMED PRELIMINARY INSPECTION. FOUND R/T TRANSMITTING POWER OUT INTERMITTENT. REPLACED MAGNETRON. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20010507005952001050700595 2001 5 7 HEEA072360 420010409G3445MI585200 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 PICTURE SCREEN SIZE FLUCTUATES AND ERRATIC. PERFORMED PRELIMINARY INSPECTION. TROUBLESHOT AND FOUND BAD HIGH VOLTAGES. REPLACED Q604 AND Q605. REPAIRED HIGH VOLTAGE PROBLEM. DISPLAY SLIGHTLY DISTORTED, REPLACED STABILIZATION BOARD, REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002022001050800202 2001 5 8 HEEA072361 420010409G3445MI585200 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 UNIT WILL NOT POWER UP. PERFORMED PRELIMINARY INSPECTION. TROUBLESHOT AND REPLACED F202 FUSE. ADJUSTED STC AND GAIN VOLTAGE. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002032001050800203 2001 5 8 HEEA072362 420010409G3445MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 FAILS TARGETS AT HIGH RANGE SETTINGS. PERFORMED PRELIMINARY INSPECTION. FOUND MANUAL GAIN SET TOO HIGH, SHOWING FALSE TARGETS. ADJUSTED ANC, MANUAL GAIN AND COLORS. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002042001050800204 2001 5 8 HEEA072363 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 RADAR SYSTEM WOULD NOT POWER UP. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT NOT POWERING UP. FOUND BURNT FOIL ON SWITCH PANEL. REPAIRED FOIL AND BENCH CHECK GOOD. 1G72 4U H4SW 20010508002052001050800205 2001 5 8 HEEA072364 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 NO INDICATION, BLANK SCREEN. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT NOT DRAW AMPS. REPLACED Q4204, Q4205 TRANSISTORS ON POWER SUPPLY. REPAIRED. ADJUSTED UNIT TO SPECS. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002062001050800206 2001 5 8 HEEA072365 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 DOES NOT INDICATE. PERFORMED PRELIMINARY INSPECTION. COULD NOT DUPLICATE. ADJUSTED COLORS, ANC AND MANUAL GAIN. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002072001050800207 2001 5 8 HEEA072366 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 BLANK SCREEN. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT DRAWS EXCESSIVE CURRENT. REPLACED Q4204, Q4205 TRANSISTORS ON POWER SUPPLY. REPAIRED. FOUND RED AND YELLOW COLORS IN NOISE BAND. REPLACED IC U1402, U1403, U1406. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002082001050800208 2001 5 8 HEEA072367 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 WILL NOT COME ON BUT WILL POWER UP. PERFORMED PRELIMINARY INSPECTION. FOUND DISPLAY FADES IN AND OUT. CLEANED ALL BOARDS AND PINS. FOUND CORROSION ON MEMORY BOARD CONNECTOR. CLEANED CORROSION. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002092001050800209 2001 5 8 HEEA072368 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 CYCLES ON AND OFF. FLICKERS MOST OF THE TIME AND DOES NOT BRING UP PICTURE. PERFORMED PRELIMINARY INSPECTION. COULD NOT VERIFY COMPLAINT. ADJUSTED ANC AND INTENSITY. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002102001050800210 2001 5 8 HEEA072369 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 LEFT SIDE OF DISPLAY WILL NOT DIM. PERFORMED PRELIMINARY INSPECTION. COULD NOT VERIFY COMPLAINT. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002112001050800211 2001 5 8 HEEA072370 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 TOP HALF OF DISPLAY DISTORTED. PERFORMED PRELIMINARY INSPECTION. REPLACED SOCKET PINS ON VARIOUS CONNECTORS. REPLACED CRT ASSEMBLY. ALIGNED TO SPECS. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002122001050800212 2001 5 8 HEEA072371 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 SCREEN WENT BLANK. PERFORMED PRELIMINARY INSPECTION. FOUND DISPLAY SHRUNK ON SCREEN. REPLACED R133 AND Q1318 ON VIDEO BOARD. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002132001050800213 2001 5 8 HEEA072372 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 COLORS INCORRECT ON TEST MODE. TEST UNSTABLE INTERMITTENTLY. PERFORMED PRELIMINARY INSPECTION. COULD NOT VERIFY COMPLAINT. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002142001050800214 2001 5 8 HEEA072373 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 SCREEN TURNS BLUE. PERFORMED PRELIMINARY INSPECTION. FOUND HIGH VOLTAGE POWER SUPPLY CAUSING LOUD POPPING NOISE. REPLACED HIGH VOLTAGE POWER SUPPLY. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002152001050800215 2001 5 8 HEEA072374 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 VIDEO IS WAVY. SCREEN IS BLANK ON THE TOP AND BOTTOM. PERFORMED PRELIMINARY INSPECTION. FOUND DISPLAY BLANKS OUT AND COLORS FADE IN AND OUT. FOUND IC U1241 BAD ON TIMING BOARD. REPLACED IC U1241. REPAIRED. ALSO REPLACED 30 EACH SOCKET PINS ON CONNECTORS. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002162001050800216 2001 5 8 HEEA072375 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 INOPERATIVE. NO DISPLAY ON SCREEN. PERFORMED PRELIMINARY INSPECTION. COULD NOT VERIFY COMPLAINT. CLEANED SLIGHT CORROSION ON BOARDS AND CONNECTORS. ADJUSTED TO SPECS. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002172001050800217 2001 5 8 HEEA072376 420010409G3442MI5852013 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 DISPLAY ERRATIC. PERFORMED PRELIMINARY INSPECTION. REPLACED P1201 CONNECTOR AND CLEANED CORROSION FROM PINS ON SEVERAL CONNECTORS. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002182001050800218 2001 5 8 HEEA072377 420010409G3442MI585202 ANTENNA BELL 412 412 1182202SW RADAR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 WILL NOT HOLD PROPER TILT. PERFORMED PRELIMINARY INSPECTION. COULD NOT DUPLICATE. BENCH CHECK GOOD. 1G72 4U H4SW 20010508002192001050800219 2001 5 8 HEEA072378 420010409G2561PHI10090 LIFE VEST BELL 412 412 1182202SW CABIN LEAKING E HEEAK NONE L NO TEST ININSP/MAINT 1 SW037128R 36007 LEAKS. SENT TO J.D. MANUFACTURING FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20010508002202001050800220 2001 5 8 HEEA072379 420010409G3442MI585202 ANTENNA BELL 412 412 1182202SW RADAR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 WILL NOT SHOW SWEEP AND NO TARGETS DISPLAYED. REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010508002212001050800221SW 2001 5 8 HEEA072380 120010409G5260PHI101741 STEP BELL 412 412 1182202SW RIGHT STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 RIGHT STEP STUCK IN STOW POSITION. REPLACED WITH SERVICEABLE UNIT. 1G72 4U H4SW 20010508002222001050800222SW 2001 5 8 HEEA072381 120010409G2510222320823119 SEAT BELT BELL 206 206L3 1182108SW COCKPIT DAMAGED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW0331077 51520 BAD SHOULDER HARNESS TENSION ADJUSTERS BACKWARDS AND RUB AGAINST BODY AND CANNOT BE ADJUSTED. 1G71 3U H2SW 20010508002232001050800223 2001 5 8 HEEA072382 420010409G34225040017901 INDICATOR BELL 206 206L3 1182108SW ATTITUDE FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0330KH 51527 WOULD NOT ERECT. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20030815000112003081500011SW 2003 8 15 HEEA072383 120010409G2820206063650001 VALVE BELL 206 206L1 1182107SW FUEL SYSTEM LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW035019F 45244 LEAKING FUEL VALVE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508002242001050800224SW 2001 5 8 HEEA072384 120010409G7120206064107109 LEG ASSY BELL 206 206L3 1182108SW ENGINE MOUNT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW0342EA 51542 BEARING WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508002252001050800225SW 2001 5 8 HEEA072385 120010409G7810206064203101 DUCT BELL 206 206L3 1182108SW EXHAUST CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0342EA 51542 CRACKED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508002262001050800226SW 2001 5 8 HEEA072386 120010409G2510206072841113 SEAT BELT BELL 206 206L3 1182108SW COCKPIT STUCK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW034835 51131 INERTIA REEL RATCHETY AND INTERMITTENTLY STICKS WHEN EXTENDING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508002272001050800227SW 2001 5 8 HEEA072387 120010409G2913206076030101 PUMP BELL 206 206L3 1182108SW HYD SYSTEM NOISY E HEEAK NONE E VIBRATION/BUFFET ININSP/MAINT 1 SW0330KH 51527 NOISE COMING FROM HYDRAULIC SYSTEM DURING CRUISE AND ON APPROACHES INTERMITTENT. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508002282001050800228SW 2001 5 8 HEEA072388 120010409G3212206050247109 COVER BELL 206 206L1 1182107SW FLOAT LOOSE E HEEAK NONE O OTHER ININSP/MAINT 1 SW035007Q 45187 LEFT AFT FLOAT COVER FLAP VELCRO HAS COME LOOSE FROM COVER. STITCHING CAME OUT. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508002292001050800229SW 2001 5 8 HEEA072389 120010409G3210206323018 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 CORROSION PITS UNDER SADDLE MOUNTS. SCRAPPED AND REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20010508002302001050800230SW 2001 5 8 HEEA072390 120010409G2824205060612003 VALVE BELL 412 412 1182202SW FUEL SYSTEM BYPASSING E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R 36007 ALLOWS FUEL TO BYPASS IN THE CLOSED POSITION. SENT TO ITT AEROSPACE FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20010508002312001050800231SW 2001 5 8 HEEA072391 120010409G2844209062003001 SWITCH BELL 412 412 1182202SW FUEL SYSTEM MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 LOW PRESSURE LIGHT WILL NOT COME ON. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002322001050800232SW 2001 5 8 HEEA072392 120010409G2844209062003001 SWITCH BELL 412 412 1182202SW FUEL SYSTEM LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW033893L 33006 LEAKING THROUGH SWITCH BODY. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002332001050800233SW 2001 5 8 HEEA072393 120010409G2844209062003001 SWITCH BELL 412 412 1182202SW FUEL SYSTEM MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R 36007 C-BOX PRESSURE LIGHT ILLUMINATES INTERMITTENTLY AND REMAINS ON 1 TO 2 MINUTES, THEN GOES OUT. C-BOX OIL PRESSURE REMAINS STEADY. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002342001050800234SW 2001 5 8 HEEA072394 120010409G7810212061201011 EJECTOR BELL 412 412 1182202SW ENGINE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002352001050800235SW 2001 5 8 HEEA072395 120010409G7810212061201012 EJECTOR BELL 412 412 1182202SW EXHAUST CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 CRACKED AT MOUNTING PADS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002362001050800236SW 2001 5 8 HEEA072396 120010409G7810212061210001 DUCT BELL 412 412 1182202SW EXHAUST CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002372001050800237 2001 5 8 HEEA072397 420010409G3413212070239001 INDICATOR BELL 412 412 1182202SW COCKPIT VSI ERRATIC E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R 36007 ERRATIC READINGS FAILED STATIC CHECK. 1G72 4U H4SW 20010508002382001050800238 2001 5 8 HEEA072398 420010409G3413212070239001 INDICATOR BELL 412 412 1182202SW COCKPIT VSI ERRATIC E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R 36007 ERRATIC ABOVE 2000 FEET MSL. 1G72 4U H4SW 20010508002392001050800239SW 2001 5 8 HEEA072399 120010409G5260212070418105 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW035759N 33002 STEP ACTUATOR DOES NOT FUNCTION. 1G72 4U H4SW 20010508002402001050800240SW 2001 5 8 HEEA072400 120010409G7714212075037101 INDICATOR BELL 412 412 1182202SW N1 ERRATIC E HEEAK NONE O OTHER ININSP/MAINT 1 SW033911L 33023 BOUNCES ERRATICALLY. 1G72 4U H4SW 20010508002412001050800241SW 2001 5 8 HEEA072401 120010409G5260212075418103 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R 36007 ROD BROKEN ON ACTUATOR AND IS INOPERATIVE. 1G72 4U H4SW 20010508002422001050800242SW 2001 5 8 HEEA072402 120010409G5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893N 33010 STEP WILL NOT RETRACT. 1G72 4U H4SW 20010508002432001050800243SW 2001 5 8 HEEA072403 120010409G5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP FROZEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 STEP ACTUATOR FROZEN. 1G72 4U H4SW 20010508002442001050800244SW 2001 5 8 HEEA072404 120010409G2510214070966101 SEAT BELT BELL 412 412 1182202SW COCKPIT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 END UNSTITCHED. 1G72 4U H4SW 20010508002452001050800245SW 2001 5 8 HEEA072405 120010409G2510214070966101 SEAT BELT BELL 412 412 1182202SW COCKPIT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 END UNSTITCHED. 1G72 4U H4SW 20010508002462001050800246SW 2001 5 8 HEEA072406 120010409G6420412010418105 BEARING BELL 412 412 1182202SW MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 PITTING ON RACE. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT. 1G72 4U H4SW 20010508002472001050800247SW 2001 5 8 HEEA072407 120010409G5320206033201167S STIFFENER BELL 206 206L1 1182107SW FUSELAGE BENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 STIFFENER CHANNELS ARE NOT BENT CORRECTLY. U-CHANNEL VERTICAL FLANGES ARE SUPPOSED TO BE BENT UP 90 DEGREES. THE FLANGES ON THESE TWO CHANNELS ARE 85 DEGREES AND 95 DEGREES. THIS CAUSES THE FITTING, P/N 206-031-629-103 TO BE INSTALLED AT AN ANGLE, AND WILL CAUSE THE ENGINE MOUNT BOLT TO BE INSTALLED AT AN ANGLE THROUGH THE BULKHEAD. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT. 1G71 3U H2SW 20010508002482001050800248SW 2001 5 8 HEEA072408 120010409G7714214074280107 DETECTOR BELL 412 412 1182202SW RPM LIMIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 RPM WARNING LIGHT FLICKERS ON AND OFF AROUND 75 PERCENT N2. 1G72 4U H4SW 20010508002492001050800249 2001 5 8 HEEA072409 420010409G3424214075244001 GYRO BELL 412 412 1182202SW TURN RATE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 TURN NEEDLE OSCILLATES. 1G72 4U H4SW 20010508002502001050800250SW 2001 5 8 HEEA072410 120010409G5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 DOES NOT WORK. 1G72 4U H4SW 20010508002512001050800251SW 2001 5 8 HEEA072411 120010409G5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 STEP WILL NOT EXTEND. 1G72 4U H4SW 20010508002522001050800252 2001 5 8 HEEA072412 420010409G3424214075244001 GYRO BELL 412 412 1182202SW RATE OF TURN INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 NO RATE OF TURN INDICATION. 1G72 4U H4SW 20010508002532001050800253 2001 5 8 HEEA072413 420010409G3424214075244001 GYRO BELL 412 412 1182202SW RATE OF TURN INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 TURN NEEDLE IS INOPERATIVE. 1G72 4U H4SW 20010508002542001050800254SW 2001 5 8 HEEA072414 120010409G52302353 HANDLE BELL 412 412 1182202SW CARGO DOOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 HEAT COATING WORN OFF BAGGAGE DOOR HANDLE. HANDLE LOOSE ON IT''S SHAFT. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002552001050800255NE 2001 5 8 HEEA072415 220010409G732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE FREE TURBINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 N2 WILL NOT REACH 100 PERCENT. FOUND INTERIOR OF UNIT VERY DIRTY. TEFLON TUBE WAS WORN. REPLACED TEFLON TUBE WITH NEW PART AND CLEANED INTERIOR PARTS. 1G72 4U4 U H4SW E22EA 20010508002562001050800256NE 2001 5 8 HEEA072416 220010409G732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE FREE TURBINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 N2 WENT HIGH WITH THROTTLE AT IDLE. FOUND UNIT TO BE SLIGHTLY HANGING. SPLIT UNIT AND FOUND INTERIOR OF UNIT TO BE DIRTY, WITH FLYWEIGHTS STICKING. THIS WAS THE CAUSE OF THE HANGING ON BENCH. CLEANED INTERIOR OF UNIT AND GOVERNOR TESTED OK. 1G72 4U4 U H4SW E22EA 20010508002572001050800257NE 2001 5 8 HEEA072417 220010409G73202526385 BELLOWS 324473514 BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE FUEL CONTROL DEFECTIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N212 A34690 33010 IDLES AT 45 PERCENT N1 AND WILL NOT ACCELERATE. FOUND ALL FLOWS TO BE VERY LOW AND UNADJUSTABLE. SPLIT UNIT AND FOUND BELLOWS TO BE DEFECTIVE. 1G72 4U4 U H4SW E22EA 20010508002582001050800258NE 2001 5 8 HEEA072418 220010409G7320324473514 FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 ENGINE SLOW TO START. SMOKES ON START CYCLE. RAN UNIT AS RECEIVED ON TEST BENCH. COULD NOT DUPLICATE PROBLEM. 1G72 4U4 U H4SW E22EA 20010508002592001050800259NE 2001 5 8 HEEA072419 220010409G7320324473514 FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 ENGINE SLOW TO START. SMOKES ON START CYCLE. RAN UNIT AS RECEIVED ON TEST BENCH. COULD NOT DUPLICATE PROBLEM. 1G72 4U4 U H4SW E22EA 20010508002602001050800260NE 2001 5 8 HEEA072420 220010409G7320324473514 FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 7 PERCENT TORQUE SURGE AT FLAT PITCH. RAN UNIT AS RECEIVED ON TEST BENCH. COULD NOT DUPLICATE PROBLEM. 1G72 4U4 U H4SW E22EA 20010508002612001050800261NE 2001 5 8 HEEA072421 220010409G732032447368 FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 7 PERCENT N1 OSCILLATION, TOO MUCH CUSHION ON THE HIGH SIDE, UNABLE TO ADJUST. RAN UNIT AS RECEIVED ON TEST BENCH. COULD NOT DUPLICATE PROBLEM. 1G72 4U4 U H4SW E22EA 20030815000122003081500012SW 2003 8 15 HEEA072422 120010409G673041005496101 SERVO BELL 412 412 1182202SW FLT CONTROLS LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03 SERVO CAUSING EXCESSIVE INTERNAL LEAKAGE DURING TESTING. 1G72 4U H4SW 20010508002622001050800262SW 2001 5 8 HEEA072423 120010409G6710212076005105 CYLINDER BELL 412 412 1182202SW MAIN ROTOR BYPASSING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 CAUSING EXCESSIVE BYPASS DURING TESTING. 1G72 4U H4SW 20010508002632001050800263SW 2001 5 8 HEEA072424 120010409G3213412050010111A CROSSTUBE BELL 412 412 1182202SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033911L 33023 AFT CROSSTUBE SPREAD BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002642001050800264SW 2001 5 8 HEEA072425 120010409G3213412015060102 SKID SHOE BELL 412 412 1182202SW MAIN SKID TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 SHOE TORN AT MOUNT POINTS. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002652001050800265SW 2001 5 8 HEEA072426 120010409G3213412030437103 CAP BELL 412 412 1182202SW MLG DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 RUBBER ON CAP DETERIORATED. 1G72 4U H4SW 20010508002662001050800266SW 2001 5 8 HEEA072427 120010409G3213412050016102 SHOE BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002672001050800267SW 2001 5 8 HEEA072428 120010409G3213412050016102 SHOE BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002682001050800268SW 2001 5 8 HEEA072429 120010409G3212412050017133 COVER BELL 412 412 1182202SW FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 FLOAT COVER TORN. 1G72 4U H4SW 20010508002692001050800269SW 2001 5 8 HEEA072430 120010409G3212412050017133 COVER BELL 412 412 1182202SW FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 FLOAT COVER TORN. REPLACED WITH SERVICEABLE COVER. 1G72 4U H4SW 20010508002702001050800270SW 2001 5 8 HEEA072431 120010409G3212412050017135 COVER BELL 412 412 1182202SW FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 WORN VELCRO. 1G72 4U H4SW 20010508002712001050800271SW 2001 5 8 HEEA072432 120010409G3213412050045107 CROSSTUBE BELL 412 412 1182202SW MLG DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 UPON REMOVING CENTER PIVOT SADDLE; IT WAS FOUND THAT THERE WAS NO HOT BOND AGENT UNDER PIVOT. REPAIRED. 1G72 4U H4SW 20010508002722001050800272SW 2001 5 8 HEEA072433 120010409G2510412070843105 STRAP BELL 412 412 1182202SW COCKPIT FRAYED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 STRAPS FRAYED. REPLACED RESTRAINTS. 1G72 4U H4SW 20010508002732001050800273SW 2001 5 8 HEEA072434 120010409G7712412075008111 INDICATOR BELL 412 412 1182202SW COCKPIT READS LOW E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 NUMBER TWO NEEDLE READS LOW. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002742001050800274 2001 5 8 HEEA072435 420010409G3414412075009105 INDICATOR BELL 412 412 1182202SW COCKPIT INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 13 KNOT DIFFERENCE BETWEEN PILOTS AND COPILOTS INSTRUMENTS. 1G72 4U H4SW 20010508002752001050800275SW 2001 5 8 HEEA072436 120010409G7714412075010109 INDICATOR BELL 412 412 1182202SW TRIPLE TACH READS LOW E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 INDICATES 2 PERCENT LOW. SENT TO MASCO FOR WARRANTY REPAIR. 1G72 4U H4SW 20010508002762001050800276SW 2001 5 8 HEEA072437 120010409G7714412075010109 INDICATOR BELL 412 412 1182202SW TRIPLE TACH STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037128R 36007 N2 NEEDLES STICK WHEN POWER IS CHANGED. 1G72 4U H4SW 20010508002772001050800277SW 2001 5 8 HEEA072438 120010409G7714412075010109 INDICATOR BELL 412 412 1182202SW TRIPLE TACH INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893N 33010 NR 1 TACH NEEDLE STOPPED ALL INDICATING. 1G72 4U H4SW 20010508002782001050800278SW 2001 5 8 HEEA072439 120010409G243651539002N GCU BELL 412 412 1182202SW NR 1 GENERATOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 NR 2 GENERATOR FAILED IN FLIGHT, WOULD NOT RESET. 1G72 4U H4SW 20010508002792001050800279SW 2001 5 8 HEEA072440 120010409G3213AB412050016101 SKID SHOE BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 SKID SHOE WORN THROUGH. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002802001050800280SW 2001 5 8 HEEA072441 120010410G6720PHI41294 BUSHING BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 BUSHINGS AND ROD ENDS WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20030815000132003081500013SW 2003 8 15 HEEA072442 120010410G6420PHI41294 ROTOR HEAD BELL 412 412 1182202SW TAIL ROTOR VIBRATION E HEEAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW03108X 33115 TAIL ROTOR PRODUCING A HIGH FREQ VIBRATION. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002812001050800281 2001 5 8 HEEA072443 420010410G2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW COCKPIT NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 A LOT OF BACKGROUND NOISE IN RECEPTION MODE. PERFORMED PRELIMINARY INSPECTION AND FOUND CARRIER SQUELCH INTERMITTENT, ADJUSTED R184. 1G71 3U H2SW 20010508002822001050800282 2001 5 8 HEEA072444 420010410G2312064105430 TRANSCEIVER BELL 206 206L1 1182107SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 DISPLAY BLINKS ON AND OFF. PERFORMED PRELIMINARY INSPECTION. SWAPPED OUT DISPLAY. NO HELP. REPLACED BAD VOLUME POTENTIOMETER, CRACKED TRANSFER SWITCH AND PUSH BUTTON AND IC I901. FOUND BRIGHT DASHES TO APPEAR ACROSS MIDDLE OF USE FREQUENCY. REPLACED IC I505 AND I506. NO HELP. 1G71 3U H2SW 20010508002832001050800283SW 2001 5 8 HEEA072445 120010410G6330206033506101 RESTRAINT BELL 206 206L1 1182107SW TRANSMISSION WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW035019F 45244 BEARINGS WORN. REPLACED WITH SERVICEABLE RESTRAINT. 1G71 3U H2SW 20010508002842001050800284SW 2001 5 8 HEEA072446 120010410G6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036610C 51425 BEARINGS WORN. REPLACED WITH SERVICEABLE RESTRAINT. 1G71 3U H2SW 20010508002852001050800285 2001 5 8 HEEA072447 420010410G2312064105430 TRANSCEIVER BELL 206 206L1 1182107SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032135V 45657 WILL NOT TRANSMIT ON ALL FREQUENCIES AND WILL NOT SWITCH. PERFORMED PRELIMINARY INSPECTION. COULD NOT DUPLICATE PROBLEM. ADJUSTED FREQUENCY. FOUND DISPLAY STAYING DIM ALL THE TIME. REPLACED BAD V901 PHOTOCELL. REPAIRED PROBLEM. BENCH CHECK GOOD. 1G71 3U H2SW 20010508002862001050800286SW 2001 5 8 HEEA072448 120010410G7933209070262101 INDICATOR BELL 412 412 1182202SW ENGINE OIL READS HIGH E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036559Z 36019 INDICATES ABOVE RED LINE. 1G72 4U H4SW 20010508002872001050800287SW 2001 5 8 HEEA072449 120010410G7933209070262101 INDICATOR BELL 412 412 1182202SW ENGINE OIL READS HIGH E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033911L 33023 INDICATES ABOVE RED LINE. 1G72 4U H4SW 20010508002882001050800288SW 2001 5 8 HEEA072450 120010410G7933209070262101 INDICATOR BELL 412 412 1182202SW ENGINE OIL STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW033911L 33023 STICKS WHEN ENGINE IS FIRST RUN UP. 1G72 4U H4SW 20010508002892001050800289SW 2001 5 8 HEEA072451 120010410G6720PHI41294 BUSHING BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 WORN BEARINGS/BUSHINGS. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002902001050800290 2001 5 8 HEEA072452 420010410G3421PHI4121017601 CONNECTOR BELL 412 412 1182202SW ATTITIUDE GYRO LOOSE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 CONNECTOR PLUG RECEPTACLE LOOSE IN HOUSING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002912001050800291SW 2001 5 8 HEEA072453 120010410G2821AC985F10 FUEL FILTER BELL 214 214ST 1182106SW FUEL SYSTEM MALFUNCTIONED E HEEAK NONE J WARNING INDICATION ININSP/MAINT 1 SW033897N 28106 FUEL FILTER LIGHT. REPLACED WITH SERVICEABLE PART. 2G72 4U H10SW 20010508002922001050800292SW 2001 5 8 HEEA072454 120010410G7712412075008111 INDICATOR BELL 412 412 1182202SW TORQUE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 NR 1 NEEDLE IS INOPERATIVE. 1G72 4U H4SW 20010508002932001050800293SW 2001 5 8 HEEA072455 120010410G7712412075008111 INDICATOR BELL 412 412 1182202SW TORQUE SPLIT E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 HAS A 10 PERCENT SPLIT. ALSO NOTICED WITH JUST THE NR 1 ENGINE RUNNING THE TRANSMISSION NEEDLE FLUCTUATING AND BRINGING THE NR 2 NEEDLE WITH IT. 1G72 4U H4SW 20010508002942001050800294SW 2001 5 8 HEEA072456 120010410G7714412075010109 INDICATOR BELL 412 412 1182202SW TRIPLE TACH READS LOW E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 NR 1 ENGINE READING LOW. 1G72 4U H4SW 20010508002952001050800295SW 2001 5 8 HEEA072457 120010410G7714412075010111 INDICATOR BELL 412 412 1182202SW TRIPLE TACH INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 NR 1 NEEDLE INOPERATIVE. 1G72 4U H4SW 20010508002962001050800296SW 2001 5 8 HEEA072458 120010410G3213AB205050403031 CROSSTUBE BELL 412 412 1182202SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0322347 36005 CORRODED BEYOND LIMITS UNDER BOTH SADDLE MOUNTS. SCRAPPED AND REPLACED WITH SERVICEABLE TUBE. 1G72 4U H4SW 20010508002972001050800297SW 2001 5 8 HEEA072459 120010410G5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 WILL NOT OPERATE LEFT STEP ACTUATOR. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002982001050800298SW 2001 5 8 HEEA072460 120010410G5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032261D 33076 LEFT STEP WILL NOT RAISE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508002992001050800299SW 2001 5 8 HEEA072461 120010410G5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033893L 33006 LT STEP WILL NOT EXTEND. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508003002001050800300SW 2001 5 8 HEEA072462 120010410G5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036559Z 36019 LT STEP WILL NOT RETRACT. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010508003012001050800301GL 2001 5 8 HEEA072463 220010410G732025490924 FUEL CONTROL BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL ENGINE LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW032133X 45634 CAE890024 FUEL LEAKING FROM AROUND BYPASS COVER. DURING OVERHAUL FOUND EXCESSIVE CORROSION AND PITTING AROUND BYPASS COVER AND BORE. THIS CONDITION WILL CAUSE LEAKING FROM THE BYPASS COVER. REPLACED COMPLETE MAIN FLOW BODY ASSY. UNIT TESTED SATISFACTORY. 1G71 3U3 U H2SW E1GL 20010508003022001050800302GL 2001 5 8 HEEA072464 220010410G7320252464430 FUEL CONTROL BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032753F 2729 GOING HOT AND WOULD NOT RESPOND TO ADJUSTMENTS. REPLACED WITH SERVICEABLE FUEL CONTROL. 1G71 3U3 U H2SW E4CE 20010508003032001050800303GL 2001 5 8 HEEA072465 220010410G732025490925 FUEL CONTROL BELL 206 206L3 1182108SW ALLSN 250C 250C20B 03013GL ENGINE ERRATIC E HEEAK NONE L NO TEST ININSP/MAINT 1 SW038589X 51487 INCONSISTENT STARTS. SOME STARTS NORMAL. OTHERS DELAYED AND TENDED TO HAVE HIGH TOT. REPLACED WITH SERVICEABLE FUEL CONTROL. 1G71 3U3 U H2SW E4CE 20010508003042001050800304 2001 5 8 HEEA072466 420010410G34215040017901 INDICATOR BELL 206 206L1 1182107SW COCKPIT PRECESSES E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0345RP 45521 EXCESSIVE PRECESSING. REPLACED WITH SERVICEABLE ATTITUDE INDICATOR. 1G71 3U H2SW 20010508003052001050800305 2001 5 8 HEEA072467 420010410G34215040017901 INDICATOR BELL 206 206L3 1182108SW COCKPIT INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 INDICATES 7-8 DEGREE LEFT TURN IN LEVEL FLIGHT. REPLACED WITH SERVICEABLE ATTITUDE INDICATOR. 1G71 3U H2SW 20010508003062001050800306 2001 5 8 HEEA072468 420010410G34215040017901 INDICATOR BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW038591X 51495 ROLLING AND WILL NOT HOLD A LEVEL ATTITUDE. REPLACED WITH SERVICEABLE ATTITUDE INDICATOR. 1G71 3U H2SW 20010508003072001050800307 2001 5 8 HEEA072469 420010410G34225050010902 GYRO BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036251X 51552 LAGS 40 DEGREE IN 180 DEGREE TURN. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003082001050800308SW 2001 5 8 HEEA072470 120010410G6520PHI2062003 HOUSING BELL 206 206L3 1182108SW TAIL ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW0321497 51518 TAIL ROTOR GEARBOX INPUT SEAL LEAKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003092001050800309GL 2001 5 8 HEEA072471 220010410G732025490925 FUEL CONTROL BELL 206 206L3 1182108SW ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED E HEEAK NONE R PARTIAL RPM/PWR LOSS ININSP/MAINT 1 SW034835 51131 STARTS STAGNATES AT 33 PERCENT N1. RAN UNIT ON TEST BENCH AND COULD NOT DUPLICATE PROBLEM. 1G71 3U3 U H2SW E4CE 20010508003102001050800310SW 2001 5 8 HEEA072472 120010410G6210200578S69D BOLT BELL 206 206L1 1182107SW M/R BLADE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035019F 45244 AREA OF SHANK BEHIND THREADS, IS OVERSIZED AND WILL NOT ALLOW BOLT TO GO THROUGH BUSHING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003112001050800311SW 2001 5 8 HEEA072473 120010410G5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 LT STEP WILL NOT RETRACT. 1G72 4U H4SW 20010508003122001050800312SW 2001 5 8 HEEA072474 120010410G7332206061535007 TRANSDUCER BELL 206 206L1 1182107SW FUEL PRESSURE MALFUNCTIONED E HEEAO OTHER O OTHER CRCRUISE 1 SW03513EH 45421 WHILE IN CRUISE FLIGHT THE FUEL PRESSURE INDICATOR SHOWED A DECREASE IN FUEL PRESSURE. REPLACED PRESSURE TRANSMITTER. 1G71 3U H2SW 20010508003132001050800313SW 2001 5 8 HEEA072475 120010410G5610222180109 WINDOW BELL 430 430 1182150SW COCKPIT SEPARATED E HEEAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SW03430X 49058 ENROUTE TO MP283 AT 3000 FEET AT 135 KNOTS, THE CO-PILOT''S DOOR WINDOW DEPARTED THE AIRCRAFT. INSPECTED AND FOUND NO DAMAGE TO AIRCRAFT. 1G72 3U RTH9SW 20010508003142001050800314 2001 5 8 HEEA072476 420010411G34578143902240B GPS BELL 412 412 1182202SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032149S 36002 WILL NOT RECEIVE SATELLITES. COULD NOT DUPLICATE PROBLEM. BENCH CHECK GOOD. 1G72 4U H4SW 20010508003152001050800315 2001 5 8 HEEA072477 420010411G34578143902240B GPS BELL 412 412 1182202SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032149S 36002 GPS WENT OFF LINE/ON LINE. COULD NOT DUPLICATE PROBLEM. BENCH CHECK GOOD. 1G72 4U H4SW 20010508003162001050800316 2001 5 8 HEEA072478 420010411G34578143902240B GPS BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW034835 51131 CDI (EXTERNAL) DOES NOT INDICATE PROPERLY. DOES NOT AGREE WITH GPS CDI REMAINS 2 DIVISIONS DIFFERENT. SENT TO TRIMBLE NAVIGATION FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010508003172001050800317 2001 5 8 HEEA072480 420010411G34578143802240D GPS BELL 407 407 SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03492PH 53390 FALLS OFF LINE. 1G71 3U O H2SW 20010508003182001050800318 2001 5 8 HEEA072481 420010411G34578143802240D GPS BELL 206 206B3 1181506SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0322743 3624 LOCKS ON ONE LOCATION, WILL NOT UPDATE IN FLIGHT. SENT TO TRIMBLE NAVIGATION FOR WARRANTY REPAIR. 1G71 3U H2SW 20010508003192001050800319 2001 5 8 HEEA072482 420010411G344280510800001 CONTROL BOX BELL 206 206L3 1182108SW RADAR FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036610Y 51419 NO TARGETS DISPLAYED. 1G71 3U H2SW 20010508003202001050800320 2001 5 8 HEEA072483 420010411G344380510890001 CONTROL BOX BELL 206 206L3 1182108SW RADAR FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036610Y 51419 WOULD NOT TRACK AIRCRAFT PROPERLY. 1G71 3U H2SW 20010508003212001050800321SW 2001 5 8 HEEA072484 120010411G79218538100 OIL COOLER BELL 412 412 1182202SW ENGINE LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW031202T 33112 LEAKING FROM CENTER CORE AREA. 1G72 4U H4SW 20010508003222001050800322SW 2001 5 8 HEEA072485 120010411G2820869A6TT CHECK VALVE BELL 206 206L1 1182107SW ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033178K 45765 CHECK VALVES POSSIBLY CAUSING ENGINE FLAME OUT. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003232001050800323SW 2001 5 8 HEEA072486 120010411G2820869A6TT VALVE BELL 206 206L1 1182107SW ENGINE STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 STICKING OPEN. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003242001050800324 2001 5 8 HEEA072487 420010411G22147000298901 COMPUTER BELL 412 412 1182202SW AFCS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 NR 2 HELIPILOT WOULD NOT COME ON. 1G72 4U H4SW 20010508003252001050800325 2001 5 8 HEEA072488 420010411G22127000299901 CONTROL UNIT BELL 412 412 1182202SW AFCS FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 NR 2 HELIPILOT WILL NOT CYCLE AFCS CAUTION LIGHT WITH HELIPILOT ON AND TURNING HELIPILOT NR 2 ON AND OFF. 1G72 4U H4SW 20010508003262001050800326 2001 5 8 HEEA072489 420010411G34447000839901 INDICATOR BELL 412 412 1182202SW RADAR ALTIMETER MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03108X 33115 FLAG WILL NOT PULL. 1G72 4U H4SW 20010508003272001050800327 2001 5 8 HEEA072490 420010411G34447000839904 INDICATOR BELL 412 412 1182202SW RADAR ALTIMETER FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0333008 36004 READS LOW AND DH LIGHT DOES NOT COME ON AT SET ALTITUDE. 1G72 4U H4SW 20010508003282001050800328SW 2001 5 8 HEEA072491 120010411G291070066L000R230 HOSE BELL 412 412 1182202SW HYD SYSTEM LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03108X 33115 LEAKING THROUGH STEEL BRAIDED SLEEVE. REPLACED WITH SERVICEABLE HOSE. 1G72 4U H4SW 20010508003292001050800329SW 2001 5 8 HEEA072492 120010411G311078805059008 INDICATOR BELL 206 206L3 1182108SW COCKPIT INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW034282Z 51499 INTERMITTENT DISPLAY. 1G71 3U H2SW 20010508003302001050800330 2001 5 8 HEEA072493 420010411G34166221205004 ALTIMETER BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW031202T 33112 TESTS AT 42 INSTEAD OF 50 +/-5. 1G72 4U H4SW 20010508003312001050800331SW 2001 5 8 HEEA072494 120010411G67306225194001 SERVO BELL 206 206L1 1182107SW AUTOPILOT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035744Y 45465 INTERMITTENT FEEDBACK (KICKING) IN AUTOPILOT SYSTEM. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003322001050800332SW 2001 5 8 HEEA072495 120010411G67306225194001 SERVO BELL 206 206L1 1182107SW AUTOPILOT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035744Y 45465 CAUSES AUTOPILOT SYSTEM TO DISENGAGE AND FEEDBACK IN CONTROLS (KICKING). REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003332001050800333SW 2001 5 8 HEEA072496 120010411G67306225194001 SERVO BELL 206 206L1 1182107SW AUTOPILOT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035744Y 45465 SERVO CAUTION LIGHT ILLUMINATES AND AUTOPILOT SYSTEM DISENGAGES. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003342001050800334SW 2001 5 8 HEEA072497 120010411G67306225194001 SERVO BELL 206 206L1 1182107SW AUTOPILOT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035744Y 45465 AUTOPILOT SYSTEM INTERMITTENTLY DISENGAGES AND SERVO CAUSES KICKING IN PILOT''''S CYCLIC STICK. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003352001050800335SW 2001 5 8 HEEA072498 120010411G311065013008 INDICATOR BELL 206 206L3 1182108SW COCKPIT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 STICKS. FACEPLATE CAME OFF DURING REMOVAL OF INDICATOR. SENT TO MASCO FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010508003362001050800336GL 2001 5 8 HEEA072499 220010411G72406854255 VALVE BELL 206 206L3 1182108SW ALLSN 250B 250B* GL ENGINE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03206FS 51506 THREADS DAMAGED THAT GO INTO COMBUSTION CASE. REPLACED WITH SERVICEABLE PART. 1G71 3U3 T H2SW E10CE 20010508003372001050800337SW 2001 5 8 HEEA072500 120010411G7120 BEARING BELL 407 407 SW ENGINE MOUNT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03719PH 53266 REAR ENGINE MOUNT BEARING UNSTAKED. SENT TO DALLAS AIRMOTIVE FOR OVERHAUL. 1G71 3U O H2SW 20010508003382001050800338SW 2001 5 8 HEEA072501 120010411G71006892836 TUBE BELL 206 206L3 1182108SW ENGINE LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW036610C 51425 TUBE ASSY LEAKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003392001050800339GL 2001 5 8 HEEA072502 220010411G74206893283 IGNITION LEAD BELL 206 206L4 1182110SW ALLSN 250B 250B* GL ENGINE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW037077F 52038 IGNITION LEAD INOPERATIVE. 1G71 3U3 TNCH2SW E10CE 20010509000932001050900093GL 2001 5 9 HEEA072505 220010411G75326894063 BLEED VALVE BELL 206 206L3 1182108SW ALLSN 250B 250B* GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038588X 51486 WOULD NOT ACTUATE. REPLACED WITH SERVICEABLE PART. 1G71 3U3 T H2SW E10CE 20010508003402001050800340 2001 5 8 HEEA072506 420010411G34215040017901 INDICATOR BELL 206 206L3 1182108SW ATTITUDE FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW038591X 51495 ROLLING, WILL NOT HOLD A LEVEL ALTITUDE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003412001050800341 2001 5 8 HEEA072507 420010411G34215040017901 INDICATOR BELL 206 206L1 1182107SW ATTITUDE PRECESSES E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 PRECESSES. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003422001050800342 2001 5 8 HEEA072508 420010411G34215040017901 INDICATOR BELL 206 206L3 1182108SW ATTITUDE PRECESSES E HEEAK NONE O OTHER ININSP/MAINT 1 SW036160Y 51609 PILOT REPORTS THAT AFTER INSTRUMENT SLOWLY STARTED TO PRECESS THE CARD WAS CORRECTED AND INSTRUMENT FROZE UP IN WINGS LEVEL AND NOSE ON HORIZON POSITION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003432001050800343 2001 5 8 HEEA072509 420010411G34215040017901 INDICATOR BELL 206 206L1 1182107SW ATTITUDE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035019F 45244 PILOT REPORTED INDICATOR INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003442001050800344 2001 5 8 HEEA072510 420010411G34225050010902 GYRO BELL 206 206L3 1182108SW COCKPIT SMOKE E HEEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW0341791 51465 SMOKING AND POPS CIRCUIT BREAKER. REPLACED TRANSFORMER, RESISTORS AND BEARINGS. BENCH CHECK GOOD. 1G71 3U H2SW 20010508003452001050800345 2001 5 8 HEEA072511 420010411G34225050010902 GYRO BELL 206 206L1 1182107SW COCKPIT PRECESSES E HEEAK NONE O OTHER ININSP/MAINT 1 SW035007Q 45187 PRECESSES 2 DEGREES EVERY 5 MINUTES. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003462001050800346SW 2001 5 8 HEEA072512 120010411G632050501008380401 SEAL BELL 206 206L3 1182108SW OIL PUMP LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW036160Y 51609 OIL LEAKING FROM TRANSMISSION OIL PUMP DRIVE SHAFT SEAL. REPLACED TRANSMISSION OIL PUMP. 1G71 3U H2SW 20010508003472001050800347 2001 5 8 HEEA072514 420010411G2562569880101 SWITCH BELL 206 206L4 1182110SW ELT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW037077F 52038 RED LIGHT STAYS ON DIM. REPLACED WITH SERVICEABLE SWITCH. 1G71 3U NCH2SW 20010508003482001050800348NE 2001 5 8 HEEA072515 220010411G74203029107 LEAD BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE IGNITER FRAYED E K NONE O OTHER ININSP/MAINT 1 SW031202T 33112 FRAYED. REPLACED WITH SERVICEABLE CABLE. 1G72 4U4 U H4SW E22EA 20010508003492001050800349SW 2001 5 8 HEEA072516 120010411G77223030083 COMPENSATOR BELL 412 412 1182202SW TRIM FLUCTUATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 ITT FLUCTUATES IN FLIGHT AT OR ABOVE 2500 FEET ALTITUDE. 1G72 4U H4SW 20010508003502001050800350NE 2001 5 8 HEEA072517 220010411G732132447066 CONTROL UNIT BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 TORQUE OSCILLATIONS DURING POWER CHANGES. TESTED UNIT AND COULD NOT DUPLICATE PROBLEM. 1G72 4U4 U H4SW E22EA 20010508003512001050800351NE 2001 5 8 HEEA072518 220010411G732132447066 CONTROL UNIT BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE CONTAMINATED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW033893N 33010 DROOPING IN FLIGHT, FOUND TURCO IN FITTINGS. CLEANED AND POLISHED SERVO VALVE, LEVERS AND FITTINGS. UNIT TESTED OK. 1G72 4U4 U H4SW E22EA 20010508003522001050800352SW 2001 5 8 HEEA072519 120010411G6510327211 DISC PACK BELL 206 206L3 1182108SW T/R SHAFT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03206LS 51070 CORRODED BEYOND LIMITS. REPLACED WITH NEW PARTS. 1G71 3U H2SW 20010508003532001050800353SW 2001 5 8 HEEA072520 120010411G6510327211 DISC PACK BELL 206 206L3 1182108SW T/R DRIVE SHAFT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0341128 51134 PITTED BEYOND LIMITS. REPLACED WITH NEW PARTS. 1G71 3U H2SW 20010508003542001050800354SW 2001 5 8 HEEA072521 120010411G6510327211 DISC PACK BELL 206 206L3 1182108SW T/R DRIVE SHAFT FRETTED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0341791 51465 FRETTING BEYOND LIMITS. REPLACED WITH NEW PARTS. 1G71 3U H2SW 20010508003552001050800355SW 2001 5 8 HEEA072522 120010411G6510327211 DISC PACK BELL 206 206L1 1182107SW T/R DRIVE SHAFT CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 CRACKED. REPLACED WITH NEW PARTS. 1G71 3U H2SW 20010508003562001050800356SW 2001 5 8 HEEA072523 120010411G6510327211 DISC PACK BELL 206 206L1 1182107SW T/R DRIVE SHAFT CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 CRACKED. REPLACED WITH NEW PARTS. 1G71 3U H2SW 20010508003572001050800357SW 2001 5 8 HEEA072524 120010411G6510327211 DISC PACK BELL 407 407 SW T/R DRIVE SHAFT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03436PH 51436 CORRODED BEYOND LIMITS. REPLACED WITH NEW PARTS. 1G71 3U O H2SW 20010508003582001050800358SW 2001 5 8 HEEA072525 120010411G6510327211 DISC PACK BELL 206 206L1 1182107SW T/R DRIVE SHAFT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035014V 45217 CORRODED BEYOND LIMITS. REPLACED WITH NEW PARTS. 1G71 3U H2SW 20010508003592001050800359SW 2001 5 8 HEEA072526 120010411G6510327211 DISC PACK BELL 206 206L3 1182108SW T/R DRIVE SHAFT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036251X 51552 CORRODED BEYOND LIMITS. REPLACED WITH NEW PARTS. 1G71 3U H2SW 20010508003602001050800360SW 2001 5 8 HEEA072527 120010411G6510327211 DISC PACK BELL 206 206L4 1182110SW T/R DRIVE SHAFT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037077F 52038 CORRODED BEYOND LIMITS. REPLACED WITH NEW PARTS. 1G71 3U NCH2SW 20010508003612001050800361 2001 5 8 HEEA072528 420010411G2330002000002 AMPLIFIER BELL 206 206L3 1182108SW PA SYSTEM INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331077 51520 INOPERATIVE. WILL NOT TURN ON. PERFORMED PRELIMINARY INSPECTION. FOUND Q3204 BAD. REPLACED. CLEANED RUST ON HOUSING AND PAINTED. FUNCTION CHECK GOOD. 1G71 3U H2SW 20010508003622001050800362 2001 5 8 HEEA072529 420010411G34570110005400 GPS BELL 206 206L1 1182107SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035007Q 45187 LOOSES SATELLITES DURING FLIGHT. 1G71 3U H2SW 20010508003632001050800363 2001 5 8 HEEA072530 420010411G34570110005400 GPS BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0321497 51518 WILL NOT ACQUIRE SATELLITE SIGNAL. 1G71 3U H2SW 20010508003642001050800364 2001 5 8 HEEA072531 420010411G34570110005400 GPS BELL 206 206L1 1182107SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0321240 45647 DROPPING OFF. 1G71 3U H2SW 20010508003652001050800365 2001 5 8 HEEA072532 420010411G34570110005400 GPS BELL 206 206L1 1182107SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035007Y 45192 WILL NOT COME ON LINE FOR 20-40 MINUTES. 1G71 3U H2SW 20010508003662001050800366 2001 5 8 HEEA072533 420010411G3457 BATTERY BELL 206 206L3 1182108SW GPS DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036748D 81509251 51106 INTERNAL BATTERY WEAK. SENT TO GARMIN INTERNATIONAL FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010508003672001050800367 2001 5 8 HEEA072534 420010411G34570110005400 GPS BELL 206 206L3 1182108SW COCKPIT UNRELIABLE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03979BH 51403 GPS UNRELIABLE. SENT TO GARMIN INTERNATIONAL FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010508003682001050800368GL 2001 5 8 HEEA072535 220010411G726103808808 ELEMENT BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENG OIL SYSTEM BYPASSING E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331077 51520 BYPASSED EARLY. SCRAPPED LOCALLY AND REPLACED WITH NEW FILTER. 1G71 3U3 U H2SW E1GL 20010508003692001050800369 2001 5 8 HEEA072536 420010411G34570845000000 GPS BELL 206 206L1 1182107SW COCKPIT INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032775A 45297 1ST DIGIT OF DISPLAY INOPERATIVE. SENT TO MAGELLAN SYSTEMS FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010508003702001050800370 2001 5 8 HEEA072537 420010411G34570845000000 GPS BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0381671 51301 WILL NOT KEEP USER WAYPOINTS WHEN POWER IS CYCLED. SENT TO MAGELLAN SYSTEMS FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010508003712001050800371 2001 5 8 HEEA072538 420010411G34570845000000 GPS BELL 206 206L3 1182108SW COCKPIT INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0381671 51301 POWER BUTTON IS INOPERATIVE. SENT TO MAGELLAN SYSTEMS FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010508003722001050800372SW 2001 5 8 HEEA072539 120010411G6510406040340101 DISC PACK BELL 206 206L3 1182108SW T/R DRIVE SHAFT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0341128 51134 PITTED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003732001050800373SW 2001 5 8 HEEA072540 120010411G6720206001058101 CONTROL ROD BELL 206 206L3 1182108SW TAIL ROTOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0341791 51465 CORROSION UNDER NYLATRON SLEEVE FOUND TO BE .020 INCH DEEP. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003742001050800374SW 2001 5 8 HEEA072541 120010411G6720206001058101 CONTROL ROD BELL 206 206L4 1182110SW TAIL ROTOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037074W 52033 CORROSION BEYOND LIMITS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20010508003752001050800375SW 2001 5 8 HEEA072542 120010411G6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW0342EA 51542 WORN SPHERICAL BEARINGS. 1G71 3U H2SW 20010508003762001050800376SW 2001 5 8 HEEA072543 120010411G6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032619 51375 BEARING IN TRANSMISSION RESTRAINT CAME UNSTAKED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003772001050800377SW 2001 5 8 HEEA072544 120010411G6330206033506103 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036251X 51552 BEARING WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003782001050800378SW 2001 5 8 HEEA072545 120010411G6330206033506103 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381671 51301 BOTH RESTRAINT ARM BEARINGS HAS EXCESSIVE WEAR IN BEARINGS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003792001050800379SW 2001 5 8 HEEA072546 120010411G6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW0353119 51575 BEARING WORN AND ONE BEARING UNSTAKED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003802001050800380SW 2001 5 8 HEEA072547 120010411G6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010508003812001050800381SW 2001 5 8 HEEA072548 120010411G2810206064611001 FUEL CELL BELL 206 206L1 1182107SW FUSELAGE TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 LEAKING, FOUND SMALL TEAR AT FRONT OF CELL. 1G71 3U H2SW 20010508003822001050800382SW 2001 5 8 HEEA072549 120010411G2810206064611001 FUEL CELL BELL 206 206L1 1182107SW FUSELAGE LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW033178K 45765 MAIN FUEL CELL LEAKS. 1G71 3U H2SW 20010508003832001050800383SW 2001 5 8 HEEA072550 120010411G7714206075681101 INDICATOR BELL 206 206L1 1182107SW DUAL TACH MALFUNCTIONED E HEEAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SW033178K 45765 DUAL TACH HAS NO LIGHT. 1G71 3U H2SW 20010508003842001050800384SW 2001 5 8 HEEA072551 120010411G7714206075681101 INDICATOR BELL 206 206L1 1182107SW DUAL TACH SPLIT E HEEAK NONE O OTHER ININSP/MAINT 1 SW035007Q 45187 2 PERCENT SPLIT IN NEEDLE INDICATION. 1G71 3U H2SW 20010508003852001050800385SW 2001 5 8 HEEA072552 120010411G7714206075681117 INDICATOR BELL 206 206L3 1182108SW DUAL TACH STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 TURBINE NEEDLE STAYING AT ZERO AT TIMES AND VERY UNRELIABLE. 1G71 3U H2SW 20010508003862001050800386SW 2001 5 8 HEEA072553 120010411G7712206075739103 INDICATOR BELL 206 206L3 1182108SW TORQUEMETER FLUCTUATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW0342EA 51542 INDICATOR FLUCTUATES 4 TO 5 PERCENT AT ALL TIMES. 1G71 3U H2SW 20010508003872001050800387SW 2001 5 8 HEEA072554 120010411G7712206075739103 INDICATOR BELL 206 206L3 1182108SW TORQUEMETER FLUCTUATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381671 51301 FLUCTUATES 3 TO 5 PERCENT ABOVE 80 PERCENT TORQUE. 1G71 3U H2SW 20010508003882001050800388SW 2001 5 8 HEEA072555 120010411G7712206075739103 INDICATOR BELL 206 206L1 1182107SW TORQUEMETER FLUCTUATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 TORQUE NEEDLE BOUNCES 2 TO 4 PERCENT. 1G71 3U H2SW 20010508003892001050800389SW 2001 5 8 HEEA072556 120010411G7712206075739103 INDICATOR BELL 206 206L3 1182108SW TORQUEMETER FLUCTUATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW0353119 51575 FLUCTUATES 10 PERCENT AND INTERMITTENTLY STICKS AT 6 PERCENT AFTER SHUTDOWN. 1G71 3U H2SW 20010508003902001050800390SW 2001 5 8 HEEA072557 120010411G6730206076062003 CYLINDER BELL 206 206L3 1182108SW SERVO DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331077 51520 THE PILOT VALVE THROUGH BOLTS (2 EA) ARE VERY STIFF AND CANNOT BE MOVED BY HAND. STIFF FLIGHT CONTROLS. REPLACED WITH SERVICEABLE SERVO. 1G71 3U H2SW 20010508003912001050800391SW 2001 5 8 HEEA072558 120010411G6730206076062003 CYLINDER BELL 206 206L3 1182108SW SERVO LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW036610Y 51419 LEAKING AT REAR SEAL. REPLACED WITH SERVICEABLE SERVO. 1G71 3U H2SW 20010508003922001050800392SW 2001 5 8 HEEA072559 120010411G3212206369002 FLOAT BELL 206 206L1 1182107SW MLG DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 HAS HOLE ON FRONT END. 1G71 3U H2SW 20010508003932001050800393SW 2001 5 8 HEEA072560 120010411G2821222366621101 FUEL FILTER BELL 206 206L3 1182108SW FUEL SYSTEM MALFUNCTIONED E HEEAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SW0330KH 51527 LIGHT WILL NOT COME ON. 1G71 3U H2SW 20010508003942001050800394SW 2001 5 8 HEEA072561 120010411G2821222366621101 FUEL FILTER BELL 206 206L4 1182110SW FUEL SYSTEM MALFUNCTIONED E HEEAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SW037074W 52033 LIGHT STAYS ON. 1G71 3U NCH2SW 20010508003952001050800395SW 2001 5 8 HEEA072562 120010411G2821222366621101 FUEL FILTER BELL 206 206L1 1182107SW FUEL SYSTEM STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW033178K 45765 BYPASS BUTTON STICKS. SENT TO PUROFLOW CORP. FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010508003962001050800396SW 2001 5 8 HEEA072563 120010411G2821222366621101 FUEL FILTER BELL 206 206L1 1182107SW FUEL SYSTEM MALFUNCTIONED E HEEAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SW0345RP 45521 ELECTRICAL PIN IN FILTER HEAD BROKEN. REPLACED WITH SERVICEABLE FUEL FILTER ASSY. 1G71 3U H2SW 20010508003972001050800397GL 2001 5 8 HEEA072564 220010411G742023060816 LEAD BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL IGNITER SHORTED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036160Y 51609 ONE OF THE FOUR TANGS ON B RECEPTACLE END BROKEN. 1G71 3U3 U H2SW E1GL 20010508003982001050800398GL 2001 5 8 HEEA072565 220010411G7323252467711 GOVERNOR BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL ENGINE DIRTY E HEEAK NONE O OTHER ININSP/MAINT 1 SW035019F 45244 WILL NOT RECOVER RPM AFTER COLLECTIVE POWER CHANGES. FOUND INTERIOR OF UNIT TO BE DIRTY WHICH COULD HAVE CAUSED GOVERNOR TO HANG AND HAVE HYSTERSIS PROBLEMS. 1G71 3U3 U H2SW E1GL 20010509000942001050900094GL 2001 5 9 HEEA072566 220010411G7323252469211 GOVERNOR BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 AIRCRAFT EXPERIENCES OVERSPEEDS ON LANDINGS AND DROOPS DURING TAKE OFF. REPLACED GOVERNOR ASSY. 1G71 3U3 U H2SW E1GL 20010509000952001050900095GL 2001 5 9 HEEA072567 220010411G7323252469211 GOVERNOR BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036610C8138 51425 N2 SLOW TO RECOVER AFTER POWER CHANGES. GOVERNOR RESPONDED POORLY ON TEST BENCH. SLOPE RESPONDED SLOWLY. CLEANED INTERIOR AND UNIT TESTED OK. 1G71 3U3 U H2SW E1GL 20010509000962001050900096GL 2001 5 9 HEEA072568 220010411G732025490925 FUEL CONTROL BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE FLUCTUATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381671 51301 TORQUE FLUCTUATING 10 PERCENT ON TAKE OFF. PERFORMED PRELIMINARY INSPECTION AND FOUND EXCESSIVE SIDE PLAY AT THE CUTOFF LINKAGE. REPLACED AND UNIT TESTED OK. 1G71 3U3 U H2SW E1GL 20010509000972001050900097GL 2001 5 9 HEEA072569 220010411G732025490925 FUEL CONTROL BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381671 51301 STARTING PROBLEMS AND OSCILLATIONS ABOVE 80 PERCENT TORQUE. PERFORMED PRELIMINARY INSPECTION AND COULD NOT DUPLICATE PROBLEM. 1G71 3U3 U H2SW E1GL 20010509000982001050900098GL 2001 5 9 HEEA072570 220010411G732025490925 FUEL CONTROL BELL 206 206L1 1182107SW ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 HUNG STARTS IN THE 40 TO 50 PERCENT N1 RANGE. PERFORMED PRELIMINARY INSPECTION AND FOUND NO DISCREPANCIES. UNIT TESTED OK. 1G71 3U3 U H2SW E1GL 20010509000992001050900099GL 2001 5 9 HEEA072571 220010411G732025490925 FUEL CONTROL BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381671 51301 ENGINE LIGHTS OFF VERY HOT ON ALL STARTS AND THERE IS NO MORE ADJUSTMENT LEFT FOR LIGHTOFF DERICHMENT. IF ACCELERATION IS MOVED BACK, START IS STILL HOT AND ACCELERATION SLOW. PERFORMED PRELIMINARY INSPECTION AND FOUND NO DISCREPANCIES. UNIT TESTED OK. 1G71 3U3 U H2SW E1GL 20010508003992001050800399SW 2001 5 8 HEEA072572 120010412G6322206061432121 HOUSING BELL 407 407 SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03510PH 53209 PART IS CRACKED. 1G71 3U O H2SW 20010508004002001050800400SW 2001 5 8 HEEA072573 120010412G7810407062021101 DUCT BELL 407 407 SW EXHAUST CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03510PH 53209 PART IS CRACKED. 1G71 3U O H2SW 20010508004012001050800401SW 2001 5 8 HEEA072574 120010412G2840407362005103 SWITCH BELL 407 407 SW LIGHT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03417PH 53038 LOW LEVEL LIGHT WILL NOT GO OUT. 1G71 3U O H2SW 20010509001002001050900100SW 2001 5 9 HEEA072576 120010412G3212206373902103 RELIEF VALVE BELL 407 407 SW FLOAT LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 RELIEF VALVE ON FLOAT LEAKING. 1G71 3U O H2SW 20010509001012001050900101SW 2001 5 9 HEEA072577 120010412G6420406312100101 BEARING 407012101111BELL 407 407 SW T/R HUB WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53198 53142 TAIL ROTOR HUB BEARING WORN. 1G71 3U O H2SW 20010509001022001050900102SW 2001 5 9 HEEA072578 120010412G6420406312100101 BEARING 407012101111BELL 407 407 SW T/R HUB WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53198 53142 TAIL ROTOR HUB BEARING WORN. 1G71 3U O H2SW 20010509001032001050900103SW 2001 5 9 HEEA072579 120010412G6420406312100101 BEARING 407012101111BELL 407 407 SW T/R HUB WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53198 53142 TAIL ROTOR HUB BEARINGWORN. 1G71 3U O H2SW 20010509001042001050900104SW 2001 5 9 HEEA072580 120010412G2510222320823130 SEAT BELT BELL 407 407 SW COCKPIT TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03417PH 53038 SEAT BELT TAG TORN. 1G71 3U O H2SW 20010509001052001050900105SW 2001 5 9 HEEA072581 120010412G2820AV23B11754 VALVE BELL 412 412 1182202SW FUEL SYSTEM LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW037128R 36007 LEAKING SHAFT SEAL. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010510001672001051000167EU 2001 5 10 HEEA072582 120010409G5531350A1400200802 SPAR SNIAS 350 AS350B2 8680813EU STABILIZER CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03350BZ 2653 SPAR INSIDE CHAFED FROM CONDUIT. REPLACED WITH SERVICEABLE PART. 1G71 3U H9EU 20010510001682001051000168EU 2001 5 10 HEEA072583 120010409G3213350A41108602 CROSSTUBE SNIAS 350 AS350B2 8680813EU MLG CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03350BZ 2653 CHAFED BY FLOAT ASSEMBLY. REPLACED WITH SERVICEABLE PART. 1G71 3U H9EU 20010510001692001051000169EU 2001 5 10 HEEA072584 120010409G3213350A41108702 CROSSTUBE SNIAS 350 AS350B2 8680813EU MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03350BZ 2653 SURFACE CORROSION EXCEEDS COVERAGE AREA AND DEPTH LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H9EU 20010510001702001051000170 2001 5 10 HEEA072585 420010411G34578143802240D GPS SNIAS 350 AS350B 8680801EU COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03973AE 3229 LOST POSITION. CANT FIND ITSELF. 1G71 3U H9EU 20010510001712001051000171 2001 5 10 HEEA072586 420010411G34578143802240D GPS SNIAS 350 AS350B 8680801EU COCKPIT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03970AE 3235 FACE PLATE DELAMINATED. 1G71 3U H9EU 20010510001722001051000172 2001 5 10 HEEA072587 420010411G3421504001790116 GYRO SNIAS 350 AS350B2 8680813EU COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0340466 3004 WOULD NOT FAST ERECT. REPLACED WITH SERVICEABLE PART. 1G71 3U H9EU 20010510001732001051000173EU 2001 5 10 HEEA072588 120010411G6510552200 BEARING BOLKMS105 BO105S 5626006EU T/R DRIVESHAFT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724MB S756 WHILE ROTATING M/R HEAD, NOTICED CLICKING SOUND COMING FROM BEARING ON TAILBOOM. REMOVED T/R DRIVESHAFT AND REPLACED ROUGH BEARING. 1G72 3U H3EU 20010507005562001050700556 2001 5 7 HEEA072594 420010417G3450071106603 RECEIVER SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW031546G 760076 WILL NOT GIVE BEARING INFO OR AUDIO. PERFORMED PRELIMINARY INSPECTION AND FOUND HUNDREDS SECTION S101 TERMINAL #26 HAS BROKEN WIRE AND VOLUME CONTROL NOISY. RESOLDERED WIRE ON S101 TERMINAL 26 AND CLEANED VOLUME CONTROL. REPAIRED. BENCH CHECK GOOD. 1G72 3U H1NE 20010507005572001050700557 2001 5 7 HEEA072595 420010417G3451066106602 TRANSCEIVER SKRSKYS76 S76A 8143006NE DME WEAK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03761PH 760224 WEAK RECEIVE AND TRANSMIT. 1G72 3U H1NE 20010507005582001050700558 2001 5 7 HEEA072596 420010417G3454066400700 RECEIVER SKRSKYS76 S76A 8143006NE VOR MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035435V 760158 CAUSES VOR GREEN NEEDLE TO INDICATE 15-20 DEGREES OFF. REPLACED I404, I406, I403, I407, C413, C430 AND C438. NO HELP. REPLACED I408 AND C438, I406. TROUBLESHOT AND REPAIRED A BROKEN FOIL UNDER I404. REPAIRED PROBLEM. RMI AND VOR BEARINGS OUT OF TOLERANCE. ALIGNED THE VOR AND RMI BOARDS. BENCH CHECK GOOD. 1G72 3U H1NE 20010507005592001050700559 2001 5 7 HEEA072597 420010419G2312VFS10902 ANTENNA SKRSKYS76 S76A 8143006NE VHF DAMAGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03911MJ 760231 REPORTED TO TRANSMIT GARBLED. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G72 3U H1NE 20010507005602001050700560 2001 5 7 HEEA072598 420010419G2340A3016W INTERPHONE SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035128 760181 AFTER UNIT WARMS UP, TRANSMITS AND RECEIVES BROKEN. PERFORMED PRELIMINARY INSPECTION. FOUND AMP BOARD AR1 AND TRANSISTOR Q8 BAD, REPLACED SAME. REPAIRED. BENCH CHECK GOOD. 1G72 3U H1NE 20010507005612001050700561NE 2001 5 7 HEEA072599 120010419G2510A1077B RELAY SKRSKYS76 S76A 8143006NE COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW034253S 760035 WOULD NOT PULL WITH GENERATORS ON THE LINE, FOUND LOW RESISTANCE BETWEEN X1 AND X2. SENT TO PRECISION AVIONICS & INSTR. INC. FOR INSPECTION AND REPAIR. 1G72 3U H1NE 20010507005622001050700562SW 2001 5 7 HEEA072600 120010419G3340ACR4F LIGHT BELL 412 412 1182202SW EXTERNAL INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033893N 33010 NOT WORKING. SENT TO OFFSHORE HELICOPTER SUPPORT FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20010509001062001050900106SW 2001 5 9 HEEA072601 120010416G2822205061635005 SWITCH BELL 412 412 1182202SW BOOST PUMP MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 BOOST PUMP LIGHT WILL NOT GO OUT. 1G72 4U H4SW 20010509001072001050900107NE 2001 5 9 HEEA072602 220010416G75323043023 BLEED VALVE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW033893P 33012 CPPS62415 IN CRUISE FLIGHT OBSERVED A 6 PERCENT TORQUE SPLIT. REPLACED WITH SERVICEABLE PART. 1G72 4U4 U H4SW E22EA 20010509001082001050900108SW 2001 5 9 HEEA072603 120010416G2435200SGL132Q STARTER GEN BELL 206 206L1 1182107SW ENGINE VIBRATION E HEEAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SW032761N2032 45277 HIGH FREQUENCY VIBRATION. ALSO THERE IS A CONSIDERABLE AMOUNT OF RUST COLORED RESIDUE OR DUST COMING FROM THE FRONT BEARING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010509001092001050900109NE 2001 5 9 HEEA072604 220010416G732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NR 1 ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 NR 1 ENGINE OSCILLATES DURING POWER TRANSITION AT APPROX. 80 PERCENT TORQUE. FOUND GOVERNOR WAS HANGING. FOUND INTERIOR OF UNIT VERY DIRTY WHICH CAUSED THE FLYWEIGHTS TO STICK. CLEANED FLYWEIGHTS AND REPLACED FLYWEIGHT PINS DUE TO WEAR. UNIT TESTED OK. 1G72 4U4 U H4SW E22EA 20010509001102001050900110SW 2001 5 9 HEEA072605 120010416G6710C4264215 SLEEVE BELL 206 206L3 1182108SW M/R CONTROL LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW038587X 51464 CAUSING EXCESSIVE INTERNAL LEAKAGE DURING TESTING. SENT TO FORTNER ACCESSORY SERVICE CORP. FOR WARRANTY REPAIR. 1G71 3U H2SW 20010509001112001050900111GL 2001 5 9 HEEA072606 220010416G7421CH34187A IGNITER BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036610C 51425 AIRCRAFT HAS DELAYED LIGHT OFF AFTER ENGINE WASH. REPLACED WITH SERVICEABLE IGNITER. 1G71 3U3 U H2SW E1GL 20010509001122001050900112SW 2001 5 9 HEEA072607 120010416G6730206076031023 SERVO BELL 206 206L1 1182107SW MAIN ROTOR STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 SPOOL STICKS IN SLEEVE OF LAP ASSY. SUSPECT DEFECTIVE LAPPING. 1G71 3U H2SW 20010509001132001050900113SW 2001 5 9 HEEA072608 120010416G6730C4264113 PLUG 206076062003BELL 206 206L3 1182108SW CYLINDER STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03937S RH3037A 51258 FOUND PLUG STICKS IN SLEEVE AND SPRING STICKS ON SPOOL. SENT TO FORTNER ACCESSORY SERVICE CORP. FOR WARRANTY REPAIR. 1G71 3U H2SW 20010509001142001050900114SW 2001 5 9 HEEA072609 120010416G6730 SERVO 206076062003BELL 206 206L3 1182108SW MAIN ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03 RH0958 CAUSING EXTERNAL LEAKAGE OF SERVO DURING TESTING. FOUND DEFECTIVE LAPPING. SENT TO FORTNER ACCESSORY SERVICE CORP. FOR WARRANTY REPAIR. 1G71 3U H2SW 20010509001152001050900115SW 2001 5 9 HEEA072610 120010416G6730 SERVO 206076062003BELL 206 206L3 1182108SW MAIN ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW0349EA RH3886A 51507 CAUSING EXCESSIVE INTERNAL LEAKAGE. FOUND DEFECTIVE LAPPING. SENT TO FORTNER ACCESSORY SERVICE CORP. FOR WARRANTY REPAIR. 1G71 3U H2SW 20010509001162001050900116SW 2001 5 9 HEEA072611 120010416G6730 SERVO 206076062003BELL 206 206L3 1182108SW MAIN ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03206FS RH1092 51506 CAUSING EXCESSIVE INTERNAL LEAKAGE. FOUND DEFECTIVE LAPPING. SENT TO FORTNER ACCESSORY SERVICE CORP. FOR WARRANTY REPAIR. 1G71 3U H2SW 20010509001172001050900117 2001 5 9 HEEA072612 420010417G3444071111400 CONNECTOR BELL 206 206L1 1182107SW ALTIMETER LOOSE E HEEAK NONE O OTHER ININSP/MAINT 1 SW035744Y 45465 ANTENNA CABLE CONNECTOR LOOSE FROM CABLE. INSPECTED ANTENNA AND FOUND BROKEN BEYOND REPAIR. SCRAPPED ANTENNA. 1G71 3U H2SW 20010509001182001050900118 2001 5 9 HEEA072613 420010417G3444071111401 ANTENNA BELL 206 206L3 1182108SW RADAR ALTIMETER UNRELIABLE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03141BH 51303 INTERMITTENT AND UNRELIABLE. 1G71 3U H2SW 20010509001192001050900119 2001 5 9 HEEA072614 420010417G3444071111401 ANTENNA BELL 206 206L3 1182108SW RADAR ALTIMETER INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW0330KH 51527 ANTENNA HAS A 50 FOOT ERROR. 1G71 3U H2SW 20010509001202001050900120 2001 5 9 HEEA072615 420010417G3442 WIRE BELL 206 206L3 1182108SW ANTENNA SEPARATED E K NONE O OTHER ININSP/MAINT 1 SW038591X 13278 51495 ANTENNA CABLE PULLED OUT. 1G71 3U H2SW 20010509001212001050900121 2001 5 9 HEEA072616 420010417G3452071119208 CONTROL UNIT BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03108X 33115 DISPLAY BLANKS OUT WHEN CHANGING DIGITS. PERFORMED PRELIMINARY INSPECTION AND REPLACED DISPLAY LENS AND I203, I204, I205 AND I206 IC CHIPS. NO HELP. FOUND J303 FLEX CABLE BAD. REPLACED J303 CABLE, I303 IC CHIP, I306 IC CHIP AND I202 IC CHIP. NO HELP. 1G72 4U H4SW 20010509001222001050900122 2001 5 9 HEEA072617 420010417G3454069102505 TRANSCEIVER BELL 206 206L4 1182110SW VOR SYSTEM WEAK E HEEAK NONE O OTHER ININSP/MAINT 1 SW037077B 52037 WEAK RECEIVE. PERFORMED PRELIMINARY INSPECTION. FOUND MODULATION LOW AND WILL NOT ADJUST. REPLACED Q313, Q312 AND R505. ALSO FOUND NAV RECEIVER WEAK. TROUBLESHOT AND FOUND SEVERAL COIL AND INDUCTORS FROZEN. REPLACED L202, L206, L300, L301, L303 AND L304. ALSO REPLACED T205. COMM RECEIVER SENSITIVITY VERY WEAK AND WILL NOT ADJUST. 1G71 3U NCH2SW 20010509001232001050900123 2001 5 9 HEEA072618 420010417G2312064100900 TRANSCEIVER BELL 212 212 1181420SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035736J 31140 ON INITIAL INSTALLATION UNIT WOULD NOT TRANSMIT DURING FUNCTIONAL TEST. FOUND MODULATION WEAK WHEN UNIT WAS COOL AND WOULD GO UP AS UNIT WARMED UP. REPLACED CR325 DIODE AND REALIGNED TRANSMITTER. REPAIRED. BENCH CHECK GOOD. 1G71 4U H4SW 20010509001242001050900124 2001 5 9 HEEA072619 420010417G2312064102300 TRANSCEIVER BELL 412 412 1182202SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 WILL NOT RECEIVE. REMOVED BROKEN PIN FROM RF CONNECTOR. REMOVED CORROSION FROM CHASIS. ADJUSTED C/N SQUELCH, CARRIER SQUELCH, MIC GAIN AND SIDETONE. BENCH CHECK GOOD. 1G72 4U H4SW 20010509001252001050900125 2001 5 9 HEEA072620 420010417G2312064102300 TRANSCEIVER BELL 412 412 1182202SW COCKPIT OUT OF ADJ E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 TRANSMIT SCRATCHY. FOUND RF CONNECTOR LOOSE ON UNIT. TIGHTENED RF CONNECTOR. ALIGNED TRANSMITTER. REPAIRED. ADJUSTED CARRIER SQUELCH. REMOVED CORROSION FROM CHASIS. BENCH CHECK GOOD. 1G72 4U H4SW 20010509001262001050900126 2001 5 9 HEEA072621 420010417G2312064102300 TRANSCEIVER BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 INOPERATIVE, WILL NOT COME ON. FOUND FUSE OPEN. REPLACED HEADER AND APPLIED HUMISEAL TO HEADER FOR CORROSION CONTROL. ADJUSTED C/N SQUELCH, MIC GAIN, AND SIDETONE. BENCH CHECK GOOD. 1G72 4U H4SW 20010509001272001050900127 2001 5 9 HEEA072622 420010417G2312064102302 RECEIVER BELL 214 214ST 1182106SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0359805 28141 SQUELCH STAYS ON. ALIGNED RECEIVER SEVERAL TIMES. SWAPPED Q317 AND Q319 TRANSISTORS. REALIGNED RECEIVER BOARD. REPLACED Q304, Q305, Q306, Q307, Q308, Q317, Q318, Q319, Q320 AND Q321 TRANSISTORS AND I301 IC CHIP. ALSO REPLACED BROKEN NAMEPLATE. ADJUSTED VCO VOLTAGE AND REALIGNED RECEIVER. REPLACED RECEIVER BOARD. BENCH CHECK GOOD. 2G72 4U H10SW 20010509001282001050900128 2001 5 9 HEEA072623 420010417G2312064105430 TRANSCEIVER BELL 407 407 SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 INTERMITTENT RADIO WOULD NOT BREAK SQUELCH. FOUND LENS BAD AND MHZ SWITCH HOUSING BAD. REPLACED SWITCH HOUSING, LENS AND FOUND POWER OUT LOW. ADJUSTED. REPLACED COIL T604. REPAIRED. ALSO FOUND MODULATION DISTORTED. REPLACED TRANSISTOR KIT Q124, Q130. REPAIRED. BENCH CHECK GOOD. 1G71 3U O H2SW 20010509001292001050900129 2001 5 9 HEEA072624 420010417G3422060001500 GYRO BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331077 51520 D.G. DOES NOT TRACK IN TURNS. 1G71 3U H2SW 20010509001302001050900130 2001 5 9 HEEA072625 420010417G3422060001500 GYRO BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331077 51520 CAUSES HIS TO STICK AND BE ERRATIC. 1G71 3U H2SW 20010509001312001050900131 2001 5 9 HEEA072626 420010417G3444066106103 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER ERRATIC E HEEAK NONE O OTHER ININSP/MAINT 1 SW038591X 51495 ERRATIC AND INACCURATE READINGS. 1G71 3U H2SW 20010509001322001050900132 2001 5 9 HEEA072627 420010417G3444066106103 INDICATOR BELL 206 206L1 1182107SW RADAR ALTIMETER ERRATIC E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 RADAR ALTIMETER ERRATIC. 1G71 3U H2SW 20010509001332001050900133 2001 5 9 HEEA072628 420010417G3444066106103 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03141BH 51303 WILL NOT INDICATE CORRECT ALTITUDE. 1G71 3U H2SW 20010509001342001050900134 2001 5 9 HEEA072629 420010417G3444066106103 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER ERRATIC E HEEAK NONE O OTHER ININSP/MAINT 1 SW038587X 51464 ABOVE 300 FEET READINGS ARE ERRATIC OVER ROUGH TERRAIN. 1G71 3U H2SW 20010509001352001050900135 2001 5 9 HEEA072631 420010417G3444066106103 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW0330KH 51527 50 FOOT INDICATING ERROR. 1G71 3U H2SW 20010509001362001050900136 2001 5 9 HEEA072632 420010417G3452066106200 TRANSCEIVER BELL 206 206L3 1182108SW COCKPIT DEFECTIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW033116P 51530 KNOB DEFECTIVE. PERFORMED PRELIMINARY INSPECTION. REPLACED KNOB SHAFT. TRANSMIT POWER WEAK. INSTALLED V101 REPAIRED. FOUND UNIT MISSING IDENT BUTTON. INSTALLED BUTTON. ADJUSTED PULSE WIDTH. BENCH CHECK GOOD. 1G71 3U H2SW 20010509001372001050900137 2001 5 9 HEEA072633 420010417G3452066106200 TRANSPONDER BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 TRANSPONDER WILL NOT TRANSMIT. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT NOT RECEIVING OR TRANSMITTING. FOUND V101 TUBE BAD. REPLACED V101 TUBE. REPAIRED. ALSO FOUND SWITCH PANEL BAD. REPLACED. BENCH CHECK GOOD. 1G71 3U H2SW 20010509001382001050900138 2001 5 9 HEEA072634 420010417G3452066106200 TRANSPONDER BELL 206 206L4 1182110SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037077F 52038 REPLY LIGHT INOPERATIVE. 1G71 3U NCH2SW 20010509001392001050900139 2001 5 9 HEEA072635 420010417G3452066106200 TRANSPONDER BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036160Y 51609 WILL NOT COME ON. 1G71 3U H2SW 20010509001402001050900140 2001 5 9 HEEA072636 420010417G3452066106200 TRANSPONDER BELL 206 206L3 1182108SW COCKPIT INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331821 51076 TRANSMITS INTERMITTENTLY. MTL LOW. CANNOT MEASURE FREQUENCY. 1G71 3U H2SW 20010509001412001050900141 2001 5 9 HEEA072637 420010417G3451066106600 TRANSCEIVER BELL 212 212 1181420SW DME MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035009N 30936 NO OUTPUT TO THE INDICATOR. 1G71 4U H4SW 20010509001422001050900142 2001 5 9 HEEA072638 420010417G3431066107800 RECEIVER BELL 412 412 1182202SW VOR MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R 36007 MARKER BEACON WOULD NOT TEST. PERFORMED PRELIMINARY INSPECTION AND REPLACED FRONT CONNECTOR J6341 BECAUSE OF A BAD PIN. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20010509001432001050900143 2001 5 9 HEEA072639 420010417G3431066107800 RECEIVER BELL 412 412 1182202SW GLIDE SLOPE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 GLIDE SLOPE INOPERATIVE. PERFORMED PRELIMINARY INSPECTION AND REPLACED TRANSISTOR Q311. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20010509001442001050900144 2001 5 9 HEEA072640 420010417G3431066107800 RECEIVER BELL 412 412 1182202SW GLIDE SLOPE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 GLIDE SLOPE INOPERATIVE. PERFORMED PRELIMINARY INSPECTION AND FOUND GS NEEDLE PEGS OUT WHEN VIBRATED. REPLACED RECEPTACLES I-5 ON GLIDESLOPE BOARD. REPAIRED. ADJUSTED VOR HEADING. ADJUSTED HI/LOW SENSE ON MARKER BEACON. BENCH CHECK GOOD. 1G72 4U H4SW 20010509001452001050900145 2001 5 9 HEEA072641 420010417G3444066304400 INDICATOR BELL 412 412 1182202SW RADAR ALTIMETER ERRATIC E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 ERRATIC IN FLIGHT. 1G72 4U H4SW 20010509001462001050900146 2001 5 9 HEEA072642 420010417G3444066305401 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW038591X 51495 ERRATIC AND INACCURATE. 1G71 3U H2SW 20010509001472001050900147 2001 5 9 HEEA072643 420010417G3444066305401 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038593X 51509 WILL NOT INDICATE OR POWER UP. 1G71 3U H2SW 20010509001482001050900148 2001 5 9 HEEA072644 420010417G3444066305401 INDICATOR BELL 407 407 SW RADAR ALTIMETER INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW034999 53323 INTERMITTENT.. 1G71 3U O H2SW 20010509001492001050900149 2001 5 9 HEEA072645 420010417G3444066305401 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER READS LOW E HEEAK NONE O OTHER ININSP/MAINT 1 SW036603X 51412 NEEDLE READS LOW. SENT TO HONEYWELL, KANSAS FOR WARRANTY REPAIR. 1G71 3U H2SW 20010509001502001050900150 2001 5 9 HEEA072646 420010417G3444066305401 INDICATOR BELL 206 206L3 1182108SW RADAR ALTIMETER INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW03141BH 51303 INTERMITTENT, UNRELIABLE WHEN WORKING. SENT TO HONEYWELL, KANSAS FOR WARRANTY REPAIR. 1G71 3U H2SW 20010509001512001050900151 2001 5 9 HEEA072647 420010417G3432066400700 RECEIVER BELL 412 412 1182202SW VOR FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033911L 33023 WILL NOT RECEIVE. PERFORMED PRELIMINARY INSPECTION. REPLACED OPEN FUSE F501. REPAIRED PROBLEM. ADJUSTED LOCALIZER DEVIATION. BENCH CHECK GOOD. 1G72 4U H4SW 20010509001522001050900152 2001 5 9 HEEA072648 420010417G3453066402600 RECEIVER BELL 206 206L3 1182108SW LORAN MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038590X 51494 UNABLE TO PUT IN A DIFFERENT WAYPOINT DUE TO KNOB OUT. PERFORMED PRELIMINARY INSPECTION. FOUND S202 SWITCH BROKEN AND RETAINER RING MISSING FROM END OF PULL SCAN KNOB SHAFT. REPLACED S202 SWITCH AND RETAINER RING. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20010509001532001050900153 2001 5 9 HEEA072649 420010417G3453066402600 RECEIVER BELL 206 206L3 1182108SW LORAN INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW038588X 51486 INOPERATIVE. NO DISPLAY. 1G71 3U H2SW 20010509001542001050900154 2001 5 9 HEEA072651 420010418G3453066402600 RECEIVER BELL 206 206L3 1182108SW LORAN FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038592X 51508 SCREEN GOES BLANK AFTER EXTENDED USE. SUSPECT OVERHEATING DUE TO FAULTY COOLING FAN. 1G71 3U H2SW 20010509001552001050900155SW 2001 5 9 HEEA072652 120010418G2436163404751 VOLT REGULATOR BELL 206 206L3 1182108SW ELECTRICAL FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0330KH 51527 GENERATOR KICKS OFF LINE. 1G71 3U H2SW 20010509001562001050900156GL 2001 5 9 HEEA072653 220010418G7261174000101 FILTER BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL ENGINE OIL LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW035007Q 45187 COULD NOT GET FACET FILTER TO STOP LEAKING. 1G71 3U3 U H2SW E1GL 20010509001572001050900157GL 2001 5 9 HEEA072654 220010418G7261174000103 FILTER BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE OIL LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW036610C 51425 UNABLE TO STOP FILTER HOUSING FROM LEAKING. SENT TO PUROLATOR FACETS FOR INSPECTION AND REPAIR. 1G71 3U3 U H2SW E1GL 20030815000502003081500050SW 2003 8 15 HEEA072655 120010418G79101740352 INDICATOR BELL 206 206L1 1182107SW ENGINE OIL DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 BUTTON WOULD NOT EXTEND DURING BYPASS CHECK. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010509001582001050900158NE 2001 5 9 HEEA072657 220010418G7412103815504 EXCITER BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE WEAK E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 WEAK. 1G72 4U4 U H4SW E22EA 20010509001592001050900159 2001 5 9 HEEA072658 420010418G34251113025 INDICATOR BELL 412 412 1182202SW HSI INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 CDI OFF FLAG DISPLAYS INTERMITTENTLY. SENT TO MASCO FOR WARRANTY REPAIR. 1G72 4U H4SW 20010509001602001050900160 2001 5 9 HEEA072659 420010418G34251113025 INDICATOR BELL 412 412 1182202SW HSI PRECESSES E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 PRECESSES. 1G72 4U H4SW 20010509001612001050900161 2001 5 9 HEEA072660 420010418G34211113034 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 RT FLAG STICKS TO THE RIGHT. 1G72 4U H4SW 20010509001622001050900162 2001 5 9 HEEA072661 420010418G34211113034 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 ADI TUMBLES WHEN POWER IS APPLIED. 1G72 4U H4SW 20010509001632001050900163GL 2001 5 9 HEEA072662 220010418G7261174000101 FILTER BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE OIL LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW033116P 51530 LEAKING. 1G71 3U3 U H2SW E1GL 20010509001642001050900164 2001 5 9 HEEA072663 420010418G2300122024102 CONTROL UNIT BELL 407 407 SW COCKPIT INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03495PH 53397 INOPERATIVE. LIGHTS WONT PULSE AND WONT ILLUMINATE. 1G71 3U O H2SW 20010509001652001050900165SW 2001 5 9 HEEA072664 120010418G3340122024102 CONTROL UNIT BELL 407 407 SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03719PH 53266 WHEN BATTERY SWITCH IS TURNED ON, FWD LANDING WOULD NOT TURN OFF. ALSO FWD LIGHT WOULD NOT PULSATE. 1G71 3U O H2SW 20010509001662001050900166 2001 5 9 HEEA072666 420010418G23114000038 TRANSMITTER BELL 206 206L4 1182110SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037074W 52033 CANNOT GET SQUELCH TEST OR ANY TRANSMISSION FROM ANY CHANNEL ON FM RADIO. REPLACED VOLUME CONTROL, VOLUME KNOB AND FRONT PANEL. REPAIRED. BENCH CHECK GOOD. 1G71 3U NCH2SW 20010509001672001050900167 2001 5 9 HEEA072667 420010418G23114000038 TRANSMITTER BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 RATCHETING VOLUME KNOB. REPLACED VOLUME POTENTIOMETER. REPAIRED PROBLEM. BENCH CHECK GOOD. 1G72 4U H4SW 20010509001682001050900168 2001 5 9 HEEA072668 420010418G23114000038 TRANSMITTER BELL 206 206L3 1182108SW COCKPIT INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW036251X 51552 INTERMITTENT. REPLACED VOLUME POTENTIOMETER, VOLUME KNOB AND CHANNEL KNOB. REPAIRED PROBLEM. BENCH CHECK GOOD. 1G71 3U H2SW 20010509001692001050900169 2001 5 9 HEEA072669 420010418G23124000103000 TRANSCEIVER BELL 206 206L1 1182107SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035744Y 45465 HIGH LEVEL OF SQUELCH BLEEDING OVER INTO ALL AUDIO SYSTEMS. FOUND CORROSION ON UNIT. CLEANED CORROSION FROM UNIT. FOUND INTERMITTENT TRANSMIT ON HIGHER FREQUENCIES 469.9875 MHZ. ALIGNED TRANSMITTER TO SPECS. BENCH CHECK GOOD. 1G71 3U H2SW 20010509001702001050900170 2001 5 9 HEEA072670 420010418G23124000103000 TRANSCEIVER BELL 206 206L1 1182107SW COCKPIT INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW035744Y 45465 FM UHF BAND INTERMITTENTLY DOES NOT TRANSMIT OR RECEIVE. 1G71 3U H2SW 20010509001712001050900171 2001 5 9 HEEA072671 420010418G22114033089901 COMPUTER BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03108X 33115 WONT HOLD ALTITUDE. 1G72 4U H4SW 20010509001722001050900172SW 2001 5 9 HEEA072672 120010418G6710412001300105 BELLCRANK BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893N 33010 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509001732001050900173SW 2001 5 9 HEEA072673 120010418G6220412010216105 BEARING BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 BEARING RETAINING RING POPPED OUT OF GROOVE. ALSO BEARING SPINS IN HOUSING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509001742001050900174SW 2001 5 9 HEEA072674 120010418G6220412010216107 BEARING BELL 412 412 1182202SW MAIN ROTOR FROZEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 BEARING FROZEN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010510001182001051000118SW 2001 5 10 HEEA072675 120010418G5610412018060111 CAM BELL 412 412 1182202SW WINDOW WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 WORN WINDOW. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509001752001050900175SW 2001 5 9 HEEA072676 120010418G5310 STRUCTURE BELL 412 412 1182202SW ENGINE BAY DELAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03108X 33115 ENGINE BAY STRUCTURE DELAMINATED. 1G72 4U H4SW 20010509001762001050900176SW 2001 5 9 HEEA072677 120010418G6220412030437103 CAP BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032298Z 33077 RUBBER IS DAMAGED. 1G72 4U H4SW 20010509001772001050900177SW 2001 5 9 HEEA072678 120010418G6220412030437103 CAP BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893N 33010 RUBBER LORD MOUNT WEAR FROM OIL. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509001782001050900178SW 2001 5 9 HEEA072679 120010418G6220412030437103 CAP BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033911L 33023 RUBBER WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509001792001050900179SW 2001 5 9 HEEA072680 120010418G6220412030437103 CAP BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R 36007 RUBBER EXTRUDED. 1G72 4U H4SW 20010509001802001050900180SW 2001 5 9 HEEA072681 120010419G6710214001347005 ACTUATOR BELL 412 412 1182202SW MAIN ROTOR STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 FORCE TRIM STICKING. 1G72 4U H4SW 20010509001812001050900181SW 2001 5 9 HEEA072682 120010419G7330206364601101 TRANSMITTER BELL 206 206L3 1182108SW FUEL SYSTEM MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 UNABLE TO CALIBRATE FUEL SYSTEM. 1G71 3U H2SW 20010509001822001050900182SW 2001 5 9 HEEA072683 120010419G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 WILL NOT ENGAGE OR SPIN. 2G72 4U H10SW 20010509001832001050900183SW 2001 5 9 HEEA072684 120010419G5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 STICKS EXENDED. 1G72 4U H4SW 20010509001842001050900184 2001 5 9 HEEA072685 420010419G341344600045800 INDICATOR BELL 407 407 SW VERTICAL SPEED STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 VERTICAL SPEED INDICATOR STICKING. SENT TO MASCO FOR INSPECTION AND REPAIR. 1G71 3U O H2SW 20010509001852001050900185SW 2001 5 9 HEEA072686 120010419G7333473203003 SIGNAL COND UNIT BELL 412 412 1182202SW TRANS PUMPS FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 NR 1 AND 2 TRANSFER PUMPS WOULD NOT SHUT OFF AFTER FORWARD FUEL TANKS EMPTIED. 1G72 4U H4SW 20010509001862001050900186SW 2001 5 9 HEEA072687 120010419G7333473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FUEL SYSTEM INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 CAUSES FUEL QUANTITY INDICATOR RO READ ZERO. 1G72 4U H4SW 20010509001872001050900187SW 2001 5 9 HEEA072688 120010419G7333473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FUEL SYSTEM INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 LOW FUEL LIGHT COMES ON AT 1320 LBS. 1G72 4U H4SW 20010509001882001050900188SW 2001 5 9 HEEA072689 120010419G7333473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FUEL SYSTEM FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 LOW FUEL LIGHT COMES ON AT 1320 LBS. 1G72 4U H4SW 20010509001892001050900189SW 2001 5 9 HEEA072690 120010419G2140S5008EC3 HOSE BELL 206 206L3 1182108SW HEATER LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW0331077 51520 HOSE ASSY WIRE BRAIDING IS CHAFED AND HOSE IS LEAKING. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20010510001192001051000119SW 2001 5 10 HEEA072691 120010419G2140S5008EC3 HOSE BELL 206 206L3 1182108SW HEATER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0341128 51134 FERRULE CRACKED ON HOSE. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20010509001902001050900190SW 2001 5 9 HEEA072692 120010419G2140S5008EC3 HOSE BELL 206 206L3 1182108SW HEATER LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03206LS 51070 HEATER HOSE LEAKING FROM FITTINGS. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20010509001912001050900191SW 2001 5 9 HEEA072693 120010419G2140S50301 VALVE BELL 206 206L3 1182108SW CABIN HEAT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03206LS 51070 BALL BEARING AND SPRING CORRODED INSIDE OF VALVE. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20010509001922001050900192SW 2001 5 9 HEEA072694 120010419G2140S50301 VALVE BELL 206 206L3 1182108SW CABIN HEAT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0341128 51134 CORRODED BALL BEARING AND SPRING. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20010509001932001050900193 2001 5 9 HEEA072695 420010419G3418SC628P HORN BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 HORN HAS STEADY SOUND ONLY, MUST PULSATE. SCRAPPED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20010509001942001050900194SW 2001 5 9 HEEA072696 120010419G7714SC628P HORN BELL 206 206L1 1182107SW COCKPIT INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 WORKS INTERMITTENTLY. REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20010509001952001050900195SW 2001 5 9 HEEA072697 120010419G2140R02221 VENT BELL 412 412 1182202SW HEATER INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 HEATER INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509001962001050900196 2001 5 9 HEEA072698 420010419G3444DMC632 ANTENNA BELL 206 206L3 1182108SW RADAR ALTIMETER WEAK E HEEAK NONE O OTHER ININSP/MAINT 1 SW038594X 51531 CORRODED CAUSING WEAK RECEPTION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010509001972001050900197 2001 5 9 HEEA072699 420010419G3444DMC634A ANTENNA BELL 412 412 1182202SW RADAR ALTIMETER DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893N 33010 BASE IS DAMAGED. BASE IS CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509001982001050900198 2001 5 9 HEEA072700 420010419G2562ELT910 ELT BELL 206 206L4 1182110SW CABIN MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037077F 52038 WOULD NOT SHUT OFF. REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20010509001992001050900199SW 2001 5 9 HEEA072701 120010419G2844BSE20630G TRANSDUCER BELL 206 206L3 1182108SW FUEL PRESSURE INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 FUEL PRESSURE GAUGE INTERMITTENTLY PEGS OUT. 1G71 3U H2SW 20010509002002001050900200NE 2001 5 9 HEEA072702 220010419G7420CH5339901 LEAD BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE IGNITER BURNED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 BURN HOLE IN LEAD. 1G72 4U4 U H4SW E22EA 20010509002012001050900201 2001 5 9 HEEA072703 420010419G3423CB2100T6C COMPASS BELL 412 412 1182202SW COCKPIT LOW E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893N 33010 LOW ON FLUID. 1G72 4U H4SW 20010509002022001050900202 2001 5 9 HEEA072704 420010419G3423C2300DL4B COMPASS BELL 206 206L1 1182107SW COCKPIT INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW033178K 45765 INDICATES 25 DEGREES OFF FROM ACTUAL COURSE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010509002032001050900203 2001 5 9 HEEA072705 420010419G3423CB2100T6D COMPASS BELL 214 214ST 1182106SW COCKPIT INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW035748M 28102 HAS FRICTION LIGHT INTERMITTENT, WILL NOT CALIBRATE. 2G72 4U H10SW 20010509002042001050900204 2001 5 9 HEEA072706 420010419G3442MI5851345 INDICATOR BELL 212 212 1181420SW RADAR FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035010F 30936 DOES NOT PAINT TARGETS. FOUND UNIT HAS NO NOISE, ADJUSTED AUTOMATIC NOISE CONTROL. TROUBLESHOT VIDEO BOARD AND REPLACED R1450 RESISTOR. REPAIRED. BENCH CHECK GOOD. 1G71 4U H4SW 20010509002052001050900205 2001 5 9 HEEA072707 420010419G3442MI5851345 INDICATOR BELL 412 412 1182202SW RADAR FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 PAINTS FALSE TARGETS AND BAD TEST PATTERN. PERFORMED PRELIMINARY INSPECTION AND ADJUSTED ANC AND INTENSITY. BENCH CHECK GOOD. 1G72 4U H4SW 20010509002062001050900206 2001 5 9 HEEA072708 420010419G3442MI5851345 INDICATOR BELL 412 412 1182202SW RADAR FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 WOULD NOT GO INTO TEST MODE. ALSO HAD FALSE TARGETS ON HIGH RANGE SETTINGS. FOUND DISPLAY TEST PATTERN INTERMITTENTLY DROPPING OFF. FOUND LOGIC NR 1 BOARD CAUSING PROBLEM. REPLACED LOGIC #1 BOARD FROM P40 INDICATOR. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20010509002072001050900207 2001 5 9 HEEA072709 420010419G3442MI5851345 INDICATOR BELL 412 412 1182202SW RADAR INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 NOT PAINTING PROPER PICTURE. PERFORMED PRELIMINARY INSPECTION. FOUND SPIKES ON TEST PATTERN. TROUBLESHOT AND FOUND C1220 ON LOGIC NR 1 BOARD BAD. REPLACED C1220. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20010509002082001050900208 2001 5 9 HEEA072710 420010419G3442MI5851345 INDICATOR BELL 412 412 1182202SW RADAR INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 WHEN RADAR IS IN STANDBY MODE AZIMUTH LINES ARE VISIBLE. PERFORMED PRELIMINARY INSPECTION. FOUND LOGIC NR 2 BOARD IC U1346 HAS COLD SOLDER JOINT ON PIN 9. RESOLDERED IC. REPAIRED. BENCH CHECK GOOD. 1G72 4U H4SW 20010509002092001050900209 2001 5 9 HEEA072711 420010419G2561PHI10090 LIFE VEST BELL 206 206L4 1182110SW CABIN WILL NOT TEST E HEEAK NONE L NO TEST ININSP/MAINT 1 SW037074W 52033 FAILED TO PASS 3 MONTH INFLATION TEST. 1G71 3U NCH2SW 20010509002112001050900211 2001 5 9 HEEA072713 420010419G2340AA34300 INTERPHONE BELL 412 412 1182202SW CABIN INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 INOPERATIVE - LOW RECEIVE AUDIO. 1G72 4U H4SW 20010509002122001050900212 2001 5 9 HEEA072714 420010419G2340AA34300 INTERPHONE BELL 206 206L1 1182107SW CABIN MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0327766 45312 SENSITIVITY TOO LOW. 1G71 3U H2SW 20010509002132001050900213 2001 5 9 HEEA072715 420010419G2340AA95759 CONTROLLER SNIAS 350 AS350B 8680801EU AUDIO MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03971AE 3230 MIC STAYS HOT IN VOX POSITION. SENT TO NORTHERN AIRBORNE TECHNOLOGY FOR INSPECTION AND REPAIR. 1G71 3U H9EU 20010509002142001050900214 2001 5 9 HEEA072716 420010419G2340A3016W INTERPHONE BELL 412 412 1182202SW CABIN WEAK E HEEAK NONE O OTHER ININSP/MAINT 1 SW032298Z 33077 BOTH VHF RADIOS WEAK AND GARBLED. PERFORMED PRELIMINARY INSPECTION. FOUND TRANSMIT LEVELS R36-R41 SET TOO LOW. SET LEVELS TO 9V. REPAIRED. ALSO FOUND LIGHT PANEL AND VOLUME AND TRANSMIT KNOBS BAD. REPLACED. BENCH CHECK GOOD. 1G72 4U H4SW 20010509002152001050900215 2001 5 9 HEEA072717 420010419G2340A3016W INTERPHONE BELL 212 212 1181420SW CABIN MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW031074C 30989 NO AUDIO OUT AT ANY POSITION ON ROTARY SELECTOR. FOUND R36-R41 TRANSMIT LEVELS ADJUSTED ALL THE WAY DOWN. ALSO FOUND SWITCHES S1, S2, S3, S11, LIGHT PANEL, TRANSMIT AND VOLUME KNOBS ALL BAD. ADJUSTED TRANSMIT LEVELS ON R36-R41 AND REPLACED ALL BAD PARTS. REPAIRED. BENCH CHECK GOOD. 1G71 4U H4SW 20010509002162001050900216 2001 5 9 HEEA072718 420010419G2564ACR108BP LIFE RAFT BELL 206 206L3 1182108SW EMERGENCY EQUIP DISLODGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0330KH 51527 DURING POSTFLIGHT INSPECTION, NOTICED THAT LIFE RAFT WAS COMING OUT OF COVER. FURTHER INVESTIGATION FOUND THAT INFLATION BOTTLE VALVE WAS SLOWLY LEAKING GAS INTO THE RAFT. SENT TO OFFSHORE HELICOPTER SUPPORT FOR WARRANTY REPAIR. 1G71 3U H2SW 20010509002172001050900217SW 2001 5 9 HEEA072719 120010419G3030 HEATER BELL 412 412 1182202SW PITOT TUBE INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032261D 33076 HEATER INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509002182001050900218SW 2001 5 9 HEEA072720 120010419G2422ASH5845 INVERTER BELL 212 212 1181420SW ELECTRICAL FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03102PH 30899 NO VOLTAGE OUTPUT. 1G71 4U H4SW 20010509002192001050900219SW 2001 5 9 HEEA072721 120010419G6320412040123101 QUILL ASSY BELL 412 412 1182202SW ROTOR BRAKE LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 ROTORBRAKE QUILL LEAKING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509002202001050900220SW 2001 5 9 HEEA072722 120010419G5320412060802117 BRACKET BELL 412 412 1182202SW FUSELAGE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509002212001050900221SW 2001 5 9 HEEA072723 120010419G5210 BEARING BELL 412 412 1182202SW HINGE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 BEARINGS WORN AND MAKING MUD. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509002222001050900222SW 2001 5 9 HEEA072724 120010419G5210412060804101 HINGE BELL 412 412 1182202SW PAX DOOR BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 BROKEN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509002232001050900223SW 2001 5 9 HEEA072725 120010419G5330412070528107 PANEL BELL 412 412 1182202SW FUSELAGE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 CRACKED. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509002242001050900224SW 2001 5 9 HEEA072727 120010419G2422412075101103 INVERTER BELL 412 412 1182202SW ELECTRICAL FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 WOULD NOT TURN ON. 1G72 4U H4SW 20010509002252001050900225 2001 5 9 HEEA072728 420010419G3442 PLATE BELL 412 412 1182202SW ANTENNA MISSING E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 FACE PLATE MISSING. 1G72 4U H4SW 20010509002262001050900226 2001 5 9 HEEA072729 420010419G22114025008918 COMPUTER BELL 412 412 1182202SW AFCS FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033911L 33023 KICK OFF IN FLIGHT AND WANDERS AFTER SET IN CRUISE FLIGHT. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010509002272001050900227SW 2001 5 9 HEEA072730 120010419G6220407010101101 YOKE BELL 407 407 SW MAIN ROTOR HEAD DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH2481 53327 AT 2500 HOUR INSPECTION FOUND YOKE DAMAGED IN WEB AREA. ITEM WAS SENT ON FOR ULTRASONIC INSPECTION. 1G71 3U O H2SW 20010510001742001051000174 2001 5 10 HEEA072731 420010416G34578143902240B GPS SNIAS 350 AS350B 8680801EU COCKPIT FAILED E HEEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW03855PH 3351 ON CLIMB, GPS SCREEN WENT BLANK AND COCKPIT FILLED WITH A BURNT ELECTRICAL ODOR. REPLACED WITH SERVICEABLE PART. 1G71 3U H9EU 20010510001752001051000175 2001 5 10 HEEA072732 420010417G2312069102525 TRANSCEIVER SNIAS 350 AS350B2 8680813EU COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036095S 2777 DOES NOT TRANSMIT OR RECEIVE. FOUND VCO TO BE BAD. 1G71 3U H9EU 20010510001762001051000176 2001 5 10 HEEA072733 420010417G3444066106103 INDICATOR SNIAS 350 AS350B2 8680813EU RADAR ALTIMETER MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036095S 2777 WILL NOT SELF TEST PROPERLY. 1G71 3U H9EU 20010510001772001051000177EU 2001 5 10 HEEA072734 120010419G2422SS50 INVERTER SNIAS 350 AS350B 8680801EU ELELCTRICAL FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03970AE689 3235 NOT CHARGING MEDICAL EQUIPMENT. 1G71 3U H9EU 20010509002282001050900228SW 2001 5 9 HEEA072746 120010423G2435206062200113 STARTER GEN BELL 407 407 SW ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03740PH276 53435 FAILED 300 HOUR INSPECTION. 1G71 3U O H2SW 20010509002292001050900229SW 2001 5 9 HEEA072747 120010423G6720C807382 CONTROL ROD BELL 407 407 SW TAIL ROTOR INTERFERENCE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03998SP127 53403 INSPECTION OF INTERFERENCE BETWEEN T/R CONTROL TUBE AND N1 TELEFLEX CABLE IN ROOF BEAM. INSPECTION DUE TO FINDING A N1 TELEFLEX CABLE ROUTED THROUGH THE WRONG LIGHTENING HOLE AND INTERFERING WITH THE T/R CONTROL TUBE. 1G71 3U O H2SW 20010509002302001050900230SW 2001 5 9 HEEA072748 120010423G2913214076334101 PUMP BELL 214 214ST 1182106SW HYD SYSTEM LEAKING E HEEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0359806 28140 WHILE IN CRUISE FLIGHT, LOST UTILITY HYDRAULIC POWER. RETURNED TO BASE FOR MAINTENANCE. 2G72 4U H10SW 20010509002312001050900231SW 2001 5 9 HEEA072749 120010424G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 KICKING OFF AT START. 2G72 4U H10SW 20010509002322001050900232SW 2001 5 9 HEEA072751 120010424G6300214030603111 SUPPORT BRACKET BELL 214 214ST 1182106SW MAIN ROTOR MISMANUFACTURED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 BEARING DOES NOT FIT IN BEARING BORE. 2G72 4U H10SW 20010510001202001051000120SW 2001 5 10 HEEA072752 120010424G6300214030603111 SUPPORT BELL 214 214ST 1182106SW MAIN ROTOR MISMANUFACTURED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 BEARING DOES NOT FIT IN BEARING BORE. 2G72 4U H10SW 20010510001212001051000121SW 2001 5 10 HEEA072753 120010424G2730214001970111 ACTUATOR BELL 214 214ST 1182106SW NR 1 ELEVATOR MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 NR 1 ELEVATOR WONT STAY ON LINE. 2G72 4U H10SW 20010510001222001051000122SW 2001 5 10 HEEA072754 120010424G6300206001364001 TRUNNION BELL 206 206L3 1182108SW MAIN ROTOR DR RATCHETING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 BEARING RATCHETING. 1G71 3U H2SW 20010510001232001051000123SW 2001 5 10 HEEA072762 120010427G6710214001347005 ACTUATOR BELL 214 214ST 1182106SW ROTARY STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 STICKS INTERMITTENTLY. 2G72 4U H10SW 20010510001242001051000124SW 2001 5 10 HEEA072763 120010427G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 WILL NOT START ON AIRCRAFT BATTERIES. 2G72 4U H10SW 20010510001252001051000125SW 2001 5 10 HEEA072764 120010427G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 WILL NOT START ON AIRCRAFT BATTERIES. 2G72 4U H10SW 20010510001262001051000126SW 2001 5 10 HEEA072765 120010427G2730214001970111 ACTUATOR BELL 214 214ST 1182106SW ELEVATOR MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 NR 1 ELEVATOR KICKS OFF LINE. 2G72 4U H10SW 20010510001272001051000127SW 2001 5 10 HEEA072766 120010427G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 WILL NOT ENGAGE. 2G72 4U H10SW 20010510001782001051000178EU 2001 5 10 HEEA072767 120010423G5510 STRUCTURE SNIAS 350 AS350B 8680801EU STABILIZER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03854PH887 3248 CRACKED. 1G71 3U H9EU 20010515004332001051500433NE 2001 5 15 HEEA072890 220010501G720070BM041720 TURBINE SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1D NE ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03973AE831 3229 22126 HIGH OIL CONSUMPTION. SENT TO TURBOMECA FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. 1G71 3U3 U H9EU E19EU 20010515004342001051500434NE 2001 5 15 HEEA072891 220010501G720070BM041720 TURBINE SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1D NE ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03971AE685 3230 22072 HIGH OIL CONSUMPTION. SENT TO TURBOMECA FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. 1G71 3U3 U H9EU E19EU 20010515004422001051500442SW 2001 5 15 HEEA072893 120010430G6210206015001115 BLADE BELL 206 206L3 1182108SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038592X120 51508 NUMBER ONE FINGER ON UPPER SURFACE TRAILING EDGE HAS 7 INCHES OF THE FINGER MISSING. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT. 1G71 3U H2SW 20010515004432001051500443SW 2001 5 15 HEEA072894 120010430G6300214040844109 RETAINER BELL 214 214ST 1182106SW M/R DRIVE CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 PITTING ON SPRAGS. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT. 2G72 4U H10SW 20010515004442001051500444SW 2001 5 15 HEEA072895 120010501G2910212076176001 TUBE BELL 412 412 1182202SW HYD SYSTEM CRACKED E HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW033911L 33023 DURING CRUISE FLIGHT THE NR 1 HYDRAULIC SYSTEM LIGHT CAME ON. MAINTENANCE FOUND A CRACKED TUBE. 1G72 4U H4SW 20010515004452001051500445SW 2001 5 15 HEEA072896 120010501G2910M832481906 O-RING BELL 214 214ST 1182106SW HYD MOTOR LEAKING E HEEAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW0359806 28140 THE UTILITY HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE REPLACED LEAKING O-RINGS ON HYDRAULIC MOTOR. 2G72 4U H10SW 20010515004462001051500446SW 2001 5 15 HEEA072897 120010501G2910M832481904 O-RING BELL 214 214ST 1182106SW HYD MOTOR LEAKING E HEEAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW0359806 28140 THE UTILITY HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE REPLACED LEAKING O-RINGS ON HYDRAULIC MOTOR. 2G72 4U H10SW 20010515004472001051500447SW 2001 5 15 HEEA072898 120010501G2910214076333103 MOTOR BELL 214 214ST 1182106SW HYD SYSTEM SEIZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0359806 28140 THE UTILITY HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE REPLACED SEIZED HYDRAULIC MOTOR. 2G72 4U H10SW 20010515004482001051500448SW 2001 5 15 HEEA072899 120010501G62302005712103D BOLT BELL 206 206L1 1182107SW SWASHPLATE CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035014V 45217 CORROSION PITTING ON SURFACE OF BOLTS. REPLACED WITH SERVICEABLE BOLTS. 1G71 3U H2SW 20010515004492001051500449SW 2001 5 15 HEEA072900 120010501G3040204070907001 CONVERTER BELL 412 412 1182202SW WINDSHIELD WIPERINOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 CONVERTER INOPERATIVE. 1G72 4U H4SW 20010515004502001051500450SW 2001 5 15 HEEA072901 120010501G2140205072277009 VALVE BELL 412 412 1182202SW HEATER FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 WILL NOT REGULATE TEMPERATURE, STAYS FULL HOT. 1G72 4U H4SW 20010515004512001051500451SW 2001 5 15 HEEA072902 120010501G5230 STRUCTURE BELL 206 206L3 1182108SW CARGO DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036160Y 51609 CRACKED IN SEVERAL PLACES. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010515004522001051500452SW 2001 5 15 HEEA072903 120010501G6710206001343001 ELBOW BELL 206 206L1 1182107SW CYCLIC CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035014V 45217 CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010515004532001051500453SW 2001 5 15 HEEA072904 120010501G6710206001344001 CYCLIC STICK BELL 206 206L1 1182107SW COCKPIT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035014V 45217 CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010515004542001051500454SW 2001 5 15 HEEA072905 120010501G6710206001396001 SHAFT BELL 206 206L3 1182108SW CYCLIC STICK STRIPPED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331077 51520 THREADS STRIPPED ON SHAFT; PILOT WAS UNABLE TO FRICTION DOWN CYCLIC STICK. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010515004552001051500455SW 2001 5 15 HEEA072906 120010501G6710206001397101 PIVOT SUPPORT BELL 206 206L3 1182108SW CYCLIC DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03206LS 51070 BORE FOR BARREL NUTS DAMAGED BEYOND LIMITS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010515004562001051500456SW 2001 5 15 HEEA072907 120010501G6710 BEARING BELL 206 206L1 1182107SW BELLCRANK DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035019F RE1927 45244 BEARING UNSTAKED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010515004572001051500457SW 2001 5 15 HEEA072908 120010501G6710 BEARING BELL 206 206L1 1182107SW BELLCRANK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP RE1303 45521 WORN BEARINGS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010515004582001051500458SW 2001 5 15 HEEA072909 120010501G6710 BEARING BELL 206 206L1 1182107SW BELLCRANK DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP RE3050 45521 CENTER BEARING UNSTAKED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010515004592001051500459SW 2001 5 15 HEEA072910 120010501G6710 BEARING BELL 206 206L1 1182107SW BELLCRANK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW035019F 45244 WORN BEARING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010515004602001051500460SW 2001 5 15 HEEA072911 120010501G6710 BEARING BELL 206 206L3 1182108SW BELLCRANK DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 BEARING UNSTAKED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010515004612001051500461SW 2001 5 15 HEEA072912 120010501G6710 WASHER BELL 206 206L4 1182110SW BELLCRANK UNBONDED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037077F 52038 WASHER UNBONDED AND BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20010515004622001051500462SW 2001 5 15 HEEA072913 120010501G6710 BEARING BELL 206 206L1 1182107SW BELLCRANK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW0345RP 45521 WORN BEARINGS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010515004632001051500463SW 2001 5 15 HEEA072914 120010501G6710 PAD BELL 206 206L3 1182108SW BELLCRANK UNBONDED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0341128 51134 BUFFER PADS NEAR BEARINGS UNBONDED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010726000822001072600082GL 2001 7 26 HEEA073007 220010511G72616892846 LINE BELL 407 407 SW ALLSN 250C 250C47B GL COMPRESSOR CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03417PH 53038 CAE847194 LINE IS CHAFED. REPLACED LINE. 1G71 3U3 UO H2SW E1GL 20010726000842001072600084NE 2001 7 26 HEEA073008 120010511G24356854424 SEAL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL STARTER GEN DISLODGED E HEEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW031546K 760082 CAE890071S IN CRUISE FLIGHT, NR 1 ENGINE OIL PRESSURE BEGAN TO FLUCTUATE BETWEEN GREEN ARC AND LOWER RED ARC. MAINTENANCE FOUND STARTER GENERATOR SEAL UNSEATED. REPLACED, SERVICED ENGINE OIL SYSTEM AND RETURNED AIRCRAFT TO SERVICE. 1G72 3U3 U H1NE E1GL 20010726000862001072600086NE 2001 7 26 HEEA073009 120010511G3212 VALVE SKRSKYS76 S76A 8143006NE FLOAT BOTTLE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 WHILE IN FLIGHT THE LT NOSE FLOAT ASSEMBLY STARTED TO DEPLOY. MAINTENANCE FOUND FLOAT VALVE LEAKING INTERNALY AND STARTED TO INFLATE BAG. 1G72 3U H1NE 20010803000872001080300087 2001 8 3 HEEA073010 420010514G3140 LIGHT COCKPIT ILLUMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 INSTRUMENT PANEL LIGHT WILL NOT EXTINGUISH. 20010726000902001072600090NE 2001 7 26 HEEA073011 220010518G7230 BLADE SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1D NE COMPRESSOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03971AE720 3230 22072 CRACKED COMPRESSOR BLADE. 1G71 3U3 U H9EU E19EU 20010726000962001072600096NE 2001 7 26 HEEA073012 220010518G7230 BLADE SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1D NE COMPRESSOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03971AE720 3230 22072 CRACKED COMPRESSOR BLADE. 1G71 3U3 U H9EU E19EU 20010726001022001072600102SW 2001 7 26 HEEA073013 120010507G2450 HARNESS BELL 412 412 1182202SW COCKPIT CHAFED E HEEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW03142PH 33150 WHILE IN CRUISE FLIGHT THE 115 VOLT AFCS CIRCUIT BREAKER POPPED. MAINTENANCE TURNED BATTERY POWER ON AND THE MASTER CAUTION PANEL CIRCUIT BREAKER POPPED ALSO, WITH VISIBLE SMOKE. FOUND CHAFED WIRE BUNDLE WHERE IT EXITS WINDSHIELD POST AREA AT FORWARD EDGE OF R/H PANEL. 1G72 4U H4SW 20010726001132001072600113SW 2001 7 26 HEEA073014 120010507G7933407375004101 INDICATOR BELL 407 407 SW COCKPIT READS HIGH E HEEAK NONE N FALSE WARNING ININSP/MAINT 1 SW03740PH 53435 READS HIGH 150+ AT TIMES THEN GOES TO 130 WHICH IS STILL 5 TO 10 PSI HIGH PER DIRECT READING GAUGE. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#715195. 1G71 3U O H2SW 20010726001202001072600120SW 2001 7 26 HEEA073015 120010507G6300407310203101 MOUNT BELL 407 407 SW MAIN ROTOR SEPARATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH991 53386 MOUNT SEPARATED. 1G71 3U O H2SW 20010726001312001072600131SW 2001 7 26 HEEA073016 120010507G2424206075447101 VOLT REGULATOR BELL 407 407 SW ELECTRICAL FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 WILL NOT PICK UP LOAD. 1G71 3U O H2SW 20010726001372001072600137SW 2001 7 26 HEEA073017 120010507G6321206340301101 DISK BELL 407 407 SW ROTOR BRAKE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH3135 53142 WORN. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#715175. 1G71 3U O H2SW 20010726001452001072600145SW 2001 7 26 HEEA073022 120010507G6730212076005105 CYLINDER BELL 412 412EP 1182205SW M/R CONTROL LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW036106C196 36257 LEAKING FROM BOTTOM WEEP HOLE. 1G72 4U H4SW 20010726001462001072600146SW 2001 7 26 HEEA073023 120010507G2822407362013101 PRESSURE SWITCH BELL 407 407 SW BOOST PUMP FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH 53397 LEFT HAND BOOST PUMP LIGHT WOULD NOT COME ON. 1G71 3U O H2SW 20010726001482001072600148SW 2001 7 26 HEEA073024 120010507G7921406360500101 COOLER BELL 407 407 SW ENGINE OIL LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03510PH 53209 COOLER LEAKING. 1G71 3U O H2SW 20010726001502001072600150SW 2001 7 26 HEEA073025 120010507G6410406016100119 BLADE BELL 407 407 SW TAIL ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH 53277 VOID BETWEEN SKIN AND BLOCK. 1G71 3U O H2SW 20010726001512001072600151SW 2001 7 26 HEEA073026 120010507G3246407050201101 CROSSTUBE BELL 407 407 SW MLG CORRODED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03409PH4056 53059 CORROSION, SENDING IN FOR EVALUATION DUE TO POSSIBLE MFG. DEFECT. 1G71 3U O H2SW 20010726001532001072600153SW 2001 7 26 HEEA073027 120010507G6520406040400117FM GEARBOX BELL 407 407 SW TAIL ROTOR MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH2282 53277 TAIL ROTOR GEARBOX MAKING METAL. 1G71 3U O H2SW 20010726001542001072600154SW 2001 7 26 HEEA073028 120010507G6230406010401117 SWASHPLATE BELL 407 407 SW MAIN ROTOR ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH1231 53378 SWASHPLATE BEARING HAS A ROUGH SOUND WHEN ROTATED. 1G71 3U O H2SW 20010726001552001072600155SW 2001 7 26 HEEA073029 120010507G7714407375008101 INDICATOR BELL 407 407 SW DUAL TACH INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03722PH 53288 ROTOR NEEDLE INOPERATIVE. 1G71 3U O H2SW 20010726001562001072600156SW 2001 7 26 HEEA073030 120010507G7921406360500101 COOLER BELL 407 407 SW ENGINE OIL OVERHEATED E HEEAK NONE M OVER TEMP ININSP/MAINT 1 SW03409PH 53059 OIL COOLER OVERHEATING. 1G71 3U O H2SW 20010726001572001072600157SW 2001 7 26 HEEA073031 120010507G6220407010103101 PITCH HORN BELL 407 407 SW MAIN ROTOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH2481 53327 CORROSION BEYOND LIMITS. 1G71 3U O H2SW 20010726001582001072600158SW 2001 7 26 HEEA073032 120010507G6220406010107105 ADAPTER BELL 407 407 SW MAIN ROTOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 MAIN ROTOR HUB ADAPTER CORRODED. 1G71 3U O H2SW 20010726001612001072600161SW 2001 7 26 HEEA073036 120010507G28221C2710 CARTRIDGE BELL 407 407 SW BOOST PUMP INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW038595X 53267 BOOST PUMP CARTRIDGE INOPERATIVE. 1G71 3U O H2SW 20010726001622001072600162SW 2001 7 26 HEEA073037 120010507G6510206061432121 HOUSING BELL 407 407 SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03457PH 53147 BLOWER HOUSING CRACKED AND POPPED RIVETS. 1G71 3U O H2SW 20010726001642001072600164SW 2001 7 26 HEEA073038 120010507G6500407040316101 FLYWHEEL BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 FLYWHEEL HAS WORN SPLINES. 1G71 3U O H2SW 20010726001652001072600165SW 2001 7 26 HEEA073039 120010507G6720 BOLT BELL 407 407 SW TAIL ROTOR SEIZED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 LINK BOLT FROZEN IN BEARING. 1G71 3U O H2SW 20010726001662001072600166SW 2001 7 26 HEEA073040 120010507G3212206050247137 COVER BELL 407 407 SW FLOAT TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03719PH 53266 FLOAT COVER HAS TORN END CAPS. 1G71 3U O H2SW 20010726001672001072600167SW 2001 7 26 HEEA073041 120010507G3212212073905001 INDICATOR BELL 407 407 SW FLOAT BOTTLE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH 53397 FLOAT BOTTLE INDICATOR FULL OF WATER, NOT READABLE. 1G71 3U O H2SW 20010726001682001072600168SW 2001 7 26 HEEA073042 120010507G6220407010105101 STUD 407010100115BELL 407 407 SW DROOP STOP CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH A351 53327 STUD CRACKED. 1G71 3U O H2SW 20010726001692001072600169SW 2001 7 26 HEEA073043 120010507G6710 BEARING BELL 407 407 SW UNIVERSAL LOOSE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH610 53397 UNIVERSAL UPPER BEARING LOOSE. 1G71 3U O H2SW 20010726001702001072600170SW 2001 7 26 HEEA073044 120010507G7120407060111101 MOUNT BELL 407 407 SW ENGINE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH 53386 WORN BEARING IN ENGINE MOUNT. 1G71 3U O H2SW 20010726001762001072600176SW 2001 7 26 HEEA073045 120010507G2560 PLACARD BELL 407 407 SW SEAT BELT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH 53277 TAG UNREADABLE ON SEAT BELT. 1G71 3U O H2SW 20010726001772001072600177SW 2001 7 26 HEEA073046 120010507G2560 PLACARD BELL 407 407 SW SEAT BELT TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03417PH 53038 TAG TORN. 1G71 3U O H2SW 20010726001842001072600184SW 2001 7 26 HEEA073047 120010507G2840407362005103 SWITCH BELL 407 407 SW COCKPIT STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 SWITCH STICKS IN CLOSED POSITION. 1G71 3U O H2SW 20010726001862001072600186SW 2001 7 26 HEEA073048 120010507G3212206050247135 COVER BELL 407 407 SW FLOAT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 FLOAT COVER IS WORN. 1G71 3U O H2SW 20010726001882001072600188SW 2001 7 26 HEEA073049 120010507G3212206050247135 COVER BELL 407 407 SW FLOAT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH 53400 FLOAT COVER WORN. 1G71 3U O H2SW 20010726001892001072600189SW 2001 7 26 HEEA073050 120010507G6420407340339101 BEARING BELL 407 407 SW COOLER BLOWER NOISY E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH181 53396 BEARING MAKING NOISE. 1G71 3U O H2SW 20010726001902001072600190SW 2001 7 26 HEEA073051 120010507G321270079H100F210 HOSE BELL 407 407 SW MLG DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 SLIGHT DAMAGE NEAR FITTING. 1G71 3U O H2SW 20010726001912001072600191SW 2001 7 26 HEEA073052 120010507G6510206061432121 HOUSING BELL 407 407 SW BLOWER DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 NUT PLATES BAD. 1G71 3U O H2SW 20010726001942001072600194SW 2001 7 26 HEEA073053 120010507G6300407310203101 MOUNT BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW038595X2481 53267 WORN RUBBER ON MAIN ROTOR DRIVE MOUNT. 1G71 3U O H2SW 20010726001962001072600196SW 2001 7 26 HEEA073054 120010507G6710406010425107 LEVER BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH2366 53159 LEVER WORN AND SLOPPY. 1G71 3U O H2SW 20010726001972001072600197SW 2001 7 26 HEEA073055 120010507G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03457PH2332 53147 UNIVERSAL ON MAIN ROTOR DRIVE, WORN. 1G71 3U O H2SW 20010726002022001072600202SW 2001 7 26 HEEA073056 120010507G2560 PLACARD BELL 407 407 SW SEAT BELT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03721PH 53278 BAD LABELS. 1G71 3U O H2SW 20010726002032001072600203SW 2001 7 26 HEEA073057 120010507G2560 PLACARD BELL 407 407 SW SEAT BELT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03721PH 53278 BAD LABELS. 1G71 3U O H2SW 20010726002042001072600204SW 2001 7 26 HEEA073058 120010507G2560 PLACARD BELL 407 407 SW SEAT BELT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03721PH 53278 BAD LABELS. 1G71 3U O H2SW 20010726002052001072600205SW 2001 7 26 HEEA073059 120010507G2560 PLACARD BELL 407 407 SW SEAT BELT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03721PH 53278 BAD LABELS. 1G71 3U O H2SW 20010726002062001072600206SW 2001 7 26 HEEA073060 120010509G6510206061432121 HOUSING BELL 407 407 SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03510PH 53209 TAIL ROTOR OIL COOLER BLOWER HOUSING IS CRACKED. 1G71 3U O H2SW 20010726002072001072600207SW 2001 7 26 HEEA073061 120010509G2560 PLACARD BELL 407 407 SW SEAT BELT LOOSE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH 53277 LABEL COMING OFF BELT. 1G71 3U O H2SW 20010726002082001072600208SW 2001 7 26 HEEA073062 120010509G6420406312100101 BEARING 407012101111BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH 53398 53277 TAIL ROTOR BEARING WORN. 1G71 3U O H2SW 20010726002092001072600209SW 2001 7 26 HEEA073063 120010509G6310214040841101 SEAL 406040500123BELL 407 407 SW FREEWHEEL UNIT LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH A3174 53142 FREEWHEEL UNIT SEAL LEAKING. 1G71 3U O H2SW 20010726002102001072600210SW 2001 7 26 HEEA073064 120010509G6310406340102101 CARBON SEAL 406040500123BELL 407 407 SW FREEWHEEL UNIT LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH A3174 53142 CARBON SEAL LEAKING. 1G71 3U O H2SW 20010726002112001072600211SW 2001 7 26 HEEA073065 120010509G3210407040624101 TUBE BELL 407 407 SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03406PH 53198 TUBE WORN. 1G71 3U O H2SW 20010726002122001072600212SW 2001 7 26 HEEA073066 120010509G3210407040623101 LINE BELL 407 407 SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03406PH 53198 LINE WORN. 1G71 3U O H2SW 20010726002132001072600213SW 2001 7 26 HEEA073067 120010509G7921407062021101 DUCT BELL 407 407 SW OIL COOLER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03406PH 53198 OIL COOLER DUCT CRACKED. 1G71 3U O H2SW 20010726002142001072600214SW 2001 7 26 HEEA073068 120010509G6510206061432121 HOUSING BELL 407 407 SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03406PH 53198 BLOWER HOUSING CRACKED. 1G71 3U O H2SW 20010726002152001072600215SW 2001 7 26 HEEA073069 120010509G5210206064819005S SKIN BELL 407 407 SW CREW DOOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03510PH 53209 CORRODED, SENDING IN FOR EVALUATION. IT HAS BEEN DETERMINED, POSSIBLE MFG DEFECT. NO PREVENTIVE MAINT BETWEEN 2 METALS. 1G71 3U O H2SW 20010726002162001072600216SW 2001 7 26 HEEA073070 120010509G5210206064819006S SKIN BELL 407 407 SW CREW DOOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03510PH 53209 CORRODED, SENDING IN FOR EVALUATION. IT HAS BEEN DETERMINED, POSSIBLE MFG DEFECT. NO PREVENTIVE MAINT BETWEEN 2 METALS. 1G71 3U O H2SW 20010726002172001072600217SW 2001 7 26 HEEA073071 120010509G6710406310404101 ROD END BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH2977 53159 ROD END ON MAIN ROTOR IS WORN. 1G71 3U O H2SW 20010726002192001072600219SW 2001 7 26 HEEA073072 120010509G6710406010417101 LINER BELL 407 407 SW BEARING WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH 53159 BEARING LINER WORN. 1G71 3U O H2SW 20010726002202001072600220SW 2001 7 26 HEEA073073 120010509G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH463 53400 WORN BEARING. 1G71 3U O H2SW 20010726002222001072600222SW 2001 7 26 HEEA073074 120010509G6720407001026101 TUBE BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH 53059 TAIL ROTOR CONTROL TUBE HAS A WORN BEARING. 1G71 3U O H2SW 20010726002232001072600223SW 2001 7 26 HEEA073075 120010509G6510206061432121 HOUSING BELL 407 407 SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03722PH 53288 BLOWER HOUSING CRACKED. 1G71 3U O H2SW 20010726002242001072600224SW 2001 7 26 HEEA073076 120010509G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH730 53397 WORN BEARING. 1G71 3U O H2SW 20010726002252001072600225SW 2001 7 26 HEEA073077 120010509G3201206052105035 CUSHION BELL 407 407 SW MLG DEBONDED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH 53059 CUSHION UNBONDED. 1G71 3U O H2SW 20010726002262001072600226SW 2001 7 26 HEEA073078 120010509G6510206061432121 HOUSING BELL 407 407 SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH 53059 BLOWER HOUSING CRACKED. 1G71 3U O H2SW 20010726002272001072600227SW 2001 7 26 HEEA073079 120010509G6510206061432121 HOUSING BELL 407 407 SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03498PH 53399 CRACKED AND WORKING RIVETS. 1G71 3U O H2SW 20010726002282001072600228SW 2001 7 26 HEEA073080 120010509G6510406040320101 SHAFT PHIPBH40701 BELL 407 407 SW COOLER BLOWER WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH PHI0012 53207 COOLER BLOWER SHAFT HAS WORN SPLINES. 1G71 3U O H2SW 20010726002292001072600229SW 2001 7 26 HEEA073081 120010509G6310406340102101 CARBON SEAL BELL 407 407 SW TRANSMISSION LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW038595X 53267 CARBON SEAL LEAKING. 1G71 3U O H2SW 20010726002302001072600230SW 2001 7 26 HEEA073082 120010509G6720PHI407112 TRUNNION BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 TRUNNION EAR WORN. LEAKING. 1G71 3U O H2SW 20010726002312001072600231SW 2001 7 26 HEEA073083 120010509G6310406040550101 ADAPTER BELL 407 407 SW TRANSMISSION LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03722PH 53288 ADAPTER SEAL LEAKING. 1G71 3U O H2SW 20010726002322001072600232SW 2001 7 26 HEEA073085 120010509G6510407340339103 BEARING PHIPBH40701 BELL 407 407 SW COOLER BLOWER WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH190 PHI0010 53397 WORN BEARINGS. 1G71 3U O H2SW 20010726002342001072600234SW 2001 7 26 HEEA073086 120010509G6710214001347005 ACTUATOR BELL 214 214ST 1182106SW MAIN ROTOR SLOW E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 RELEASES SLOW. 2G72 4U H10SW 20010726002362001072600236SW 2001 7 26 HEEA073087 120010509G6710214001347005 ACTUATOR BELL 214 214ST 1182106SW MAIN ROTOR STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 FORE/AFT TRIM RELEASE STICKING. 2G72 4U H10SW 20010726002372001072600237SW 2001 7 26 HEEA073088 120010509G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE SLIPPED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 CLUTCH SLIPPAGE OUT OF LIMITS. 2G72 4U H10SW 20010726002392001072600239SW 2001 7 26 HEEA073089 120010509G7120209062105001 BEARING BELL 412 412 1182202SW MOUNT ROD END DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 BEARINGS EXTREMELY TIGHT. BURNISHED BEARING USING BOLT AND TURNING SLOWLY. A SLIVER OF BEARING RACE FELL OUT. APPARENTLY WHAT WAS CAUSING THE TIGHTNESS IN THE FIRST PLACE. ONCE THIS SLIVER WAS OUT THE BEARINGS ARE TOO LOOSE AND WOULD ONLY HAVE HALF ITS LIFE. 1G72 4U H4SW 20010726002422001072600242SW 2001 7 26 HEEA073090 120010511G2933222375019105 TRANSMITTER BELL 214 214ST 1182106SW HYD INDICATOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0359806 28140 NR 1 HYDRAULIC PRESSURE GAUGE MALFUNCTIONED. REPLACED PRESSURE GAUGE. 2G72 4U H10SW 20010726002432001072600243SW 2001 7 26 HEEA073091 120010511G6300407340339101 BEARING BELL 407 407 SW BLOWER SHAFT FAILED E HEEAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW03740PH223 53435 AIRCRAFT DEVELOPED A VIBRATION IN FLIGHT. FOUND FWD. BEARING ON BLOWER SHAFT FAILED. 1G71 3U O H2SW 20010726002442001072600244SW 2001 7 26 HEEA073092 120010514G7740DPUA0101 COMPUTER BELL 206 206L3 1182108SW COCKPIT FAILED E O OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0330KH 51527 INTELLASTART CAUTION LIGHTS COMES ON INTERMITTENTLY AND WILL NOT LINK TO LAPTOP COMPUTER. SYSTEM FAILED DOWNLOAD PORT TEST. 1G71 3U H2SW 20010726002462001072600246SW 2001 7 26 HEEA073093 120010514G2910 ELBOW BELL 214 214ST 1182106SW HYD SYSTEM CHAFED E HEEAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW0359806 28140 ON FINAL APPROACH, THE OIL COOLER LIGHT ILLUMINATED. FOUND THE UTILITY HYDRAULIC SYSTEM LOST FLUID. MAINTENANCE FOUND LEAK AT ELBOW WHERE THE SUPPORT HAD CHAFED THROUGH DUE TO JAM NUT BEING LOOSE. 2G72 4U H10SW 20010726002472001072600247EU 2001 7 26 HEEA073094 120010510G8010845UN01Q4AA5F SWITCH SNIAS 350 AS350B 8680801EU STARTER FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03973AE105 3229 VEMD RECORDING START SWITCH. 1G71 3U H9EU 20010726002492001072600249EU 2001 7 26 HEEA073095 120010510G6321350A32050002 BRAKE ASSY SNIAS 350 AS350B 8680801EU MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03970AE282 3235 OIL SOAKED FROM LEAKING SEAL OF INPUT. 1G71 3U H9EU 20010726002512001072600251 2001 7 26 HEEA073096 420010510G3120B1894522282A CLOCK SNIAS 350 AS350B 8680801EU COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03974AE 2653 CANNOT RESET SWEEP SECOND HAND FOR ELAPSED TIMER. 1G71 3U H9EU 20010726002522001072600252 2001 7 26 HEEA073097 420010510G3120B1894522282A CLOCK SNIAS 350 AS350B 8680801EU COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03970AE754 3235 PILOT REPORTS SECOND HAND DOESN'T FUNCTION. 1G71 3U H9EU 20010726002532001072600253EU 2001 7 26 HEEA073098 120010510G6730SC5084 SERVO SNIAS 350 AS350B 8680801EU MAIN ROTOR LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03974AE1976 2653 LEAKED AT TOP SIDE OF PISTON. 1G71 3U H9EU 20010726002552001072600255EU 2001 7 26 HEEA073099 120010510G6410355A12004008 BLADE SNIAS 350 AS350B 8680801EU TAIL ROTOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03974AE3045 2653 CRACK AT TRIM TAB AREA ON TRAILING EDGE. 1G71 3U H9EU 20010726002582001072600258EU 2001 7 26 HEEA073100 120010510G6730SC5083 SERVO SNIAS 350 AS350B 8680801EU MAIN ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03974AE374 2653 LEAKING AT UPPER PISTON SEAL AREA. 1G71 3U H9EU 20010726002602001072600260EU 2001 7 26 HEEA073101 120010510G6410355A09103601 BEARING SNIAS 350 AS350B 8680801EU TAIL ROTOR SEPARATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03973AE473 3229 SEPARATED AT EDGES. 1G71 3U H9EU 20010726002632001072600263 2001 7 26 HEEA073102 420010510G3100614764031 INDICATOR SNIAS 350 AS350B 8680801EU COCKPIT STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03854PH 3248 NEEDLE STICKS. 1G71 3U H9EU 20010726002652001072600265EU 2001 7 26 HEEA073103 120010510G2910MA12401 PRESSURE SWITCH SNIAS 350 AS350B2 8680813EU HYD SYSTEM INACCURATE E HEEAO OTHER N FALSE WARNING ININSP/MAINT 1 SW034000L 2873 INACCURATE READINGS. 1G71 3U H9EU 20010726002672001072600267 2001 7 26 HEEA073104 420010510G3100614764031 INDICATOR SNIAS 350 AS350B 8680801EU COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03854PH 3248 NOT INDICATING. 1G71 3U H9EU 20010726002702001072600270 2001 7 26 HEEA073105 420010510G3160845UN01Q4AA5F SWITCH SNIAS 350 AS350B 8680801EU VEMD FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03971AE 3230 FAILURE ON VEMD. 1G71 3U H9EU 20010726002722001072600272EU 2001 7 26 HEEA073107 120010510G3252350A75208000 DAMPER SNIAS 350 AS350B 8680801EU MLG LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03972AE295 3234 LEAKING AROUND SHAFT SEAL. 1G71 3U H9EU 20010726002852001072600285EU 2001 7 26 HEEA073109 120010510G7714G300103 WARNING SYSTEM SNIAS 350 AS350B 8680801EU ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03854PH 3248 ROTOR LIGHT DOES NOT FLASH AT LOWER RPMS. 1G71 3U H9EU 20010726002882001072600288EU 2001 7 26 HEEA073110 120010510G6240614764031 INDICATOR SNIAS 350 AS350B 8680801EU COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03854PH 3248 ROTOR NEEDLE WILL NOT GO ABOVE 340 RPM. 1G71 3U H9EU 20010726002902001072600290EU 2001 7 26 HEEA073111 120010510G6240G300102 WARNING SYSTEM SNIAS 350 AS350B2 8680813EU ROTOR MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034034Q 2918 ROTOR ALARM SYSTEM WILL NOT WORK PROPERLY. 1G71 3U H9EU 20010726003212001072600321 2001 7 26 HEEA073112 420010510G3416150201182 ALTIMETER SNIAS 350 AS350B 8680801EU COCKPIT INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03973AE 3229 150 TO 200 FEET OFF ACTUAL ALTITUDE. 1G71 3U H9EU 20010727000042001072700004EU 2001 7 27 HEEA073113 120010510G6240614764031 INDICATOR SNIAS 350 AS350B 8680801EU COCKPIT INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03856PH 3352 INDICATOR INOPERATIVE. 1G71 3U H9EU 20010727000052001072700005EU 2001 7 27 HEEA073114 120010510G634050071550020 SENSOR SNIAS 350 AS350B 8680801EU ROTOR TACH FLUCTUATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW03856PH 3352 ROTOR TACH FLUCTUATES. PIN B IN CONNECTOR WILL NOT SEAT. 1G71 3U H9EU 20010727000062001072700006EU 2001 7 27 HEEA073115 120010510G6520 BEARING SNIAS 350 AS350B2 8680813EU PITCH CONTROL CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0340466 3811 3004 PITCH CONTROL BEARINGS CRACKED. 1G71 3U H9EU 20010727000072001072700007EU 2001 7 27 HEEA073116 120010510G6410355A09103600 BEARING SNIAS 350 AS350B2 8680813EU TAIL ROTOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0340466 3004 TAIL ROTOR BEARINGS CRACKED. 1G71 3U H9EU 20010727000122001072700012SW 2001 7 27 HEEA073164 120010523G8011214060056103 STARTER BELL 214 214ST 1182106SW CLUTCH HOUSING CONTAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033897N 28106 OIL IN CLUTCH HOUSING ON 250 HOUR INSPECTION. 2G72 4U H10SW 20010727000132001072700013SW 2001 7 27 HEEA073165 120010524G33406500306N RECEPTACLE BELL 407 407 SW TAIL FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03719PH 53266 TAIL LIGHT WON'T LIGHT. SCRAPPED LOCALLY. 1G71 3U O H2SW 20010727000162001072700016SW 2001 7 27 HEEA073170 120010524G7920204040760109 FILTER ELEMENT BELL 407 407 SW ENGINE OIL MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 MAKING METAL. SCRAPPED LOCALLY. 1G71 3U O H2SW 20010727000172001072700017SW 2001 7 27 HEEA073172 120010524G7932S207A GAUGE BELL 407 407 SW OIL LEVEL CONTAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 OIL LEVEL INDICATOR HAZED. SCRAPPED LOCALLY. 1G71 3U O H2SW 20010727000492001072700049SW 2001 7 27 HEEA073191 120010524G6510206061432118 INLET BELL 407 407 SW TAIL ROTOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 INLET CRACKED; WORN. 1G71 3U O H2SW 20010727000512001072700051SW 2001 7 27 HEEA073192 120010525G2841206063633103 INDICATOR BELL 206 206L1 1182107SW FUEL QTY STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 NEEDLE STICKS THROUGHOUT SCALE INTERMITTENTLY. 1G71 3U H2SW 20010727000532001072700053SW 2001 7 27 HEEA073193 120010531G6300212340100103 SEAL BELL 212 212 1181420SW MAIN ROTOR DEFECTIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 DEFECTS FOUND ON SEAL LIP. 1G71 4U H4SW 20010727000552001072700055SW 2001 7 27 HEEA073194 120010531G6300212340105101 SEAL BELL 212 212 1181420SW MAIN ROTOR DEFECTIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 DEFECTS FOUND ON SEAL LIP. 1G71 4U H4SW 20010727000562001072700056SW 2001 7 27 HEEA073195 120010531G6300MS2764642 BEARING BELL 212 212 1181420SW MAIN ROTOR MISMARKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 MISIDENTIFIED. PICK TICKET SHOWS P/N MS27646-42 BUT TICKET HAS A BOLT P/N UNKNOWN. 1G71 4U H4SW 20010727000682001072700068SW 2001 7 27 HEEA073197 120010601G6300 BEARING BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW038595X2481 53267 WORN BEARINGS AND BOLT HOLES. SERIAL NUMBERS REMOVED ARE LK0963 AND LK1030. 1G71 3U O H2SW 20010727000712001072700071SW 2001 7 27 HEEA073198 120010601G2844407362013101 PRESSURE SWITCH BELL 407 407 SW BOOST PUMP MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03510PH 53209 BOOST PUMP LIGHT FAILED TO ILLUMINATE. 1G71 3U O H2SW 20010727000722001072700072SW 2001 7 27 HEEA073199 120010601G2820222366621103 FUEL FILTER BELL 407 407 SW ENGINE CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 FUEL FILTER CHAFED ON BOWL. 1G71 3U O H2SW 20010727000732001072700073SW 2001 7 27 HEEA073200 120010601G3110407375001105 INDICATOR BELL 407 407 SW MGT INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03493PH 53393 NO INDICATION. 1G71 3U O H2SW 20010727000762001072700076SW 2001 7 27 HEEA073201 120010601G3212206373901103 SOLENOID VALVE BELL 407 407 SW MLG FLOAT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03721PH 53278 WOULD NOT SEAT WHEN SERVICED. 1G71 3U O H2SW 20010727000852001072700085SW 2001 7 27 HEEA073202 120010601G6710 BEARING BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03498PH1291 53399 WORN BEARING. 1G71 3U O H2SW 20010727000862001072700086SW 2001 7 27 HEEA073203 120010601G2420SM20ACD300A21 RELAY BELL 407 407 SW FADEC MALFUNCTIONED E HEEAO OTHER O OTHER ININSP/MAINT 1 SW03720PH 53277 FADEC DEGRADE LIGHT 3 LIGHTS. 1G71 3U O H2SW 20010727000872001072700087SW 2001 7 27 HEEA073204 120010601G6320407040006107 GEARBOX BELL 407 407 SW MAIN ROTOR MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH2074 53199 MAIN ROTOR GEARBOX MAKING METAL. 1G71 3U O H2SW 20010727000892001072700089SW 2001 7 27 HEEA073205 120010601G2420SM20ACD300A21 RELAY BELL 407 407 SW GENERATOR MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034999 53323 INTERMITTENT START LIGHT. 1G71 3U O H2SW 20010727000912001072700091SW 2001 7 27 HEEA073206 120010601G7712407375003107 INDICATOR BELL 407 407 SW TORQUE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03501PH 53401 INDICATES APPROX. 8% LOW. INDICATES 0% AT FLIGHT IDLE. 1G71 3U O H2SW 20010727000932001072700093SW 2001 7 27 HEEA073207 120010601G7931407375004101 INDICATOR BELL 407 407 SW ENGINE OIL MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03742PH26 53461 OIL PRESSURE DROPPED TO 90 PSI. 1G71 3U O H2SW 20010727000942001072700094SW 2001 7 27 HEEA073210 120010601G7933407375004101 INDICATOR BELL 407 407 SW ENGINE OIL FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03740PH 53435 TEMP SIDE QUIT INDICATING. 1G71 3U O H2SW 20010727000952001072700095SW 2001 7 27 HEEA073214 120010601G7933407375004101 INDICATOR BELL 407 407 SW ENGINE OIL MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03723PH 53283 WHEN GAUGE GETS HOT (4 TO 6 MIN) ENG OIL PRESSURE GOES TO ZERO. 1G71 3U O H2SW 20010727000962001072700096 2001 7 27 HEEA073215 420010601G3120M803B205VBATT CLOCK BELL 407 407 SW COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03407PH 53003 LIGHT WILL NOT WORK. 1G71 3U O H2SW 20010727000972001072700097SW 2001 7 27 HEEA073216 120010601G2420SM20ACD300A21 RELAY BELL 407 407 SW FADEC FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03499PH 53400 FADEC FAULT WORD IGN I FLT. 1G71 3U O H2SW 20010727000982001072700098SW 2001 7 27 HEEA073217 120010601G3212206373901103 SOLENOID VALVE BELL 407 407 SW MLG FLOAT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038595X 53267 CANNOT SERVICE FLOAT BOTTLES. 1G71 3U O H2SW 20010727000992001072700099SW 2001 7 27 HEEA073218 120010601G2420SM20ACD300A21 RELAY BELL 407 407 SW GENERATOR STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH 53396 STICKING INTERMITTENTLY. 1G71 3U O H2SW 20010803000902001080300090SW 2001 8 3 HEEA073351 120010605G3150214175122111 PANEL BELL 214 214ST 1182106SW COCKPIT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 EXCHANGE UNIT RECEIVED INOPERATIVE. 2G72 4U H10SW 20010803000922001080300092SW 2001 8 3 HEEA073352 120010606G6710214001347005 ACTUATOR BELL 214 214ST 1182106SW CYCLIC STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 LATERAL FORCE TRIM STICKING. 2G72 4U H10SW 20010803001002001080300100SW 2001 8 3 HEEA073354 120010608G6321D01631 PAD BELL 407 407 SW ROTOR BRAKE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW038595X 53267 WORN AND GLAZED. 1G71 3U O H2SW 20010803001082001080300108SW 2001 8 3 HEEA073355 120010608G6720406312103101 LINK BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH 53378 WORN BEARINGS. SERIAL NUMBERS REMOVED ARE NHFS4534 AND NHFS4483. 1G71 3U O H2SW 20010803001092001080300109SW 2001 8 3 HEEA073356 120010608G3212206050247131 COVER BELL 407 407 SW FLOAT TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03457PH 53147 TORN AND DETERIORATED. 1G71 3U O H2SW 20010803001142001080300114SW 2001 8 3 HEEA073357 120010608G7921407062021101 DUCT BELL 407 407 SW OIL COOLER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03510PH 53209 OIL COOLER DUCT CRACKED. 1G71 3U O H2SW 20010803001152001080300115SW 2001 8 3 HEEA073358 120010608G6510206061432121 HOUSING BELL 407 407 SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH 53277 CRACKED. 1G71 3U O H2SW 20010803001162001080300116SW 2001 8 3 HEEA073359 120010608G3212212073905001 GAUGE BELL 407 407 SW MLG CONTAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03740PH 53435 WATER IN GAUGE. 1G71 3U O H2SW 20010803001172001080300117SW 2001 8 3 HEEA073360 120010608G32608869K59 SWITCH BELL 407 407 SW MLG INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 INTERMITTENT OPERATION. NO POSITIVE MOVEMENT. 1G71 3U O H2SW 20010803001282001080300128SW 2001 8 3 HEEA073361 120010608G3310FCB205AT4 RELAY BELL 407 407 SW COCKPIT INTERMITTENT E HEEAK NONE L NO TEST ININSP/MAINT 1 SW034999 53323 INTERMITTENT IGNITION WHENEVER STARTER IS LATCHED. 1G71 3U O H2SW 20010803001332001080300133SW 2001 8 3 HEEA073362 120010608G7810407063001101 EXHAUST STACK BELL 407 407 SW ENGINE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 CRACKED AT WELDED AREA. 1G71 3U O H2SW 20010803001372001080300137SW 2001 8 3 HEEA073363 120010608G6720406012129101 LINK BELL 407 407 SW TAIL ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH 53059 RATCHETY. 1G71 3U O H2SW 20010803001382001080300138SW 2001 8 3 HEEA073365 120010608G6320407340339103 BEARING PHIPBH40701 BELL 407 407 SW COOLER BLOWER ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH PHI0012 53159 ROUGH. SERIAL NUMBERS REMOVED ARE B01-0584 AND B01-0569. 1G71 3U O H2SW 20010803001392001080300139SW 2001 8 3 HEEA073366 120010608G3212212073905001 GAUGE BELL 407 407 SW MLG CONTAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03719PH 53266 MOISTURE IN GAUGE. 1G71 3U O H2SW 20010803001402001080300140SW 2001 8 3 HEEA073367 120010608G3212212073905001 GAUGE BELL 407 407 SW MLG READS LOW E HEEAK NONE O OTHER ININSP/MAINT 1 SW03719PH 53266 READS LOW. 1G71 3U O H2SW 20010803001412001080300141SW 2001 8 3 HEEA073368 120010608G6720406312103101 LINK BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW034999 53323 WORN BEARINGS. 1G71 3U O H2SW 20010803001422001080300142SW 2001 8 3 HEEA073369 120010608G6720406312103101 LINK BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW034999 53323 WORN BEARINGS. 1G71 3U O H2SW 20010803001432001080300143SW 2001 8 3 HEEA073370 120010608G3212206050247135 COVER BELL 407 407 SW FLOAT TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH 53396 END CAP TORN AND FRAYED. 1G71 3U O H2SW 20010803001442001080300144SW 2001 8 3 HEEA073371 120010608G6220406310200101 ROD END BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH 53398 BEARING WORN. 1G71 3U O H2SW 20010803001452001080300145SW 2001 8 3 HEEA073372 120010608G7100407001026101 TUBE BELL 407 407 1182206SW TAIL ROTOR WORN E K NONE O OTHER ININSP/MAINT 1 SW03720PH 53277 TAIL ROTOR CONTROL TUBE HAS A BEARING WORN. 1G71 3U O H2SW 20010803001462001080300146SW 2001 8 3 HEEA073373 120010608G2400M835362028M RELAY BELL 407 407 SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03417PH 53038 FADEC AUTO/MANUAL LIGHT COMES ON THEN GOES OUT. 1G71 3U O H2SW 20010803001472001080300147SW 2001 8 3 HEEA073374 120010608G6322407340339103 BEARING PHIPBH40701 BELL 407 407 SW COOLER BLOWER ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03498PH PHI0034 53399 ROUGH. SERIAL NUMBERS REMOVED ARE H99-2406 AND H99-2403. 1G71 3U O H2SW 20010803001482001080300148SW 2001 8 3 HEEA073375 120010608G6322406040320101 SHAFT PHIPBH40701 BELL 407 407 SW COOLER BLOWER WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03498PH PHI0034 53399 ROUGH. 1G71 3U O H2SW 20010803001492001080300149SW 2001 8 3 HEEA073376 120010608G6300407040316101 FLYWHEEL BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 WORN SPLINES. 1G71 3U O H2SW 20010803001592001080300159SW 2001 8 3 HEEA073377 120010608G6510206061432121 HOUSING BELL 407 407 SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03447PH 53114 CRACKED. 1G71 3U O H2SW 20010803001602001080300160SW 2001 8 3 HEEA073378 120010608G6300407340339103 BEARING PHIPBH40701 BELL 407 407 SW COOLER BLOWER ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH PHI0007 53059 ROUGH. SERIAL NUMBERS REMOVED ARE K98-0736 AND H99-1758. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PARTS PURCHASED. REPLACED WITH SERIAL NUMBERS SNB01-0793 AND SNB01-0755. REFERENCE: DMR#71726100 AND 71726101. LABOR CREDIT ACCOMPLISHED ON J0161088-WA (INVOICE AND DMR NO. 687026). 1G71 3U O H2SW 20010803001622001080300162SW 2001 8 3 HEEA073379 120010608G3212206050247132 COVER BELL 407 407 SW FLOAT TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH 53396 TORN. 1G71 3U O H2SW 20010803001632001080300163SW 2001 8 3 HEEA073380 120010608G2560407370720101 RESTRAINT BELL 407 407 SW COCKPIT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03404PH 53188 LABELS DETERIORATING. 1G71 3U O H2SW 20010803001652001080300165SW 2001 8 3 HEEA073381 120010608G2560407370721101 RESTRAINT BELL 407 407 SW COCKPIT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03404PH 53188 LABELS DETERIORATING. 1G71 3U O H2SW 20010803001662001080300166SW 2001 8 3 HEEA073382 120010608G6310222060084101 PRESSURE SWITCH BELL 407 407 SW M/R GEARBOX FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH 53277 ANTI ICE LIGHT WILL NOT GO OUT. 1G71 3U O H2SW 20010803001672001080300167SW 2001 8 3 HEEA073383 120010608G6510206061432121 HOUSING BELL 407 407 SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH 53159 CRACKED. 1G71 3U O H2SW 20010803001682001080300168SW 2001 8 3 HEEA073384 120010608G3310FCB205AT4 RELAY BELL 407 407 SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH 53400 CAUSED FADEC FAULT WORD IGN 1 FLT. 1G71 3U O H2SW 20010803001702001080300170SW 2001 8 3 HEEA073385 120010608G6510406040339105 BEARING 407040302101BELL 407 407 SW T/R DRIVESHAFT ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH A926 53142 VIBRATION ON TAILBOOM. BEARING ROUGH. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#71513300. LABOR CREDIT ACCOMPLISHED ON J0162309-WA (INVOICE AND DMR NO. 687029). 1G71 3U O H2SW 20010803001712001080300171SW 2001 8 3 HEEA073386 120010608G6300407040320101 SHAFT PHIPBH40701 BELL 407 407 SW COOLER BLOWER WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH PHI0020 53142 WORN SPLINES. 1G71 3U O H2SW 20010803001732001080300173SW 2001 8 3 HEEA073388 120010608G7720MS280343 BULB BELL 407 407 SW TEMP INDICATOR FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03740PH 53435 PRESSURE INDICATION READS ZERO. 1G71 3U O H2SW 20010803001742001080300174 2001 8 3 HEEA073389 420010608G3120602EN6026 SWITCH BELL 407 407 SW CLOCK FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 CAUSES FLIGHT TIME MODE OF CLOCK TO NOT WORK. 1G71 3U O H2SW 20010803001752001080300175SW 2001 8 3 HEEA073390 120010608G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW TAIL ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03447PH1110 53114 EXCESSIVE PLAY. 1G71 3U O H2SW 20010803001762001080300176SW 2001 8 3 HEEA073391 120010608G6500406040072105 SPLINE ADAPTER BELL 407 407 SW TAIL ROTOR DRIVEWORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH 53277 WORN. 1G71 3U O H2SW 20010803001772001080300177SW 2001 8 3 HEEA073392 120010608G7810407063001101 EXHAUST STACK BELL 407 407 SW ENGINE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH 53396 CRACKED. 1G71 3U O H2SW 20010803001782001080300178SW 2001 8 3 HEEA073393 120010608G291070079H000Y150 HOSE BELL 407 407 SW MLG KINKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03498PH 53399 KINKED ON 90 DEGREE END. 1G71 3U O H2SW 20010803001802001080300180SW 2001 8 3 HEEA073394 120010608G6230406310411101 BOOT BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH 53378 SMALL HOLE WORN IN BOOT. 1G71 3U O H2SW 20010803001822001080300182SW 2001 8 3 HEEA073395 120010611G3300407076501109 HARNESS BELL 407 407 SW ELECTRICAL CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH 53400 CHAFED NEAR PROBE NR 3 CONNECTOR. HARNESS NOT SECURED PROPERLY. 1G71 3U O H2SW 20010803001832001080300183SW 2001 8 3 HEEA073396 120010611G6510206061432119 BLOWER BELL 407 407 SW TAIL ROTOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH 53159 CRACKED. 1G71 3U O H2SW 20010803001842001080300184SW 2001 8 3 HEEA073397 120010611G3212206050247135 COVER BELL 407 407 SW FLOAT TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH 53159 FORWARD CAP-THREAD BARE AND TORN. 1G71 3U O H2SW 20010803001852001080300185SW 2001 8 3 HEEA073398 120010611G6300 BEARING PHIPBH40701 BELL 407 407 SW COOLER BLOWER FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03740PH PHI0002 53435 NR 1 BEARING FAILED IN FLIGHT. 1G71 3U O H2SW 20010803001862001080300186SW 2001 8 3 HEEA073399 120010611G6300 BEARING PHIPBH40701 BELL 407 407 SW COOLER BLOWER FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03740PH PHI0002 53435 NR 1 BEARING FAILED IN FLIGHT. 1G71 3U O H2SW 20010803001872001080300187SW 2001 8 3 HEEA073400 120010611G6300406040322101 BEARING PHIPBH40701 BELL 407 407 SW COOLER BLOWER FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03740PH PHI0002 53435 NR 1 BEARING FAILED IN FLIGHT. 1G71 3U O H2SW 20010803001882001080300188SW 2001 8 3 HEEA073401 120010611G6300407340339103 BEARING PHIPBH40701 BELL 407 407 SW COOLER BLOWER FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03740PH PHI0002 53435 NR 1 BEARING FAILED IN FLIGHT. SERIAL NUMBERS REMOVED ARE M00-0854 AND M00-0882. 1G71 3U O H2SW 20010803001892001080300189SW 2001 8 3 HEEA073402 120010611G6300407340339103 BEARING PHIPBH40701 BELL 407 407 SW COOLER BLOWER OVERHEATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH PHI0007 53142 DISCOLORATION OF BEARING GREASE. SERIAL NUMBERS REMOVED ARE B01-0810 AND B01-0817. 1G71 3U O H2SW 20010803001902001080300190SW 2001 8 3 HEEA073403 120010611G6510206061432121 HOUSING BELL 407 407 SW COOLER BLOWER DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH 53396 WORKING RIVETS. 1G71 3U O H2SW 20010803001912001080300191SW 2001 8 3 HEEA073405 120010611G6510206061432121 HOUSING BELL 407 407 SW COOLER BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 CRACKED. 1G71 3U O H2SW 20010803001922001080300192SW 2001 8 3 HEEA073406 120010611G6710406310404101 ROD END BELL 407 407 1182206SW MAIN ROTOR WORN E K NONE O OTHER ININSP/MAINT 1 SW03574164857 53070 MAIN ROTOR ROD END HAS WORN BEARINGS. 1G71 3U O H2SW 20010803001932001080300193SW 2001 8 3 HEEA073407 120010611G3212206050247131 COVER BELL 407 407 SW FLOAT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH 53400 VELCRO ON END CAPS WORN. 1G71 3U O H2SW 20010803001942001080300194SW 2001 8 3 HEEA073408 120010611G3212206050247132 COVER BELL 407 407 SW FLOAT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH 53400 VELCRO ON END CAPS WORN. 1G71 3U O H2SW 20010803001952001080300195SW 2001 8 3 HEEA073409 120010611G6320407040623101 LINE BELL 407 407 SW OIL SYSTEM LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 LEAKING AT FLARE. 1G71 3U O H2SW 20010803001962001080300196SW 2001 8 3 HEEA073410 120010611G6510206061432121 HOUSING BELL 407 407 SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 CRACKED IN TWO PLACES. 1G71 3U O H2SW 20010803001972001080300197SW 2001 8 3 HEEA073411 120010611G7810407063001101 EXHAUST STACK BELL 407 407 SW ENGINE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 CRACKED AROUND BASE. 1G71 3U O H2SW 20010803001982001080300198SW 2001 8 3 HEEA073412 120010611G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH654 53386 WORN BEARING. 1G71 3U O H2SW 20010803001992001080300199SW 2001 8 3 HEEA073413 120010611G6320407040623101 LINE BELL 407 407 SW OIL SYSTEM LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03408PH 53228 FLARE LEAKING. 1G71 3U O H2SW 20010803002162001080300216SW 2001 8 3 HEEA073414 120010611G6220407310101101 BEARING BELL 407 407 SW MAIN ROTOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH2331 53277 SHIM CRACKED. 1G71 3U O H2SW 20010803002192001080300219SW 2001 8 3 HEEA073416 120010611G6230406310411101 BOOT BELL 407 407 SW MAIN ROTOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 CRACKED. SCRAPPED ON SITE. 1G71 3U O H2SW 20010803002202001080300220SW 2001 8 3 HEEA073417 120010611G6321 PAD BELL 407 407 SW ROTOR BRAKE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03492PH 53390 WORN PADS. 1G71 3U O H2SW 20010803002222001080300222SW 2001 8 3 HEEA073418 120010611G6710407030211101 COVER BELL 407 407 SW COLLECTIVE BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 BROKEN. SCRAPPED ON SITE. PHI REQUESTS FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#711790. 1G71 3U O H2SW 20010803002292001080300229SW 2001 8 3 HEEA073419 120010611G6710407030211101 COVER BELL 407 407 SW COLLECTIVE BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 BROKEN. SCRAPPED ON SITE. 1G71 3U O H2SW 20010803002312001080300231SW 2001 8 3 HEEA073422 120010611G6310214040841101 SEAL BELL 407 407 SW FREEWHEEL UNIT LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03407PH 53003 LEAKING. SCRAPPED IN HOUSE. 1G71 3U O H2SW 20010803002322001080300232SW 2001 8 3 HEEA073423 120010611G291070079H000Y150 HOSE BELL 407 407 SW MLG FRAYED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH 53059 FRAYED. SCRAPPED IN HOUSE. 1G71 3U O H2SW 20010803002552001080300255EU 2001 8 3 HEEA073433 120010611G2560AFG0348056 HARNESS SNIAS 350 AS350B2 8680813EU SEAT BELT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034034Q 2918 REEL INOPERATIVE. 1G71 3U H9EU 20010803002592001080300259EU 2001 8 3 HEEA073434 120010611G2822P94B12209 PUMP SNIAS 350 AS350B 8680801EU FUEL SYSTEM INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03973AE691 3229 PUMP INTERMITTENTLY NOT COMING ON. 1G71 3U H9EU 20010803002602001080300260 2001 8 3 HEEA073437 420010611G34215040111916 GYRO SNIAS 350 AS350B 8680801EU COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03972AE 3234 TUMBLES WHEN POWER APPLIED. 1G71 3U H9EU 20010803002612001080300261EU 2001 8 3 HEEA073515 120010619G26129560132140 FIRE DETECTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ENGINE INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW034034Q 2918 9432 INTERMITTENT. 1G71 3U3 U H9EU E19EU 20010803002922001080300292NE 2001 8 3 HEEA073516 220010619G74129550173220 EXCITER SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1D NE ENGINE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03505PH 760505 INOPERATIVE. 1G72 3U3 UNCH1NE E19EU 20010806000062001080600006NE 2001 8 6 HEEA073517 220010619G73100292958050 VALVE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE ENGINE LEAKING E HEEAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03505PH1441 760505 20017 FUEL SMELL IN COCKPIT DURING START. 1G72 3U3 UNCH1NE E19EU 20010806000082001080600008NE 2001 8 6 HEEA073518 220010619G72009560115450 MAGNETIC SEAL SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1D NE ENGINE LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03856PH 3352 9728 LEAKING. 1G71 3U3 U H9EU E19EU 20010806000092001080600009NE 2001 8 6 HEEA073519 220010619G72009560137520 MAGNETIC SEAL SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1D NE ENGINE LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03856PH 3352 9728 LEAKING. 1G71 3U3 U H9EU E19EU 20010806000112001080600011NE 2001 8 6 HEEA073520 220010619G72000292005310 ENGINE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE NACELLE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03505PH1622 760505 HIGH OIL CONSUMPTION. 1G72 3U3 UNCH1NE E19EU 20010806000162001080600016NE 2001 8 6 HEEA073521 120010619G673030006762102 MANIFOLD 766500980511SKRSKYS76 S76A 8143006NE MAIN ROTOR LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 1002 CAUSING LEAKAGE BETWEEN MAIN AND BYPASS SERVO VALVES ON SYSTEM ONE ON FINAL TEST. FOUND MISSING LEE PLUG IN DRILLED PASSAGE ON SYSTEM ONE BETWEEN MAIN AND BYPASS SERVO VALVES. SENDING TO VENDOR FOR REPAIR. 1G72 3U H1NE 20010806000222001080600022 2001 8 6 HEEA073522 420010619G34427021450601 COMPUTER SKRSKYS76 S76A 8143006NE COCKPIT INOPERATIVE E O OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 WX RADAR SYSTEM INOPERATIVE. 1G72 3U H1NE 20010806000232001080600023NE 2001 8 6 HEEA073523 120010619G62307610408020047 SCISSORS SKRSKYS76 S76A 8143006NE MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034253S 760035 WORN BUSHINGS. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20010806000252001080600025NE 2001 8 6 HEEA073524 120010619G24357630007661043 DUCT SKRSKYS76 S76C 8143008NE STARTER GEN CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 CRACKED. SENDING TO VENDOR FOR REPAIR. 1G72 3U NCH1NE 20010806000272001080600027NE 2001 8 6 HEEA073525 120010619G63007635109045102 GEAR SKRSKYS76 S76A 8143006NE M/R DRIVE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 NO RIVET IN CENTER OF GEAR. SENDING TO VENDOR FOR REPAIR. 1G72 3U H1NE 20010806000292001080600029 2001 8 6 HEEA073526 420010619G31607645001098105 DISPLAY SKRSKYS76 S76C 8143008NE COCKPIT INTERMITTENT E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03505PH 760505 CENTER DISPLAY UNIT SHOWING AN INTERMITTENT FAIL FAULT ALONG WITH GIVING INTERMITTENT INCORRECT INFORMATION AND CAUSING INTERMITTENT NR 1 AND 2 ENGINE OUT WARNING LIGHTS TO COME ON IN FLIGHT. SENT TO VENDOR FOR REPAIR. 1G72 3U NCH1NE 20010806000312001080600031NE 2001 8 6 HEEA073527 120010619G21207650007901103 BLOWER SKRSKYS76 S76C 8143008NE CABIN INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 OPEN BETWEEN PINS A AND C. SENT TO VENDOR FOR REPAIR. 1G72 3U NCH1NE 20010806000342001080600034 2001 8 6 HEEA073529 420010619G22157690001802106 ACTUATOR SKRSKYS76 S76C 8143008NE AFCS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 FULL RIGHT HARD OVER. SENT TO VENDOR FOR REPAIR. 1G72 3U NCH1NE 20010806000362001080600036 2001 8 6 HEEA073530 420010619G22157690001802106 ACTUATOR SKRSKYS76 S76C 8143008NE AFCS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 SHOWS NO MOVEMENT ON INDICATOR. SENT TO VENDOR FOR REPAIR. 1G72 3U NCH1NE 20010806000382001080600038 2001 8 6 HEEA073531 420010619G22157690001802106 ACTUATOR SKRSKYS76 S76C 8143008NE AFCS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 AFCS SYSTEM SHOWS NO MOVEMENT ON INDICATOR. SENT TO VENDOR FOR REPAIR. 1G72 3U NCH1NE 20010806000402001080600040NE 2001 8 6 HEEA073532 120010619G67307826002 SERVO SKRSKYS76 S76C 8143008NE TAIL ROTOR LEAKING E HEEAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW03505PH 760505 LEAKING PAST SERVO ACTUATOR PISTON. SENT TO VENDOR FOR REPAIR. 1G72 3U NCH1NE 20010806000412001080600041 2001 8 6 HEEA073533 420010619G345781439000232 RECEIVER SKRSKYS76 S76A 8143006NE GPS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033122G 760232 WILL NOT RECOGNIZE DATA CARD. SENDING TO VENDOR FOR REPAIR. 1G72 3U H1NE 20010806000442001080600044GL 2001 8 6 HEEA073534 220010620G726123066681 FILTER HOUSING BELL 407 407 SW ALLSN 250C 250C47B GL OIL FILTER BOWL MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 OIL FILTER BOWL BYPASS BUTTON POPS CONTINUOUSLY. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20010806000492001080600049SW 2001 8 6 HEEA073535 120010620G282123066697 FILTER BELL 407 407 SW FUEL SYSTEM CLOGGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 POPPED BYPASS BUTTON. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20010806000512001080600051GL 2001 8 6 HEEA073537 220010620G732023072725 HMU BELL 407 407 SW ALLSN 250C 250C47B GL ENGINE NOISY E HEEAK NONE O OTHER ININSP/MAINT 1 SW03723PH 53283 LOUD HUMMING NOISE IN ENGINE COMPARTMENT WITH BOOST PUMPS ON. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20010806000522001080600052NE 2001 8 6 HEEA073538 220010620G72000292005310 ENGINE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE ENGINE BAY MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW03505PH1734 760505 FOUND OIL SAMPLE HAS HIGH IRON. 1G72 3U3 UNCH1NE E19EU 20010806000532001080600053NE 2001 8 6 HEEA073539 220010620G720070BMA01030 ECU SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE NR 1 ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER ININSP/MAINT 1 SW03505PH2021 760505 REVERSION LIGHT ON NR 1 THROTTLE STAYS ON. 1G72 3U3 UNCH1NE E19EU 20010806000542001080600054NE 2001 8 6 HEEA073540 120010620G2820PT06CE84SSR CONNECTOR SKRSKYS76 S76A 8143006NE NR 2 ENGINE DIRTY E HEEAO OTHER N FALSE WARNING CRCRUISE 1 SW031546K 760082 WHILE IN CRUISE FLIGHT, THE NR 2 ENGINE FUEL FLOW INDICATOR BEGAN TO FLUCTUATE. CLEANED CANNON PLUG AT TRANSMITTER. 1G72 3U H1NE 20010806000552001080600055SW 2001 8 6 HEEA073558 120010615G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 SLOW TO START. 2G72 4U H10SW 20010806000562001080600056SW 2001 8 6 HEEA073559 120010615G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 DISENGAGES DURING BATTERY START. 2G72 4U H10SW 20010806000572001080600057SW 2001 8 6 HEEA073563 120010618G6700206001552001 BELLCRANK BELL 206 206L3 1182108SW FLIGHT CONTROLS WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 PIVOT BUSHING WORN AND BEARINGS WORN. REPLACED WITH SERVICEABLE BELLCRANK ASSEMBLY. 1G71 3U H2SW 20010806000582001080600058SW 2001 8 6 HEEA073564 120010618G6700206001554001 SUPPORT FITTING BELL 206 206L3 1182108SW CYCLIC BELLCRANKWARPED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206LS 51070 CYCLIC BELLCRANK SUPPORT ASSY. WARPED. SCRAPPED AND REPLACED WITH SERVICEABLE SUPPORT ASSY. 1G71 3U H2SW 20010806000592001080600059SW 2001 8 6 HEEA073565 120010618G6710206001713101 SUPPORT BRACKET BELL 206 206L1 1182107SW MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035014V 45217 EXCESSIVE CORROSION. SCRAPPED AND REPLACED WITH SERVICEABLE SUPPORT ASSY. 1G71 3U H2SW 20010806000602001080600060SW 2001 8 6 HEEA073566 120010618G6220206010003007 CONE SET BELL 206 206L1 1182107SW M/R HEAD CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035014V 45217 CORROSION PITTING ON SURFACE OF CONES. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000642001080600064SW 2001 8 6 HEEA073567 120010618G6420206010795103 PITCH LINK BELL 206 206L3 1182108SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 WORN. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000652001080600065SW 2001 8 6 HEEA073568 120010618G6420206010795105 PITCH LINK BELL 206 206L3 1182108SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 WORN. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000662001080600066SW 2001 8 6 HEEA073569 120010618G6420206010802101 BUSHING BELL 206 206L1 1182107SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035007Q 45187 WORN. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000672001080600067SW 2001 8 6 HEEA073570 120010618G6220206011117003 RESTRAINT BELL 206 206L3 1182108SW FLAP WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206FS 51506 SPRINGS WEAK AND STICKING ARMS. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000682001080600068SW 2001 8 6 HEEA073571 120010618G6220206011117003 RESTRAINT BELL 206 206L1 1182107SW FLAP STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035019F 45244 YELLOW BLADE RESTRAINT STICKING IN STOWED POSITION. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000692001080600069SW 2001 8 6 HEEA073572 120010618G6220206011117003 RESTRAINT BELL 206 206L4 1182110SW FLAP STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037077F 52038 STICKING. REPLACED WITH SERVICEABLE ASSY. 1G71 3U NCH2SW 20010806000702001080600070SW 2001 8 6 HEEA073573 120010618G6200206011135007 BOLT BELL 206 206L3 1182108SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032619 51375 END CAP CRACKED. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000712001080600071SW 2001 8 6 HEEA073574 120010618G6400206011725001 ROD BELL 206 206L3 1182108SW TAIL ROTOR BINDING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 BINDING. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000732001080600073SW 2001 8 6 HEEA073575 120010618G6400206011725001 ROD BELL 206 206L1 1182107SW TAIL ROTOR ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0345RP 45521 ROUGH BEARING. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000742001080600074SW 2001 8 6 HEEA073576 120010618G6400206011725001 ROD BELL 206 206L3 1182108SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 WORN BEARING. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000752001080600075SW 2001 8 6 HEEA073577 120010618G5302206032308003 FRAME BELL 206 206L3 1182108SW TAIL BOOM CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341791 51465 CRACKED TAILBOOM MOUNTING RING. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000772001080600077SW 2001 8 6 HEEA073578 120010618G5302206032308103 FRAME BELL 206 206L3 1182108SW TAIL BOOM CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 TAILBOOM RING CRACKED AT ATTACHMENT HOLE. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000792001080600079SW 2001 8 6 HEEA073579 120010618G5312206033107107B BULKHEAD BELL 206 206L3 1182108SW FUSELAGE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341128 51134 SEVERE CORROSION AT LATCH AREA WHERE SHIM WAS BONDED WITH ADHESIVE. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000812001080600081SW 2001 8 6 HEEA073580 120010618G5320206033302101 CHANNEL BELL 206 206L3 1182108SW FUSELAGE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 BULKHEAD CRACKED AT LT FWD ENGINE MOUNT HOLE IN UPPER FLANGE RADIUS. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000822001080600082SW 2001 8 6 HEEA073581 120010618G5330206033310139 ACCESS PANEL BELL 206 206L3 1182108SW FUSELAGE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 CORRODED AT ACCESS PANEL AREA BEYOND LIMITS. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000842001080600084SW 2001 8 6 HEEA073582 120010618G5302206033407101 COWLING BELL 206 206L4 1182110SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 CRACKED AND CHAFED. REPLACED WITH SERVICEABLE ASSY. 1G71 3U NCH2SW 20010806000862001080600086SW 2001 8 6 HEEA073583 120010618G3212206030104023 FITTING BELL 206 206L3 1182108SW FLOAT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 RUBBER MISSING. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000882001080600088SW 2001 8 6 HEEA073584 120010618G2730 BELLCRANK BELL 206 206L3 1182108SW ELEVATOR ASSY BINDING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 BELLCRANK BEARING BINDING AT TIMES. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000922001080600092SW 2001 8 6 HEEA073585 120010618G3212206030104023 FITTING BELL 206 206L3 1182108SW FLOAT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 RUBBER MISSING. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010806000942001080600094SW 2001 8 6 HEEA073586 120010618G6330206033506101 RESTRAINT BELL 206 206L1 1182107SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0345RP 45521 WORN BEARINGS. 1G71 3U H2SW 20010806000972001080600097SW 2001 8 6 HEEA073587 120010618G6330206033516101 FLEXURE BELL 206 206L3 1182108SW TRANSMISSION DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 RUBBER DETERIORATED. 1G71 3U H2SW 20010806001392001080600139SW 2001 8 6 HEEA073588 120010618G6300206033518007 STOP BELL 206 206L3 1182108SW M/R DRIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 WORN BEARING. 1G71 3U H2SW 20010806001412001080600141SW 2001 8 6 HEEA073589 120010618G6300206033554101 LINK BELL 206 206L3 1182108SW M/ROTOR DRIVE DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341128 51134 BEARINGS SEPARATED AND DETERIORATED BEYOND LIMITS. 1G71 3U H2SW 20010806001462001080600146SW 2001 8 6 HEEA073590 120010618G6300206033554101 LINK BELL 206 206L3 1182108SW M/R DRIVE DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341128 51134 BEARINGS SEPARATED AND DETERIORATED BEYOND LIMITS. 1G71 3U H2SW 20010806001472001080600147SW 2001 8 6 HEEA073591 120010618G6300206033554101 LINK BELL 206 206L3 1182108SW M/R DRIVE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341128 51134 MECHANICAL DAMAGE BEYOND LIMITS. 1G71 3U H2SW 20010806001492001080600149SW 2001 8 6 HEEA073592 120010618G6300206033554101 LINK BELL 206 206L3 1182108SW LT PYLON DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038591X 51495 LT AFT PYLON LINK UPPER BEARING EXTRUDING. 1G71 3U H2SW 20010806001502001080600150SW 2001 8 6 HEEA073593 120010618G6300206033554101 LINK BELL 206 206L3 1182108SW M/R DRIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251Y 51556 ELASTOMERIC BEARING SEPARATED. 1G71 3U H2SW 20010806001512001080600151SW 2001 8 6 HEEA073594 120010618G6300206033554101 LINK BELL 206 206L3 1182108SW M/R DRIVE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038591X 51495 RT FWD PYLON LINK UPPER BEARING EXTRUDING. 1G71 3U H2SW 20010806001522001080600152SW 2001 8 6 HEEA073595 120010618G6300206033554101 LINK BELL 206 206L3 1182108SW M/R DRIVE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 ELASTOMERIC BEARING AT UPPER END HAS RUBBER COMING UNBONDED. 1G71 3U H2SW 20010806001582001080600158SW 2001 8 6 HEEA073596 120010618G6300206033554101 LINK BELL 206 206L3 1182108SW M/R DRIVE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0392MT 51175 ELASTOMERIC DEBONDED. 1G71 3U H2SW 20010806001592001080600159SW 2001 8 6 HEEA073597 120010618G7600206062721103 ACTUATOR BELL 206 206L1 1182107SW ENGINE CONTROLS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 SPREAD WILL NOT WORK. 1G71 3U H2SW 20010806001602001080600160SW 2001 8 6 HEEA073598 120010618G7600206062721105 ACTUATOR BELL 206 206L3 1182108SW ENGINE CONTROLS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 INTERMITTENT. 1G71 3U H2SW 20010806001612001080600161SW 2001 8 6 HEEA073599 120010618G7600206062721109 ACTUATOR BELL 206 206L3 1182108SW ENGINE CONTROLS STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038588X 51486 STICKING, WILL NOT ACTUATE. 1G71 3U H2SW 20010806001622001080600162SW 2001 8 6 HEEA073600 120010618G7600206062721109 ACTUATOR BELL 206 206L3 1182108SW ENGINE CONTROLS STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038594X 51531 STICKING, WILL NOT ACTUATE. 1G71 3U H2SW 20010806001632001080600163SW 2001 8 6 HEEA073601 120010618G7600206062721109 ACTUATOR BELL 206 206L3 1182108SW ENGINE CONTROLS STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 STICKING. 1G71 3U H2SW 20010806001642001080600164SW 2001 8 6 HEEA073602 120010618G2121206070475005 BLOWER BELL 412 412 1182202SW CABIN FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 POPS CIRCUIT BREAKER. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010806001652001080600165SW 2001 8 6 HEEA073603 120010618G2424206075447007 VOLT REGULATOR BELL 206 206L3 1182108SW GENERATOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036610C 51425 GENERATOR DROPS OFF LINE. 1G71 3U H2SW 20010806001662001080600166SW 2001 8 6 HEEA073604 120010618G3246206323017 CROSSTUBE BELL 206 206L1 1182107SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033178K 45765 CORROSION BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20010806001672001080600167SW 2001 8 6 HEEA073605 120010618G3246206323018 CROSSTUBE BELL 206 206L1 1182107SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033178K 45765 CORROSION BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20010806001682001080600168SW 2001 8 6 HEEA073606 120010618G3246206323018 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 CORROSION BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20010806001692001080600169SW 2001 8 6 HEEA073607 120010618G2842206364601101 TRANSMITTER BELL 206 206L3 1182108SW FUEL INDICATOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 WILL NOT INDICATE FUEL QUANTITY IN FORWARD CELLS. 1G71 3U H2SW 20010806002122001080600212SW 2001 8 6 HEEA073609 120010618G2437209070263003 INDICATOR BELL 412 412 1182202SW DUAL VOLT STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 NEEDLE STICKS, AMP METER SIDE. 1G72 4U H4SW 20010806002152001080600215SW 2001 8 6 HEEA073610 120010618G6720212001705001 BELLCRANK BELL 412 412 1182202SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 BEARING UNSTAKED. REPLACED WITH SERVICEABLE BELLCRANK. 1G72 4U H4SW 20010806002182001080600218SW 2001 8 6 HEEA073611 120010618G6720212001705001 BELLCRANK BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 WORN BEARINGS. REPLACED WITH SERVICEABLE BELLCRANK. 1G72 4U H4SW 20010806002202001080600220SW 2001 8 6 HEEA073612 120010618G6720212001710001 BELLCRANK BELL 412 412 1182202SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 SNAP RING MISSING FROM BEARING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010806002212001080600221SW 2001 8 6 HEEA073613 120010618G6720212060740001 BELLCRANK BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 BEARING WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010806002222001080600222SW 2001 8 6 HEEA073614 120010618G6720212060740001 BELLCRANK BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 BEARING WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010806002242001080600224SW 2001 8 6 HEEA073615 120010618G7600212061101001 BEARING BELL 412 412 1182202SW ENGINE CONTROLS WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03108X 33115 BEARING WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010806002252001080600225SW 2001 8 6 HEEA073616 120010618G7600206062721109 ACTUATOR BELL 206 206L1 1182107SW ENGINE CONTROLS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032124Z 45646 BEEP ACTUATOR INOPERATIVE. 1G71 3U H2SW 20010806002272001080600227SW 2001 8 6 HEEA073617 120010618G2810206063632101 FUEL CELL BELL 206 206L3 1182108SW FUSELAGE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 FILLED CELL WITH FUEL AND LT FWD FUEL CELL STARTING LEAKING AT WEEP HOLE. 1G71 3U H2SW 20010806002282001080600228SW 2001 8 6 HEEA073618 120010618G2840206064635101 TRANSMITTER BELL 206 206L3 1182108SW FUEL INDICTOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 CAUSES NEEDLE TO DROP TO ZERO IN FLIGHT. 1G71 3U H2SW 20010806002292001080600229SW 2001 8 6 HEEA073619 120010618G3110206070266007 INDICATOR BELL 206 206L1 1182107SW COCKPIT MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW035007Q 45187 INSTRUMENT INDICATES 3-4 PERCENT WHEN SYSTEMS ARE SHUT DOWN AND TAKES 5-6 SECONDS TO START INDICATING DURING STARTS. 1G71 3U H2SW 20010806002322001080600232SW 2001 8 6 HEEA073620 120010618G2436206075447007 VOLT REGULATOR BELL 206 206L3 1182108SW GENERATOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 GENERATOR WENT OFF LINE AND WON'T RESET. 1G71 3U H2SW 20010806002332001080600233SW 2001 8 6 HEEA073621 120010618G2436206075447007 VOLT REGULATOR BELL 206 206L3 1182108SW GENERATOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 ON FIRST START OF THE DAY, GENERATOR WILL NOT COME ON LINE. 1G71 3U H2SW 20010806002362001080600236SW 2001 8 6 HEEA073622 120010618G7714206075545005 SENSOR BELL 206 206L3 1182108SW MAIN ROTOR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 LOW RPM AUDIO COMES ON INTERMITTENTLY AT IDLE AFTER MUTE BUTTON HAS BEEN DEPRESSED. AUDIO AND LIGHT FLICKER AT 100 PERCENT N2. 1G71 3U H2SW 20010806002402001080600240SW 2001 8 6 HEEA073623 120010618G7933206075678107 INDICATOR BELL 206 206L3 1182108SW OIL TEMP FAILED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW036603X 51412 OIL TEMPERATURE WOULD NOT COME UP OFF BOTTOM OF IND. 1G71 3U H2SW 20010806002422001080600242SW 2001 8 6 HEEA073624 120010618G7714206075681105 INDICATOR BELL 206 206L3 1182108SW DUAL TACH FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 ROTOR NEEDLE DOESN'T ENGAGE UNTIL ALMOST 100 PERCENT ENGINE RPM. 1G71 3U H2SW 20010806002442001080600244SW 2001 8 6 HEEA073625 120010618G7714206075682103 INDICATOR BELL 206 206L3 1182108SW ENGINE TACH FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Y 51609 UNRELIABLE AT LOW RPM DURING STARTS. 1G71 3U H2SW 20010806002462001080600246SW 2001 8 6 HEEA073626 120010618G7714206075682107 INDICATOR BELL 206 206L3 1182108SW ENGINE TACH FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141BH 51303 INOPERATIVE. 1G71 3U H2SW 20010806002472001080600247SW 2001 8 6 HEEA073627 120010618G3246206323002M CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206FS 51506 CORROSION PITS BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20010806002502001080600250SW 2001 8 6 HEEA073628 120010618G3246206323017 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341128 51134 FWD CROSSTUBE CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20010806002512001080600251SW 2001 8 6 HEEA073629 120010618G3246206323017 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206FS 51506 CORROSION PITS BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20010806002522001080600252SW 2001 8 6 HEEA073630 120010618G3246206323018 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341128 51134 AFT CROSSTUBE CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20010806002532001080600253SW 2001 8 6 HEEA073631 120010618G3246206323018 CROSSTUBE BELL 206 206L1 1182107SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035019F 45244 CORROSION NEAR OR AT CROSSTUBE SADDLE MOUNTING AREA. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20010806002542001080600254SW 2001 8 6 HEEA073632 120010618G3246206324003 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0341128 51134 LT SKID TUBE CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20010806002552001080600255SW 2001 8 6 HEEA073633 120010618G3246206324007 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206FS 51506 CORROSION PITS BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20010806002572001080600257SW 2001 8 6 HEEA073634 120010618G3246206324008 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03206FS 51506 CORROSION PITS BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010806002582001080600258SW 2001 8 6 HEEA073635 120010618G7933206375006101 INDICATOR BELL 206 206L1 1182107SW TOT FLUCTUATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033905B 45598 FLUCTUATES WHEN VHF IS KEYED. SENT TO MASCO FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010806002602001080600260SW 2001 8 6 HEEA073636 120010618G7933206375007103 INDICATOR BELL 206 206L3 1182108SW TOT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038593X 51509 NEEDLE WENT TO ZERO. 1G71 3U H2SW 20010806002762001080600276SW 2001 8 6 HEEA073637 120010618G7160209062214001 ACTUATOR BELL 412 412 1182202SW AIR INTAKE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 INOPERATIVE. 1G72 4U H4SW 20010806002772001080600277SW 2001 8 6 HEEA073638 120010618G7923209072433101 VALVE BELL 412 412 1182202SW ENGINE OIL STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 WILL NOT OPEN - STICKS. 1G72 4U H4SW 20010806002792001080600279SW 2001 8 6 HEEA073639 120010618G7923209072433101 VALVE BELL 412 412 1182202SW ENGINE OIL CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 CANNON PLUG WAS CORRODED TO CONNECTOR AND WHEN CANNON PLUG WAS REMOVED VALVE CONNECTOR CAME OFF WITH CANNON PLUG. 1G72 4U H4SW 20010806002862001080600286 2001 8 6 HEEA073641 420010619G3454066107810 RECEIVER BELL 230 230 1182149SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0314UH 23028 CAUSES DISPLAY TO FLICKER AND TURN OFF. SENDING TO VENDOR FOR REPAIR. 1G72 3U NCH9SW 20010806002902001080600290SW 2001 8 6 HEEA073642 120010619G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T 28101 FUNCTIONAL CHECKED GOOD AND FOUND STARTER WOULD NOT STAY ENGAGED. IT WOULD KICK OFF AFTER APPROX. 5 TO 6 SECONDS. SENDING TO VENDOR FOR REPAIR. 2G72 4U H10SW 20010806002962001080600296SW 2001 8 6 HEEA073643 120010619G63226038T59P02 BLOWER BELL 214 214ST 1182106SW COOLING FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033897N 28106 SHAFT SHEARED. SENDING TO VENDOR FOR REPAIR. 2G72 4U H10SW 20010806002982001080600298 2001 8 6 HEEA073644 420010619G34570110010600 GPS BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 CANNOT FIND ITSELF. IN SHOP REPAIR. 1G72 4U H4SW 20010806003012001080600301 2001 8 6 HEEA073645 420010619G3416066104800 ALTIMETER BELL 412 412 1182202SW COCKPIT ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 DISPLAYS ERRATIC ALTITUDE. IN SHOP REPAIR. 1G72 4U H4SW 20010806003032001080600303 2001 8 6 HEEA073646 420010619G3451066106900 INDICATOR BELL 412 412 1182202SW DME/ TACAN FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 DIGITS OUT. IN SHOP REPAIR. 1G72 4U H4SW 20010806003052001080600305 2001 8 6 HEEA073647 420010619G3451066106900 INDICATOR BELL 412 412 1182202SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 SEGMENT LIGHT INTERMITTENTLY GOES BLANK IN NR 2 POSITION. IN SHOP REPAIR. 1G72 4U H4SW 20010806003062001080600306 2001 8 6 HEEA073648 420010619G3451066106902 INDICATOR BELL 412 412 1182202SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 DISPLAY FLASHES ON/OFF INTERMITTENTLY. IN SHOP REPAIR. 1G72 4U H4SW 20010806003072001080600307 2001 8 6 HEEA073649 420010619G341613012001 ALTIMETER BELL 412 412 1182202SW COCKPIT READS HIGH E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03107X 33113 READS 90 FEET HIGH. IN SHOP REPAIR. 1G72 4U H4SW 20010806003082001080600308SW 2001 8 6 HEEA073650 120010619G2121206070475005 BLOWER BELL 412 412 1182202SW CABIN FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 BURNT OUT. IN SHOP REPAIR. 1G72 4U H4SW 20010806003092001080600309SW 2001 8 6 HEEA073651 120010619G7921209011710005 TUBE BELL 412 412 1182202SW OIL COOLER WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 WORN AT LOCATION WHERE EXCLUDER SEAL RIDES. IN SHOP REPAIR. 1G72 4U H4SW 20010806003102001080600310SW 2001 8 6 HEEA073652 120010619G7921 BEARING BELL 412 412 1182202SW OIL COOLER DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 51009046 33077 BEARING RACE SPINNING. IN SHOP REPAIR. 1G72 4U H4SW 20010806003112001080600311SW 2001 8 6 HEEA073653 120010619G6320212070116009 INDICATOR BELL 412 412 1182202SW XMSN OIL READS LOW E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 READS LOW. SENDING TO VENDOR FOR REPAIR. 1G72 4U H4SW 20010806003122001080600312 2001 8 6 HEEA073654 420010619G3100212075067119 INDICATOR BELL 412 412EP 1182205SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036106C 36257 I.T.T WOULD NOT INDICATE ANY TEMP. AT ALL; NEEDLES DID NOT MOVE. SENDING TO VENDOR FOR REPAIR. 1G72 4U H4SW 20010806003142001080600314SW 2001 8 6 HEEA073655 120010619G2910212076006007 VALVE BELL 412 412 1182202SW HYD SYSTEM BYPASSING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 BYPASS BUTTON POPPED. SENDING TO VENDOR FOR REPAIR. 1G72 4U H4SW 20010806003152001080600315SW 2001 8 6 HEEA073656 120010619G3246212321103 CROSSTUBE BELL 412 412 1182202SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 FOUND CORROSION UNDER SADDLE TO A DEPTH OF .022 BEFORE TOTAL CLEAN UP. SENDING TO VENDOR FOR CREDIT. 1G72 4U H4SW 20010806003222001080600322GL 2001 8 6 HEEA073657 220010619G732325249994 GOVERNOR BELL 412 412 1182202SW ALLSN 250C 250C* GL FREE TURBINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 ACCELERATES VERY FAST. IN SHOP REPAIR. 1G72 4U3 U H4SW E4CE 20010806003252001080600325 2001 8 6 HEEA073658 420010619G22102593996333 TARSYN BELL 412 412 1182202SW AFCS INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 INTERMITTENT KICK IN THE AFCS SYSTEM WHEN SWITCHING BETWEEN SAS AND ATT MODES. IN SHOP REPAIR. 1G72 4U H4SW 20010806003272001080600327SW 2001 8 6 HEEA073659 120010619G71003024780 GEARBOX BELL 412 412 1182202SW NR 1 ENGINE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N2510 33002 TRANSFERRING OIL FROM C-BOX TO NR 1 ENGINE. IN SHOP REPAIR. 1G72 4U H4SW 20010806003282001080600328GL 2001 8 6 HEEA073660 220010619G7532312320301 BLEED VALVE BELL 412 412 1182202SW ALLSN 250C 250C* GL COMPRESSOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032298Z 33077 CAUSED COMPRESSOR STALL AT 84 PERCENT N1. SENDING TO VENDOR FOR REPAIR. 1G72 4U3 U H4SW E4CE 20010806003292001080600329SW 2001 8 6 HEEA073661 120010619G771432005007 TACH GENERATOR BELL 412 412 1182202SW NR 2 ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 NR 2 ENGINE N1 INDICATOR WENT TO ZERO IN FLIGHT. SENDING TO VENDOR FOR REPAIR. 1G72 4U H4SW 20010806003312001080600331SW 2001 8 6 HEEA073662 120010619G771232447066 CONTROL UNIT BELL 412 412 1182202SW TORQUE ERRATIC E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 ERRATIC TORQUE LIMITING, N2 DROOPING EARLY. IN SHOP REPAIR. 1G72 4U H4SW 20010806003332001080600333SW 2001 8 6 HEEA073663 120010619G771232447066 CONTROL UNIT BELL 412 412 1182202SW TORQUE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 AIRCRAFT HAS 6 PERCENT TORQUE SPLIT AT HIGH POWER SETTINGS. IN SHOP REPAIR. 1G72 4U H4SW 20010806003342001080600334SW 2001 8 6 HEEA073664 120010619G771232447066 CONTROL UNIT BELL 412 412 1182202SW TORQUE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 10 PERCENT TORQUE SPLIT. IN SHOP REPAIR. 1G72 4U H4SW 20010806003362001080600336 2001 8 6 HEEA073665 420010619G34424000038 KNOB BELL 412 412 1182202SW CONTROL HEAD BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 BROKEN KNOB. IN SHOP REPAIR. 1G72 4U H4SW 20010806003382001080600338 2001 8 6 HEEA073666 420010619G34224020936903 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 SHOWS 30 DEGREE CLIMB WITH ACFT LEVEL. SENDING TO VENDOR FOR REPAIR. 1G72 4U H4SW 20010806003422001080600342 2001 8 6 HEEA073667 420010619G22104033089901 COMPUTER BELL 412 412 1182202SW COCKPIT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 CAUSES DECOUPLE LIGHT TO COME ON INTERMITTENTLY. SENDING TO VENDOR FOR REPAIR. 1G72 4U H4SW 20010806003442001080600344SW 2001 8 6 HEEA073668 120010619G6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K14262 36001 OUTBOARD ABRASION STRIP HAS SEVERAL HOLES FROM EROSION. SENDING TO VENDOR FOR REPAIR. 1G72 4U H4SW 20010806003452001080600345SW 2001 8 6 HEEA073669 120010619G6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 HAS SMALL SECTION OF SKIN MISSING NEAR OUTBOARD TAB. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003462001080600346SW 2001 8 6 HEEA073670 120010619G6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 SCARF JOINT SEPARATED AND LOOSE. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003482001080600348SW 2001 8 6 HEEA073671 120010619G6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893P 33012 CRACKED LEADING EDGE ABRASION STRIP. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003502001080600350SW 2001 8 6 HEEA073672 120010619G7712412075008111 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 COPILOT READS 3 PERCENT HIGHER THAN PILOTS AND ENG TORQUE SHOW 4 PERCENT SPLIT WHERE AS THE PILOTS SHOW ONLY A 1%. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003522001080600352SW 2001 8 6 HEEA073673 120010619G7714412075010109 INDICATOR BELL 412 412 1182202SW TRIPLE TACH READS LOW E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 NR 2 ENGINE AND N2 ROTOR NEEDLE READS 2 PERCENT LOW. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003562001080600356 2001 8 6 HEEA073674 420010619G34605205160006 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 NAV FLAG WILL NOT PULL. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003572001080600357 2001 8 6 HEEA073675 420010619G2340A3016W INTERPHONE BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 FM AUDIO BLEEDS OVER WHEN FM NR 1 SELECTOR SWITCH IS SET TO DOWN POSITION. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003592001080600359 2001 8 6 HEEA073676 420010619G2340A3016W INTERPHONE BELL 412 412 1182202SW COCKPIT WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 VERY WEAK ON RADIO CHANNELS. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003612001080600361 2001 8 6 HEEA073677 420010619G3443MI5851345 INDICATOR BELL 412 412 1182202SW RADAR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 RADAR WILL NOT INDICATE TARGETS, ALSO WILL NOT SHOW TEST BAND. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003632001080600363 2001 8 6 HEEA073678 420010619G3442MI5851345 DISPLAY BELL 412 412 1182202SW RADAR SYS INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 RADAR INOPERATIVE WITH BLANK SCREEN. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003662001080600366 2001 8 6 HEEA073679 420010619G3442MI5851352 RADAR BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 RADAR INOPERATIVE WITH BLANK SCREEN. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003672001080600367 2001 8 6 HEEA073680 420010619G3442MI585136 RADAR BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 RADAR INOPERATIVE WITH BLANK SCREEN. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003712001080600371 2001 8 6 HEEA073682 420010619G3442MI585200 RADAR BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW032261D 33076 RF BAND BROKEN AND TEST PATTERN BREAKS UP. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003732001080600373SW 2001 8 6 HEEA073683 120010619G6720PHI41294 BUSHING BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 WORN. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003752001080600375SW 2001 8 6 HEEA073684 120010619G6730212076005105 CYLINDER BELL 412 412 1182202SW ROTOR SERVO LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032261D 33076 LEAKING. IN SHOP FOR REPAIR. 1G72 4U H4SW 20010806003762001080600376 2001 8 6 HEEA073685 420010619G2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW VHF SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 DISPLAY NUMBERS DON'T COME ON. IN SHOP FOR REPAIR. 1G71 3U H2SW 20010806003772001080600377 2001 8 6 HEEA073686 420010619G2312069102435 RADIO BELL 206 206L3 1182108SW VHF SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 VHF RADIO WILL NOT POWER UP. IN SHOP FOR REPAIR. 1G71 3U H2SW 20010806003782001080600378SW 2001 8 6 HEEA073687 120010619G28211110900 FILTER BELL 206 206L1 1182107SW FUEL SYSTEM BYPASSING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035019F 45244 BUTTON POPS FOR NO REASON, INTERMITTENTLY. IN SHOP FOR REPAIR. 1G71 3U H2SW 20010806003792001080600379SW 2001 8 6 HEEA073688 120010619G2510206033105115 SEAT BELL 206 206L3 1182108SW COCKPIT MISMARKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033108E 51498 PANEL IS MISIDENTIFIED. IN SHOP FOR REPAIR. 1G71 3U H2SW 20010806003802001080600380SW 2001 8 6 HEEA073689 120010619G6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 WORN AND UNSTAKED BEARINGS. IN SHOP FOR REPAIR. 1G71 3U H2SW 20010806003812001080600381SW 2001 8 6 HEEA073690 120010619G6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 BOTH BEARINGS UNSTAKED. SENDING TO VENDOR FOR REPAIR. 1G71 3U H2SW 20010806003822001080600382SW 2001 8 6 HEEA073691 120010619G6330206033506101 RESTRAINT BELL 206 206L3 1182108SW TRANSMISSION DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 BEARINGS WORN. IN SHOP FOR REPAIR. 1G71 3U H2SW 20010806003832001080600383SW 2001 8 6 HEEA073692 120010619G6330206033506103 RESTRAINT BELL 206 206L4 1182110SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037074W 52033 BEARINGS WORN. IN SHOP FOR REPAIR. 1G71 3U NCH2SW 20010806003842001080600384SW 2001 8 6 HEEA073693 120010619G7933206375007103 INDICATOR BELL 206 206L3 1182108SW TOT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036160Z 51610 DURING START TOT INDICATOR DID NOT INDICATE TEMPERATURE. SENDING TO VENDOR FOR REPAIR. 1G71 3U H2SW 20010806003852001080600385SW 2001 8 6 HEEA073694 120010619G243523081018 STARTER GEN BELL 206 206L3 1182108SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 TROUBLESHOOTING GENERATOR PROBLEM. IN SHOP FOR REPAIR. 1G71 3U H2SW 20010806003862001080600386GL 2001 8 6 HEEA073695 220010619G7323252469211 GOVERNOR BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0330KH 51527 WILL NOT HOLD 100 PERCENT N2 SETTING. IN SHOP FOR REPAIR. 1G71 3U3 U H2SW E4CE 20010806003872001080600387GL 2001 8 6 HEEA073696 220010619G732125490925 FUEL CONTROL BELL 206 206L3 1182108SW ALLSN 250C 250C* GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331073 51519 ENGINE WOULD HIT 850 DEGREE ON START. ADJUSTING START/DERICH AND START/ACCELERATION TO MINIMUM WOULD NOT BRING THE ENGINE TO AN ACCEPTABLE START TEMPERATURE. IN SHOP FOR REPAIR. 1G71 3U3 U H2SW E4CE 20010806003882001080600388SW 2001 8 6 HEEA073697 120010619G28222C271 CARTRIDGE BELL 206 206L3 1182108SW BOOST PUMP FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 BOOST PUMP QUIT RUNNING IN FLIGHT. SENDING TO VENDOR FOR REPAIR. 1G71 3U H2SW 20010806003892001080600389 2001 8 6 HEEA073698 420010619G34215040017901 INDICATOR BELL 206 206L3 1182108SW ATTITUDE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 SLOW TO ERECT. IN SHOP FOR REPAIR. 1G71 3U H2SW 20010806003912001080600391 2001 8 6 HEEA073700 420010619G34578143802240D GPS BELL 206 206B3 1181506SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322743 3624 LOSES MEMORY. SENDING TO VENDOR FOR REPAIR. 1G71 3U H2SW 20010806003922001080600392 2001 8 6 HEEA073701 420010619G2350AA34200 RADIO BELL 206 206L4 1182110SW COCKPIT LOW E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW037077B 52037 VOLUME TOO LOW AND WOULD NOT ADJUST. SENDING TO VENDOR FOR REPAIR. 1G71 3U NCH2SW 20010806003932001080600393 2001 8 6 HEEA073703 420010619G2350PHI001200001201 MIXER BOX BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033116P 51530 WILL NOT RECEIVE ON PILOT'S SIDE. IN SHOP FOR REPAIR. 1G71 3U H2SW 20010806003942001080600394 2001 8 6 HEEA073704 420010619G2561 BOTTLE BELL 206 206L3 1182108SW LIFE VEST BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 "JERK TO INFLATE" TAG ON C02 BOTTLE ASSEMBLY BROKEN. SENDING TO VENDOR FOR REPAIR. 1G71 3U H2SW 20010806003952001080600395SW 2001 8 6 HEEA073705 120010619G6320206033518007 STOP BELL 206 206L3 1182108SW M/R GEARBOC DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0321497 51518 RUBBER DETERIORATED. SENDING TO VENDOR FOR REPAIR. 1G71 3U H2SW 20010806003962001080600396SW 2001 8 6 HEEA073706 120010619G2432RG214 BATTERY BELL 214 214ST 1182106SW BATTERY BAY DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T485 28101 BATTERY WEAK. WON'T HOLD A CHARGE. 2G72 4U H10SW 20010806003972001080600397SW 2001 8 6 HEEA073707 120010619G2432RG214 BATTERY BELL 214 214ST 1182106SW BATTERY BAY DISCHARGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T485 28101 BATTERY WEAK. WON'T HOLD A CHARGE. 2G72 4U H10SW 20010806003982001080600398 2001 8 6 HEEA073708 420010619G3452066106200 TRANSCEIVER BELL 407 407 SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 COULD NOT BE PICKED UP BY TOWER. SENDING TO VENDOR FOR REPAIR. 1G71 3U O H2SW 20010806003992001080600399SW 2001 8 6 HEEA073709 120010620G6210206015001115 BLADE BELL 206 206L3 1182108SW MAIN ROTOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03979BH903 51403 CORRODED AT BLADE TIP AND LATCH PLATE UNBONDED. 1G71 3U H2SW 20010806004002001080600400SW 2001 8 6 HEEA073710 120010620G6210206015001115 BLADE BELL 206 206L3 1182108SW MAIN ROTOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03979BH903 51403 CORRODED AT BLADE TIP. 1G71 3U H2SW 20010806004012001080600401SW 2001 8 6 HEEA073712 120010620G5302 STRUCTURE BELL 407 407 SW VERTICAL FIN CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH BP1875 53207 VERTICAL FIN CORRODED. 1G71 3U O H2SW 20010806004022001080600402SW 2001 8 6 HEEA073713 120010620G3212206050247131 COVER BELL 407 407 SW MLG WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH 53396 AFT END CAP IS WORN AND TORN. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010806004032001080600403SW 2001 8 6 HEEA073714 120010620G3212206050247138 COVER BELL 407 407 SW FLOAT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03719PH 53266 COVER WORN AND END CAP LOOSE. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000052001080700005SW 2001 8 7 HEEA073715 120010620G6510206061432118 INLET BELL 407 407 SW T/R OIL COOLER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03719PH 53266 OIL COOLER INLET COVER CRACKED. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000062001080700006SW 2001 8 7 HEEA073716 120010620G6510206061432121 HOUSING BELL 407 407 SW T/R BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 BLOWER HOUSING HAS CRACKS. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000072001080700007SW 2001 8 7 HEEA073717 120010620G6510206061432121 HOUSING BELL 407 407 SW T/R BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03719PH 53266 BLOWER HOUSING HAS CRACKS. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000082001080700008SW 2001 8 7 HEEA073718 120010620G2435206062200113 STARTER GEN BELL 407 407 SW ENGINE ARCED E HEEAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW03741PH357 53457 ARCING 1G71 3U O H2SW 20010807000092001080700009SW 2001 8 7 HEEA073719 120010620G2435206062200113 STARTER GEN BELL 407 407 SW ENGINE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03447PH1558 53114 STARTER GENERATOR BRUSHES WORN BEYOND LIMITS. 1G71 3U O H2SW 20010807000102001080700010SW 2001 8 7 HEEA073721 120010620G2435 SHAFT BELL 407 407 SW STARTER GEN BENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW03417PH1190 99405 53038 SHAFT BENT. 1G71 3U O H2SW 20010807000112001080700011SW 2001 8 7 HEEA073722 120010620G2435 BRUSHES BELL 407 407 SW STARTER GEN WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03740PH3794 1828 53435 BRUSHES WORN BEYOND LIMITS. REPAIRED BY PHI. (BELL WILL BE INVOICED) 1G71 3U O H2SW 20010807000122001080700012SW 2001 8 7 HEEA073723 120010620G6321 PAD BELL 407 407 SW ROTOR BRAKE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03417PH 337 53038 WORN PAD. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000132001080700013SW 2001 8 7 HEEA073724 120010620G3212206373901103 SOLENOID VALVE BELL 407 407 SW FLOAT BOTTLE LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03722PH 53288 AFTER FLOAT BOTTLE CHANGE VALVE ASSY LEAKED NITROGEN FROM SOLENOID OPENING ADJUSTMENT CAP. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000142001080700014SW 2001 8 7 HEEA073725 120010620G7931222375077113 TRANSMITTER BELL 407 407 SW OIL PRESSURE READS LOW E HEEAK NONE O OTHER ININSP/MAINT 1 SW03719PH 53266 ENGINE OIL PRESSURE READING LOW. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000152001080700015SW 2001 8 7 HEEA073726 120010620G7931222375077113 TRANSMITTER BELL 407 407 SW OIL PRESSURE READS LOW E HEEAK NONE O OTHER ININSP/MAINT 1 SW03742PH 53461 ENGINE OIL PRESSURE INDICATING 30 PSI LOW IN CRUISE FLIGHT. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000182001080700018GL 2001 8 7 HEEA073727 220010620G741223064130 IGNITER BOX BELL 407 407 SW ALLSN 250C 250C47B GL ENGINE INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW034999 53323 WORKS INTERMITTENTLY. AIRCRAFT WOULD NOT LIGHT OFF. TO BE RETURNED TO VENDOR. 1G71 3U3 UO H2SW E1GL 20010807000192001080700019SW 2001 8 7 HEEA073728 120010620G6520406040453101 SEAL BELL 407 407 SW T/R GEARBOX LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH228 53199 SEAL LEAKING OIL. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000232001080700023SW 2001 8 7 HEEA073729 120010620G6310406040500123B FREEWHEEL UNIT BELL 407 407 SW MAIN ROTOR LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH2236 53207 FRONT SEAL LEAKING. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000252001080700025SW 2001 8 7 HEEA073730 120010620G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW M/R PITCH CHANGEWORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 BLUE MAIN ROTOR PITCH CHANGE BEARING WORN. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000262001080700026SW 2001 8 7 HEEA073731 120010620G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW M/R PITCH CHANGEWORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 BEARING WORN. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000282001080700028SW 2001 8 7 HEEA073732 120010620G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW M/R PITCH CHANGEWORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH1201 53386 BEARING WORN. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000292001080700029SW 2001 8 7 HEEA073733 120010620G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW M/R PITCH CHANGEWORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH 53277 BEARING WORN. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000302001080700030SW 2001 8 7 HEEA073734 120010620G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW M/R PITCH CHANGEWORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03447PH 53114 BEARING WORN. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000312001080700031SW 2001 8 7 HEEA073735 120010620G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW M/R PITCH CHANGEWORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW034999 436 53323 BEARING WORN. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000322001080700032SW 2001 8 7 HEEA073736 120010620G6300407010206103 BEARING BELL 407 407 SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 BEARING WORN. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000352001080700035SW 2001 8 7 HEEA073737 120010620G6420406312100101 BEARING 407012101111BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03510PH 53311 53209 WORN. TO BE RETURNED TO VENDOR. (J0169320) 1G71 3U O H2SW 20010807000362001080700036SW 2001 8 7 HEEA073738 120010620G6420406312100101 BEARING 407012101111BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH 53393 53400 WORN. TO BE RETURNED TO VENDOR. (J0159304) 1G71 3U O H2SW 20010807000372001080700037SW 2001 8 7 HEEA073739 120010620G6420406312100101 BEARING 407012101111BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH 53397 53397 WORN. TO BE RETURNED TO VENDOR. (J0154475) 1G71 3U O H2SW 20010807000382001080700038SW 2001 8 7 HEEA073740 120010620G3210407030112103 STRAP BELL 407 407 SW MLG DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 SURFACE DAMAGE. SCRAPPED LOCALLY. 1G71 3U O H2SW 20010807000392001080700039SW 2001 8 7 HEEA073741 120010620G5210407070620138 PANEL BELL 407 407 SW PAX DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 CRACKED AND WORN. SCRAPPED LOCALLY. 1G71 3U O H2SW 20010807000402001080700040SW 2001 8 7 HEEA073742 120010620G5210407070620157 PANEL BELL 407 407 SW PAX/CREW DOOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03404PH 53188 DOOR PANEL DAMAGED. SCRAPPED LOCALLY. 1G71 3U O H2SW 20010807000412001080700041SW 2001 8 7 HEEA073743 120010620G5210407070620157 PANEL BELL 407 407 SW PAX/CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH 53059 CRACKED AND BROKEN. SCRAPPED LOCALLY. 1G71 3U O H2SW 20010807000422001080700042SW 2001 8 7 HEEA073744 120010620G5210407070620158 PANEL BELL 407 407 SW PAX/CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH 53059 CRACKED AND BROKEN. SCRAPPED LOCALLY. 1G71 3U O H2SW 20010807000432001080700043SW 2001 8 7 HEEA073745 120010620G5210407070620158 PANEL BELL 407 407 SW PAX/CREW DOOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03404PH 53188 DAMAGED. SCRAPPED LOCALLY. 1G71 3U O H2SW 20010807000442001080700044SW 2001 8 7 HEEA073746 120010620G5210407070620218 PANEL BELL 407 407 SW PAX/CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 CRACKED AND STAINED. SCRAPPED LOCALLY. 1G71 3U O H2SW 20010807000462001080700046SW 2001 8 7 HEEA073747 120010620G5260407301109 STEP BELL 407 407 SW FUSELAGE CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 HEAVY CORROSION AROUND MOUNTING HOLES. SCRAPPED LOCALLY. 1G71 3U O H2SW 20010807000492001080700049 2001 8 7 HEEA073748 420010620G2350PA1120NVPHI HEADSET BELL 407 407 SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407XM 53464 WILL NOT TRANSMIT. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20010807000522001080700052SW 2001 8 7 HEEA073749 120010620G6520PHI407111 HOUSING BELL 407 407 SW INPUT SEAL LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 LEAKING. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20010807000532001080700053 2001 8 7 HEEA073750 420010620G3400CI196 ANTENNA BELL 407 407 SW NAVIGATION CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH 53147 CORROSION AT BASE. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20010807000542001080700054GL 2001 8 7 HEEA073751 220010620G7421CH34187A IGNITER BELL 407 407 SW ALLSN 250C 250C47B GL ENGINE ERODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 ELECTRODE ERODED CAUSING DELAYED LIGHT OFF. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20010807000562001080700056SW 2001 8 7 HEEA073752 120010620G3110407375038101 PANEL BELL 407 407 SW COCKPIT BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 SWITCH GUARD BROKEN. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20010807000572001080700057GL 2001 8 7 HEEA073753 220010620G73136899001 NOZZLE BELL 407 407 SW ALLSN 250C 250C47B GL FUEL SYSTEM CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03740PH291 53435 CAE847473 THREADS RUSTED AND DAMAGED. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20010807000582001080700058SW 2001 8 7 HEEA073754 120010620G7921407062021101 DUCT BELL 407 407 SW OIL COOLER CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 OIL COOLER TRANSITION DUCT IS CRACKED. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000592001080700059SW 2001 8 7 HEEA073755 120010620G6330407310203101 MOUNT BELL 407 407 SW TRANSMISSION DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 RUBBER IN MOUNT BAD. SERIAL NUMBERS REMOVED ARE LP1891 AND LP1902. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000602001080700060SW 2001 8 7 HEEA073756 120010620G6510407340340101 DISC PACK BELL 407 407 SW T/R DRIVE BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 BROKEN. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000612001080700061SW 2001 8 7 HEEA073757 120010620G2840407362005103 SWITCH BELL 407 407 SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 FALSE INDICATION, LIGHT ON WITH 400 LBS OF FUEL. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000622001080700062SW 2001 8 7 HEEA073758 120010620G2840407362005103 SWITCH BELL 407 407 SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH 53147 LOW LEVEL LIGHT COMES ON INTERMITTENTLY. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000632001080700063SW 2001 8 7 HEEA073759 120010620G2822407362013101 PRESSURE SWITCH BELL 407 407 SW ENGINE MALFUNCTIONED E O OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 RT PUMP LIGHT DOES NOT ILLUMINATE WITH A/C POWER ON AND PUMP OFF. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000642001080700064SW 2001 8 7 HEEA073760 120010620G2822407362013101 PRESSURE SWITCH BELL 407 407 SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 LT TRANSFER PUMP LIGHT DOES NOT ILLUMINATE WITH A/C POWER ON AND PUMP OFF. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000662001080700066SW 2001 8 7 HEEA073761 120010620G2822407362013101 PRESSURE SWITCH BELL 407 407 SW ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 RT BOOST PUMP LIGHT DOES NOT ILLUMINATE WITH CIRCUIT BREAKER PULLED. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000672001080700067SW 2001 8 7 HEEA073762 120010620G7930407375004101 INDICATOR BELL 407 407 SW ENGINE OIL INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 ENGINE OIL PRESSURE READS 70 PSI WITH NO ENGINE POWER. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000682001080700068SW 2001 8 7 HEEA073763 120010620G291070061V000V444A TUBE BELL 407 407 SW HYD SYSTEM CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 CHAFED. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000722001080700072SW 2001 8 7 HEEA073764 120010620G8000SM20ACD300A21 RELAY BELL 407 407 SW STARTER STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407XM 53464 STARTER RELAY STUCK IN CLOSED POSITION ON ENGINE WASH. TO BE RETURNED TO VENDOR. 1G71 3U O H2SW 20010807000732001080700073SW 2001 8 7 HEEA073765 120010620G284170077P140B370 HOSE BELL 412 412 1182202SW FUEL SYSTEM DAMAGED E HEEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW03108X 33115 SHORTLY AFTER TAKEOFF, BOTH FUEL TRANSFER CAUTION LIGHTS ILLUMINATED. THE FUEL QUANTITY INDICATOR SHOWED BOTH FORWARD FUEL CELLS EMPTY AND MID TANKS SHOWING 50 LBS. WITH 1500 LBS ON BOARD. REPLACED 3 EACH HOSES. (P/N 70-077P140B370, P/N 70-077P288W294, P/N 412-061-610-103) 1G72 4U H4SW 20010807000742001080700074SW 2001 8 7 HEEA073766 120010620G2931222375019105 TRANSMITTER BELL 214 214ST 1182106SW HYD SYSTEM MALFUNCTIONED E HEEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0359806 28140 SHORTLY AFTER TAKEOFF, THE NR 1 HYDRAULIC PRESSURE GAUGE PEGGED OUT. REPLACED PRESSURE TRANSMITTER. 2G72 4U H10SW 20010807000752001080700075SW 2001 8 7 HEEA073767 120010620G6420407312100101 BEARING 407012101111BELL 407 407 SW TAIL ROTOR DEBONDED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03141MA 53038 53016 ELASTOMERIC BEARING DEBONDED. TO BE RETURNED TO VENDOR. (J0165342-WA) 1G71 3U O H2SW 20010807000762001080700076SW 2001 8 7 HEEA073768 120010620G6510406040339105 BEARING 407040302101BELL 407 407 SW TAIL ROTOR VIBRATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH A164 53142 ROUGH VIBRATION ON TAILBOOM. TO BE RETURNED TO VENDOR. (J0162310-WA) 1G71 3U O H2SW 20010807000772001080700077SW 2001 8 7 HEEA073769 120010620G6510407340339103 BEARING 407040302101BELL 407 407 SW TAIL ROTOR OVERHEATED E HEEAO OTHER M OVER TEMP ININSP/MAINT 1 SW03467PH A15 53142 OVERHEATED. TO BE RETURNED TO VENDOR. (J0164213-WA) 1G71 3U O H2SW 20010807002352001080700235SW 2001 8 7 HEEA073770 120010620G6510407340339103 BEARING 407040302107BELL 407 407 SW TAIL ROTOR MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH A1964 53400 METAL. TO BE RETURNED TO VENDOR. (J0167780-WA) 1G71 3U O H2SW 20010807002362001080700236SW 2001 8 7 HEEA073771 120010620G6510407340339103 BEARING 407040302107BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03719PH A1949 53266 WORN. TO BE RETURNED TO VENDOR. (J0168105-WA) 1G71 3U O H2SW 20010807002372001080700237SW 2001 8 7 HEEA073772 120010620G6420406312100101 BEARING 407012101111BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53277 53327 WORN. TO BE RETURNED TO VENDOR. (J0166791-WA) 1G71 3U O H2SW 20010807002382001080700238SW 2001 8 7 HEEA073773 120010620G6310406340102101 CARBON SEAL 406040500123BELL 407 407 SW FREEWHEEL UNIT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH A4361 53059 WORN. TO BE RETURNED TO VENDOR. (J0165492-WA) 1G71 3U O H2SW 20010807002392001080700239SW 2001 8 7 HEEA073774 120010620G6420406312100101 BEARING 407012101111BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH 53396 53159 WORN. TO BE RETURNED TO VENDOR. (J0165250-WA) 1G71 3U O H2SW 20010807002402001080700240SW 2001 8 7 HEEA073775 120010620G6310406340102101 CARBON SEAL PHI407109 BELL 407 407 SW FREEWHEEL UNIT LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03490PH 53378 FREEWHEELING UNIT FORWARD SEAL LEAKING OIL. TO BE RETURNED TO VENDOR. (J0160511-WA) 1G71 3U O H2SW 20010807002412001080700241SW 2001 8 7 HEEA073776 120010620G6300406040320101 SHAFT PHIPBH40701 BELL 407 407 SW COOLER BLOWER WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH PHI0015 53378 WORN SPLINES. TO BE RETURNED TO VENDOR. (J0167662-WA) 1G71 3U O H2SW 20010807002422001080700242SW 2001 8 7 HEEA073777 120010620G6300407340339103 BEARING PHIPBH40701 BELL 407 407 SW COOLER BLOWER ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH PHI0015 53378 ROUGH. SERIAL NUMBERS REMOVED ARE B00-2007 AND B00-2035. TO BE RETURNED TO VENDOR. (J0167662-WA) 1G71 3U O H2SW 20010807002432001080700243SW 2001 8 7 HEEA073779 120010620G6300406040320101 SHAFT PHIPBH40701 BELL 407 407 SW COOLER BLOWER WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH PHI0004 53400 WORN SPLINES. TO BE RETURNED TO VENDOR (J0166773-WA) 1G71 3U O H2SW 20010807002442001080700244SW 2001 8 7 HEEA073780 120010620G6300407340339103 BEARING PHIPBH40701 BELL 407 407 SW COOLER BLOWER WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH PHI0004 53400 WORN. SERIAL NUMBERS REMOVED ARE F99-2018 AND F99-1690. TO BE RETURNED TO VENDOR (J0166773-WA) 1G71 3U O H2SW 20010807002452001080700245SW 2001 8 7 HEEA073781 120010620G6420407312100101 BEARING 407012101111BELL 407 407 SW TAIL ROTOR CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03141MA1733 53393 53016 ELASTOMER SHEETING AND CHAFING. TO BE RETURNED TO VENDOR (J0169927-WA) 1G71 3U O H2SW 20010807002462001080700246SW 2001 8 7 HEEA073782 120010620G6420406312100101 BEARING 407012101111BELL 407 407 SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03141MA613 53393 53016 WORN. TO BE RETURNED TO VENDOR (J0169927-WA) 1G71 3U O H2SW 20010807002822001080700282EU 2001 8 7 HEEA073783 120010619G621010515141 BLADE BOLKMS105 BO105S 5626006EU MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03819826167 S818 THE OUTBOARD LEADING EDGE STRIP SEPARATED ON THE OUTBOARD TIP. SENDING TO VENDOR FOR REPAIR. 1G72 3U H3EU 20010807002832001080700283EU 2001 8 7 HEEA073784 120010619G621010515150 BLADE BOLKMS105 BO105S 5626006EU MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03819825832 S818 THE OUTBOARD LEADING EDGE STRIP SEPARATED IN SEVERAL AREAS. SENDING TO VENDOR FOR REPAIR. 1G72 3U H3EU 20010807002852001080700285EU 2001 8 7 HEEA073785 120010619G5320350A21010108 DRAIN LINE SNIAS 350 AS350B2 8680813EU FUSELAGE LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0340466 3004 PIPE LEAKS AT CONNECTION. REPLACED WITH SERVICEABLE PIPE. 1G71 3U H9EU 20010807002872001080700287EU 2001 8 7 HEEA073786 120010619G79211184961 OIL COOLER SNIAS 350 AS350B2 8680813EU ENGINE OIL CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0340466 3004 OIL COOLER CORRODED. REPLACED WITH SERVICEABLE ENG OIL COOLER. 1G71 3U H9EU 20010807002882001080700288EU 2001 8 7 HEEA073787 120010619G63221184964 OIL COOLER SNIAS 350 AS350B2 8680813EU TRANSMISSION CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0340466 3004 OIL COOLER CORRODED. REPLACED WITH SERVICEABLE TRANS OIL COOLER. 1G71 3U H9EU 20010807003252001080700325EU 2001 8 7 HEEA073788 120010619G6520 BEARING SNIAS 350 AS350B 8680801EU PITCH LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03856PH 3352 INBOARD BEARING WORN. REPLACED WITH SERVICEABLE T/R PITCH LINK. 1G71 3U H9EU 20010807003272001080700327EU 2001 8 7 HEEA073789 120010619G6300350A57117720 STOP SNIAS 350 AS350B2 8680813EU MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0340466 3004 WORN AT STOP. REPLACED WITH SERVICEABLE STOP PLATE. 1G71 3U H9EU 20010807003312001080700331EU 2001 8 7 HEEA073791 120010619G3040350A89103701 ARM SNIAS 350 AS350B2 8680813EU WINDSHIELD WIPERCRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0340466 3004 CRACKED AT MOUNT. REPLACED WITH SERVICEABLE WIPER ARM. 1G71 3U H9EU 20010807003322001080700332EU 2001 8 7 HEEA073792 120010619G2560504305401 INERTIA REEL SNIAS 350 AS350B2 8680813EU SEAT BELT BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034000L 2873 RECEIVED NEW INERTIAL REEL AND FOUND RELEASE CABLE AT ATTACHMENT BROKEN AT REEL. SENDING TO VENDOR FOR REPAIR. 1G71 3U H9EU 20010807003332001080700333EU 2001 8 7 HEEA073793 120010619G6220704A33633116 BEARING SNIAS 350 AS350B2 8680813EU MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0340466 3004 ELASTOMERIC RUBBER SEPARATED BEYOND LIMITS. SENDING TO VENDOR FOR REPAIR. 1G71 3U H9EU 20010807003362001080700336EU 2001 8 7 HEEA073794 120010619G2931MA12401 PRESSURE SWITCH SNIAS 350 AS350B 8680801EU HYD SYSTEM DEFECTIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03856PH 3352 HYD. CAUTION LIGHT ILLUMINATED INTERMITTENTLY. SENDING TO VENDOR FOR REPAIR. 1G71 3U H9EU 20010807003372001080700337 2001 8 7 HEEA073795 420010619G3452066106200 TRANSCEIVER BOLKMS117 BK117A1 5626010EU COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911LK 7068 ATC REPORTED NOT GETTING THE RIGHT NUMBER. PERFORMED PRELIMINARY INSPECTION AND FOUND INTERMITTENT DIAL, ALSO MTL OUT OF SPECIFICATIONS, SIGNAL CUTS OUT AT -64DB WHEN DYNAMIC RANGE IS SET TO -9DB, ADJUSTED IF SECTION AND PRESELECTOR, NO HELP. PROBLEM ON MAIN BOARD. SENDING TO VENDOR FOR REPAIR. 1G72 3U H13EU 20010911000122001091100012GL 2001 9 11 HEEA075478 220010821G725023033861 COVER 6898735 BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL SUMP CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035031U CAT34156F S678 TURBINE REMOVED DUE TO NR 1 & 2 WHEEL CYCLES. UPON INSPECTION OF TURBINE NOTED NR 8 SUMP NUT BRAZEMENT ERODED AND CRACKED. SCRAPPED COVER AND REPLACED WITH SERVICEABLE PART. 1G72 3U3 U H3EU E4CE 20010911000132001091100013GL 2001 9 11 HEEA075479 220010821G725023053299 TURBINE WHEEL BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036251X1904 51552 CAE895491 ENGINE REMOVED DUE TO 2000 HOUR INSPECTION. UPON INSPECTION OF TURIBNE PARTS NOTED SULFIDATION ON LEADING EDGE OF NR 1 WHEEL BLADES. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E1GL 20010911000142001091100014GL 2001 9 11 HEEA075480 220010821G723023066675 LINER BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL COMPRESSOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 TORQUE OSCILLATIONS ABOVE 80%. 1G71 3U3 U H2SW E1GL 20010911000152001091100015SW 2001 9 11 HEEA075481 120010821G712023069751 MOUNT BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0330KH 51527 BEARING UNSTAKED. REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E1GL 20010911000162001091100016 2001 9 11 HEEA075482 420010827G3434066301201 SENSOR SKRSKYS76 S76A 8143006NE MARKER BEACON BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW031546G 760076 LIGHT SENSOR BROKEN. PERFORMED PRELIMINARY INSPECTION. FOUND V101 PHOTOCELL BROKEN OFF. REPLACED. REPAIRED. ALSO INSTALLED 3 LIGHT HOODS. BENCH CHECK GOOD. 1G72 3U H1NE 20010911000172001091100017 2001 9 11 HEEA075483 420010828G2350100005430 HEADSET SKRSKYS76 S76A 8143006NE RADIO BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03760PH 760078 BROKEN WIRES. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20010911000182001091100018GL 2001 9 11 HEEA075484 220010828G7412106149501 IGNITER BOX SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW034253S 760035 IGNITER BOX INOPERATIVE. 1G72 3U3 U H1NE E1GL 20010912000012001091200001 2001 9 12 HEEA075485 420010828G34251113025 INDICATOR SKRSKYS76 S76A 8143006NE HSI DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G 760076 HSI COURSE KNOB COMES OFF. 1G72 3U H1NE 20010912000022001091200002SW 2001 9 12 HEEA075486 120010821G6320204040379003 QUILL BELL 412 412 1182202SW LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW032149S 36002 QUILL ASSY SEEPING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010912000032001091200003SW 2001 9 12 HEEA075487 120010821G3246205050400101 SADDLE 412050015110BELL 412 412 1182202SW SKID TUBE MISDRILLED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R DRK100692 36007 MISDRILLED HOLES. THE HOLES FOR THE BOLTS (99-13-1), THAT ATTACHES THE FWD. CROSSTUBE TO THE SKID TUBE SADDLE ARE DRILLED FOR AN4 BOLTS. 1G72 4U H4SW 20010912000042001091200004SW 2001 9 12 HEEA075488 120010821G2822205060606003 PUMP BELL 412 412 1182202SW FUEL BOOST MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 PUMP PRODUCES NO PRESSURE. 1G72 4U H4SW 20010912000182001091200018SW 2001 9 12 HEEA075489 120010821G6320205076034007 FILTER ELEMENT BELL 412 412 1182202SW M/R GEARBOX FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 FILTER BYPASS EXTENDED. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010912000192001091200019SW 2001 9 12 HEEA075490 120010821G6420206001725001 PAD BELL 206 206L3 1182108SW TAIL ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036748D 51106 GREASE SEALS MISSING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912000202001091200020SW 2001 9 12 HEEA075491 120010821G6720206001763001 BELLCRANK BELL 206 206L3 1182108SW TAIL ROTOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036748D 51106 TAIL ROTOR BELLCRANK ASSY HAS CORROSION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912000212001091200021SW 2001 9 12 HEEA075492 120010821G6210206010200133 BLADE BELL 206 206B3 1181506SW MAIN ROTOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032277A2336 3630 EXTREME TRAILING EDGE SPAR CORRODED AT THE TIP OF THE BLADE. 1G71 3U H2SW 20010912000222001091200022SW 2001 9 12 HEEA075493 120010821G6230206010360005 LINK BELL 206 206L3 1182108SW MAIN ROTOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381671 51301 MAIN ROTOR HEAD LINK ASSY IS CORRODED. SCRAPPED. 1G71 3U H2SW 20010912000232001091200023SW 2001 9 12 HEEA075494 120010821G6220206011117003 RESTRAINT BELL 206 206L3 1182108SW MAIN ROTOR STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW0330KH 51527 STICKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912000242001091200024SW 2001 9 12 HEEA075495 120010821G6220206011117003 RESTRAINT BELL 206 206L3 1182108SW MAIN ROTOR STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW036160Z 51610 STICKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912000252001091200025SW 2001 9 12 HEEA075496 120010821G6420206011725001 ROD BELL 206 206L3 1182108SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 ROD BEARING WORN. SCRAPPED. 1G71 3U H2SW 20010912000262001091200026SW 2001 9 12 HEEA075497 120010821G6300206033553001 STOP BELL 206 206L3 1182108SW MAIN ROTOR DEBONDED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038591X 51495 RUBBER DEBONDED. SCRAPPED. 1G71 3U H2SW 20010912000272001091200027SW 2001 9 12 HEEA075498 120010821G6300206033554101 LINK BELL 206 206L3 1182108SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 BEARING BAD. 1G71 3U H2SW 20010912000282001091200028SW 2001 9 12 HEEA075499 120010821G6310206040015015 DISK BELL 206 206L3 1182108SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03214978748 51518 DISC WORN CAUSING NOISE WHEN ROTOR BRAKES APPLIED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912000292001091200029SW 2001 9 12 HEEA075500 120010821G6310206040270101 SUPPORT BELL 206 206L3 1182108SW MAIN ROTOR LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 LEAKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912000302001091200030SW 2001 9 12 HEEA075501 120010821G6310206040270101 SUPPORT BELL 206 206B3 1181506SW MAIN ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW0322751 3627 LEAKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912000312001091200031SW 2001 9 12 HEEA075502 120010821G6520206040402105 GEARBOX BELL 206 206L3 1182108SW TAIL ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03214978684 51518 PLAY IN OUTPUT SHAFT, UNABLE TO BALANCE TAIL ROTOR. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912000322001091200032SW 2001 9 12 HEEA075503 120010821G6520206040402105 GEARBOX BELL 206 206L3 1182108SW TAIL ROTOR MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 MAKING METAL. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912000332001091200033SW 2001 9 12 HEEA075504 120010821G3246206050128001 SHOE BELL 206 206L3 1182108SW MLG SKID WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW0342EA 51542 SKID SHOE WORN. SCRAPPED. 1G71 3U H2SW 20010912000342001091200034SW 2001 9 12 HEEA075505 120010821G3246206050129001 SHOE BELL 206 206L3 1182108SW MLG SKID WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW0342EA 51542 SKID SHOE WORN. SCRAPPED. 1G71 3U H2SW 20010912000352001091200035SW 2001 9 12 HEEA075506 120010821G3213206053109007 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03979BH 51403 CORRODED BEYOND LIMITS. SCRAPPED. 1G71 3U H2SW 20010912000362001091200036SW 2001 9 12 HEEA075507 120010821G3213206053109008 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03979BH 51403 CROSSTUBE CORRODED BEYOND LIMITS. SCRAPPED. 1G71 3U H2SW 20010912000372001091200037SW 2001 9 12 HEEA075508 120010821G3213206053203101 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03108PH 51334 CROSSTUBE CORRODED BEYOND LIMITS. SCRAPPED. 1G71 3U H2SW 20010912000382001091200038SW 2001 9 12 HEEA075509 120010821G2820206061613003 FITTING BELL 206 206L3 1182108SW FUEL SUMP CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033108E 51498 FWD. FUEL SUMP FITTINGS CORRODED. REPLACED WITH SERVICEABLE FITTINGS. 1G71 3U H2SW 20010912000392001091200039SW 2001 9 12 HEEA075510 120010821G2820206061634003 VALVE BELL 206 206L3 1182108SW FUEL SYSTEM LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW0342EA 51542 LEAKING FROM FUEL COCK. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912000422001091200042SW 2001 9 12 HEEA075511 120010821G6710206062721109 ACTUATOR BELL 206 206L1 1182107SW ENGINE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW035019F 45244 ACTUATOR INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912000442001091200044SW 2001 9 12 HEEA075512 120010821G6710206062721109 ACTUATOR BELL 206 206L3 1182108SW ENGINE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 ACTUATOR WILL NOT EXTEND OR RETRACT. 1G71 3U H2SW 20010912000452001091200045SW 2001 9 12 HEEA075513 120010821G6710206062721109 ACTUATOR BELL 206 206L3 1182108SW ENGINE INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381SP 51029 WOULD NOT BEEP. BEEP WAS INTERMITTENT THROUGHOUT ADJUSTMENT ATTEMPTS. 1G71 3U H2SW 20010912000472001091200047SW 2001 9 12 HEEA075514 120010821G6710206062721109 ACTUATOR BELL 206 206L3 1182108SW ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0330KH 51527 N2 CHANGES IN FLIGHT. 1G71 3U H2SW 20010912000482001091200048SW 2001 9 12 HEEA075515 120010821G6710206062721109 ACTUATOR BELL 206 206L3 1182108SW ENGINE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 ACTUATOR INOPERATIVE. 1G71 3U H2SW 20010912000492001091200049SW 2001 9 12 HEEA075516 120010821G6710206062721109 ACTUATOR BELL 206 206L4 1182110SW ENGINE INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW037074W 52033 ACTUATOR INTERMITTENT OPERATION. 1G71 3U NCH2SW 20010912000622001091200062SW 2001 9 12 HEEA075517 120010821G6710206062721109 ACTUATOR BELL 206 206L3 1182108SW ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0341791 51465 ACTUATOR MOTOR WORKED SEVERAL TIMES ON AIRCRAFT AND QUIT. BENCH TEST WAS ABLE TO RETRACT BUT NOT EXTEND. 1G71 3U H2SW 20010912000642001091200064SW 2001 9 12 HEEA075518 120010821G6710206062721113 ACTUATOR BELL 206 206L3 1182108SW DROOP COMP FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 ACTUATOR WILL NOT RETRACT. 1G71 3U H2SW 20010912000662001091200066SW 2001 9 12 HEEA075519 120010821G2841206063633103 INDICATOR BELL 206 206L3 1182108SW FUEL QTY FLUCTUATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW038592X 51508 FLUCTUATING; OCCASIONALLY PEGGING OUT ON THE HIGH SIDE. 1G71 3U H2SW 20010912000882001091200088SW 2001 9 12 HEEA075520 120010821G7120206064105101 LEG ASSY BELL 206 206L4 1182110SW ENGINE MOUNT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0362127 52023 CORROSION ON INSIDE OF TUBE. REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20010912000932001091200093SW 2001 9 12 HEEA075521 120010821G7120206064105101 LEG ASSY BELL 206 206L3 1182108SW ENGINE MOUNT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381671 51301 PITTING ON INSIDE OF TUBE. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912000942001091200094SW 2001 9 12 HEEA075522 120010821G7120206064105102 LEG ASSY BELL 206 206L4 1182110SW ENGINE MOUNT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0362127 52023 ELONGATED HI-LOC HOLES. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20010912000962001091200096SW 2001 9 12 HEEA075523 120010821G7120206064106101 LEG ASSY BELL 206 206L4 1182110SW ENGINE MOUNT CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0362127 52023 CORROSION ON INSIDE OF TUBE. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20010912000992001091200099SW 2001 9 12 HEEA075524 120010821G6220206011100159 HUB BELL 206 206L3 1182108SW MAIN ROTOR LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 YELLOW GRIP SLINGING GREASE. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010912001002001091200100SW 2001 9 12 HEEA075525 120010821G6320206040004107 TRANSMISSION BELL 206 206L3 1182108SW MAIN ROTOR MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331077 51520 MAKING METAL. REPLACED WITH SERVICEABLE ASSY. 1G71 3U H2SW 20010912001012001091200101SW 2001 9 12 HEEA075526 120010821G7120206064106101 LEG ASSY BELL 206 206L4 1182110SW ENGINE MOUNT CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0362127 52023 CHAFED BEYOND LIMITS. SCAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20010912001022001091200102SW 2001 9 12 HEEA075527 120010821G7120206064106101 LEG ASSY BELL 206 206L3 1182108SW ENGINE MOUNT CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381671 51301 CHAFED BEYOND LIMITS. SCAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001032001091200103SW 2001 9 12 HEEA075528 120010821G7120206064106101 LEG ASSY BELL 206 206L3 1182108SW ENGINE MOUNT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03979BH 51403 END FITTING RIVET HOLES ARE ELONGATED AND WORN BEYOND LIMITS. SCAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001472001091200147SW 2001 9 12 HEEA075529 120010821G7120206064107101 LEG ASSY BELL 206 206L3 1182108SW ENGINE MOUNT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381671 51301 RIVET HOLES ARE ELONGATED. SCAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001482001091200148SW 2001 9 12 HEEA075530 120010821G7120206064107109 LEG ASSY BELL 206 206L4 1182110SW ENGINE MOUNT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0362127 52023 ELONGATED HI-LOC HOLES. SCAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20010912001492001091200149SW 2001 9 12 HEEA075531 120010821G7120206064107111 LEG ASSY BELL 206 206L4 1182110SW ENGINE MOUNT CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0362127 52023 CHAFED BEYOND LIMITS. SCAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20010912001502001091200150SW 2001 9 12 HEEA075532 120010821G6730206076062003 CYLINDER BELL 206 206L3 1182108SW SERVO SYSTEM LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW038594X 51531 LEAKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001512001091200151SW 2001 9 12 HEEA075533 120010821G6730206076062003 CYLINDER BELL 206 206L3 1182108SW SERVO SYSTEM LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW038591X 51495 LEAKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001522001091200152SW 2001 9 12 HEEA075534 120010821G3246206323002M CROSSTUBE BELL 206 206L3 1182108SW MLG SKID CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03108PH 51334 CORRODED BEYOND LIMITS IN SADDLE AREA. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001532001091200153SW 2001 9 12 HEEA075535 120010821G3246206323017 CROSSTUBE BELL 206 206L1 1182107SW MLG SKID CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035007Q 45187 CORROSION PITS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001542001091200154SW 2001 9 12 HEEA075536 120010821G3246206323017 CROSSTUBE BELL 206 206L3 1182108SW MLG SKID CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038592X 51508 CORRODED BEYOND LIMITS IN AREA AROUND SADDLES. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001562001091200156SW 2001 9 12 HEEA075537 120010821G3246206323017 CROSSTUBE BELL 206 206L3 1182108SW MLG SKID CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036748D 51106 CORROSION BEYOND LIMITS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001572001091200157SW 2001 9 12 HEEA075538 120010821G3246206323017 CROSSTUBE BELL 206 206L3 1182108SW MLG SKID CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0342EA 51542 CORROSION PITS UNDER BOTH SADDLE MOUNT AREAS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001582001091200158SW 2001 9 12 HEEA075539 120010821G3246206323018 CROSSTUBE BELL 206 206L3 1182108SW MLG SKID CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036748D 51106 CORROSION BEYOND LIMITS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001592001091200159SW 2001 9 12 HEEA075540 120010821G3246206324007 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03979BH 51403 CORROSION BEYOND LIMITS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001602001091200160SW 2001 9 12 HEEA075541 120010821G3246206324008 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03979BH 51403 CORROSION BEYOND LIMITS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001612001091200161SW 2001 9 12 HEEA075542 120010821G3246206324459 SKID BELL 206 206L3 1182108SW MLG DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 RIVET POPPED. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001622001091200162SW 2001 9 12 HEEA075543 120010821G3246206324459 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036748D 51106 CORROSION BEYOND LIMITS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001742001091200174SW 2001 9 12 HEEA075544 120010821G3246206324460 SKID BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036748D 51106 CORROSION BEYOND LIMITS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001752001091200175SW 2001 9 12 HEEA075545 120010821G6520212040004009 GEARBOX BELL 412 412 1182202SW TAIL ROTOR LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 INPUT QUILL SEAL LEAKING. REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010912001772001091200177SW 2001 9 12 HEEA075546 120010821G6300212040005103 DRIVE SHAFT BELL 412 412 1182202SW MAIN ROTOR LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 GREASE SEALS LEAKING. REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010912001792001091200179SW 2001 9 12 HEEA075548 120010821G6510212040600005 BEARING BELL 412 412 1182202SW TAIL ROTOR OVERHEATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 OVERTEMP INDICATION. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010912001802001091200180GL 2001 9 12 HEEA075549 220010821G753223005366 BLEED VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 ENGINE T.O.T. RUNNING HIGHER THAN NORMAL. REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E1GL 20010912001822001091200182GL 2001 9 12 HEEA075550 220010821G753223005366 BLEED VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 ENGINE T.O.T. RUNNING HIGHER THAN NORMAL. REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E1GL 20010912001852001091200185GL 2001 9 12 HEEA075551 220010821G720023008727 SOLENOID BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034835 51131 STUCK OPEN CAUSING HIGH T.O.T. REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E1GL 20010912001902001091200190SW 2001 9 12 HEEA075552 120010821G716023033400 FILTER BELL 206 206L3 1182108SW ENGINE INTAKE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 N1 HANGS UP DURING STARTS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001922001091200192SW 2001 9 12 HEEA075553 120010821G243523081018 STARTER GEN BELL 206 206L3 1182108SW ELECTRICAL FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 GENERATOR WILL NOT RESET. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010912001942001091200194GL 2001 9 12 HEEA075554 220010821G7321252464430 FUEL CONTROL BELL 206 206B3 1181506SW ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0322743 3624 UNABLE TO ADJUST START TEMP. LOW ENOUGH TO GET ENG. STARTED. START MODE FUEL FLOW APPROX. 3 TIMES ALLISON LIMITS. FOUND FLOWS 12PPH HIGH. (METERING VALVE SHIFTED), RECALIBRATED AND TESTED OK. 1G71 3U3 U H2SW E1GL 20010912001972001091200197GL 2001 9 12 HEEA075555 220010821G7323252469211 GOVERNOR BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 UNABLE TO CORRECT OVERSPEED. FOUND GOVERNOR BREAK RESPONDED 100 RPM EARLY. TESTED SATISFACTORY. 1G71 3U3 U H2SW E1GL 20010912002032001091200203GL 2001 9 12 HEEA075556 220010821G732125490925 FUEL CONTROL BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03310732534 51519 ENGINE WOULD NOT ACCELERATE ON START, ADJUSTING START DERICHMENT AND START ACCELERATION TO MAXIMUM HAD NO EFFECT. FOUND PRESSURIZING VALVE TO BE STICKING. REMOVED VALVE AND POLISHED. VALVE WOULD STILL HANG UP. REPLACED VALVE AND UNIT TESTED SATISFACTORY. 1G71 3U3 U H2SW E1GL 20010912002042001091200204GL 2001 9 12 HEEA075557 220010821G732125490925 FUEL CONTROL BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034282Z9935 51499 START ACCEL ADJUSTMENT FROZEN. REPLACED WITH SERVICEABLE FUEL CONTROL. 1G71 3U3 U H2SW E1GL 20010912002082001091200208SW 2001 9 12 HEEA075558 120010821G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN BATTERY DISCHARGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038587X 51464 LOW STARTING CAPACITY AND WILL NOT TAKE A FULL CHARGE. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20010912002092001091200209SW 2001 9 12 HEEA075559 120010821G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN BATTERY OVERHEATED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW034835 51131 BATTERY HOT LIGHT CAME ON. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20010912002122001091200212SW 2001 9 12 HEEA075560 120010821G6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R11837 36007 BLADE DIVES UNABLE TO TRACK. 1G72 4U H4SW 20010912002132001091200213SW 2001 9 12 HEEA075561 120010821G6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR MISMANUFACTURED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R11544 36007 BLADE EXCESSIVELY HEAVY AND CANNOT GET TO 80 PERCENT ROTOR RPM. 1G72 4U H4SW 20010912002142001091200214SW 2001 9 12 HEEA075562 120010821G3213412050010111A CROSSTUBE BELL 412 412 1182202SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z3621 36019 CROSSTUBE CORRODED. SCRAPPED. 1G72 4U H4SW 20010913000012001091300001SW 2001 9 13 HEEA075563 120010821G3212412050013113 FLOAT BELL 412 412 1182202SW RT MLG LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 RT MID FLOAT BAG LEAKING AROUND RELIEF VALVE. SENT TO OFFSHORE HELICOPTER SUPPORT FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20010913000022001091300002SW 2001 9 13 HEEA075564 120010821G3212412050013113 FLOAT BELL 412 412 1182202SW MLG LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 FLOAT BAG LEAKING. 1G72 4U H4SW 20010913000032001091300003SW 2001 9 13 HEEA075565 120010821G3246412050015110 SKID BELL 412 412 1182202SW MLG DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 FWD SADDLE RIVETS LOOSE. SCRAPPED AND REPLACED WITH SERVICEABLE TUBE. 1G72 4U H4SW 20010913000042001091300004SW 2001 9 13 HEEA075566 120010821G3212412050017133 COVER BELL 412 412 1182202SW FLOAT BAG TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032258F 33073 FLOAT BAG COVER VELCRO TORN. 1G72 4U H4SW 20010913000052001091300005SW 2001 9 13 HEEA075567 120010821G3212412050017133 COVER BELL 412 412 1182202SW FLOAT BAG WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 FLOAT BAG COVER VELCRO WORN. 1G72 4U H4SW 20010913000062001091300006SW 2001 9 13 HEEA075568 120010821G3212412050017135 COVER BELL 412 412 1182202SW FLOAT BAG TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032258F 33073 FLOAT BAG VELCRO TORN. 1G72 4U H4SW 20010913000072001091300007SW 2001 9 13 HEEA075569 120010821G3213412050045107 CROSSTUBE BELL 412 412 1182202SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R1290 36007 FOUND CORROSION UNDER CENTER PIVOT MOUNT. SCRAPPED AND REPLACED WITH SERVICEABLE TUBE. 1G72 4U H4SW 20010913000082001091300008SW 2001 9 13 HEEA075570 120010821G5210412060804101 HINGE BELL 412 412 1182202SW PAX DOOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 RIVET LOOSE. REPLACED WITH SERVICEABLE HINGE. 1G72 4U H4SW 20010913000092001091300009SW 2001 9 13 HEEA075571 120010821G2810412061668101 CAP BELL 412 412 1182202SW FUEL CELL DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035759N 33002 CAP CAN TURN BEYOND OPEN POSITION OR OFTEN MISPOSITIONS CLOSURE CLAWS CAUSING CAP TO BE DIFFICULT TO REMOVE. REPLACED WITH SERVICEABLE ASSY. 1G72 4U H4SW 20010913000102001091300010 2001 9 13 HEEA075572 420010821G2330002000002 AMPLIFIER BELL 412 412 1182202SW PA SYSTEM INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW0333008 36004 PA INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. FOUND FUSE F1 AND TRANSISTOR Q8 BAD. REPLACED. BENCH CHECK GOOD. 1G72 4U H4SW 20010913000112001091300011 2001 9 13 HEEA075573 420010821G2312064101900 RADIO BELL 206 206L3 1182108SW VHF COMMS WEAK E HEEAK NONE O OTHER ININSP/MAINT 1 SW033107N 51512 GARBLED AND WEAK. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT HAD TOO MUCH POWER OUT BUT GOOD MODULATION. THEN MODULATORS BECAME VERY WEAK AND DISTORTED. FOUND Q121, Q122 TRANSISTORS BAD. REPLACED Q121 AND Q122 TRANSISTORS. ADJUSTED MIC GAIN AND SIDETONE. REPAIRED. FOUND MEMORY NOT WORKING DUE TO BROKEN FOIL ON SW102 SWITCH. REPAIRED BROKEN FOIL. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20010913000122001091300012 2001 9 13 HEEA075574 420010821G2312064101900 RADIO BELL 206 206L1 1182107SW VHF COMMS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW031076Y 45380 WOULD NOT CHANGE FREQUENCY. REPLACED BAD KHZ KNOB/SHAFT AND RESOLDERED COLD SOLDER ON SW102 SWITCH. REPAIRED. ALIGNED RECEIVER AND ADJUSTED C/N SQUELCH, MIC GAIN AND SIDETONE. REPLACED BAD DISPLAY LENS. BENCH CHECK GOOD. 1G71 3U H2SW 20010913000132001091300013 2001 9 13 HEEA075575 420010824G2312064101902 RADIO BELL 206 206L3 1182108SW VHF COMMS INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW038593X 51509 INTERMITTENTLY UNABLE TO CHANGE FREQUENCY. PERFORMED PRELIMINARY INSPECTION. FOUND SELECTOR KNOBS INTERMITTENTLY DO NOT CHANGE FREQUENCY. CLEANED WAFER SWITCHES. REPAIRED. FOUND POWER OUT LOW AT 135 MHZ. REPLACED C623 AND C624 CAPACITORS. REPAIRED. ADJUSTED C/N SQUELCH, MIC GAIN AND SIDETONE. BENCH CHECK GOOD. 1G71 3U H2SW 20010913000142001091300014 2001 9 13 HEEA075576 420010824G2312064102300 TRANSCEIVER BELL 412 412 1182202SW VHF COMMS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 SQUELCH STAYS ON ALL THE TIME AND THE RF CONNECTOR IS DAMAGED. PERFORMED PRELIMINARY INSPECTION. REPLACED BAD RF CONNECTOR. REPAIRED. ADJUSTED CARRIER SQUELCH, FREQUENCY AND POWER OUT. BENCH CHECK GOOD. 1G72 4U H4SW 20010913000152001091300015 2001 9 13 HEEA075577 420010824G2312064102300 TRANSCEIVER BELL 412 412 1182202SW VHF COMMS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0330YM 36032 NO SIDETONE. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT NOT MODULATING AND TRANSMIT POWER OUT EXCESSIVE AND COULD NOT ADJUST EITHER. REPLACED BAD Q109 AND Q110 TRANSISTORS. REPAIRED. ADJUSTED POWER OUT AND SIDETONE. FOUND L505 COIL BROKEN. REPLACED COIL. REMOVED LIGHT CORROSION FROM CHASSIS. BENCH CHECK GOOD. 1G72 4U H4SW 20010913000162001091300016 2001 9 13 HEEA075578 420010824G2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW VHF COMMS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038588X 51486 TRANSMISSION GARBLED. PERFORMED PRELIMINARY INSPECTION. COULD NOT DUPLICATE COMPLAINT BUT FOUND DISPLAY LENS BAD. REPLACED LENS AND REPAIRED. ADJUSTED FREQUENCY AND SIDETONE. BENCH CHECK GOOD. 1G71 3U H2SW 20010913000172001091300017 2001 9 13 HEEA075579 420010824G2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW VHF COMMS FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03205FC 51130 FIRST AND LAST DIGITS DISAPPEAR INTERMITTENTLY. PERFORMED PRELIMINARY INSPECTION. FOUND DISPLAY NOT DIMMING PROPERLY. REPLACED V901 PHOTOCELL. REPAIRED. FOUND FREQUENCY SELECTORS INTERMITTENT AND MHZ CHANGED BY ITSELF A COUPLE OF TIMES. FOUND FREQUENCY SELECTOR CONTACTS VERY DIRTY. CLEANED. REPAIRED. REGLUED DISPLAY LENS WHICH WAS LOOSE. ADJUSTED FREQUENCY. BENCH CHECK GOOD. 1G71 3U H2SW 20010913000182001091300018 2001 9 13 HEEA075580 420010824G2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW VHF COMMS FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038588X 51486 SQUELCH WILL NOT RESET AFTER RECEPTION OR TEST. SENT TO HONEYWELL, KANSAS FOR WARRANTY REPAIR. 1G71 3U H2SW 20010913000192001091300019 2001 9 13 HEEA075581 420010824G2312066106200 TRANSCEIVER BELL 206 206B3 1181506SW VHF COMMS FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0322743 3624 WILL NOT TRANSMIT AT THE RIGHT FREQUENCY. PERFORMED PRELIMINARY INSPECTION. ADJUSTED FREQUENCY, PULSE WIDTH AND POWER. ALIGNED PRESELECTOR AND IF. REPAIRED. ALSO REPLACED BAD V301 PHOTOCELL. UNIT BENCH CHECK GOOD. 1G71 3U H2SW 20010913000202001091300020 2001 9 13 HEEA075582 420010824G2312066106200 TRANSCEIVER BELL 206 206L1 1182107SW VHF COMMS BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033905B 45598 SELECTOR KNOB BROKEN INTERNALLY. PERFORMED PRELIMINARY INSPECTION. FOUND FACEPLATE BAD. REPLACED FACEPLATE. REPAIRED. CLEANED CODE SELECTOR WAFER SWITCHES. ALIGNED IF SECTION. UNIT BENCH CHECK GOOD. 1G71 3U H2SW 20010913000212001091300021 2001 9 13 HEEA075583 420010824G2312066106200 TRANSCEIVER BELL 206 206L4 1182110SW VHF COMMS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0362127 52023 NO REPLY. PERFORMED PRELIMINARY INSPECTION. FOUND REPLY LIGHT VERY DIM DUE TO BAD PHOTOCELL. REPLACED V301 PHOTOCELL. REPAIRED PROBLEM. ALSO REPLACED BAD R477 RESISTOR AND ADJUSTED FREQUENCY AND PULSE WIDTH. BENCH CHECK GOOD. 1G71 3U NCH2SW 20010913000222001091300022 2001 9 13 HEEA075584 420010824G2312066106200 TRANSCEIVER BELL 206 206L3 1182108SW VHF COMMS FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0330KH 51527 NO TRANSMIT. PERFORMED PRELIMINARY INSPECTION. FOUND FOUND V101 CAVITY OSCILLATOR BAD. REPLACED V101, REPAIRED. ADJUSTED TO SPECS. BENCH CHECK GOOD. 1G71 3U H2SW 20010913000232001091300023 2001 9 13 HEEA075585 420010824G2312066106200 TRANSCEIVER BELL 206 206L3 1182108SW VHF COMMS FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0341128 51134 UNIT FAILED ALTITUDE CERTIFICATION. UNIT TRANSMITS IMPROPER CODES BETWEEN 700 AND 900 PA. PERFORMED PRELIMINARY INSPECTION. ADJUSTED TUBE FOR PROPER FREQUENCY BAND WIDTH. BENCH CHECK GOOD. 1G71 3U H2SW 20010913000242001091300024 2001 9 13 HEEA075586 420010824G2312066106200 TRANSCEIVER BELL 206 206L3 1182108SW VHF COMMS FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036161A 51611 NOT TRANSMITTING. PERFORMED PRELIMINARY INSPECTION. FOUND DRAWING EXCESSIVE CURRENT. FOUND Q1 AND Q3 SHORTED. SENT TO AVCOM AVIONICS & INSTRUMENTS FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010913000252001091300025 2001 9 13 HEEA075587 420010824G3452066107100 TRANSPONDER BELL 412 412 1182202SW ATC FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321498 36003 WENT DEAD. PERFORMED PRELIMINARY INSPECTION. FOUND CR106 DIODE BURNT AND C111 CAPACITOR SHORTED. ALSO FOUND C115 CAPACITOR BAD. REPLACED CR106 DIOD AND C111 AND C115 CAPACITORS. ADJUSTED MTL. UNIT BENCH CHECK GOOD. 1G72 4U H4SW 20010913000262001091300026 2001 9 13 HEEA075589 420010827G2312066107800 RECEIVER BELL 412 412 1182202SW NAVIGATION FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0322347 36005 BAD FROM STOCK. FOUND AT 60 DEGREES TO. NEEDLE DOES NOT FOLLOW WHEN TURNING COMPASS. SENT TO GREATLAKES AVIONICS FOR WARRANTY REPAIR. 1G72 4U H4SW 20010913000272001091300027 2001 9 13 HEEA075590 420010827G3416066304400 ALTIMETER BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 DH LIGHT IS INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. FOUND DH SWITCH BROKEN AND LENS CLAMP BROKEN. INSTALLED DH SWITCH AND LENS CLAMP. ALSO REPLACED THE PHOTOCELL. THE DH LIGHT STAYS ON AT ALL TIMES AND NO SELF TEST. SENT TO GREATLAKES AVIONICS FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20010913000822001091300082 2001 9 13 HEEA075591 420010827G23120691024155 TRANSCEIVER BELL 206 206L3 1182108SW VHF COMMS INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW036251X 51552 DIGITAL SEGMENTS ARE INTERMITTENT. PERFORMED PRELIMINARY INSPECTION. REPLACED DISPLAY. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20010913000832001091300083 2001 9 13 HEEA075592 420010827G3452071119218 CONTROL PANEL BELL 214 214ST 1182106SW ATC INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW0359806 28140 DIGITS INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. FOUND HEADER BAD. DIGITS INTERMITTENTLY FLICKERS. DRIVER BOARD CAUSING SOME BRIGHT SEGMENTS ON DISPLAY. INSTALLED HEADER P305, J304, CAPACITOR NETWORK U301. DIGITS WILL NOT CHANGE WHEN DIAL IS TURNED. SENT TO HONEYWELL, KANSAS FOR INSPECTION AND REPAIR. 2G72 4U H10SW 20010913000842001091300084 2001 9 13 HEEA075593 420010827G2312071121525 CONTROL UNIT BELL 214 214ST 1182106SW COCKPIT INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW0359806 28140 DISPLAY HAS ONE DIGIT INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. FOUND IC 201 BAD. REPLACED. BENCH CHECK GOOD. 2G72 4U H10SW 20010913000852001091300085 2001 9 13 HEEA075594 420010827G2312071121540 CONTROL UNIT BELL 412 412 1182202SW VHF COMMS FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037128R 36007 UNIT DOES NOT KEEP LAST TWO DIGITS WHEN TURNED ON. PERFORMED PRELIMINARY INSPECTION. FOUND IC 1205 BAD. REPLACED. BENCH CHECK GOOD. 1G72 4U H4SW 20010913000862001091300086 2001 9 13 HEEA075595 420010827G3455066107700 RECEIVER BELL 412 412 1182202SW ADF INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 ADF RECEIVER INOPERATIVE. 1G72 4U H4SW 20010913000872001091300087SW 2001 9 13 HEEA075596 120010827G2824205060606003 PUMP BELL 412 412 1182202SW FUEL TRANSFER INOPERATIVE E HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW032149S 36002 WHILE IN CRUISE FLIGHT, NR 2 FUEL TRANSFER LIGHT ILLUMINATED. REPLACED INOPERATIVE NR 2 TRANSFER PUMP. 1G72 4U H4SW 20010913000882001091300088SW 2001 9 13 HEEA075598 120010827G6320406340100101 PUMP BELL 407 407 SW OIL SYSTEM LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03407PH 53003 INTERNAL SEAL LEAKING. 1G71 3U O H2SW 20010913000892001091300089SW 2001 9 13 HEEA075605 120010827G2844407362013101 PRESSURE SWITCH BELL 407 407 SW FUEL SYSTEM FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03510PH 53209 NO LIGHT WHEN PUMP IS OFF. 1G71 3U O H2SW 20010913000902001091300090SW 2001 9 13 HEEA075607 120010827G3340407076502103S CONNECTOR BELL 407 407 SW CABIN CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 CANNON PLUG CORRODED. REPEATED PROBLEM WITH CANNON PLUG, SENDING IN FOR EVALUATION FOR POSSIBLE MFG DEFECT. 1G71 3U O H2SW 20010913000912001091300091 2001 9 13 HEEA075609 420010828G2350100005430 HEADSET BELL 206 206L3 1182108SW AUDIO SYSTEM INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 INOPERATIVE. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913000932001091300093 2001 9 13 HEEA075610 420010828G34101113025 INDICATOR BELL 412 412 1182202SW HSI MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 CAUSED THE FLIGHT DIRECTOR TO OSCILLATE IN HEADING MODE. 1G72 4U H4SW 20010913000962001091300096 2001 9 13 HEEA075611 420010828G34201113025 INDICATOR BELL 412 412 1182202SW HSI MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 COURSE NEEDLE WILL NOT FOLLOW COPILOT'S COURSE NEEDLE. 1G72 4U H4SW 20010913000972001091300097 2001 9 13 HEEA075612 420010828G34211113034 INDICATOR BELL 412 412 1182202SW AFCS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0330YM 36032 RATCHETY IN FLIGHT AND CAUSES AFCS TO KICK. 1G72 4U H4SW 20010913000992001091300099 2001 9 13 HEEA075613 420010828G34201258103 INDICATOR BELL 412 412 1182202SW HSI INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW035759N 33002 COURSE SET 10 DEGREES OFF. 1G72 4U H4SW 20010913001002001091300100 2001 9 13 HEEA075614 420010828G345713824120234 RECEIVER BELL 206 206B3 1181506SW GPS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032268V 3605 LOSES ITSELF. PERFORMED PRELIMINARY INSPECTION. COULD NOT DUPLICATE PROBLEM. FOUND NAV, AUX AND ENT BUTTONS VERY INTERMITTENT. REPLACED. FOUND D12 BACKLIGHTING BULB INOPERATIVE. REPLACED. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20010913001022001091300102 2001 9 13 HEEA075615 420010828G345713824120234 RECEIVER BELL 206 206L3 1182108SW GPS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03129MR 51129 CLEARS ITSELF WHEN TURNED OFF, HAS TO HAVE MGUA CODE ENTERED AND UNABLE TO DISABLE SAFEGUARD. PERFORMED PRELIMINARY INSPECTION. CLEANED MEMORY AND REPROGRAMMED. ALSO DISABLED SAFEGUARD CODE. REPAIRED. BENCH CHECK GOOD. 1G71 3U H2SW 20010913001032001091300103SW 2001 9 13 HEEA075616 120010828G5302206031329103S ATTACH FITTING BELL 206 206L3 1182108SW TAIL BOOM CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 UPPER LT TAIL BOOM FITTING CRACKED AT MOST FWD OUTBOARD RIVET HOLE. REPLACED WITH SERVICEABLE FITTING. 1G71 3U H2SW 20010913001042001091300104SW 2001 9 13 HEEA075617 120010828G5340206033109001 FITTING BELL 206 206L3 1182108SW FUSELAGE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW0342EA 51542 WORN. SCRAPPED AND REPLACED WITH SERVICEABLE FITTING. 1G71 3U H2SW 20010913001052001091300105SW 2001 9 13 HEEA075618 120010828G3213206053203115 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 CORROSION PITS. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20010913001072001091300107SW 2001 9 13 HEEA075619 120010828G6710206062721109 ACTUATOR BELL 206 206L3 1182108SW ENGINE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW036160Z 51610 ACTUATOR INOPERATIVE. 1G71 3U H2SW 20010913001092001091300109SW 2001 9 13 HEEA075620 120010828G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0342EA 51542 EXHAUST STACK CRACKED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913001102001091300110SW 2001 9 13 HEEA075621 120010828G7810206064300005 EXHAUST STACK BELL 206 206L3 1182108SW ENGINE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 EXHAUST STACK CRACKED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913001132001091300113SW 2001 9 13 HEEA075622 120010828G7910206064522101 TUBE BELL 206 206L3 1182108SW OIL SYSTEM MISMANUFACTURED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038588X 51486 APPROXIMATELY 3/8 INCH TOO SHORT SPANWISE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913001142001091300114SW 2001 9 13 HEEA075623 120010828G2120206070936001 FLAPPER VALVE BELL 206 206L3 1182108SW AIR DISTRIBUTIONBROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036251Y 51556 LEVER ON FLAPPER BROKEN. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913001252001091300125SW 2001 9 13 HEEA075624 120010828G2510206072841111 SEAT BELT BELL 206 206L3 1182108SW COCKPIT FRAYED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0330KH 51527 FRAYED BELT. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913001272001091300127SW 2001 9 13 HEEA075625 120010828G7930206075187003 INDICATOR BELL 206 206L3 1182108SW OIL TEMP READS HIGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 INDICATOR READS 8 PSI HIGH. 1G71 3U H2SW 20010913001312001091300131SW 2001 9 13 HEEA075626 120010828G2420206075447007 VOLT REGULATOR BELL 206 206L3 1182108SW AC SYSTEM MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 GENERATOR FAIL CAUTION LIGHT CAME ON. 1G71 3U H2SW 20010913001332001091300133SW 2001 9 13 HEEA075627 120010828G2420206075447007 VOLT REGULATOR BELL 206 206L3 1182108SW AC SYSTEM FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036161A 51611 GEN FAILED LIGHT ILLUMINATED, GEN WENT OFF LINE WHEN THROTTLE ROLLED DOWN TO IDLE. 1G71 3U H2SW 20010913001342001091300134SW 2001 9 13 HEEA075628 120010828G2420206075447007 VOLT REGULATOR BELL 206 206L3 1182108SW AC SYSTEM FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 GENERATOR WILL NOT STAY ON LINE. 1G71 3U H2SW 20010913001362001091300136SW 2001 9 13 HEEA075629 120010828G6420206075545005 SENSOR BELL 206 206L3 1182108SW ROTOR RPM FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033116P 51530 NO SIGNAL SENT TO INDICATOR. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913001392001091300139 2001 9 13 HEEA075630 420010828G3421206075606103 GYRO BELL 206 206L3 1182108SW COCKPIT PRECESSES E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 PRECESSING 10 DEGREES PER MINUTE. 1G71 3U H2SW 20010913001402001091300140SW 2001 9 13 HEEA075631 120010828G7714206075681101 INDICATOR BELL 206 206L1 1182107SW DUAL TACH STICKS E HEEAK NONE O OTHER ININSP/MAINT 1 SW035019F 45244 TURBINE NEEDLE STICKS DURING START. 1G71 3U H2SW 20010913001422001091300142SW 2001 9 13 HEEA075632 120010828G7714206075681105 INDICATOR BELL 206 206L3 1182108SW DUAL TACH FLUCTUATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW033116P 51530 FLUCTUATE IN FLIGHT OR GOES TO ZERO. 1G71 3U H2SW 20010913001432001091300143SW 2001 9 13 HEEA075633 120010828G7714206075681117 INDICATOR BELL 206 206L3 1182108SW DUAL TACH FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 TURBINE NEEDLE NOT WORKING. 1G71 3U H2SW 20010913001442001091300144SW 2001 9 13 HEEA075634 120010828G7714206075681123 INDICATOR BELL 206 206L3 1182108SW DUAL TACH INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 NEEDLES OFF ZERO. 1G71 3U H2SW 20010913001462001091300146SW 2001 9 13 HEEA075635 120010828G7714206075682107 INDICATOR BELL 206 206L3 1182108SW GAS PRODUCER ERRATIC E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 INDICATOR VERY ERRATIC AND UNRELIABLE IN THE LOW RANGE DURING STARTS. 1G71 3U H2SW 20010913001612001091300161SW 2001 9 13 HEEA075636 120010828G7712206075739103 TORQUEMETER BELL 206 206L3 1182108SW COCKPIT FLUCTUATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW0342EA 51542 INDICATOR HAS A CONSTANT FLUCTUATION IN CRUISE FLIGHT. REPLACED WITH SERVICEABLE INDICATOR. 1G71 3U H2SW 20010913001782001091300178SW 2001 9 13 HEEA075637 120010828G6321206076047003 CYLINDER BELL 206 206L1 1182107SW ROTOR BRAKE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035019F 45244 ROTOR BRAKE WILL NOT ENGAGE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913001792001091300179SW 2001 9 13 HEEA075638 120010828G5260206301109 STEP BELL 206 206L3 1182108SW FUSELAGE CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036748D 51106 CORROSION ON STEP BEYOND LIMITS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913001812001091300181SW 2001 9 13 HEEA075639 120010828G7933206375007103 INDICATOR BELL 206 206L3 1182108SW TOT WILL NOT TEST E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0330KH 51527 TOT LIGHT WILL NOT TEST. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913001822001091300182SW 2001 9 13 HEEA075640 120010828G5260206301110 STEP BELL 206 206L3 1182108SW FUSELAGE CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036748D 51106 CORROSION ON STEP BEYOND LIMITS. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913001832001091300183SW 2001 9 13 HEEA075641 120010828G7933206375007103 INDICATOR BELL 206 206L3 1182108SW TOT INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW0392MT 51175 TOT INDICATOR NEEDLE INTERMITTENTLY STICKS AT ZERO DURING START. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913001872001091300187SW 2001 9 13 HEEA075642 120010828G2844209062003001 SWITCH BELL 412 412 1182202SW FUEL SYSTEM MALFUNCTIONED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW036559Z 36019 FLICKERING LIGHT. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010913001922001091300192SW 2001 9 13 HEEA075643 120010828G7160209062214001 ACTUATOR BELL 412 412 1182202SW AIR INTAKE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03108X 33115 ACTUATOR INOPERATIVE. 1G72 4U H4SW 20010913001932001091300193SW 2001 9 13 HEEA075644 120010828G7922209070262101 REGULATOR BELL 412 412 1182202SW OIL TEMP MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 NOT MARKING PROPERLY. 1G72 4U H4SW 20010913001942001091300194SW 2001 9 13 HEEA075645 120010828G7933209070262101 INDICATOR BELL 412 412 1182202SW ENGINE OIL READS HIGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 READS 30 PSI HIGH. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010913001952001091300195SW 2001 9 13 HEEA075646 120010828G7931209070262101 INDICATOR BELL 412 412 1182202SW ENGINE OIL READS LOW E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 READS 5 PSI LOW. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010913001962001091300196SW 2001 9 13 HEEA075647 120010828G29122111328 FILTER ELEMENT BELL 206 206L1 1182107SW HYD SYSTEM BYPASSING E HEEAK NONE O OTHER ININSP/MAINT 1 SW035019F 45244 BYPASS INDICATOR EXTENDED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20010913001972001091300197SW 2001 9 13 HEEA075648 120010828G29122111328 FILTER ELEMENT BELL 206 206L4 1182110SW HYD SYSTEM BYPASSING E HEEAK NONE O OTHER ININSP/MAINT 1 SW037074W 52033 BYPASS BUTTON POPPED. REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20010913001982001091300198SW 2001 9 13 HEEA075649 120010828G7120212060718001 BEARING BELL 412 412 1182202SW ENGINE MOUNT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20010913001992001091300199SW 2001 9 13 HEEA075650 120010828G8011214060056705 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 CLUTCH SLIPPAGE, OUT OF LIMITS AND STICKING 2G72 4U H10SW 20010913002002001091300200SW 2001 9 13 HEEA075651 120010829G3212206050247135 COVER BELL 407 407 SW FLOAT BAG DETERIORATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0357416 53070 DETERIORATED. SCRAPPED IN HOUSE. PHI REQUESTS FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#68645101. 1G71 3U O H2SW 20010913002182001091300218SW 2001 9 13 HEEA075653 120010831G6220206011149105 YOKE BELL 206 206L3 1182108SW MAIN ROTOR HEAD SPALLED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 SPAULDING ON OUTBOARD JOURNAL, SCUFFING ON INBOARD JOURNAL AND CORROSION ON RETAINER BORE. SENT TO BELL HELICOPTER TEXTRON FOR WARRANTY REPAIR. REFERENCE: DMR#727503. 1G71 3U H2SW 20010913002202001091300220SW 2001 9 13 HEEA075654 120010831G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 BURNED AND WON'T CROSS START. 2G72 4U H10SW 20010913002212001091300221EU 2001 9 13 HEEA075655 120010821G63204638302002 PINION GEAR 4638001004 BOLKMS105 BO105S 5626006EU M/R GEARBOX SPALLED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911HM 226 S683 GEAR TEETH SPALLING AT TOOTH TIP. REPLACED WITH SERVICEABLE PART. 1G72 3U H3EU 20010913002232001091300223EU 2001 9 13 HEEA075656 120010821G63204638303001 BEVEL GEAR 4638001004 BOLKMS105 BO105S 5626006EU M/R GEARBOX SPALLED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911HM 226 S683 GEAR TEETH SPALLING AT TOOTH ROOT. REPLACED WITH SERVICEABLE PART. 1G72 3U H3EU 20010913002242001091300224 2001 9 13 HEEA075657 420010824G2350066105571 AUDIO PANEL BOLKMS105 BO105S 5626006EU COCKPIT INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381982 S818 ICS INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. FOUND SWITCH S211 BAD AND SWITCHES S201 THROUGH 210 NOISY. REPLACED SWITCH S211 AND CLEANED SWITCHES S201 THROUGH 210 WITH MISTY CONTACT CLEANER. REPAIRED. BENCH CHECK GOOD. 1G72 3U H3EU 20010913002442001091300244EU 2001 9 13 HEEA075658 120010824G2435150SG122Q STARTER GEN SNIAS 350 AS350B2 8680813EU ELECTRICAL FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0340466345 3004 WOULD NOT START OR GENERATE POWER. 1G71 3U H9EU 20010913002452001091300245EU 2001 9 13 HEEA075659 120010824G6410355A12004008 BLADE SNIAS 350 AS350B2 8680813EU TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034000L3850 2873 TAIL ROTOR BLADE HAS A CRACKED SPAR. 1G71 3U H9EU 20010913002482001091300248 2001 9 13 HEEA075660 420010827G2312071121540 CONTROL PANEL BOLKMS105 BO105S 5626006EU VHF COMMS FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034302G S853 DISPLAY UNREADABLE. PERFORMED PRELIMINARY INSPECTION. FOUND DISPLAY SEGMENTS UNREADABLE. FOUND CORROSION UNDER J203 HEADER CAUSING PROBLEM. REMOVED HEADER AND REMOVED CORROSION. REPLACED J203 HEADER AND APPLIED HUMISEAL AROUND HEADER FOR CORROSION CONTROL. REPAIRED DISPLAY PROBLEM. FOUND TRANSFER SWITCH INTERMITTENT. CLEANED S102 TRANSFER SWITCH. REPAIRED AND BENCH CHECK GOOD. 1G72 3U H3EU 20010913002492001091300249EU 2001 9 13 HEEA075661 120010828G793310590947 INDICATOR BOLKMS105 BO105S 5626006EU TOT INCORRECT E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 COULD NOT REMOVE ERRORS. OFF AT EACH END OF SCALE. 1G72 3U H3EU 20010913002512001091300251EU 2001 9 13 HEEA075662 120010828G551011730550 STRUCTURE BOLKMS117 BK117A1 5626010EU HORIZONTAL STAB DEBONDED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03911TL 7198 PAINT PEELED AND TRAILING EDGE DEBONDED. 1G72 3U H13EU 20010913002522001091300252EU 2001 9 13 HEEA075663 120010828G551011730550 STRUCTURE BOLKMS117 BK117A1 5626010EU HORIZONTAL STAB DETERIORATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03911RZ 7092 PAINT DETERIORATED, STRIP. METAL TRAILING EDGE ALODINED AND PRIMED. RIGHT DEVORE FLOODLIGHT INSERT LOOSE. 1G72 3U H13EU 20011001000932001100100093 2001 10 1 HEEA075926 420010910G3416066303102 ALTIMETER COCKPIT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 PARTS LOOSE INSIDE. SENT TO FIELDTECH AVIONICS, INC. FOR WARRANTY REPAIR. 20011002000632001100200063GL 2001 10 2 HEEA075927 220010910G7323252469211 GOVERNOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE FAILED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW035435V 760158 CAE890469S ENGINE N2, T5, FUEL FLOW AND N1 ALL BLEED OFF PRIOR TO REACHING ENGINE LIMITING CHECK PARAMETERS. REPLACED WITH SERVICEABLE PART. 1G72 3U3 U H1NE E1GL 20011002000662001100200066GL 2001 10 2 HEEA075928 220010918G725023062753 NOZZLE BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL TURBINE VANE BURNED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032270G 3610 CAE835824 BOLT BROKEN OFF IN NR 6 & 7 JET MOUNT. NR 1 NOZZLE VANES BURNED BEYOND REPAIRABLE LIMITS. OVERTEMP INSPECTION CW 2-23-00 FOR A 930 DEGREE EXCEEDANCE AND FOUND ACCEPTABLE. PART SCRAPPED. REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E4CE 20011002000682001100200068GL 2001 10 2 HEEA075929 220010918G72506886407 TURBINE WHEEL BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL TURBINE SECTION DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032270G808 3610 CAE835824 BOLT BROKEN OFF IN #6&7 JET MOUNT. WHEEL BLADES SULPHIDATED DUE TO OVERTEMP OF 930 DEGREES ON 2-23-00. PARTS WERE FOUND TO BE ACCEPTABLE WHEN INSPECTED FOR OVERTEMP. PART SCRAPPED. REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E4CE 20011002000692001100200069GL 2001 10 2 HEEA075930 220010918G72506898782 TURBINE WHEEL BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL ENGINE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032270G808 3610 CAE835824 BOLT BROKEN OFF IN 6&7 JET MOUNT. WHEEL BLADES SULPHIDATED DUE TO OVERTEMP OF 930 DEGREES ON 2-23-00. PARTS WERE FOUND TO BE ACCEPTABLE WHEN INSPECTED FOR OVERTEMP. PART SCRAPPED. REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E4CE 20011002000712001100200071NE 2001 10 2 HEEA075931 120010924G7500650852201 VALVE SKRSKYS76 S76A 8143006NE NR 1 ENGINE MALFUNCTIONED E HEEAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION HOHOVERING 1 SW03760PH 760078 WHEN ATTEMPTING TO DEPART, A LARGE TORQUE SPLIT OCCURRED WHEN ATTEMPTING TO PICK UP INTO A HOVER. INSPECTION OF NR 1 ENGINE BY PILOT REVEALED THE PC SAFETY VALVE PARTIALLY CLOSED. PILOT OPENED VALVE AND COMPLIED WITH POWER CHECK AND FOUND NORMAL. MAINTENANCE INSPECTED VALVE AND ENGINE. RELEASED AIRCRAFT FOR SERVICE. 1G72 3U H1NE 20011002000722001100200072SW 2001 10 2 HEEA075933 120010910G2824205060606003 PUMP BELL 412 412 1182202SW FUEL TRANFER INOPERATIVE E HEEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW032149S 36002 WHILE IN CRUISE FLIGHT, NR 2 TRANSFER LIGHT ILLUMINATED. REPLACED INOPERATIVE NR 2 TRANSFER PUMP. 1G72 4U H4SW 20011002000752001100200075 2001 10 2 HEEA075934 420010910G2312064101902 TRANSCEIVER BELL 206 206L1 1182107SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035007N 45184 FIRST START OF THE DAY UNIT WOULD NOT TRANSMIT. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011002000762001100200076 2001 10 2 HEEA075935 420010910G2312066106200 TRANSCEIVER BELL 206 206L1 1182107SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035019F 45244 NO INDICATED OUTPUT. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011002000772001100200077GL 2001 10 2 HEEA075936 220010910G7412103815504 EXCITER BELL 412 412 1182202SW ALLSN 250B 250B* GL ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032258F 33073 CAUSING THE CIRCUIT BREAKER TO POP. 1G72 4U3 T H4SW E10CE 20011002000892001100200089SW 2001 10 2 HEEA075938 120010910G6330206033554101 LINK BELL 206 206L4 1182110SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037074W 52033 ELASTOMERIC PURGING OUT OF MOUNT. 1G71 3U NCH2SW 20011002000902001100200090SW 2001 10 2 HEEA075939 120010910G7714206075682107 INDICATOR BELL 206 206L3 1182108SW GAS PRODUCER ERRATIC E HEEAK NONE O OTHER ININSP/MAINT 1 SW036251X 51552 ERRATIC BETWEEN 0-15 DEGREES. 1G71 3U H2SW 20011002000912001100200091SW 2001 10 2 HEEA075941 120010910G6510212040600005 HANGER ASSY BELL 412 412 1182202SW TAIL ROTOR LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 COUPLING LEAKING GREASE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011002000932001100200093SW 2001 10 2 HEEA075942 120010910G7722212075067105 INDICATOR BELL 412 412 1182202SW ITT FLUCTUATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW035759N 33002 FLUCTUATING AT HIGH TEMPERATURES. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011002000942001100200094SW 2001 10 2 HEEA075943 120010910G6730212076005111 SERVO BELL 412 412 1182202SW ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW032149S 36002 TOP PILOT VALVES LEAK WHEN THE AIRCRAFT IS STATIC, NOT RUNNING. NO LEAKS WHEN AIRCRAFT RUNS IS A STATIC LEAK ONLY. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011002000952001100200095SW 2001 10 2 HEEA075944 120010910G2820214066226103 CHECK VALVE BELL 412 412 1182202SW INTERMITTENT E HEEAK NONE N FALSE WARNING ININSP/MAINT 1 SW032148K 36001 INTERMITTENT LIGHT. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011002000972001100200097 2001 10 2 HEEA075945 420010910G22002593996333 TARSYN BELL 212 212 1181420SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035736D 31135 PILOTS ADI BEGAN TUMBLING IN LEVEL FLIGHT. REPLACED WITH SERVICEABLE PART. 1G71 4U H4SW 20011002000982001100200098SW 2001 10 2 HEEA075946 120010910G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0331077 51520 WEAK BATTERY. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011002000992001100200099GL 2001 10 2 HEEA075947 220010910G7320324473513 FUEL CONTROL BELL 412 412 1182202SW ALLSN 250B 250B* GL ENGINE OUT OF ADJ E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 NO TOPPING ADJUSTMENT LEFT. REPLACED WITH SERVICEABLE PART. 1G72 4U3 T H4SW E10CE 20011002001002001100200100SW 2001 10 2 HEEA075948 120010910G6220412010182101 BEARING BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 WORN BEARING. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011002001022001100200102SW 2001 10 2 HEEA075949 120010910G6230412010405109 LINK BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW035759N 33002 WORN BEARING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011002001032001100200103SW 2001 10 2 HEEA075950 120010910G6230412010406115 LINK BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 WORN BEARING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011002001042001100200104SW 2001 10 2 HEEA075951 120010910G6230412010406115 LINK BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 WORN BEARING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011002001052001100200105SW 2001 10 2 HEEA075952 120010910G6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 LARGE CRACK BY MID TRIM TAB. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011002001062001100200106SW 2001 10 2 HEEA075953 120010910G3213412050016102 SHOE BELL 412 412 1182202SW MLG WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW035759N 33002 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011002001072001100200107SW 2001 10 2 HEEA075954 120010910G6710412310400101 ROD END BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011002001102001100200110 2001 10 2 HEEA075955 420010910G342150400179015 INDICATOR BELL 206 206L1 1182107SW COCKPIT PRECESSES E HEEAK NONE O OTHER ININSP/MAINT 1 SW035007Q 45187 WILL NOT CAGE AND PRECESSES. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011002001112001100200111 2001 10 2 HEEA075956 420010910G34578143902240B GPS BELL 412 412 1182202SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0333008 36004 RAIM UNAVAILABLE. 1G72 4U H4SW 20011002001122001100200112 2001 10 2 HEEA075957 420010910G34168800T ENCODER BELL 412 412 1182202SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 GPS DISPLAYS EXTERNAL ALTIMETER LOST COMMUNICATIONS MESSAGE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011002001142001100200114SW 2001 10 2 HEEA075958 120010910G7740DPUA0101 COMPUTER BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E K NONE O OTHER ININSP/MAINT 1 SW0341791 51465 INTELLISTART LIGHT STAYS ON, COULDN'T ACCESS WITH MLP. SENT TO ALTAIR AVIONICS CORP. FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20011002001152001100200115SW 2001 10 2 HEEA075959 120010910G6520PHI2062003 SEAL BELL 206 206L3 1182108SW T/R GEARBOX LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW0330KH 51527 SEAL LEAKING. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011002001172001100200117 2001 10 2 HEEA075960 420010910G3400212075399101 INDICATOR BELL 212 212 1181420SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 WILL NOT REFLECT AN INDICATION. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT. 1G71 4U H4SW 20011002001182001100200118SW 2001 10 2 HEEA075961 120010910G5302206031329103S ATTACH FITTING BELL 206 206L3 1182108SW TAILBOOM MISMANUFACTURED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 FITTING WILL NOT SIT FLAT AGAINST TAILBOOM RING. FITTING IS NOT MACHINED FLAT AND HAS A SLIGHTLY ROUNDED CONTOUR SO THERE IS A GAP AROUND THE PERIMETER OF THE FACE OF THE FITTING. ALSO FOUND FITTING TO BE APPROXIMATELY .30 THICKER AT THE TAILBOOM ATTACH BOLT HOLE. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT. 1G71 3U H2SW 20011003000092001100300009SW 2001 10 3 HEEA075971 120010913G5302407030801105 SKIN BELL 407 407 SW TAILBOOM CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034999 2516 53323 CRACK IN SKIN ON LEFT HAND SIDE. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#720464. 1G71 3U O H2SW 20011003000102001100300010SW 2001 10 3 HEEA075972 120010913G6210407015001117 BLADE BELL 407 407 SW MAIN ROTOR DELAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH3683 53207 DELAMINATION NEAR BLADE TIP. 1G71 3U O H2SW 20011003000112001100300011SW 2001 10 3 HEEA075974 120010913G6230406010401117 SWASHPLATE BELL 407 407 SW MAIN ROTOR LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH1368 53327 GREASE DISCOLORED AND LEAKING. 1G71 3U O H2SW 20011003000122001100300012SW 2001 10 3 HEEA075975 120010913G3246407050202101 CROSSTUBE BELL 407 407 SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH 53059 CORROSION AT CHAFE PADS. SENT IN FOR EVALUATION DUE TO PREVIOUS MANUFACTURE DEFECTS. 1G71 3U O H2SW 20011003000162001100300016SW 2001 10 3 HEEA075977 120010913G2700412301300101 ACTUATOR BELL 412 412EP 1182205SW FLIGHT CONTROLS STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW036106C 36257 STICKING INTERMITTENTLY IN FLIGHT. 1G72 4U H4SW 20011003000172001100300017SW 2001 10 3 HEEA075978 120010914G6710406310404101 ROD END BELL 407 407 SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH3352 53188 ROD END WORN. 1G71 3U O H2SW 20011003000182001100300018SW 2001 10 3 HEEA075980 120010914G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH923 53283 UNIVERSAL WORN. 1G71 3U O H2SW 20011003000192001100300019SW 2001 10 3 HEEA075981 120010914G6310214040814105 SLEEVE BELL 407 407 SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 WORN. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#720445. 1G71 3U O H2SW 20011003000222001100300022SW 2001 10 3 HEEA075987 120010914G6510407340340103 DISC PACK BELL 407 407 SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 DISC PACK CRACKED. 1G71 3U O H2SW 20011003000232001100300023SW 2001 10 3 HEEA075988 120010914G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH1442 53277 WORN BEYOND LIMITS. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#71908903. 1G71 3U O H2SW 20011003000252001100300025SW 2001 10 3 HEEA075989 120010914G2840407362005103 SWITCH BELL 407 407 SW FUEL INDICATOR FAILED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03498PH 53399 LOW LEVEL ANNUNCIATOR LIGHT WOULD NOT GO OUT. 1G71 3U O H2SW 20011003000422001100300042SW 2001 10 3 HEEA075990 120010914G6510406001704101 BELLCRANK BELL 407 407 SW TAIL ROTOR CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 CHAFED FROM CONTROL TUBE. 1G71 3U O H2SW 20011003000532001100300053SW 2001 10 3 HEEA075993 120010914G2910 FITTING BELL 407 407 SW HYD HOSE BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 FITTING BROKE OFF IN HOSE END, CANNOT REMOVE. 1G71 3U O H2SW 20011003000542001100300054SW 2001 10 3 HEEA075994 120010914G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH767 53198 WEAR BEYOND ALLOWABLE LIMITS. 1G71 3U O H2SW 20011003000552001100300055SW 2001 10 3 HEEA075995 120010914G2910 B-NUT BELL 407 407 SW HYD SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03740PH729 53435 B NUT THREADS ARE UNDERCUT AND WILL NOT TIGHTEN. 1G71 3U O H2SW 20011003000562001100300056SW 2001 10 3 HEEA075996 120010914G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH2509 53147 WORN BEARING. 1G71 3U O H2SW 20011003000572001100300057SW 2001 10 3 HEEA075997 120010914G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 WORN BEARING. 1G71 3U O H2SW 20011003000592001100300059SW 2001 10 3 HEEA075998 120010914G6710406010425107 LEVER BELL 407 407 SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH1848 53396 WORN BUSHINGS. 1G71 3U O H2SW 20011003000602001100300060SW 2001 10 3 HEEA075999 120010914G6710406010425107 LEVER BELL 407 407 SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH1848 53396 WORN BUSHINGS. 1G71 3U O H2SW 20011003000612001100300061SW 2001 10 3 HEEA076000 120010914G5320407070620125 PANEL BELL 407 407 SW COLLECTIVE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 PANEL CRACKED. 1G71 3U O H2SW 20011003000622001100300062SW 2001 10 3 HEEA076001 120010914G6710406310405101 UNIVERSAL JOINT BELL 407 407 SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH1139 53397 BEARING UNSTAKED. 1G71 3U O H2SW 20011003000632001100300063SW 2001 10 3 HEEA076006 120010914G6510407340340103 DISC PACK BELL 407 407 SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 CRACKED. SCRAPPED IN HOUSE. 1G71 3U O H2SW 20011003000702001100300070SW 2001 10 3 HEEA076007 120010914G6510407340340101 DISC PACK BELL 407 407 SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 CRACKED. SCRAPPED IN HOUSE. 1G71 3U O H2SW 20011003000732001100300073SW 2001 10 3 HEEA076008 120010914G6510407340340101 DISC PACK BELL 407 407 SW TAIL ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03722PH 53288 CRACKED. SCRAPPED IN HOUSE. 1G71 3U O H2SW 20011003000742001100300074SW 2001 10 3 HEEA076009 120010914G6310204040760109 FILTER ELEMENT BELL 407 407 SW TRANSMISSION FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 RUN IN AFTER TRANS CHANGE. SCRAPPED IN HOUSE. 1G71 3U O H2SW 20011003000762001100300076SW 2001 10 3 HEEA076012 120010914G717070031A202000 LINE BELL 407 407 SW EXH DRAIN CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 DRAIN LINE WAS WORN THROUGH STEEL BRAIDING. SCRAPPED IN HOUSE. 1G71 3U O H2SW 20011003000782001100300078SW 2001 10 3 HEEA076016 120010917G6710214001347005 ACTUATOR BELL 214 214ST 1182106SW AUTOFLIGHT SYS STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 ROTARY ACTUATOR STICKING. 2G72 4U H10SW 20011003000792001100300079SW 2001 10 3 HEEA076017 120010917G5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP FROZEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 ACTUATOR MOTOR FROZEN. 1G72 4U H4SW 20011003000812001100300081SW 2001 10 3 HEEA076018 120010917G2840473203003 SIGNAL COND UNIT BELL 412 412 1182202SW FUEL SYSTEM OUT OF ADJ E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 COULD NOT ADJUST E TO -.03PF WHEN CALIBRATING NR 1 FUEL SYSTEM. 1G72 4U H4SW 20011003000832001100300083SW 2001 10 3 HEEA076019 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW038045T233 28101 WEAK. WOULD NOT TAKE A CHARGE. 2G72 4U H10SW 20011003000842001100300084SW 2001 10 3 HEEA076020 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW038045T233 28101 WEAK. WOULD NOT TAKE A CHARGE. 2G72 4U H10SW 20011003000852001100300085SW 2001 10 3 HEEA076021 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359806487 28140 WEAK. 2G72 4U H10SW 20011003000862001100300086SW 2001 10 3 HEEA076022 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359806473 28140 WON'T START AIRCRAFT. 2G72 4U H10SW 20011003000872001100300087SW 2001 10 3 HEEA076023 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035748M465 28102 WEAK. 2G72 4U H10SW 20011003000892001100300089SW 2001 10 3 HEEA076024 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035748M465 28102 WEAK. 2G72 4U H10SW 20011003000902001100300090SW 2001 10 3 HEEA076025 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033897N902 28106 WEAK. 2G72 4U H10SW 20011003000922001100300092SW 2001 10 3 HEEA076026 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359806911 28140 WON'T START AIRCRAFT. 2G72 4U H10SW 20011003000942001100300094SW 2001 10 3 HEEA076027 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033897N380 28106 WEAK. 2G72 4U H10SW 20011003000952001100300095SW 2001 10 3 HEEA076028 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN SHORTED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033897N380 28106 WEAK. FOUND UNIT INTERNALLY SHORTED. 2G72 4U H10SW 20011003000972001100300097SW 2001 10 3 HEEA076029 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036957Y89 28139 WEAK. 2G72 4U H10SW 20011003000982001100300098SW 2001 10 3 HEEA076030 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036957Y89 28139 WEAK. 2G72 4U H10SW 20011003000992001100300099SW 2001 10 3 HEEA076031 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW038045T 28101 WEAK. 2G72 4U H10SW 20011003001002001100300100SW 2001 10 3 HEEA076032 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW038045T 28101 WEAK. 2G72 4U H10SW 20011003001012001100300101SW 2001 10 3 HEEA076033 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036957Y253 28139 WON'T HOLD A CHARGE. 2G72 4U H10SW 20011003001022001100300102SW 2001 10 3 HEEA076034 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359806742 28140 WON'T START AIRCRAFT. SCRAPPED. 2G72 4U H10SW 20011004000052001100400005SW 2001 10 4 HEEA076035 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033897N226 28106 WEAK. 2G72 4U H10SW 20011004000062001100400006SW 2001 10 4 HEEA076036 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359806372 28140 WEAK. 2G72 4U H10SW 20011004000072001100400007SW 2001 10 4 HEEA076037 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN OVERHEATED E HEEAK NONE ML OVER TEMP NO TEST ININSP/MAINT 1 SW035748M 28102 OVERHEAT AND ACID SMELL. REPLACED WITH SERVICEABE BATTERY. 2G72 4U H10SW 20011004000082001100400008SW 2001 10 4 HEEA076038 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN OVERHEATED E HEEAK NONE M OVER TEMP ININSP/MAINT 1 SW035748M 28102 OVERHEAT AND ACID SMELL. REPLACED WITH SERVICEABE BATTERY. 2G72 4U H10SW 20011004000092001100400009SW 2001 10 4 HEEA076039 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359805 28141 WON'T START AIRCRAFT. REPLACED WITH SERVICEABE BATTERY. 2G72 4U H10SW 20011004000102001100400010SW 2001 10 4 HEEA076040 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359805 28141 WON'T START AIRCRAFT. REPLACED WITH SERVICEABE BATTERY. 2G72 4U H10SW 20011004000112001100400011SW 2001 10 4 HEEA076041 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359806 28140 WEAK. REPLACED WITH SERVICEABE BATTERY. 2G72 4U H10SW 20011004000122001100400012SW 2001 10 4 HEEA076042 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359806 28140 WEAK. REPLACED WITH SERVICEABE BATTERY. 2G72 4U H10SW 20011004000132001100400013SW 2001 10 4 HEEA076043 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036957Y 28139 WON'T HOLD A CHARGE. REPLACED WITH SERVICEABE BATTERY. 2G72 4U H10SW 20011004000142001100400014SW 2001 10 4 HEEA076044 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW038045T 28101 WEAK. 2G72 4U H10SW 20011004000152001100400015SW 2001 10 4 HEEA076045 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359806 28140 WEAK. 2G72 4U H10SW 20011004000162001100400016SW 2001 10 4 HEEA076046 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359806 28140 WEAK. REPLACED WITH SERVICEABLE BATTERY. 2G72 4U H10SW 20011004000222001100400022SW 2001 10 4 HEEA076047 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359805461 28141 WON'T START AIRCRAFT. 2G72 4U H10SW 20011004000292001100400029SW 2001 10 4 HEEA076048 120010919G2432RG214 BATTERY BELL 214 214ST 1182106SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03 BATTERY DEAD. 2G72 4U H10SW 20011004000302001100400030SW 2001 10 4 HEEA076049 120010924G3212214031792102 COVER BELL 214 214ST 1182106SW MLG FLOAT MISSING E HEEAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SW038045T 28101 AFTER SHUTDOWN AT HELIPORT, FOUND AFT PORTION OF RIGHT HAND FLOAT COVER MISSING. REPLACED FLOAT COVER. 2G72 4U H10SW 20011004000312001100400031 2001 10 4 HEEA076050 420010924G2397M39012160004 CONNECTOR BELL 212 212 1181420SW NR 1 VHF RADIO SHORTED E HEEAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW03102PH 30899 PRIOR TO TAKEOFF, SMELLED ELECTRICAL "BURNING" ODOR. MAINTENANCE FOUND WIRING HARNESS FROM NR 1 VHF RADIO TO BULKHEAD FITTING SHORTED AT CANNON PLUG. 1G71 4U H4SW 20011004000382001100400038SW 2001 10 4 HEEA076051 120010924G63226038T59P02 BLOWER BELL 214 214ST 1182106SW SHAFT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T 28101 THE #1 PARTICLE SEPARATOR CAUTION LIGHT CAME ON. MAINTENANCE FOUND PARTICLE SEPARATOR BLOWER SHAFT SHEARED. 2G72 4U H10SW 20011004000512001100400051SW 2001 10 4 HEEA076054 120010924G6220407310101101 BEARING 407010100115BELL 407 407 SW MAIN ROTOR SEPARATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH A222 53003 SEPARATION. 1G71 3U O H2SW 20011004000542001100400054SW 2001 10 4 HEEA076056 120010924G7931222375077113 TRANSMITTER BELL 407 407 SW ENGINE OIL MALFUNCTIONED E HEEAO OTHER N FALSE WARNING ININSP/MAINT 1 SW03723PH 53283 ENGINE PRESSURE DROPPED TO ZERO. 1G71 3U O H2SW 20011004000562001100400056SW 2001 10 4 HEEA076058 120010928G7120206064107103 LEG ASSY BELL 206 206L3 1182108SW ENGINE MOUNT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 ROD END BEARING ON NEW LEG ASSEMBLY IS NEAR WEAR LIMITS. 1G71 3U H2SW 20011004000832001100400083SW 2001 10 4 HEEA076060 120010928G7120206064106101 LEG ASSY BELL 206 206L3 1182108SW ENGINE MOUNT MISMANUFACTURED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 PART DOES NOT FIT PHI INSPECTION FIXTURE WHICH WAS MANUFACTURED TO MATCH SEVERAL OF THESE PART NUMBERED LEG ASSEMBLIES. 1G71 3U H2SW 20011004000842001100400084EU 2001 10 4 HEEA076062 120010910G6230126891P BEARING SNIAS 350 AS350B 8680801EU MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03974AE 2653 WORN ROD END BEARINGS ON MAIN ROTOR PC LINKS. PENDING VENDOR RETURN. 1G71 3U H9EU 20011004000852001100400085EU 2001 10 4 HEEA076063 120010910G243230248001 BATTERY BOLKMS105 BO105S 5626006EU MAIN MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036607K S841 "BATT 60" LIGHT CAME ON WHEN ATTEMPTING ENGINE START. REPLACED WITH SERVICEABLE PART. 1G72 3U H3EU 20011004000862001100400086EU 2001 10 4 HEEA076064 120010910G6321350A32050002 BRAKE ASSY SNIAS 350 AS350B 8680801EU MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03972AE502 3234 WORN BRAKE LINING. PENDING VENDOR RETURN. 1G71 3U H9EU 20011004000872001100400087EU 2001 10 4 HEEA076066 120010910G6410355A09103601 BEARING 355A12005004SNIAS 350 AS350B 8680801EU TAIL ROTOR DELAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03971AE 7458 3230 LAMINANT SEPARATION AT THE END OF THE BEARINGS. PENDING VENDOR RETURN. 1G71 3U H9EU 20011004000882001100400088GL 2001 10 4 HEEA076067 220010910G74219550168770 IGNITER SNIAS 350 AS350B 8680801EU ALLSN 250C 250C* GL ENGINE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03856PH612 3352 LT IGNITER PLUG WORN. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H9EU E4CE 20011004000892001100400089EU 2001 10 4 HEEA076068 120010910G6230 BEARING SNIAS 350 AS350B 8680801EU MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03974AE 2653 WORN ROD END BEARINGS ON MAIN ROTOR PC LINKS. PENDING VENDOR RETURN. 1G71 3U H9EU 20011022001102001102200110GL 2001 10 22 HEEA076247 220011002G723023064570 LINER BELL 407 407 1182206SW ALLSN 250B 250B* GL COMPRESSOR CHAFED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 RUMBLING NOISE AROUND 30 PERCENT N1 DURING START. SENT TO STANDARD AERO FOR EXCHANGE. 1G71 3U3 TO H2SW E10CE 20011022001122001102200112GL 2001 10 22 HEEA076248 220011002G741223064130 IGNITER BELL 407 407 1182206SW ALLSN 250B 250B* GL ENGINE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03741PH 53457 IGNITOR BOX INOPERATIVE. 1G71 3U3 TO H2SW E10CE 20011022001152001102200115NE 2001 10 22 HEEA076249 220011003G73200292928650 VALVE SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1D NE FUEL METERING MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03971AE936 3230 22072 NG AND TORQUE FLUCTUATIONS. PENDING VENDOR RETURN. 1G71 3U3 U H9EU E19EU 20011023000032001102300003EU 2001 10 23 HEEA076250 120011003G71970301037070 HARNESS SNIAS 350 AS350B 8680801EU ENGINE ERRATIC E HEEAK NONE O OTHER ININSP/MAINT 1 SW03856PH703 3352 T-4 ERRATIC. PENDING VENDOR RETURN. 1G71 3U H9EU 20011023000042001102300004 2001 10 23 HEEA076251 420011004G83003024780 GEARBOX BELL 412 412 1182202SW RGB MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 RGB SECTION MAKING METAL CHIPS IN FILTER AND CHIP PLUG. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011023000052001102300005NE 2001 10 23 HEEA076252 120011004G7714 BUTTON SKRSKYS76 S76A 8143006NE N1 INDICATOR MISSING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 TACHO CHECK BUTTON MISSING. PENDING VENDOR REPAIR. 1G72 3U H1NE 20011023000062001102300006NE 2001 10 23 HEEA076253 120011004G32127625101102101 FLOAT SKRSKYS76 S76A 8143006NE MLG WILL NOT TEST E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03911MJ 760231 FAILED INFLATION TEST. PENDING VENDOR REPAIR. 1G72 3U H1NE 20011023000072001102300007 2001 10 23 HEEA076254 420011004G22157690001802106 ACTUATOR SKRSKYS76 S76A 8143006NE AFCS CHATTERING E HEEAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 SW03760PH 760078 CHATTERING INDUCING PORPOISE IN AIRCRAFT. PENDING VENDOR REPAIR. 1G72 3U H1NE 20011023000082001102300008EA 2001 10 23 HEEA076255 220011009G7200 ENGINE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA NACELLE MALFUNCTIONED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03102PH 30899 HIGH OIL CONSUMPTION. SENT TO PRATT AND WHITNEY FOR WARRANTY REPAIR. 1G71 4U4 U H4SW E22EA 20011023000092001102300009EA 2001 10 23 HEEA076256 220011009G7200 ENGINE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA NACELLE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031079U16590 31122 CORROSION AT 12 OCLOCK. SENT TO PRATT AND WHITNEY FOR INSPECTION AND REPAIR. 1G71 4U4 U H4SW E22EA 20011023000102001102300010EA 2001 10 23 HEEA076257 220011009G7200 ENGINE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA NACELLE STALLED E HEEAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW035736D9772 31135 COMPRESSOR STALLS AND HIGH ITT. SENT TO PRATT AND WHITNEY FOR INSPECTION AND REPAIR. 1G71 4U4 U H4SW E22EA 20011023000112001102300011NE 2001 10 23 HEEA076258 220011009G7200 ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NACELLE STALLED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW033893N20429 33010 COMPRESSOR STALLS ABOVE 85 PERCENT N1 AND OVERTEMP (PEGGED OUT GAUGE). SENT TO PRATT AND WHITNEY FOR INSPECTION AND REPAIR. 1G72 4U4 U H4SW E22EA 20011023000122001102300012EA 2001 10 23 HEEA076259 220011009G7200 ENGINE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA NACELLE MALFUNCTIONED E HEEAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SW035009N6539 30936 LOW POWER. SENT TO PRATT AND WHITNEY FOR INSPECTION AND REPAIR. 1G71 4U4 U H4SW E22EA 20011023000132001102300013NE 2001 10 23 HEEA076260 220011009G7200 ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NACELLE OSCILLATES E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03223471620 36005 TORQUE OSCILLATIONS. SENT TO PRATT AND WHITNEY FOR INSPECTION AND REPAIR. 1G72 4U4 U H4SW E22EA 20011023000142001102300014EA 2001 10 23 HEEA076261 220011009G7200 ENGINE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA NACELLE HOT START E HEEAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW035736D7809 31135 HOT STARTS. SENT TO PRATT AND WHITNEY FOR INSPECTION AND REPAIR. 1G71 4U4 U H4SW E22EA 20011023000152001102300015NE 2001 10 23 HEEA076262 220011009G7200 ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NACELLE STALLED E HEEAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW03223475034 36005 COMPRESSOR STALLS AND ITT OVER 1000 DEGREES. SENT TO PRATT AND WHITNEY FOR INSPECTION AND REPAIR. 1G72 4U4 U H4SW E22EA 20011023000162001102300016NE 2001 10 23 HEEA076263 220011009G7200 ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NACELLE STALLED E HEEAO OTHER CJ F.O.D. WARNING INDICATION NRNOT REPORTED 1 SW037128R11662 36007 COMPRESSOR STALLS - FOD TO COMPRESSOR BLADES. SENT TO PRATT AND WHITNEY FOR OVERHAUL. 1G72 4U4 U H4SW E22EA 20011023000172001102300017SW 2001 10 23 HEEA076264 120011009G5412 FIREWALL BELL 412 412 1182202SW ENGINE BAY LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N15595 33002 AFT ENGINE FIRE WALL ATTACHMENT FLANGE RIVETS LOOSE. 1G72 4U H4SW 20011023000182001102300018NE 2001 10 23 HEEA076265 220011009G7200 ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE BAY OVERHEATED E HEEAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW032149S1691 36002 ITT WENT ABOVE 900 DEGREES DURING MANUAL GOVERNOR CHECK.. 1G72 4U4 U H4SW E22EA 20011023000192001102300019NE 2001 10 23 HEEA076266 220011009G7200 ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE BAY OVERHEATED E HEEAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW033893P15285 33012 HIGH N1 ON POWER CHECK. 1G72 4U4 U H4SW E22EA 20011023000202001102300020NE 2001 10 23 HEEA076267 220011009G7200 ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE BAY OVERHEATED E HEEAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW032298Z12293 33077 HIGH ITT AND WEAR ON GEARBOX CASE AND COVER. 1G72 4U4 U H4SW E22EA 20011023000212001102300021NE 2001 10 23 HEEA076268 220011009G7200 ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE BAY OVERSPEED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03223478022 36005 N1 OVERSPEED AT 116 PERCENT. 1G72 4U4 U H4SW E22EA 20011023000222001102300022EA 2001 10 23 HEEA076269 220011009G7200 BLADE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA ENG COMPRESSOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031082G16728 31109 COMPRESSOR BLADE CORRODED. 1G71 4U4 U H4SW E22EA 20011023000232001102300023NE 2001 10 23 HEEA076270 220011009G7200 COMPRESSOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE SEIZED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L6819 33006 COMPRESSOR SEIZED. 1G72 4U4 U H4SW E22EA 20011023000242001102300024NE 2001 10 23 HEEA076271 220011009G7297 ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE BAY MALFUNCTIONED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03800Y 7681 33134 ENGINE HAS HIGH T-5 HARNESS OHMS OUT LESS THAN 100 OHMS. 1G72 4U4 U H4SW E22EA 20011023000252001102300025NE 2001 10 23 HEEA076272 220011009G7200 ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE BAY OVERSPEED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW032234717028 36005 N1 OVERSPEED AT 116 PERCENT. REPLACED WITH SERVICEABLE ENGINE. 1G72 4U4 U H4SW E22EA 20011023000262001102300026GL 2001 10 23 HEEA076273 220011011G7323252469211 GOVERNOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE OSCILLATES E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035435V10875 760158 CAE890432S ENGINE N1, T5, TORQUE AND FUEL FLOW OSCILLATES AT HIGH POWER SETTINGS. REPLACED WITH SERVICEABLE PART. 1G72 3U3 U H1NE E1GL 20011023000272001102300027NE 2001 10 23 HEEA076274 120011011G632140004769R CALIPER SKRSKYS76 S76A 8143006NE ROTOR BRAKE LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03911MJ 760231 CALIPER LEAKING. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20011023000282001102300028NE 2001 10 23 HEEA076275 120011011G632140004769R CALIPER SKRSKYS76 S76A 8143006NE ROTOR BRAKE LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03911MJ 760231 CALIPER LEAKING. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20011023000292001102300029NE 2001 10 23 HEEA076276 120011011G21217650007901102 BLOWER SKRSKYS76 S76A 8143006NE VENT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033122H 760233 VENT BLOWER POPS CIRCUIT BREAKER. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20011023000302001102300030 2001 10 23 HEEA076277 420011012G3450258719342 COMPASS SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03760PH 760078 HIS OFF FLAG WILL NOT PULL. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20011023000312001102300031NE 2001 10 23 HEEA076278 120011012G63217665009803105 MODULE 350A33200406SKRSKYS76 S76A 8143006NE ROTOR BRAKE ASSYINTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW03760PH MA1154 760078 ROTOR BRAKE WARNING LIGHT INTERMITTENTLY DOES NOT ILLUMINATE WITH ROTOR BRAKE ENGAGED. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20011023000322001102300032NE 2001 10 23 HEEA076279 220011012G74219550166670 IGNITER SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1 60030NE ENGINE INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03760PH 760078 INOPERATIVE NO SPARK. REPLACED WITH SERVICEABLE PART. 1G72 3U3 U H1NE E19EU 20011023000332001102300033SW 2001 10 23 HEEA076280 120011001G3212407073848101 BOTTLE BELL 407 407 1182206SW FLOAT BAG DISCHARGED E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03491PH 53386 VALVE VENTING. COULD NOT SERVICE WITH NITROGEN. 1G71 3U O H2SW 20011023000342001102300034SW 2001 10 23 HEEA076281 120011001G3212407073848101 BOTTLE BELL 407 407 1182206SW FLOAT BAG DISCHARGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH 53386 VALVE VENTING. COULD NOT SERVICE WITH NITROGEN. 1G71 3U O H2SW 20011023000352001102300035SW 2001 10 23 HEEA076283 120011001G2435206062200113 STARTER GEN BELL 407 407 1182206SW ENGINE MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03495PH2628 53397 STARTING PROBLEMS. DEAD SPOT. 1G71 3U O H2SW 20011023000362001102300036SW 2001 10 23 HEEA076284 120011001G2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH622 Y0099 53207 WORN BRUSHES. 1G71 3U O H2SW 20011023000372001102300037SW 2001 10 23 HEEA076285 120011001G6420407012101111 HUB BELL 407 407 1182206SW TAIL ROTOR PEELING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03742PH248 53461 PAINT PEELING FROM BLADE. 1G71 3U O H2SW 20011023000382001102300038SW 2001 10 23 HEEA076286 120011001G79218538100 OIL COOLER BELL 412 412 1182202SW OIL SYSTEM MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 METAL IN OIL. 1G72 4U H4SW 20011023000392001102300039SW 2001 10 23 HEEA076287 120011001G79218538100 OIL COOLER BELL 412 412 1182202SW OIL SYSTEM LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW031202T 33112 LEAKING FROM CENTER SECTION. REPLACED WITH SERVICEABLE COOLER. 1G72 4U H4SW 20011023000402001102300040SW 2001 10 23 HEEA076288 120011001G79218538100 OIL COOLER BELL 412 412 1182202SW OIL SYSTEM MALFUNCTIONED E HEEAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW031202T 33112 HIGH TEMPERATURE READINGS ABOUT 100 DEGREES IN RED LINE. ALSO C-BOX CAUTION LIGHT CAME ON. REPLACED WITH SERVICEABLE COOLER. 1G72 4U H4SW 20011023000412001102300041SW 2001 10 23 HEEA076289 120011001G79218538100 OIL COOLER BELL 212 212 1181420SW OIL SYSTEM CONTAMINATED E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW033131S 30953 CONTAMINATED FROM MAST, ALSO LEAKS. 1G71 4U H4SW 20011023000422001102300042SW 2001 10 23 HEEA076290 120011001G79218538100 OIL COOLER BELL 412 412 1182202SW OIL SYSTEM CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 METAL CONTAMINATED. 1G72 4U H4SW 20011023000432001102300043SW 2001 10 23 HEEA076291 120011001G6320 TRANSMISSION BELL 412 412 1182202SW MAIN ROTOR MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03800Y 33134 TRANSMISSION MAKING METAL. SENT TO DRAKE AIR FOR INSPECTION AND REPAIR. 1G72 4U H4SW 20011023000442001102300044SW 2001 10 23 HEEA076292 120011001G6310 COMBINING BOX BELL 412 412 1182202SW TRANSMISSION MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03800Y 33134 C-BOX MAKING METAL. 1G72 4U H4SW 20011023000452001102300045SW 2001 10 23 HEEA076293 120011001G79218538100 OIL COOLER BELL 412 412 1182202SW OIL SYSTEM LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW032258F 33073 OIL COOLER LEAKS. 1G72 4U H4SW 20011023000462001102300046SW 2001 10 23 HEEA076294 120011001G79218538100 OIL COOLER BELL 212 212 1181420SW OIL SYSTEM CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035736J 31140 METAL CONTAMINATION. 1G71 4U H4SW 20011023000522001102300052SW 2001 10 23 HEEA076295 120011001G6310 COMBINING BOX BELL 412 412 1182202SW TRANSMISSION MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 C-BOX MAKING METAL. 1G72 4U H4SW 20011023000642001102300064SW 2001 10 23 HEEA076296 120011001G63008538100 OIL COOLER BELL 412 412 1182202SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW031202T 33112 OIL COOLER LEAKING FROM CENTER CORE. 1G72 4U H4SW 20011023000712001102300071SW 2001 10 23 HEEA076298 120011001G63008538100 OIL COOLER BELL 412 412 1182202SW MAIN ROTOR CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0333008 36004 METAL CONTAMINATION. 1G72 4U H4SW 20011023001312001102300131SW 2001 10 23 HEEA076299 120011001G63008538100 OIL COOLER BELL 212 212 1181420SW MAIN ROTOR CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035736D 31135 OIL COOLER HAS METAL CONTAMINATION. 1G71 4U H4SW 20011023001322001102300132SW 2001 10 23 HEEA076300 120011001G63008538100 OIL COOLER BELL 412 412 1182202SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03 OIL COOER LEAKING OIL. 1G72 4U H4SW 20011023001332001102300133SW 2001 10 23 HEEA076301 120011001G63008538100 OIL COOLER BELL 412 412 1182202SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0322347 36005 OIL COOLER SEEPING. 1G72 4U H4SW 20011023001342001102300134SW 2001 10 23 HEEA076302 120011001G6320 TRANSMISSION BELL 212 212 1181420SW MAIN ROTOR MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035736D 31135 TRANSMISSION MAKING METAL. 1G71 4U H4SW 20011023001352001102300135SW 2001 10 23 HEEA076303 120011002G2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH1566 2109 53277 BRUSHES WORN. 1G71 3U O H2SW 20011023001362001102300136SW 2001 10 23 HEEA076307 120011002G6500206061432121 HOUSING BELL 407 407 1182206SW COOLER BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03447PH 53114 BLOWER HOUSING CRACKED. 1G71 3U O H2SW 20011023001392001102300139SW 2001 10 23 HEEA076308 120011002G6500206061432121 HOUSING BELL 407 407 1182206SW COOLER BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH 53398 TAIL ROTOR COOLER BLOWER HOUSING IS CRACKED. 1G71 3U O H2SW 20011023001402001102300140SW 2001 10 23 HEEA076309 120011002G6500206061432121 HOUSING BELL 407 407 1182206SW COOLER BLOWER DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038595X 53267 TAIL ROTOR COOLER BLOWER HOUSING HAS WORKING RIVETS. 1G71 3U O H2SW 20011023001422001102300142SW 2001 10 23 HEEA076310 120011002G2821206061634003 VALVE BELL 407 407 1182206SW FUEL FILTER LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03406PH 53198 EXTERNAL FUEL FILTER DRAIN VALVE LEAKING AROUND HANDLE WHEN DRAINING FUEL. 1G71 3U O H2SW 20011023001462001102300146SW 2001 10 23 HEEA076311 120011002G2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03501PH 95189 53401 300 HOUR SCHEDULE CHANGE. WORN BRUSHES. 1G71 3U O H2SW 20011023001482001102300148SW 2001 10 23 HEEA076312 120011002G2435206062200113 STARTER GEN BELL 407 407 1182206SW ENGINE FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW038595X1808 53267 STARTER GENERATOR WOULD NOT CRANK ENGINE ON LAST START OF THE DAY. 1G71 3U O H2SW 20011023001492001102300149SW 2001 10 23 HEEA076313 120011002G2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH2203 98136 53378 STARTER GEN HAS WORN BRUSHES. 1G71 3U O H2SW 20011023001672001102300167SW 2001 10 23 HEEA076314 120011002G2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH1607 99100 53398 STARTER GEN HAS WORN BRUSHES. 1G71 3U O H2SW 20011023001682001102300168SW 2001 10 23 HEEA076317 120011002G5347206072215102 SUPPORT BELL 407 407 1182206SW CABIN BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03722PH 53288 FOUND SEAT SUPPORT BROKEN IN TWO. 1G71 3U O H2SW 20011023001692001102300169SW 2001 10 23 HEEA076318 120011002G6321 HOUSING BELL 407 407 1182206SW ROTOR BRAKE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH1701 53398 REMOVED FOR MODIFICATION. FOUND EXCESSIVE WEAR ON HOUSING, BRAKE PAD BOLT RETAINER HOLES AND PAD RETAINER BOLTS. 1G71 3U O H2SW 20011023001702001102300170SW 2001 10 23 HEEA076319 120011002G3212212073905001 GAUGE BELL 407 407 1182206SW FLOAT PRESSURE CONTAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH 53059 UNREADABLE DUE TO MOISTURE IN GLASS. 1G71 3U O H2SW 20011023001712001102300171SW 2001 10 23 HEEA076320 120011002G3212212073905001 GAUGE BELL 407 407 1182206SW FLOAT PRESSURE CONTAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH 53277 WATER IN GAUGE. 1G71 3U O H2SW 20011023001752001102300175SW 2001 10 23 HEEA076321 120011002G2510222320823130 SEAT BELT BELL 407 407 1182206SW COCKPIT FRAYED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 SEAT BELT FRAYED. 1G71 3U O H2SW 20011023001762001102300176SW 2001 10 23 HEEA076322 120011002G2844222375077115 TRANSDUCER BELL 407 407 1182206SW FUEL SYSTEM READS LOW E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03467PH3307 53142 PRESSURE READS LOW. 1G71 3U O H2SW 20011023001772001102300177SW 2001 10 23 HEEA076323 120011002G7714222375077119 TRANSMITTER BELL 407 407 1182206SW ENGINE TORQUE MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03405PH3728 53207 FADEC DEGRADE LIGHT. 1G71 3U O H2SW 20011023001782001102300178GL 2001 10 23 HEEA076324 220011002G753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03496PH 53398 HIGH MGT. REPLACED WITH SERVICEABLE BLEED VALVE. 1G71 3U3 UO H2SW E1GL 20011023001792001102300179GL 2001 10 23 HEEA076325 220011002G729723065805 HARNESS BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03405PH 53207 FADEC DEGRADE LIGHT ILLUMINATED ON SHUTDOWN. 1G71 3U3 UO H2SW E1GL 20011023001802001102300180GL 2001 10 23 HEEA076326 220011002G729723065805 HARNESS BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03405PH 53207 CONSTANT FADEC DEGRADE LIGHT. TO BE SENT TO VENDOR FOR CREDIT. 1G71 3U3 UO H2SW E1GL 20011023001812001102300181GL 2001 10 23 HEEA076327 220011002G729723065805 HARNESS BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03496PH 53398 FADEC DEGRADE LIGHT. TO BE SENT TO VENDOR FOR CREDIT. 1G71 3U3 UO H2SW E1GL 20011023001822001102300182GL 2001 10 23 HEEA076328 220011002G729723065805 HARNESS BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03405PH 53207 SHORT BETWEEN PIN D & C OF TORQUE TRANSMITTER CONNECTOR. TO BE SENT TO VENDOR FOR CREDIT. 1G71 3U3 UO H2SW E1GL 20011023001832001102300183SW 2001 10 23 HEEA076329 120011002G770023071644 ECU BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03490PH 53378 CONTINUES TO HAVE NPOS & OS FAULTS. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U3 UO H2SW E1GL 20011023001842001102300184SW 2001 10 23 HEEA076330 120011002G243231908001 BATTERY BELL 407 407 1182206SW MAIN WEAK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03501PH 53401 BATTERY WEAK. 1G71 3U O H2SW 20011023001852001102300185SW 2001 10 23 HEEA076331 120011002G3201400052007109 BEAM BELL 407 407 1182206SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0357416 53070 BEAM ASSY CORRODED AND BOLT HOLE WORN. 1G71 3U O H2SW 20011023001862001102300186SW 2001 10 23 HEEA076332 120011002G3201400052007115 BEAM BELL 407 407 1182206SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH 53059 BEAM CORRODED AROUND BUSHINGS. IN SHEETMETAL SHOP FOR REPAIR. 1G71 3U O H2SW 20011023001872001102300187SW 2001 10 23 HEEA076333 120011002G3201400052009101 BOLT BELL 407 407 1182206SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH 53059 PITTED THROUGH COATING. SCRAPPED AND REPLACED WITH SERVICEABLE BOLT. 1G71 3U O H2SW 20011023001882001102300188SW 2001 10 23 HEEA076334 120011002G6720406012129101 LINK BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 ROD END BEARINGS WORN. 1G71 3U O H2SW 20011023001892001102300189SW 2001 10 23 HEEA076335 120011002G6310 BEARING 406040500119BELL 407 407 1182206SW SUPPORT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038595X A1505 53267 ROLLER FELL OUT OF BEARING. 1G71 3U O H2SW 20011023001902001102300190SW 2001 10 23 HEEA076336 120011002G6310 SEAL 406040500123BELL 407 407 1182206SW FREEWHEEL UNIT LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH A4015 53199 FRONT SEAL LEAKING. 1G71 3U O H2SW 20011023001912001102300191SW 2001 10 23 HEEA076337 120011002G6310 SEAL 406040500127BELL 407 407 1182206SW FREEWHEEL UNIT LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03407PH A3753 53003 FRONT SEAL LEAKING. 1G71 3U O H2SW 20011023001932001102300193SW 2001 10 23 HEEA076338 120011002G6710406310404101 ROD END BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03404PH3368 53188 ROD END ASSY WORN. 1G71 3U O H2SW 20011023002002001102300200SW 2001 10 23 HEEA076339 120011002G6710406310405101 UNIVERSAL JOINT BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH1498 53199 MAIN ROTOR UNIVERSAL WORN. 1G71 3U O H2SW 20011023002022001102300202SW 2001 10 23 HEEA076340 120011002G6710406310405101 UNIVERSAL JOINT BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03408PH1817 53228 BEARINGS WORN. 1G71 3U O H2SW 20011023002032001102300203SW 2001 10 23 HEEA076341 120011002G6710406310405101 UNIVERSAL JOINT BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH 53378 WORN. 1G71 3U O H2SW 20011023002042001102300204SW 2001 10 23 HEEA076342 120011002G6710406310405101 UNIVERSAL JOINT BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03408PH 53228 UNIVERSAL WORN. 1G71 3U O H2SW 20011023002062001102300206SW 2001 10 23 HEEA076343 120011002G6720406312103101 LINK BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 WORN BEARING. 1G71 3U O H2SW 20011023002092001102300209SW 2001 10 23 HEEA076344 120011002G6720406312103101 LINK BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 WORN BEARING. 1G71 3U O H2SW 20011023002112001102300211SW 2001 10 23 HEEA076345 120011002G6710407001523101 IDLER ASSY BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 MAIN ROTOR CONTROL IDLER ASSY HAS WORN BEARINGS. 1G71 3U O H2SW 20011023002142001102300214SW 2001 10 23 HEEA076348 120011002G6420407012101111 HUB BELL 407 407 1182206SW TAIL ROTOR NOISY E HEEAK NONE O OTHER ININSP/MAINT 1 SW03721PH4756 53278 CLICKING NOISE. 1G71 3U O H2SW 20011023002162001102300216SW 2001 10 23 HEEA076349 120011002G6420 BEARING BELL 407 407 1182206SW T/R TRUNNION NOISY E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH2540 53199 CLICKING NOISE COMING FROM TRUNNION BEARING. 1G71 3U O H2SW 20011023002172001102300217SW 2001 10 23 HEEA076350 120011002G6420407012101111 HUB BELL 407 407 1182206SW TAIL ROTOR NOISY E HEEAK NONE O OTHER ININSP/MAINT 1 SW03722PH1468 53288 CLICKING NOISE WHEN PUSHED TO STOPS. 1G71 3U O H2SW 20011023002192001102300219SW 2001 10 23 HEEA076351 120011002G6300407340339103 BEARING 407040302101BELL 407 407 1182206SW T/R DRIVESHAFT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH A926 53142 WORN ON INNER DIAMETER. 1G71 3U O H2SW 20011023002212001102300221SW 2001 10 23 HEEA076352 120011002G7810407062021101 DUCT BELL 407 407 1182206SW EXHAUST CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03720PH 53277 EXHAUST DUCT CRACKED. 1G71 3U O H2SW 20011024000012001102400001SW 2001 10 24 HEEA076353 120011003G6420 BEARING BELL 407 407 1182206SW T/R TRUNNION NOISY E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH2803 53199 T/R TRUNNION BEARING CLICKS WHEN FLAPPED. 1G71 3U O H2SW 20011024000022001102400002SW 2001 10 24 HEEA076354 120011003G6410 BLADE BELL 407 407 1182206SW TAIL ROTOR FLAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03722PH251 53288 PAINT FLAKING OFF BLADES. 1G71 3U O H2SW 20011024000032001102400003SW 2001 10 24 HEEA076355 120011003G3212212073905001 GAUGE 407073848101BELL 407 407 1182206SW FLOAT BOTTLE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH 242 53397 NEEDLE STICKING AND FACE CRACKED. TO BE RETURNED TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. 1G71 3U O H2SW 20011024000042001102400004SW 2001 10 24 HEEA076356 120011003G6500407340340101 DISC PACK BELL 407 407 1182206SW TAIL ROTOR DRIVECRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03408PH 53228 NR 3 SHORT SHAFT FWD COUPLING DISK PACK FOUND CRACKED. 1G71 3U O H2SW 20011024000052001102400005SW 2001 10 24 HEEA076357 120011003G6500407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR DRIVECRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 FWD COUPLING DISC ON NR 4 T/R SEGMENTED DRIVE SHAFT CRACKED. 1G71 3U O H2SW 20011024000062001102400006SW 2001 10 24 HEEA076358 120011003G6500407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR DRIVECRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 CRACKED. TO BE RETURNED TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. 1G71 3U O H2SW 20011024000072001102400007SW 2001 10 24 HEEA076359 120011003G3212407350300101 FLOAT BELL 407 407 1182206SW MLG TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 FLOAT BAG TORN. 1G71 3U O H2SW 20011024000082001102400008SW 2001 10 24 HEEA076360 120011003G3212407350302101 FLOAT BELL 407 407 1182206SW MLG LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 FLOAT BAG LEAKING. 1G71 3U O H2SW 20011024000092001102400009SW 2001 10 24 HEEA076361 120011003G2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL CELL MALFUNCTIONED E HEEAO OTHER N FALSE WARNING ININSP/MAINT 1 SW03417PH4129 53038 TRANSFER LIGHT WILL NOT GO OUT. 1G71 3U O H2SW 20011024000102001102400010SW 2001 10 24 HEEA076362 120011003G2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL CELL STUCK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03495PH 53397 PRESSURE SWITCH STUCK IN OFF POSITION. 1G71 3U O H2SW 20011024000112001102400011SW 2001 10 24 HEEA076363 120011003G7712407375003107 INDICATOR BELL 407 407 1182206SW COCKPIT INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW034999 2556 53323 TORQUE INDICATOR LIGHT INOPERATIVE. 1G71 3U O H2SW 20011024000122001102400012SW 2001 10 24 HEEA076364 120011003G7714407375008101 TACHOMETER BELL 407 407 1182206SW COCKPIT WILL NOT TEST E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03405PH3728 53207 ROTOR NEEDLE FAILS BIT TEST. 1G71 3U O H2SW 20011024000132001102400013SW 2001 10 24 HEEA076365 120011003G321070079H000Y150 HOSE BELL 407 407 1182206SW MLG KINKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 HOSE ASSY KINKED. 1G71 3U O H2SW 20011024000142001102400014SW 2001 10 24 HEEA076366 120011003G32128226003 FUSEABLE PLUG BELL 407 407 1182206SW FLOAT BOTTLE LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 LT FLOAT BOTTLE LEAKING AT CENTER OF FUSIBLE PLUG. 1G71 3U O H2SW 20011024000152001102400015SW 2001 10 24 HEEA076367 120011003G32128226003 FUSEABLE PLUG BELL 407 407 1182206SW FLOAT BOTTLE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03722PH 53288 FUSIBLE PLUG FAILED RELEASING ALL PRESSURE FROM FLOAT BOTTLE. 1G71 3U O H2SW 20011024000162001102400016SW 2001 10 24 HEEA076371 120011003G6300 SPLINE ADAPTER PHIPBH40701 BELL 407 407 1182206SW COOLER BLOWER WORN E K NONE O OTHER ININSP/MAINT 1 SW03406PH PHI0010 53198 WORN SPLINES. 1G71 3U O H2SW 20011024000172001102400017SW 2001 10 24 HEEA076372 120011003G6300407340339101 BEARING PHIPBH40701 BELL 407 407 1182206SW COOLER BLOWER OVERHEATED E HEEAK NONE M OVER TEMP ININSP/MAINT 1 SW03407PH PHI0013 53003 OIL COOLER BLOWER BEARING OVERHEATED. 1G71 3U O H2SW 20011024000182001102400018SW 2001 10 24 HEEA076375 120011003G6300407340339103 BEARING PHIPBH40701 BELL 407 407 1182206SW COOLER BLOWER ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03409PH PHI0019 53059 BEARING ROUGH. 1G71 3U O H2SW 20011024000192001102400019SW 2001 10 24 HEEA076376 120011003G6300 BEARING PHIPBH40701 BELL 407 407 1182206SW COOLER BLOWER ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW0357416 PHI0022 53070 WORN AND ROUGH BEARINGS. 1G71 3U O H2SW 20011024000202001102400020SW 2001 10 24 HEEA076378 120011003G6300407340339103 BEARING PHIPBH40701 BELL 407 407 1182206SW COOLER BLOWER WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03447PH PHI0031 53114 COOLER BLOWER BEARING IS WORN. 1G71 3U O H2SW 20011024000212001102400021SW 2001 10 24 HEEA076383 120011003G6520PHI407112 BOOT BELL 407 407 1182206SW TAIL ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03405PH 53207 BOOT SEAL LEAKING. 1G71 3U O H2SW 20011024000222001102400022SW 2001 10 24 HEEA076384 120011003G6520PHI407112 BOOT BELL 407 407 1182206SW TAIL ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03409PH 53059 BOOT SEAL LEAKING. 1G71 3U O H2SW 20011024000232001102400023SW 2001 10 24 HEEA076385 120011003G6720 BUSHING PHI407112 BELL 407 407 1182206SW IDLER WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 WEAR ON BUSHINGS. 1G71 3U O H2SW 20011024000242001102400024SW 2001 10 24 HEEA076386 120011003G28221C2710 CARTRIDGE BELL 407 407 1182206SW BOOST PUMP INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 INOPERATIVE. REPLACED WITH SERVICEABLE BOOST PUMP CARTRIDGE. 1G71 3U O H2SW 20011024000252001102400025SW 2001 10 24 HEEA076387 120011003G2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH 2239 53378 STARTER GEN BRUSHES FAILED INSPECTION. 1G71 3U O H2SW 20011024000262001102400026GL 2001 10 24 HEEA076388 220011003G732023007827 VALVE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 VALVE STICKING. REPLACED WITH SERVICEABLE VALVE. 1G71 3U3 UO H2SW E1GL 20011024000272001102400027SW 2001 10 24 HEEA076389 120011003G6300406310405101 BEARING BELL 407 407 1182206SW UNIVERSAL WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 WORN BEARING. 1G71 3U O H2SW 20011024000282001102400028SW 2001 10 24 HEEA076390 120011003G6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 WORN BEARING. 1G71 3U O H2SW 20011024000292001102400029SW 2001 10 24 HEEA076391 120011003G6230406310411101 BOOT BELL 407 407 1182206SW MAIN ROTOR TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03447PH 53114 BOOT TORN. 1G71 3U O H2SW 20011024000302001102400030SW 2001 10 24 HEEA076392 120011003G6720406312103101 LINK BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 WORN BEARINGS. 1G71 3U O H2SW 20011024000312001102400031SW 2001 10 24 HEEA076394 120011003G6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03406PH3924 53198 MAIN ROTOR BLADE IS CRACKED. 1G71 3U O H2SW 20011024000322001102400032SW 2001 10 24 HEEA076395 120011003G6510407340339101 BEARING 407040302107BELL 407 407 1182206SW T/R DRIVESHAFT ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH A1937 53386 TAIL ROTOR DRIVESHAFT BEARING ROUGH. 1G71 3U O H2SW 20011024000342001102400034SW 2001 10 24 HEEA076396 120011003G7120 BEARING BELL 407 407 1182206SW BIPOD MOUNT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 BIPOD MOUNT HAS A WORN BEARING. 1G71 3U O H2SW 20011024000352001102400035SW 2001 10 24 HEEA076397 120011003G7120 BEARING BELL 407 407 1182206SW BIPOD MOUNT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 WORN BEARING. 1G71 3U O H2SW 20011024000362001102400036SW 2001 10 24 HEEA076398 120011003G6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034999 53323 TAIL ROTOR DISC PACK IS CRACKED. 1G71 3U O H2SW 20011024000372001102400037SW 2001 10 24 HEEA076399 120011003G7933407375005101 INDICATOR BELL 407 407 1182206SW XMSN OIL TEMP MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03492PH 53390 TRANSMISSION OIL TEMP INDICATOR SHOWED ONLY 2 BAR SEGMENTS. 1G71 3U O H2SW 20011024000382001102400038 2001 10 24 HEEA076400 420011003G342150400179015 ADI BELL 407 407 1182206SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03406PH 53198 FLAG DOES NOT PULL AND GAUGE DOES NOT CORRESPOND TO ATTITUDE. REPLACED WITH SERVICEABLE ATTITUDE IND. 1G71 3U O H2SW 20011024000392001102400039 2001 10 24 HEEA076401 420011003G342150400179015 ADI BELL 407 407 1182206SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03406PH 53198 ATTITUDE INDICATOR STAYS IN LEFT TURN. REPLACED WITH SERVICEABLE ATTITUDE IND. 1G71 3U O H2SW 20011024000402001102400040SW 2001 10 24 HEEA076403 120011003G6300 BEARING PHIPBH40701FBELL 407 407 1182206SW COOLER BLOWER ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH PHI0015 53386 OIL COOLER BLOWER HAS ROUGH BEARINGS. 1G71 3U O H2SW 20011024000412001102400041SW 2001 10 24 HEEA076404 120011003G3213407050201101 CROSSTUBE BELL 407 407 1182206SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0357416 53070 FORWARD CROSSTUBE HAS CORROSION. SCRAPPED AND REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U O H2SW 20011024000422001102400042SW 2001 10 24 HEEA076405 120011003G3213407050202101 CROSSTUBE BELL 407 407 1182206SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0357416 53070 AFT CROSSTUBE HAS CORROSION. SCRAPPED AND REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U O H2SW 20011024000432001102400043SW 2001 10 24 HEEA076406 120011003G2510407070720117 SEAT BACK BELL 407 407 1182206SW COCKPIT TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03722PH 53288 TORN. SCRAPPED AND REPLACED WITH SERVICEABLE SEAT BACK. 1G71 3U O H2SW 20011024000442001102400044SW 2001 10 24 HEEA076407 120011003G5210407070620137 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH 53398 CRACKS. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000452001102400045SW 2001 10 24 HEEA076408 120011003G5210407070620138 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03722PH 53288 CRACKED AND BROKEN IN SEVERAL PLACES. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000462001102400046SW 2001 10 24 HEEA076409 120011003G5210407070620138 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 SEVERAL CRACKS. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000472001102400047SW 2001 10 24 HEEA076410 120011003G5230407070620143 PANEL BELL 407 407 1182206SW CARGO DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 LITTER DOOR PANEL CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000482001102400048SW 2001 10 24 HEEA076411 120011003G5230407070620157 PANEL BELL 407 407 1182206SW CARGO DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 LT REAR DOOR PANEL HAS NUMEROUS CRACKS. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000492001102400049SW 2001 10 24 HEEA076412 120011003G5210407070620157 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH 53398 DOOR TRIM PANEL CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000502001102400050SW 2001 10 24 HEEA076413 120011003G5210407070620157 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 LT PASSENGER DOOR PANEL CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000512001102400051SW 2001 10 24 HEEA076414 120011003G5210407070620158 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH 53398 CRACKED PANEL. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000522001102400052SW 2001 10 24 HEEA076415 120011003G5230407070620158 PANEL BELL 407 407 1182206SW CARGO DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 RT REAR DOOR PANEL CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000532001102400053SW 2001 10 24 HEEA076416 120011003G5210407070620179 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH 53398 DOOR PANEL CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000542001102400054SW 2001 10 24 HEEA076417 120011003G5310407070620180 PANEL BELL 407 407 1182206SW DOOR FRAME CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 PILOT DOOR POST TRIM PANEL CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000552001102400055SW 2001 10 24 HEEA076418 120011003G5230407070620205 COVER BELL 407 407 1182206SW CARGO DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH 53398 LITTER DOOR LATCH COVER CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE COVER. 1G71 3U O H2SW 20011024000562001102400056SW 2001 10 24 HEEA076419 120011003G5210407070620217 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 PANEL CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000572001102400057SW 2001 10 24 HEEA076420 120011003G5210407070620218 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 PANEL CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000582001102400058SW 2001 10 24 HEEA076421 120011003G5230407070620205 COVER BELL 407 407 1182206SW CARGO DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 LITTER DOOR LATCH COVER CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE COVER. 1G71 3U O H2SW 20011024000592001102400059SW 2001 10 24 HEEA076422 120011003G5210407070620218 PANEL BELL 407 407 1182206SW CREW DOOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 PANEL CRACKED. SCRAPPED AND REPLACED WITH SERVICEABLE PANEL. 1G71 3U O H2SW 20011024000602001102400060SW 2001 10 24 HEEA076423 120011003G2510407070622115 SEAT BELL 407 407 1182206SW ARM REST CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03612PH 53199 LT AFT FACING SEAT ARM REST FABRIC TORN. SCRAPPED AND REPLACED WITH SERVICEABLE ARM REST. 1G71 3U O H2SW 20011024000612001102400061 2001 10 24 HEEA076424 420011003G2312064100900 TRANSCEIVER BELL 412 412 1182202SW RADIO SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035759N 33002 WEAK AND GARBLED. IN SHOP REPAIR. 1G72 4U H4SW 20011024000622001102400062 2001 10 24 HEEA076425 420011003G2312064101900 TRANSCEIVER BELL 206 206L3 1182108SW RADIO SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033116P 51530 DOES NOT RECEIVE. IN SHOP REPAIR. 1G71 3U H2SW 20011024000632001102400063 2001 10 24 HEEA076426 420011003G3452066106200 TRANSCEIVER BELL 206 206L3 1182108SW ATC SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0321497 51518 WOULD NOT TRANSMIT POWER MODE C SIGNALS. IN SHOP REPAIR. 1G71 3U H2SW 20011024000642001102400064 2001 10 24 HEEA076427 420011003G3451066106600 TRANSCEIVER BELL 412 412 1182202SW DME SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036559Z 36019 DME SYSTEM TRANSCEIVER INOPERATIVE; WILL NOT COME ON. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011024000652001102400065 2001 10 24 HEEA076428 420011003G3452066107100 TRANSPONDER BELL 412 412 1182202SW ATC SYSTEM MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032149S 36002 TRANSMIT OFF FREQUENCY AND REPLY RATE IS LOW AND ERRATIC. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011024000662001102400066 2001 10 24 HEEA076429 420011003G3416066304400 ALTIMETER BELL 412 412 1182202SW RADAR MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032149S 36002 KEEPS CYCLING AFTER PUSHING TEST BUTTON. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011024000672001102400067 2001 10 24 HEEA076430 420011003G3453066402600 TRANSCEIVER LORAN SYSTEM MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 DISPLAY REMAINED BLANK AFTER BEING ON FOR 10 MINUTES AND REMAINED BLANK AFTERWARDS. PENDING VENDOR REPAIR. 20011024000682001102400068 2001 10 24 HEEA076431 420011003G3452071119218 CONTROL UNIT BELL 412 412 1182202SW TRANSPONDER WILL NOT TEST E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03142PH 33150 WON'T TEST PROPERLY. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011024000692001102400069SW 2001 10 24 HEEA076432 120011003G5520205030856131 STRUCTURE BELL 412 412 1182202SW ELEVATOR CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035759N 33002 SHEETMETAL CRACK WHERE SPAR IS MOUNTED TO ELEVATOR. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011024000702001102400070SW 2001 10 24 HEEA076433 120011003G6700 BEARING BELL 206 206L3 1182108SW BELLCRANK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW036251X 51552 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011024000712001102400071SW 2001 10 24 HEEA076434 120011003G6220206011117003 RESTRAINT BELL 206 206L3 1182108SW MAIN ROTOR HEAD STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW034180F STICKS IN THE DOWN POSITION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011024000792001102400079SW 2001 10 24 HEEA076435 120011003G6220206011117003 RESTRAINT BELL 206 206L3 1182108SW MAIN ROTOR HEAD STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 STICKING IN RETRACT POSITION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011024000862001102400086SW 2001 10 24 HEEA076436 120011003G6320206040088005 VALVE BELL 206 206L3 1182108SW MAIN ROTOR MISMANUFACTURED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 IMPROPERLY MANUFACTURED THREADS, CANNOT BE INSTALLED INTO TRANSMISSION CASE WITHOUT CAUSING DAMAGE TO CASE THREADS. TRIED TO INSTALL VALVE INTO TWO DIFFERENT CASES AND COULD NOT. 1G71 3U H2SW 20011024000872001102400087SW 2001 10 24 HEEA076437 120011003G6320206040190005 PUMP BELL 206 206L3 1182108SW MAIN ROTOR LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 LEAKS PAST SEAL. REPLACED WITH SERVICEABLE PUMP. 1G71 3U H2SW 20011024001272001102400127SW 2001 10 24 HEEA076438 120011003G6710206062721109 ACTUATOR BELL 206 206L1 1182107SW M/R CONTROL INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW035014Y 45219 INOPERATIVE NO EXTENSION OR RETRACTION OF CONTROL SHAFT. REPLACED WITH SERVICEABLE ACTUATOR. 1G71 3U H2SW 20011024001302001102400130SW 2001 10 24 HEEA076439 120011003G3212206073926109 VALVE BELL 412 412 1182202SW MLG LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 LEAKS ABOVE 2900 PSI. REPLACED WITH SERVICEABLE VALVE. 1G72 4U H4SW 20011024001322001102400132SW 2001 10 24 HEEA076440 120011003G3213206323017 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0353119 51575 CORRODED BEYOND LIMITS AT SUPPORT MOUNT AREA, MEASURED .010 INCHES IN ZONE 1. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20011024001332001102400133SW 2001 10 24 HEEA076441 120011003G3213206323018 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0353119 51575 CORRODED BEYOND LIMITS AT SUPPORT MOUNT AREA, MEASURED .010 INCHES IN ZONE 1. REPLACED WITH SERVICEABLE CROSSTUBE. 1G71 3U H2SW 20011024001342001102400134SW 2001 10 24 HEEA076442 120011004G3246206324008 SKID BELL 206 206L3 1182108SW MLG CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331821 51076 18 INCH CRACK AT LOWER SIDE SKID TUBE. REPLACED WITH SERVICEABLE SKID TUBE. 1G71 3U H2SW 20011024001352001102400135SW 2001 10 24 HEEA076443 120011004G5260206331119 STEP BELL 206 206L3 1182108SW FUSELAGE CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0353119 51575 INTERGRANULAR CORROSION BEYOND LIMITS AT MOUNT AREA. REPLACED WITH SERVICEABLE STEP. 1G71 3U H2SW 20011024001362001102400136SW 2001 10 24 HEEA076444 120011004G5260206331120 STEP BELL 206 206L3 1182108SW FUSELAGE CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0353119 51575 INTERGRANULAR CORROSION BEYOND LIMITS AT MOUNT AREA. REPLACED WITH SERVICEABLE STEP. 1G71 3U H2SW 20011024001372001102400137SW 2001 10 24 HEEA076445 120011004G7933206375007103 INDICATOR BELL 206 206L3 1182108SW OVERTEMP WILL NOT TEST E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033116P 51530 OVERTEMP LIGHT WILL NOT TEST. PENDING VENDOR REPAIR. 1G71 3U H2SW 20011024001382001102400138SW 2001 10 24 HEEA076446 120011004G7921209062501005 OIL COOLER BELL 412 412 1182202SW ENGINE LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW032149S 36002 LEAKING. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011024001452001102400145SW 2001 10 24 HEEA076447 120011004G7600212061101001 BEARING BELL 412 412 1182202SW ENGINE CONTROLS WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 WORN BEARING. REPLACED WITH SERVICEABLE BEARING. 1G72 4U H4SW 20011024001462001102400146 2001 10 24 HEEA076448 420011004G3100212070262101 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035759N 33002 PRESSURE NEEDLE STICKS AFTER START UP ONLY SHOWS PRESSURE IF GAUGE IS TAPPED. REPLACED WITH SERVICEABLE INDICATOR. 1G72 4U H4SW 20011024001472001102400147SW 2001 10 24 HEEA076449 120011004G5260212075418105 STEP BELL 412 412 1182202SW FUSELAGE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036559Z 36019 WILL NOT EXTEND. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011024001482001102400148SW 2001 10 24 HEEA076450 120011004G6730212076004101 SERVO BELL 412 412 1182202SW TAIL ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03107X 33113 LEAKING. REPLACED WITH SERVICEABLE SERVO. 1G72 4U H4SW 20011024001492001102400149SW 2001 10 24 HEEA076451 120011004G6730212076005111 SERVO BELL 412 412 1182202SW TAIL ROTOR STIFF E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 MOVEMENTS ARE STIFFENED AND VERY HARD TO MOVE. REPLACED WITH SERVICEABLE SERVO. 1G72 4U H4SW 20011024001512001102400151SW 2001 10 24 HEEA076452 120011004G6710214001347005 ACTUATOR BELL 412 412 1182202SW ROTARY STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 STICKING. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011024001532001102400153GL 2001 10 24 HEEA076453 220011004G753223005366 BLEED VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036251X7023 51552 HIGH TOT, DIDN'T CLOSE SMOOTHLY WHEN PRESSURE WAS APPLIED. REPLACED WITH SERVICEABLE BLEED VALVE. 1G71 3U3 U H2SW E1GL 20011024001542001102400154GL 2001 10 24 HEEA076454 220011004G731023005667 LINE BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL FUEL SYSTEM CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0321497 51518 LINE IS CRACKED AT FLARE. REPLACED WITH SERVICEABLE LINE. 1G71 3U3 U H2SW E1GL 20011024001572001102400157GL 2001 10 24 HEEA076455 220011004G731023007827 SOLENOID VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL FUEL SYSTEM STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW033108E 51498 STICKS INTERMITTENTLY. REPLACED WITH SOLENOID VALVE. 1G71 3U3 U H2SW E1GL 20011024001582001102400158SW 2001 10 24 HEEA076456 120011004G712023069751 MOUNT BELL 206 206L3 1182108SW ENGINE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331077 51520 BEARING CAME UNSTAKED. REPLACED WITH SERVICEABLE MOUNT. 1G71 3U H2SW 20011024001592001102400159GL 2001 10 24 HEEA076457 220011004G7323252469211 GOVERNOR BELL 206 206L1 1182107SW ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035014V13616 45217 N2 DROOP TO 97 PERCENT. COMPLETED DROOP COMPENSATION ADJUSTMENTS AND COMPLETED OPERATIONAL CHECK. FOUND ACCEPTABLE. AFTER 2:45 ADDITIONAL FLIGHT HOURS REPORTED N2 DROOP TO 97 PERCENT WITH N2 OVERSPEED TO 102 PERCENT. REPLACED WITH SERVICEABLE GOVERNOR. 1G71 3U3 U H2SW E1GL 20011024001642001102400164NE 2001 10 24 HEEA076458 220011004G732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE FREE TURBINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 NR 2 ENGINE SURGES. REPLACED WITH SERVICEABLE GOVERNOR. 1G72 4U4 U H4SW E22EA 20011024001682001102400168NE 2001 10 24 HEEA076459 220011004G732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE FREE TURBINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 ENGINE OSCILLATES CONSTANTLY 1 TO 3 PERCENT N1 WITH ITT FLUCTUATIONS. REPLACED WITH SERVICEABLE GOVERNOR. 1G72 4U4 U H4SW E22EA 20011024001702001102400170NE 2001 10 24 HEEA076460 220011004G732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE FREE TURBINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03800Y 33134 SURGING. REPLACED WITH SERVICEABLE GOVERNOR. 1G72 4U4 U H4SW E22EA 20011024001712001102400171SW 2001 10 24 HEEA076461 120011004G7603 THROTTLE BELL 206 206L3 1182108SW ENGINE CONTROLS STIFF E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331077 51520 THROTTLE STIFF. REPLACED WITH SERVICEABLE FUEL CONTROL. 1G71 3U H2SW 20011024001732001102400173SW 2001 10 24 HEEA076462 120011004G7603 THROTTLE BELL 206 206L3 1182108SW FUEL CONTROL STIFF E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331077 51520 THROTTLE STIFF. REPLACED WITH SERVICEABLE FUEL CONTROL. 1G71 3U H2SW 20011024001792001102400179 2001 10 24 HEEA076463 420011004G22002593996333 TARSYN BELL 412 412 1182202SW AUTOFLIGHT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW033893L 33006 COMPASS CONTROL PANEL NEEDLE FLIPPING CONSTANTLY. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011024001832001102400183EA 2001 10 24 HEEA076464 220011004G7532 DIAPHRAGM 3033063 BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA BLEED VALVE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03102PH 2A599 30899 INCREASE OF 40 DEGREES ITT AND 4 PERCENT N1 AT POWER CHECK SETTINGS. FOUND HOLE IN DIAPHRAGM. REPLACED WITH SERVICEABLE DIAPHRAGM. 1G71 4U4 U H4SW E22EA 20011024001842001102400184SW 2001 10 24 HEEA076465 120011004G710032447066 CONTROL UNIT BELL 412 412 1182202SW TORQUE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 CAUSING TORQUE SPLITS. REPLACED WITH SERVICEABLE TORQUE CONTROL UNIT. 1G72 4U H4SW 20011024001952001102400195NE 2001 10 24 HEEA076466 220011004G7320324473514 FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 ENGINE SURGING DURING POWER CHANGES CAUSING AIRCRAFT TO YAW. REPLACED WITH SERVICEABLE FUEL CONTROL. 1G72 4U4 U H4SW E22EA 20011024001982001102400198 2001 10 24 HEEA076467 420011004G34424000023010 RADAR BELL 206 206L3 1182108SW WX RADAR SYS MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 NO MODULATION OUT. REPLACED WITH SERVICEABLE RT-15. 1G71 3U H2SW 20011024002002001102400200 2001 10 24 HEEA076468 420011004G34424000038 CONTROL HEAD BELL 206 206L3 1182108SW WX RADAR MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0342EA 51542 HAS DEAD SPOT ON VOLUME CONTROL. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011024002022001102400202SW 2001 10 24 HEEA076469 120011004G6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 UNABLE TO TRACK. REPLACED WITH SERVICEABLE BLADE. 1G72 4U H4SW 20011024002032001102400203SW 2001 10 24 HEEA076470 120011004G6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 LEADING EDGE EROSION. REPLACED WITH SERVICEABLE BLADE. 1G72 4U H4SW 20011024002042001102400204SW 2001 10 24 HEEA076471 120011004G3212412050013109 FLOAT BELL 412 412 1182202SW MLG LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 LEAKING. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011024002052001102400205SW 2001 10 24 HEEA076472 120011004G3212412050017135 COVER BELL 412 412 1182202SW FLOAT BAG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 WORN AND TORN. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011025000012001102500001SW 2001 10 25 HEEA076473 120011004G3213412050045107 CROSSTUBE BELL 412 412 1182202SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03800Y 3378 33134 CORRODED IN SEVERAL AREAS BEYOND LIMITS. THE CORRODED AREAS ARE NEAR THE SKID MOUNTS TO 18" TOWARD THE CENTER. RETURNING FOR CREDIT. 1G72 4U H4SW 20011025000022001102500002SW 2001 10 25 HEEA076475 120011004G6220412310400101 BEARING BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 WORN LOWER BEARING. REPLACED WITH SERVICEABLE BEARING. 1G72 4U H4SW 20011025000032001102500003SW 2001 10 25 HEEA076476 120011004G632041800044 TRANSMITTER BELL 412 412 1182202SW M/R GEARBOX MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW033893N 33010 PRESSURE INDICATOR NEEDLE PEGGED OUT ON HIGH SIDE. REPLACED WITH SERVICEABLE TRANSMITTER. 1G72 4U H4SW 20011025000042001102500004 2001 10 25 HEEA076477 420011004G34215040017928 INDICATOR BELL 412 412 1182202SW ATTITUDE PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 INDICATOR PRECESSES 5-8 DEGREES. REPLACED WITH SERVICEABLE INDICATOR. 1G72 4U H4SW 20011025000052001102500005 2001 10 25 HEEA076478 420011004G31306895D4655 SWITCH BELL 412 412 1182202SW CVR MALFUNCTIONED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03107X 33113 CVR INTERMITTENTLY WON'T TEST. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011025000062001102500006SW 2001 10 25 HEEA076479 120011004G28447G547 SWITCH BELL 206 206B3 1181506SW FUEL PRESSURE FAILED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0322751 3627 FUEL PRESSURE SWITCH OPERATED CORRECTLY ON INSTALLATION - NEXT MORNING FUEL PUMP LIGHT CAME ON AND WOULD NOT GO OUT. REPLACED WITH SERVICEABLE SWITCH. 1G71 3U H2SW 20011025000072001102500007 2001 10 25 HEEA076480 420011004G34427021450601 COMPUTER BELL 214 214ST 1182106SW COCKPIT FAILED E O OTHER O OTHER NRNOT REPORTED 1 SW035748M 28102 WEATHER RADAR SYSTEM DROPS OFF IN FLIGHT. PENDING VENDOR REPAIR. 2G72 4U H10SW 20011025000082001102500008 2001 10 25 HEEA076481 420011004G2350AA38300 AMPLIFIER BELL 412 412 1182202SW ICS NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 LOUD STATIC NOISE WHEN AIRCRAFT IS RUNNING. PENDING VENDOR RETURN. 1G72 4U H4SW 20011025000092001102500009 2001 10 25 HEEA076482 420011004G2350AA38300 AMPLIFIER BELL 412 412 1182202SW ICS NOISY E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 LOUD STATIC NOISE WHEN AIRCRAFT IS RUNNING. PENDING VENDOR RETURN. 1G72 4U H4SW 20011025000102001102500010SW 2001 10 25 HEEA076483 120011004G3213AB412050016101 SKID SHOE BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 WORN. REPLACED WITH SERVICEABLE SKID SHOE. 1G72 4U H4SW 20011025000112001102500011SW 2001 10 25 HEEA076484 120011004G3213AB412050016102 SKID SHOE BELL 412 412 1182202SW MLG WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036559Z 36019 WORN. REPLACED WITH SERVICEABLE SKID SHOE. 1G72 4U H4SW 20011025000122001102500012 2001 10 25 HEEA076485 420011004G3442MI5851345 INDICATOR BELL 412 412 1182202SW RADAR SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 WON'T PAINT TARGETS ON 10 MILE SCALE. REPLACED WITH SERVICEABLE INDICATOR. 1G72 4U H4SW 20011025000132001102500013 2001 10 25 HEEA076486 420011004G3442MI5852013 INDICATOR BELL 412 412 1182202SW RADAR SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 SCREEN GOES BLANK AND SHOWS YELLOW VERTICAL LINES. REPLACED WITH SERVICEABLE INDICATOR. 1G72 4U H4SW 20011025000142001102500014 2001 10 25 HEEA076487 420011004G3442MI5852013 INDICATOR BELL 412 412 1182202SW RADAR SYSTEM FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 SCREEN SHRINKS. REPLACED WITH SERVICEABLE INDICATOR. 1G72 4U H4SW 20011025000152001102500015SW 2001 10 25 HEEA076488 120011004G2497MS915872 SHUNT BELL 206 206L3 1182108SW GENERATOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 GENERATOR LIGHT ILLUMINATED IN FLIGHT AND GEN. WOULD RESET. REPLACED WITH SERVICEABLE SHUNT. 1G71 3U H2SW 20011025000162001102500016 2001 10 25 HEEA076489 420011004G3421PHI4121017601 INDICATOR BELL 412 412 1182202SW ATTITUDE PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033893L 33006 PRECESSES EXCESSIVELY. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025000172001102500017SW 2001 10 25 HEEA076490 120011004G5260407301107 STEP BELL 407 407 1182206SW FUSELAGE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03409PH 53059 CORROSION BEYOND LIMITS. SCRAPPED. 1G71 3U O H2SW 20011025000182001102500018SW 2001 10 25 HEEA076491 120011004G5260407301108 STEP BELL 407 407 1182206SW FUSELAGE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03409PH 53059 CORROSION BEYOND LIMITS. SCRAPPED. 1G71 3U O H2SW 20011025000192001102500019SW 2001 10 25 HEEA076492 120011004G6320407375005101 INDICATOR BELL 407 407 1182206SW XMSN OIL TEMP FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03740PH 53435 NO TRANSMISSION TEMPERATURE INDICATION. INDICATOR READ ZERO. 1G71 3U O H2SW 20011025000202001102500020SW 2001 10 25 HEEA076495 120011005G3212206050247137 COVER BELL 407 407 1182206SW FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 FLOAT COVER HAS WORN END CAPS. 1G71 3U O H2SW 20011025000212001102500021SW 2001 10 25 HEEA076496 120011005G6510206061432121 HOUSING BELL 407 407 1182206SW COOLER BLOWER CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 BLOWER HOUSING HAS A CRACKED AT CORNER. 1G71 3U O H2SW 20011025000222001102500022SW 2001 10 25 HEEA076497 120011005G6710406310404101 ROD END BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH1749 53399 MAIN ROTOR ROD END HAS WORN BEARINGS. 1G71 3U O H2SW 20011025000232001102500023SW 2001 10 25 HEEA076498 120011005G6220412010219101 BEARING BELL 412 412EP 1182205SW PENDULUM DAMPER TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036106C388 36257 SEAL ON PENDULUM DAMPER TORN CAUSING LOSS OF GREASE AND WEAR ON INNER RACE. 1G72 4U H4SW 20011025000242001102500024SW 2001 10 25 HEEA076499 120011005G6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03721PH451 53278 UNIVERSAL WORN. 1G71 3U O H2SW 20011025000252001102500025SW 2001 10 25 HEEA076500 120011005G6720 BEARING BELL 407 407 1182206SW LINK ASSY STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 STICKING BEARING. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#720438. 1G71 3U O H2SW 20011025000262001102500026SW 2001 10 25 HEEA076501 120011005G6300206362002103 CAP BELL 407 407 1182206SW M/R DRIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 WORN AND HARD TO OPEN. 1G71 3U O H2SW 20011025000272001102500027SW 2001 10 25 HEEA076502 120011005G6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH1246 53198 BEARING WORN. 1G71 3U O H2SW 20011025000282001102500028SW 2001 10 25 HEEA076503 120011005G243228SP100 CELL BELL 407 407 1182206SW BATTERY BURNED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH 53401 CELL BURNT. 1G71 3U O H2SW 20011025000292001102500029SW 2001 10 25 HEEA076504 120011005G7120407060111101 MOUNT BELL 407 407 1182206SW ENGINE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 ONE BEARING WORN. 1G71 3U O H2SW 20011025000302001102500030SW 2001 10 25 HEEA076505 120011005G3212206050247131 COVER BELL 407 407 1182206SW FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 TATTERED AND TORN. 1G71 3U O H2SW 20011025000342001102500034SW 2001 10 25 HEEA076506 120011005G6310406040316101 ADAPTER BELL 407 407 1182206SW ENG XMSN COUP WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 WORN SPLINES. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#720545. 1G71 3U O H2SW 20011025000352001102500035SW 2001 10 25 HEEA076507 120011005G6510206061432121 HOUSING BELL 407 407 1182206SW COOLER BLOWER CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03409PH 53059 COOLER BLOWER HOUSING CRACKED. 1G71 3U O H2SW 20011025000362001102500036SW 2001 10 25 HEEA076508 120011005G6510206061432121 HOUSING BELL 407 407 1182206SW COOLER BLOWER CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0357416 53070 COOLER BLOWER HOUSING CRACKED AND RIVETS WORKING. 1G71 3U O H2SW 20011025000372001102500037SW 2001 10 25 HEEA076509 120011005G3212206050247131 COVER BELL 407 407 1182206SW FLOAT TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 TORN END COVER. 1G71 3U O H2SW 20011025000382001102500038SW 2001 10 25 HEEA076510 120011005G2510407370720101 RESTRAINT BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 INERTIA REEL LOCKS UP AND STRAPS FRAYED. 1G71 3U O H2SW 20011025000392001102500039SW 2001 10 25 HEEA076511 120011005G28222C273 CARTRIDGE BELL 412 412EP 1182205SW BOOST PUMP INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW036106C 36257 FUEL CARTRIDGE INOPERATIVE. 1G72 4U H4SW 20011025000402001102500040SW 2001 10 25 HEEA076513 120011005G2820206061634003 VALVE BELL 407 407 1182206SW FUEL SYSTEM STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 FUEL VALVE STICKING. 1G71 3U O H2SW 20011025000412001102500041SW 2001 10 25 HEEA076520 120011008G6510407340339103 BEARING 407040302101BELL 407 407 1182206SW T/R DRIVESHAFT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH A15 53400 WORN BEARING. SCRAPPED IN HOUSE. 1G71 3U O H2SW 20011025000422001102500042SW 2001 10 25 HEEA076521 120011008G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE BURNED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035748M161 28102 BURNT. WILL NOT OPERATE. 2G72 4U H10SW 20011025000432001102500043SW 2001 10 25 HEEA076522 120011008G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035748M210 28102 WILL NOT DISENGAGE. 2G72 4U H10SW 20011025000442001102500044SW 2001 10 25 HEEA076523 120011008G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035980642 28140 WILL NOT ENGAGE. CLUTCH IN PIECES. 2G72 4U H10SW 20011025000452001102500045SW 2001 10 25 HEEA076524 120011008G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035748M51 28102 DOES NOT DISENGAGE. 2G72 4U H10SW 20011025000462001102500046SW 2001 10 25 HEEA076525 120011009G5320206020113173S CAP BELL 206 206A 1181508SW FUSELAGE CRACKED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03 RECEIVED DENTED AND CRACK AT LEADING EDGE. 1G71 3U H2SW 20011025000502001102500050SW 2001 10 25 HEEA076527 120011010G7712222375077119 TRANSMITTER BELL 407 407 1182206SW TORQUE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH1228 53396 LOW TORQUE INDICATION. 1G71 3U O H2SW 20011025000612001102500061SW 2001 10 25 HEEA076528 120011010G3212206373901103 SOLENOID VALVE BELL 407 407 1182206SW MLG FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 DISCHARGED ON ITS OWN. INSTALLED 11-9-99 AT A/C TOTAL TIME 2102:15 AND REMOVED AT A/C TOTAL TIME 3683:40. 1G71 3U O H2SW 20011025000622001102500062SW 2001 10 25 HEEA076529 120011010G2400A490ATSCF1428 POWER SUPPLY BELL 407 407 1182206SW WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH2297 53393 POWER SUPPLY HAS WEAK OUTPUT. 1G71 3U O H2SW 20011025000632001102500063SW 2001 10 25 HEEA076530 120011010G7700222375077113 TRANSMITTER BELL 407 407 1182206SW OIL PRESSURE FLUCTUATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH6597 53003 FLUCTUATING APPROX. 10 PSI. 1G71 3U O H2SW 20011025000682001102500068SW 2001 10 25 HEEA076531 120011010G7714212075037109 INDICATOR BELL 412 412EP 1182205SW ENGINE FLUCTUATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036106C 36257 FLUCTUATES ON START CYCLE UNTIL 30 PERCENT N1 SPEED ATTAINED. 1G72 4U H4SW 20011025000692001102500069SW 2001 10 25 HEEA076532 120011010G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033897N477 28106 FAILED CLUTCH INSPECTION AND BEARING EXTENDING FROM HOUSING. 2G72 4U H10SW 20011025001042001102500104SW 2001 10 25 HEEA076534 120011010G3110SM20ACD300A21 RELAY BELL 407 407 1182206SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 START LIGHT WILL NOT ILLUMINATE. 1G71 3U O H2SW 20011025001062001102500106SW 2001 10 25 HEEA076535 120011010G7933407375004101 INDICATOR BELL 407 407 1182206SW ENG OIL TEMP FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 WILL GO TO ZERO INTERMITTENTLY. 1G71 3U O H2SW 20011025001072001102500107SW 2001 10 25 HEEA076536 120011010G7712407375003107 INDICATOR BELL 407 407 1182206SW TORQUE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH 53277 NO INDICATION ON GAUGE. IT WILL NOT TEST. 1G71 3U O H2SW 20011025001082001102500108SW 2001 10 25 HEEA076537 120011010G7931222375077113 TRANSMITTER BELL 407 407 1182206SW ENGINE OIL FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 ENGINE PRESSURE DROPPED TO ZERO. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#720488. 1G71 3U O H2SW 20011025001092001102500109SW 2001 10 25 HEEA076538 120011010G3212206373901103 SOLENOID VALVE BELL 407 407 1182206SW MLG FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 UNABLE TO SEAT FILLER VALVE. 1G71 3U O H2SW 20011025001102001102500110SW 2001 10 25 HEEA076539 120011010G2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW BOOST PUMP FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH30 53283 LEFT BOOST PUMP LIGHT DOESN'T ILLUMINATE WHEN SWITCH IS IN OFF POSITION. 1G71 3U O H2SW 20011025001112001102500111SW 2001 10 25 HEEA076540 120011010G3212206373901103 SOLENOID VALVE BELL 407 407 1182206SW MLG FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 FLOAT BAG SOLENOID VALVE LEAKING. 1G71 3U O H2SW 20011025001122001102500112SW 2001 10 25 HEEA076541 120011010G2913206076030111 PUMP BELL 407 407 1182206SW HYD SYSTEM DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH1452 53386 DRIVE SPLINES WORN. 1G71 3U O H2SW 20011025001132001102500113SW 2001 10 25 HEEA076542 120011010G6320 BEARING BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH3893 53198 BEARINGS WORN. 1G71 3U O H2SW 20011025001172001102500117SW 2001 10 25 HEEA076543 120011010G3212206373901103 SOLENOID VALVE BELL 407 407 1182206SW FLOAT BAG LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 FLOAT BAG SOLENOID VALVE IS LEAKING. 1G71 3U O H2SW 20011025001192001102500119SW 2001 10 25 HEEA076545 120011010G6230406010401117 SWASHPLATE BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH1163 53396 GREASE PURGES THROUGH THE TOP. 1G71 3U O H2SW 20011025001202001102500120SW 2001 10 25 HEEA076546 120011010G3212206373901103 SOLENOID VALVE BELL 407 407 1182206SW FLOAT BAG LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03467PH 53142 SOLENOID VALVE FOR FLOAT BAG LEAKING. 1G71 3U O H2SW 20011025001212001102500121SW 2001 10 25 HEEA076547 120011010G6300407310203101 MOUNT BELL 407 407 1182206SW MAIN ROTOR DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH1974 53400 MAIN ROTOR MOUNT DETERIORATED. 1G71 3U O H2SW 20011025001222001102500122SW 2001 10 25 HEEA076550 120011010G6310406040500123B FREEWHEEL UNIT BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03723PH3100 53283 LEAKING AT FRONT SEAL. . 1G71 3U O H2SW 20011025001232001102500123SW 2001 10 25 HEEA076551 120011010G6300407010206103 SPRING BELL 407 407 1182206SW MAIN ROTOR SEPARATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH2485 53283 SPRING HAS SEPARATION. 1G71 3U O H2SW 20011025001252001102500125SW 2001 10 25 HEEA076555 120011010G6730206076062107 SERVO BELL 407 407 1182206SW CYCLIC LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03494PH1866 53396 CYCLIC SERVO LEAKING. 1G71 3U O H2SW 20011025001262001102500126SW 2001 10 25 HEEA076556 120011010G6730206076062107 SERVO BELL 407 407 1182206SW CYCLIC LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03494PH1866 53396 CYCLIC SERVO LEAKING. 1G71 3U O H2SW 20011025001282001102500128SW 2001 10 25 HEEA076557 120011010G6210407015001117 BLADE BELL 407 407 1182206SW MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03409PH4173 53059 MAIN ROTOR BLADE CRACKED AT OUTBOUND TRIM TAB. 1G71 3U O H2SW 20011025001292001102500129SW 2001 10 25 HEEA076558 120011010G6320407040006107 TRANSMISSION BELL 407 407 1182206SW MAIN ROTOR MAKING METAL E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03721PH1594 53278 MAIN ROTOR TRANSMISSION MAKING METAL. 1G71 3U O H2SW 20011025001302001102500130SW 2001 10 25 HEEA076559 120011010G6300 BEARING BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH3728 53207 WORN BEARINGS. 1G71 3U O H2SW 20011025001332001102500133 2001 10 25 HEEA076560 420011010G3197 CONNECTOR BELL 407 407 1182206SW INSTRUMENT PANELDAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH3728 53207 BENT PIN IN PLUG. 1G71 3U O H2SW 20011025001342001102500134SW 2001 10 25 HEEA076564 120011010G771432005037 TACH GENERATOR BELL 412 412 1182202SW NR 2 ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 ON INBOUND FLIGHT, THE NR 2 ENGINE OUT LIGHT ILLUMINATED. REPLACED NR 2 ENGINE N1 TACH GEN. 1G72 4U H4SW 20011025001362001102500136SW 2001 10 25 HEEA076565 120011010G2910212076433001 LINE BELL 412 412 1182202SW HYD SYSTEM CRACKED E HEEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW031202T 33112 WHILE IN CRUISE FLIGHT, NR 1 HYDRAULIC SYSTEM FAILED. MAINTENANCE REPLACED HYDRAULIC TUBE ASSY DUE TO CRACK IN ONE OF THE CURVES. 1G72 4U H4SW 20011025001402001102500140NE 2001 10 25 HEEA076566 220011011G720023063412 HOSE BELL 407 407 1182206SW ALLSN 250C 250C40B 03032NE ENGINE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 HOSE LEAKS UNDER PRESSURE. REPLACED WITH SERVICEABLE HOSE. 1G71 3U3 UO H2SW E1GL 20011025001422001102500142SW 2001 10 25 HEEA076567 120011011G6230406010401117 SWASHPLATE BELL 407 407 1182206SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03720PH1861 53277 SWASHPLATE SEAL SPINNING IN CAP. 1G71 3U O H2SW 20011025001432001102500143SW 2001 10 25 HEEA076568 120011011G6310406040500119 SUPPORT BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW038595X 53267 SUPPORT LEAKING FROM SEAL. 1G71 3U O H2SW 20011025001442001102500144SW 2001 10 25 HEEA076572 120011011G6420 BEARING BELL 407 407 1182206SW TAIL ROTOR HUB WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03742PH1146 53461 TAIL ROTOR HUB HAS A WORN BEARING. 1G71 3U O H2SW 20011025001452001102500145SW 2001 10 25 HEEA076573 120011011G6300407310203101 MOUNT BELL 407 407 1182206SW MAIN ROTOR DETERIORATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH 53159 DETERIORATED. 1G71 3U O H2SW 20011025001462001102500146SW 2001 10 25 HEEA076574 120011011G6510407340340103 DISC PACK BELL 407 407 1182206SW T/R DRIVE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03723PH 53283 DISC PACK CRACKED. 1G71 3U O H2SW 20011025001482001102500148SW 2001 10 25 HEEA076575 120011011G6510407340340103 DISC PACK BELL 407 407 1182206SW T/R DRIVE CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 DISC PACK CRACKED. 1G71 3U O H2SW 20011025001492001102500149 2001 10 25 HEEA076580 420011011G2312064100900 TRANSCEIVER BELL 412 412 1182202SW VHF SYSTEM WEAK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032261D 33076 TRANSMITS WEAK. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001502001102500150 2001 10 25 HEEA076581 420011011G3420071105200 INDICATOR BELL 230 230 1182149SW ATTITUDE PRECESSES E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03911RC 23037 INTERMITTENT PROBLEM OF PRECESSING 30 DEGREES. REPLACED WITH SERVICEABLE PART. 1G72 3U NCH9SW 20011025001512001102500151 2001 10 25 HEEA076582 420011011G3442071111401 ANTENNA BELL 206 206L3 1182108SW RADAR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW036748D 51106 COAX PULLED OUT FROM ANTENNA CONNECTOR. REPLACED WITH SERVICEABLE PART. TO BE SENT TO VENDOR FOR REPAIR. 1G71 3U H2SW 20011025001522001102500152 2001 10 25 HEEA076583 420011011G345713824120234 GPS BELL 206 206L1 1182107SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033905B 45598 FAILED DUMPING ALL WAYPOINTS, RECEIVER AND BATTERY BACK UP FAIL KEPT FLASHING IN MESSAGE MODE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011025001532001102500153SW 2001 10 25 HEEA076584 120011011G6510204040620011 SHAFT BELL 412 412 1182202SW TAIL ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW031202T 33112 WEIGHT MISSING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001542001102500154SW 2001 10 25 HEEA076585 120011011G2140205072277009 VALVE BELL 412 412 1182202SW HEATER INTERMITTENT E K NONE L NO TEST ININSP/MAINT 1 SW03107X 33113 HEATER MIXING VALVE WORKS INTERMITTENTLY. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001632001102500163SW 2001 10 25 HEEA076586 120011011G6400 BEARING BELL 206 206L3 1182108SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033108E 51498 BEARINGS WORN AND RUSTED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011025001642001102500164SW 2001 10 25 HEEA076587 120011011G3212206050248111 FLOAT BELL 206 206L3 1182108SW MLG FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW034835 51131 FAILED ALTERNATE CHAMBER CHECK. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011025001652001102500165GL 2001 10 25 HEEA076588 220011011G7230206075682107 INDICATOR BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL GAS PRODUCER MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036748D 51106 DID NOT FUNCTION PROPERLY. NEEDLE SLOW TO REACT AND HANGS UP AT APPROX. 10 PERCENT. REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E1GL 20011025001662001102500166NE 2001 10 25 HEEA076589 220011011G7510209062214001 ACTUATOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE STUCK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03107X 33113 STICKING. REPLACED WITH SERVICEABLE PART. 1G72 4U4 U H4SW E22EA 20011025001672001102500167SW 2001 10 25 HEEA076590 120011011G2910212076433011 TUBE BELL 412 412 1182202SW HYD SYSTEM CRACKED E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW031202T 33112 TUBE ASSY CRACKED. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001692001102500169SW 2001 10 25 HEEA076591 120011011G2510222320823119 SEAT BELT BELL 206 206L4 1182110SW COCKPIT FRAYED E HEEAK NONE O OTHER ININSP/MAINT 1 SW037074W 52033 SEAT BELT FRAYED. REPLACED WITH SERVICEABLE PART. 1G71 3U NCH2SW 20011025001702001102500170SW 2001 10 25 HEEA076592 120011011G243230126001 BATTERY BELL 412 412 1182202SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW031202T 33112 SLOW TO CHARGE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001712001102500171SW 2001 10 25 HEEA076593 120011011G771432005037 TACH GENERATOR BELL 412 412 1182202SW ENGINE FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 ENGINE OUT LIGHT WON'T GO OUT. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001722001102500172SW 2001 10 25 HEEA076594 120011011G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN WEAK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW034835 51131 WEAK AND AIRCRAFT SLOW TO START. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011025001732001102500173NE 2001 10 25 HEEA076595 220011011G7320324473511 FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE MALFUNCTIONED E HEEAK NONE J WARNING INDICATION ININSP/MAINT 1 SW032149S 36002 CAUSING TORQUE OSCILLATIONS OF 10-15 PERCENT AT A HOVER. REPLACED WITH SERVICEABLE PART. 1G72 4U4 U H4SW E22EA 20011025001742001102500174 2001 10 25 HEEA076596 420011011G25613500145NL72 LIFE VEST BELL 412 412 1182202SW EMERGENCY EQUIP LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03142PH 33150 LIFE VEST LEAKS. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001752001102500175SW 2001 10 25 HEEA076597 120011011G2422412075101101 INVERTER BELL 412 412 1182202SW ELECTRICAL INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 WORKS INTERMITTENTLY DUE TO WATER DAMAGE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001852001102500185 2001 10 25 HEEA076598 420011011G34215050010902 GYRO BELL 206 206L1 1182107SW COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW035019F 45244 ADJUSTMENT KNOB WILL NOT FUNCTION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011025001862001102500186SW 2001 10 25 HEEA076599 120011011G33407028521 LIGHT BELL 412 412 1182202SW STROBE FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032261D 33076 WILL NOT COME ON. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001882001102500188 2001 10 25 HEEA076600 420011011G34578143902240B GPS BELL 412 412 1182202SW COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0333008 36004 WHEN UNIT IS TURNED ON, POWERS UP FOR APPROX. 15 SECONDS TO ONE MINUTE THEN GOES BLANK. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001892001102500189SW 2001 10 25 HEEA076601 120011011G2497A1077V CONTACTOR BELL 206 206L3 1182108SW ELECTRICAL LOOSE E HEEAK NONE O OTHER ININSP/MAINT 1 SW034835 51131 A2 TERMINAL STUD LOOSE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011025001902001102500190 2001 10 25 HEEA076602 420011011G2340A3016R MIXER BOX BELL 412 412 1182202SW INTERPHONE MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW031202T 33112 LIGHT BLINKS ON AND OFF. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001922001102500192 2001 10 25 HEEA076603 420011011G2562ELP362D ELT BELL 412 412 1182202SW CABIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03142PH 33150 BATTERY WEAK, LOW VOLTAGE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001932001102500193 2001 10 25 HEEA076604 420011011G2562ELT910 ELT BELL 412 412 1182202SW CABIN INTERMITTENT E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03107X 33113 INTERMITTENTLY COMES ON IN FLIGHT. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001952001102500195 2001 10 25 HEEA076605 420011011G2300G4434A CONTROL HEAD BELL 412 412 1182202SW COMM SYSTEM INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032261D 33076 ON/OFF SWITCH INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025001962001102500196 2001 10 25 HEEA076606 420011011G3140MI5852013 INDICATOR BELL 412 412 1182202SW INSTRUMENT PANELFAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03107X 33113 DISPLAYS ONLY GREEN IN MAP MODE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025002002001102500200 2001 10 25 HEEA076607 420011011G3442MI5852013 INDICATOR BELL 412 412 1182202SW RADAR MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03107X 33113 DISPLAYS RANDOM RANGES. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025002022001102500202 2001 10 25 HEEA076608 420011011G3442MI585200 INDICATOR BELL 412 412 1182202SW RADAR MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03107X 33113 DISPLAYS RANDOM RANGES. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025002042001102500204SW 2001 10 25 HEEA076609 120011011G5260PHI101741 ACTUATOR BELL 412 412 1182202SW STEP FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW031202T 33112 STEP WON'T GO DOWN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025002072001102500207SW 2001 10 25 HEEA076610 120011011G6720PHI41294 CONTROL UNIT BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW035759N 33002 WORN BEARINGS. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025002092001102500209SW 2001 10 25 HEEA076611 120011012G6720406312103101 LINK BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 BEARING WORN. TO BE SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. 1G71 3U O H2SW 20011025002112001102500211SW 2001 10 25 HEEA076612 120011012G6720406312103101 LINK BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 BEARING WORN. 1G71 3U O H2SW 20011025002122001102500212SW 2001 10 25 HEEA076613 120011012G6420407312100101 BEARING 407012101111BELL 407 407 1182206SW TAIL ROTOR HUB WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH 53025 53386 WORN ELASTOMER. TO BE SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. LABOR CREDIT ACCOMPLISHED ON J0188327-WA (INVOICE AND DMR NO. 687168). 1G71 3U O H2SW 20011025002142001102500214NE 2001 10 25 HEEA076614 220011012G731402527730008 PUMP BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE FUEL FAILED E HEEAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SW032149S 36002 ENGINE OSCILLATIONS AND SEAL LEAKING. REPLACED WITH SERVICEABLE FUEL PUMP. 1G72 4U4 U H4SW E22EA 20011025002162001102500216SW 2001 10 25 HEEA076615 120011012G3040204070907101 MOTOR BELL 412 412 1182202SW WINDSHIELD WIPERFAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033893L 33006 PILOT WIPER INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025002182001102500218SW 2001 10 25 HEEA076616 120011012G5310 BEARING BELL 412 412 1182202SW STRUCTURE MISMANUFACTURED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW032298Z 33077 I/D BORE BEARING TOO SMALL. (BEARING P/N 209-031-351-001) REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025002192001102500219SW 2001 10 25 HEEA076617 120011012G7700B4429 CHIP DETECTOR 350A33200406BELL 412 412 1182202SW MAIN ROTOR MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032148K MA1154 36001 CAUSES REMOTE CAT'S EYE TO TRIP. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011025002212001102500221 2001 10 25 HEEA076618 420011003G34570110010600 GPS BOLKMS117 BK117A1 5626010EU COCKPIT FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03217UC 7152 GPS WENT BLANK. PENDING VENDOR REPAIR. 1G72 3U H13EU 20011025002222001102500222EU 2001 10 25 HEEA076622 120011004G6300350A33215300 BEARING SNIAS 350 AS350B1 8680811EU MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03856PH 3352 BEARING WORN. 1G71 3U H9EU 20011025002232001102500223EU 2001 10 25 HEEA076623 120011004G7500704A34415099 HOSE SNIAS 350 AS350B 8680801EU BLEED AIR TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03972AE88 3234 TORN. PENDING VENDOR RETURN FOR CREDIT. 1G71 3U H9EU 20011025002242001102500224EU 2001 10 25 HEEA076625 120011004G6730EMRL8RSP3C BEARING SNIAS 350 AS350B 8680801EU MAIN ROTOR SERVOWORN E HEEAK NONE O OTHER NRNOT REPORTED 1 SW03974AE 2653 WORN ROD END BEARINGS ON MAIN ROTOR SERVOS. PENDING VENDOR RETURN FOR CREDIT. 1G71 3U H9EU 20011025002252001102500225EU 2001 10 25 HEEA076628 120011004G6520350A33215001 BEARING SNIAS 350 AS350B 8680801EU TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03856PH 3352 WORN BEARING. 1G71 3U H9EU 20011025002262001102500226EU 2001 10 25 HEEA076629 120011004G772156375600010 INDICATOR SNIAS 350 AS350B 8680801EU COCKPIT WORN E HEEAK NONE O OTHER NRNOT REPORTED 1 SW03856PH 3352 ERRATIC INDICATIONS. SENT TO AMERICAN EUROCOPTER CORP. FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: RMA# R032847. 1G71 3U H9EU 20011025002282001102500228EU 2001 10 25 HEEA076630 120011004G6730704A34240015 ACCUMULATOR SNIAS 350 AS350B 8680801EU ROTO SERVO LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03974AE 2653 WILL NOT HOLD CHARGE. LEAKING. 1G71 3U H9EU 20011025002292001102500229EU 2001 10 25 HEEA076631 120011011G2435 BRUSHES SNIAS 350 AS350B 8680801EU STARTER GEN ARCED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03856PH 3352 BRUSHES ARCING WHEN STARTER IS TURNING. REPLACED WITH SERVICEABLE PART. 1G71 3U H9EU 20011025002312001102500231 2001 10 25 HEEA076632 420011011G3120B1894522282A CLOCK SNIAS 350 AS350B 8680801EU COCKPIT INACCURATE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03856PH 3352 DOES NOT KEEP CORRECT TIME. REPLACED WITH SERVICEABLE PART. 1G71 3U H9EU 20011114000012001111400001GL 2001 11 14 HEEA076800 220011016G72506898977 COUPLING ALLSN 250C 250C20J 03013GL ENGINE CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 CAE272598 N1 COUPLING HAS EXCESSIVE RUST CAUSING PITTING. 3 U E4CE 20011114000022001111400002NE 2001 11 14 HEEA076801 220011019G74219550168760 IGNITER SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03856PH 3352 CONDUCTOR WORN. SENT TO TURBOMECA FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. 1G71 3U3 U H9EU E19EU 20011114000032001111400003NE 2001 11 14 HEEA076802 120011019G77009550176740 THERMOCOUPLE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1A 60030NE ENGINE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03505PH 760505 WORN PROBES. 1G72 3U3 UNCH1NE E19EU 20011114000042001111400004NE 2001 11 14 HEEA076803 120011025G71000292005310 ENGINE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1 60030NE NACELLE LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH1306 760505 LOW POWER, LEAKING. 1G72 3U3 UNCH1NE E19EU 20011114000052001111400005SW 2001 11 14 HEEA076806 120011016G6300407340339103 BEARING BELL 407 407 1182206SW MAIN ROTOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 BEARING INNER RACE TURNING ON SHAFT JOURNAL. 1G71 3U O H2SW 20011114000062001111400006SW 2001 11 14 HEEA076807 120011016G6300407340339103 BEARING BELL 407 407 1182206SW MAIN ROTOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 BEARING INNER RACE TURNING ON SHAFT JOURNAL. 1G71 3U O H2SW 20011114000072001111400007SW 2001 11 14 HEEA076808 120011016G6300407340339103 BEARING BELL 407 407 1182206SW MAIN ROTOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 BEARING INNER RACE TURNING ON SHAFT JOURNAL. 1G71 3U O H2SW 20011114000082001111400008SW 2001 11 14 HEEA076809 120011016G6300407340339103 BEARING BELL 407 407 1182206SW MAIN ROTOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 BEARING INNER RACE TURNING ON SHAFT JOURNAL. 1G71 3U O H2SW 20011114000092001111400009SW 2001 11 14 HEEA076810 120011016G6510407040302107 DRIVE SHAFT BELL 407 407 1182206SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH1903 53398 BEARING INNER RACE TURNING ON SHAFT JOURNAL. 1G71 3U O H2SW 20011114000102001111400010SW 2001 11 14 HEEA076811 120011016G6510407040302107 DRIVE SHAFT BELL 407 407 1182206SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH1299 53398 BEARING INNER RACE TURNING ON SHAFT JOURNAL. 1G71 3U O H2SW 20011114000112001111400011SW 2001 11 14 HEEA076812 120011016G6510407040302103 DRIVE SHAFT BELL 407 407 1182206SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 BEARING INNER RACE TURNING ON SHAFT JOURNAL. 1G71 3U O H2SW 20011114000132001111400013SW 2001 11 14 HEEA076813 120011016G6510407040302107 DRIVE SHAFT BELL 407 407 1182206SW TAIL ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH1597 53390 BEARING INNER RACE TURNING ON SHAFT JOURNAL. 1G71 3U O H2SW 20011114000152001111400015SW 2001 11 14 HEEA076814 120011016G6510 SHAFT BELL 407 407 1182206SW COOLER BLOWER FAILED E HEEAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SW034999 53323 IN CRUISE, AIRCRAFT DEVELOPED SEVERE VERTICAL VIBRATION. FOUND FORWARD BEARING ON NR 2 TAIL ROTOR OIL COOLER BLOWER SHAFT FAILURE. 1G71 3U O H2SW 20011114000172001111400017SW 2001 11 14 HEEA076815 120011017G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0331821 51076 RECEIVED FROM PARTS. WEAK FROM INSTALLATION AND FAILED COMPLETELY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000182001111400018SW 2001 11 14 HEEA076816 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN FAILED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW033116P 51530 WILL NOT HOLD CHARGE. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000202001111400020SW 2001 11 14 HEEA076817 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW034180F TOO WEAK TO START AIRCRAFT. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000272001111400027NE 2001 11 14 HEEA076820 220011018G732132448891 FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE FLUCTUATES E HEEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW032260810321 33075 AFTER DEPARTURE, NR 1 ENGINE STARTED TO HAVE N1 FLUCTUATIONS. REPLACED FUEL CONTROL. 1G72 4U4 U H4SW E22EA 20011114000282001111400028SW 2001 11 14 HEEA076821 120011018G243232007001 BATTERY BELL 206 206L1 1182107SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03406EH 45183 WEAK BATTERY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000292001111400029SW 2001 11 14 HEEA076822 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03206LS 51070 WEAK BATTERY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000312001111400031SW 2001 11 14 HEEA076823 120011018G243232007001 BATTERY BELL 206 206L1 1182107SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW035745S 45491 DEAD BATTERY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000322001111400032SW 2001 11 14 HEEA076824 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW038593X 51509 WEAK BATTERY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000342001111400034SW 2001 11 14 HEEA076825 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0354641 51184 WEAK BATTERY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000352001111400035SW 2001 11 14 HEEA076826 120011018G243232007001 BATTERY BELL 206 206L1 1182107SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW032777D 45299 DEAD BATTERY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000462001111400046SW 2001 11 14 HEEA076827 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW038587X 51464 WEAK BATTERY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000472001111400047SW 2001 11 14 HEEA076828 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW036610C 51425 WEAK BATTERY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000482001111400048SW 2001 11 14 HEEA076829 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0341791 51465 WEAK BATTERY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000502001111400050SW 2001 11 14 HEEA076830 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW036161A 51611 WEAK BATTERY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000512001111400051SW 2001 11 14 HEEA076831 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN FAILED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0331077 51520 WON'T TAKE A CHARGE. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000522001111400052SW 2001 11 14 HEEA076832 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0341791 51465 DEAD BATTERY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000542001111400054SW 2001 11 14 HEEA076833 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03 WEAK BATTERY. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000552001111400055SW 2001 11 14 HEEA076834 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN FAILED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03141BH 51303 WON'T TAKE CHARGE. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000572001111400057SW 2001 11 14 HEEA076835 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW036160Y 51609 DEAD. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000592001111400059SW 2001 11 14 HEEA076836 120011018G243232007001 BATTERY BELL 206 206L1 1182107SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW031078D 45397 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000612001111400061SW 2001 11 14 HEEA076837 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW03141BH 51303 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000662001111400066SW 2001 11 14 HEEA076838 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW036161A 51611 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000672001111400067SW 2001 11 14 HEEA076839 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0341791 51465 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000682001111400068SW 2001 11 14 HEEA076840 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0354641 51184 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000692001111400069SW 2001 11 14 HEEA076841 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW034835 51131 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000712001111400071SW 2001 11 14 HEEA076842 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW036251Y 51556 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000722001111400072SW 2001 11 14 HEEA076843 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW034835 51131 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000732001111400073SW 2001 11 14 HEEA076844 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW036160Z 51610 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000752001111400075SW 2001 11 14 HEEA076845 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW036160Z 51610 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000762001111400076SW 2001 11 14 HEEA076846 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW038591X 51495 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000802001111400080SW 2001 11 14 HEEA076847 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN OVERHEATED E HEEAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW0381SP 51029 BATTERY HOT LIGHT. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000932001111400093SW 2001 11 14 HEEA076848 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0332041 51539 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000942001111400094SW 2001 11 14 HEEA076849 120011018G243232007001 BATTERY BELL 206 206L3 1182108SW MAIN DISCHARGED E HEEAO OTHER L NO TEST NRNOT REPORTED 1 SW0341791 51465 WEAK. REPLACED WITH SERVICEABLE BATTERY. 1G71 3U H2SW 20011114000952001111400095SW 2001 11 14 HEEA076850 120011019G2840407362005103 SWITCH BELL 407 407 1182206SW FUEL INDICATION MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03417PH 53038 LOW LEVEL LIGHT STAYS ON. 1G71 3U O H2SW 20011114000962001111400096SW 2001 11 14 HEEA076851 120011019G6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 UNIVERSAL WORN. 1G71 3U O H2SW 20011114000982001111400098SW 2001 11 14 HEEA076852 120011019G3212206373902103 RELIEF VALVE BELL 407 407 1182206SW MLG MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03404PH 53188 RELIEF VALVE KEPT RELEASING PRESSURE DOWN TO 2750 PSI. 1G71 3U O H2SW 20011114000992001111400099SW 2001 11 14 HEEA076853 120011019G3212206050247135 COVER BELL 407 407 1182206SW MLG FLOAT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 END COVERS COMING UNSEWN. 1G71 3U O H2SW 20011114001132001111400113SW 2001 11 14 HEEA076854 120011019G3212206050247138 COVER BELL 407 407 1182206SW MLG FLOAT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 END COVERS COMING UNSEWN. 1G71 3U O H2SW 20011114001142001111400114SW 2001 11 14 HEEA076856 120011019G2510407370720101 SEAT BELT BELL 407 407 1182206SW COCKPIT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 SHOULDER STRAP FRAYED FROM WEAR. 1G71 3U O H2SW 20011114001152001111400115SW 2001 11 14 HEEA076857 120011019G3212206050247138 COVER BELL 407 407 1182206SW MLG FLOAT DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 DETERIORATED. 1G71 3U O H2SW 20011114001172001111400117SW 2001 11 14 HEEA076858 120011019G3212212073905001 GAUGE BELL 407 407 1182206SW MLG FLOAT DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 PRESSURE GAUGE HAS MOISTURE AND RUST. 1G71 3U O H2SW 20011114001212001111400121SW 2001 11 14 HEEA076859 120011019G7810407063001101 EXHAUST STACK BELL 407 407 1182206SW ENGINE CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 EXHAUST STACK CRACKED. 1G71 3U O H2SW 20011114001222001111400122SW 2001 11 14 HEEA076860 120011019G6720406312103101 LINK BELL 407 407 1182206SW TAI ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 LINK HAS WORN BEARINGS. 1G71 3U O H2SW 20011114001252001111400125SW 2001 11 14 HEEA076862 120011019G2822206076030111 PUMP BELL 407 407 1182206SW FUEL BOOST WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH864 53401 PUMP SHAFT SPLINE WEAR. 1G71 3U O H2SW 20011114001262001111400126SW 2001 11 14 HEEA076863 120011019G6300407010206103 SPRING BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03721PH2952 53278 WORN BEARINGS. 1G71 3U O H2SW 20011114001272001111400127SW 2001 11 14 HEEA076864 120011019G6710406010426101 LINK BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH2025 53400 LINK HAS WORN BUSHINGS. 1G71 3U O H2SW 20011114001402001111400140SW 2001 11 14 HEEA076865 120011019G6710406010426101 LINK BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH2025 53400 LINK HAS WORN BUSHINGS. 1G71 3U O H2SW 20011114001422001111400142SW 2001 11 14 HEEA076866 120011019G6710406010426101 LINK BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 LINK HAS WORN BUSHINGS. 1G71 3U O H2SW 20011114001432001111400143SW 2001 11 14 HEEA076867 120011019G6710406010426101 LINK BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH2025 53400 LINK HAS WORN BUSHINGS. 1G71 3U O H2SW 20011114001452001111400145SW 2001 11 14 HEEA076869 120011019G2840407375016103 SIGNAL COND UNIT BELL 407 407 1182206SW FUEL INDICTION MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03495PH 53397 LOW LEVEL LIGHT WILL NOT GO OUT. 1G71 3U O H2SW 20011114001462001111400146SW 2001 11 14 HEEA076870 120011019G3110407375005101 INDICATOR BELL 407 407 1182206SW XMSN OIL TEMP INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03457PH 53147 TRANSMISSION OIL TEMP INDICATOR INOPERATIVE. 1G71 3U O H2SW 20011114001472001111400147SW 2001 11 14 HEEA076871 120011019G2840407375016103 SIGNAL COND UNIT BELL 407 407 1182206SW FUEL INDICATION MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03495PH 53397 LEVEL LIGHT STAYING ON WITH 550 POUNDS OF FUEL. 1G71 3U O H2SW 20011114001482001111400148SW 2001 11 14 HEEA076872 120011022G3210206323006 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 MLG CROSSTUBE CORRODED. 1G71 3U H2SW 20011114001522001111400152SW 2001 11 14 HEEA076873 120011023G6710406010429101 PIN BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 PIN WORN. 1G71 3U O H2SW 20011114001582001111400158SW 2001 11 14 HEEA076874 120011023G6300406040316101 ADAPTER BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 ADAPTER HAS WORN SPLINES. 1G71 3U O H2SW 20011114001592001111400159SW 2001 11 14 HEEA076875 120011023G6710406010429101 PIN BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH 53038 PIN WORN. 1G71 3U O H2SW 20011114001602001111400160SW 2001 11 14 HEEA076878 120011023G6321206340301103 BRAKE BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03467PH3152 53142 ROTOR BRAKE IS DAMAGED AND LEAKS. 1G71 3U O H2SW 20011114001612001111400161SW 2001 11 14 HEEA076879 120011023G6321 HOUSING BELL 407 407 1182206SW ROTOR BRAKE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH1638 53378 EXCESSIVE HOUSING WEAR. 1G71 3U O H2SW 20011114001622001111400162SW 2001 11 14 HEEA076880 120011023G6230406010401115 SWASHPLATE BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03447PH 53114 DUPLEX BEARING WORN. 1G71 3U O H2SW 20011115000012001111500001SW 2001 11 15 HEEA076881 120011023G6710406010428109 HUB BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH646 53038 HUB IS WORN. 1G71 3U O H2SW 20011115000082001111500008SW 2001 11 15 HEEA076884 120011024G3110407375003107 INDICATOR BELL 407 407 1182206SW TORQUE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03404PH 53188 GOES TO TEST IN FLIGHT. 1G71 3U O H2SW 20011115000092001111500009SW 2001 11 15 HEEA076885 120011024G6320407340339101 BEARING PHIPBH40701 BELL 407 407 1182206SW COOLER BLOWER ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03742PH44 PHI0039 53461 ROUGH AND NOISY. 1G71 3U O H2SW 20011115000102001111500010SW 2001 11 15 HEEA076886 120011024G6320206040156001 SEAL BELL 407 407 1182206SW M/R GEARBOX LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03417PH 53038 SEAL HAS OIL LEAK. 1G71 3U O H2SW 20011115000162001111500016SW 2001 11 15 HEEA076887 120011024G3212206050247132 COVER BELL 407 407 1182206SW MLG FLOAT TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH 53398 TORN. 1G71 3U O H2SW 20011115000172001111500017SW 2001 11 15 HEEA076888 120011024G3212206050247138 COVER BELL 407 407 1182206SW MLG FLOAT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03492PH 53390 WORN. TO BE SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. 1G71 3U O H2SW 20011115000182001111500018SW 2001 11 15 HEEA076889 120011024G3212206050247138 FLOAT BELL 407 407 1182206SW MLG FLOAT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW038595X 53267 WORN. 1G71 3U O H2SW 20011115000192001111500019SW 2001 11 15 HEEA076890 120011024G6510206061432121 HOUSING BELL 407 407 1182206SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034999 53323 BLOWER HOUSING CRACKED. 1G71 3U O H2SW 20011115000202001111500020SW 2001 11 15 HEEA076891 120011024G6510206061432121 HOUSING BELL 407 407 1182206SW BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03723PH 53283 BLOWER HOUSING CRACKED. 1G71 3U O H2SW 20011115000222001111500022SW 2001 11 15 HEEA076892 120011024G2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03723PH 96240 53283 STARTER GENERATOR HAS WORN BRUSHES. 1G71 3U O H2SW 20011115000252001111500025SW 2001 11 15 HEEA076893 120011024G6730206076062107 SERVO BELL 407 407 1182206SW CYCLIC WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW034999 53323 PISTON ROD END BEARING WORN. 1G71 3U O H2SW 20011115000262001111500026SW 2001 11 15 HEEA076894 120011024G6321206340301103 BRAKE BELL 407 407 1182206SW ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW033193E2496 53276 FOUND EXCESSIVE WEAR ON HOUSING, BRAKE PAD BOLT RETAINER HOLES AND PAD RETAINER BOLTS. OVERHAULED, MODIFIED, TESTED AND RETURNED TO AIRCRAFT. 1G71 3U O H2SW 20011115000282001111500028SW 2001 11 15 HEEA076895 120011024G3212212073905001 GAUGE BELL 407 407 1182206SW FLOAT PRESSURE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 FOGGED OVER. CANNOT READ AMOUNT OF PRESSURE IN FLOAT BOTTLE. 1G71 3U O H2SW 20011115000292001111500029SW 2001 11 15 HEEA076896 120011024G3212212073905001 GAUGE BELL 407 407 1182206SW FLOAT PRESSURE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03467PH 53142 NUMBERED DIAL MOVES. UNABLE TO VERIFY EXACT AMOUNT OF PRESSURE IN FLOAT BOTTLE. T 1G71 3U O H2SW 20011115000322001111500032GL 2001 11 15 HEEA076897 220011024G753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 SW034999 53323 LOW POWER ENGINE. IN SHOP REPAIR. 1G71 3U3 UO H2SW E1GL 20011115000362001111500036SW 2001 11 15 HEEA076898 120011024G6230406010401117 SWASHPLATE BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 GREASE LEAKING FROM TOP SEAL. 1G71 3U O H2SW 20011115000372001111500037SW 2001 11 15 HEEA076899 120011024G6520406040400117 GEARBOX BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH 53378 OUTPUT SHAFT SPLINE WORN. REPLACED WITH SERVICEABLE T/R GEARBOX ASSEMBLY. 1G71 3U O H2SW 20011115000492001111500049SW 2001 11 15 HEEA076900 120011024G6310406040500123B FREEWHEEL UNIT BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW038595X 53267 LEAKING FROM SEAL. REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20011115000502001111500050SW 2001 11 15 HEEA076901 120011024G6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 RED MAIN ROTOR P/C LINK BEARING WORN WITH PLAY. 1G71 3U O H2SW 20011115000512001111500051SW 2001 11 15 HEEA076902 120011024G6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR LOOSE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03498PH 53399 BEARING HAD RADIAL PLAY. 1G71 3U O H2SW 20011115000552001111500055SW 2001 11 15 HEEA076903 120011024G6710406310407101 SEAL 406010401115BELL 407 407 1182206SW SWASHPLATE LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03406PH A707 53198 UPPER BEARING GREASE SEAL LEAKING ON UNIBALL. 1G71 3U O H2SW 20011115000562001111500056SW 2001 11 15 HEEA076904 120011024G6230406310411101 BOOT BELL 407 407 1182206SW M/R MAST TORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH 53397 MAST BOOT TORN. 1G71 3U O H2SW 20011115000582001111500058SW 2001 11 15 HEEA076905 120011024G6710407001523101 IDLER ASSY BELL 407 407 1182206SW M/R CONTROL WORN E K NONE O OTHER ININSP/MAINT 1 SW03724PH 53327 TAIL ROTOR CONTROL IDLER ASSY HAS BEARINGS WORN. 1G71 3U O H2SW 20011115000592001111500059SW 2001 11 15 HEEA076906 120011024G6420407012101111 HUB BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH1765 53378 WORN ELASTOMERIC BEARING. TO BE SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. 1G71 3U O H2SW 20011115000612001111500061SW 2001 11 15 HEEA076907 120011024G6797407076508103 HARNESS BELL 407 407 1182206SW INSTRUMENT PANELFAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03457PH 53147 PEDAL STOP SWITCH DAMAGED BY INTERFERENCE WITH INSTRUMENT PANEL FRAME. 1G71 3U O H2SW 20011115000632001111500063SW 2001 11 15 HEEA076908 120011024G5260407301110 STEP BELL 407 407 1182206SW FUSELAGE CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03492PH 53390 CORRODED AT BRACKET MOUNT BOLT HOLES. REPLACED WITH SERVICEABLE STEP. 1G71 3U O H2SW 20011115000642001111500064SW 2001 11 15 HEEA076909 120011024G6220407310101101 BEARING 407010100115BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03501PH A436 53401 SHEAR BEARINGS WORN AND SEPARATING. TO BE SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. 1G71 3U O H2SW 20011115000672001111500067SW 2001 11 15 HEEA076910 120011024G6220407310104103 SPRING 407010150105BELL 407 407 1182206SW FRAHM ASSY BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03501PH A560 53401 SPRINGS FOUND BROKEN. 1G71 3U O H2SW 20011115000682001111500068SW 2001 11 15 HEEA076911 120011024G6320407340339101 BEARING BELL 407 407 1182206SW MAIN ROTOR OVERHEATED E HEEAK NONE M OVER TEMP ININSP/MAINT 1 SW03404PH 53188 BEARING OVERHEATED. 1G71 3U O H2SW 20011115000692001111500069SW 2001 11 15 HEEA076912 120011024G6510407340340103 DISC PACK BELL 407 407 1182206SW TAIL ROTOR FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034999 53323 FORWARD BLOWER SHAFT BEARING FAILED. 1G71 3U O H2SW 20011115000702001111500070 2001 11 15 HEEA076913 420011024G3120M803B205VBATT LIGHT BELL 407 407 1182206SW CLOCK INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03498PH 53399 HALF OF INDICATOR BACKLIGHT INOPERATIVE. 1G71 3U O H2SW 20011115000712001111500071SW 2001 11 15 HEEA076914 120011024G2400MS24509A10 SWITCH BELL 407 407 1182206SW ELECTRICAL DIST BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW038595X 53267 BROKEN INTERNALLY. REPLACED WITH SERVICEABLE SWITCH. 1G71 3U O H2SW 20011115000932001111500093SW 2001 11 15 HEEA076918 120011024G6200206011135105 BOLT BELL 206 206L3 1182108SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 NICKS IN THREADED AREA. 1G71 3U H2SW 20011115000942001111500094SW 2001 11 15 HEEA076919 120011026G6700206011732103 SLEEVE BELL 407 407 1182206SW CONTROL TUBE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 PART IS WORN EXCESSIVELY. 1G71 3U O H2SW 20011115000952001111500095SW 2001 11 15 HEEA076920 120011026G6220 BEARING 407010100115BELL 407 407 1182206SW M/R HUB SHEARED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH A436 53401 SHEARING BEARINGS SEPARATION. 1G71 3U O H2SW 20011115000962001111500096SW 2001 11 15 HEEA076921 120011026G6420407012101111 HUB BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03741PH1022 53457 WORN BEARING, CLICKING NOISE. PARTS AND LABOR CREDIT ACCOMPLISHED ON J0189948-WA. 1G71 3U O H2SW 20011115000972001111500097SW 2001 11 15 HEEA076922 120011026G6510407340339103 BEARING 407040302107BELL 407 407 1182206SW TAIL ROTOR ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH A1871 53386 BEARING ROUGH. 1G71 3U O H2SW 20011115000982001111500098SW 2001 11 15 HEEA076923 120011026G6510407340339103 BEARING 407040302107BELL 407 407 1182206SW TAIL ROTOR ROUGH E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH A1875 53386 ROUGH. 1G71 3U O H2SW 20011115000992001111500099SW 2001 11 15 HEEA076924 120011026G6300407340339101 BEARING BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 BEARING WORN. 1G71 3U O H2SW 20011115001082001111500108SW 2001 11 15 HEEA076926 120011026G7931209070262101 INDICATOR BELL 412 412 1182202SW OIL PRESSURE READS HIGH E HEEAO OTHER N FALSE WARNING CLCLIMB 1 SW0333008 36004 AFTER TAKEOFF, PILOT NOTED NR 2 ENGINE OIL PRESSURE WAS INDICATING HIGH. REPLACED OIL TEMP/PRESS INDICATOR. 1G72 4U H4SW 20011115001102001111500110EU 2001 11 15 HEEA076927 120011019G6220350A31191600 STARFLEX SNIAS 350 AS350B 8680801EU MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03970AE317 3235 CRACKED SPHERICAL STOP CUT OUT AREA, LOWER AFT AS MARKED. 1G71 3U H9EU 20011115001122001111500112 2001 11 15 HEEA076928 420011019G3120B1894522282A CLOCK SNIAS 350 AS350B 8680801EU COCKPIT INACCURATE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03856PH 3352 DOES NOT KEEP CORRECT TIME. 1G71 3U H9EU 20011115001132001111500113 2001 11 15 HEEA076936 420011030G3416066104800 ALTIMETER SKRSKYS76 S76A 8143006NE COCKPIT ERRATIC E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03911MJ 760231 RT WAS CAUSING ERRATIC READING ON APPROACH. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20011115001142001111500114NE 2001 11 15 HEEA076937 120011031G64107610105101041 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031546G8350 760076 CORROSION ON BOX BEAM AND TRAILING IS SPLIT OPEN ON PADDLE "B". PENDING VENDOR REPAIR. 1G72 3U H1NE 20011115001152001111500115NE 2001 11 15 HEEA076938 120011031G62207610208500046 SPINDLE SKRSKYS76 S76A 8143006NE MAIN ROTOR BINDING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K 760047 DROOP STOP BINDS UP WHEN INSTALLED. FOUND WHEN TORQUEING UP SPINDLE. A BIND PREVENTS THE DROOP STOP FROM RETURNING TO STATIC POSITION AT SHUTDOWN. IT IS FREE TO MOVE WHEN NOT INSTALLED. PENDING VENDOR REPAIR. 1G72 3U H1NE 20011115001162001111500116NE 2001 11 15 HEEA076939 120011031G62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03760PH 760078 OUTER DOUBLER ON LOWER SIDE CRACKED AND HAS "C" CHANNEL DEBONDED. PENDING VENDOR REPAIR. 1G72 3U H1NE 20011115001182001111500118NE 2001 11 15 HEEA076940 120011031G62107615009043054 TIP CAP SKRSKYS76 S76C 8143008NE MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03505PH 760505 FIBERGLASS SKIN NEAR THE TRAILING EDGE IS CRACKED AND HAS SOME SEPARATION NEXT TO THE ABRASION STRIP. PENDING VENDOR REPAIR. 1G72 3U NCH1NE 20011115001192001111500119NE 2001 11 15 HEEA076941 120011031G62107615009100041A BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545K12595 760047 LEADING EDGE TITANIUM STRIP HAS A COMPLETE CHORDWISE CRACK WITH MULTIPLE BRANCH WHICH EXTENDS BEYOND LIMITS. PENDING VENDOR REPAIR. 1G72 3U H1NE 20011115001202001111500120NE 2001 11 15 HEEA076942 120011031G62107615009100042A BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ14090 760231 TRAILING EDGE CRACKED JUST INBOARD OF TRIM TAB. REPLACED WITH SERVICEABLE BLADE. 1G72 3U H1NE 20011115001212001111500121NE 2001 11 15 HEEA076943 120011031G62107615009100053 BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911MJ5266 760231 TRAILING EDGE DAMAGE AT AREA OF P/N - S/N STENCIL. REPLACED WITH SERVICEABLE BLADE. 1G72 3U H1NE 20011115001222001111500122NE 2001 11 15 HEEA076944 120011031G63207635109045102 GEAR SKRSKYS76 S76A 8143006NE M/R GEARBOX MISMANUFACTURED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 RIVET NOT INSTALLED IN GEAR. RIVET REQUIRED TO PREVENT OIL FROM LEAKING. PENDING VENDOR REPAIR. 1G72 3U H1NE 20011115001232001111500123NE 2001 11 15 HEEA076945 120011031G63207635109500043 TRANSMISSION SKRSKYS76 S76A 8143006NE MAIN ROTOR MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW03911MJ10333 760231 CHIP LIGHT ON LANDING. INSPECTED AND FOUND A 1/2" BY 3/16" PIECE OF A GEAR TOOTH ON THE LEFT CHIP PLUG. REPLACED WITH SERVICEABLE ASSEMBLY. 1G72 3U H1NE 20011115001252001111500125NE 2001 11 15 HEEA076946 120011031G33407655002005101 LIGHT SKRSKYS76 S76A 8143006NE SEARCH LIGHT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03792CH 760193 WILL NOT MOVE UP OR DOWN. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20011115001272001111500127NE 2001 11 15 HEEA076947 120011031G67307665009803106 POWERPACK SKRSKYS76 S76A 8143006NE SERVO SYSTEM CRACKED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03911MJ 760231 POWER PACK HOUSING CRACKED AT DRAIN FITTING. PENDING VENDOR REPAIR. 1G72 3U H1NE 20011115001302001111500130GL 2001 11 15 HEEA076948 220011031G74219550166530 LEAD SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL IGNITER FRAYED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03760PH 760078 FRAYED AND WORN. REPLACED WITH SERVICEABLE PART. 1G72 3U3 U H1NE E1GL 20011115001322001111500132GL 2001 11 15 HEEA076949 220011031G74219550166670 IGNITER SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE FRAYED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03760PH 760078 FRAYED AND WORN. REPLACED WITH SERVICEABLE PART. 1G72 3U3 U H1NE E1GL 20011115001332001111500133GL 2001 11 15 HEEA076950 220011031G74219550168770 IGNITER SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ENGINE DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03760PH 760078 INOPERATIVE - WILL NOT FIRE. CENTER ELETRODE CAME OUT. REPLACED WITH SERVICEABLE PART. 1G72 3U3 U H1NE E1GL 20011115001342001111500134NE 2001 11 15 HEEA076951 120011031G74109550176020 GENERATOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL IGNITER CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03760PH 760078 CORROSION. REPLACED WITH SERVICEABLE PART. 1G72 3U3 U H1NE E1GL 20011115001352001111500135 2001 11 15 HEEA076952 420011031G2340A3016W INTERPHONE SKRSKYS76 S76A 8143006NE COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035435V 760158 COMM NR 1 TRANSMITS GARBLED. REPLACED WITH SERVICEABLE PART. 1G72 3U H1NE 20011115001362001111500136 2001 11 15 HEEA076953 420011031G34427007700613 INDICATOR SKRSKYS76 S76C 8143008NE RADAR SYSTEM INTERMITTENT E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03505PH 760505 INTERMITTENTLY DISPLAYS FAIL. PENDING VENDOR REPAIR. 1G72 3U NCH1NE 20011115001372001111500137 2001 11 15 HEEA076954 420011031G2350AA34300 CONNECTOR SKRSKYS76 S76A 8143006NE RADIO FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03913UK 760276 CANNOT PROGRAM MOTOROLA MCS 2000 RADIO. PENDING VENDOR REPAIR. 1G72 3U H1NE 20011115001392001111500139 2001 11 15 HEEA076955 420011031G3457N0002000 GPS COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 NEW UNIT DOES NOT GIVE GPS POSITION AND TRANSMITS INTERMITTENTLY WITH CDU. TO BE SENT TO VENDOR FOR WARRANTY REPAIR. 20011116000472001111600047EU 2001 11 16 HEEA076956 120011101G71000292005220 ENGINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE NACELLE MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW03404665392 3004 ENGINE MAKING METAL. 1G71 3U3 U H9EU E19EU 20011116000502001111600050 2001 11 16 HEEA076957 420011030G34570110005400 GPS BELL 206 206L1 1182107SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035007Q 45187 TAKES AN EXTENDED PERIOD OF TIME TO ACQUIRE SATTELITES. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011116000512001111600051 2001 11 16 HEEA076958 420011030G2312064100900 TRANSCEIVER BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW032261D 33076 TRANSMITS WEAK AND GARBLED. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116000532001111600053 2001 11 16 HEEA076959 420011030G2312064102300 TRANSCEIVER BELL 412 412 1182202SW COCKPIT INTERMITTENT E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03107X 33113 UNIT CUTS OUT IN FLIGHT INTERMTTENTLY. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116000542001111600054 2001 11 16 HEEA076960 420011030G2312064102300 TRANSCEIVER BELL 412 412 1182202SW COCKPIT WEAK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036559Z 36019 RECEIVES VERY WEAK/ TRANSMITS GOOD. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116000552001111600055 2001 11 16 HEEA076961 420011030G2312064105430 TRANSCEIVER BELL 206 206L3 1182108SW COCKPIT INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0330KH 51527 INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011116000562001111600056 2001 11 16 HEEA076962 420011030G3455066104701 TRANSCEIVER BELL 412 412 1182202SW ADF SYSTEM MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032261D 33076 WILL NOT PAINT AND NO AUDIO. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116000582001111600058 2001 11 16 HEEA076963 420011030G3452066106200 TRANSPONDER BELL 206 206L3 1182108SW COCKPIT INTERFERENCE E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331821 51076 TRANSPONDER SQUAWKING 24000 FEET. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011116000602001111600060 2001 11 16 HEEA076964 420011030G3452066107100 TRANSPONDER BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW037128R 36007 INOPERATIVE, WILL NOT TRANSMIT. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011116000612001111600061 2001 11 16 HEEA076965 420011030G3452066107100 TRANSPONDER BELL 214 214ST 1182106SW COCKPIT INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW0359806 28140 INOPERATIVE. PENDING VENDOR REPAIR. 2G72 4U H10SW 20011116000662001111600066 2001 11 16 HEEA076966 420011030G3100071119208 CONTROL SWITCH BELL 412 412 1182202SW COCKPIT FAILED E HEEAO OTHER O OTHER ININSP/MAINT 1 SW032148K 36001 STATION KNOB WHEN TURN TO RIGHT IT SPRINGS BACK TO LEFT. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116000672001111600067 2001 11 16 HEEA076967 420011030G3400071121525 CONTROL UNIT BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 SEVERAL SEGMENTS INOPERATIVE. REPLACED WITH SERVICEABLE PART. COULD NOT VERIFY COMPLAINT. BENCH CHECK GOOD. 1G72 4U H4SW 20011116000732001111600073 2001 11 16 HEEA076968 420011030G2312071121525 CONTROL UNIT BELL 412 412 1182202SW COCKPIT INTERMITTENT E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 DIGITS INTERMITTENTLY LOSE PART OF NUMBERS. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116000822001111600082 2001 11 16 HEEA076969 420011030G3454071121627 CONTROL UNIT BELL 412 412 1182202SW NAVIGATION FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032148K 36001 WHEN SUN HITS KFS, IT DOES NOT GET BRIGHT. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116000832001111600083SW 2001 11 16 HEEA076970 120011030G2422 INVERTER BELL 412 412 1182202SW ELECTRIAL FAILED E HEEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03142PH 33150 NR 1 INVERTER DROPPED OFF LINE AND ELECTRICAL FUMES WERE NOTED BY PILOT. FOUND BURNED WIRE IN WINDSHIELD POST COVER AT TOP OF POST. 1G72 4U H4SW 20011116000842001111600084SW 2001 11 16 HEEA076971 120011030G2820AE89411M VENT BELL 412 412 1182202SW FUEL SYSTEM LEAKING E HEEAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW0322608 33075 HAD STRONG FUEL ODOR IN COCKPIT. FOUND A SMALL AMOUNT OF FUEL HAD SEEPED THROUGH THE RT EXTERNAL TANK VENT DUE TO HIGH FUEL LEVEL AND THE ATTITUDE OF THE AIRCRAFT. 1G72 4U H4SW 20011116000852001111600085SW 2001 11 16 HEEA076972 120011031G3212206030104023 FITTING BELL 206 206L3 1182108SW MLG FLOAT CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 PART IS CHAFED. REPLACED WITH SERVICEABLE FITTING. 1G71 3U H2SW 20011116000862001111600086SW 2001 11 16 HEEA076973 120011031G6300206033501004 FITTING BELL 206 206L3 1182108SW MAIN ROTOR CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0354641 51184 FITTING IS CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011116000882001111600088SW 2001 11 16 HEEA076974 120011031G6320206033518007 STOP BELL 206 206L3 1182108SW M/R GEARBOX DETERIORATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0331077 51520 DETERIORATION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011116000892001111600089SW 2001 11 16 HEEA076975 120011031G3210206052105013 STRAP BELL 206 206L3 1182108SW MLG CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW036251X 51552 CORROSION. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011116000902001111600090SW 2001 11 16 HEEA076976 120011031G6710206076062003 CYLINDER BELL 206 206L3 1182108SW CYCLIC LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW033116L 51529 LEAKING BEYOND LIMITS ON END CAP SIDE OF SERVO. PENDING VENDOR REPAIR. 1G71 3U H2SW 20011116000912001111600091SW 2001 11 16 HEEA076977 120011031G7800212061117001 TUBE BELL 412 412 1182202SW EXHAUST WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 WORN BEARINGS. REPLACED WITH SERVICEABLE TUBE ASSY. 1G72 4U H4SW 20011116000932001111600093SW 2001 11 16 HEEA076978 120011031G6710214001347005 ACTUATOR BELL 412 412 1182202SW AUTO FLIGHT INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 STICKS INTERMITTENTLY. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011116000962001111600096 2001 11 16 HEEA076979 420011031G3424214075244001 GYRO BELL 412 412 1182202SW COCKPIT INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032148K 36001 CO-PILOT RATE OF TURN NEEDLE DOES NOT MOVE. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011116000982001111600098SW 2001 11 16 HEEA076980 120011031G6220222310504101 BEARING BELL 230 230 1182149SW MAIN ROTOR DELAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911RC 23037 DELAMINATION. PENDING VENDOR REPAIR. 1G72 3U NCH9SW 20011116001022001111600102SW 2001 11 16 HEEA076981 120011031G243523032048 STARTER GEN BELL 212 212 1181420SW ENGINE FAILED E HEEAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03102PH 30899 RED GLOW WAS OBSERVED IN THE STARTER GENERATOR FOLLOWED BY SMOKE, STARTER NEVER ENGAGED. REPLACED WITH SERVICEABLE PART. 1G71 4U H4SW 20011116001032001111600103NE 2001 11 16 HEEA076982 220011031G732325249994 GOVERNOR BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE OSCILLATES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 ENGINE OSCILLATES AT 100 PERCENT ON GROUND. REPLACED WITH SERVICEABLE PART. 1G72 4U4 U H4SW E22EA 20011116001042001111600104SW 2001 11 16 HEEA076983 120011031G28222C271 CARTRIDGE BELL 206 206L1 1182107SW BOOST PUMP FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035007N 45184 LT BOOST PUMP FUEL PRESSURE DROPPED TO ZERO, LT BOOST PUMP LIGHT ILLUMINATED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011116001092001111600109NE 2001 11 16 HEEA076984 220011031G7320324473514 FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE ENGINE SURGES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW032149S 36002 ENGINE SURGING AT 100 PERCENT NR. REPLACED WITH SERVICEABLE PART. 1G72 4U4 U H4SW E22EA 20011116001112001111600111SW 2001 11 16 HEEA076985 120011031G2841393008047 INDICATOR BELL 212 212 1181420SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035736J 31140 UNIT READ ZERO. PENDING VENDOR REPAIR. 1G71 4U H4SW 20011116001122001111600112SW 2001 11 16 HEEA076986 120011031G6710412001300105 BELLCRANK BELL 412 412 1182202SW MAIN ROTOR INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 BEARING WILL NOT ROTATE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116001132001111600113SW 2001 11 16 HEEA076987 120011031G6220412001900101 SUPPORT BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 WORN BEARING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116001152001111600115SW 2001 11 16 HEEA076988 120011031G6230412010405109 LINK BELL 412 412 1182202SW MAIN ROTOR DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031202T 33112 SPUN BEARING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116001162001111600116SW 2001 11 16 HEEA076989 120011031G5260412076620101 UNIVERSAL BELL 412 412 1182202SW STEPS WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035759N 33002 WORN BEARING. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116001172001111600117SW 2001 11 16 HEEA076990 120011031G240051539002N CONTROL UNIT BELL 412 412 1182202SW ELELCTRICAL FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 WON'T HOLD PARALLEL VOLTAGE. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011116001192001111600119SW 2001 11 16 HEEA076991 120011031G243051509002R CONTROL UNIT BELL 412 412 1182202SW GENERATOR FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03142PH 33150 CAUSES GENERATOR TO KICK OFF LINE. PENDING VENDOR REPAIR. 1G72 4U H4SW 20011116001202001111600120 2001 11 16 HEEA076992 420011031G34168503S20LW ALTIMETER BELL 412 412 1182202SW COCKPIT READS LOW E HEEAO OTHER O OTHER ININSP/MAINT 1 SW03142PH 33150 READS 125 FEET LOW. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116001212001111600121SW 2001 11 16 HEEA076993 120011031G632194501031 BRAKE BELL 412 412 1182202SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 PUCKS WORN AND BROKEN MICRO SWITCH. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116001232001111600123 2001 11 16 HEEA076994 420011031G2340A3016W INTERPHONE BELL 412 412 1182202SW COCKPIT DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 VOLUME KNOB SHAFT LOOSE. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116001242001111600124 2001 11 16 HEEA076995 420011031G3442MI5851352 RADAR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 ANTENNA WOULD NOT SWEEP. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116001252001111600125 2001 11 16 HEEA076996 420011031G3140MI5852013 INDICATOR BELL 412 412 1182202SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03107X 33113 PICTURE PULSES AND TEST PATTERN IS BROKEN AND OFF COLOR. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116001262001111600126 2001 11 16 HEEA076997 420011031G3140MI585200 RADAR BELL 212 212 1181420SW COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03102PH 30899 PILOT HSI CIRCUIT BREAKER POPS IN FLIGHT. REPLACED WITH SERVICEABLE PART. 1G71 4U H4SW 20011116001272001111600127 2001 11 16 HEEA076998 420011031G3140MI5852013 INDICATOR BELL 212 212 1181420SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03102PH 30899 SCREEN FLASHES ON THEN OFF WITH DISTORTED IMAGING. REPLACED WITH SERVICEABLE PART. 1G71 4U H4SW 20011116001302001111600130 2001 11 16 HEEA076999 420011031G3442MI585202 RADAR BELL 412 412 1182202SW WX SYSTEM CONTAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 WEATHER RADAR HAS GAPS IN DISPLAY, FLUTTER WHILE SWEEPING. FOUND WATER IN UNIT. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116001322001111600132SW 2001 11 16 HEEA077000 120011031G6720 BUSHING BELL 412 412 1182202SW TAIL ROTOR WORN E HEEAO OTHER O OTHER ININSP/MAINT 1 SW031202T 33112 WORN BUSHINGS AND BEARINGS. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116001332001111600133SW 2001 11 16 HEEA077001 120011031G2840MS3108R14S5S CONNECTOR BELL 412 412 1182202SW NR 2 ENGINE SHORTED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0322347 36005 FUEL VALVE LIGHT CAME ON. MAINTENANCE FOUND SHORTED CANNON PLUG AT NR 2 ENGINE LORI VALVE CAUSING FUEL VALVE TO CYCLE. 1G72 4U H4SW 20011116001342001111600134 2001 11 16 HEEA077002 420011031G2200212001139001 PIN BELL 412 412 1182202SW NR 2 ENGINE LOOSE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03107X 33113 COPILOT THROTTLE WOULD NOT CONTROL THE NR 2 ENGINE. MAINTENANCE FOUND PIN CONNECTING COPILOT THROTTLE GRIP TO SHAFT IN COLLECTIVE STICK TO HAD BACKED OUT. REINSTALLED PIN. 1G72 4U H4SW 20011116001372001111600137 2001 11 16 HEEA077003 420011031G3453066402600 COMPUTER BELL 206 206L3 1182108SW COCKPIT FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW038592X 51508 WILL NOT POWER UP. PENDING VENDOR REPAIR. 1G71 3U H2SW 20011116001392001111600139SW 2001 11 16 HEEA077004 120011031G3246206324007 SKID BELL 206 206L3 1182108SW MLG CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0331801 51074 BOTTOM OF SKID TUBE HAS A 20 INCH CRACK EXTENDING FROM BELOW WHEEL LUG AFT. THERE ARE TWO ADDITIONAL CRACKS IN THE SAME AREA. PENDING VENDOR REPAIR. 1G71 3U H2SW 20011116001402001111600140SW 2001 11 16 HEEA077005 120011031G2810222366652003 FITTING BELL 206 206L3 1182108SW FUEL CELL CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381SP 51029 THREADS ON FITTING CORRODED. REPLACED WITH SERVICEABLE PART. 1G71 3U H2SW 20011116001622001111600162 2001 11 16 HEEA077006 420011031G25615018362071028 HARNESS BELL 412 412 1182202SW SAFETY EQUIP WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW032149S 36002 WORN. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20011116001632001111600163SW 2001 11 16 HEEA077007 120011031G2823206063640109 VALVE BELL 407 407 1182206SW FUEL SHUT OFF FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 FUEL SHUT OFF VALVE MAKING GRINDING NOISE. REPLACED WITH SERVICEABLE VALVE. 1G71 3U O H2SW 20011119000012001111900001SW 2001 11 19 HEEA077008 120011031G2820206063640109 VALVE BELL 407 407 1182206SW FUEL SYSTEM STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 INOPERATIVE - STUCK IN THE MID TRAVEL POSITION. TO BE SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. 1G71 3U O H2SW 20011119000022001111900002GL 2001 11 19 HEEA077009 220011031G753223005366 BLEED VALVE BELL 407 407 1182206SW ALLSN 250C 250C30 03013GL ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 HIGH MGT. REPLACED WITH SERVICEABLE BLEED VALVE. 1G71 3U3 UO H2SW E1GL 20011119000042001111900004SW 2001 11 19 HEEA077010 120011031G710023069706 TUBE BELL 407 407 1182206SW ENGINE WRONG PART E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 INCORRECT LINE. REPLACED WITH SERVICEABLE TUBE. 1G71 3U O H2SW 20011119000052001111900005SW 2001 11 19 HEEA077011 120011031G6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 RED BLADE PITCH ROD UNIVERSAL BEARING IS WORN. 1G71 3U O H2SW 20011119000062001111900006SW 2001 11 19 HEEA077012 120011031G6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 WORN BEARING. 1G71 3U O H2SW 20011119000072001111900007SW 2001 11 19 HEEA077013 120011031G6710406310411101 BOOT BELL 407 407 1182206SW MAIN ROTOR TORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 BOOT TORN. 1G71 3U O H2SW 20011119000082001111900008SW 2001 11 19 HEEA077014 120011031G6720406312103101 LINK BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 T/R P/C LINK WORN BEARING. 1G71 3U O H2SW 20011119000092001111900009SW 2001 11 19 HEEA077015 120011031G6720406312103101 LINK BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 T/R P/C LINK WORN BEARING. 1G71 3U O H2SW 20011119000102001111900010SW 2001 11 19 HEEA077016 120011031G6420407012101111 HUB BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 WORN FEATHERING BEARINGS. 1G71 3U O H2SW 20011119000122001111900012SW 2001 11 19 HEEA077019 120011031G2840407375016103 SIGNAL COND UNIT BELL 407 407 1182206SW FUEL INDICATION MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03495PH 53397 LOW LEVEL LIGHT ON WITH PLENTY OF FUEL ON BOARD. 1G71 3U O H2SW 20011119000132001111900013SW 2001 11 19 HEEA077020 120011031G6240407375008101 INDICATOR BELL 407 407 1182206SW DUAL TACH INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 DUAL TACH INOPERATIVE. 1G71 3U O H2SW 20011119000382001111900038SW 2001 11 19 HEEA077022 120011031G33404596 LAMP BELL 407 407 1182206SW EXTERIOR BURNED OUT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X 53267 BURNED OUT. SCRAPPED LOCALLY AND REPLACED WITH SERVICEABLE PART. 1G71 3U O H2SW 20011119000402001111900040GL 2001 11 19 HEEA077023 220011031G75106899080B VALVE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ANTI ICE SYSTEM STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 ANTI ICE VALVE STICKS IN ON POSITION INTERMITTENTLY. REPLACED WITH SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20011119000412001111900041SW 2001 11 19 HEEA077024 120011031G321070079H000Y150 HOSE BELL 407 407 1182206SW MLG KINKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03493PH 53393 HOSE ASSY KINKED. 1G71 3U O H2SW 20011119000422001111900042SW 2001 11 19 HEEA077025 120011031G6321D01631 PAD BELL 407 407 1182206SW M/R BRAKE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 WORN PAD. 1G71 3U O H2SW 20011119000432001111900043SW 2001 11 19 HEEA077026 120011031G5320D01661 BOLT BELL 407 407 1182206SW FUSELAGE DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 GROOVED. 1G71 3U O H2SW 20011119000452001111900045 2001 11 19 HEEA077027 420011031G3120 LIGHT BELL 407 407 1182206SW COCKPIT CLOCK INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038595X3053 53267 INTERNAL LIGHT QUIT WORKING. 1G71 3U O H2SW 20011119000472001111900047SW 2001 11 19 HEEA077028 120011031G2800P49389 RELEASE SYSTEM BELL 407 407 1182206SW VALVE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03405PH 53207 FAILED INSPECTION. 1G71 3U O H2SW 20011119000532001111900053SW 2001 11 19 HEEA077032 120011101G6320407340339101 BEARING BELL 407 407 1182206SW WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 BEARING WORN. 1G71 3U O H2SW 20011119000552001111900055NE 2001 11 19 HEEA077035 220011101G7200 ENGINE BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE NR 2 FAILED E HEEAO OTHER RXJPARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW0322347 36005 SHORTLY AFTER DEPARTURE, IN CRUISE, PILOT HEARD SQUEAL, BANG AND LOW RPM AUDIO. NOTED NR 2 ENGINE FAILED. SECURED ENGINE AND COMPLETED FLIGHT WITH RUN ON LANDING. 1G72 4U4 U H4SW E22EA 20011119000562001111900056SW 2001 11 19 HEEA077036 120011102G5302214040617105 HANGER ASSY BELL 214 214ST 1182106SW MISMANUFACTURED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03825H 28137 WILL NOT FIT IN SUPPORT ON AIRCRAFT. HOLES MILLED IN WRONG AREA. 2G72 4U H10SW 20011119000582001111900058SW 2001 11 19 HEEA077037 120011102G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 DISENGAGES DURING STARTING WITH GOOD BATTERIES. 2G72 4U H10SW 20011119000602001111900060SW 2001 11 19 HEEA077038 120011102G7120206064107103 MOUNT BELL 206 206L3 1182108SW ENGINE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03623Q 292 ENGINE MOUNT LEG WORN BEARING BEYOND LIMITS. SENT TO BELL HELICOPTER TEXTRON FOR WARRANTY CREDIT ON BEHALF OF CUSTOMER U.S. WEST. REFERENCE: INVOICE AND DMR NO. 687181. 1G71 3U H2SW 20011119000772001111900077 2001 11 19 HEEA077039 420011030G2350066105571 AUDIO PANEL BOLKMS105 BO105S 5626006EU COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0381982 S818 COIL LOOSE MOUNT AND NOT CONNECTED TO BOARD. PENDING VENDOR REPAIR. 1G72 3U H3EU 20011119000782001111900078 2001 11 19 HEEA077040 420011030G3454071121612 CONTROL UNIT BOLKMS105 BO105S 5626006EU COCKPIT MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0386CH S557 LED READ OUT ARE UNREADABLE ON DISPLAY. REPLACED WITH SERVICEABLE PART. 1G72 3U H3EU 20011119000792001111900079EU 2001 11 19 HEEA077041 120011031G6321350A32501000 LINER 350A32050002SNIAS 350 AS350B 8680801EU M/R BRAKE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03971AE M918 3230 WORN LINING. 1G71 3U H9EU 20011119000802001111900080EU 2001 11 19 HEEA077042 120011031G6720350A33215001 BALL 350A33200406SNIAS 350 AS350B 8680801EU TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03972AE MA1154 3234 WORN BALL. PENDING VENDOR RETURN FOR CREDIT. 1G71 3U H9EU 20011119000812001111900081 2001 11 19 HEEA077043 420011031G34205050010902 GYRO SNIAS 350 AS350B 8680801EU COCKPIT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03856PH 3352 COMPASS CARD SPINS. REPLACED WITH SERVICEABLE PART. 1G71 3U H9EU 20011119000822001111900082EU 2001 11 19 HEEA077044 120011031G6730SC5083 SERVO SNIAS 350 AS350B 8680801EU SERVO SYSTEM LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03971AE958 3230 LEAKING PAST SHAFT SEAL. PENDING VENDOR RETURN. 1G71 3U H9EU 20011119000832001111900083EU 2001 11 19 HEEA077045 120011031G2432RG390E BATTERY BOLKMS117 BK117A1 5626010EU MAIN WEAK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911RS S670 WEAK. REPLACED BATTERY. 1G72 3U H13EU 20011119000842001111900084EU 2001 11 19 HEEA077046 120011031G67301564T1005 ACTUATOR BOLKMS117 BK117A1 5626010EU NR 2 RPM MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03911RS S670 AFTER STARTING BOTH ENGINES, NR 2 RPM COULD NOT BE INCREASED OR DECREASED WITH BEEP SWITCH. REPLACED ACTUATOR. 1G72 3U H13EU 20011204001692001120400169NE 2001 12 4 HEEA077200 120011106G6210 TIP CAP SKRSKYS76 S76A 8143006NE M/R BLADE MISMANUFACTURED E HEEAK NONE O OTHER ININSP/MAINT 1 SW032234216268 760096 UNABLE TO INSTALL TIP CAP, SCREW HOLES DO NOT LINE UP. 1G72 3U H1NE 20011204001702001120400170NE 2001 12 4 HEEA077201 120011106G3297PHIS761178002 HARNESS SKRSKYS76 S76A 8143006NE MLG OUT OF ADJ E HEEAO OTHER O OTHER TOTAKEOFF 1 SW03911UK 760275 ON TAKE OFF UPON RETRACTING LANDING GEAR GOT AN UNSAFE FLIGHT. MAINTENANCE ADJUSTED THE NOSE CENTERING PROXIMITY SENSOR. 1G72 3U H1NE 20011204001722001120400172SW 2001 12 4 HEEA077204 120011106G6322PHIPBH40701 BLOWER BELL 407 407 1182206SW OIL COOLER FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH 53398 FORWARD BEARING LOUD AND ROUGH. 1G71 3U O H2SW 20011204001742001120400174SW 2001 12 4 HEEA077205 120011106G7120214031252141 SUPPORT BELL 214 214ST 1182106SW ENG MOUNT MISMARKED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 MISIDENTIFIED. SUPPORT RECEIVED WAS A RT SUPPORT; YET WAS MARKED FOR THE LT SUPPORT P/N. 2G72 4U H10SW 20011204001772001120400177SW 2001 12 4 HEEA077206 120011106G7120206064107103 LEG ASSY BELL 206 206L3 1182108SW ENG MOUNT MISMARKED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 MISIDENTIFIED AND MISMANUFACTURED. 1G71 3U H2SW 20011204001782001120400178SW 2001 12 4 HEEA077207 120011106G5302206020113173S CAP BELL 206 206L3 1182108SW TAIL BOOM CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 DENTED AND CRACKED AT LEADING EDGE. 1G71 3U H2SW 20011204001792001120400179SW 2001 12 4 HEEA077208 120011107G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03 WON'T STAY ENGAGED AT CROSS START. 2G72 4U H10SW 20011204001802001120400180SW 2001 12 4 HEEA077209 120011107G6300214040104001 ROLLER BELL 214 214ST 1182106SW MAIN ROTOR CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 PITTING ON ROLLERS. 2G72 4U H10SW 20011204001832001120400183SW 2001 12 4 HEEA077210 120011109G3300214175140103 POWER SUPPLY BELL 214 214ST 1182106SW LIGHTS INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03 POWER SUPPLY INOPERATIVE. 2G72 4U H10SW 20011204001842001120400184SW 2001 12 4 HEEA077211 120011109G2435206062200113 STARTER GEN BELL 407 407 1182206SW ENGINE FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03402PH1157 53159 FAILED 300 HOUR INSPECTION. 1G71 3U O H2SW 20011204001862001120400186SW 2001 12 4 HEEA077212 120011113G7120206064106101 LEG ASSY BELL 206 206L3 1182108SW ENG MOUNT MISMARKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 PARTS MISIDENTIFIED. 1G71 3U H2SW 20011204001882001120400188SW 2001 12 4 HEEA077213 120011113G2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH1790 95171 53400 WORN BRUSHES. 1G71 3U O H2SW 20011204001922001120400192SW 2001 12 4 HEEA077214 120011115G3300214175140103 POWER SUPPLY BELL 214 214ST 1182106SW LIGHTS DISCHARGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03 POWER SUPPLY DEAD. 2G72 4U H10SW 20011204001942001120400194SW 2001 12 4 HEEA077215 120011115G6520214040404101 SHAFT 214540001101BELL 214 214ST 1182106SW T/R GEARBOX CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03598061711 A26 28140 EXCESSIVE CORROSION AT TAIL ROTOR OUTPUT SHAFT DRIVE SPLINES. 2G72 4U H10SW 20011204002002001120400200SW 2001 12 4 HEEA077216 120011115G7120206064106101 LEG ASSY BELL 206 206L3 1182108SW ENG MOUNT MISMARKED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 MISIDENTIFIED. IT SHOULD BE 206-064-106-001. 1G71 3U H2SW 20011204002202001120400220SW 2001 12 4 HEEA077217 120011115G6300206010003007 CONE SET BELL 206 206L3 1182108SW MAIN ROTOR MISMARKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 CONE SET MISIDENTIFIED. 1G71 3U H2SW 20011204002212001120400221SW 2001 12 4 HEEA077218 120011116G6300212010103007 FITTING BELL 212 212 1181420SW MAIN ROTOR GOUGED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 PART IS GOUGED ON TOP AND WAS NOT ACCEPTABLE PER OUR INSPECTORS. 1G71 4U H4SW 20011204002232001120400223SW 2001 12 4 HEEA077222 120011120G7712407375003107 INDICATOR BELL 407 407 1182206SW TORQUE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03408PH 53228 WON'T INDICATE TORQUE. 1G71 3U O H2SW 20011205000012001120500001SW 2001 12 5 HEEA077223 120011120G6730206076062105 SERVO BELL 407 407 1182206SW ROTOR SERVO LEAKING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH4730 53159 SERVO IS LEAKING. 1G71 3U O H2SW 20011205000022001120500002SW 2001 12 5 HEEA077228 120011120G6220407010150105A FRAHM BELL 407 407 1182206SW MAIN ROTOR BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH 53400 FRAHM HAS A BROKEN SPRING. 1G71 3U O H2SW 20011205000032001120500003SW 2001 12 5 HEEA077232 120011120G7712407375003107 INDICATOR BELL 407 407 1182206SW TORQUE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 BACK LIGHT INOPERATIVE. 1G71 3U O H2SW 20011205000042001120500004SW 2001 12 5 HEEA077233 120011120G6510407040302103 DRIVE SHAFT BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW038595X 53267 SPLINES WORN BEYOND LIMITS. 1G71 3U O H2SW 20011205000052001120500005SW 2001 12 5 HEEA077235 120011120G7714407375008101 INDICATOR BELL 407 407 1182206SW DUAL TACH INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03447PH 53114 NR NEEDLE INOPERATIVE. 1G71 3U O H2SW 20011205000062001120500006SW 2001 12 5 HEEA077238 120011120G7714407375008101 INDICATOR BELL 407 407 1182206SW DUAL TACH INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03417PH 53038 TURBINE NEEDLE PEGGED TO THE HIGH. 1G71 3U O H2SW 20011205000112001120500011SW 2001 12 5 HEEA077241 120011121G6310214040841101 SEAL BELL 407 407 1182206SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 SEAL IS WORN. 1G71 3U O H2SW 20011205000122001120500012SW 2001 12 5 HEEA077242 120011121G6310214040814105 SLEEVE BELL 407 407 1182206SW TRANSMISSION WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53390 SLEEVE WORN. 1G71 3U O H2SW 20011205000142001120500014SW 2001 12 5 HEEA077243 120011121G6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH1588 53327 BEARING WORN. 1G71 3U O H2SW 20011205000152001120500015SW 2001 12 5 HEEA077244 120011121G6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH908 53401 WORN. 1G71 3U O H2SW 20011205000162001120500016SW 2001 12 5 HEEA077245 120011121G6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH908 53401 UNIVERSAL WORN. 1G71 3U O H2SW 20011205000182001120500018SW 2001 12 5 HEEA077246 120011121G6710406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03501PH908 53401 WORN. 1G71 3U O H2SW 20011205000202001120500020SW 2001 12 5 HEEA077247 120011121G291070061J180W164A HOSE BELL 407 407 1182206SW HYD SYSTEM CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 CHAFED. 1G71 3U O H2SW 20011205000212001120500021SW 2001 12 5 HEEA077248 120011121G291070061J285W210A HOSE BELL 407 407 1182206SW HYD SYSTEM CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 CHAFED. 1G71 3U O H2SW 20011205000332001120500033SW 2001 12 5 HEEA077249 120011121G2840206362002103 ADAPTER BELL 407 407 1182206SW FUEL INDICATOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 FUEL INDICATOR ADAPTER IS WORN. 1G71 3U O H2SW 20011205000352001120500035SW 2001 12 5 HEEA077250 120011121G6510206061432121 HOUSING BELL 407 407 1182206SW COOLER BLOWER CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 COOLER BLOWER HOUSING IS CRACKED. 1G71 3U O H2SW 20011205000402001120500040SW 2001 12 5 HEEA077251 120011121G3340A490ATSDF1428 POWER SUPPLY BELL 407 407 1182206SW EXTERIOR LIGHTS FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03141MA 53016 FAULTY GROUND WIRE AT PLUG CAUSED UNIT TO FAIL. 1G71 3U O H2SW 20011205000412001120500041SW 2001 12 5 HEEA077252 120011121G2420SM20ACD300A21 RELAY BELL 407 407 1182206SW INTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 INTERMITTENT. 1G71 3U O H2SW 20011205000432001120500043SW 2001 12 5 HEEA077253 120011121G2497407375012103 WIRE BELL 407 407 1182206SW FADEC DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 CAUSING FADEC DEGRADE LIGHT. 1G71 3U O H2SW 20011205000442001120500044SW 2001 12 5 HEEA077254 120011121G2420SM20ACD300A21 RELAY BELL 407 407 1182206SW COCKPIT FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 CAUSES IGNITION FAULT TO APPEAR SEVERAL TIMES. 1G71 3U O H2SW 20011205000462001120500046SW 2001 12 5 HEEA077255 120011121G282070079H000Y150 HOSE BELL 407 407 1182206SW FUEL SYSTEM KINKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 HOSE ASSY KINKED. 1G71 3U O H2SW 20011205000482001120500048SW 2001 12 5 HEEA077256 120011121G6340214040806003 PRESSURE SWITCH BELL 407 407 1182206SW TRANSMISSION OILFAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 TRANSMISSION OIL PRESSURE LIGHT DOESN'T COME ON DURING SHUT DOWN. 1G71 3U O H2SW 20011205000492001120500049SW 2001 12 5 HEEA077257 120011121G7120407060111101 MOUNT BELL 407 407 1182206SW ENGINE INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03417PH4197 53038 INOPERATIVE. 1G71 3U O H2SW 20011205000502001120500050SW 2001 12 5 HEEA077258 120011121G6320407340339101 BEARING BELL 407 407 1182206SW MAIN ROTOR OVERHEATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 BEARING OVERHEATED 1G71 3U O H2SW 20011205000522001120500052SW 2001 12 5 HEEA077259 120011121G6710 BEARING BELL 407 407 1182206SW IDLER ASSY WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH CT1279 53386 WORN BEARING. 1G71 3U O H2SW 20011205000532001120500053SW 2001 12 5 HEEA077260 120011121G2844407362013101 PRESSURE SWITCH BELL 407 407 1182206SW FUEL PRESSURE STUCK E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03447PH 53114 STICKS IN CLOSED POSITION. 1G71 3U O H2SW 20011205000542001120500054SW 2001 12 5 HEEA077261 120011121G5210206064819006S DOOR BELL 407 407 1182206SW PAX/CREW CORRODED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03723PH 53283 CORRODED AROUND BOTH LATCHES. 1G71 3U O H2SW 20011205000552001120500055SW 2001 12 5 HEEA077262 120011121G282070079H100F210 HOSE BELL 407 407 1182206SW FUEL SYSTEM CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 INSULATION CHAFED THROUGH. 1G71 3U O H2SW 20011205000562001120500056SW 2001 12 5 HEEA077263 120011121G3210407040624101 TUBE BELL 407 407 1182206SW MLG CHAFED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 TUBE ON MLG CHAFED. 1G71 3U O H2SW 20011205000572001120500057 2001 12 5 HEEA077264 420011121G2340PM212302 SWITCH BELL 407 407 1182206SW COCKPIT BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03406PH 53198 MIC SPRING TABS WORN. REPORTED STICKING ICS. 1G71 3U O H2SW 20011205000582001120500058SW 2001 12 5 HEEA077267 120011121G6340214040806003 PRESSURE SWITCH BELL 407 407 1182206SW TRANSMISSION OILINTERMITTENT E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 INTERMITTENTLY STICKING. LIGHT WILL NOT COME ON AFTER SHUTDOWN. 1G71 3U O H2SW 20011205000692001120500069SW 2001 12 5 HEEA077269 120011121G6321 PAD BELL 407 407 1182206SW ROTOR BRAKE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03612PH 53199 WORN PADS, 1G71 3U O H2SW 20011205000702001120500070SW 2001 12 5 HEEA077270 120011121G3212206050247131 COVER BELL 407 407 1182206SW MLG FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03724PH 53327 COVER WORN. 1G71 3U O H2SW 20011205000712001120500071SW 2001 12 5 HEEA077271 120011121G6310214040841101 SEAL BELL 407 407 1182206SW TRANSMISSION LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03722PH 53288 LEAKING. 1G71 3U O H2SW 20011205000722001120500072SW 2001 12 5 HEEA077272 120011121G6400 BEARING BELL 407 407 1182206SW OIL COOLER SHAFTFAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH 53400 OIL COOLER SHAFT BEARING FAILED. 1G71 3U O H2SW 20020118000812002011800081NE 2002 1 18 HEEA077387 220011203G7200 ENGINE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE ENGINE BAY MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03505PH2030 760505 20529TEC ENGINE WOULD NOT START. 1G72 3U3 UNCH1NE E19EU 20020118000822002011800082NE 2002 1 18 HEEA077388 120011204G62107615009100048A BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR MISMANUFACTURED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03911MJ12101 760231 UNABLE TO INSTALL TIP CAPS - TWO DIFFERENT TIP CAPS. TIP CAP BLOCK HOLES APPEAR TO BE DRILLED 1/8 INCH TOO FAR FORWARD WHEN AFT SCREWS INSERTED. 1G72 3U H1NE 20020118000832002011800083NE 2002 1 18 HEEA077389 120011204G62107615009100051A RIB SKRSKYS76 S76A 8143006NE MAIN ROTOR BLADEDEBONDED E HEEAK NONE O OTHER ININSP/MAINT 1 SW035426U11828 760167 MAIN ROTOR BLADE TIP RIB UNBONDED. 1G72 3U H1NE 20020118000842002011800084NE 2002 1 18 HEEA077390 120011204G6210 TAB SKRSKYS76 S76A 8143006NE MAIN ROTOR BLADESPLIT E HEEAK NONE O OTHER ININSP/MAINT 1 SW034253S7247 760035 MAIN ROTOR BLADE TRIM TAB IS SPLIT OPEN NEAR THE TIP OF THE BLADE. 1G72 3U H1NE 20020118000882002011800088NE 2002 1 18 HEEA077391 120011204G62107615009100053 BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR DELAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW034253S7056 760035 LAMINATE AT STA 44 ON THE LOWER SIDE IS SEPARATED. . 1G72 3U H1NE 20020118000902002011800090 2002 1 18 HEEA077392 420011204G3420501145301 GYRO SKRSKYS76 S76A 8143006NE AFCS PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035435V 760158 VERTICAL GYRO PRECESSES. 1G72 3U H1NE 20020118000912002011800091 2002 1 18 HEEA077393 420011204G3420125780 INDICATOR SKRSKYS76 S76A 8143006NE ADI PRECESSES E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW035426U 760167 ADI PRECESSES HORIZONTALLY IN FLIGHT. 1G72 3U H1NE 20020118000922002011800092NE 2002 1 18 HEEA077394 220011211G72619560134100 MAGNETIC SEAL SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1 60030NE ENGINE LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03974AE 2653 ENGINE MAGNETIC SEAL IS LEAKING. 1G71 3U3 U H9EU E19EU 20020118000932002011800093NE 2002 1 18 HEEA077395 220011211G74219550168760 IGNITER SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1 60030NE ENGINE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03971AE 3230 ENGINE IGNITER WORN. 1G71 3U3 U H9EU E19EU 20020118000942002011800094NE 2002 1 18 HEEA077396 220011211G74219550168760 IGNITER SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1 60030NE ENGINE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03971AE 3230 ENGINE IGNITER WORN. 1G71 3U3 U H9EU E19EU 20020118000952002011800095EU 2002 1 18 HEEA077397 120011211G71700174078010 DRAIN VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ENGINE LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW034031L3078 2907 ENGINE DRAIN VALVE LEAKING FUEL AT PLUG. 1G71 3U3 U H9EU E19EU 20020118000962002011800096SW 2002 1 18 HEEA077401 120011126G2435 BRUSHES BELL 407 407 1182206SW STARTER GEN WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH2533 98221 53003 STARTER GENERATOR HAS WORN BRUSHES. 1G71 3U O H2SW 20020118000992002011800099 2002 1 18 HEEA077402 420011127G2210214074305105 AMPLIFIER BELL 214 214ST 1182106SW AFCS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 TRIPS OFF WHEN CONTROL IS MOVED. 2G72 4U H10SW 20020118001052002011800105 2002 1 18 HEEA077403 420011127G2210214074301105 AMPLIFIER BELL 214 214ST 1182106SW AFCS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 PITCH TRIPS AFTER 30 TO 45 MINUTES OF FLIGHT. RESETS BUT ONLY FOR SHORT PERIOD OF TIME. 2G72 4U H10SW 20020118001092002011800109SW 2002 1 18 HEEA077404 120011127G2730214001970111 ACTUATOR BELL 214 214ST 1182106SW ELEVATORS MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 ACTUATOR TRIPS OFF BOTH ELEVATOR SYSTEMS. 2G72 4U H10SW 20020118001152002011800115SW 2002 1 18 HEEA077428 120011203G7120 BEARING BELL 206 206L3 1182108SW ENGINE MOUNT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 BEARING WORN PREMATURELY. 1G71 3U H2SW 20020122000012002012200001SW 2002 1 22 HEEA077429 120011203G6300206040320103 SHAFT BELL 206 206L3 1182108SW MAIN ROTOR DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 UNABLE TO BALANCE SHAFT. 1G71 3U H2SW 20020122000022002012200002SW 2002 1 22 HEEA077430 120011203G6320206040146103 GEAR BELL 206 206L3 1182108SW M/R GEARBOX MISMARKED E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 GEAR SERIAL NUMBER A-FS9423 AND A-FS9409 ARE IMPROPERLY MARKED WITH PART NUMBER 204-040-146-103. 1G71 3U H2SW 20020122000032002012200003SW 2002 1 22 HEEA077431 120011203G3213206323017 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 CROSSTUBE HAS CORROSION. 1G71 3U H2SW 20020122000042002012200004SW 2002 1 22 HEEA077432 120011203G3213206323018 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 CROSSTUBE HAS CORROSION. 1G71 3U H2SW 20020122000052002012200005SW 2002 1 22 HEEA077433 120011203G6320214001373101 IDLER GEAR BELL 214 214ST 1182106SW NEW MISSING E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03 BEARING MISSING WHEN PACKAGED PART WAS OPENED. 2G72 4U H10SW 20020122000062002012200006SW 2002 1 22 HEEA077434 120011203G2913222380009105 PUMP BELL 430 430 1182150SW NR 1 HYD SYSTEM FAILED E HEEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03430X 1638 49058 DURING CLIMB OUT AFTER TAKEOFF, THE NR 1 HYDRAULIC SYSTEM FAILED. MAINTENANCE FOUND DRIVE SHAFT DISENGAGED FROM THE NR 1 HYDRAULIC PUMP. REPLACED PUMP. 1G72 3U RTH9SW 20020122000072002012200007SW 2002 1 22 HEEA077435 120011203G2497 WIRE BELL 412 412 1182202SW NR 1 GENERATOR BROKEN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW0333008 36004 NR 1 GENERATOR FAILED. MAINTENANCE FOUND WIRE BROKEN AT TERMINAL "A" ON NR 1 GENERATOR. 1G72 4U H4SW 20020122000082002012200008SW 2002 1 22 HEEA077436 120011206G7120206064106101 LEG ASSY BELL 206 206L3 1182108SW ENGINE MOUNT MISMARKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 PART NUMBER INCORRECT, PART MADE OF STEEL (MISIDENTIFIED) SHOULD BE 206064106001. 1G71 3U H2SW 20020122000092002012200009SW 2002 1 22 HEEA077437 120011206G5260212075418105 ACTUATOR BELL 412 412 1182202SW STEP INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 STEP ACTUATOR WOULD NOT MOVE AT ALL. 1G72 4U H4SW 20020122000102002012200010SW 2002 1 22 HEEA077438 120011206G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW035748M378 28102 STARTER WILL NOT STAY ENGAGED. 2G72 4U H10SW 20020122000112002012200011SW 2002 1 22 HEEA077439 120011206G8011214060056705 STARTER BELL 214 214ST 1182106SW ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW0359806241 28140 STARTER STAYS STUCK IN THE ON POSITION. 2G72 4U H10SW 20020122000122002012200012SW 2002 1 22 HEEA077440 120011206G6220222310503101 BEARING BELL 230 230 1182149SW MAIN ROTOR HEAD DELAMINATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03 BEARING HAS DELAMINATED ELASTOMER. 1G72 3U NCH9SW 20020122000132002012200013SW 2002 1 22 HEEA077441 120011206G2435206062200113 STARTER GEN BELL 407 407 1182206SW ENGINE INOPERATIVE E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03457PH2446 53147 STARTER GENERATOR WILL NOT MOTOR OVER. 1G71 3U O H2SW 20020122000142002012200014SW 2002 1 22 HEEA077442 120011206G2435206062200113 STARTER GEN BELL 407 407 1182206SW ENGINE ARCED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03741PH2258 53457 STARTER GENERATOR IS ARCING. 1G71 3U O H2SW 20020122000152002012200015SW 2002 1 22 HEEA077445 120011210G2910 HYDRAULIC SYSTEM BELL 430 430 1182150SW NR 1 MALFUNCTIONED E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03430X 49058 ONE HOUR AND 10 MINUTES INTO THE FLIGHT THE SCAS KICKED OFF. THE NR 1 HYDRAULIC SYSTEM PRESSURE FLUCTUATED BETWEEN 0 AND 130 PSI WITH RESITANCE IN THE TAIL ROTOR PEDALS. DURING ENGINE COOL DOWN, TURNED NR 1 HYDRAULIC SYSTEM ON AND PRESSURE WAS STEADY AT 1430 PSI WITH NO RESISTANCE IN THE TAIL ROTOR PEDALS. CLEANED ALL CONNECTORS IN HYDRAULIC SYSTEM AT BYPASS SOLENOID, PRESSURE SWITCHES, PRESSURE TRANSDUCERS AND SERVICED RESERVOIR. 1G72 3U RTH9SW 20020122000162002012200016SW 2002 1 22 HEEA077446 120011214G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE SLOW E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW033897N270 28106 STARTER IS SLOW TO START. 2G72 4U H10SW 20020122000172002012200017SW 2002 1 22 HEEA077447 120011214G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE WEAK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW033897N36 28106 STARTER IS WEAK. 2G72 4U H10SW 20020122000182002012200018SW 2002 1 22 HEEA077448 120011214G8011214060056103 STARTER BELL 214 214ST 1182106SW ENGINE MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW038045T431 28101 STARTER WON'T STAY ENGAGED. 2G72 4U H10SW 20020122000192002012200019EU 2002 1 22 HEEA077449 120011203G7931ZRA25500 TRANSMITTER SNIAS 350 AS350B 8680801EU ENG OIL PRESS MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03973AE 3229 ENGINE OIL PRESSURE HADN`T ANY INDICATION ON START FOR 3 SECONDS. 1G71 3U H9EU 20020122000202002012200020EU 2002 1 22 HEEA077450 120011203G6310350A35110500 GIMBAL JOINT SNIAS 350 AS350B 8680801EU MAIN ROTOR BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03855PH 3351 GIMBAL JOINT IS BROKEN. 1G71 3U H9EU 20020122000212002012200021EU 2002 1 22 HEEA077451 120011203G772156375600010 INDICATOR SNIAS 350 AS350B 8680801EU COCKPIT DAMAGED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03856PH 3352 T4 INDICATOR WAS RECEIVED WITH RATTLE NOISE INSIDE. DID NOT INSTALL ON AIRCRAFT. WAS ISSUED AND RETIRED UNSERVICEABLE. SOUNDS LIKE LOOSE SCREW INSIDE. 1G71 3U H9EU 20020122000222002012200022 2002 1 22 HEEA077452 420011203G3120B1894522282A CLOCK SNIAS 350 AS350B 8680801EU COCKPIT INOPERATIVE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03974AE 2653 CLOCK WILL NOT WIND UP. 1G71 3U H9EU 20020122000232002012200023EU 2002 1 22 HEEA077453 120011203G6320350A32310121 FRICTION RING SNIAS 350 AS350B 8680801EU M/R GEARBOX LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03855PH 3351 FRICTION RING LEAKS. 1G71 3U H9EU 20020122000242002012200024EU 2002 1 22 HEEA077454 120011203G6710SC5083 SERVO SNIAS 350 AS350B 8680801EU MAIN ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03855PH 3351 SERVO LEAKS. 1G71 3U H9EU 20020122000252002012200025EU 2002 1 22 HEEA077455 120011203G772156375600010 INDICATOR SNIAS 350 AS350B 8680801EU COCKPIT STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03856PH 3352 T4 INDICATOR NEEDLE STICKS INTERMITTENTLY AT 700 DURING START. 1G71 3U H9EU 20020122000262002012200026EU 2002 1 22 HEEA077456 120011203G6710SC5083 SERVO SNIAS 350 AS350B2 8680813EU MAIN ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW0340466 3004 SERVO LEAKING. 1G71 3U H9EU 20020122000272002012200027 2002 1 22 HEEA077458 420011203G3160350A67622202 INDICATOR SNIAS 350 AS350B 8680801EU PITOT HEAT MALFUNCTIONED E HEEAK NONE N FALSE WARNING ININSP/MAINT 1 SW03856PH 3352 PITOT HEAT LIGHT WOULD NOT GO OUT. 1G71 3U H9EU 20020122000282002012200028EU 2002 1 22 HEEA077459 120011203G6230 PAINT SNIAS 350 AS350B 8680801EU M/R SHAFT MISSING E HEEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW03974AE 2653 THE MAIN ROTOR SHAFT`S SPECIAL PAINT COAT MISSING. 1G71 3U H9EU 20020122000292002012200029EU 2002 1 22 HEEA077460 120011203G6220350A37112601 LINK SNIAS 350 AS350B 8680801EU MAIN ROTOR HEAD CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03974AE 2653 SCISSOR LINKS HAS CORROSION. 1G71 3U H9EU 20020122000302002012200030EU 2002 1 22 HEEA077461 120011203G6230350A37100206 STAR SNIAS 350 AS350B 8680801EU SWASHPLATE CORRODED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03974AE 2653 NON ROTATING STAR HAS CORROSION. 1G71 3U H9EU 20020122000312002012200031 2002 1 22 HEEA077462 420011206G3416150201182 ALTIMETER SNIAS 350 AS350B2 8680813EU NEW DAMAGED E HEEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW03 PART WAS RECEIVED AT PHI CLAIMING TO BE SERVICEABLE, MECHANIC CLAIMS GUAGE OFF. 1G71 3U H9EU 20020122000322002012200032 2002 1 22 HEEA077463 420011206G3416150201182 ALTIMETER SNIAS 350 AS350B 8680801EU COCKPIT STUCK E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03972AE 3234 ALTIMETER STICKS WHEN GOING UP AS MUCH AS 300 FEET. 1G71 3U H9EU 20020122000332002012200033EU 2002 1 22 HEEA077464 120011211G6520350A33214501 ROD END BEARING SNIAS 350 AS350B 8680801EU PITCH CONTROL WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03855PH 3351 PITCH CONTROL ROD SPHERICAL BEARING WORN. 1G71 3U H9EU 20020122000342002012200034GL 2002 1 22 HEEA077550 220011217G726023007248 GEARSHAFT 23035179 SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL GEARBOX SPALLED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545X339 CAG95129 760050 CAE890508S GEARSHAFT IN GEARBOX HAS SPALLING ON GEARTEETH. 1G72 3U3 U H1NE E1GL 20020122000352002012200035GL 2002 1 22 HEEA077551 220011217G726023007151 BEARING 23035179 SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL GEARBOX SPALLED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW031545X339 CAG95129 760050 CAE890508S GEAR HAS SPALLING ON BALL BEARING. 1G72 3U3 U H1NE E1GL 20020122000362002012200036NE 2002 1 22 HEEA077552 220011220G73200164248690 FUEL CONTROL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE ENGINE MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034034Q1806 2918 ENGINE SLOW START DURING COLD WEATHER. 1G71 3U3 U H9EU E19EU 20020122000422002012200042SW 2002 1 22 HEEA077559 120011217G3110407375015103 WARN PANEL BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW034999 53323 HYD. SYSTEM LIGHT FLASHING IN FLIGHT. 1G71 3U O H2SW 20020122000432002012200043SW 2002 1 22 HEEA077560 120011217G6240412075010111 INDICATOR BELL 412 412EP 1182205SW TRIPLE TACH FLUCTUATES E HEEAK NONE O OTHER ININSP/MAINT 1 SW036106C 36257 TRIPLE TACH NEEDLES FLUCTUATE. 1G72 4U H4SW 20020122000442002012200044SW 2002 1 22 HEEA077561 120011217G6240412075010111 INDICATOR BELL 412 412EP 1182205SW TRIPLE TACH FLUCTUATES E HEEAK NONE L NO TEST ININSP/MAINT 1 SW036106C 36257 TRIPLE TACH NEEDLES FLUCTUATE. 1G72 4U H4SW 20020122000452002012200045SW 2002 1 22 HEEA077562 120011217G2821222366621103 FUEL FILTER BELL 407 407 1182206SW FUEL SYSTEM DEFECTIVE E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03493PH 53393 FUEL FILTER LIGHT ILLUMINATED. 1G71 3U O H2SW 20020122000562002012200056SW 2002 1 22 HEEA077563 120011217G7700407375016103 SIGNAL COND UNIT BELL 407 407 1182206SW ENGINE INACCURATE E HEEAK NONE O OTHER ININSP/MAINT 1 SW03405PH 53207 SIGNAL CONDITIONING UNIT LOW LEVEL ON FULL FUEL. 1G71 3U O H2SW 20020122000712002012200071SW 2002 1 22 HEEA077568 120011217G6220 SPRING BELL 407 407 1182206SW FRAHM ASSY BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03742PH 53461 FRAHM ASSEMBLY HAS A BROKEN SPRING. 1G71 3U O H2SW 20020122000722002012200072SW 2002 1 22 HEEA077569 120011217G6320407040006107 GEARBOX BELL 407 407 1182206SW MAIN ROTOR MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH3052 53397 MAIN ROTOR GEARBOX MAKING METAL. 1G71 3U O H2SW 20020122000732002012200073SW 2002 1 22 HEEA077570 120011217G6310406040500131 FREEWHEEL UNIT BELL 407 407 1182206SW MAIN ROTOR LEAKING E HEEAK NONE K FLUID LOSS ININSP/MAINT 1 SW03741PH1173 53457 FREEWHEEL UNIT IS LEAKING. 1G71 3U O H2SW 20020122000752002012200075SW 2002 1 22 HEEA077572 120011217G6310406040500127 FREEWHEEL UNIT BELL 407 407 1182206SW MAIN ROTOR MAKING METAL E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH1405 53397 FREEWHEEL UNIT IS MAKING METAL. 1G71 3U O H2SW 20020122000772002012200077SW 2002 1 22 HEEA077575 120011217G6510407040302107 DRIVE SHAFT BELL 407 407 1182206SW TAIL ROTOR PEELING E HEEAK NONE O OTHER ININSP/MAINT 1 SW03501PH967 53401 PAINT PEELING OFF TAIL ROTOR DRIVE SHAFT. 1G71 3U O H2SW 20020122000782002012200078SW 2002 1 22 HEEA077576 120011217G7714407375002103 INDICATOR BELL 407 407 1182206SW COCKPIT MALFUNCTIONED E HEEAK NONE N FALSE WARNING ININSP/MAINT 1 SW03491PH 53386 NG INDICATOR SHOWS EXCEEDANCE, CANNOT CLEAR. 1G71 3U O H2SW 20020122000802002012200080SW 2002 1 22 HEEA077577 120011217G6220 SPRING BELL 407 407 1182206SW FRAHM ASSY BROKEN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH A630 53393 FRAHM ASSY HAS BROKEN SPRING. 1G71 3U O H2SW 20020122000812002012200081SW 2002 1 22 HEEA077578 120011217G7712407375003107 INDICATOR BELL 407 407 1182206SW TORQUE MALFUNCTIONED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03406PH 53198 TORQUE INDICATOR HAS DIM LIGHTING. 1G71 3U O H2SW 20020122000842002012200084 2002 1 22 HEEA077580 420011217G2210214074305105 AMPLIFIER BELL 214 214ST 1182106SW AUTO FLIGHT MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03 CAUSES ELEVATOR TO TRIP OFF LINE. 2G72 4U H10SW 20020122000872002012200087SW 2002 1 22 HEEA077583 120011218G2822407362013101 PRESSURE SWITCH BELL 407 407 1182206SW BOOST PUMP FAILED E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03402PH 53159 BOOST PUMP LIGHT WILL NOT COME ON WHEN PUMP OFF. 1G71 3U O H2SW 20020122000912002012200091SW 2002 1 22 HEEA077584 120011218G6322407062021101 DUCT BELL 407 407 1182206SW OIL COOLER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH 53398 OIL COOLER DUCT CRACKED. 1G71 3U O H2SW 20020122001242002012200124SW 2002 1 22 HEEA077585 120011218G6300407340339103 BEARING PHIPBH40701 BELL 407 407 1182206SW COOLER BLOWER WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH PHI0025 53209 WORN BEARING. 1G71 3U O H2SW 20020122001272002012200127SW 2002 1 22 HEEA077586 120011218G3212212073905001 GAUGE BELL 407 407 1182206SW FLOAT PRESSURE CONTAMINATED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW034999 53323 PRESSURE GAUGE IS FULL OF MOISTURE. 1G71 3U O H2SW 20020122001282002012200128SW 2002 1 22 HEEA077587 120011218G3212206050247137 COVER BELL 407 407 1182206SW FLOAT WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03447PH 53114 FLOAT COVER IS BADLY WORN. 1G71 3U O H2SW 20020122001302002012200130SW 2002 1 22 HEEA077589 120011218G32128226003 FUSEABLE PLUG BELL 407 407 1182206SW FLOAT LEAKING E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 FLOAT BOTTLE FUSABLE PLUG IS LEAKING. 1G71 3U O H2SW 20020122001312002012200131SW 2002 1 22 HEEA077590 120011218G6321206076047101 CYLINDER BELL 407 407 1182206SW ROTOR BRAKE LEAKING E HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03490PH 53378 CYLINDER LEAKING FROM PISTON SEAL. 1G71 3U O H2SW 20020122001322002012200132SW 2002 1 22 HEEA077592 120011218G6320206061432121 HOUSING BELL 407 407 1182206SW COOLER BLOWER DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 RIVETS WORKING. 1G71 3U O H2SW 20020122001332002012200133SW 2002 1 22 HEEA077593 120011218G6340214040806003 PRESSURE SWITCH BELL 407 407 1182206SW XMSN OIL FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03491PH 53386 TRANSMISSION OIL PRESSURE CAUTION LIGHT CAME ON. 1G71 3U O H2SW 20020122001342002012200134SW 2002 1 22 HEEA077594 120011218G6300407340339101 BEARING BELL 407 407 1182206SW MAIN ROTOR FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03447PH 53114 FAILED OPERATIONAL TEST (RAN HOT ABOVE 270 F.) 1G71 3U O H2SW 20020122001352002012200135SW 2002 1 22 HEEA077595 120011218G6420406312103101 LINK BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03721PH 53278 TAIL ROTOR LINK WORN. 1G71 3U O H2SW 20020122001362002012200136SW 2002 1 22 HEEA077596 120011218G6330407310203101 MOUNT BELL 407 407 1182206SW TRANSMISSION DAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 TRANSMISSION MOUNT RUBBER BAD. 1G71 3U O H2SW 20020122001372002012200137SW 2002 1 22 HEEA077598 120011218G6300406310405101 UNIVERSAL BELL 407 407 1182206SW M/R DRIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03499PH1198 53400 MAIN ROTOR DRIVE UNIVERSAL WORN. 1G71 3U O H2SW 20020122001392002012200139SW 2002 1 22 HEEA077600 120011218G2822407362013101 PRESSURE SWITCH BELL 407 407 1182206SW ENGINE FAILED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53398 PRESSURE SWITCH FAILED. 1G71 3U O H2SW 20020122001472002012200147SW 2002 1 22 HEEA077601 120011218G6720406312103101 PITCH LINK BELL 407 407 1182206SW TAIL ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03510PH 53209 PITCH LINK WORN. 1G71 3U O H2SW 20020122001482002012200148SW 2002 1 22 HEEA077602 120011218G6320407310203101 MOUNT BELL 407 407 1182206SW TRANSMISSION CRACKED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03494PH 53396 TRANSMISSION MOUNT CRACKED RUBBER. 1G71 3U O H2SW 20020122001492002012200149SW 2002 1 22 HEEA077603 120011218G7712222375077119 TRANSMITTER BELL 407 407 1182206SW TORQUE METER MALFUNCTIONED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 TORQUE SPIKE TO 134.1 PERCENT FOR ONE SECOND. 1G71 3U O H2SW 20020122001502002012200150SW 2002 1 22 HEEA077604 120011218G6420406312100101 BEARING 407012101111BELL 407 407 1182206SW T/R HUB WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH 53006 53398 WORN. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#73147302. LABOR CREDIT ACCOMPLISHED ON J0194971-WA (INVOICE AND DMR NO. 687199). 1G71 3U O H2SW 20020122001512002012200151SW 2002 1 22 HEEA077607 120011218G6710406010425107 LEVER BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03498PH2031 53399 LEVER ASSY HAS WORN BUSHINGS. 1G71 3U O H2SW 20020123000012002012300001SW 2002 1 23 HEEA077608 120011218G6420406312100101 BEARING 407012101111BELL 407 407 1182206SW TAIL ROTOR HUB WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03492PH 53246 53390 TAIL ROTOR HUB BEARING WORN. 1G71 3U O H2SW 20020123000922002012300092SW 2002 1 23 HEEA077609 120011218G6510 BEARING BELL 407 407 1182206SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03407PH 53003 TAIL ROTOR BELLCRANK BEARING WORN. 1G71 3U O H2SW 20020123000022002012300002SW 2002 1 23 HEEA077610 120011218G6510 BEARING BELL 407 407 1182206SW BELLCRANK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH 53159 TAIL ROTOR BELLCRANK BEARING WORN. 1G71 3U O H2SW 20020123000032002012300003SW 2002 1 23 HEEA077611 120011218G6300 BEARING BELL 407 407 1182206SW PITCH LINK WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03402PH AF6463 53159 BEARING WORN. 1G71 3U O H2SW 20020123000042002012300004SW 2002 1 23 HEEA077612 120011218G6300406310405101 UNIVERSAL BELL 407 407 1182206SW M/R DRIVE WORN E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03490PH 53378 MAIN ROTOR DRIVE UNIVERSAL IS WORN. 1G71 3U O H2SW 20020123000052002012300005SW 2002 1 23 HEEA077613 120011218G6321206076047101 CYLINDER BELL 407 407 1182206SW MAIN ROTOR BRAKEDAMAGED E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03495PH 53397 MAIN ROTOR BRAKE CYLINDER HANDLE HARD TO OPERATE. 1G71 3U O H2SW 20020123000062002012300006SW 2002 1 23 HEEA077614 120011218G28221C2710 CARTRIDGE BELL 407 407 1182206SW FUEL PUMP INOPERATIVE E HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03719PH 53266 FUEL PUMP CARTRIDGE INOPERATIVE. 1G71 3U O H2SW 20020123000072002012300007SW 2002 1 23 HEEA077615 120011219G6320214040806003 PRESSURE SWITCH BELL 407 407 1182206SW M/R GEARBOX FAILED E HEEAK NONE L NO TEST ININSP/MAINT 1 SW03499PH 53400 WOULD NOT TURN ON TRANSMISSION LIGHT AFTER SHUTDOWN. 1G71 3U O H2SW 20020123000082002012300008SW 2002 1 23 HEEA077616 120011219G6300406310405101 UNIVERSAL BELL 407 407 1182206SW M/R DRIVE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH2367 53396 MAIN ROTOR DRIVE UNIVERSAL IS WORN. 1G71 3U O H2SW 20020123000092002012300009SW 2002 1 23 HEEA077617 120011219G6300406310405101 UNIVERSAL BELL 407 407 1182206SW M/R DRIVE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH671 53396 MAIN ROTOR DRIVE UNIVERSAL IS WORN. 1G71 3U O H2SW 20020123000102002012300010SW 2002 1 23 HEEA077618 120011219G6300406310405101 UNIVERSAL BELL 407 407 1182206SW M/R DRIVE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH1150 53396 MAIN ROTOR DRIVE UNIVERAL IS WORN. 1G71 3U O H2SW 20020123000112002012300011SW 2002 1 23 HEEA077619 120011219G6300406310405101 UNIVERSAL BELL 407 407 1182206SW M/R DRIVE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03494PH2201 53396 MAIN ROTOR DRIVE UNIVERSAL IS WORN. 1G71 3U O H2SW 20020123000122002012300012SW 2002 1 23 HEEA077620 120011219G6322206061432121 HOUSING BELL 407 407 1182206SW COOLER BLOWER DAMAGED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53393 COOLER BLOWER HOUSING HAS WORKING RIVETS. 1G71 3U O H2SW 20020123000132002012300013SW 2002 1 23 HEEA077621 120011219G2840407362005103 SWITCH BELL 407 407 1182206SW FUEL SYSTEM STUCK E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH 53386 SWITCH STICKING, INACCURATE READINGS TO GAUGE. 1G71 3U O H2SW 20020123000142002012300014SW 2002 1 23 HEEA077622 120011219G6420406312100101 BEARING 407012101111BELL 407 407 1182206SW TAIL ROTOR HUB WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03493PH 53400 53393 TAIL ROTOR HUB BEARING IS WORN. 1G71 3U O H2SW 20020123000152002012300015SW 2002 1 23 HEEA077623 120011219G7712222375077119 TRANSMITTER BELL 407 407 1182206SW TORQUE INDICATORFAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03402PH 53159 CEASED SENDING PRESSURE SIGNAL TO TORQUE GAUGE. 1G71 3U O H2SW 20020123000162002012300016SW 2002 1 23 HEEA077624 120011219G6300406310405101 UNIVERSAL BELL 407 407 1182206SW M/R DRIVE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03740PH916 53435 MAIN ROTOR DRIVE UNIVERSAL WORN. 1G71 3U O H2SW 20020123000172002012300017SW 2002 1 23 HEEA077625 120011219G6300406310405101 UNIVERSAL BELL 407 407 1182206SW M/R DRIVE WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03740PH916 53435 MAIN ROTOR DRIVE UNIVERSAL IS WORN. 1G71 3U O H2SW 20020123000182002012300018SW 2002 1 23 HEEA077626 120011219G2822407362013101 PRESSURE SWITCH BELL 407 407 1182206SW BOOST PUMP FAILED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH 53386 RIGHT FUEL BOOST PUMP LIGHT DOES NOT COME ON WHEN CIRCUIT BREAKER SWITCH IS TURNED OFF. 1G71 3U O H2SW 20020123000192002012300019SW 2002 1 23 HEEA077627 120011219G2510407370720101 SEAT BELT BELL 407 407 1182206SW COCKPIT FRAYED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH 53386 SEAT BELT HAS FRAYED ENDS. 1G71 3U O H2SW 20020123000952002012300095SW 2002 1 23 HEEA077628 120011219G6300406012129101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03501PH 53401 PITCH LINK BEARING WORN ON RIVET SIDE. 1G71 3U O H2SW 20020123000972002012300097SW 2002 1 23 HEEA077629 120011219G6300407340339101 BEARING BELL 407 407 1182206SW MAIN ROTOR ROUGH E HEEAK NONE O OTHER ININSP/MAINT 1 SW03492PH 53390 GREASE TURNING DARK GREY. BEARING ROUGH. 1G71 3U O H2SW 20020123000992002012300099SW 2002 1 23 HEEA077630 120011219G6300407340339101 BEARING BELL 407 407 1182206SW MAIN ROTOR OVERHEATED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03406PH 53198 MAIN ROTOR BEARING RUNNING HOT. LABEL TURNED BLACK. 1G71 3U O H2SW 20020123001002002012300100SW 2002 1 23 HEEA077631 120011219G6510206061432121 HOUSING BELL 407 407 1182206SW COOLER BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03501PH 53401 BLOWER HOUSING CRACKED AT LEFT HAND CORNER. 1G71 3U O H2SW 20020123001012002012300101SW 2002 1 23 HEEA077632 120011219G2822407362013101 PRESSURE SWITCH BELL 407 407 1182206SW ENGINE MALFUNCTIONED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03495PH 53397 LIGHT WILL NOT COME ON. 1G71 3U O H2SW 20020123001022002012300102SW 2002 1 23 HEEA077634 120011219G6300406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03490PH1910 53378 MAIN ROTOR UNIVERSAL WORN. 1G71 3U O H2SW 20020123001032002012300103SW 2002 1 23 HEEA077635 120011219G6510206061432121 HOUSING BELL 407 407 1182206SW COOLER BLOWER CRACKED E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH 53400 COOLER BLOWER HOUSING CRACKED. 1G71 3U O H2SW 20020123001042002012300104SW 2002 1 23 HEEA077638 120011219G6420 BEARING BELL 407 407 1182206SW PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03499PH 53400 BEARINGS WORN. 1G71 3U O H2SW 20020123001052002012300105SW 2002 1 23 HEEA077640 120011219G6420 BEARING BELL 407 407 1182206SW PITCH LINK WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03496PH 53398 PITCH LINK HAS WORN BEARINGS. 1G71 3U O H2SW 20020123001062002012300106SW 2002 1 23 HEEA077641 120011219G3212206050247138 COVER BELL 407 407 1182206SW FLOAT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH 53386 FLOAT COVER ASSY WORN. 1G71 3U O H2SW 20020123001072002012300107SW 2002 1 23 HEEA077642 120011219G3212206050247137 COVER BELL 407 407 1182206SW FLOAT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH 53386 FLOAT COVER END CAP WORN. 1G71 3U O H2SW 20020123001082002012300108SW 2002 1 23 HEEA077643 120011219G3212206050247132 COVER BELL 407 407 1182206SW FLOAT WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03491PH 53386 FLOAT COVER ASSY WORN. 1G71 3U O H2SW 20020123001092002012300109SW 2002 1 23 HEEA077644 120011219G6420406012129101 LINK BELL 407 407 1182206SW PITCH LINK ASSY WORN E HEEAK NONE O OTHER ININSP/MAINT 1 SW03407PH 53003 PITCH LINK ASSY WORN. 1G71 3U O H2SW 20020606000822002060600082SW 2002 6 6 HEEA079393 120010910G7740DPUA0101 COMPUTER BELL 206 206L3 1182108SW COCKPIT MALFUNCTIONED E K NONE O OTHER ININSP/MAINT 1 SW0341791 51465 INTELLISTART LIGHT STAYS ON, COULDN'T ACCESS WITH MLP. SENT TO ALTAIR AVIONICS CORP. FOR INSPECTION AND REPAIR. 1G71 3U H2SW 20010419001952001041900195 2001 4 19 HEED072193 420010314G22107690001802106 ACTUATOR SKRSKYS76 S76C 8143008NE AFCS ERRATIC E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03278X 760440 ERRATIC OPERATION WHEN CYCLIC ISMOVED TO THE RIGHT OF CENTER. REPLACED UNIT. 1G72 3U NCH1NE 20010419002182001041900218SW 2001 4 19 HEED072195 120010314G2435206062200113 STARTER GEN BELL 407 407 SW ENGINE FAILED E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW033193E 53276 PILOT INFLIGHT HEARD BANG IN HEADSET FOLLOWED BY SERVERE STATIC IN HEADSET. GENERATOR VOLTAGE METER STARTED DROPPING FROM 28 VOLTS UP ON LANDING. REPLACED UNIT. 1G71 3U O H2SW 20010419002192001041900219 2001 4 19 HEED072198 420010314G341606603640005 ENCODER BELL 407 407 SW ALTIMETER MALFUNCTIONED E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW033193E 53276 UNRELIABLE SIGNAL RYAN TCAD DISPLAYS STARS CODE. PART WAS BAD FROM STOCK. MODE C SIGNAL WAS 22,000 FT (SHOULD HAVE BEEN 1,000 FT) REPLACED UNIT. 1G71 3U O H2SW 20010419001962001041900196 2001 4 19 HEED072200 420010314G3454066107810 RECEIVER SKRSKYS76 S76C 8143008NE COCKPIT INOPERATIVE E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03476X 760436 DOES NOT DRIVE NR 1 POINTER ON HSI PILOTS OR COPILOTS. REPLACED UNIT. 1G72 3U NCH1NE 20010419001972001041900197 2001 4 19 HEED072201 420010314G2300A30161ACR MIXER BOX SKRSKYS76 S76C 8143008NE COCKPIT INTERMITTENT E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03476X 760436 INTERMITTANT LOSS OF HEADSET SIDETONE. REPLACED UNIT. 1G72 3U NCH1NE 20010419001982001041900198NE 2001 4 19 HEED072202 120010314G79200292105230 PUMP SKRSKYS76 S76C 8143008NE OIL SYSTEM FAILED E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03476X 760436 OIL DRAINS BACK INTO ACCESSORY GEARBOX AFTER SHUTDOWN. REPLACED UNIT. 1G72 3U NCH1NE 20010419001992001041900199NE 2001 4 19 HEED072203 220010314G74219550166670 IGNITER SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE ENGINE WEAK E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03476X 760436 WEAK- WILL NOT START AIRCRAFT. FOUND BAD ON 150 HOURS INSPECTION. REPLACED UNIT. 1G72 3U3 UNCH1NE E19EU 20010419002002001041900200NE 2001 4 19 HEED072204 220010314G72109560134100 MAGNETIC SEAL SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE ENGINE LEAKING E HEEDO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03476X 760436 THIS SEAL LEAKED SINCE THE ENGINE 15529 WAS INSTALLED ON 9/7/2000 AT ATT: 4867.15 REPLACED UNIT. 1G72 3U3 UNCH1NE E19EU 20010419002012001041900201 2001 4 19 HEED072205 420010314G2300A30161ACR MIXER BOX SKRSKYS76 S76C 8143008NE COCKPIT INTERMITTENT E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03478X 760493 BOX CUTS OUT IN ICS. REPLACED UNIT. 1G72 3U NCH1NE 20010419002022001041900202 2001 4 19 HEED072206 420010314G2300A30161ACR MIXER BOX SKRSKYS76 S76C 8143008NE COCKPIT INTERMITTENT E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03478X 760493 INTERMITTLY INOPERATIVE COMPLETELY IN ALL SWITCH POSITIONS. REPLACED UNIT. 1G72 3U NCH1NE 20010419002032001041900203 2001 4 19 HEED072207 420010314G2300A30161ACR MIXER BOX SKRSKYS76 S76C 8143008NE COCKPIT MALFUNCTIONED E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03278X 760440 THIDS ICS BOX WAS JUST RETURNED FROM REPAIR FOR THE SAME THING-BLEED OVER ON VHF''''S AND NAV''''S. REPLACED UNIT. 1G72 3U NCH1NE 20010419002042001041900204NE 2001 4 19 HEED072208 120010314G29107665009801104 MODULE SKRSKYS76 S76C 8143008NE HYD SYSTEM MALFUNCTIONED E HEEDO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03478X 760493 HYD MODULE CAUSES INTERMITT 32 SYSTEM SERVO LITE. REPLACED UNIT. 1G72 3U NCH1NE 20010419002052001041900205NE 2001 4 19 HEED072211 120010314G62107615009100053 BLADE SKRSKYS76 S76C 8143008NE MAIN ROTOR CRACKED E HEEDK NONE O OTHER ININSP/MAINT 1 SW03476X 760436 SUSPECT CRACKING OF MAIN ROTOR SPAR. REPLACED UNIT. 1G72 3U NCH1NE 20010419002062001041900206NE 2001 4 19 HEED072212 220010314G74219550166670 IGNITER SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE ENGINE ERODED E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03476X 760436 ERODED CENTER ELECTRODE. REPLACED UNIT. 1G72 3U3 UNCH1NE E19EU 20010419002072001041900207NE 2001 4 19 HEED072213 220010314G72610292105230 PUMP SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE OIL SYSTEM FLUCTUATES E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03476X 760436 15529TEC FLUCTUATING OIL PRESSURE . REPLACED UNIT. 1G72 3U3 UNCH1NE E19EU 20010419002082001041900208NE 2001 4 19 HEED072214 120010314G243750284003 PANEL SKRSKYS76 S76C 8143008NE COCKPIT WILL NOT TEST E HEEDO OTHER L NO TEST NRNOT REPORTED 1 SW03476X 760436 BATTERY FEED FAULT WILL NOT TEST PROPERLY. REPLACED UNIT. 1G72 3U NCH1NE 20010419002092001041900209 2001 4 19 HEED072215 420010314G34578144002241D GPS SKRSKYS76 S76C 8143008NE COCKPIT MALFUNCTIONED E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03476X 760436 COPILOT HSI NEEDLE WILL NOT POINT TO LRN HEADING, SYSTEM WENT OFFLINE AND LOST. REPLACED UNIT. 1G72 3U NCH1NE 20010419002102001041900210NE 2001 4 19 HEED072216 220010314G72001S1 ENGINE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE ENGINE BAY MAKING METAL E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW0389H 760406 GENERATING METAL AT THE ACCESSORY MAG PLUG. REPLACED UNIT. 1G72 3U3 UNCH1NE E19EU 20010419002112001041900211NE 2001 4 19 HEED072218 120010315G6220SB5080102 ROD END BEARING SKRSKYS76 S76C 8143008NE MAIN ROTOR WORN E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW0389H 760406 BEARING WORN. REPLACED UNIT. 1G72 3U NCH1NE 20010419002122001041900212 2001 4 19 HEED072220 420010315G2300A30161ACYR MIXER BOX SKRSKYS76 S76C 8143008NE COCKPIT INTERMITTENT E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03278X 760440 ICS BOX INTERMITTENT OPERATION IN ALL CHANNELS. REPLACED UNIT. 1G72 3U NCH1NE 20010419002132001041900213NE 2001 4 19 HEED072221 120010315G79228A308203 THERMOSTAT SKRSKYS76 S76C 8143008NE OIL TEMP MALFUNCTIONED E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW0389H 760406 CAUSING HIGH OIL TEMPERATURE. LOCALLY SCRAPPED. REPLACED UNIT. 1G72 3U NCH1NE 20010420000792001042000079NE 2001 4 20 HEED072223 120010315G324650075551 WHEEL SKRSKYS76 S76C 8143008NE NLG WORN E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW0389H 760406 LININGS P/N 50007665, WORN. REPLACED UNIT. 1G72 3U NCH1NE 20010419002142001041900214 2001 4 19 HEED072224 420010315G2300A30161ACR MIXER BOX SKRSKYS76 S76C 8143008NE COCKPIT INTERMITTENT E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW0389H 760406 CUTS OUT ALL STATIONS DURING TRANSMITTION AND RECEPTION. REPLACED UNIT. 1G72 3U NCH1NE 20010419002152001041900215NE 2001 4 19 HEED072225 120010315G324650075551 WHEEL SKRSKYS76 S76C 8143008NE NLG WORN E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW0389H 760406 LININGS ARE WORN. REPLACED UNIT. 1G72 3U NCH1NE 20010419002202001041900220SW 2001 4 19 HEED072226 120010315G2841407375006101 INDICATOR BELL 407 407 SW FUEL QUANITY INOPERATIVE E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW033193E 53276 DISPLAY, BLANK, NO NUMBER ON BARS SHOWING. REPLACED UNIT. 1G71 3U O H2SW 20010419002212001041900221SW 2001 4 19 HEED072233 120010315G3244028630 TIRE BELL 430 430 1182150SW MLG WORN E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03430X 857 49058 EXCESSIVE WEAR. REPLACED UNIT. 1G72 3U RTH9SW 20010419002162001041900216NE 2001 4 19 HEED072251 120010316G36107650007903102 SHUTOFF VALVE SKRSKYS76 S76C 8143008NE BLEED AIR LEAKING E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW0389H 760406 LEAKING WILL NOT SHUT OFF. REPLACED UNIT. 1G72 3U NCH1NE 20010419002172001041900217NE 2001 4 19 HEED072254 220010316G72109560115450 MAGNETIC SEAL SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE ENGINE LEAKING E HEEDO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03476X 760436 THIS SEAL LEAKED SINCE THE ENGINE S/N 15529 WAS INSTALLED ON 9/7/2000. REPLACED UNIT. 1G72 3U3 UNCH1NE E19EU 20010807003382001080700338 2001 8 7 HEED073491 420010614G2350A30161ACVR ICS BOX SKRSKYS76 S76C 8143008NE COCKPIT INTERMITTENT E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03478X 61 760493 INTERMITTENTLY TRANSMISSION ON ALL CHANNELS. REPLACED UNIT. 1G72 3U NCH1NE 20010807003392001080700339NE 2001 8 7 HEED073492 120010614G33403012543 LIGHT SKRSKYS76 S76C 8143008NE STROBE BURNED OUT E HEEDK NONE O OTHER ININSP/MAINT 1 SW03478X 760493 FLASH TUBE BURNED OUT. SCRAPPED REPLACED UNIT. 1G72 3U NCH1NE 20010807003402001080700340NE 2001 8 7 HEED073493 120010614G7714H190110 INDICATOR SKRSKYS76 S76C 8143008NE ENGINE N1 FAILED E HEEDK NONE O OTHER ININSP/MAINT 1 SW03478X 760493 PIECES OF LED SECTIONS MISSING IN NUMBER DISPLAY. BURNED OUT. REPLACED UNIT. 1G72 3U NCH1NE 20010807003412001080700341NE 2001 8 7 HEED073494 120010614G2432RG380E44 BATTERY SKRSKYS76 S76C 8143008NE MAIN DISCHARGED E HEEDK NONE L NO TEST ININSP/MAINT 1 SW03478X 760493 WOULD CRANK AIRCRAFT ENGINES TO START BATTERY DEAD. VERY WEAK ON FIRST START OFTHE DAY. REPLACED UNIT. 1G72 3U NCH1NE 20010807003442001080700344NE 2001 8 7 HEED073495 120010614G3110 SCREW SKRSKYS76 S76C 8143008NE AHRS BROKEN E HEEDK NONE O OTHER ININSP/MAINT 1 SW03476X 3507 1005 760436 J2 PLUG ATTACHMENT SCREW IS BROKEN. REPLACED UNIT. 1G72 3U NCH1NE 20010807003462001080700346NE 2001 8 7 HEED073496 120010614G53209550147560 FITTING SKRSKYS76 S76C 8143008NE THREADS CORRODED E HEEDK NONE O OTHER ININSP/MAINT 1 SW03476X 760436 INTERNAL THREADS FOR BANJO FITTING ARE CORRODED. REPLACED UNIT. 1G72 3U NCH1NE 20010807003472001080700347NE 2001 8 7 HEED073497 220010614G73210164348810 FUEL CONTROL SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE ENGINE MALFUNCTIONED E HEEDK NONE O OTHER ININSP/MAINT 1 SW03476X 760436 N2 LAGS CREATING A 20 PERCENT TORQUE SPLIT. REPLACED UNIT. 1G72 3U3 UNCH1NE E19EU 20010807003512001080700351NE 2001 8 7 HEED073498 220010614G7261 CHECK VALVE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE OIL PUMP STUCK E HEEDK NONE O OTHER ININSP/MAINT 1 SW03476X 722SO 760436 CHECK VALVE STICKING. REPLACED UNIT. 1G72 3U3 UNCH1NE E19EU 20010807003532001080700353NE 2001 8 7 HEED073499 120010614G2560110175601 SEAT BELT SKRSKYS76 S76C 8143008NE COCKPIT WORN E HEEDK NONE O OTHER ININSP/MAINT 1 SW03476X 5687 760436 WORN SEAT BELT. REPLACED UNIT. 1G72 3U NCH1NE 20010807003552001080700355 2001 8 7 HEED073500 420010614G2210 BEARING SKRSKYS76 S76C 8143008NE AFCS ACTUATOR WORN E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW0389H 760406 PIVOT BEARINGS WORN. REPLACED UNIT. 1G72 3U NCH1NE 20010807003572001080700357 2001 8 7 HEED073501 420010614G2312071128265 CONTROL HEAD SKRSKYS76 S76C 8143008NE VHF SYSTEM MALFUNCTIONED E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW0389H 760406 TURNS ITSELF OFF AFTER 2 OR 3 MINUTES. REPLACED UNIT. 1G72 3U NCH1NE 20010807003592001080700359 2001 8 7 HEED073502 420010614G2350A30161ACVR ICS BOX SKRSKYS76 S76C 8143008NE COCKPIT NOISY E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW0389H 760406 LOUD NOISE IN MIC. REPLACED UNIT. 1G72 3U NCH1NE 20010807003612001080700361 2001 8 7 HEED073503 420010614G2350A30161ACVR ICS BOX SKRSKYS76 S76C 8143008NE COCKPIT FAILED E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW0389H 760406 COPILOT HEADSET FREQUENTLY CUTS OUT. BAD FROM STOCK. REPLACED UNIT. 1G72 3U NCH1NE 20010807003632001080700363 2001 8 7 HEED073504 420010614G2350A30161ACVR ICS BOX SKRSKYS76 S76C 8143008NE COCKPIT FAILED E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW0389H 760406 COPILOT HEADSET FREQUENTLY CUTS OUT. BAD FROM STOCK. REPLACED UNIT. 1G72 3U NCH1NE 20010807003652001080700365 2001 8 7 HEED073505 420010614G22107690001802106 ACTUATOR SKRSKYS76 S76C 8143008NE AFCS CHATTERING E HEEDK NONE O OTHER ININSP/MAINT 1 SW03478X 760493 CHATTERING. REPLACED UNIT. 1G72 3U NCH1NE 20010807003662001080700366NE 2001 8 7 HEED073506 220010614G720070BMA01040 CONTROL UNIT SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE ENGINE FAILED E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03478X 2968 760493 20063 NR 1 ENGINE RUN UP FAULT. REPLACED UNIT. 1G72 3U3 UNCH1NE E19EU 20010807003672001080700367 2001 8 7 HEED073507 420010614G2370D5152010112 CVR SKRSKYS76 S76C 8143008NE COCKPIT WILL NOT TEST E HEEDK NONE L NO TEST ININSP/MAINT 1 SW03478X 760493 FDR WILL NOT TEST. REPLACED UNIT. 1G72 3U NCH1NE 20010807003682001080700368 2001 8 7 HEED073508 420010614G22107690001802106 ACTUATOR SKRSKYS76 S76C 8143008NE AFCS INTERMITTENT E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03478X 760493 KICKING INTERMITTLY. REPLACED UNIT. 1G72 3U NCH1NE 20010807003962001080700396 2001 8 7 HEED073511 420010614G22107690001802106 ACTUATOR SKRSKYS76 S76C 8143008NE AFCS CHATTERING E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW03278X 760440 CHATTERING, ROUGH IN TRAVEL, STICKING. REPLACED UNIT. 1G72 3U NCH1NE 20010807003982001080700398NE 2001 8 7 HEED073512 120010614G3240 BRAKE SKRSKYS76 S76C 8143008NE NLG WORN E HEEDK NONE O OTHER ININSP/MAINT 1 SW03278X 760440 WORN BRAKES. S/NOS: DEC-82-217, AND NOV-3-467. REPLACED UNIT. S/NOS: JAN 80-286, AND MAR 84-677. 1G72 3U NCH1NE 20010807003992001080700399 2001 8 7 HEED073513 420010614G22107690001802106 ACTUATOR SKRSKYS76 S76C 8143008NE AFCS CHATTERING E HEEDK NONE O OTHER ININSP/MAINT 1 SW03278X 760440 JUMPING, CHATTERING. REPLACED UNIT. 1G72 3U NCH1NE 20010807004012001080700401NE 2001 8 7 HEED073514 120010614G32304608 PRIORITY VALVE SKRSKYS76 S76C 8143008NE MLG FAULTY E HEEDK NONE O OTHER ININSP/MAINT 1 SW03278X 5007 760440 IRREGULAR PRESSURE CAUSES RANGING GEAR TO RETRACT UNEVENLY. REPLACED UNIT. 1G72 3U NCH1NE 20010807004032001080700403SW 2001 8 7 HEED073543 120010614G3260222336001105 ACTUATOR BELL 430 430 1182150SW DOWNLOCK LEAKING E HEEDK NONE O OTHER ININSP/MAINT 1 SW03430X 1081 49058 LEAKS. REPLACED UNIT. 1G72 3U RTH9SW 20010807004282001080700428SW 2001 8 7 HEED073545 120010614G7400FCB205AT9 RELAY BELL 407 407 SW ALLSN 250B 250B* GL IGNITER FAILED E HEEDO OTHER O OTHER NRNOT REPORTED 1 SW033193E1986 53276 AUTO RELIGHT ON CAUTION PANEL FAILED TO COME ON AT ENGINE START ATTEMPLT AND NO ENGINE IGNITION OR LIGHT OFF. SCRAPPED. REPLACED UNIT. 1G71 3U3 TO H2SW E10CE 20010807004292001080700429GL 2001 8 7 HEED073546 220010614G7421CH34187A IGNITER BELL 407 407 SW ALLSN 250B 250B* GL ENGINE CRACKED E HEEDK NONE O OTHER ININSP/MAINT 1 SW033193E1986 53276 CRACKED CERAMIC AND ERROIDED TIP. REPLACED UNIT. 1G71 3U3 TO H2SW E10CE 20010807004302001080700430SW 2001 8 7 HEED073548 120010614G6500ES731861 BLOWER BELL 407 407 SW TAIL ROTOR SHORTED E HEEDK NONE O OTHER ININSP/MAINT 1 SW033193E 53276 POPS CIRCUIT BREAKER. REPLACED UNIT. 1G71 3U O H2SW 20010807004312001080700431SW 2001 8 7 HEED073549 120010614G2841407375006101 INDICATOR BELL 407 407 SW FUEL QUANITY FAILED E HEEDK NONE O OTHER ININSP/MAINT 1 SW033193E 53276 DISPLAY BLANK REPLACED UNIT. 1G71 3U O H2SW 20010807004322001080700432 2001 8 7 HEED073550 420010614G3120775330200 CLOCK BELL 407 407 SW COCKPIT STOPPED E HEEDK NONE O OTHER ININSP/MAINT 1 SW033193E 53276 CLOCK STOPPED. REPLACED UNIT. 1G71 3U O H2SW 20010807004332001080700433SW 2001 8 7 HEED073552 120010614G6322407040303101 SHAFT BELL 407 407 SW FAN VIBRATION E HEEDO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW033193E1178 53276 HIGH RDA VIBRATION LEVEL. REPLACED UNIT. 1G71 3U O H2SW 20010807004342001080700434SW 2001 8 7 HEED073553 120010614G6510ES731861 MOTOR BELL 407 407 SW BLOWER FAILED E HEEDK NONE O OTHER ININSP/MAINT 1 SW033193E 53276 POP CIRCUIT BREAKER. REPLACED UNIT. 1G71 3U O H2SW 20010924001012001092400101SW 2001 9 24 HEED073554 120010614G6300406310405101 BEARING BELL 407 407 SW P/C LINK WORN E HEEDK NONE O OTHER ININSP/MAINT 1 SW033193E2164 53276 WORN BEARINGS, SCRAPPED. REPLACED UNIT. 1G71 3U O H2SW 20010924001032001092400103SW 2001 9 24 HEED073555 120010614G6300406010417101 BEARING BELL 407 407 SW P/C LINK WORN E HEEDK NONE O OTHER ININSP/MAINT 1 SW033193E2189 53276 WORN BEARINGS, SCRAPPED. REPLACED UNIT. 1G71 3U O H2SW 20010924001042001092400104SW 2001 9 24 HEED073556 120010614G6300406010417101 BEARING BELL 407 407 SW P/C LINK WORN E HEEDK NONE O OTHER ININSP/MAINT 1 SW033193E2189 53276 WORN BEARINGS, SCRAPPED. REPLACED UNIT. 1G71 3U O H2SW 20010924001052001092400105SW 2001 9 24 HEED073557 120010614G7931222375077113 TRANSMITTER BELL 407 407 SW OIL PRESSURE FLUCTUATES E HEEDK NONE O OTHER ININSP/MAINT 1 SW033193E2065 53276 FLUCTUATING OIL PRESSURE. REPLACED UNIT. 1G71 3U O H2SW 20010713000792001071300079NM 2001 7 13 HN6R0000218 120010618G5311 FRAME BOEING737 737400 NM FUSELAGE CRACKED B HN6RK NONE O OTHER ININSP/MAINT 1 NM01932NU 25248 BS 827 FRAME IS CRACKED AT PSU RAIL ATTACHMENT BRACKET INBOARD FASTENER (LEFT HAND SIDE). CAUSE UNKNOWN . REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED. 2L72 4F RTA16WE 20020123001332002012300133EU 2002 1 23 ISHA077178 120011119G6520350A3310021 PINION GEAR 350A33020005SNIAS 350 AS350D 8680803EU T/R GEARBOX DEFECTIVE H ISHAK NONE O OTHER ININSP/MAINT 1 FS0167GE 3243 M1280 1604 GEAR REJECTED AT INTERMOUNTAIN TURBINE FOR PITTING AND UNABLE TO ESTABLISH PROPER STATIC GEAR PATTERN REPLACED ASSY. WITH EXCHANGE 1G71 3U H9EU 20020123001342002012300134EU 2002 1 23 ISHA077179 120011119G6520350A33100121 BEVEL GEAR 350A33020005SNIAS 350 AS350D 8680803EU T/R GEARBOX DEFECTIVE H ISHAK NONE O OTHER ININSP/MAINT 1 FS0167GE 3243 M1280 1604 REJECTED BY NAMPA VALLEY HELICOPTERS DUE TO PITTING AND UNABLE TO ESTABLISH STATIC GEAR PATTERN REPLACED WITH EXCHANGE ASSY. 1G71 3U H9EU 20010924001072001092400107EU 2001 9 24 IVSA074819 120010806G3340122394R5123 MODULE UROCOPEC120 EC120B 8680987EU LIGHT BURNED OUT H IVSAO OTHER O OTHER CRCRUISE 1 FS01166DL227 1066 PILOT REPORTED ANTI COLLISION LIGHT INOP. FLASH TUBE FOUND BURNED AND CRACKED. REPLACEMENT TUBE ORDERED AND INSTALLED. OPS CHECKED OK. 1G72 3U NCR0001RD 20010924001082001092400108WP 2001 9 24 IVSA075461 120010831G6310D2761 ACTUATOR ROBSINR44 R44 7640120WP CLUTCH DEFECTIVE H IVSAO OTHER O OTHER NRNOT REPORTED 1 FS01UNK 76 1031 MOTOR FAILED TO OPERATE WHEN CALLED ON TO ENGAGE M/R DRIVE BELTS. WOULD NOT OPERATE IN EITHER DIRECTION. MOTOR REPLACED, DEFECTIVE MOTOR RETURNED TOROBINSON FOR WARRANTY CREDIT. 1G71 3O H11NM 20011004000912001100400091WP 2001 10 4 IVSA075920 120010924G6320D2761 ACTUATOR ROBSINR44 R44 7640120WP CLUTCH FAILED H IVSAO OTHER O OTHER NRNOT REPORTED 1 FS017189C176 1031 CLUTCH ACTUATOR MOTOR FAILED FOR THE 2ND TIME. REPLACEMENT MOTOR INSTALLED. FURTHER TOUBLESHOOTING REVEALED SHEAVE ALIGNMENT OUT OF LIMITS CAUSING INFLIGHT ILLUMINATION OF CLUTCH LIGHT. ALIGNMENT CORRECTED AND FLIGHTS CONTINUED NORMALLY. BAD MOTOR RETURNED FOR WARRANTY CREDIT. 1G71 3O H11NM 20020110001622002011000162EU 2002 1 10 IVSA076105 120011003G6210355A11002009 BLADE AEROSPAS355 AS355* EU MAIN ROTOR CRACKED H IVSAK NONE O OTHER ININSP/MAINT 1 FS01335FP4892 5456 BLADE REMOVED FOR REPAIR OF LEADING EDGE ABRASION STRIP CRACKS. CUSTOMER REQUESTED EXCHANGE BLADE IN ORDER TO RESUME FLIGHTS. EXCHANGE BLADE INSTALLED, REPAIRABLE BLADE RETURNED TO AEC 1G72 3U H11EU 20020123001362002012300136WP 2002 1 23 IVSA077371 120011212G6300D1742 WHEEL ROBSINR44 R44 7640120WP CENTER HUB CORRODED H IVSAK NONE O OTHER ININSP/MAINT 1 FS017186Z190 737C PAINT ON FAN WHEEL LOOSE AND FLAKING OFF DUE TO POOR ADHESION, PROBABLY CAUSED BY IMPROPER PREPARATION, ALLOWING PREMATURE CORROSION. 1G71 3O H11NM 20010924001112001092400111SW 2001 9 24 JJWA073276 120010612G6320206040236017 HOUSING BELL 206 206B 1181511SW GEARBOX STRIPPED H JJWAK NONE O OTHER ININSP/MAINT 1 FS015005N8864 1931 STUD PULLED OUT WITH LESS THAN 50 INCH POUND ON TORQUE WRENCH WHEN INSTALLING FW UNIT IN ENGINE - HIDDEN DAMAGE NOT FOUND BY BELL CSF OVERHAUL FACILITY. NEW HOUSING SENT BY CSF. 1G71 3U H2SW 20020124000012002012400001SW 2002 1 24 JJWA077061 120011105G6710206062721113 ACTUATOR BELL 206 206B 1181511SW MAIN ROTOR CORRODED H JJWAK NONE O OTHER ININSP/MAINT 1 FS01281CB 3303 ACTUATOR FAILED AFTER FEBRUARY 2001 OVERHAUL. NO ALODINE OR OTHER CORROSION PROTECTION ON INSIDE OF CASE.INTERNAL CORROSION CAUSED FAILURE. 1G71 3U H2SW 20011211001362001121100136NE 2001 12 11 JV652J 220010828G7250UL36199 CASE RROYCERB211 RB211535E4 54555NE ENGINE CRACKED D K NONE O OTHER ININSP/MAINT 1 SW07 21825 ESN31340 CASE ASSEMBLY EXHIBITED 2 AXIAL CRACKS APPROXIMATELY 2.0 INCHES IN LENGTH AND 3.5 TO 4 INCHES APART. CRACKS PROPAGATED THROUGH THE CASE WALL. CASE HAD 7277 TOTAL CYCLE. 4 F E12EU 20010405001102001040500110EU 2001 4 5 KBMA88583 120010205G6520350A33215300 LAMINATED HINGE SNIAS 350 AS350BA 8680817EU TAIL ROTOR DELAMINATED E KBMAK NONE O OTHER ININSP/MAINT 1 WP191188P9755 2347 HINGE DELAMINATED 1G71 3U NCH9EU 20010307006302001030700630EU 2001 3 7 KBMA88585 120010127G6720350A33214501 BUSHING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE T/R ROD BEARING CRACKED I KBMAK NONE O OTHER ININSP/MAINT 1 WP19115SH2136 3141 BUSHING CRACKED 1G71 3U3 U H9EU E19EU 20010307006332001030700633EU 2001 3 7 KBMA88634 120010127G5320350A54112420 BRACKET SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE STARTER GEN CRACKED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19115SH2136 3141 STARTER GENTERATOR AIR VENT DUCT BRACKET IS CRACKED. 1G71 3U3 U H9EU E19EU 20010307006312001030700631EU 2001 3 7 KBMA88637 120010201G77140177555170 CONTROL BOX SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TACH GEN MALFUNCTIONED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19350SH4435 2957 TACH BOX CLOSES BLEED VALVE AT 96% AND OPENS AT 95% 1G71 3U3 UNCH9EU E19EU 20010307006292001030700629EU 2001 3 7 KBMA88638 120010127G5320TL100AXE12L50DK LATCH SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE FUSELAGE STUCK I KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19180EH3439 2337 LATCH WAS STICKING. 1G71 3U3 UNCH9EU E19EU 20010307006212001030700621EU 2001 3 7 KBMA88639 120010130G291512TW13 SWITCH SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1 60030NE HYDRAULIC SYSTEMINOPERATIVE E KBMAK NONE O OTHER ININSP/MAINT 1 WP1937SH 9207 2300 HYDRAULIC SWITCH WAS FAULTY. 1G71 3U3 U H9EU E19EU 20010405001002001040500100EU 2001 4 5 KBMA88643 120010215G7110350A58154322 HINGE PIN SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ENG COWLING BROKEN E KBMAK NONE O OTHER ININSP/MAINT 1 WP19115SH2169 3141 COWLING HINGE PIN BROKEN. 1G71 3U3 U H9EU E19EU 20010405001242001040500124EU 2001 4 5 KBMA88645 120010217G77129580113720 TRANSMITTER SNIAS 350 AS350B 8680801EU TORQUE INDICATORINOPERATIVE E KBMAK NONE L NO TEST ININSP/MAINT 1 WP1937SH 9250 2300 TORQUE GUAGE NOT WORKING PROPERLY. 1G71 3U H9EU 20010405001052001040500105 2001 4 5 KBMA88646 420010218G2312064105430 VHF COMM SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE COCKPIT INOPERATIVE E KBMAK NONE L NO TEST ININSP/MAINT 1 WP19350SH4474 2957 VHF INOPERATIVE, COMES ON ONLY WHEN VOLUME IS ALL THE WAY DOWN. 1G71 3U3 UNCH9EU E19EU 20010405001062001040500106 2001 4 5 KBMA88649 420010220G2312064010540030 VHF COMM SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE COCKPIT MALFUNCTIONED E KBMAK NONE L NO TEST ININSP/MAINT 1 WP191188P9792 2347 VHF HAS CONSTANT SQUELCH ON AFTER APPROX 30 MINUTES OF OPERATION. WILL NOT RESET. 1G71 3U3 UNCH9EU E19EU 20010405001092001040500109GL 2001 4 5 KBMA88679 220010227G73107G547 PRESSURE SWITCH BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL FUEL SYSTEM MALFUNCTIONED E KBMAK NONE J WARNING INDICATION ININSP/MAINT 1 WP19667JM9830 3444 FUEL PRESSURE SWITCHES NOT OPERATING PROPERLY. CAUTION LITE REMAINS ON WITH CIRCUIT BREAKER IN. 1G71 3U3 U H2SW E4CE 20010503000022001050300002NE 2001 5 3 KBMA88694 220010320G72109560134100 MAGNETIC SEAL SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE ENGINE LEAKING B KBMAK NONE K FLUID LOSS ININSP/MAINT 1 WP19230SH3523 2337 ENGINE FRONT MAG SEAL LEAKING. 1G71 3U3 UNCH9EU E19EU 20010503000042001050300004EU 2001 5 3 KBMA88695 120010320G6420350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN B KBMAK NONE O OTHER ININSP/MAINT 1 WP19230SH3523 2337 TAIL ROTOR TETTER BEARINGS WORN. 1G71 3U3 UNCH9EU E19EU 20010503000202001050300020EU 2001 5 3 KBMA88698 120010320G6220 BUSHING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR DEBONDED B KBMAK NONE O OTHER ININSP/MAINT 1 WP19230SH3523 2337 REBONDED BUSHING. DUE TO STATIONARY SCISSORS BUSHING DEBONDED. 1G71 3U3 UNCH9EU E19EU 20010417000182001041700018NE 2001 4 17 KBMA88699 220010320G74149560137520 MAGNETO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE RIGHT LEAKING C KBMAK NONE O OTHER ININSP/MAINT 1 WP19230SH3523 2337 REAR ENGINE MAGNETO SEAL LEAKING. 1G71 3U3 UNCH9EU E19EU 20010503000222001050300022EU 2001 5 3 KBMA88700 120010320G24359560134100 MAGNETIC SEAL SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE ENGINE LEAKING B KBMAK NONE K FLUID LOSS ININSP/MAINT 1 WP19230SH3523 2337 STARTER GENERATOR MAGNETIC SEAL LEAKING. REMOVED AND REPLACED SEAL. 1G71 3U3 UNCH9EU E19EU 20010417000202001041700020 2001 4 17 KBMA88706 420010317G34225050031904 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE COCKPIT PRECESSES C KBMAK NONE O OTHER ININSP/MAINT 1 WP19345SH69 3345 DIRECTIONAL GYRO RAPIDLY PRESSESSING. GYRO HAD APPROX. 10 HOURS ON UNIT. 1G71 3U3 U H9EU E19EU 20010417000172001041700017EU 2001 4 17 KBMA88707 120010318G6710SC5083 SERVO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR LEAKING C KBMAK NONE K FLUID LOSS ININSP/MAINT 1 WP19115SH2268 3141 LEAKING FROM WEEPHOLE. 1G71 3U3 U H9EU E19EU 20010417000232001041700023EU 2001 4 17 KBMA88709 120010318G77129580113720 TRANSMITTER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE ENGINE TORQUE MALFUNCTIONED C KBMAK NONE O OTHER ININSP/MAINT 1 WP19270SH7577 1864 NEEDLE MOVES TO UPPER LIMIT OF SCALE AND STOPS THERE FOR A COUPLE OF MINUTES. 1G71 3U3 UNCH9EU E19EU 20010417000212001041700021NE 2001 4 17 KBMA88711 220010323G7412955016870 IGNITER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE RIGHT INTERMITTENT C KBMAK NONE O OTHER ININSP/MAINT 1 WP19270SH7599 1864 RIGHT IGNITER INTERMITTENT. 1G71 3U3 UNCH9EU E19EU 20010417000192001041700019EU 2001 4 17 KBMA88712 120010311G7410HE402F IGNITER BOX SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE RIGHT INOPERATIVE C KBMAK NONE O OTHER ININSP/MAINT 1 WP191188P9846 2347 RIGHT IGNITOR IS INOPERATIVE. 1G71 3U3 UNCH9EU E19EU 20010417000222001041700022NE 2001 4 17 KBMA88713 220010312G7230420800003 FAN SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ENGINE CHAFED C KBMAK NONE O OTHER ININSP/MAINT 1 WP1953SH 4998 2009 FAN BLADES HITTING HOUSING. ADJUSTED BLADES. OPS CHECKED GOOD. 1G71 3U3 U H9EU E19EU 20010529000402001052900040EU 2001 5 29 KBMA88728 120010418G555322201BC060016L BOLT SNIAS 350 AS350BA 8680817EU VERTICAL STAB SHEARED E KBMAK NONE O OTHER NRNOT REPORTED 1 WP19270SH7704 1864 BOLTS SHEARED, INSTALLED NEW BOLTS AS REQUIRED. 1G71 3U NCH9EU 20010405001082001040500108 2001 4 5 KBMA88818 420010208G34215040017901 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE COCKPIT INOPERATIVE E KBMAK NONE O OTHER ININSP/MAINT 1 WP19270SH7475 1864 PRECESSING AND FLAG INDICATOR INOPERATIVE. 1G71 3U3 UNCH9EU E19EU 20010405001072001040500107 2001 4 5 KBMA88819 420010208G3422200DCL GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE COCKPIT MALFUNCTIONED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19270SH7475 1864 DIRECTIONAL GYRO MAKES EXCESSIVE NOISE. 1G71 3U3 UNCH9EU E19EU 20010405001252001040500125EU 2001 4 5 KBMA99419 120010109G6520350A33215001 BEARING SNIAS 350 AS350BA 8680817EU TAIL ROTOR WORN E KBMAK NONE O OTHER ININSP/MAINT 1 WP19350SH4396 2957 BEARING WORN. 1G71 3U NCH9EU 20011004001382001100400138EU 2001 10 4 KUVA075921 120010928G6420109013105111 PIVOT AGUSTAA109 A109A2 0260120EU TAIL ROTOR WORN H KUVAK NONE O OTHER ININSP/MAINT 1 FS01584RH2361 7356 T/R TURNNION P/N 109-0131-05-111 TT: 2360.8. THE TRUNNION SHOWED SIGNIFIGANT WEAR AT DISSASSEMBLY AFTER THE PILOT NOTED A HIGH FREQUENCY VIBRATION. THE AGUSTA T/R ASSY IS SUBJECT TO BECOMING STIFF, WHEN THIS OCCURS THE T/R HUB SHOULD BE COMPLETELY DISSASSEMBLED AND INSPECTED FOR WEAR. I WOULD SUGGEST AGUSTA INSTITUTE A SCHEDULED INSPECTION PRIOR TO THE 2400 HR. INSPECTION THAT IS NOW IN PLACE. 1G72 3U H7EU 20011004001402001100400140EU 2001 10 4 KUVA075922 120010928G6420109013105111 PIVOT AGUSTAA109 A109 0260109EU TAIL ROTOR WORN H KUVAK NONE O OTHER ININSP/MAINT 1 FS01584RH2361 7356 T/R TURNNION P/N 109-0131-05-111 TT: 2360.8. THE TRUNNION SHOWED SIGNIFIGANT WEAR AT DISSASSEMBLY AFTER THE PILOT NOTED A HIGH FREQUENCY VIBRATION. THE AGUSTA T/R ASSY IS SUBJECT TO BECOMING STIFF, WHEN THIS OCCURS THE T/R HUB SHOULD BE COMPLETELY DISSASSEMBLED AND INSPECTED FOR WEAR. I WOULD SUGGEST AGUSTA INSTITUTE A SCHEDULED INSPECTION PRIOR TO THE 2400 HR. INSPECTION THAT IS NOW IN PLACE. 1G72 3U H7EU 20020124000022002012400002GL 2002 1 24 KUVA076138 220011010G72306890483 BEARING RACE 6890550 AGUSTAA109 A109A2 0260120EU ALLSN 250C 250C20B 03013GL COMPRESSOR CHAFED H KUVAK NONE O OTHER ININSP/MAINT 1 FS01168BH CAC6026 7256 CAC6026 BEARING P/N 23034787 S/N MP78657 CHAFFED RACE P/N 6890483 S/N MP119218 CAUSING BOTH PARTS TO SCRAP. 1G72 3U3 U H7EU E4CE 20010419002222001041900222SW 2001 4 19 LS1R071905 120010404G79218538312 COOLER BELL 206 206B3 1181506SW TRANSMISSION CONTAMINATED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13206BY 2871 PART HAS TRANSMISSION CHIPS. 1G71 3U H2SW 20010419002232001041900223WP 2001 4 19 LS1R071906 120010404G33406014313 POWER SUPPLY HUGHES369 369D 4470706WP STROBE FAILED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13369AW 470117D PART WILL NOT FLASH. 1G71 3U H3WE 20010419002242001041900224WP 2001 4 19 LS1R071907 120010404G7810369A8230504 EXHAUST STACK HUGHES369 369D 4470706WP ENGINE CRACKED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA131097J 900801D PART IS CRACKED. 1G71 3U H3WE 20010419002252001041900225WP 2001 4 19 LS1R071908 120010404G3211369H6006 BRACE HUGHES369 369D 4470706WP MLG WORN E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13369AW 470117D PART IS WORN EXCESSIVELY. 1G71 3U H3WE 20010419002262001041900226WP 2001 4 19 LS1R071909 120010404G3211369H6006 BRACE HUGHES369 369D 4470706WP MLG WORN E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13369AW 470117D PART IS WORN EXCESSIVELY. 1G71 3U H3WE 20010419002272001041900227WP 2001 4 19 LS1R071910 120010404G3211369H6006 BRACE HUGHES369 369D 4470706WP MLG CRACKED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13369AW 470117D PART IS CRACKED. 1G71 3U H3WE 20010419002282001041900228WP 2001 4 19 LS1R071911 120010404G2821369A8116 FUEL FILTER HUGHES369 369D 4470706WP ENGINE BROKEN E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13369AW 470117D PART IS BROKEN. 1G71 3U H3WE 20010419002292001041900229GL 2001 4 19 LS1R071914 220010404G7210810151 MAGNETIC SEAL BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL ENGINE LEAKING E LS1RO OTHER K FLUID LOSS NRNOT REPORTED 1 EA13206BX 2872 PART IS LEAKING. 1G71 3U3 U H2SW E4CE 20010419002302001041900230GL 2001 4 19 LS1R071915 220010404G72106894171 GEARBOX HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL ENGINE LEAKING E LS1RO OTHER K FLUID LOSS NRNOT REPORTED 1 EA135211R 1161D PART IS LEAKING. 1G71 3U3 U H3WE E4CE 20010419002312001041900231SW 2001 4 19 LS1R071916 120010406G6510204040602005 SHAFT BELL 204 UH1H 1181407SW TAIL ROTOR WORN E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA1353AG 7221588 PART IS WORN EXCESSIVELY. 1G71 4U EXPA1G71 20010419002322001041900232SW 2001 4 19 LS1R071917 120010406G6510204040602005 SHAFT BELL 204 UH1H 1181407SW TAIL ROTOR WORN E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA1353AG 7221588 PART IS WORN EXCESSIVELY. 1G71 4U EXPA1G71 20010419002332001041900233SW 2001 4 19 LS1R071918 120010406G7930206011721009 BEARING BELL 206 206B3 1181506SW INDICATOR LOOSE E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA1390322 1736 PART IS LOOSE BEARINGS. 1G71 3U H2SW 20010419002342001041900234GL 2001 4 19 LS1R071919 220010406G7314369A81433 PUMP HUGHES369 369E 4470707WP ALLSN 250C 250C20B 03013GL FUEL SYSTEM NOISY E LS1RO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 EA13765KV 0082E PART IS NOISY. 1G71 3U3 U H3WE E4CE 20010419002352001041900235SW 2001 4 19 LS1R071920 120010406G6320206031509001 DRAG PIN BELL 206 206B3 1181506SW M/R GEARBOX WORN E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA1390322 1736 PART IS WORN EXCESSIVELY. 1G71 3U H2SW 20010419002362001041900236SW 2001 4 19 LS1R071921 120010406G5522206070178012 SKIN BELL 206 206B3 1181506SW ELEVATOR DAMAGED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA139907K 2040 PART HAS A HOLE. 1G71 3U H2SW 20010419001942001041900194WP 2001 4 19 LS1R072189 120010410G7714369A45167 TACHOMETER HUGHES369 369E 4470707WP COCKPIT INACCURATE E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA138330P105 0330E TACHOMETER IS INACCURATE. 1G71 3U H3WE 20030807001132003080700113SW 2003 8 7 LS1R072190 120010410G2700205001706009 CABLE DRUM BELL 204 UH1H 1181407SW FLT CONTROLS STRETCHED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA1351AG 7120178 CABLE DRUM STRETCHED. 1G71 4U EXPA1G71 20010507005522001050700552SW 2001 5 7 LS1R072589 120010416G6300206030539101 MOUNT BELL 206 206B3 1181506SW INPUT DRIVE WORN E LS1RK NONE O OTHER ININSP/MAINT 1 EA13903228439 1736 PART IS WORN EXCESSIVELY. 1G71 3U H2SW 20010507005532001050700553SW 2001 5 7 LS1R072590 120010416G331020407570545 CONTROL PANEL BELL 204 UH1H 1181407SW COCKPIT LIGHTS INOPERATIVE E LS1RK NONE L NO TEST ININSP/MAINT 1 EA1353AG 4790 7221588 LIGHTS WILL NOT COME ON. CONTROL PANEL INOPERATIVE. 1G71 4U EXPA1G71 20010507005542001050700554 2001 5 7 LS1R072591 420010416G345766000201 GPS BELL 206 OH58A 1181579SW COCKPIT INOPERATIVE E LS1RK NONE O OTHER ININSP/MAINT 1 EA1354AG 221 7120721 GPS WILL NOT RECIEVE. 1G71 3U H2SW 20010507005552001050700555SW 2001 5 7 LS1R072592 120010416G242407639CSV1152 REGULATOR BELL 204 UH1H 1181407SW ELECTRICAL OUT OF ADJ E LS1RK NONE L NO TEST ININSP/MAINT 1 EA1353AG 7221588 REGULATOR UNABLE TO HOLD ADJUSTMENT. 1G71 4U EXPA1G71 20010507005632001050700563SW 2001 5 7 LS1R072735 120010419G771432005023 TACH GENERATOR BELL 206 206B3 1181506SW ENGINE INOPERATIVE E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13206BX 2872 PART IS BROKEN. 1G71 3U H2SW 20010508002012001050800201SW 2001 5 8 LS1R072736 120010419G2740205001505001 BEARING BELL 212 212 1181420SW BELLCRANK LOOSE E LS1RK NONE O OTHER ININSP/MAINT 1 EA138530F 30920 BELLCRANK HAS LOOSE BEARINGS. 1G71 4U H4SW 20010507005642001050700564SW 2001 5 7 LS1R072737 120010419G7714212070108007 INDICATOR BELL 212 212 1181420SW TRIPLE TACH INTERMITTENT E LS1RK NONE O OTHER ININSP/MAINT 1 EA138530F1241 30920 PART IS INTERMITTENT. 1G71 4U H4SW 20010507005652001050700565WP 2001 5 7 LS1R072738 120010419G2740369A717011 MOTOR HUGHES369 369D 4470706WP LATERAL TRIM MALFUNCTIONED E LS1RK NONE O OTHER ININSP/MAINT 1 EA13500DC4014 290456D PART IS SLOW. 1G71 3U H3WE 20010507005662001050700566SW 2001 5 7 LS1R072739 120010425G7603206062721113 BEARING BELL 206 206B3 1181506SW ACTUATOR LOOSE E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13206BY318 2871 PART HAS LOOSE BEARINGS. 1G71 3U H2SW 20010507005672001050700567SW 2001 5 7 LS1R072740 120010426G28221C381 PUMP BELL 206 206B3 1181506SW FUEL BOOST INOPERATIVE E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA139907K563 2040 PART IS INOPERATIVE. 1G71 3U H2SW 20010507005682001050700568WP 2001 5 7 LS1R072741 120010427G7810369A8230503 EXHAUST PIPE HUGHES369 369D 4470706WP ENGINE CRACKED E LS1RK NONE O OTHER ININSP/MAINT 1 EA135211R529 1161D PART IS CRACKED. 1G71 3U H3WE 20010507005692001050700569WP 2001 5 7 LS1R072742 120010427G2740369A7010 LOCK HUGHES369 369E 4470707WP STAB DAMAGED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13765KV 0082E PART HAS FEED BACK. 1G71 3U H3WE 20010515004352001051500435 2001 5 15 LS1R072915 420010509G2300069102100 RADIO HUGHES369 369D 4470706WP COCKPIT WEAK E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA131097J 900801D RADIO IS WEAK. 1G71 3U H3WE 20010515004362001051500436WP 2001 5 15 LS1R072916 120010509G7714369H4551 TACH GENERATOR HUGHES369 369D 4470706WP ENGINE SHEARED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA131097J 900801D TACH GEN IS SHEARED. 1G71 3U H3WE 20010515004372001051500437 2001 5 15 LS1R072917 420010509G2300TFM1380 CONTROL UNIT HUGHES369 369D 4470706WP RADIO INOPERATIVE E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA135211R 1161D RADIO CONTROL INOP. 1G71 3U H3WE 20010515004382001051500438WP 2001 5 15 LS1R072918 120010509G3300369H64255 CONTROL UNIT HUGHES369 369D 4470706WP DIMMER SWITCH INOPERATIVE E LS1RK NONE O OTHER ININSP/MAINT 1 EA131097J1461 900801D DIMMER SWITCH CIRCUIT-SHORTED. 1G71 3U H3WE 20010515004392001051500439GL 2001 5 15 LS1R072919 220010509G741210614950 EXCITER HUGHES369 369E 4470707WP ALLSN 250C 250C20B 03013GL ENGINE UNSERVICEABLE E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13765KV952 0082E EXCITER IS UNSERVICEABLE. 1G71 3U3 U H3WE E4CE 20010515004402001051500440WP 2001 5 15 LS1R072920 120010509G7400369A45143 EPO ASSY HUGHES369 369E 4470707WP COCKPIT MALFUNCTIONED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13129GA 0052E HAS SOLID TONE. 1G71 3U H3WE 20010515004412001051500441 2001 5 15 LS1R072921 420010509G2350066105570 AUDIO PANEL HUGHES369 369E 4470707WP COCKPIT INTERMITTENT E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13129GA 0052E AUDIO PANEL IS INTERMITTENT. 1G71 3U H3WE 20010727001362001072700136WP 2001 7 27 LS1R073005 120010522G21106890550 COMPRESSOR HUGHES369 369E 4470707WP AIR CONDITIONER DAMAGED E LS1RK NONE O OTHER ININSP/MAINT 1 EA13129GA1647 0052E COMPRESSOR IS DAMAGED. 1G71 3U H3WE 20010727001372001072700137WP 2001 7 27 LS1R073117 120010524G6420369D27609501 SWASHPLATE HUGHES369 369D 4470706WP TAIL ROTOR LOOSE E LS1RK NONE O OTHER ININSP/MAINT 1 EA13500DC1006 290456D SWASHPLATE HAS EXCESIVE AXIAL PLAY. 1G71 3U H3WE 20010727001472001072700147WP 2001 7 27 LS1R073118 120010524G6520369D25400 GEARBOX HUGHES369 369D 4470706WP TAIL ROTOR MAKING METAL E LS1RK NONE O OTHER ININSP/MAINT 1 EA13369AW3154 470117D TAIL ROTOR GEARBOX IS MAKING METAL. 1G71 3U H3WE 20010727001482001072700148WP 2001 7 27 LS1R073263 120010604G7714369A45167 INDICATOR HUGHES369 369D 4470706WP TACHOMETER SHORTED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA135211R1479 1161D TACHOMETER IS SHORTED OUT. 1G71 3U H3WE 20010727001492001072700149WP 2001 7 27 LS1R073264 120010604G6700369A717011 MOTOR HUGHES369 369D 4470706WP LATERAL TRIM INTERMITTENT E LS1RK NONE O OTHER ININSP/MAINT 1 EA131097J1683 900801D LATERAL TRIM MOTER IS INTERMITTENT. 1G71 3U H3WE 20010727001502001072700150 2001 7 27 LS1R073265 420010604G2312KY195B RADIO HUGHES369 369D 4470706WP VHF DISTORTED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA135027P2220 611002D VHF RADIO IS DISTORTED. 1G71 3U H3WE 20010727001542001072700154WP 2001 7 27 LS1R073266 120010604G3300369H6425 SWITCH HUGHES369 369E 4470707WP DIMMER CONTROL INOPERATIVE E LS1RK NONE O OTHER ININSP/MAINT 1 EA138330P1215 0330E DIMMER CONTROL INOPERATIVE. 1G71 3U H3WE 20010727001562001072700156WP 2001 7 27 LS1R073267 120010604G2436369A4652 VOLT REGULATOR HUGHES369 369E 4470707WP ELECTRICAL INOPERATIVE E LS1RK NONE L NO TEST ININSP/MAINT 1 EA138330P1791 0330E VOLTAGE REGULATOR WILL NOT COME ON LINE. 1G71 3U H3WE 20010727001592001072700159SW 2001 7 27 LS1R073268 120010604G7714 SHAFT BELL 206 OH58A 1181579SW TACH GENERATOR SHEARED E LS1RK NONE L NO TEST ININSP/MAINT 1 EA1358AG 809 13702 7221131 TACH GENERATOR SHAFT IS SHEARED. 1G71 3U H2SW 20010924001152001092400115WP 2001 9 24 LS1R073476 120010618G2822164A81343 PUMP HUGHES369 369E 4470707WP FUEL SYSTEM INOPERATIVE E LS1RK NONE L NO TEST ININSP/MAINT 1 EA13765KV18 0082E PART IS WILL NOT RUN WHEN POWER A. 1G71 3U H3WE 20010924001162001092400116WP 2001 9 24 LS1R073477 120010618G6720369D21800501 SEAL HUGHES369 369D 4470706WP T/R PITCH CONTROROTATED E LS1RK NONE O OTHER ININSP/MAINT 1 EA135211R1151 1161D PART IS SEAL ROTATES. 1G71 3U H3WE 20010924001172001092400117WP 2001 9 24 LS1R073478 120010618G6300204031920003 DAMPER HUGHES369 369E 4470707WP MAIN ROTOR WORN E LS1RK NONE O OTHER ININSP/MAINT 1 EA138330P 0330E PART IS WORN EXCESSIVELY. 1G71 3U H3WE 20010924001182001092400118SW 2001 9 24 LS1R073479 120010619G67000710105200 VALVE BELL 212 212 1181420SW FLIGHT CONTROL BROKEN E LS1RK NONE O OTHER ININSP/MAINT 1 EA138530F 30920 PART IS BROKEN. 1G71 4U H4SW 20010924001192001092400119WP 2001 9 24 LS1R073480 120010619G2510369H6525503 SEAT HUGHES369 369D 4470706WP COCKPIT CRACKED E LS1RK NONE O OTHER ININSP/MAINT 1 EA135211R 1161D PART IS CRACKED. 1G71 3U H3WE 20010924001202001092400120WP 2001 9 24 LS1R073481 120010619G2810369H81013 FUEL CELL HUGHES369 369D 4470706WP FUSELAGE LEAKING E LS1RK NONE K FLUID LOSS ININSP/MAINT 1 EA13369AW 470117D PART IS LEAKING. 1G71 3U H3WE 20010924001212001092400121WP 2001 9 24 LS1R073482 120010619G7810369A8230503 EXHAUST PIPE HUGHES369 369D 4470706WP ENGINE CRACKED E LS1RK NONE O OTHER ININSP/MAINT 1 EA135211R 1161D PART IS CRACKED. 1G71 3U H3WE 20010924001222001092400122SW 2001 9 24 LS1R073483 120010619G6320206032309536 BEARING BELL 206 OH58A 1181579SW MAIN ROTOR DAMAGED E LS1RK NONE O OTHER ININSP/MAINT 1 EA1358AG 7221131 PART IS OUT OF RACE. 1G71 3U H2SW 20010924001232001092400123SW 2001 9 24 LS1R073484 120010619G2432201A GAUGE BELL 206 OH58A 1181579SW BATTERY MALFUNCTIONED E LS1RK NONE O OTHER ININSP/MAINT 1 EA1358AG 7221131 GAGE PEGS OUT. 1G71 3U H2SW 20010924001242001092400124WP 2001 9 24 LS1R073485 120010619G6300369D21400503 DAMPER HUGHES369 369D 4470706WP MAIN ROTOR STRETCHED E LS1RK NONE O OTHER ININSP/MAINT 1 EA13500DC 290456D PART IS STRETCHED. 1G71 3U H3WE 20010924001262001092400126WP 2001 9 24 LS1R073486 120010619G6230369D27609501 SWASHPLATE HUGHES369 369D 4470706WP MAIN ROTOR LOOSE E LS1RK NONE O OTHER ININSP/MAINT 1 EA13500DC 290456D PART HAS EXCESIVE AXIAL PLAY. 1G71 3U H3WE 20010924001272001092400127WP 2001 9 24 LS1R073487 120010619G6720369D21800501 BEARING HUGHES369 369E 4470707WP T/R ROTOR LOOSE E LS1RK NONE O OTHER ININSP/MAINT 1 EA13129GA 0052E BEARINGS FALL OUT. 1G71 3U H3WE 20010924001282001092400128 2001 9 24 LS1R073488 420010619G2300TFM138B RADIO HUGHES369 369D 4470706WP COCKPIT STUCK E LS1RK NONE O OTHER ININSP/MAINT 1 EA135027P 611002D PART IS STICKING. 1G71 3U H3WE 20010924001302001092400130SW 2001 9 24 LS1R074916 120010720G2432AG380E4440 BATTERY BELL 204 UH1H 1181407SW MAIN BATTERY WEAK E LS1RK NONE L NO TEST ININSP/MAINT 1 EA1351AG 7120178 PART IS WEAK. 1G71 4U EXPA1G71 20010924001312001092400131SW 2001 9 24 LS1R074917 120010720G2432G641E BATTERY BELL 206 206B3 1181506SW MAIN BATTERY DISCHARGED E LS1RK NONE O OTHER ININSP/MAINT 1 EA139907K 2040 PART IS BAD CELLS. 1G71 3U H2SW 20010924001322001092400132WP 2001 9 24 LS1R074918 120010720G6510369D2172121 BEARING HUGHES369 369E 4470707WP T/R LINK LOOSE E LS1RK NONE O OTHER ININSP/MAINT 1 EA13765KV 0082E BEARINGS FALL OUT. 1G71 3U H3WE 20010924001342001092400134WP 2001 9 24 LS1R074919 120010720G6400369D2172313 LINK HUGHES369 369D 4470706WP TAIL ROTOR WORN E LS1RK NONE O OTHER ININSP/MAINT 1 EA135027P 611002D PART IS WORN EXCESSIVELY. 1G71 3U H3WE 20010924001362001092400136WP 2001 9 24 LS1R074920 120010720G6400369D2172313 LINK HUGHES369 369D 4470706WP TAIL ROTOR WORN E LS1RK NONE O OTHER ININSP/MAINT 1 EA135027P 611002D PART IS WORN EXCESSIVELY. 1G71 3U H3WE 20010924001382001092400138WP 2001 9 24 LS1R074921 120010720G7332369H81443 PRESSURE SWITCH HUGHES369 369E 4470707WP FUEL SYSTEM MALFUNCTIONED E LS1RK NONE O OTHER ININSP/MAINT 1 EA138330P 0330E COMES IN TO LOW. 1G71 3U H3WE 20010924001402001092400140WP 2001 9 24 LS1R074922 120010720G77148DJ150FEA INDICATOR HUGHES369 369D 4470706WP COCKPIT UNSERVICEABLE E LS1RK NONE O OTHER ININSP/MAINT 1 EA135211R 1161D PART IS UNREADABLE AND UNSERVICEABLE. 1G71 3U H3WE 20010924001412001092400141WP 2001 9 24 LS1R074923 120010720G7810369A8230503 EXHAUST PIPE HUGHES369 369E 4470707WP ENGINE CRACKED E LS1RK NONE O OTHER ININSP/MAINT 1 EA13765KV457 0082E PART IS CRACKED. 1G71 3U H3WE 20010924001422001092400142WP 2001 9 24 LS1R074924 120010720G7810369A8230503 EXHAUST PIPE HUGHES369 369D 4470706WP ENGINE CRACKED E LS1RK NONE O OTHER ININSP/MAINT 1 EA135211R 1161D PART IS CRACKED. 1G71 3U H3WE 20010924001432001092400143WP 2001 9 24 LS1R074925 120010720G2432G641E BATTERY HUGHES369 369E 4470707WP MAIN BATTERY OVERHEATED E LS1RK NONE O OTHER ININSP/MAINT 1 EA138330P 0330E PART OVERHEATED. 1G71 3U H3WE 20010924001442001092400144SW 2001 9 24 LS1R074926 120010720G5320206031302269 SUPPORT BELL 206 206B3 1181506SW FUSELAGE CRACKED E LS1RK NONE O OTHER ININSP/MAINT 1 EA1349718 1917 PART IS CRACKED. 1G71 3U H2SW 20010924001452001092400145SW 2001 9 24 LS1R074927 120010720G5320206031301129 SUPPORT BELL 206 206B3 1181506SW FUSELAGE CRACKED E LS1RK NONE O OTHER ININSP/MAINT 1 EA1349718 1917 PART IS CRACKED. 1G71 3U H2SW 20010924001472001092400147SW 2001 9 24 LS1R074928 120010720G2730205001905001 BELLCRANK BELL 212 212 1181420SW ELEVATOR WORN E LS1RK NONE O OTHER ININSP/MAINT 1 EA138530B 30702 PART IS WORN EXCESSIVELY. 1G71 4U H4SW 20010924001482001092400148WP 2001 9 24 LS1R074929 120010720G7810369A8230504 EXHAUST STACK HUGHES369 369D 4470706WP ENGINE CRACKED E LS1RK NONE O OTHER ININSP/MAINT 1 EA13500DC 290456D PART IS CRACKED. 1G71 3U H3WE 20010924001502001092400150GL 2001 9 24 LS1R074930 220010720G7320369A717011 MOTOR HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL LATERAL TRIM NOISY E LS1RK NONE O OTHER ININSP/MAINT 1 EA135211R 1161D PART IS NOISY. 1G71 3U3 U H3WE E4CE 20010924001512001092400151SW 2001 9 24 LS1R074931 120010720G281020601675001 FUEL CELL BELL 206 206B3 1181506SW FUSELAGE LEAKING E LS1RK NONE O OTHER ININSP/MAINT 1 EA1349718 1917 PART IS LEAKING. 1G71 3U H2SW 20010924001532001092400153SW 2001 9 24 LS1R074932 120010720G2910205076099007 CYLINDER BELL 204 UH1H 1181407SW HYD SYSTEM WORN E LS1RK NONE O OTHER ININSP/MAINT 1 EA1353AG 7221588 PART IS WORN EXCESSIVELY. 1G71 4U EXPA1G71 20010924001552001092400155SW 2001 9 24 LS1R074934 120010803G53202060313291 FITTING BELL 206 206B3 1181506SW FUSELAGE CRACKED E LS1RK NONE O OTHER ININSP/MAINT 1 EA13206BX 2872 PART IS CRACKED. 1G71 3U H2SW 20010924001572001092400157SW 2001 9 24 LS1R074935 120010813G6321204001376003 BRAKE BELL 206 OH58A 1181579SW MAIN ROTOR STUCK E LS1RK NONE O OTHER ININSP/MAINT 1 EA1358AG 1360 7221131 PART MOVEMENT RESTRICTED. 1G71 3U H2SW 20010924001592001092400159WP 2001 9 24 LS1R074936 120010813G8000IC34 BRUSHES HUGHES369 369E 4470707WP STARTER FAILED E LS1RK NONE O OTHER ININSP/MAINT 1 EA138330P 0330E PART IS BAD BRUSHES. 1G71 3U H3WE 20010924001602001092400160WP 2001 9 24 LS1R074937 120010813G2810164A134 FUEL CELL HUGHES369 369D 4470706WP FUSELAGE INOPERATIVE E LS1RK NONE O OTHER ININSP/MAINT 1 EA131097J 900801D NO POWER. 1G71 3U H3WE 20010924001622001092400162WP 2001 9 24 LS1R074938 120010813G2821369H8102 HOSE HUGHES369 369E 4470707WP FUEL SYSTEM DIRTY E LS1RK NONE O OTHER ININSP/MAINT 1 EA138330P 0330E DIRT IN FUEL FILTER. 1G71 3U H3WE 20010924001632001092400163WP 2001 9 24 LS1R074939 120010813G2822IC34 PUMP HUGHES369 369E 4470707WP FUEL SYSTEM INOPERATIVE E LS1RK NONE O OTHER ININSP/MAINT 1 EA138330P 0330E PART WILL NOT OPERATE. 1G71 3U H3WE 20010924001682001092400168WP 2001 9 24 LS1R074940 120010813G7400369A45143 EPO ASSY HUGHES369 369E 4470707WP ENGINE MALFUNCTIONED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA138330P 0330E PART WON'T TURN OFF. 1G71 3U H3WE 20010924001692001092400169SW 2001 9 24 LS1R074941 120010813G2432G641 BATTERY BELL 206 206B3 1181506SW MAIN BATTERY BURNED E LS1RK NONE O OTHER ININSP/MAINT 1 EA139907K 2040 PART IS BURNED. 1G71 3U H2SW 20010924001712001092400171SW 2001 9 24 LS1R074942 120010817G79218537651 OIL COOLER BELL 212 212 1181420SW ENGINE MAKING METAL E LS1RK NONE O OTHER ININSP/MAINT 1 EA138530F 30920 PART MAKING METAL. 1G71 4U H4SW 20010924001722001092400172 2001 9 24 LS1R074943 420010817G2300FM138 RADIO HUGHES369 369E 4470707WP COCKPIT FAILED E LS1RK NONE O OTHER ININSP/MAINT 1 EA138330P 0330E PART WILL NOT TRANSMITT. 1G71 3U H3WE 20010924001732001092400173WP 2001 9 24 LS1R075709 120010905G7400369A45133 EPO ASSY HUGHES369 369E 4470707WP ENGINE MALFUNCTIONED E LS1RK NONE O OTHER ININSP/MAINT 1 EA138330P 0330E PART WARNING SIGNAL ACTIVATES. 1G71 3U H3WE 20010924001742001092400174WP 2001 9 24 LS1R075710 120010905G7400369A45143 EPO ASSY HUGHES369 369D 4470706WP MALFUNCTIONED E LS1RK NONE O OTHER ININSP/MAINT 1 EA135027P14 611002D PART WARNING SIGNAL ACTIVATES. 1G71 3U H3WE 20010924001752001092400175WP 2001 9 24 LS1R075711 120010905G7400369A45143 EPO ASSY HUGHES369 369E 4470707WP ENGINE MALFUNCTIONED E LS1RK NONE O OTHER ININSP/MAINT 1 EA138330P51 0330E PART WARNING SIGNAL ACTIVATES. 1G71 3U H3WE 20011004001432001100400143WP 2001 10 4 LS1R075923 120010928G7400369A45143 EPO ASSY 369D HUGHES369 369D 4470706WP COCKPIT OUT OF ADJ E LS1RK NONE O OTHER ININSP/MAINT 1 EA13369AW673 470117D 470117D PART IS OUT OF CALIBRATION. 1G71 3U H3WE 20011004001442001100400144SW 2001 10 4 LS1R075924 120010928G7720SEL019BC INDICATOR BELL 206 206B3 1181506SW COCKPIT INACCURATE E LS1RK NONE O OTHER ININSP/MAINT 1 EA139907K1000 2040 PART IS INACCURATE. 1G71 3U H2SW 20011004001452001100400145WP 2001 10 4 LS1R075925 120010928G7400369A45143 EPO ASSY HUGHES369 369D 4470706WP COCKPIT MALFUNCTIONED E LS1RO OTHER N FALSE WARNING NRNOT REPORTED 1 EA13369AW 470117D PART IS ACTUATES WARNING HORN. 1G71 3U H3WE 20020124000032002012400003GL 2002 1 24 LS1R076721 220011022G732123065104 FUEL CONTROL HUGHES369 369D 4470706WP ALLSN 250C 250C20 03013GL ENGINE MALFUNCTIONED E LS1RK NONE O OTHER ININSP/MAINT 1 EA135027P 611002D MAKES ENGINE RUMBLE AT IDLE; ENGINE N1 DECREASES 1/2 TO 1 PERCENT WITH START PUMP ON AND RETURNS TO NORMAL WHEN OFF. 1G71 3U3 U H3WE E4CE 20020124000042002012400004WP 2002 1 24 LS1R076722 120011022G3150369H64255 CONTROL UNIT 369D HUGHES369 369D 4470706WP INSTRUMENT PANELFAILED E LS1RK NONE L NO TEST ININSP/MAINT 1 EA13369AW 470117D 470117D INSTRUMENT PANEL LIGHT DIMMER CONTROL FAILED. 1G71 3U H3WE 20020124000052002012400005 2002 1 24 LS1R076723 420011022G3420206070274005 INDICATOR BELL 206 206B3 1181506SW COCKPIT INOPERATIVE E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13206BY 2871 ATTITUDE INDICATOR NEEDLE WILL NOT MOVE. 1G71 3U H2SW 20020124000062002012400006WP 2002 1 24 LS1R076724 120011022G28221C34 PUMP HUGHES369 369D 4470706WP FUEL BOOST FAILED E LS1RK NONE O OTHER ININSP/MAINT 1 EA13369AW 470117D BOOST PUMP WILL NOT TURN ON. 1G71 3U H3WE 20020124000072002012400007 2002 1 24 LS1R076725 420011022G3424206070274005 INDICATOR BELL 206 206B3 1181506SW COCKPIT INOPERATIVE E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA139907K 2040 TURN AND BANK INDICATOR NEEDLE WILL NOT MOVE. 1G71 3U H2SW 20020124000082002012400008SW 2002 1 24 LS1R076726 120011022G2822206062681101 PUMP BELL 206 206B3 1181506SW FUEL BOOST MALFUNCTIONED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13206BY 2871 BOOST PUMP PRODUCING LOW PRESSURE AND LOUD NOISE. 1G71 3U H2SW 20020124000092002012400009WP 2002 1 24 LS1R076727 120011022G7400369A45143 EPO ASSY HUGHES369 369D 4470706WP COCKPIT MALFUNCTIONED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA135027P 611002D LOW ROTOR RPM ACTUATES WHEN EPO IS ACTIVATED. 1G71 3U H3WE 20020124000102002012400010WP 2002 1 24 LS1R076728 120011022G6400369D27514 BELLCRANK HUGHES369 369D 4470706WP TAIL ROTOR WORN E LS1RK NONE O OTHER ININSP/MAINT 1 EA135027P 611002D TAIL ROTOR BELLCRANK EARS WORN AND SPRUNG. 1G71 3U H3WE 20020124000112002012400011WP 2002 1 24 LS1R076729 120011022G6720369D21800501 PITCH CONTROL HUGHES369 369D 4470706WP TAIL ROTOR WORN E LS1RK NONE O OTHER ININSP/MAINT 1 EA135027P 611002D TAIL ROTOR PITCH CONTROL IS WORN EXCESSIVELY. 1G71 3U H3WE 20020124000122002012400012SW 2002 1 24 LS1R076730 120011022G76031606470001 THROTTLE CABLE BELL 206 206B3 1181506SW ENGINE BROKEN E LS1RK NONE O OTHER ININSP/MAINT 1 EA1390322 1736 THROTTLE CABLE IS BROKEN. 1G71 3U H2SW 20020124000132002012400013GL 2002 1 24 LS1R076731 220011022G72611740996 FILTER BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL ENGINE OIL LEAKING E LS1RK NONE K FLUID LOSS ININSP/MAINT 1 EA13206BX 2872 ENGINE OIL FILTER IS LEAKING. 1G71 3U3 U H2SW E4CE 20020124000142002012400014WP 2002 1 24 LS1R076732 120011022G2820369D281081 VENT LINE HUGHES369 369D 4470706WP ENGINE FUEL BENT E LS1RK NONE O OTHER ININSP/MAINT 1 EA135027P 611002D FUEL VENT LINE IS BENT. 1G71 3U H3WE 20020124000152002012400015 2002 1 24 LS1R076733 420011022G3422103002201 GYRO BELL 206 206B3 1181506SW COCKPIT INOPERATIVE E LS1RK NONE O OTHER ININSP/MAINT 1 EA139907K 2040 DIRECTIONAL GYRO IS INOPERATIVE. 1G71 3U H2SW 20020124000162002012400016 2002 1 24 LS1R076734 420011022G3421500DC GYRO BELL 206 206B3 1181506SW COCKPIT INOPERATIVE E LS1RK NONE O OTHER ININSP/MAINT 1 EA139907K 2040 ATTITUDE GYRO CONTROL INOPERATIVE. 1G71 3U H2SW 20020124000172002012400017WP 2002 1 24 LS1R076929 120011031G7400369A45143 EPO ASSY HUGHES369 369D 4470706WP COCKPIT MALFUNCTIONED E LS1RK NONE O OTHER ININSP/MAINT 1 EA13369AW 470117D EPO UNIT FEEDS BACK. 1G71 3U H3WE 20020124000182002012400018WP 2002 1 24 LS1R076930 120011031G7400369A45143 EPO ASSY HUGHES369 369D 4470706WP COCKPIT MALFUNCTIONED E LS1RK NONE O OTHER ININSP/MAINT 1 EA13369AW 470117D EPO ASSY FEEDS BACK. 1G71 3U H3WE 20020124000192002012400019SW 2002 1 24 LS1R076931 120011031G7931209070262009 INDICATOR BELL 212 212 1181420SW ENGINE OIL INTERMITTENT E LS1RK NONE O OTHER ININSP/MAINT 1 EA138530B 30702 INTERMITTENT. 1G71 4U H4SW 20020124000202002012400020WP 2002 1 24 LS1R076932 120011031G2430A700ZG RCCB HUGHES369 369D 4470706WP ELECTRICAL FAILED E LS1RO OTHER O OTHER NRNOT REPORTED 1 EA13369AW 470117D RCCB HAS NO OUTPUT. 1G71 3U H3WE 20020124000212002012400021WP 2002 1 24 LS1R076933 120011031G2424369A4652 VOLT REGULATOR HUGHES369 369D 4470706WP ELELCTRICAL OUT OF ADJ E LS1RK NONE O OTHER ININSP/MAINT 1 EA13369AW 470117D PART IS OUT OF CALIBRATION. 1G71 3U H3WE 20020124000222002012400022 2002 1 24 LS1R076934 420011031G34205040017901 INDICATOR BELL 212 212 1181420SW COCKPIT INOPERATIVE E LS1RK NONE L NO TEST ININSP/MAINT 1 EA138530B 30702 ARTIFICIAL HORIZON WILL NOT COME ON LINE. 1G71 4U H4SW 20020124000232002012400023 2002 1 24 LS1R076935 420011031G34205040017901 INDICATOR BELL 212 212 1181420SW COCKPIT INOPERATIVE E LS1RK NONE L NO TEST ININSP/MAINT 1 EA138530F 30920 ARTIFICIAL HORIZON WILL NOT COME ON LINE. 1G71 4U H4SW 20010326003962001032600396EU 2001 3 26 MALA010220 120010220G5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424XJ 424 FOUND DURING C-CHECK, CORROSION ON LT FLOOR SUPPORT FLANGE ON SEAT TRACK AT BL-0 STA 294 THRU STA 413. REFER TO CELSIUS W/O 19347, TASK 1526. MAINTENANCE REMOVED CORROSION AND CHECK LIMIT. REMOVED CORROSION IAW 51-70-40 MATERIAL REMOVED IS OUT OF LIMITS IAW SRM 53-70-60. REMOVED FWD CLIP IAW SRM 51-40-21, FABRICATED NEW ANGLE IAW SRM 51-20-20/30, ALODINED, PRIMED AND PAINTED IAW SRM 51-20-42/43. INSTALLED IAW SRM 51-40-21/23. REMAINING AREA WITHIN ALLOWABLE LIMIT REF SRM 53-70-60. 2L72 4T RTA52EU 20010417000832001041700083SO 2001 4 17 MQGR20013601 120010412G57401159W307012 ATTACH FITTING GULSTMG1159 G1159B 3953535SO WINGLET CORRODED B K NONE O OTHER ININSP/MAINT 1 SW9974A 5720 036 DURING RECOMMENDED INSPECTION OF WINGLET ATTACH HARDWARE FOR CORROSION, FOUND CORROSION IN THE WINGLET TO WING ATTACHMENT FITTING. IT APPEARS THIS CORROSION IS THE RESULT OF IMPROPER SEALING OF THE ATTACHMENT HARDWARE SINCE WATER WAS FOUND TRAPPED IN THE ONLY AREA OF CORRSION. THIS CORROSION WAS VERY DEEP AND WAS IN THE VOID BETWEEN THE UPPER AND LOWER BUSHINGS. 2L72 4F RTA12EA 20030918000712003091800071WP 2003 9 18 N32B2001004 120010910G5713 STRINGER DOUG DC6 DC6A 3021706WP PWA R2800 R2800* 52026NE STA17, LT WING CRACKED G O OTHER O OTHER NRNOT REPORTED 1 AL017780B21494 45372 STRINGER 17 CRACKED AT WING, STA 140. REPAIRED 17 AT WING STA L40 IAW NAC 2001-05. 2L74 4R4 R 6A3 5E8 20010924001782001092400178CE 2001 9 24 N988ME 120010918G2752505211516 PISTON BEECH BEECH B300 B300 1159232CE RT FLAP ACTUATORCRACKED C K NONE K FLUID LOSS ININSP/MAINT 1 SW99988ME4611 935A91 RIGHT OUTBOARD FLAP ACTUATOR CRACKED AT BASE OF PISTON WHERE THE END PLUG IS ATTACHED. THE CRACK WAS 1.5 INCHES LONG AND RESULTED IN THE LOSS OF THE LUBRICATING OIL FROM OUT OF THE PISTON AND SCREW ASSEMBLY. THE LOSS OF OIL WAS THE FIRST INDICATION OF A PROBLEM, AND IT WAS WHILE INVESTIGATING THE OIL LEAK THAT THE CRACK WAS DISCOVERED.THIS CRACK COULD RESULT IN A SIGNIFICANT LOSS OF STRUCTURAL STRENGTH OF THE ACTUATOR WHICH COULD RESULT IN THE STRUCTURAL FAILURE OF THE ACTUATOR ASSEMBLY. 2L72 4T RTA24CE 20010524000072001052400007NE 2001 5 24 NE032001B2128 220010330G7260 BEARING HAMSTD SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE GEARCASE CRACKED D MHMFK NONE O OTHER ININSP/MAINT 1 NE03 20743 UDAG0844 GEE785555 UPON DISASSEMBLY OF GEARCASE FOUND THE RIGHT AFT BEARING AND FORWARD ROLLER BEARING CRACKED. ALSO THE LEFT IDLER BEARING WAS FOUND WITH BRINNELLING/SPALLING ON RACEWAYS. 2L72 4T4 TRTA52EU E8NE 20010924001792001092400179CE 2001 9 24 NMO192 120010912G3230S217830144 HOSE CESSNA210 T210L 2073449CE NOSE GEAR FAILED G K NONE K FLUID LOSS LDLANDING 1 NM016721M3000 34 21061137 DURING LANDING, NOSE GEAR EXTENDED AND LOCKED, BUT MAIN GEAR DID NOT LOCK INTO PLACE. PILOT TRIED TO LOCK MAIN GEAR USING HAND HYDRAULIC PUMP WITH NO SUCCESS. AIRCRAFT LANDED WITH LOCKED NOSE GEAR AND COLLAPSED MAIN GEAR. SUFFERED DAMAGE TO REAR OF FUSELAGE, LEFT ELEVATOR, AND LEFT HORIZONTAL STABILIZER. INVESTIGATION FOUND FAILED NOSE GEAR HYDRAULIC FLEX LINE. THE FAILURE OF THIS LINE ALLOWED EXHAUSTION OF LANDING GEAR HYDRAULIC FLUID AFTER THE NOSE GEAR EXTENDED AND LOCKED, PREVENTING THE MAIN GEAR FROM LOCKING INTO PLACE.CONDITIONAL PART FAILURE. NO HISTORY NOTED IN AIRCRAFT MAINTENANCE RECORDS ASSOCIATED WITH NOSE GEAR HYDRAULIC HOSE REPLACEMENT SINCE 1976. 1H71 3O 3A21 20010409005202001040900520GL 2001 4 9 NWOR140K 320010301G6111V8433NS4 BLADE HARTZLHCA3V HCA3VK2 GL PROPELLER CRACKED B K NONE O OTHER ININSP/MAINT 1 SW05 490 BJ567 INSPECTION FOUND CRACKS AT TRAILING EDGE SIDE OF RETENTION AREA. 5 CP6EA 20010409005212001040900521GL 2001 4 9 NWOR140K1 320010301G6111V8433NS4 BLADE HARTZLHCA3V HCA3VK2 GL PROPELLER CRACKED B K NONE O OTHER ININSP/MAINT 1 SW05 490 BJ567 INSPECTION FOUND CRACK ALONG LEADING EDGE SIDE OF RETENTION AREA. 5 CP6EA 20010409004932001040900493GL 2001 4 9 NWOR140K2 320010301G6111V8433NS4 BLADE HARTZLHCA3V HCA3VK2 GL PROPELLER CRACKED B NWORK NONE O OTHER ININSP/MAINT 1 SW05 490 560 DURING INSPECTION, CRACK FOUND ALONG TRAILING EDGE OF RETENTION AREA OF BLADE. 5 CP6EA 20010409005402001040900540GL 2001 4 9 NWOR140K3 320010301G6111V8433NS4 BLADE HARTZLHCA3V HCA3VK2 GL PROPELLER CRACKED B K NONE O OTHER ININSP/MAINT 1 SW05 490 560 DURING INSPECTION CRACK WAS FOUND ALONG TRAILING EDGE OF RETENTION AREA. 5 CP6EA 20010409005512001040900551GL 2001 4 9 NWOR140K4 320010301G6111V8433NS4 BLADE HARTZLHCA3V HCA3VK2 GL PROPELLER CRACKED B K NONE O OTHER ININSP/MAINT 1 SW05 490 560 ON INSPECTION 4.5 INCH CRACK WAS FOUND ON TRAILING EDGE SIDE OF BLADE RETENTION AREA. 5 CP6EA 20010409005522001040900552GL 2001 4 9 NWOR140K5 320010301G6111V8433NS4 BLADE HARTZLHCA3V HCA3VK2 GL PROPELLER CRACKED B K NONE O OTHER ININSP/MAINT 1 SW05 490 FOUND 3.5 INCH CRACK ALONG TRAILING EDGE SIDE OF RETENTION AREA OF BLADE. 5 CP6EA 20010409001632001040900163EA 2001 4 9 NX4200315 220010207G855078531 PUMP LYC IO360 IO360L2A EA ENGINE OIL DEFECTIVE B NX42K NONE O OTHER ININSP/MAINT 1 SO15 2177 L2780951A WHEN REASSEMBLING THE OIL PUMP, IT WAS NOTED THAT DESPITE ATTEMPTS TO CENTER THE OIL PUMP BODY, THE IMPELLERS WOUL BIND WITH TORQUE APPLIED TO THE HOUSING. ALL DIMENTIONAL INSPECTIONS WERE WITHIN LIMITS. THE PROBLEM DISAPPEARED AFTER REPLACING THE COMBINATION OF THE OIL PUMP HOUSING AND DRIVEN IMPELLER. IT IS ASSUMED THAT THERE WAS A MACHING ALIGNMENT ERROR IN THE HOUSING, DRIVEN IMPELLER SHAFT, OR POSSIBLY A COMBINATION OF BOTH. 3 O 1E10 20010409001592001040900159EA 2001 4 9 NX4200420 220010207G8520LW16711 BEARING LYC IO360 IO360L2A EA ENGINE DEFECTIVE B NX42K NONE O OTHER ININSP/MAINT 1 SO15 2179 L2780651A DURING ENGINE DISASSEMBLY FOR ROUTINE OVERHAUL IT WAS NOTED THAT SOME NR 3 MAIN BEARING SURFACE MATERIAL HAD RELEASED FROM THE BEARING SHELL. 3 O 1E10 20010409001602001040900160EA 2001 4 9 NX4200440 220010207G8520LW13884 MAIN BEARING LYC IO360 IO360L2A EA ENGINE DEFECTIVE B K NONE O OTHER ININSP/MAINT 1 SO15 2169 L2784651A DURING ENGINE DISASSEMBLY FOR ROUTINE OVERHAUL IT WAS NOTED THAT SOME NR 2 MAIN BEARING SURFACE MATERIAL HAD RELEASED FROM THE BEARING SHELL. 3 O 1E10 20011213000202001121300020 2001 12 13 O3HR111501 420011115G2564 INLET LIFE RAFT OBSTRUCTED B O3HRK NONE O OTHER ININSP/MAINT 1 SW03 DURING SCHEDULED MAINTENANCE INSPECTION ON RAFT (PN 64449101, SN 0150), IT WAS NOTED THAT ONE COMPARTMENT INFLATED AT A FASTER RATE THAN THE OTHER, SUBSEQUENT INSPECTION REVEALED A FOREIGN OBJECT BLOCKING THE INLET PORT. THE DEBRIS APPEARS TO BE INTERNAL HOSE MATERIAL, WHICH ACCUMULATED DURING THE MANUFACTURING PROCESS. RECOMMENDATION: INSPECT HOSE ASSEMBLIES INTERNALLY PRIOR TO BUILD UP OF MANIFOLD. MANIFOLD ASSY PN BREAKDOWN: HOSE 64457-101 (1 EA) , HOSE 64457-103 (2 EA)) 20020118000552002011800055WP 2002 1 18 OMNIDMR01 120011220G5302369D23601501 STRUCTURE HUGHES369 369D 4470706WP HORIZONTAL STAB CRACKED C K NONE O OTHER ININSP/MAINT 1 SW9986ST 711012D HORIZONTAL STABILIZER CRACKED ON TRAILING EDGE AND TRIM TAB CRACKED ON LEADING EDGE DUE TO EXCESS FLUTTER. CRACKING CONCENTRATED AROUND AREA OF DAMPER WEIGHTS. TABS WERE TOO LONG AND ARE SUPPORTED ONLY BY RIVETS LOCATED ON LEADING EDGE,THE DAMPER WEIGHTS ADDED TO COMPENSATE. THE WEIGHTS NOT FLUSH TO TAB CREATES EXCESSIVE DRAG AND FURTHER CONTRIBUTES TO EXCESSIVE VIBRATION. THE EXCESSIVE FLUTTER COMMON IN 369 SERIES. 1G71 3U H3WE 20020118000562002011800056WP 2002 1 18 OMNIDMR02 120010917G5302421087505 STRUCTURE HUGHES369 369E 4470707WP HORIZONTAL STAB CRACKED C K NONE O OTHER ININSP/MAINT 1 SW997065C HORIZONTAL STABILIZER CRACKED ON TRAILING AND TRIM TAB CRACKED ON LEADING EDGE DUE TO EXCESSIVE FLUTTER. CRACKING IS CONCENTRATED AROUND AREA FO DAMPER WEIGHTS. TABS WERE TOO LONG AND ONLY SUPPORTED BY RIVETS LOCATED ON LEADING EDGE, THE DAMPER WEIGHTS ADDED TO COMPENSATE. THE WEIGHTS ARE NOT FLUSH TO TAB AND CREATES EXCESSIVE DRAG AND FURTHER CONTRIBUTES TO EXCESSIVE VIBRATION. THE EXCESSIVE FLUTTER IS COMMIN 369 SERIES. PROBLEM HAS BEEN IDENTIFIEDIN SERVICE NOTICE EN-44 (REWORK OF HORIZONTAL STABILIZER ASSEMBLY) 1G71 3U H3WE 20020118000572002011800057WP 2002 1 18 OMNIDMR03 120010807G5302421087905 STRUCTURE HUGHES369 369E 4470707WP HORIZONTAL STAB CRACKED C K NONE O OTHER ININSP/MAINT 1 SW99440TJ 0099990812 HORIZONTAL STABILIZER IS CRACKED ON TRAILING EDGE AND TRIM TAB IS CRACKED ON LEADING EDGE DUE TO EXCESSIVE FLUTTER.CRACKING IS CONCENTRATED AROUND AREA OF DAMPER WEIGHTS. TABS WERE TOO LONG AND ONLY SUPPORTED BY RIVETS LOCATED ON LEADING EDGE, CAUSING EXCESSIVE FLUTTER DURING FLIGHT; THE DAMPER WEIGHTS WERE ADDED TO CONPENSATE. THESE WEIGHTS ARE NOT FLUSH TO TAB, CREATING EXCESSIVE DRAG ON TABS AND FURTHER CONTRIBUTES TO EXCESSIVE VIBRATION. THIS EXCESSIVE FLUTTER IS COMMON IS THE 369 SERIES. PROBLEM HAS BEEN IDENTIFIED IN SERVICE NOTICE EN-44 1G71 3U H3WE 20020118000582002011800058EU 2002 1 18 OMNIDMR04 120011214G5302421087503 STRUCTURE HUGHES369 369FF 4470709EU HORIZONTAL STAB CRACKED C K NONE O OTHER ININSP/MAINT 1 SW9930042 0099990855 HORIZONTAL STABILIZER CRACKED ON TRAILING EDGE ABD TRAIM TAB CRACKED ON LEADING EDGE DUE TO EXCESSIVE FLUTTER. CRACKING IS CONCENTRATED AROUND AREA OF DAMPER WEIGHTS. TABS WERE TOO LONG AND ONLY SUPORTED BY RIVET ON THE LEADING EDGE, CAUSING EXCESSIVE FLUTTER DURING FLIGHT; THE DAMPER WEIGHTS ARE NOT FLUSH TO THE TAB CREATING EXCESSIVE DRAG ON THE TABS AND FURTHER CONTRIBUTES TO THE EXCESSIVE VIBRATION. THIS EXCESSIVE FLUTTER IS COMMON IN THE 369 SERIES, AND HAS BEEN IDENTIFIED IN SERVICE NOTICE FN-29.1 1G71 3U H3WE 20010502000512001050200051SO 2001 5 2 PNSA010201 120010227G3297 WIRE PIPER PA31 PA31350 7103110SO MLG INDICATOR DAMAGED E PNSAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 AL0328KE 318152049 AFTER SELECTING GEAR DOWN, LT DOWN LIGHT DID NOT ILLUMINATE. RETURNED TO BASE. REPAIRED WIRE ON LH DOWN LIGHT SWITCH. OPS CHECKED OK. 1L72 3O A20SO 20010502000522001050200052SO 2001 5 2 PNSA010203 120010228G6120 CONTROL CABLE PIPER PA31 PA31350 7103110SO PROP CONTROL FAILED E PNSAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AL033588Z 318052130 DURING TAKE-OFF ROLL RT ENGINE DID NOT DEVELOPE FULL RPM. ABORTED TAKE-OFF RETURNED FOR MAINTENANCE. REPLACED PROP CONTROL CABLE DUE TO INTERNAL FAILURE. 1L72 3O A20SO 20010410000132001041000013SO 2001 4 10 PNSA010205 120010201G3297 WIRE PIPER PA31 PA31350 7103110SO MLG BROKEN E PNSAA UNSCHED LANDING O OTHER CLCLIMB 1 AL033588Z 318052130 DURING CLIMB PILOT COULD NOT PLACE THE GEAR LEVER IN THE UP POSITION. RETURNED TO BASE FOR MAINTENANCE. REPAIRED BROKEN WIRE ON GEAR ANTI RETRACT SOLENOID. 1L72 3O A20SO 20010918001352001091800135EA 2001 9 18 PNSA010506 220010501G732225245009 SERVO PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA LT ENGINE FAILED A PNSAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AL033588Z 318052130 L840061A LT ENGINE WOULD NOT DEVELOP TAKEOFF POWER. ABORTED TAKEOFF. RETURNED FOR MAINTENANCE. REPLACED FUEL SERVO. 1L72 3O3 O A20SO E14EA 20010502000532001050200053NE 2001 5 2 R004765 320010313G6114D51105 FORK DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE HUB BROKEN B SJ3RO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 GL05SJ3R 2503 2503 HL327 THE PROPELLER WAS RECEIVED FOR COMPLAINT OF VIOLENT VIBRATION. AFTER DISASSEMBLY, INSPECTION REVEALED C7075 BLADE BEARINGS BROKEN, BEARINGS FRAGMENTS EMBEDDED IN BLADE SOCKETS 3, 4 & 6, COMPLOSITE WINDING DAMAGE TO BLADE NR 6, BLADE NR 6 FORK SLOT THIN WALL SIDE BROKEN ON FORK CAM FOLLOWER AND RETENTION WASHER DAMAGED BEYOND LIMITS ON BLADE NR 6 PITCH CHANGE BRACKET, BLADE NR 6 PITCH CHANGE BRACKET BOLTS FAILED INCOMMING TORQUE TEST. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20010502000542001050200054NE 2001 5 2 R004808 320010315G6114C7075 BEARING DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE HUB BROKEN B SJ3RO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 GL05SJ3R 1724 HL87 THE PROPELLER WAS RECEIVED FOR COMPLAINT OF EXCESSIVE VIBRATION. AFTER DISASSEMBLY, INSPECTION REVEALED C7075 BLADE BEARINGS BROKEN, BEARING FRAGMENTS FOUND IN HUB BLADE SOCKETS 2 THROUGH 6, COMPOSITE WINDING DAMAGE TO BLADES 2 THROUGH 4, BLADE NR 4 FORK SLOT THIN WALL SIDE BRIKEN ON FORK CAM FOLLOWER AND B-475 RETENTION WASHER DAMAGED BEYOND REPAIR ON BLADE NR 4 PITCH CHANGE BRACKET, PITCH CHANGE BRACKET BOLTS FAILED TORQUE TEST ON BLADES 3 & 4. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20020129000202002012900020SW 2002 1 29 R20888 120011108G3710 SCREW MOONEYM20 M20J 5870219SW FILTER ATTACH CORRODED B K NONE O OTHER ININSP/MAINT 1 CE03300YB 243010 INSTRUMENT AIR FILTER ATTACHING SCREW CORRODED AND CAUSES METAL DEBRIS TO ENTER VACUUM SYSTEM UNFILTERED. 1L71 3O 2A3 20010925000172001092500017NE 2001 9 25 R3R220010621 220010618G72003015537 SEAL PWA CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE NR 2 ENGINE LEAKING B R3R2K NONE K FLUID LOSS ININSP/MAINT 1 SW01586RE PT285 5500199 PCE70585 FOUND HYDRAULIC PUMP DRIVE PAD ON ENGINE NR 2 LEAKING. NEWLY INSTALLED SEAL I.D. FOUND APPROX. .015 INCH TOO LARGE FOR SHAFT IT IS SUPPOSED TO SEAL. SHAFT DIAMETER: 0.865 INCH, SEAL ID: 0.880 INCH. THIS PROBLEM OCCURRED WITH AT LEAST SIX SEALS BEFORE ONE WAS FOUND WITH THE CORRECT "TIGHT" FIT ON THE DRIVE SHAFT. 1L72 4F4 F A22CE E1NE 20010307006042001030700604 2001 3 7 R7MR291732569 420010108G2311TFM403G TRANSCEIVER SNIAS 350 AS350B2 8680813EU UHF/FM TRANS FAILED B R7MRO OTHER O OTHER NRNOT REPORTED 1 NM0797LG 2917 UNIT FAILED UPON INSTALLATION. UNACCEPTABLE SIDETONE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 20010307006062001030700606EU 2001 3 7 R7MR325232577 120010119G2460SS120 INVERTER SNIAS 350 AS350B3 8680954EU ELELCTRICAL INOPERATIVE B R7MRK NONE O OTHER ININSP/MAINT 1 NM07392LG374 3252 UNIT INOPERATIVE. NO AC OUT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 20010307006052001030700605NM 2001 3 7 R7MR32573 120010110G3150900A3720002111 DISPLAY DOUG MD900 MD900 3027375NM COCKPIT INOPERATIVE B R7MRK NONE O OTHER ININSP/MAINT 1 NM07901CF75 90000012 UNIT INOPERATIVE. ROW OF LIGHTS ON ALPHA DISPLAY MISSING. 1G72 3U NCH19NM 20010307006082001030700608NE 2001 3 7 R7MR32581 220010115G723070BM035420 COMPRESSOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ENGINE SEIZED B R7MRO OTHER O OTHER NRNOT REPORTED 1 NM0797LG 413 2917 COMPRESSOR SEIZED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U3 U H9EU E19EU 20010307006092001030700609NE 2001 3 7 R7MR32582 220010115G723070BM025020 BLADE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE COMPRESSOR FAILED B R7MRO OTHER O OTHER NRNOT REPORTED 1 NM0797LG 413 2917 COMPRESSOR BLADE WILL NOT ROTATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U3 U H9EU E19EU 20010307006362001030700636 2001 3 7 R7MR32592 420010117G2312064010540030 TRANSCEIVER SNIAS 350 AS350B3 8680954EU VHF RADIO INOPERATIVE B R7MRK NONE O OTHER ININSP/MAINT 1 NM07103LN848 3128 UNIT INOPERATIVE. BREKS SQUELCH ON ITS OWN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 20010307006352001030700635EU 2001 3 7 R7MR32595 120010117G77141179405603 INDICATOR BOLKMS117 BK117A4 5626017EU COCKPIT INOPERATIVE B R7MAK NONE O OTHER ININSP/MAINT 1 NM07527RM53 7111 UNIT INOPERATIVE. NO INDICATION WHILE ENGINE IS RUNNING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 20010405001162001040500116NM 2001 4 5 R7MR32618 120010126G6710900C3820021105 ACTUATOR DOUG MD900 MD900 3027375NM M/ROTOR CONTROL LEAKING B R7MRK NONE O OTHER ININSP/MAINT 1 NM07901CF1926 90000012 HYDRAULIC UNIT, DUAL SERVO ACTUATOR, MR CONTROL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEMS. 1G72 3U NCH19NM 20010405001232001040500123NM 2001 4 5 R7MR32619 120010127G2916900H3821502107 GAUGE DOUG MD900 MD900 3027375NM HYD RESERVOIR LOOSE B R7MRK NONE O OTHER ININSP/MAINT 1 NM07901CF2625 90000012 SIGHT GAUGE RIBBON WILL NOT STAY ATTACHED AT BOTTOM OF INDICATOR TUBE, WHICH RENDERS THE QUANTITY OF HYDRAULIC FLUID IN THE RESERVOIR UNRELIABLE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH19NM 20010405001172001040500117EU 2001 4 5 R7MR32629 120010102G6410355A12004008 BLADE SNIAS 350 AS350B2 8680813EU TAIL ROTOR PEELING B R7MRK NONE O OTHER ININSP/MAINT 1 NM0797LG 73 2917 PAINT PEELING. REPLACED WITH NEW UNIT CORRECTED PROBLEM. 1G71 3U H9EU 20010409001902001040900190EU 2001 4 9 R7MR32643 120010104G6720350A33214501 ROD SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL1 60030NE PITCH CONTROL WORN B R7MRK NONE O OTHER ININSP/MAINT 1 NM07103LN310 3128 PITCH CONTROL ROD WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U3 U H9EU E19EU 20010409000062001040900006EU 2001 4 9 R7MR32651 120010128G2460SP461310 SWITCH BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE DC SYSTEM WORN B R7MRK NONE O OTHER ININSP/MAINT 1 NM07117SU1080 7527 TOGGLE SWITCH WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 UNCH13EU E19EU 20010503002302001050300230EU 2001 5 3 R7MR32654 120010111G8000845UN1Q4AA5F SWITCH SNIAS 350 AS350B3 8680954EU STARTER INOPERATIVE B R7MRK NONE O OTHER ININSP/MAINT 1 NM0752281541 3249 UNIT INOPERATIVE. REMOVED AND REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 20010409000072001040900007EU 2001 4 9 R7MR32656 120010226G6320ZARISEC135 TRANSMISSION UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR COLLAPSED B R7MAK NONE L NO TEST NRNOT REPORTED 1 NM07135SJ594 EC1350054 MAIN ROTOR TRANSMISSION COLLAPSED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 UO H88EU E42NE 20010409000092001040900009EU 2001 4 9 R7MR32657 120010228G6220L621M1003101 DAMPER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR WORN B R7MAK NONE O OTHER ININSP/MAINT 1 NM07135SJ946 EC1350054 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. THE REPLACEMENT DAMPER HAS LESS THAN 1 YEAR TO SERVICE LIFE. 1G72 3U3 UO H88EU E42NE 20010409000102001040900010EU 2001 4 9 R7MR32658 120010228G6220L621M1003101 DAMPER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR WORN B R7MAK NONE O OTHER ININSP/MAINT 1 NM07135SJ946 EC1350054 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. SPLITLINE CRACK LONGER THAN 40MM. REPLACED WITH NEW UNIT, CORRECTED PROBLEM NOTE: THE REPLACEMENT DAMPER HAS LESS THAN 1 YEAR TO SERVICE LIFE. 1G72 3U3 UO H88EU E42NE 20010409000202001040900020EU 2001 4 9 R7MR32659 120010228G6220L621M1003101 DAMPER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR WORN B R7MAK NONE O OTHER ININSP/MAINT 1 NM07135SJ390 EC1350054 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. SPLITLINE CRACK LONGER THAN 40MM. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. NOTE: THE REPLACEMENT DAMPER HAS LESS THAN 1 YEAR TO SERVICE LIFE. 1G72 3U3 UO H88EU E42NE 20010409000212001040900021EU 2001 4 9 R7MR32660 120010228G6220L621M1003101 DAMPER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR WORN B R7MAK NONE O OTHER ININSP/MAINT 1 NM07135SJ390 EC1350054 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. SPLITLINE CRACK LONGER THAN 40MM. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. NOTE: THE REPLACEMENT DAMPER HAS LESS THAN 1 YEAR TO SERVICE LIFE. 1G72 3U3 UO H88EU E42NE 20010409000232001040900023EU 2001 4 9 R7MR32661 120010228G6220L621M1003101 DAMPER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR WORN B R7MAK NONE O OTHER ININSP/MAINT 1 NM07135SJ390 EC1350054 REPLACED WITH LOWER DAMPER. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. NOTE: THE REPLACEMENT DAMPER HAS LESS THAN 1 YEAR TO SERVICE LIFE. 1G72 3U3 UO H88EU E42NE 20010409000242001040900024EU 2001 4 9 R7MR32662 120010228G6220L621M1003101 DAMPER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR WORN B R7MAK NONE O OTHER ININSP/MAINT 1 NM07135SJ390 EC1350054 REPLACED WITH LOWER DAMPER. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. NOTE: THE REPLACEMENT DAMPER HAS LESS THAN 1 YEAR TO SERVICE LIFE. 1G72 3U3 UO H88EU E42NE 20010409000252001040900025EU 2001 4 9 R7MR32663 120010228G6220L621M1003101 DAMPER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR WORN B R7MAK NONE O OTHER ININSP/MAINT 1 NM07135SJ390 EC1350054 REPLACED WITH LOWER DAMPER. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. NOTE: THE REPLACEMENT DAMPER HAS LESS THAN 1 YEAR TO SERVICE LIFE. 1G72 3U3 UO H88EU E42NE 20010409000292001040900029EU 2001 4 9 R7MR32664 120010228G6220L621M1003101 DAMPER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR WORN B R7MAK NONE O OTHER ININSP/MAINT 1 NM07135SJ390 EC1350054 SPLITLINE CRACK LONGER THAN 40MM. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. NOTE: THE REPLACEMENT DAMPER HAS LESS THAN 1 YEAR TO SERVICE LIFE. 1G72 3U3 UO H88EU E42NE 20010409003262001040900326SO 2001 4 9 R7MR32667 120010125G6410704A33633171 HINGE EMB 120 EMB120 3260201SO TAIL ROTOR WORN C R7MRK NONE O OTHER ININSP/MAINT 1 NM0792GL 460 120092 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS FROM 1 EACH KIT PART NUMBER 355A33-2153-00, CORRECTED PROBLEM. 2 TEETERING BEARINGS EQUALS 1 KIT. 2L72 4T RTA31SO 20010409000312001040900031EU 2001 4 9 R7MR32670 120010125G6410704A33633116 BEARING SNIAS 350 AS350B2 8680813EU TAIL ROTOR WORN C R7MRK NONE O OTHER ININSP/MAINT 1 NM0792LG 460 2575 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS FROM 1 EACH KIT PART NUMBER 355A09-1036-01 CORRECTED PROBLEM. 4 HALF SHELLS EQUALS 1 KIT. 1G71 3U H9EU 20010409000322001040900032EU 2001 4 9 R7MR32671 120010105G6410704A33633116 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN C R7MRK NONE O OTHER ININSP/MAINT 1 NM0794LG 649 2728 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS FROM 1 EACH KIT PART NUMBER 355A09-1036-01, CORRECTED PROBLEM. 4 HALF SHELLS EQUALS 1 KIT. 1G71 3U3 U H9EU E19EU 20010409000382001040900038EU 2001 4 9 R7MR32675 120010130G6220704A3363320851 STOP SNIAS 350 AS350B2 8680813EU M/R STARFLEX WORN C R7MRK NONE O OTHER ININSP/MAINT 1 NM0792LG 1203 2575 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 20010409000392001040900039EU 2001 4 9 R7MR32676 120010130G6220704A3363320851 STOP SNIAS 350 AS350B2 8680813EU M/R STARFLEX WORN C R7MRK NONE O OTHER ININSP/MAINT 1 NM0792LG 1203 2575 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 20010409003772001040900377EU 2001 4 9 R7MR32677 120010130G6220704A3363320851 STOP SNIAS 350 AS350B2 8680813EU M/R STARFLEX WORN C R7MRK NONE O OTHER ININSP/MAINT 1 NM0792LG 1203 2575 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 20010409000462001040900046EU 2001 4 9 R7MR32683 120010204G2932MA12401 PRESSURE SWITCH SNIAS 350 AS350B2 8680813EU HYD SYSTEM INOPERATIVE C R7MRK NONE O OTHER ININSP/MAINT 1 NM0792LG 12 2575 PRESSURE SWITCH INOPERATIVE. HYDRAULIC LIGHT GOES OUT WHEN SWITCH IS TAPPED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 20010409001572001040900157EU 2001 4 9 R7MR32697 120010127G6230350A37112602 SCISSORS SNIAS 350 AS350B2 8680813EU SWASHPLATE WORN C R7MRK NONE O OTHER ININSP/MAINT 1 NM0792LG 460 2575 WORN BEYOND SERVICEABLE LIMITS. SCARRED BUSHING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 20010409001582001040900158EU 2001 4 9 R7MR32698 120010127G6230704A33640021 SPACER SNIAS 350 AS350B2 8680813EU SWASHPLATE WORN C R7MRK NONE O OTHER ININSP/MAINT 1 NM0792LG 460 2575 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM. 1G71 3U H9EU 20010409002112001040900211 2001 4 9 R7MR32704 420010221G3120B1894522282A CLOCK SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL1 60030NE COCKPIT INOPERATIVE B R7MRK NONE O OTHER ININSP/MAINT 1 NM07397LG193 3268 UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U3 U H9EU E19EU 20010409002152001040900215 2001 4 9 R7MR32706 420010202G3416150201182 ALTIMETER SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL1 60030NE COCKPIT INOPERATIVE B R7MRK NONE O OTHER ININSP/MAINT 1 NM07397LG175 3268 UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U3 U H9EU E19EU 20010409002382001040900238NE 2001 4 9 R7MR32713 220010222G7261350A54113800 TUBE SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL1 60030NE AIR OIL VENT CRACKED B R7MRK NONE O OTHER ININSP/MAINT 1 NM07397LG91 3268 CRACKED BEYOND SERVICABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U3 U H9EU E19EU 20010409002402001040900240 2001 4 9 R7MR32716 420010103G3160B19030MC02 DISPLAY SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL1 60030NE COCKPIT INOPERATIVE B R7MRK NONE O OTHER ININSP/MAINT 1 NM07397LG163 3268 UNIT INOPERATIVE. WILL NOT TRANSFER INFORMATION BETWEEN SCREENS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U3 U H9EU E19EU 20011127000262001112700026CE 2001 11 27 RASFTYRK178 120011113G712045A34361005 MOUNT BRACKET BEECH MU300 400A 1155402CE LT ENGINE CRACKED B ERY2K NONE O OTHER ININSP/MAINT 1 SO11708TA3367 RK178 WHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 50 PERCENT THROUGH THE LOWER HALF. 2H72 4F RTA16SW 20011127000282001112700028CE 2001 11 27 RASFTYRK180 120011113G712045A34361005 MOUNT BRACKET BEECH MU300 400A 1155402CE LT ENGINE CRACKED B ERY2K NONE O OTHER ININSP/MAINT 1 SO11709TA3201 RK180 WHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 75 PERCENT THROUGH THE LOWER HALF. 2H72 4F RTA16SW 20011127000292001112700029CE 2001 11 27 RASFTYRK183 120011113G712045A34361005 MOUNT BRACKET BEECH MU300 400A 1155402CE LT ENGINE CRACKED B ERY2K NONE O OTHER ININSP/MAINT 1 SO11710TA3195 RK183 WHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 75 PERCENT THROUGH THE LOWER HALF. 2H72 4F RTA16SW 20011127000302001112700030CE 2001 11 27 RASFTYRK189 120011113G712045A34361005 MOUNT BRACKET BEECH MU300 400A 1155402CE LT ENGINE CRACKED B ERY2K NONE O OTHER ININSP/MAINT 1 SO11715TA3107 RK189 WHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 80 PERCENT THROUGH THE LOWER HALF. 2H72 4F RTA16SW 20020110000922002011000092CE 2002 1 10 RASFTYRK195 120011231G712045A34361005 MOUNT BRACKET BEECH MU300 400A 1155402CE LT ENGINE CRACKED B ERY2K NONE O OTHER ININSP/MAINT 1 SO11718TA2992 RK195 CRACK FOUND IN LT FORWARD ENGINE MOUNT BRACKET WHILE PERFORMING FLUORESCENT PENETRANT INSPECTION AS PER RAYTHEON AIRCRAFT SAFETY COMMUNIQUE NR 189. 2H72 4F RTA16SW 20020110000932002011000093CE 2002 1 10 RASFTYRK198 120011127G712045A34361005 MOUNT BRACKET BEECH MU300 400A 1155402CE LT ENGINE CRACKED B ERY2K NONE O OTHER ININSP/MAINT 1 SO11798TA2805 RK198 WHILE PERFORMING A ROUTINE SCHEDULED INSPECTION, INSPECTORS NOTED THE LT FORWARD ENGINE MOUNT BRACKET TO BE CRACKED APPROX 75 PERCENT THROUGH THE LOWER HALF. 2H72 4F RTA16SW 20010925000232001092500023CE 2001 9 25 RFS20011 120010808G3233NAS464P4A29 BOLT CESSNA CESSNA210 210K 2073446CE MLG ACTUATOR CRACKED B K NONE O OTHER ININSP/MAINT 1 SW998142G5891 1781 21059442 WHILE REPLACING THE RT MLG ACTUATOR AS PART OF COMPIANCE WITH CESSNA SEB01-2, IT WAS DISCOVERED THAT ONE OF THE THREE NAS ATTACH BOLTS WAS BROKEN.IT WAS ONLY BEING HELD IN PLACE BY THE SAFETY WIRE LINKING THE THREE BOLTS. THE BOLT HAD FAILED BETWEEN THE FIRST AND SECOND THREADS COUNTING FROM THE SHANK OF THE BOLT. PROCURED AND INSTALLED 3EA NEW NAS BOLTS TO CORRECT. 1H71 3O 3A21 20010925000322001092500032NE 2001 9 25 RO 220010820G723030756441 CARBON SEAL ALIDSG AMD FALC90FALCON900EX 2730009EU GARRTTTFE731TFE73160 NE HP CASE BROKEN B E ENGINE SHUTDOWN K FLUID LOSS NRNOT REPORTED 1 SW99 1101 NA N990WM 112239 THE NR 4 CARBON SEAL CERAMIC RING WAS FOUND TO BE BROKEN DURING THE ENGINE TEARDOWN. THE CARBON RING SEAL WAS ALSO FOUND BROKEN. THERE WAS MUCH COLLATERIAL DAMAGE. THE OPERATOR REPORTED OIL LOSS DURING FLIGHT WITH SUBSEQUENT OIL CONTAMINATION UPON POST FLIGHT ENGINE EXAMINATION. THERE WILL BE AN ENGINE CONDITION REPORT GENERATED TO DETAIL THE FINDINGS POST ANALYTICAL INSPECTION. 2L73 4F4 FRTA46EU E1NM 20010925000342001092500034WP 2001 9 25 RO462097 220010905G723030745557 STATOR AMD FALC50FALCON900 2700160EU GARRTTTFE731TFE7315BR WP COMPRESSOR SEPARATED B C ABORTED TAKEOFF MY OVER TEMP ENGINE STOPPAGE TOTAKEOFF 1 SW99 2462 95146 ENGINE RETURNED FOR MAINTENANCE WHEN AIRCRAFT WAS EXPERIENCING ENGINE TEMPERATURE LIMIT AT TAKE OFF AND SUBSEQUENT HUNG STARTS. THE INNER HUB OF THE 4TH LOW COMPRESSOR STATOR WAS FOUND SEPARATED DURING ENGINE MAINTENANCE DISASSEMBLY. MAJOR ENGINE COMPONENT DOWNSTREAM DAMAGE OCCURED AS SECONDARY DAMAGE. ENGINE MANUFACTURER NOTIFIED OF THIS UNIQUE FINDINGS. 2L73 4F4 FRTA46EU E6WE 20010424002822001042400282SO 2001 4 24 RX8R2001001 120010413G52804252931 SKIN PIPER PA42 PA42720 7104212SO PWA PT6 PT6A61 52043EA HARTZLHCB3T HCB3TN3 GL MLG DOOR DEBONDED B RX8RK NONE O OTHER ININSP/MAINT 1 SO15RX8R 5203 11 425501038 PCE99080 BU10583 AFTER LANDING IT WAS NOTICED THAT THE RIGHT INBOARD LANDING GEAR DOOR SKIN HAD PEELED OFF FROM THE REST OF THE DOOR AT THE LEADING EDGE. UPON FURTHER EXAMINATION THE DOOR SKIN AND SUPPORTING STRUCTURE WHICH ARE BONDED TOGETHER WITH STRUCTURAL ADHESIVE SHOWED CORROSION AT THE BONDING SURFACE ON BOTH THE DOOR SKIN AND THE DOOR STRUCTURE. OPERATORS OF PA42-720 AIRCRAFT MAY WANT TO INSPECT THE LEADING EDGE OF THE INB. LNDG. DOORS FOR CORROSION AND SEPARATION OF THE SKIN. 1L72 4T4 T A23SO E4EA 6 CP15EA 20010503000412001050300041EU 2001 5 3 RYMR32642 120010106G6420350A33214501 CONTROL ROD SNIAS 350 AS350B3 8680954EU PITCH CONTRL WORN B R7MAK NONE O OTHER ININSP/MAINT 1 NM0752285505 3251 WORN BEYOND SERVICEABLE LIMITS. REMOVED AND REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 20010724005232001072400523NM 2001 7 24 S012730131 120010403G7100 FCU BOEING747 747209B NM PWA JT9 JT9D7R4G2 52054NE W SAJFE ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 WP03 24628 725343 B-18771 #2 ENG FLAME OUT AT FL330,TAT -4C,EGT 352 DEG.C,EPR 1.02 & DROPPING,ENG SHUTDOWN,WINDMILLED APPROX. 1 MIN AT OIL PRESS 22 PSI,ENG WAS RESTARTED & OPERATED NORMALLAY.C/A:1.I.A.W AMM 71-00-43,MAIN FUEL FILTER AND EVBC FUEL FILTER INSPED NML AND REPLACED. 2.CHECKED EVBC PT3 AND PS3 WATER TRAP,NO WATER EVIDENCE FOUND. 3.PFMED FUEL TANKS WATER DRAINING. 4.REPLACED FUEL CONTROL UNIT AND FUEL PUMP ASSY. 5.REPLACED FUEL HEATER DUE MOUNT BOLTS INSERT DAMAGED. 6.PFMED WINDMILLING INSP,MAIN OIL FILTER AND ALL MAGNETIC CHIP DETECTORS INSPED NML. 7.ENG RUN-UP TEST WITH TAKEOFF POWER SATISFACTORY. 8.AFTER TEST OF REMOVED PARTS FOR FINAL INVESTIGATION,THE MAIN CAUSE OF THE IFSD APPEARS TO BE A LEAN FCU ALONG WITH PO 2L74 4F4 FRTA20WE E3NE 20010614000192001061400019NE 2001 6 14 S01472016 220010426G7200 ENGINE BOEING747 747400 NM PWA 4056 PW4056 NE NR 4 FAILED W SAJFC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP03 40413 24311 717621 COMPLETE REGISTRATION NUMBER (B18273) AFTER T/O THRUST HAS SET ON T/O ROLLING, LOUD BANG SOUND WAS HEARD, T/O IS ABORTED AT 110 KNOTS. (1) IAW FIM 71-00-00, ENGINE SURGE DURING FORWARD THRUST FIG 107 PERFORM ENGINE 4 INLET FAN BLADE, FAN CASE DUCT SEGMENTS, TURBINE EXHAUST AREA AND 6TH TURBINE BLADE INSP NORMAL. (2) BORESCOPE INSP (HPC 5,6,10TH STAGE AND HPT 1,2ND STAGE: LPT 3RD STAGE BLADE), CONDITION NORMAL. (3)2.5 AND 2.9 BLEED VALVE AND VSV SYS CHECK NORMAL. (4 )REPLACED NR 4 ENGINE AND RUN UP CHECK NORMAL. 2L74 4F4 FRTA20WE E24NE 20010111027352001011102735CE 2001 1 11 SAILJ1052 120010102G3230508200646 TORQUE TUBE RAYTHN NA BEECH 90 C90 1152913CE PWA PT6 PT6A21 52043EA HARTZLHCB3T HCB3TN3 GL MLG CRACKED B K NONE O OTHER ININSP/MAINT 1 SO136356C5726 NA LJ1052 AIRCRAFT CAME INTO MAINTENANCE FOR SCHEDULED TBO OF THE LANDING GEAR MOTOR. THE MOTOR IS ATTACHED TO THE LANDING GEAR GEARBOX WHICH IS ALSO ATTACHED TO THE FAILED TORQUE TUBE. INSPECTION SHOWED NO EVIDENCE OF CORROSION. FAILURE AREA IS LOCATED AT AND AROUND THE ATTACH HARDWARE HOLES HOWEVER,INSPECTION REVEALED NO EVIDENCE OF IMPOPER INSTALLATION, ALIGNMENT, BINDING OR CONDITION THAT MIGHT BE ATTRIBUTE TO THE FAILURE. A COPY OF THIS REPORT WAS PROVIDED TO LOCAL FSDO 13 WEST COLUMBIA, SC. ASI/BOB SWITTER/ASI BILL ROBERTS FOR THEIR REVIEW. NO INCIDENT OR INJURY WAS INVOLVED. 1L72 3T4 T 3A20 E4EA 6 CP15EA 20010111005632001011100563NM 2001 1 11 SROM200100001 120010102G323065446916 HYDROMECH UNIT BOEING737 737205 NM NLG MALFUNCTIONED C SROMA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03733AR6 23466 DEPARTING ANC NOSE GEAR WOULD NOT RETRACT - STAYED DOWN & LOCKED - TRIED TWICE WITH SAME RESULTS. RETURNED TO ANC LANDING WT 111.7 SMOOTH LANDING.ACCOMPLISHED OVERWEIGHT LANDING INSPECTION PER M/M 5-51-291. REPLACED NOSE GEAR HYD. MODULAR PACKAGE REF. MM 32-33-31. REPLACED NOSE GEAR ACT. FLOW RESTRICTOR REF. MM 32-00. REPLACED NG GRAVEL DEFLECTOR ACTU. REF. MM SUP. 32-23-22NOTE: MODULAR PACKAGE REPLACED TO CORRECT PROBLEM - RESTRICTOR AND ACTUATOR REPLACEMENT WERE PRECAUTIONARY. 2L72 4F A16WE 20010111005892001011100589NM 2001 1 11 SROM200100002 120010104G3233 ACTUATOR BOEING737 737205 NM NLG FAILED C SROMA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03733AR 23466 AIR TURNBACK DUE TO NOSE GEAR WOULD NOT RETRACT THIS IS A REPEAT EVENT THAT LAST HAPPENED 7 LANDINGS AGO. REPLACED NOSE GEAR LOCK MECHANISM AND SPRINGS, CONSISTING OF INDIVIDUAL ITEMS P/N 65-46245-4, 65-46242-11, 65-46240-13 & 69-6745-1, ALL WITH 1327 HOURS AND 1009 LANDINGS SINCE OVERHAUL. REPLACED HYDRAULIC TRANSFER CYCLINDER P/N 69-14106-7 WITH 10 HOURS AND 7 LANDINGS SINCE OVERHAUL. REPLACED LOCK ACTUATOR P/N 65-17819-14 WITH 1327 HOURS AND 1009 LANDINGS SINCE OVERHAUL. RE-RIGGED NOSE GEAR DOORS. PERFORMED NORMAL RETRACTION AND EXTENSION TESTS. PERFORMED EMERGENCY EXTENSION TEST. ALL TESTS NORMAL. 2L72 4F A16WE 20010409001812001040900181NM 2001 4 9 SROM200100003 120010201G335058782 LEAD BOEING737 737205 NM CABIN FAILED C SROMK NONE L NO TEST ININSP/MAINT 1 AL03733AR 6 23466 FLOOR TRACK LIGHTING - FORWARD CABIN INOP REPLACED FORWARD TRACE STRIP. OPS CHECKED OK FOUND OPEN IN ELECTRICAL CIRCUIT OF STRIP. 2L72 4F A16WE 20010409000612001040900061NM 2001 4 9 SROM200100004 120010202G33501010425 LENS BOEING737 737205 NM CABIN BROKEN C SROMK NONE O OTHER ININSP/MAINT 1 AL03736BP 3 23465 OVERHEAD ENERGENCY LIGHT ROW 2 IS BROKEN NOTE: LENS ONLY BROKEN. REPLACED UNIT P/N 10-1042-5. EMER LT OPS CK GOOD. 2L72 4F A16WE 20010502000502001050200050NM 2001 5 2 SROM200100005 120010308G322265737625 STRUT BOEING737 737290C 138448VNM NLR DISCHARGED C SROMA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03740AS581723 22578 AFTER TAKEOFF NOSE GEAR DID NOT LOCK UP, RED NOSE GEAR LIGHT ON, SYS A PRESURE NORMAL BUT FLUCTUATING SLIGHTLY AND ABNORMAL NOISES COMING FROM NOSE WHEEL, CYCLED GEAR DOWN 3 GREEN, RETRACTED SAME PROBLEM, LANDED NORMALLY. FOUND NOSE STRUT FLAT, ACCOMPLISHED NOSE GEAR STRUT SERVICE PER TASK CARD 18232017. ACCOMPLISHED GEAR RETRACT & FREE FALL TEST, OPS CHECKS GOOD, REMOVED NOSE GEAR JACK AND PAR. CHANGES SCHRADER VALVE. 2L72 4F A16WE 20010502000622001050200062 2001 5 2 SROM200100006 420010319G34228221088001 INDICATOR BOEING737 737205 NM COCKPIT FAILED C SROMA UNSCHED LANDING O OTHER CRCRUISE 1 AL03736BP1 1 23465 DURING NORMAL CRUISE FLIGHT, 45 MINUTES INTO THE FLIGHT, THE FIRST OFFICIERS 5ATI EHSI WENT BLACK, FLICKERED BACK ON MOMENTARILY A FEW TIMES AND THEN STAYED BLACK. THIS WAS A NEW DISPLAY ON ITS FIRST FLIGHT. 2L72 4F A16WE 20010418002982001041800298NM 2001 4 18 SROM200100007 120010223G531165582805 FRAME BOEING737 737205 NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED C SROMK NONE O OTHER ININSP/MAINT 1 AL03736BP 23465 DURING C CHECK INSPECTION, FOUND CORROSION ON FRAME. 2L72 4F4 F A16WE E2EA 20010418002992001041800299NM 2001 4 18 SROM200100008 120010223G5310694820416 SHEAR TIE BOEING737 737205 NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED C SROMK NONE O OTHER ININSP/MAINT 1 AL03736BP 23465 DURING C CHECK, FOUND CORROSION ON SHEAR TIE. 2L72 4F4 F A16WE E2EA 20010418003002001041800300NM 2001 4 18 SROM200100009 120010223G532065582806 ANGLE BOEING737 737205 NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED C SROMK NONE O OTHER ININSP/MAINT 1 AL03736BP 23465 DURING C CHECK INSPECTION, FOUND LEVEL 1 CORROSION ON ANGLE. 2L72 4F4 F A16WE E2EA 20010418003022001041800302NM 2001 4 18 SROM200100010 120010223G53136948948501 STRINGER BOEING737 737205 NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED C SROMK NONE O OTHER ININSP/MAINT 1 AL03736BP 23465 DURING C CHECK INSPECTION, FOUND CORROSION ON STRINGER. 2L72 4F4 F A16WE E2EA 20010418003032001041800303NM 2001 4 18 SROM200100011 120010307G5743658276415 BEAM BOEING737 737205 NM PWA JT8 JT8D17 52049NE LT MLG CORRODED C SROMK NONE O OTHER ININSP/MAINT 1 AL03736BP29717 23465 DURING C CHECK INSPECTION, FOUND THE LEFT MLG BEAM HAS SEVERAL AREA OF LEVEL 1 CORROSION ON LOWER SURFACE AT PANEL MOUNTING HOLES. 2L72 4F4 F A16WE E2EA 20010418003092001041800309NM 2001 4 18 SROM200100012 120010310G5330 SKIN BOEING737 737205 NM PWA JT8 JT8D17 52049NE FUSELAGE CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03736BP29717 23465 DURING C CHECK INSPECTION, FOUND A CRACK IN THE FORWARD GALLEY DOOR (R1) EXTERIOR SKIN AT LOWER HINGE CUTOUT CRACKED AT UPPER CORNER. 2L72 4F4 F A16WE E2EA 20010418003042001041800304NM 2001 4 18 SROM200100013 120010310G5330 SKIN BOEING737 737205 NM PWA JT8 JT8D17 52049NE FUSELAGE CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03736BP29717 23465 DURING C CHECK INSPECTION, FOUND A CRACK IN SKIN AT UPPER HINGE CUTOUT ON THE FORWARD GALLEY DOOR. 2L72 4F4 F A16WE E2EA 20010418003052001041800305NM 2001 4 18 SROM200100014 120010312G53306546881143 SKIN BOEING737 737205 NM PWA JT8 JT8D17 52049NE FUSELAGE CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03736BP29717 23465 DURING C CHECK INSPECTION, FOUND SKIN DAMAGE/CRACK AT THE FORWARD APU DOOR HINGE CUTOUT. 2L72 4F4 F A16WE E2EA 20010410002722001041000272NM 2001 4 10 SROM200100015 120010312G53306546881143 SKIN BOEING737 737205 NM FUSELAGE CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03736BP29717 23465 DURING C CHECK INSPECTION FOUND SKIN DAMAGE/CRACK AT APU DOOR AFT HINGE CUTOUT. 2L72 4F A16WE 20010418003062001041800306NM 2001 4 18 SROM200100016 120010313G5330655298873 SKIN BOEING737 737205 NM PWA JT8 JT8D17 52049NE FUSELAGE CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03736BP 23465 DURING C CHECK INSPECTION, FOUND A SKIN CRACK AT AFT ENTRY DOOR (L2) CUTOUT (LOWER). 2L72 4F4 F A16WE E2EA 20010424002662001042400266NM 2001 4 24 SROM200100017 120010323G534365465431 ATTACH FITTING BOEING737 737205 NM FUSELAGE CORRODED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733AR294493332 23466 DURING C CHECK INSPECTION FOUND CORROSION ON BORE AND FACES OF BS 685 LUG, LT. REPAIRED PER EA 5310-01930. 2L72 4F A16WE 20010424002672001042400267NM 2001 4 24 SROM200100018 120010323G5330654576960 SKIN BOEING737 737205 NM FUSELAGE CORRODED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733AR294493332 23466 DURING C CHECK INSPECTION, FOUND LEVEL 1 CORROSION ON SKIN. REPAIRED PER EA 5330-01517. 2L72 4F A16WE 20010424002682001042400268NM 2001 4 24 SROM200100019 120010403G5720656717217 FITTING BOEING737 737205 NM LT WING CORRODED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733AR294493332 23466 DURING C CHECK INSPECTION, FOUND CORROSION ON ATTACH FITTING. REPLACED FITTING PER MM 57-15-50. 2L72 4F A16WE 20010424002692001042400269NM 2001 4 24 SROM200100020 120010321G5330654577453 SKIN BOEING737 737205 NM FUSELAGE GOUGED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733AR294491704 23466 DURING C CHECK INSPECTION, FOUND FUSELAGE EXTERNAL SKIN GOUGE BS 830 STRINGER 22 LT. REPAIRED PER SRM 53-30-03 FIGURE 6. 2L72 4F A16WE 20010424002702001042400270NM 2001 4 24 SROM200100021 120010321G5330654577453 SKIN BOEING737 737205 NM FUSELAGE GOUGED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733AR294491704 23466 DURING C CHECK INSPECTION, FOUND FUSELAGE EXTERNAL SKIN GOUGED AT BS 890 STRINGER 21 LT. REPAIRED PER SRM 53-30-03 FIGURE 6. 2L72 4F A16WE 20010424002712001042400271NM 2001 4 24 SROM200100022 120010323G5743656717218 FITTING BOEING737 737205 NM LT WING CORRODED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733AR294493332 23466 DURING C CHECK INSPECTION AND MAIN LANDING GEAR TIME CHANGE, FOUND FACES OF RT MLG I/B STABILIZER AFT MOUNT FITTING CORRODED. REPLACED FITTING PER MM 57-15-0/SOPM 20-50-01 DWG 65-82770. 2L72 4F A16WE 20010925000352001092500035 2001 9 25 SROM200100023 420010522G34208221088001 DISPLAY BOEING737 737205 NM COCKPIT FAILED C SROMA UNSCHED LANDING O OTHER CRCRUISE 1 AL03736BP299 299 23465 CAPTAINS 5 ATI EHSI FAILED IN CRUISE FLIGHT. INSTUMENT DISPLAY WAS STILL PRESENTED, BUT WAS NON-FUNCTIONAL WITH A "DU FAILURE" ANNUNCIATOR LIT. REPLACEMENT UNIT CORRECTED THE PROBLEM. 2L72 4F A16WE 20010925000362001092500036NM 2001 9 25 SROM200100025 120010712G335058209 LIGHT BOEING737 737205 NM CABIN DEFECTIVE C SROMK NONE L NO TEST ININSP/MAINT 1 AL03733PA 6 23466 L1 EXIT LIGHT AT BOTTOM RIGHT CORNER IS VERY DIM. REPLACED BATTERY PACK AND LIGHT/LENS, ALSO REPAIRED BROKEN WIRE AT CONNECTOR. PERFORMED OPS CHECK WITH NO AMBIENT LIGHT, BRIGHTNESS EQUAL TO OTHER EXIT SIGNS. 2L72 4F A16WE 20010925000372001092500037NM 2001 9 25 SROM200100026 120010821G2910106056342 LINE BOEING737 737205 NM HYD SYSTEM CHAFED C SROMHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL03736BP 1 23465 DURING NORMAL CRUISE FLIGHT LEFT "A" SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED, LEFT "A" SYSTEM PUMP TURNED OFF AND NOTICED QUNTITY WAS LOW, THEN "A" SYSTEM RIGHT SIDE STARTED TO FLUCUATE AND SHUT DOWN WITH RETURN TO ANC. INSPECTION FOUND PRESSURE LINE CHAFFED THRU AT GENERATOR BLAST TUBE SUPPORT JUST AFT OF PUMP. REPLACE LINE. AND ADDED CLAMP STAND OFF. REPLACED CASE DRAIN FILTER WHICH WAS FOUND CLEAN. OPS AND LEAK CHECKED GOOD. REFILLED HYD SYSTEM. REF. 29-11-41. 2L72 4F A16WE 20011009000352001100900035NM 2001 10 9 SROM200100027 120011008G5210694070310 COVER BOEING737 737205 NM PAX DOOR BROKEN C SROMA UNSCHED LANDING O OTHER CLCLIMB 1 AL03736BP 47 23465 "EXTREMELY LOUD AIR LEAK FROM L1 DOOR. RETURNED TO PANC." INSP FOUND L-1 DOOR LOWER HINGE TOP TRIM PIECE HAD BROKEN LOOSE AND JAMMED IN DOOR HINGE. REPLACED HINGE FLAP ASSY. PRESS A/C NO LEAKS. 2L72 4F A16WE 20020129001522002012900152NM 2002 1 29 SROM200100028 120011101G32336544604 ACTUATOR BOEING737 737205 1384456NM MLG DEFECTIVE C SROMA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03733PA 1084 23466 ON GRAVEL DEFLECTOR EQUIPED AIRCRAFT NOSE GEAR WOULD NOT LOCK UP AFTER T/O. CYCLED GEAR WITH SAME RESULTS. NOSE GREEN LIGHT GOES OUT, BUT RED LIGHT STAYS ON WITH AIR NOISE HEARD. GEAR LOCKED DOWN OK. REMOVED AND REPLACED NOSE GEAR GRAVEL DEFLECTOR ACTUATOR PER MM 32-23-22. LUBED NOSE GEAR PER TASK CARD 18212000. OPS CK PER TASK 18132003. EMERGENCY EXTENSION CK GOOD. FOUND STRUT FLAT SERVICED PER A/C PLACARD. 2L72 4F RTA16WE 20020129001532002012900153NM 2002 1 29 SROM200100029 120011123G3222657376210 MODULE BOEING737 737205 1384456NM NLG INTERMITTENT A SROMA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03733PA 2795 23466 ON GRAVEL DEFLECTOR EQUIPED AIRCRAFT "ON DEPARTURE FROM ANCHORAGE NOSE WHEEL WOULD NOT RETRACT CYCLED GEAR ONCE, NOSE WHEEL WOULD NOT RETRACT, RETURNED TO AIRPORT FOR OVERWEIGHT LANDING WAS SMOOTH AND NORMAL". AIRCRAFT PLACED ON JACKS AND GEAR TESTED NORMAL. AS PRECAUTION REPLACED NLG MODULAR PACKAGE, AND LUBED GEAR. GEAR AGAIN TESTED NORMAL. 2L72 4F RTA16WE 20020130000222002013000022NM 2002 1 30 SROM200100030 120011125G3220657376210 LANDING GEAR BOEING737 737205 1384456NM NOSE INOPERATIVE C SROMA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03733PA 2796 23466 ON GRAVEL DEFLECTOR EQUIPED AIRCRAFT "NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF - RETURNED TO AIRPORT". 2L72 4F RTA16WE 20020130000232002013000023NM 2002 1 30 SROM200100031 120011213G3220657376210 LANDING GEAR BOEING737 737205 1384456NM NOSE CONTAMINATED C SROMA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03733PA 2869 23466 ON GRAVEL DEFLECTOR EQUIPED AIRCRAFT "NOSE GEAR RED LIGHT STAYED ON AFTER GEAR RETRACTION (GEAR SOUNDED LIKE IT DID NOT RETRACT COMPLETELY) RECYCLED GEAR SAME PROBLEM. RETURNED TO ANC LANDING WT. WAS 109.7. INSP. FOUND SLUSH IN GEAR AREA (NOSE) AND STRUT WAS A LITTLE LOW. CLEANED GEAR OF SLUSH AND RESET NOSE STRUT PRESS. LUBED NOSE GEAR CYCLED NOSE SEVERAL TIMES OPS CK GOOD. 2L72 4F RTA16WE 20010419001342001041900134SW 2001 4 19 SW152001 120010321G6510476441809 SHAFT BELL 47 47 1180602SW TAIL ROTOR FAILED G HFZSBR EMER. DESCENT AUTOROTATION DF INFLIGHT SEPARATION FLT CONT AFFECTED UKUNKNOWN 1 SW151575 73 TAIL ROTOR DRIVE FAILURE. TAIL ROTOR FORWARD SHAFT, AFT COUPLING FAILURE. LOSS OF LUBRICATION DUE TO STRIPPED TREADS ON SCREW ILLUSTRATED PARTS BREAKDOWN. 1G71 3O H1 20010510002492001051000249WP 2001 5 10 SW15200110389 120010315G6230369D22014 MAST HUGHES369 369E 4470707WP ALLSN 250C 250C20B 03013GL MAIN ROTOR FLAKING H K NONE O OTHER ININSP/MAINT 1 SW15500TP5200 5200 0494E CAE836593 COATING FLAKING OFF INNER DIAMETER OF MAIN ROTOR STATIC MAST. COATING CHIPS FALLING INTO MAIN ROTOR TRANSMISSION. CAUSE OF FLAKING, UNKNOWN. NO FACTORY REPAIR AUTHORIZED IN THE MHI. FACTORY REPS HAVE NOT YET AUTHORIZED A REPAIR. EFFECT ON MAST AND TRANSMISSION. 1G71 3U3 U H3WE E4CE 20010510002482001051000248WP 2001 5 10 SW15200110390 120010315G6230369D22014 MAST HUGHES369 369E 4470707WP ALLSN 250C 250C20B 03013GL MAIN ROTOR FLAKING H K NONE O OTHER ININSP/MAINT 1 SW15600TP5200 5200 525 CAE836593 COATING FLAKING OFF INNER DIAMETER OF MAIN ROTOR STATIC MAST. COATING CHIPS FALLING INTO MAIN ROTOR TRANSMISSION. CAUSE OF FLAKING UNKNOWN. NO FACTORY REPAIR AUTHORIZED IN THE HMI. FACTORY REPS HAVE NOT YET AUTHORIZED A REPAIR. EFFECT ON MAST AND TRANSMISSION? 1G71 3U3 U H3WE E4CE 20010503001352001050300135CE 2001 5 3 SW15200110531 120010326G5330002440000143 DOUBLER BEECH 33 35C33 1151408CE CONT O470 IO470* 17026SO FUSELAGE CRACKED H K NONE O OTHER ININSP/MAINT 1 SW1594SS 9446 CD1089 DURING 100 HOUR INSPECTION FOUND CRACKS IN THE DOUBLER TALL PN 002440000143. THE DOUBLER IS CRACKED JUST FORWARD OF THE AFT BULKHEAD APPROX 1 INCH JUST BEFORE THE RADIUSED AREA EXTENDING OUTBOARD .2500. 1L71 3O3 O 3A15 E1CE 20010503001492001050300149CE 2001 5 3 SW15200110535 120010326G5520639204 BUSHING BEECH 33 35C33 1151408CE CONT O470 IO470* 17026SO COUNTERWEIGHT IMPROPER PART H K NONE O OTHER ININSP/MAINT 1 SW1594SS CD1089 THE INCORRECT BUSHING WAS IDENTIFIED DURING DEMINSIONAL INSPECTION OF THE COUNTER- WEIGHT PRIOR TO INSTALLATION. 1L71 3O3 O 3A15 E1CE 20010503000032001050300003CE 2001 5 3 SW15200110536 120010328G531200244002465 BULKHEAD BEECH 33 35C33 1151408CE CONT O470 IO470* 17026SO FUSELAGE CRACKED H K NONE O OTHER ININSP/MAINT 1 SW151444M7583 CD827 DURING 100 HOUR INSPECTION FOUND CRACKS IN THE DOUBLER TAIL, A CRACK ON THE RIGHT HAND SKIN SECTION AND A CRACK ON THE AFT BULKHEAD APPROX 1 INCH AT THE BEGINNING OF THE RADIUSED AREA RADIATING OUTBOARD .7500 ON THE RIGHT SIDE AND .5000 ON THE LEFT SIDE. THE SKIN SECTION IS CRACKED 1.75 INCH FROM THE AFT EDGE OF THE SKIN, JUST ABOVE THE CRACK IN THE DOUBLER EXTENDING OUTBOARD .7500 INCH. THE BULKHEAD CRACKS EXTENDS .3750 INCH DOWN THE RADIUSED AREA AT THE TOP LEFT HAND CORNER. 1L71 3O3 O 3A15 E1CE 20010503003152001050300315EA 2001 5 3 SW15200110851 220010405G7314LW15473 PUMP PIPER PA28 PA28* SO LYC O360 IO360A1A 41514EA FUEL SYSTEM DEFECTIVE D K NONE O OTHER ININSP/MAINT 1 SW15 0 L977336A PART INSTALLED NEW AT OVERHAUL. TEST CESS OPERATION WITHIN REQUIRED PRESSURE AND FLOW. AT INSTALLATION IN AIRCRAFT, PUMP WOULD NOT FUNCTION AND WOULD NOT ALLOW FUEL TO BE PUMPED THRU USING BOOST PUMP. 1L71 3O3 O 2A13 1E10 20010802000862001080200086SO 2001 8 2 SW15200111824 120010425G3110 KNOB PIPER PA46 PA46310P 7104605SO MOR CONTROL INOPERATIVE C K NONE O OTHER ININSP/MAINT 1 SW15184AL 4697026 MANUAL OVER RIDE (MOR) CONTROL LEVER KNOB CAME APART CAUSING THIS SYSTEM TO BE RENDERED INOPERATIVE AND A CERTAIN SAFETY ISSUE. PROBLEM CAN BE SOLVED WITH PROPER INSTALLATION. THIS AIRCRAFT JUST COMPLETED A PHASE I AND II INSPECTION. 1L71 3O RTA25SO 20010802000872001080200087CE 2001 8 2 SW15200112233 120010423G6123B15941 SPRING HARTZL BEECH 95 95B55 1152729CE FEATHERING SPRNGCORRODED C K NONE O OTHER ININSP/MAINT 1 SW152023Z EB488 TC2171 UPON DISASSEMBLY OF THIS PROPELLER FOR OVERHAUL IT WAS NOTED THAT THIS FEATHERING SPRING WAS BROKEN AND SHOWS SIGNS THAT IT HAS BEEN BROKEN FOR SOME TIME. THE BREAK WAS BETWEEN THE 1ST AND 2ND COIL AND WAS ALSO CORRODED. 1L72 3O RT3A16 20010802000892001080200089SO 2001 8 2 SW15200112234 120010427G6120 FORK HARTZL PIPER PA23 PA23160 7102304SO PITCH CHANGE CRACKED C K NONE O OTHER ININSP/MAINT 1 SW1576HK 3341 AY34B 231423 AT OVERHAUL THE PITCH CHANGE FORK NR B2457-3 WAS FOUND TO HAVE A CRACK APPROX. .1875 INCHES IN LENGTH LOCATED AT THE LOWER INSIDE RADIUS OF THE NR 2 BLADE PITCH CHANGE SLOT. 1L72 3O 1A10 20010802000912001080200091GL 2001 8 2 SW15200112284 320010517G6110 BULKHEAD CESSNA172 172D 2072410CE LYC O320 O320* 41508EA MCAULY1C172 1C172EM GL PROPELLER CRACKED G K NONE O OTHER ININSP/MAINT 1 SW1554855497 497 17275068 FORWARD PROPELLER BULKHEAD HAS BEEN CRACKING WITH MINIMAL HOURS. BOLTS HAVE BEEN PROPERLY TORQUED AND SAFETY WIND. 1H71 3O3 ONT3A12 E274 5 NP910 20010802000932001080200093CE 2001 8 2 SW15200112285 120010516G554104330106 SPAR CESSNA150 152 2071835CE RUDDER CRACKED D K NONE O OTHER ININSP/MAINT 1 SW15497804684 15281314 CRACK IN UPPER LIGHTING HOLE, UNDER THE TOP HINGE, IN THE LEADING EDGE RUDDER SKIN/SPAR. TO PREVENT RECURRANCE, REMOVE OR ELEMINATE LIGHTING HOLE IN NEW OR REPLACEMENT PARTS. 1H71 3O NT3A19 20010925000582001092500058EU 2001 9 25 TI1R001403 120010122G62401179405303 TACHOMETER BOLKMS117 BK117A1 5626010EU COCKPIT FAILED B TI1RO OTHER O OTHER NRNOT REPORTED 1 SW05 TRIPLE TACHOMETER - ROTOR TACHOMETER FAILED. REMOVED AND REPLACED. 1G72 3U H13EU 20010821000552001082100055 2001 8 21 TI1R001405 420010221G34161042011968E ALTIMETER COCKPIT INOPERATIVE B TI1RO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW05 ALTIMETER, ENCO - CODE OFF FLAG WILL NOT STOW. REMOVED AND REPLACED. 20010821000632001082100063 2001 8 21 TI1R001428 420010409G34215040017926 LIGHT BOLKMS117 BK117B2 5626013EU ATTITUDE GYRO INOPERATIVE B TI1RO OTHER O OTHER NRNOT REPORTED 1 SW05117MK 7196 ATTITUDE GYRO, INTERNAL LIGHTING, INOPERATIVE. REMOVED AND REPLACED. 1G72 3U NCH13EU 20010913002732001091300273EU 2001 9 13 TI1R001441 120010407G78103039621 CLAMP UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE EXHAUST CRACKED B TI1RK NONE O OTHER ININSP/MAINT 1 SW05911SV 0070 EXHAUST CLAMP, CRACK ON BAND END. REMOVED AND REPLACED. 1G72 3U3 UO H88EU E42NE 20010925001012001092500101EU 2001 9 25 TI1R001442 120010424G2810L281M20C1002 TANK UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN FUEL CELL LEAKING B TI1RK NONE K FLUID LOSS ININSP/MAINT 1 SW05911SV 0070 MAIN TANK LEAKING. REMOVED AND REPLACED. 1G72 3U3 UO H88EU E42NE 20010913002752001091300275EU 2001 9 13 TI1R001444 120010409G6230L623M2005101 SWASHPLATE UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR EXCESS PLAY B TI1RO OTHER O OTHER NRNOT REPORTED 1 SW05911SV1034 0070 SWASHPLATE, REMOVED AT AEC REQUEST, EXCESSIVE PLAY. REMOVED AND REPLACED. 1G72 3U3 UO H88EU E42NE 20010925001022001092500102EU 2001 9 25 TI1R001445 120010409G53204649305034 SUPPORT UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE SUPPORT TUBE LOOSE B TI1RK NONE O OTHER ININSP/MAINT 1 SW05911SV 0070 SUPPORT TUBE, REMOVED AT AEC REQUEST, EXCESSIVE PLAY BETWEEN SUPPORT TUBE AND SLIDING TUBE. REMOVED AND REPLACED. 1G72 3U3 UO H88EU E42NE 20010925001032001092500103EU 2001 9 25 TI1R001446 120010409G6220L623M1002105 CLAMP UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR INOPERATIVE B TI1RK NONE O OTHER ININSP/MAINT 1 SW05911SV 0070 ROTOR SCISSOR CLAMP, REMOVED AT AEC REQUEST, REMOVED AND REPLACED. 1G72 3U3 UO H88EU E42NE 20010925001042001092500104EU 2001 9 25 TI1R001447 120010422G324010477665 CYLINDER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE BRAKE ASSY LEAKING B TI1RK NONE K FLUID LOSS ININSP/MAINT 1 SW05911SV1231 0070 BRAKE CYLINDER, LEAKING FLUID, REMOVED AND REPLACED. 1G72 3U3 UO H88EU E42NE 20010925001062001092500106EU 2001 9 25 TI1R001449 120010503G532011780184111 SPACER BOLKMS117 BK117A1 5626010EU FUSELAGE MISMANUFACTURED B TI1RK NONE W INADEQUATE Q C ININSP/MAINT 1 SW05 SPACER - SPACERS HAVE NO GROOVE CUT INTO THEM FOR THE ORING. REMOVED AND REPLACED. 1G72 3U H13EU 20010925001132001092500113EU 2001 9 25 TI1R001464 120010428G28229A2045 CARTRIDGE UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE FUEL PUMP INOPERATIVE B TI1RK NONE O OTHER ININSP/MAINT 1 SW05911SV 0070 FUEL PUMP CARTRIDGE, PUMP INOPERATIVE, TRIPS CIRCUIT BREAKER. 1G72 3U3 UO H88EU E42NE 20010913002832001091300283 2001 9 13 TI1R001467 420010512G34215040017926 GYRO BOLKMS117 BK117B2 5626013EU ATTITUDE TUMBLES B TI1RO OTHER O OTHER NRNOT REPORTED 1 SW05117MK 7196 ATTITUDE GYRO, TUMBLING, REMOVED AND REPLACED. 1G72 3U NCH13EU 20010913002852001091300285EU 2001 9 13 TI1R001471 120010522G7714L771M40C1005 INDICATOR UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE TRIPLE TACH ERRATIC B TI1RO OTHER O OTHER NRNOT REPORTED 1 SW05911SV 0070 TRIPLE TACHOMETER INDICATOR, NR NEEDLE ERRATIC, REMOVED AND REPLACED. 1G72 3U3 UO H88EU E42NE 20010913002862001091300286EU 2001 9 13 TI1R001472 120010526G28229A2045 CARTRIDGE UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE FUEL PUMP FAULTY B TI1RO OTHER O OTHER NRNOT REPORTED 1 SW05911SV 0070 FUEL PUMP CARTRIDGE, POSITIVE TERMINAL GROUNDED, TRIPS BREAKER. REMOVED AND REPLACED. 1G72 3U3 UO H88EU E42NE 20010913002872001091300287EU 2001 9 13 TI1R001473 120010526G28229A2045 CARTRIDGE UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE FUEL PUMP INTERMITTENT B TI1RO OTHER O OTHER NRNOT REPORTED 1 SW05911SV 0070 FUEL PUMP CARTRIDGE, MOTOR INTERMITTENT, REMOVED AND REPLACED. 1G72 3U3 UO H88EU E42NE 20010913002952001091300295 2001 9 13 TI1R001481 420010618G3160066040211411 SYMBOL GENERATOR BOLKMS117 BK117B2 5626013EU COCKPIT MALFUNCTIONED B TI1RO OTHER O OTHER NRNOT REPORTED 1 SW05117MK SIGNAL GENERATOR, INTERMITTENTLY CAUSES EFIS TO GO TO (TEST IN PROGRESS)-THEN ERROR OF SIGNAL ON EFIS T, REMOVED AND REPLACED. 1G72 3U NCH13EU 20010913002962001091300296 2001 9 13 TI1R001482 420010616G34254021541671 INDICATOR COCKPIT DEFECTIVE B TI1RO OTHER O OTHER NRNOT REPORTED 1 SW05 ARTIFICIAL HORIZON, HSI - WILL NOT STABILIZE, ROLLING RIGHT/ DIVING. REMOVED AND REPLACED. 20010913002972001091300297 2001 9 13 TI1R001483 420010606G3422060001500 GYRO DIRECTIONAL GYRODAMAGED B TI1RK NONE W INADEQUATE Q C ININSP/MAINT 1 SW05 KG102A DIRECTIONAL GYRO - RECEIVED WITH CONNECTOR GUIDE PIN BROKEN AND LOOSE HARDWARE INSIDE AND SEAL ON BOTTOM. REMOVED AND REPLACED. 20010913003012001091300301EU 2001 9 13 TI1R001488 120010410G243523081057 STARTER GEN UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE ENGINE INOPERATIVE B TI1RO OTHER O OTHER NRNOT REPORTED 1 SW05911SV1231 0070 STARTER GENERATOR, NEEDS BRUSH REPLACEMENT AND RUN-IN. 2000 TBO REMOVED AND REPLACED. 1G72 3U3 UO H88EU E42NE 20010913003022001091300302 2001 9 13 TI1R001489 420010628G3442066308432 INDICATOR BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE RADAR INOPERATIVE B TI1RO OTHER O OTHER NRNOT REPORTED 1 SW05313LS2773 7509 IN FLIGHT 6, INDICATION UNIT STOPS FUNCTIONING. SCREW FELL OUT FROM INSIDE. REMOVED AND REPLACED COLOR RADAR IND. 1G72 3U3 UNCH13EU E19EU 20010809002572001080900257EU 2001 8 9 TXEA81788 120010423G6420350A33200406 BEARING SNIAS 350 AS350BA 8680817EU T/R SPIDER LOOSE H K NONE O OTHER ININSP/MAINT 1 SW0922TV 10 1591 BEARING HAS PLAY. 1G71 3U NCH9EU 20020205000522002020500052GL 2002 2 5 V5MR198Y 120010924G322011799001 BRACKET CIRRUSSR SR22 2130001GL NLG DAMAGED B V5MRK NONE O OTHER ININSP/MAINT 1 GL15705CD54 0005 NOSE WHEEL PANT BRACKETS, QTY 2, FOUND WITH ELONGATED MOUNTING HOLES UNDER NORMAL USE. AIRCRAFT HAS BEEN OPERATED BY A SINGLE INDIVIDUAL WITH MINIMAL TAKEOFFS AND LANDING IN APPROXIMATELY FOUR MONTHS TIME. FURTHERMORE, THE MOUNTING HOLES IN THE NEW REPLACEMENT PART ARE LARGER THAN THE AN3 BOLT THAT IS SPECIFIED TO SECURE IT TO THE FORK ASSEMBLY. THE HOLE IS LARGER THAN .1875 OF INCH (AN3) BUT SMALLER THAN .2500 OF AN INCH. NO BUSHINGS ARE SPECIFIED IN THE MFG IPC. 1L71 3O NTA00009CH 20020205000532002020500053GL 2002 2 5 V5MR198Y1 120010924G322011799001 BRACKET CIRRUSSR SR20 05628AJGL CONT IO360 IO360* 17025CE NLG ELONGATED B V5MRK NONE O OTHER ININSP/MAINT 1 GL156000C244 1037 NOSE WHEEL PANT BRACKETS, QTY2, FOUND WITH ELONGATED MOUNTING HOLES UNDER NORMAL USE. AIRCRAFT HAS BEEN OPERATED BY A SINGLE INDIVIDUAL WITH MINIMAL TAKEOFFS AND LANDING IN APPROXIMATELY ONE YEARS TIME. FURTHERMORE, THE MOUNTING HOLES IN THE NEW REPLACEMENT PART ARE APPRECIABLY LARGER THAN THE AN3 BOLT THAT IS SPECIFIED TO SECURE IT TO THE FORK ASSEMBLY. THE HOLE IS LARGER THANT .1875 OF INCH BUT SMALLER THAN .2500 OF AN INCH. 1L71 3O3 ONTA00009CHE1CE 20020205000542002020500054GL 2002 2 5 V5MR198Y2 120010924G322012936001 BUMPER BLOCK CIRRUSSR SR20 05628AJGL CONT IO360 IO360* 17025CE NLG DETERIORATED B V5MRK NONE O OTHER ININSP/MAINT 1 GL152014Y344 1078 REBOUND BUMPERS, QTY 2, FOUND VERY DETERIORATED UNDER NORMAL USE. THEY WERE IN SERVICE FOR 344.4 HOURS IN LESS THAN ONE YEAR. THE AIRCRAFT IS OPERATED AS PART OF A CLUB AND SEES MANY TAKEOFF AND LANDING CYCLES. THE DETERIORATION COULD BE DUE TO INTERACTION WITH ENGINE SOLVENTS AND/OR HEAT. 1L71 3O3 ONTA00009CHE1CE 20020205000552002020500055GL 2002 2 5 V5MR198Y3 120010924G322011799001 BRACKET CIRRUSSR SR20 05628AJGL CONT IO360 IO360* 17025CE NLG ELONGATED B V5MRK NONE O OTHER ININSP/MAINT 1 GL152014Y402 1078 NOSE WHEEL PANT BRACKETS, QTY 2, FOUND WITH ELONGATED MOUNTING HOLES UNDER NORMAL USE. AIRCRAFT HAS BEEN OPERATED AS A CLUB AIRCRAFT WITH MANY TAKEOFFS AND LANDING IN LESS THAN ONE YEARS TIME. FURTHERMORE, THE MOUNING HOLES IN THE NEW REPLACEMENT PART ARE APPRECIABLY LARGER THAN THE AN3 BOLT THAT IS SPECIFIED TO SECURE IT TO THE FORK ASSEMBLY. 1L71 3O3 ONTA00009CHE1CE 20020205000572002020500057GL 2002 2 5 V5MR198Y5 120010924G322012936001 BUMPER BLOCK CIRRUSSR SR20 05628AJGL CONT IO360 IO360* 17025CE NLG DETERIORATED B V5MRK NONE O OTHER ININSP/MAINT 1 GL15197CD344 1098 REBOUND BUMPERS, QTY 2, FOUND MISSING SINCE LAST INSPECTION. THEY WERE IN NORMAL SERVICE FOR 223.7 HOURS IN LESS THAN ONE YEAR. AIRCRAFT SEES MINIMAL TAKEOFF AND LANDING CYCLES. THE DETERIORATION AND SUBSEQUENT LOSS OF THE PARTS IN QUESTION COULD BE DUE TO INTERACTION WITH ENGINE SOLVENTS AND/OR HEAT. DUE TO VIBRATION CAUSED BY SHIMMY OF THE NOSE LANDING GEAR STRUT ASSEMBLY PN 11907-003 OR BY SHIMMY OF A NOES WHEEL PANT THAT IS LOOSE ON ITS PANT BRACKETS PN 1179-001. 1L71 3O3 ONTA00009CHE1CE 20010509002902001050900290SO 2001 5 9 WI2 220010422G7260632617 GEAR CESSNA337 337 2075702CE CONT O360 IO360C 17025SO ACCESSORY DRIVE WORN D K NONE O OTHER ININSP/MAINT 1 GL132364S104 0664 060696R ACCESSORY DRIVE GEAR TEETH WORN AWAY 104 HOURS SINCE INSTALLATION. GEAR HAD BEEN INSTALLED DUE TO FAILURE OF PREVIOUS GEAR FOR THE SAME REASON. DRIVEN GEAR WAS NOT WORN. 1H72 3O3 O A6CE E1CE 20010509002912001050900291SO 2001 5 9 WI3 220010427G7260632617 GEAR CESSNA337 337 2075702CE CONT O360 IO360C 17025SO ACCESSORY DRIVE WORN D K NONE O OTHER ININSP/MAINT 1 GL132397S317 0697 060694R ACCESSORY DRIVE GEAR TEETH WORN AWAY 317 HOURS SINCE FACTORY REBUILD OF ENGINE. DRIVEN GEAR WAS NOT WORN. 1H72 3O3 O A6CE E1CE 20010515000842001051500084SO 2001 5 15 WP012001B1728 120010102G3244850X6 TIRE PIPER PA12 PA12 7101202SO MLG MISMANUFACTURED G K NONE O OTHER ININSP/MAINT 1 WP013021M 121576 MOUNTED TWO GOODYEAR 8.50 X 6 6PR TIRES, PN856C61-3, ON CLEVELAND WHEELS. ONE TIRE APPEARED LARGER IN DIAMETER THAN THE OTHER. MEASURED BOTH TIRES, AT 25PSI ONE TIRE IS 20.1250 AND THE OTHER IS 20.9375 IN DIAMETER. 1H71 3O A780 20011009000362001100900036SW 2001 10 9 WTXR200100277 120010926G282031024691 LINE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP FUEL MANIFOLD CRACKED B WTXRK NONE K FLUID LOSS TXTAXI/GRND HDL 1 SW99332BA TC222E P54132 AFTER LANDING AND TAXING TO RAMP, PILOT NOTICED FLUID RUNNING OUT OF BOTTOM OF ENGINE COWLING. ENGINE WAS SHUT DOWN AND MAINTENANCE WAS CALLED.MAINTENANCE FOUND A CRACK IN THE FUEL MANIFOLD AT THE 6 O'CLOCK POSITION,IN THE "B" NUT FITTING NECK. INSTALLED SERVICABLE MANIFOLD, LEAK CHECKED OK. 2L72 4T4 TRTA8SW E4WE 20010802001172001080200117 2001 8 2 WVBA2001034 420010521G2210KA132 SWITCH ALIDSG PIPER PA31 PA31350 7103110SO ACCEL SWITCH FAILED C WVBAO OTHER O OTHER NRNOT REPORTED 1 AL0142WP 2305 2305 3512 318252038 PILOT REPORTED SWITCH WOULD NOT TEST IN EITHER POSITION. SWITCH WAS REMOVED FROM SERVICE. PARTS TAKE FROM 3 TO 12 WEEKS TO BE DELIVERED RENDERING THE AUTOPILOT INOPEATIVE FOR THAT TIME FRAME. WITH SWITCHES FAILING RIGHT OUT OF THE BOX OR VERY FEW HOURS IN SERVICE, WE RECOMMEND ELIMINATING THIS SWITCH FRO THE SYSTEM AS THE AUTOPILOT CAN STILL BE PHYSICALLY OVERCOME OR MANUALLY CUT OFF BY A SWITCH ON THE YOKE. 1L72 3O A20SO 20010802001182001080200118SO 2001 8 2 WVBA2001035 120010521G29131213HBG310 PUMP PIPER PA31 PA31350 7103110SO HYDRAULIC SYS FAILED C WVBAO OTHER J WARNING INDICATION NRNOT REPORTED 1 AL01300ED 192 317852008 PILOT REPORTED RIGHT HYDRAULIC PUMP FAILED CHECK DURING RUN UP. PUMP WAS REMOVED AND IT WAS DISCOVERED THAT THE SHAFT HAD SHEARED. DURING REMOVAL OF THE FITTINGS IT WAS DISCOVERED THAT THE SMALL PRESSED IN NOZZLE, SPRING AND BALL HAD COME LOOSE WITH THE BALL JAMMING THE PUMP VANES AND CAUSING THE SHAFT TO SHEAR. NOTE: THIS WAS ON THE PRESSURE OUTLET SIDE. THE PUMP WAS REMOVED AND REPLACED. 1L72 3O A20SO 20010802001192001080200119SO 2001 8 2 WVBA2001036 120010529G2140A23D04 REGULATOR PIPER PA31 PA31350 7103110SO HEATER LEAKING C WVBAK NONE K FLUID LOSS ININSP/MAINT 1 AL0142WP 160 318252038 DURING INSPECTION IT WAS NOTICED THAT FUEL STAIN WAS IN THE DRAIN TUBE OF THE FUEL PRESSURE REGULATOR OF THE FRONT COMBUSTION HEATER. THE REGULATOR WAS INSPECTED AND FOUND TO BE LEAKING FROM THE GASKET OF THE UPPER PARTING SURFACE. UNIT WAS REMOVED AND REPLACED. IT SHOULD BE NOTED THAT THIS UNIT WAS INSPECTED PER SB WHICH INCLUDES A PRESSURE CHECK TO COMPLY WITH AD AND WAS DETERMINED SERVICABLE. TIME SINCE INSPECTION WAS 59 HOURS. 1L72 3O A20SO 20020124000252002012400025SW 2002 1 24 YTRR077311 120011129G6330 BEARING BELL 206 206L1 1182107SW RESTRAINT WORN H YTRAK NONE O OTHER ININSP/MAINT 1 FS01142DP331 LK0765 45585 SPHERICAL BEARING CAME UNSTAKED WHICH ALLOWED THE BEARING TO FLOAT IN THE LATERAL SPRING ARM. 1G71 3U H2SW 20020124000282002012400028SW 2002 1 24 YTRR077356 120011206G6710206062721103 ACTUATOR BELL 206 206L1 1182107SW MAIN ROTOR SEIZED H YTRAO OTHER O OTHER NRNOT REPORTED 1 FS01142DP386 45585 THE LINEAR ACTUATOR OPERATED FOR APPROXIMATELY 3 MONTHS BEFORE FAILING. CAUSE OF THE FAILURE IS UNKNOWN. PART RETURNED TO PRECISION HELIPARTS FOR EVALUATION. 1G71 3U H2SW 20010502000412001050200041SO 2001 5 2 ZVSR409Y 120010220G5522 SKIN GULSTMG1159 G1159 3953505SO ELEVATOR CORRODED B K NONE O OTHER ININSP/MAINT 1 SO11117JJ 163 EXTENSIVE SURFACE CORROSION ON HORIZONTAL STABILIZER AND ELEVATORS. CORROSION ON ELEVATORS EXTENDED THROUGH THE SKIN SURFACE. CORROSION WAS FOUND WHILE AIRCRAFT WAS IN MAINTENANCE FOR AN EXTERIOR PAINT JOB. CORROSION WAS FOUND AFTER PAINT WAS STRIPPED AND A VISUAL INSPECTION WAS PREFORMED. 2L72 4F RTA12EA