Revision:

INFORMATION SYSTEMS

Mounting Device

(Class 2) (Continued)

(M) May be inoperative provided:

a) Associated EFB and hardware is secured by an alternate means or removed from the aircraft, and

b) Procedures do not require its use.



				Revision:	ORIGINAL
				Date: 01/15/2009





DEPARTMENT OF TRANSPORTATION

FEDERAL AVIATION ADMINISTRATION

WASHINGTON , D.C.





MASTER MINIMUM EQUIPMENT LIST





EMB-500

	Douglas L. Edwards
	Chairman, Flight Operations Evaluation Board (FOEB)




Federal Aviation Administration
Kansas City Aircraft Evaluation Group
DOT Building
901 Locust Street , Room 332
Kansas City , MO 64106-2641


		Telephone:	(816)-329-3233
		FAX:	(816)-329-3241


--	Cover Page	--
--	Table of Contents	I
--	Log of Revisions	II
--	Control Page(s)	III, IV
--	Highlights of Change	V
--	Definitions	VI
--	Preamble	VII
--	Guidelines for (O) & (M) Procedures	VIII, IX, X
--	Guidelines for (O) & (M) Procedures	XI, XII, XIII
--	Guidelines for (O) & (M) Procedures	XIV
21	Air Conditioning	21-1, 2, 3
22	Autopilot	22-1, 2, 3
23	Communications	23-1, 2, 3
24	Electrical	24-1
25	Equipment/Furnishings	25-1 THRU 5
27	Flight Controls	27-1
28	Fuel	28-1
30	Ice & Rain Protection	30-1, 2
31	Indicating/Recording Systems	31-1, 2
33	Lights	33-1, 2
34	Navigation	34-1 THRU 6
35	Oxygen	35-1, 2
36	Pneumatics	36-1
38	Water/Waste	38-1
46	Information Systems	46-1, 2
52	Doors	52-1
73	Engine Fuel & Control	73-1
79	Engine Oil	79-1


Cover Page	-	ORIGINAL	01/15/2009
Table of Contents	I	ORIGINAL	01/15/2009
Log of Revisions	II	ORIGINAL	01/15/2009
Control Page	III	ORIGINAL	01/15/2009
	IV	ORIGINAL	01/15/2009
Highlights of Change	V	ORIGINAL	01/15/2009
Definitions	VI	ORIGINAL	01/15/2009
Preamble	VII	ORIGINAL	01/15/2009
Guidelines for (O) & (M) Procedures	VIII	ORIGINAL	01/15/2009
	IX	ORIGINAL	01/15/2009
	X	ORIGINAL	01/15/2009
	XI	ORIGINAL	01/15/2009
	XII	ORIGINAL	01/15/2009
	XIII	ORIGINAL	01/15/2009
	XIV	ORIGINAL	01/15/2009
21	21-1	ORIGINAL	01/15/2009
	21-2	ORIGINAL	01/15/2009
	21-3	ORIGINAL	01/15/2009
22	22-1	ORIGINAL	01/15/2009
	22-2	ORIGINAL	01/15/2009
	22-3	ORIGINAL	01/15/2009
23	23-1	ORIGINAL	01/15/2009
	23-2	ORIGINAL	01/15/2009
	23-3	ORIGINAL	01/15/2009
24	24-1	ORIGINAL	01/15/2009
25	25-1	ORIGINAL	01/15/2009
	25-2	ORIGINAL	01/15/2009
	25-3	ORIGINAL	01/15/2009
	25-4	ORIGINAL	01/15/2009
	25-5	ORIGINAL	01/15/2009
27	27-1	ORIGINAL	01/15/2009
28	28-1	ORIGINAL	01/15/2009
30	30-1	ORIGINAL	01/15/2009
	30-2	ORIGINAL	01/15/2009
31	31-1	ORIGINAL	01/15/2009
	31-2	ORIGINAL	01/15/2009
33	33-1	ORIGINAL	01/15/2009
	33-2	ORIGINAL	01/15/2009


34	34-1	ORIGINAL	01/15/2009
	34-2	ORIGINAL	01/15/2009
	34-3	ORIGINAL	01/15/2009
	34-4	ORIGINAL	01/15/2009
	34-5	ORIGINAL	01/15/2009
	34-6	ORIGINAL	01/15/2009
35	35-1	ORIGINAL	01/15/2009
	35-2	ORIGINAL	01/15/2009
36	36-1	ORIGINAL	01/15/2009
38	38-1	ORIGINAL	01/15/2009
46	46-1	ORIGINAL	01/15/2009
	46-2	ORIGINAL	01/15/2009
52	52-1	ORIGINAL	01/15/2009
73	73-1	ORIGINAL	01/15/2009
79	79-1	ORIGINAL	01/15/2009

The FOEB has identified a need for certain procedures to provide an adequate level of safety while providing relief for the following items. These procedures must be established by the operator. The following guidelines are to help establish these required procedures:

21-23-05	(O) Operations procedure to ensure both Bleed Systems and the Vapor Cycle System are not operated on the ground and flight operations are not conducted in icing conditions.
21-31-00-1	(O) Operations procedure to ensure airplane is operated by a crew of two, Outflow Valve indication on the MFD operates normally, Manual Control is used and verified operative before each flight, Cabin Pressure Indicators are operative, and the aircraft is not operated above FL 250. (O) Operations procedure to ensure flight is conducted unpressurized at or below 10,000 feet MSL.
21-31-00-3	(O) Operations procedure to ensure flight is conducted unpressurized at or below 10,000 feet MSL.
21-31-00-4	(O) Operations procedure to ensure aircraft is manually depressurized for landings at field elevations above 8,000 feet MSL.
21-31-02	(O) Operations procedure to ensure flight is conducted unpressurized at or below 10,000 feet MSL. (M) Maintenance procedure to ensure NPRV is removed.
21-31-03	(O) Operations procedure to ensure flight is conducted unpressurized at or below 10,000 feet MSL.
21-31-04	(O) Operations procedure to ensure flight is conducted unpressurized at or below 10,000 feet MSL.

21-61-00

(O) Operations procedure to ensure both Pressure Regulating and Shutoff Valves operate normally, Temperature Sensor Indicator on the MFD operates normally, and the Temperature Control Manual Mode is used and verified operative before each flight.

22-122 22-10-01

(O) Operations procedure to ensure PFDs are coupled to operative Flight Director.

22-11-01-4

(O) Operations procedure to ensure the Autopilot is engaged above FL 250/ 250 knots indicated.

22-11-23

(O) Operations procedure to ensure alternate procedures are established and used.

23-51-01-1

(O) Operations procedure to ensure associated function is checked operative by an alternate means.

23-51-00-1

(O) Operations procedure to ensure PA is not required by FAR and alternate procedures are established and used.

23-23-11

(O) Operations procedure to ensure SATCOM Voice or Data Link operates normally, alternate procedures are established and used, SATCOM coverage is available over the intended route of flight, and if INMARSAT Codes are not available while using SATCOM Voice prior coordination with the appropriate ATS facility is required.

24-41-00-1

(O) Operations procedure to ensure alternate procedures are established and used.

25-11-01-2

(M) Maintenance procedure to ensure Armrest is secured in the retracted (UP) position or removed.

25-21-01-1

(M) Maintenance procedure to ensure Seat Back is IMMOVABLE in the full UPRIGHT position.

25-62-01-1

(O) Operations procedure to ensure FAK is resealed in a manner that will identify it as a Unit that cannot be mistaken for a fully serviceable Unit.

25-62-02	(M) Maintenance procedure to ensure inoperative Lifejacket is placarded inoperative and stored out of sight so it cannot be mistaken for a functional unit and the minimum functional units required by regulation are available.
27-14-00	(O) Operations procedure to ensure Aileron Trim Tabs are verified in the NEUTRAL position prior to each flight and the Roll Trim Circuit Breaker is PULLED.
27-14-00-1	(O) Operations procedure to ensure Aileron Trim Tabs are verified CENTERED before each flight.
27-24-00	(O) Operations procedure to ensure Rudder Trim Tab is verified CENTERED before each flight.
28-00-00	(O) Operations procedure to ensure MFD Indications not addressed elsewhere in the MMEL may be inoperative.
28-11-07	(M) Maintenance procedure to ensure inoperative Valve is OPEN and checked for no leakage.
28-11-09	(O) Operations procedure to ensure Fuel Quantity Indication System is operative and if refueling is necessary is done following single side refueling procedure and limited to 60% tanks capacity.
28-41-00	(O) Operations procedure to ensure Aircraft is refueled to full capacity, Fuel Used Indication on the MFD and both Fuel Flow Indicators are operative and monitored throughout the flight, and both Gravity Fuel Caps operate normally.
28-45-01	(O) Operations procedure to ensure the On Side DC Pump is selected ON throughout the flight.
30-00-00	(O) Operations procedure to ensure MFD Indications not addressed elsewhere in the MMEL may be inoperative.
30-13-00	(O) Operations procedure to ensure aircraft is not operated in known or forecast icing conditions and the Wing Boots are verified DEFLATED before each flight. (M) Maintenance procedure to ensure System is DEACTIVATED.

30-15-00

(O) Operations procedure to ensure aircraft is not operated in known or forecast icing conditions and the Wing Boots are verified DEFLATED before each flight.

(M) Maintenance procedure to ensure System is DEACTIVATED.

30-21-00

(O) Operations procedure to ensure aircraft is not operated in known or forecast icing conditions, MFD Nacelle Anti-Ice Switch remains selected OFF, and Anti-Ice Valve is confirmed CLOSED.

30-21-01

(O) Operations procedure to ensure AFM Anti-Icing ON Performance is used.

(M) Maintenance procedure to ensure both Valves are secured OPEN.

31-61-01

(O) Operations procedure to ensure PFD2 Circuit Breaker is PULLED.

(O) Operations procedure to ensure HSDB Switch is set to REV position and MFD Circuit Breakers are PULLED.

33-23-01

(O) Operations procedure to ensure appropriate verbal briefings are given to the passengers.

33-45-01

(O) Operations procedure to ensure Anti-Collision Lights are operative and ON before engine operation.

34-11-01-4

(O) Operations procedure to ensure IESI is reinitialized before each flight.

34-21-00

(O) Operations procedure to ensure operative AHRS is selected as as attitude and heading source to both PFDs and operations are conducted in day VMC only.

34-23-01

(O) Operations procedure to ensure any combination of three Gyro or INS (IRU) Stabilized Compass Systems are operative.

(O) Operations procedure to ensure any combination of two Gyro or INS (IRU) Stabilized Compass Systems operate normally, the Airplane is operated with Dual Independent Navigation Capability, and is under Positive Radar Control by ATC on the enroute portion of the flight.

(O) Operations procedure to ensure the flight is entirely within areas of magnetic unreliability provided at least two Stabilized Directional Gyro Systems are installed, operate normally, and are used in conjunction with approved Free Gyro Navigation Techniques.

34-61-00-1

(O) Operations procedure to ensure current Aeronautical Charts are used, status and suitability of Navigation Facilities to be used are verified, and Approach Navigation Radios are manually tuned and identified.

34-61-01

(O) Operations procedure to ensure alternate procedures are established and used.

34-43-00

(M) Maintenance procedure to ensure System is deactivated and SECURED. Applies to both provisos.

34-43-00

(M) Maintenance procedure to ensure System is deactivated and SECURED. Applies to both provisos.

34-43-00-2

(O) Operations procedure to ensure TA Visual Display and Audio Functions are operative, TA ONLY Mode is selected by the crew, and enroute or approach procedures do not require use of the RA Display System.

34-43-00-3

(O) Operations procedure to ensure RA Visual Display and Audio Functions are operative, and enroute or approach procedures do not require use of the TA Display System.

35-01-01

(M) Maintenance procedure to ensure Gauge is inspected for no leakage and alternate procedures to measure the Oxygen Cylinder pressure is established.

35-01-02	(O) Operations procedure to ensure Cylinder Pressure Gauge is operative and Oxygen pressure is checked in Cylinder before each flight.
35-02-02	(M) Maintenance procedure to ensure Valve is inspected for no leakage and Cylinder is filled outside the aircraft or replaced by a fully charged one.
35-21-00	(O) Operations procedure to ensure flight is conducted unpressurized at or below 10,000 feet MSL.
35-21-00-1	(M) Maintenance procedure to ensure manual deployment function is verified operative each flight day and both Air Bleed Sources operate normally. (O) Operations procedure to ensure flight is conducted at or below 30,000 feet MSL.
35-21-01	(M) Maintenance procedure to ensure affected Seat is placarded and BLOCKED to prevent occupancy.
38-30-00	(M) Maintenance procedure to ensure associated Components are deactivated or isolated and System Components do not have leaks. (M) Maintenance procedure to ensure associated Components are deactivated or isolated, System Components do not have leaks, and the Lavatory Door is secured CLOSED and properly placarded.
46-21-1	(O) Operations procedure to ensure alternate procedures are established and used.
46-21-2	(O) Operations procedure to ensure alternate procedures are established and used.

46-21-3	(O) Operations procedure to ensure alternate procedures are established and used.
46-21-4	M) Maintenance procedure to ensure associated EFB and hardware is secured by an alternate means or removed from the aircraft. (O) Operations procedure to ensure alternate procedures are established and used. (M) Maintenance procedure to ensure associated EFB and hardware is secured by an alternate means or removed from the aircraft.
52-70-00-1	(O) Operations procedure to ensure Door is verified CLOSED and all Latch and/or Lock Indicators are confirmed CLOSED.
52-70-00-2	(O) Operations procedure to ensure Door is verified CLOSED and all Latch and/or Lock Indicators are confirmed CLOSED.
52-70-00-3	(O) Operations procedure to ensure Door is verified CLOSED and all Latch and/or Lock Indicators are confirmed CLOSED.
52-70-00-4	(O) Operations procedure to ensure Door is verified CLOSED and all Latch and/or Lock Indicators are confirmed CLOSED.
73-33-00	(O) Operations procedure to ensure both Wings Fuel Quantity Indications on the EIS are operative and used fuel information on Synoptic Fuel Page and remaining fuel information on the FMS are not used by the flight crew.
79-34-00	(M) Maintenance procedure to ensure there is no chip indication on either engine, Oil Filter is inspected for no clogging, and the oil level is checked and at maximum.
79-34-01	(M) Maintenance procedure to ensure impending bypass information is on only one engine, no chip indication is on either engine, oil level is checked before each flight and repairs are made within two flight hours.

21	AIR CONDITIONING

10-00	Environment Control System Synoptic Display (MFD ECS Page)	C	1	0	MFD Indications not addressed elsewhere in the MMEL may be inoperative.

22-00	Gasper Valves	D	-	0

23-05	Ground Cooling Fan (GCF)	C	1	0	(O) May be inoperative provided: a) Both Bleed Systems are selected OFF on ground operations, b) Operations are not conducted in icing conditions, and c) Vapor Cycle System (VCS) is considered inoperative on ground.

31-00	Cabin Pressure Control System

1)	Automatic Control	C	1	0	(O) May be inoperative provided: a) Airplane is operated by a crew of two, b) Outflow Valve indication on MFD operates normally, c) Manual Control is used and verified operative before each flight, d) Cabin Pressure indications are operative, and

					(Continued)

21	AIR CONDITIONING

1)	Automatic Control (Continued)

					e) Airplane is operated at or below FL 250.

		C	1	0	(O) May be inoperative provided flight is conducted unpressurized at or below 10,000 feet MSL.

2)	Manual Control	C	1	0	May be inoperative provided: a) Automatic Mode is operative, and b) Airplane is operated at or below FL 250.

		C	1	0	May be inoperative provided flight is conducted unpressurized at or below 10,000 feet MSL.

3)	Cabin Pressure Parameters (Altitude, Rate, Delta-P) Indication	C	1	0	(O) May be inoperative provided flight is conducted unpressurized at or below 10,000 feet MSL.

4)	Landing Field Elevation (LFE) Indication	C	1	0	(O) May be inoperative provided that for landing field elevation above 8,000 feet MSL, the airplane is manually depressurized before landing.

31-02	Outflow Valve (OFV)	C	1	0	(O)(M) May be inoperative provided: a) NPRV is removed and, b) Flight is conducted unpressurized at or below 10,000 feet MSL.

31-03	Negative Pressure Relief Valve (NPRV)	C	1	0	(O) May be inoperative provided flight is conducted unpressurized at or below 10,000 feet MSL.

21	AIR CONDITIONING

31-04	Pressure Relief Valve (PRV)	C	1	0	(O) May be inoperative provided flight is conducted unpressurized at or below 10,000 feet MSL.

52-00	Vapor Cycle System (VCS)	C	1	0	May be inoperative provided OAT is limited to no more than ISA +19C.

52-04	Evaporator Fans

1)	Cabin Fan	C	1	0

2)	Cockpit Fan	C	1	0	May be inoperative provided: a) Cabin Fan is operative, b) Vapor Cycle System is operative, and c) OAT is limited to no more than ISA +22C.

		C	1	0	May be inoperative provided: a) Cabin Fan is operative, and b) OAT is limited to no more than ISA +19C.

61-00	Temperature Control System – Automatic Control	C	1	0	(O) May be inoperative provided: a) Both Pressure Regulating and Shutoff Valves (PRSOV) operate normally, b) Temperature Sensor indication on MFD operates normally, and c) Temperature Control Manual Mode is used and verified operative before each flight.

22	AUTOPILOT

10-00	Autopilot System	C	1	0	May be inoperative provided: a) Flight is conducted with a two pilot flight crew, and b) RVSM operations are not conducted. NOTE: Altitude Hold function required for RVSM.

10-01	Flight Director	C	2	1	(O) If Flight Director is required, PFDs must be coupled to operative one.

					NOTE: Navigation and Approach Modes sources are selected only through the PFD on the side of the operative Flight Director, unless CDIs are synchronized.

		C	2	0	May be inoperative provided operations do not require Autopilot use.

10-02	Yaw Damper Function	C	1	0	May be inoperative provided the airplane is operated at or below FL 250/ 250 knots indicated.

11-01	Guidance Panel (GP)

1)	Course Buttons (CRS)	C	2	0	May be inoperative provided operations do not require its use.

2)	Flight Director (FD) Buttons	C	2	0	May be inoperative provided operations do not require its use.

3)	Autopilot (AP) Button	C	1	0	May be inoperative provided Autopilot is considered inoperative.

22	AUTOPILOT

4)	Yaw Damper (YD) Button	C	1	0	(O) May be inoperative provided Autopilot is operative and engaged above FL 250 or 250 knots indicated.

		C	1	0	May be inoperative provided the airplane is operated at or below FL 250 and 250 knots indicated.

5)	Couple (CPL) Button	C	1	0

6)	Navigation (NAV) Mode Button	C	1	0	May be inoperative provided operations do not require its use.

7)	Heading (HDG) Mode Button	-	1	0	May be inoperative provided Autopilot is considered inoperative.

8)	Heading (HDG) Mode Button	C	1	0	May be inoperative provided approach minimums do not require its use.

9)	Bank Limiter (BANK) Button	C	1	0	May be inoperative provided approach minimums do not require its use.

10)	Heading Selector (HDG SEL) Knob	-	1	0	May be inoperative provided Autopilot is considered inoperative.

11)	Heading Synchronization (PUSH SYNC) Button	C	1	0

12)	Flight Level Change (FLC) Mode Button	C	1	0	May be inoperative provided operations do not require its use.

13)	Vertical Navigation (VNV) Mode Button				May be inoperative provided operations do not require its use.

14)	Altitude Hold (ALT) Mode Button	C	1	0	May be inoperative provided operations, including RVSM, do not require its use.

22	AUTOPILOT

11-01	Guidance Panel (GP) (Continued)

15)	Vertical Speed (VS) Mode Button	C	1	0	May be inoperative provided operations do not require its use.

16)	Vertical Speed (VS DN UP) Thumb Wheel	C	1	0	May be inoperative provided operations do not require its use.

17)	Airspeed To Mach (PUSH IAS/MACH) Change Button	C	1	0

18)	Altitude Selector (ALT SEL) Knob	-	1	0	May be inoperative provided Autopilot is considered inoperative.

19)	Speed Selector (SPD SEL) Knob	C	1	0	May be inoperative provided operations do not require its use.

11-21	AP/FD CWS Pushbutton	C	2	0	May be inoperative in the NOT ACTIVE position.

11-22	Autopilot Disconnect Functions (Quick Release Controls)	C B	2 2	1 0	One may be inoperative provided: a) Autopilot is not used below 1,500 feet AGL, and b) Approach minimums do not require the use of the Autopilot. May be inoperative provided Autopilot is not used.

11-23	Takeoff/Go-Around (TOGA) Button	C	2	1	One may be inoperative in the NOT ACTIVE position.

		C	2	0	(O) May be inoperative in the NOT ACTIVE position provided Alternate procedures are established and used.

23	COMMUNICATIONS

12-00	Very High Frequency (VHF) Communication System	D	2	1	VHF 2 may be inoperative.

51-01	Audio Panel

1)	Annunciators LEDs	D	-	-	(O) May be inoperative provided associated function is checked operative by alternate means.

2)	INTR COM Button	D	2	0	For single pilot operations, may be inoperative.

3)	PA Button	D	2	0

4)	CABIN Button	D	2	0

5)	MUSIC Button	D	2	0

6)	PLAY Button	D	2	0

7)	Display Backup Buttons	D	2	1	For single pilot operations, copilot side may be inoperative.

51-02	Cockpit Speakers	D	2	1	For single pilot operations, copilot side Speaker may be inoperative, provided pilot Headset is operative and used.

51-07	PTT Switches	D	4	2	For single pilot operations, both copilot side Switches (Glareshield and Yoke) may be inoperative.

		C	4	2	For operations requiring a second in command, one in each side may be inoperative.

23	COMMUNICATIONS

51-09	Headset With Boom Microphones	D	2	1	For single pilot operations, copilot side may be inoperative.

		C	2	0	For operations requiring a second in command, may be inoperative provided on side cockpit speaker and hand microphone are operative.

51-11	Hand Microphones	D	-	1	For single pilot operations, copilot side may be inoperative.

		C	-	0	For operations requiring a second in command, one or both may be inoperative provided associated Boom Microphone is operative.

51-00 ***	Passenger Address System (PA)

1)	Passenger Configuration	C	1	0	(O) May be inoperative provided: a) PA not required by FAR, and b) Alternate, normal and emergency procedures, and/or operating restrictions are established and used. NOTE: Any Station Functions that operate normally may be used.

23	COMMUNICATIONS

23-11 ***	High Frequency (HF) Communication System	D	-	-	Any in excess of those required by FAR may be inoperative.

		C	-	1	(O) May be inoperative while conducting operations that require two LRCS provided: a) SATCOM Voice or Data Link operates normally, b) Alternate procedures are established and used, c) SATCOM coverage is available over the intended route of flight, and d) If INMARSAT Codes are not available while using SATCOM Voice prior coordination with the appropriate ATS facility is required.

					NOTE: SATCOM is to be used only as a backup to normal HF communications unless otherwise authorized by the appropriate ATS facilities.

24	ELECTRICAL

00-00	Electrical Synoptic Display (MFD Electrical Page)	C	1	0	MFD indications not addressed elsewhere in the MMEL may be inoperative.

41-00	DC External Power System

1)	DC GPU AVAIL / IN USE Pushbutton Lights	D	2	0	(O) May be inoperative provided alternate procedures are established and used.

25	EQUIPMENT/ FURNISHINGS

00-00	Non-Essential Equipment And Furnishings		-	0	May be inoperative, damaged, or missing provided that the item(s) is deferred in accordance with the operator’s NEF deferral program. The NEF program, procedures, and processes are outlined in the operators (insert name) Manual. (M) and (O) procedures, if required, must be available to the flight crew and included in the operator’s appropriate document.

11-01	Pilot Seats	C	2	1	For single pilot operation, copilot Seat may be inoperative provided Seat is not occupied.

1)	Lumbar Support	C	2	0	May be inoperative provided Seat is acceptable to affected crewmember.

2)	Armrests	C	4	0	(M) May be inoperative provided Armrest is secured in the retracted (UP) position or removed.

3)	Recline Function	B	2	0	May be inoperative provided: a) Affected Seat has failed locked in a position that permits normal pilot visibility, b) Full flight control movement is available, and c) Seat is acceptable to the affected crewmember.

4)	Headrests	C	2	0	May be inoperative provided it is adequate to the occupant.

					(Continued)

25	EQUIPMENT/ FURNISHINGS

11-01	Pilot Seats (Continued)

5)	Seat Belts System	C	2	1	For single pilot operations, copilot Seat Belt may be inoperative provided the Seat is unoccupied.

6)	Vertical Seat Adjustment	B	2	0	May be inoperative provided: a) Affected Seat has failed locked in a position that permits normal pilot visibility, b) Full flight control movement is available, and c) Seat is acceptable to the affected crewmember.

21-01	Passenger Seats	D	-	-	May be inoperative provided: a) Seat does not block an Emergency Exit, b) Seat does not restrict any passenger from access to the main aircraft aisle, and c) Affected Seat(s) are blocked and placarded “DO NOT OCCUPY”.

					NOTE: A Seat with an inoperative Seat Belt is considered inoperative.

1)	Recline Mechanism	C	-	-	(M) May be inoperative and Seat occupied provided Seat Back is immovable in full UPRIGHT position.

					(Continued)

25	EQUIPMENT/ FURNISHINGS

21-01	Passenger Seats (Continued)

2)	Armrest	C	-	-	May be inoperative or missing and Seat occupied provided: a) Armrest does not block an Emergency Exit, and b) Armrest does not restrict any passenger from access to the Main Aircraft Aisle.

61-00	Emergency Locator Transmitter (ELT)

1)	Survival Type ELTs	D	-	-	Any in excess of those required by FAR may be inoperative or missing.

2)	Fixed ELTs	A	-	0	May be inoperative or missing provided repairs are made within 90 days.

		D	-	-	Any in excess of those required by FAR may be inoperative or missing.

25	EQUIPMENT/ FURNISHINGS

62-01	Emergency Medical Equipment

1)	First Aid Kit (FAK)	A	-	-	(O) If more than one is required by local regulation, only one of the required First Aid Kits may be incomplete, missing or inoperative provided: a) FAK is resealed in a manner that will identify it as a unit that can not be mistaken for a fully serviceable unit, and b) Repairs or replacements are made within 3 flight cycles.

		D	-	-	Any in excess of those required by local regulation may be inoperative or missing.

62-02 ***	Life Vests	D	-	-	(M) Any in excess of those required may be missing or inoperative provided: a) Inoperative Lifejacket is placarded inoperative, removed from the installed location and placed out of sight so it cannot be mistaken for a functional unit, and b) Required distribution of operative Lifejackets is maintained.

25	EQUIPMENT/ FURNISHINGS

62-05	Flashlights	C	-	1	For single pilot operations, any in excess of one may be inoperative.

					NOTE: The operative Flashlight must be accessible from pilot left Seat.

		C	-	-	For operations requiring a second in command, any in excess of those required by FAR may be inoperative.

27	FLIGHT CONTROLS

14-00	Roll Trim System	C	1	0	(O) May be inoperative provided: a) Aileron Trim Tabs are verified in NEUTRAL position before each flight, and b) Roll Trim Circuit Breaker is pulled.

1)	Roll Trim Position Indication On EIS	C	1	0	(O) May be inoperative provided Ailerons’ Trim Tabs are verified CENTERED before each flight.

24-00	Yaw Trim Position Indication On EIS	C	1	0	(O) May be inoperative provided Rudder Trim Tab is verified CENTERED before each flight.

34-01	Yoke Pitch Trim Switch	B	2	1	For single pilot operations, copilot side Switch may be inoperative.

		B	2	1	For operations requiring a second in command, either side may be inoperative.

28	FUEL

00-00	Fuel System Synoptic Display (MFD Fuel Page)	C	1	0	(O) MFD Indications not addressed elsewhere in the MMEL may be inoperative.

11-07	Fuel Dump Valves	D	2	0	(M) May be inoperative (OPEN) provided the affected Valve is checked for no leakage.

11-09	Gravity Fuel Caps	C	2	1	(O) May be inoperative (LOCKED) provided: a) If refueling is necessary, it must be done following single side refueling procedure and limited to 60% tanks capacity, and b) Fuel Quantity Indication System is operative.

41-00	Fuel Quantity Indication	B	2	1	(O) May be inoperative provided: a) Airplane is refueled to full fuel capacity before each flight, b) Fuel Used indication on MFD and both Fuel Flow indications are operative and monitored throughout the flight, and c) Both Gravity Fuel Caps operate normally.

45-01	Fuel Low Pressure Switches	B	2	1	(O) One may be inoperative provided the on side DC Pump is selected ON throughout the flight.

30	ICE & RAIN PROTECTION

00-00	Ice Protection System Synoptic Display (ICEPROT MFD Page)	C	1	0	(O) MFD Indications not addressed elsewhere in the MMEL may be inoperative.

13-00	Wing De-Icing System	C	1	0	(O)(M) May be inoperative provided: a) Airplane is not operated in known or forecast icing conditions, b) Wing Boots are verified DEFLATED before each flight, and c) System is DEACTIVATED.

15-00	Horizontal Stabilizer De-Icing System	C	1	0	(O)(M) May be inoperative provided: a) Airplane is not operated in known or forecast icing conditions, b) HS Boots are verified DEFLATED before each flight, and c) System is DEACTIVATED.

21-00	Nacelle Anti-Icing System	C	2	1	(O) May be inoperative provided: a) Airplane is not operated in known or forecast icing conditions, and b) MFD Nacelle Anti-Ice Switch remains selected OFF and Anti-Ice Valve is confirmed CLOSED.

30	ICE & RAIN PROTECTION

21-01	Nacelle Anti-Icing Valves	C	2	0	(O)(M) One or both may be inoperative provided: a) Both Valves are secured OPEN, and b) AFM anti-icing ON performance is used.

31-01	Static Ports Heaters	B	4	3	May be inoperative provided airplane is not operated in known or forecast icing conditions.

31-02	Pitot Heater	B	2	1	May be inoperative provided: a) Flight is conducted in day VFR conditions, and b) Airplane is not operated in known or forecast icing conditions.

42-00	Windshield Heater	C	4	2	For single pilot operations, both copilot side Heaters may be inoperative provided operations are not conducted in known or forecast icing conditions.

		C	4	2	For operations requiring a second in command, Heaters on one side may be inoperative provided operations are not conducted in known or forecast icing conditions.

31	INDICATING/ RECORDING SYSTEMS

22-01	Yoke Chronometer Pushbutton	D	2	1	For single pilot operations, copilot side may be inoperative.

		C	2	0	For operations requiring a second in command, both may be inoperative.

31-01	Cockpit Voice And Data Recorder

1)	Cockpit Voice Recorder (CVR) Function	D	1	0

2)	Flight Data Recorder (FDR) Function	D	1	0

41-07	Avionics Blower	C	1	0	May be inoperative provided: a) VCS is operative, and b) Cockpit Evaporator Fan is operative.

61-01	Flight Display Units (FDU)	D	3	2	(O) For single pilot operations, PFD2 may be inoperative provided PFD2 Circuit Breaker is PULLED.

					NOTE: Autopilot is inoperative with PFD2 inoperative .

		C	3	2	(O) For operations requiring a second in command, MFD may be inoperative provided: a) HSDB Switch is set to REV position, b) MFD Circuit Breakers are PULLED, and c) GPS, Weather radar, and Traffic Information are considered inoperative.

31	INDICATING/ RECORDING SYSTEMS

61-01	Flight Display Units (FDU) (Continued)

1)	Buttons And Knobs	D	-	-	For single pilot operations, any PFD2 Button or Knob may be inoperative or missing.

		C	-	-	For operations requiring a second in command, any button and/or knob may be inoperative in one FDU provided the Buttons and/or Knobs that perform the same function are operative on the other two FDUs.

61-02	Display Cooling Fans	C	3	0	May be inoperative provided: a) VCS is operative, and b) Cockpit Evaporator Fan is operative.

33	LIGHTS

10-00	Cockpit/ Flight Deck/ Flight Compartment And Instrument Lighting System	C	-	-	Individual Lights may be inoperative provided remaining Lights are: a) Sufficient to clearly illuminate all required instruments, controls, and other devices for which it is provided, b) Positioned so that direct rays are shielded from flight crewmembers eyes, and c) Lighting configuration and intensity is acceptable to the flight crew.

23-01	Passenger Notice System (Fasten Seat Belt-Return To Seat)	C	1	0	(O) May be inoperative provided appropriate verbal briefings are given to the passengers.

41-00	Landing/Taxi Lights	C	2	0	May be inoperative for day operations.

		B	2	1

43-00	Navigation/Anti-Collision Lights

1)	Navigation Lights	C	2	0	One or both may be inoperative for day operations.

2)	Anti-Collision Lights	B	2	0	May be inoperative for day operations.

33	LIGHTS

44-01	Wing Ice Lights	C	-	0	May be inoperative provided aircraft is not operated at night.

		C	-	0	May be inoperative provided: a) Aircraft is equipped with an approved Ice Detection System, and b) Ground deicing procedures do not require use of Wing Ice Lights.

		C	2	1	One may be inoperative provided: a) Left Light is operative for single pilot operations, and b) Ground deicing procedures do not require use of Wing Ice Lights.

45-01	Red Beacon	C	1	0	(O) May be inoperative provided Anti-Collision Lights are operative and turned ON before engine operation.

46-01	Logo Lights	D	-	0

34	NAVIGATION

11-01	Integrated Electronic Standby Instrument (IESI)

1)	Standby Attitude Indicator	C B	- -	0 0	May be inoperative provided not required by FAR. May be inoperative provided: a) Operations are conducted in day VMC only, and b) Operations are not conducted into known or forecast over-the-top conditions.

2)	STD Baro Button	C	1	0	May be inoperative provided BARO Knob on the IESI operates normally.

3)	Brightness Buttons	C	2	0	May be inoperative provided brightness level is acceptable to the crew.

4)	CAGE Button	B	1	0	(O) May be inoperative provided IESI is reinitialized before each flight.

		B	1	0	May be inoperative provided IESI attitude indication is considered inoperative.

21-00	Attitude And Heading Reference System (AHRS)	B	2	1	(O) One may be inoperative provided: a) Operations are conducted in day VMC only, b) Operative AHRS is selected as attitude and heading source to both PFDs, and c) RVSM operations are not conducted.

					NOTE: Autopilot is inoperative with one AHRS inoperative.

34	NAVIGATION

23-01	Non-Stabilized Magnetic Compass System	B	1	0	(O) May be inoperative provided any combination of three Gyro or INS (IRU) Stabilized Compass Systems are operative.

		B	1	0	(O) May be inoperative provided: a) Any combination of two Gyro or INS (IRU) Stabilized Compass Systems operate normally, and b) Airplane is operated with Dual Independent Navigation Capability and under Positive Radar Control by ATC on the enroute portion of the flight.

		B	1	0	(O) May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two Stabilized Directional Gyro Systems are installed, operate normally, and used in conjunction with approved Free Gyro Navigation Techniques.

32-00	VHF Navigation System

1)	VOR/ILS	C	2	-	Any in excess of those required by FAR may be inoperative.

2)	Marker Beacon	C	2	0	May be inoperative provided approach operating procedures do not require its use.

34	NAVIGATION

42-00 ***	Weather Radar System	D	-	0

51-00	Distance Measuring Equipment (DME) Systems	D	-	-	Any in excess of those required by FAR may be inoperative.

52-00	ATC Transponders And Automatic Altitude Reporting Systems	B D	- -	0 1	May be inoperative provided: a) Operations, including RVSM, do not require its use, and b) Prior to flight, approval is obtained from ATC facilities having jurisdiction over the planned route of flight. Any in excess of those required by FAR may be inoperative.

56-00	Global Positioning System (GPS)	C	2	1	One may be inoperative provided operations do not require its use.

57-00	Satellite Weather/Radio System	D	1	0

34	NAVIGATION

61-00	Flight Management System

1)	Navigation Databases	C	-	-	(O) May be out of currency provided: a) Current Aeronautical Charts are used to verify Navigation Fixes prior to dispatch, b) Procedures are established and used to verify status and suitability of Navigation Facilities used to define route of flight, and a) Approach Navigation Radios are manually tuned and identified.

61-01	Flight Management System (FMS) Panel	D	1	0	(O) May be inoperative provided alternate procedures are established and used.

34	NAVIGATION

43-00 ***	Traffic Alert And Collision Avoidance System (TCAS I)	B	-	0	(M) May be inoperative provided: a) System is deactivated and SECURED, and b) Enroute or approach procedures do not require its use.

		C	-	0	(M) May be inoperative provided: a) Not required by FAR, b) System is deactivated and SECURED, and c) Enroute or approach procedures do not require its use.

43-00 ***	Traffic Alert And Collision Avoidance System (TCAS II)	B	-	0	(M) May be inoperative provided: a) System is deactivated and secured, and b) Enroute or approach procedures do not require its use.

		C	-	0	(M) May be inoperative provided: a) Not required by FAR, b) System is deactivated and secured, and c) Enroute or approach procedures do not require its use.

					(Continued)

34	NAVIGATION

43-00	Traffic Alert And Collision Avoidance System (TCAS II) (Continued)

1)	Combined Traffic Alert (TA) And Resolution Advisory (RA) Dual Display System(s)	C	2	1	May be inoperative on the non-flying pilot side provided: a) TA and RA Visual Display is operative on the flying pilot side, and b) TA and RA Audio Function is operative on the flying pilot side.

2)	Resolution Advisory (RA) Display System(s)	C	2	1	May be inoperative on non-flying pilot side.

		C	-	0	(O) May be inoperative provided: a) Traffic Alert (TA) Visual Display and Audio Functions are operative, b) TA ONLY Mode is selected by the crew, and a) Enroute or approach procedures do not require its use.

3)	Traffic Alert (TA) Display System(s)	C	-	0	(O) May be inoperative provided: a) RA Visual Display and Audio Functions are operative, and b) Enroute or approach procedures do not require its use.

4)	Audio Functions	B	1	0	May be inoperative provided enroute or approach procedures do not require use of TCAS.

5) ***	Airspace Selection Function	C	-	0

35	OXYGEN

01-01	Cylinder Pressure Gauge	C	1	0	(M) May be inoperative provided: a) Gauge is inspected for no leakage, and b) Alternate procedures to measure the Oxygen Cylinder pressure for servicing must be established.

01-02	Pressure And Temperature Transducer	B	1	0	(O) May be inoperative provided: a) Cylinder Pressure Gauge is operative, and b) Oxygen pressure is checked in Cylinder before each flight.

02-02	Cylinder Fill Port	C	1	0	(M) May be inoperative provided: a) Valve is inspected for no leakage, and b) If Oxygen Cylinder refilling is necessary, it must be done outside airplane or cylinder replaced for a fully charged one.

11-02	Crew Oxygen Mask	C	2	1	For single pilot operations, copilot mask may be inoperative (no flow) provided the copilot Seat is not occupied.

21-00	Passenger Oxygen System	C	1	0	May be inoperative provided the airplane is operated with no passengers.

		C	1	0	(O) May be inoperative provided flight is conducted unpressurized at or below 10,000 feet MSL.

35	OXYGEN

21-00	Passenger Oxygen System (Continued)

1)	Passenger Auto Deployment Function	C	1	0	(M)(O) May be inoperative provided: a) Flight is conducted at or below 30,000 feet MSL, b) Manual deployment function is verified operative once each flight day, and c) Both Air Bleed Sources operate normally.

21-01	Passenger Oxygen Masks	C	-	0	(M) May be inoperative provided affected Seat is placarded and BLOCKED to prevent occupancy.

38	WATER/ WASTE

30-00	Lavatory Waste Systems (Including Wheelchair Accessible Lavatories)	C	-	-	(M) Individual Components may be inoperative provided: a) Associated Components are deactivated or isolated, and b) Associated System Components are verified not to have leaks.

					NOTE: Any portion of the System which operates normally may be used.

		C	-	-	(M) Associated Lavatory System(s) may be inoperative provided: a) Associated Components are deactivated or isolated to prevent leaks, b) The Pilot-in-Command will determine if flight duration is acceptable with a Lavatory unusable, and c) Associated Lavatory Door(s) is secured CLOSED and placarded, “INOPERATIVE – DO NOT ENTER”.

					NOTE: These provisions are not intended to prohibit inspections by crewmembers.

46	INFORMATION SYSTEMS

21-00 ***	Electronic Flight Bag Systems (EFBs)

1) ***	Class 3 EFBs	C	-	-	(O) May be inoperative provided alternate procedures are established and used.

					NOTE: Any function, program or document which operates normally may be used.

		D	-	0	May be inoperative provided procedures do not require its use.

2) ***	Data Connectivity (Class 2)	C	-	-	(O) May be inoperative provided alternate procedures are established and used.

		D	-	0	May be inoperative provided procedures do not require its use.

3) ***	Power Connection (Class 1 & 2)	C	-	-	(O) May be inoperative provided alternate procedures are established and used.

		D	-	0	May be inoperative provided procedures do not require its use.

4) ***	Mounting Device (Class 2)	C	-	0	(M)(O) May be inoperative provided: a) The associated EFB and hardware is secured by an alternate means or removed from the aircraft, and b) Alternate procedures are established and used.

					(Continued)

52	DOORS

70-00	Doors Warning System (CAS Indication)

1)	Passenger Door Warning System (CAS Indication)	C	1	0	(O) May be inoperative provided, before each flight: a) Door is verified closed and LATCHED, b) The 8 Latches Visual Indicators are checked and confirmed CLOSED, and c) The 2 Lock Indicator Flags are checked and confirmed CLOSED.

2)	Forward Baggage Door Warning System (CAS Indication)	C	1	0	(O) May be inoperative provided, before each flight: a) Affected Door is verified closed and LATCHED, and b) Locking Latches are inspected for correct engagement.

3)	Aft Baggage Door Warning System (CAS Indication)	C	1	0	(O) May be inoperative provided, before each flight: a) Affected Door is verified closed and LATCHED, and b) Locking Latches are inspected for correct engagement.

4)	Emergency Door Warning System (CAS Indication)	C	1	0	(O) May be inoperative provided the Door is verified closed and Latched before each flight.

73	ENGINE FUEL AND CONTROL

21-01	Full Authority Digital Electronic Control (FADEC)

1)	System Faults	A	2	0	May be dispatched with System Faults provided repairs are made in accordance with times established by engine manufacturer. No extensions are authorized.

					NOTE: The intent of the 0 in the number required for dispatch column is to show that dispatch is allowed with some faults present in both FADEC’s.

33-00	Fuel Flow Indication	B	2	1	(O) May be inoperative provided: a) Both Wings Fuel Quantity Indications on EIS are operative, and b) Used fuel information on Synoptic Fuel Page and remaining fuel information on FMS are not used by flight crew.