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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
A-318, A-319, A-320, A-321
REVISION NO:21
DATE: 06/17/2009
PAGE:
56-1
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
56
WINDOWS
11-01
Front Windshields
Deleted, REV 21.
|
NOTE: Refer to Aircraft Maintenance (AMM), Structural Repair Manual (SRM), or Aircraft Flight Manual.
| | | |
11-02
Fixed Lateral Windows
Deleted, REV 21.
|
NOTE: Refer to Aircraft Maintenance (AMM), Structural Repair Manual (SRM), or Aircraft Flight Manual.
.
| | | |
12-01
Sliding Windows
Deleted, REV 21.
|
NOTE: Refer to Aircraft Maintenance (AMM), Structural Repair Manual (SRM), or Aircraft Flight Manual.
|
|
|
|
21-01
Cabin Windows
Deleted, REV 21.
|
NOTE: Refer to Aircraft Maintenance (AMM), Structural Repair Manual (SRM), or Aircraft Flight Manual.
| | | |
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
A-318, A-319, A-320, A-321
REVISION NO: 20
DATE: 03/19/2008
PAGE:
71-1
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
71
POWERPLANT
71-00
CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY
1)
Fault (s) Indicated by ENG (1and/or 2) FADEC
A
2
-
May be inoperative for 10 calendar days.
|
|
2)
Fault (s) indicated by ENG (1 and/or 2) EIU
C
2
-
|
|
|
3)
Fault (s) Indicated by EVMU
C
2
-
|
NOTE: Dispatch with any of the above maintenance status messages displayed on ECAM is permitted without CFDS interrogation.
4)
Fault(s) Indicated by ENG (1 AND 2) EIU
(Aircraft Without Mod. 22327)
Deleted, REV 21
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
A-318, A-319, A-320, A-321
REVISION NO: 21
DATE: 06/17/2009
PAGE:
73-1
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
73
ENGINE FUEL & CONTROL
10-01
Fuel Switches (V2500 Engines Only)
Incorporated into 71-00.
10-02
Fuel Return-to-Tank Valves (V2500 engines Only)
Incorporated into 71-00.
11-01
Fuel Recirculation system (CFM 56-5B Engines Only)
|
1)
Valves
C
2
0
2)
Solenoids
Incorporated into 73-20-01.
3)
Oil Temperature Sensors
Incorporated into 73-20-01.
11-02
Burner Staging valve System (CFM Engines Only).
1)
Valves (Without Mod. 25887, 26338, 26577, 27725, or 28307)
C
2
0
(M) May be inoperative open.
2)
Valves (With Mod. 25887, 26338, 26577, 27725, or 28307)
Incorporated into 73-20-01.
3)
Solenoid Wraps
Incorporated into 73-20-01.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
A-318, A-319, A-320, A-321
REVISION NO: 21
DATE: 06/17/2009
PAGE:
73-2
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
73
ENGINE FUEL & CONTROL
11-03
Fuel Metering Valve System
1)
Feedback System
Incorporated into 73-20-01
20-01
Engine FADEC System
Incorporated into 71-00 sub item 1).
20-02
RESERVED
DELETED, Revision 1.
20-03
Minimum Idle on Ground
C
2
0
(O) May be inoperative provided alternate procedures are established and used.
NOTE: Continuous ignition is permanently ON. (IAE Engines only)
20-04
EPR Control Modes (IAE Engines Only)
C
2
0
(O) May be inoperative provided:
a)
N1 rated control Mode operates normally on both engines,
b)
Approach minimums do not require their use, and
c)
AFM performance penalties are applied.
NOTE: Autothrust and alpha floor are inoperative.
20-05
Flex Temp Function
C
2
0
May be inoperative provided takeoff is performed in TOGA or de-rated Mode.
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Airbus A318/A319/A320/A321 Master Minimum Equipment List(85)
