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3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
75
BLEED AIR
21-01
HP Turbine Active Clearance Control System (CFM Engines Only)
1)
HPTC Valves
Incorporated into 73-20-01.
2)
Feedback Systems
Incorporated into 73-20-01
.
3)
HPTC Torque Motor Wraps
Incorporated into 73-20-01.
4)
HPTC Thermocouples
Incorporated into 73-20-01.
21-02
Active Clearance Controls Actuators (V2500 Engines Only)
Incorporated into 73-20-01.
22-01
LP Turbine Active Clearance Control (CFM Engines Only)
1)
LPTC Valves
Incorporated into 73-20-01.
2)
Feedback Systems
Incorporated into 73-20-01.
3)
LPTC Torque Motors
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:
75-2
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
75
BLEED AIR
23-01
Rotor Active Clearance Control (CFM Engines Only)
1)
RACC Valves
Incorporated into 73-20-01.
2)
Feedback Systems
Incorporated into 73-20-01.
3)
RACC Torque Motors
Incorporated into 73-20-01.
24-01
TCC Valve (PW engines only)
B
2
1
(O) One may be inoperative in closed position provided the affected engine takeoff EGT margin is greater than 18 degrees C.
||||
25-01
TCA Valve (PW engines only)
C
4
3
(M) One may be failed closed provided TCA pipes are verified to have no cracks.
30-01
Compressor Control System
1)
VSV (V2500 Engines only)
Incorporated into 73-20-01.
2)
VSV (CFM Engines Only)
a)
Torque Motors
Incorporated into 73-20-01.
b)
Feedback System
Incorporated into 73-20-01.
30-02
Compressor Control System VBV (CFM Engines Only)
1)
Feedback Systems
Incorporated into 73-20-01.
2)
Torque Motors
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: 10
DATE: 12/07/1998
PAGE:
77-1
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
77
ENGINE INDICATING
00-01
ECAM Indications (Upper Display)
1)
Fuel Flow
B
2
1
00-02
ECAM Indications (Lower Display)
1)
Nacelle Temperature
C
2
0
2)
N1 Vibration
C
2
1
3)
N2 Vibration
C
2
1
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:
78-1
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
78
ENGINE EXHAUST
11-09
T/R Door Tertiary Lock (PW Engines Only)
C
8
4
One or more may be failed locked provided the associated T/R is considered inoperative.
11-10
T/R Tertiary Lock Valve (PW Engines Only)
C
2
0
One or both may be failed open.
30-01
Thrust Reverser Systems
C
2
1
(M)(O) One may be inoperative provided:
a)
Inoperative reverser is deactivated and secured in the stowed position, and no operations or procedures require its use,
b)
All stow and deploy switches on the inoperative reverser operate normally (CFM only),
c)
Both LVDT on the inoperative reverser are checked operative (IAE only),
d)
ENG 1 (2) REV INHIBITED caution is displayed on ECAM E/WD after deactivation (PW only),
e)
ENG 1 (2) REV UNLOCKED caution is not present on ECAM E/WD after deactivation (PW only)
f)
ENG 1 (2) REV PRESSURIZED caution is not present on ECAM E/WD after deactivation,
g)
Wheel brake tachometers operate normally,
h)
Main wheel braking system operates normally,
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
A-318, A-319, A-320, A-321
REVISION NO: 20
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Airbus A318/A319/A320/A321 Master Minimum Equipment List(87)
