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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
DATE: 03/19/2008
PAGE:
78-2
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
78 ENGINE EXHAUST
30-01 Thrust Reverser
Systems (Continued)
C 2 1 i) Flight crew is provided with the
following statement via
appropriate means (e.g.
dispatch release, MEL (O)
procedure, etc.):
“For a landing conducted with
one deactivated thrust reverser,
ensure that both engine thrust
levers are retarded to the IDLE
detent for the flare and the
touchdown. Select both thrust
levers to reverse when applying
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