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reverse thrust”, and
j) Appropriate performance
adjustments are applied.
30-02 Thrust Reverser
Inhibition Relay
Contacts (CFM)
(Thrust Reverser
Permission Switches
(V2500))
C 4 2 (M) Two contacts may be inoperative
provided they are on the same engine
and the associated reverser is
deactivated.
30-03 T/R Directional Valve
Solenoid Wraps (CFM
Engines Only)
Incorporated into 73-20-01.
30-04 T/R Pressure Switches
(CFM Engines Only)
Incorporated into 73-20-01.
30-05 T/R Stow Switches
(CFM Engines Only)
Incorporated into 73-20-01.
30-06 T/R Deploy Switches
(CFM Engines Only)
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: 20
DATE: 03/19/2008
PAGE:
78-3
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
78 ENGINE EXHAUST
30-07 T/R INDICATIONS
(IAE, CFM, and PW
Engines)
C 2 1 One may be inoperative provided the
associated T/R is considered
inoperative.
30-08 Thrust Reverser Stow
& Lock Sensors
(V2500 Engines Only)
Incorporated into 73-20-01.
30-09 T/R Pressurizing Valve
Solenoid Wraps (CFM
Engines Only)
Incorporated into 73-20-01.
(Formerly 30-02), REV 10.
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:
79-1
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
79 ENGINE OIL
20-01 Air Exchanger Air
Valves (V2500
Engines Only)
C 2 1 (O) One may be inoperative open
provided the tank fuel temperature is
above -20 degrees C at takeoff.
|
20-02
***
EMCD Visual Pop-Out
Indicator (CFM-5B)
D 2 0
20-03 Air Oil Cooler Valve
(PW Engines Only)
C 2 1 (O) One may be inoperative in the open
position provided:
a) The associated IDG operates
normally,
b) The inner tank fuel temperature
on the affected side is checked
above -20 degrees C before
each flight, and
c) Appropriate performance
adjustments are applied.
|||||||||
|
C 2 1 (O) One may be inoperative in the open
position provided:
a) The inner tank fuel temperature
on the affected side is checked
above -10 degrees C before
each flight, and
b) Appropriate performance
adjustments are applied.
|||||||
|
23-01 Bearing 4 Oil System
(IAE Engines Without
Mod. 24871)
A 2 0 (M) May be inoperative provided:
a) HI PRESS message is not
displayed under ENG 1 (2)
BEARING 4 OIL SYS caution on
ECAM E/WD,
b) Scavenge valve is verified to be
in open position, and
c) Repairs are made within three
flight days.
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:
79-2
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
(IAE Engines With
Mod. 24871)
A 2 0 May be inoperative provided:
a) HI PRESS message is not
displayed under ENG 1 (2)
BEARING 4 OIL SYS caution on
ECAM E/WD, and
b) Repairs are made within three
flight days.
31-01 Oil Quantity Indications B 2 1 (M) One may be inoperative provided:
a) Associated oil quantity is
verified before each
departure,
b) There is no evidence of
abnormal consumption or
leakage, and
c) Associated ENG OIL
PRESS, OIL TEMP
indications operate normally.
33-02 OIL LO PR Warning on
ECAM (IAE or CFM
Engines only)
C 2 1
|
|
C 2 0 May be inoperative provided RCDR
GND CTL is verified ON after engines
are started.
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:
79-3
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
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