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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 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
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Airbus A318/A319/A320/A321 Master Minimum Equipment List(88)
