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52 DOORS
30-04 Cargo Door Opening
Electrical Control
System
C 1 0 (O) May be inoperative provided
procedures are established and used
to ensure the compartments remain
empty, or are verified to contain only
empty cargo handling equipment,
ballast, (ballast may be loaded in
ULDs), and/or Fly Away Kits.
||||||
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NOTE: Operator MELs must define
which items are approved for
inclusion in the Fly Away Kits,
and which materials can be
used as ballast.
||||
|
C 1 0 May be inoperative provided:
a) Hand pump operates normally,
and
b) Cargo door is fully open during
loading and unloading
1) Open and Locked
(Green) Lights
C 2 0 May be inoperative and associated
cargo compartment used, provided
cargo door is fully open during loading
and unloading.
33-01
***
Bulk Cargo Door
Balance mechanism
C 1 0 (M) May be inoperative or damaged
provided:
a) A safety hold device is used to
maintain the door in the open
position, and
b) A visual check is made to
confirm that the door is correctly
closed and locked after each
use.
50-01 Flight Deck Door Lock
Solenoid
C 1 0 (M) May be inoperative provided:
a) Door can be locked and
unlocked manually, and
b) Latch shearing function is not
impaired.
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:
52-4
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
52 DOORS
50-02 Cockpit Door Locking
System (Automatic
System) (Mod. 32088
and 32090) FAR 25.795
compliant
A 1 0 (M)(O) May be inoperative provided:
a) Automatic locking system is
deactivated,
b) Door dead bolt operates
normally and is used to lock the
door,
c) Alternate procedures are
established and used for locking
and unlocking the door using the
deadbolt, and
d) Repairs are made within two
flight days.
1) Cockpit Door Toggle
Switch
a) UNLOCK Function C 1 0 (O) May be inoperative provided
alternate procedures are established
and used.
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b) LOCK Function C 1 0 (M)(O) May be inoperative provided:
a) The cockpit door locking system
keypad is deactivated, and
b) Alternate procedures are
established and used.
||||
|
2) OPEN Light C 1 0
|
(Continued)
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:
52-5
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
52 DOORS
50-02 Cockpit Door Locking
System (Automatic
System) (Mod. 32088
and 32090) FAR 25.795
compliant (Continued)
3) FAULT Light C 1 0 (O) May be inoperative provided all
LEDs on CKPT DOOR CONT Panel are
operative.
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|
4) Buzzer C 1 0 (M)(O) May be inoperative provided:
a) Keypad is deactivated, and
b) Alternate procedures are
established and used.
5) Keypad C 1 0 (M)(O) May be inoperative provided:
a) Keypad is deactivated, and
b) Alternate procedures are
established and used.
a) Green and Red LEDs C 2 0 (O) May be inoperative provided
Alternate procedures are established
and used.
6) Pressure Rate Sensors C 2 1
A 2 0 May be inoperative provided repairs are
made within two flight days.
||
(Continued)
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:
52-6
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
52 DOORS
50-02 Cockpit Door Locking
System (Automatic
System) (Mod. 32088
and 32090) FAR 25.795
compliant (Continued)
7) Door Release Strikes
(Catch Spring, Solenoid,
Bolt)
C 3 2 (M) One may be inoperative provided
associated door release strike is
deactivated or removed.
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|
8) Control Unit LED’s C 5 0 (O) May be inoperative provided
associated FAULT light is verified to
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