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NUMBERS
1.
4. REMARKS AND EXCEPTIONS
31 INDICATING/
RECORDING
SYSTEMS
63-02 Display Management
Computers
(without Mod. 21678) C 3 2 DMC 3 may be inoperative.
C 3 2 (M)(O) DMC 2 may be inoperative
provided:
a) AC ESS Feed Control is verified
operative once each flight day,
and
b) AC ESS Feed Fault Light is
verified operative once each flight
day.
(with Mod. 21678) C 3 2 DCM 1 or DMC 3 may be inoperative.
C 3 2 (M)(O) DMC 2 may be inoperative
provided:
a) AC ESS Feed Control is verified
operative once each flight day,
and
b) AC ESS Feed Fault Light is
verified operative once each flight
day.
63-03 ECAM Memo Display C - 0 Indications may be inoperative.
63-04 ECAM Permanent Data
Display
C - 0 Indications may be inoperative provided
TAT or SAT temperature is available.
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:
32-1
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
32-00 CLASS II MAINTENACE
MESSAGE DISPLAYED
ON ECAM STATUS
PAGE OF ECAM
SYSTEM DISPLAY
1) Fault(s) Indicated by
BRAKES
Deleted, REV 21. |
|
11-01
***
Torque Link Dampers A 2 0 May be inoperative provided repairs are
made within seven flight legs.
|
12-01 MAIN GEAR DOORS
1) Ground Opening Cables
C 2 0 (M) May be broken or missing.
31-00 Landing Gear Retraction
System
B 1 0 (O) Except for ER operations, may be
inoperative provided the airplane is
operated with landing gear down in
accordance with the AFM supplement for
gear down flight.
31-01 Landing Gear Control
And Interface Units
(LGCIU)
A 2 1 (M)(O) LGCIU No. 2 may be inoperative
provided:
a) Both radio altimeter systems
operate normally,
b) Both FCU channels operate
normally,
c) All ELACs, SECs, ADIRs, SFCCs
and FACs operate normally,
d) Both thrust lever position sensors
of engine No. 2 are operative,
e) Flex takeoff is not used,
f) Reverser No. 2 is considered
inoperative, and
g) Repairs are made within one
flight day.
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:
32-2
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
33-01 Landing Gear Gravity
Extension System
B 1 0 (O) Except for ER operations, may be
inoperative provided the airplane is
operated with landing gear down in
accordance with the AFM supplement for
gear down flight.
41-01 Wheel Tie Bolts A - - (M) One bolt may be broken or missing
provided:
a) Affected wheel is removed,
checked for broken parts or
damage, and replaced if broken
parts or damage is found,
b) Associated brake is checked for
broken parts or damage, and is
replaced or deactivated if broken
parts or damage is found,
c) After each landing, wheel is
inspected for additional broken or
missing tie bolts, and
d) Repairs are made within five
flight legs.
||
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:
32-3
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
42-01 Main Wheel Braking
Systems
C 4 3 (M)(O) One brake may be inoperative
provided:
a) Minimum runway width is 148
feet (45 meters),
b) Anti-skid system operates
normally,
c) Nose wheel steering operates
normally,
d) Affected brake is removed or
deactivated,
e) Both reversers operate normally,
f) Green and yellow systems on
operative brakes operate
normally,
g) Wheel tachometers are
operative,
h) AFM performance penalties are
applied, and
i) Approach minimums do not
require its use.
|
42-02 Green Braking System
(Without Mod. 25410)
C 1 1 (M)(O) Braking on one wheel may be
　
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