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A-318, A-319, A-320, A-321
REVISION NO:21
DATE: 06/17/2009
PAGE:
32-6
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
32
LANDING GEAR
42-04
AUTO/BRK Function
C
1
0
(O) May be inoperative provided:
a)
Approach minimums do not require its use, and
b)
Normal braking is not affected.
1)
AUTO/BRK Panel Mode Lights (LO, MED, MAX)
a)
ON
C
3
0
May be inoperative provided Auto Brake Indications on ECAM WHEEL page normally.
C
3
0
May be inoperative provided associated Autobrake Mode is not used.
b)
DECEL
C
3
0
May be inoperative provided Auto
Brake indications on ECAM WHEEL
page operate normally.
C
3
0
May be inoperative provided
associated autobrake Mode is
not used.
42-05
Tachometer
Deleted, REV 20.
42-06
Nose Wheel Brake Pads (Without Mod. 28482)
C
2
0
(M) May be inoperative provided brake pads are removed.
44-01
Yellow Brake System
C
1
1
(M) Braking on one wheel may be inoperative provided:
a)
Yellow hydraulic supply of affected brake is deactivated, and
b)
Both reversers operate normally.
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:
32-7
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
32
LANDING GEAR
44-02
ACCU PRESS Indicator
(Without Mod. 31441)
C
1
0
(M) May be inoperative provided:
a)
Both brake pressure indicators operate normally, and
b)
Pressure on both brake pressure indicators is verified with parking brake on.
(With Mod. 31441)
C
1
0
(M) May be inoperative provided:
a)
Both brake pressure indicators operate normally, and
b)
Pressure on both brake pressure indicators is verified with parking brake on.
C
1
0
(O) May be inoperative provided:
a)
ACCU PRESS/ACCU ONLY indication is available on ECAM WHEEL page, and
b)
Hydraulic pressure of the brake accumulator is checked on ECAM WHEEL page before each flight.
44-03
BRAKES Pressure Indicators
C
2
1
(O) One may be inoperative provided both BSCU channels/systems operate normally.
45-02
Parking Brake External Light
C
1
0
May be inoperative provided parking brake status is verified before moving aircraft.
47-01
Brake Temperature Monitoring Unit
C
2
0
(O) May be inoperative provided brake ground cooling time is applied.
48-01 ***
Brake Fan System
D
1
0
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:
32-8
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
32
LANDING GEAR
48-02 ***
BRAKE FAN HOT Light
D
1
0
49-01 ***
ECAM Tire Pressure Indications
D
6
0
49-02 ***
Tire Pressure Monitoring System
D
1
0
(M) May be inoperative on one or more wheels provided the tire pressure on affected wheel(s) is checked every three days.
51-01
Nose Wheel Steering System
Deleted, REV 20.
51-02
PEDALS DISC p.b
C
2
0
(O) May be inoperative in the released position (No disconnection possible and NWS still available by rudder pedals).
51-03
Nose Wheel Steering Control System Deactivation Device (for A/C Towing)
C
1
0
(O) May be inoperative (no towing Mode when lever in TOWING position).
C
1
0
(M)(O) May be inoperative provided the NWS electrical deactivation box is deactivated.
60-01
LDG Gear Indicator Panel (UNLK and/or Down & Locked Triangle Indications)
B
1
0
(O) May be inoperative provided:
a)
Both landing gear position indications (on ECAM wheel page) for all three landing gear operate normally, and
b)
Upper and lower ECAM display units operate normally.
U.S. DEPARTMENT OF TRANSPORTATION
　
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本文鏈接地址：Airbus A318/A319/A320/A321 Master Minimum Equipment List(65)