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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
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Airbus A318/A319/A320/A321 Master Minimum Equipment List(65)
