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C
10
8
(M)(O) One pair of symmetrical surfaces 1 or 3 may be inoperative in the retracted position provided:
a)
SECs associated with operative spoilers operate normally,
b)
AFM performance penalties are applied.
C
10
8
(M)(O) One pair of symmetrical surfaces 5 may be inoperative in the retracted position provided SECs associated with operative spoilers operate normally.
(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:
27-11
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27
FLIGHT CONTROLS
64-01
Spoiler Surfaces (Continued)
(A318/A319/A321 and A320 with Mod. 26334 or 26335) (Continued)
C
10
8
(M)(O) One pair of symmetrical surfaces 2 or 4 may be inoperative in the retracted position provided:
a)
SECs associated with operative spoilers operate normally,
b)
SFCS 2 flap channel operates normally, and
c)
AFM performance penalties are applied.
C
10
6
(M)(O) Two pair of symmetrical surfaces 1 and 2 may be inoperative in the retracted position provided:
a)
SECs associated with operative spoilers operate normally,
b)
SFCS 2 flap channel operates normally, and
c)
AFM performance penalties are applied.
C
10
6
(M)(O) Two pair of symmetrical surfaces 3 and 4 may be inoperative in the retracted position provided:
a)
SECs associated with operative spoilers operate normally,
b)
TR 1 and TR 2 are operate normally,
c)
DC Tie Contactor 1 is verified closed before departure,
d)
SFCS 2 flap channel operates normally, and
e)
AFM performance penalties are applied.
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:
27-12
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27
FLIGHT CONTROLS
64-02
Load Alleviation Function (LAF) (A320-200 without Mod. 26334 or 26335)
D
1
0
64-03
LAF Accumulators (A320-200 without Mod. 26334 or 26335)
D
4
0
64-04
Spoilers Hydraulic System Pressure Indication Symbol on F/CTL Page
C
3
0
81-01
Slat Wing Tip Brakes Solenoids
C
4
2
(M) Solenoids associated with SFCC 2 may be inoperative provided SFCC 1 WTBs operate normally before each flight.
84-01
Slats Hydraulic Motors
C
2
1
84-02
Slat PCU Valve Blocks
B
2
1
(M)(O) SFCS 2 Slat PCU Valve Block may be inoperative provided:
a)
Slats, Flaps, and associated monitoring and protection systems operate normally on SFCC 1,
b)
Operation of SFCC 1 WTBs are confirmed by tests before each departure,
c)
Electrical supply to SFCC 2 slat channel is inhibited,
d)
ELAC, SEC, ADIRS, LGCIU, FAC and RA systems operate normally, and
e)
Takeoff in CONF 1+F is prohibited.
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:
27-13
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27
FLIGHT CONTROLS
92-01
Speed Brake Control System
C
1
0
(O) May be inoperative provided AFM performance penalties associated with all ground spoilers inoperative are applied.
1)
Speed Brake 2 or 3 and 4
C
-
-
(O) May be inoperative provided AFM performance penalties associated with one pair or two pairs of ground spoilers inoperative are applied.
|
92-02
Ground Spoiler Control System
A
1
0
(M)(O) May be inoperative provided:
a)
A check of the thrust reverser system is performed before each flight to ensure that both thrust reversers operate normally,
b)
Autobrake function is not used,
c)
Approach minimums do not require its use,
d)
AFM takeoff and landing performance penalties are applied, and
e)
Repairs are made within three flight legs.
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