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SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
30-01 Elevator Indications on
ECAM Flight Control
Page
1) ECAM Elevator Position
Indications
C 2 0 May be inoperative provided a visual
verification of affected elevator
movement is made before each
departure.
|
2) ECAM Elevator Actuator
Indications
C 4 0
30-02 ECAM Elevator Actuator
Indications
Incorporated into 27-30-01. |
|
34-02 Elevator Servo Control
Position Transducers
C 8 4 (M) One per servo control must operate
normally.
40-01 ECAM Pitch Trim
Position Indication
C 1 0 (M)(O) May be inoperative provided a
check of pitch trim handwheel and
stabilizer verifies synchronous
movement.
44-01 Stabilizer Actuator
Electrical Motors
C 3 2 Motor 3 may be inoperative.
B 3 2 (M) Except for ER operations, motor 2
may be inoperative provided ELAC 1 is
considered inoperative.
||
|
44-02 Pitch Trim Hydraulic
System Pressure
Indication Symbol on
ECAM F/CTL Page
C 2 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:
27-7
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
51-01 Slat/Flap Control
System (SFCS)
1) FLAP Channels B 2 1 (M)(O) SFCS 2 flap channel may be
inoperative provided:
a) Slats and flaps operate
normally on SFCC 1,
b) Operation of SFCC 1 WTBs are
confirmed by tests before each
departure,
c) Electrical supply to SFCC 2 flap
channel is inhibited,
d) ELAC, SEC, ADIRS, LGCIU,
FAC, and RA systems operate
normally,
e) Spoilers surfaces 2 and 4
operate normally, and
f) The minimum idle on ground
function is considered
inoperative.
2) SLAT Channel B 2 1 (M)(O) SFCS 2 slat channel may be
inoperative provided:
a) Slats and flaps 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:
27-8
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
51-02 Flap Wing Tip Brake
Solenoids
C 4 2 (M) Solenoids associated with SFCC 2
may be inoperative provided operation
of SFCC 1 WTBs is confirmed by test
before each flight.
51-03 Flap Attachment Failure
Detection Sensors
Incorporated into 27-00, sub item 2).
54-01 Flap Hydraulic Motors
C 2 1 Green motor may be inoperative.
C 2 1 Yellow motor may be inoperative
provided blue slat motor operates
normally.
54-02 Flap PCU Valve Blocks B 2 1 (M)(O) SFCS 2 Flap PCU Valve Block
may be inoperative provided:
a) Slats and flaps operate
normally on SFCC 1,
b) Operation of SFCC 1 WTBs are
confirmed by tests before each
departure,
c) Electrical supply to SFCC 2 flap
channel is inhibited,
d) ELAC, SEC, ADIRS, LGCIU,
FAC, and RA systems operate
normally,
e) Spoilers, surfaces 2 and 4
operate normally, and
f) The minimum idle on ground
function is considered
inoperative.
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:
27-9
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
64-01 Spoiler Surfaces
(A320 without Mod.
26334 or 26335)
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, and
b) AFM performance penalties are
applied.
C 10 8 (M)(O) One pair of symmetrical
surfaces 5 may be inoperative in the
　
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