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2)
ECAM Aileron Actuator Indications
C
4
0
14-03
ECAM Aileron Actuator Indications
Incorporated into 27-14-02.
20-01
ECAM Rudder Position Indication
B
1
0
(O) May be inoperative provided:
a)
A visual verification of rudder movement is made before each departure, and
b)
RUD TRIM indication is verified at zero before each departure.
20-02
Rudder Hydraulic System Pressure Indication Symbol on ECAM F/CTL Page
C
3
0
21-01
Rudder Pedal Adjustment System
C
2
0
(O) CAPT and/or F/O may be inoperative provided:
a) Associated rudder pedals can be adjusted to a position which is acceptable to the affected crewmember, and
b) Full and unrestricted movement of rudder pedals and brake pedal deflection is possible
at both pilot stations.
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:
27-5
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27
FLIGHT CONTROLS
22-01
Rudder Trim Systems
1)
System No. 1
C
1
0
(O) Except for ER operations may be inoperative provided:
a)
Approach minimums do not require its use, and
b)
System 2 is verified to operate normally before each departure.
|
2)
System No. 2
C
1
0
(O) May be inoperative provided:
a)
Approach minimums do not require its use, and
b)
System 1 is verified to operate normally before each departure.
22-02
Rudder Manual Trim Reset Function
C
1
0
May be inoperative provided one rudder position indication is available.
22-03
Rudder Trim Position Indications
C
2
1
One indicator on ECAM or pedestal may be inoperative.
B
2
0
(O) May be inoperative provided:
a)
Rudder trim is verified to operate normally,
b)
Rudder position is verified at zero before each departure, and
c)
Rudder pedals are verified in a neutral position.
23-01
Rudder Travel Limiter Systems
C
2
1
23-02
ECAM Rudder Travel Limiter Position Indication (Aircraft with Mod. 31040 and Mod. 30368)
C
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:
27-6
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
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,
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Airbus A318/A319/A320/A321 Master Minimum Equipment List(41)
