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FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
A-318, A-319, A-320, A-321
REVISION NO:21
DATE: 06/17/2009
PAGE:
27-3
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
14-01 Aileron Servo Controls
(Continued)
(A318/A319/A321 and
A320 with Mod. 26334
or 26335)
A 4 2 (M) Two associated with ELAC 2 (left
green and right blue) may be
inoperative provided:
a) Servos remain mechanically
connected and hydraulically
supplied (damping function is
not affected),
b) All roll spoilers operate
normally,
c) Aileron Servo Controls
associated with ELAC 1
operates normally, and
d) Repairs are made within three
flight days.
A 4 2 (M)(O) Two associated with ELAC 1
(left blue and right green) may be
inoperative provided:
a) Servos remain mechanically
connected and hydraulically
supplied (damping function is
not affected),
b) All roll spoilers operate
normally,
c) Aileron Servo Controls
associated with ELAC 2
operate normally,
d) TR 1 and TR 2 operate
normally,
e) DC TIE contactor 1 is verified
closed before takeoff, and
f) Repairs are made within three
flight days.
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:
27-4
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
14-02 Aileron Indications on
ECAM Flight Control
Page
1) ECAM Aileron Position
Indications
C 2 0 (O) May be inoperative provided
capability to move affected aileron
through each servo control is verified
visually before each departure.
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
　
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