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a) Autopilot Disconnect Warning
operates normally, and
b) Autoland is not used.
NOTE: If one of the locking solenoids
is inoperative in the unlocked
position, the affected side stick
or pedals will move freely and
the “hard point” will not be felt
any longer by the pilots. This
may result in an unintentional
AP disconnection.
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:
22-3
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT
10-07 Autopilot FMA
Indications on PFD
Combined with Item 22-83-02.
30-01 Autothrust Function C 1 0 (M) May be inoperative provided:
a) All thrust lever sensors are
verified to operate normally,
and
b) Approach minimums do not
require its use.
NOTE: Alpha floor is not available
with autothrust function
inoperative.
30-02 Autothrust Instinctive
Disconnect Switches
C 2 1 (O) One may be inoperative provided
ability to disconnect A/THR by means
of the remaining Instinctive
Disconnect p.b and by the FCU
A/THR p.b is verified prior to each
departure.
|
30-03 Autothrust
Disengagement
Warning System
C 1 0 (O) May be inoperative provided:
a) Autothrust is disconnected and
is considered inoperative, and
b) Approach minimums do not
require its use.
|
NOTE: Alpha floor is not available.
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:
22-4
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT
63-01 Yaw Dampers
1) System 1 C 1 0 (M) May be inoperative provided:
a) System 1 is deactivated,
b) System 2 is operative, and
c) Approach minimums do not
require its use.
2) System 2 C 1 0 (M) May be inoperative provided:
a) System 2 is deactivated in the
case of actuator leakage,
b) System 1 is operative, and
c) Approach minimums do not
require its use.
|
|
|
66-01 Flight Augmentation
Computers (FAC)
`
1) FAC 2 C 1 0 (O) May be inoperative provided:
a) Both FCU channels operate
normally,
b) ELAC, SEC, ADIRS, SFCC,
RA, and LGCIU systems
operate normally, and
c) Approach minimums do not
require its use.
|
NOTE: Loss of FAC 1 will result in
Direct Law Mode at landing
gear down.
|
66-02 FAC p.b Switch
1) FAULT Lights
C 2 1
2) OFF Lights
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:
22-5
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT
66-03 Windshear
Detection/Guidance
And Avoidance
Systems
1) Windshear Detection
and Avoidance
System
(Predictive)
B - 0 (O) May be inoperative provided
alternate procedures are established
and used.
NOTE: Operator’s alternate
procedures should include
reviewing windshear
avoidance and windshear
recovery procedures.
C - 0 (O) May be inoperative provided:
a) Alternate procedures are
established and used, and
b) Windshear Warning and
Guidance System (Reactive)
operates normally.
2) Windshear Warning
and Flight Guidance
System
(Reactive)
B - 0 (O) May be inoperative provided
alternate procedures are established
and used.
NOTE: Operator’s alternate
procedures should include
reviewing windshear
avoidance and windshear
recovery procedures.
(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:
22-6
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
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