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PFDU 2
C
1
0
(O)
May be inoperative provided:
a)
PFDU1, NDU1, E/WDU, SDU and NDU2 are operative, and
b)
Approach minimums do not require its use.
2)
NDU 1
C
1
0
(O) May be inoperative provided:
a)
PFDU1, NDU2, E/WDU, SDU and PFDU2 are operative, and
b)
Approach minimums do not require its use.
3)
NDU 2
C
1
0
(O) May be inoperative provided:
a)
PFDU1, NDU1, E/WDU, SDU and PFDU2 are operative, and
b)
Approach minimums do not require its use.
4)
SDU
A
1
0
(M)(O) May be inoperative provided:
a) PFDU1, NDU1, E/WDU, PFDU2 and NDU2 are operative,
b) AC ESS FEED control is verified operative once each day,
c) AC ESS FEED FAULT light is verified operative once each
day, and
d) Repairs are made within three flight days.
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8U.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:
31-8
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
31
INDICATING/ RECORDING SYSTEMS
63-02
Display Management Computers
(without Mod. 21678)
C
3
2
DMC 3 may be inoperative.
C
3
2
(M)(O) DMC 2 may be inoperative provided:
a)
AC ESS Feed Control is verified operative once each flight day, and
b)
AC ESS Feed Fault Light is verified operative once each flight day.
(with Mod. 21678)
C
3
2
DCM 1 or DMC 3 may be inoperative.
C
3
2
(M)(O) DMC 2 may be inoperative provided:
a)
AC ESS Feed Control is verified operative once each flight day, and
b)
AC ESS Feed Fault Light is verified operative once each flight day.
63-03
ECAM Memo Display
C
-
0
Indications may be inoperative.
63-04
ECAM Permanent Data Display
C
-
0
Indications may be inoperative provided TAT or SAT temperature is 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:
32-1
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
32
LANDING GEAR
32-00
CLASS II MAINTENACE MESSAGE DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY
1)
Fault(s) Indicated by BRAKES
Deleted, REV 21.
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11-01 ***
Torque Link Dampers
A
2
0
May be inoperative provided repairs are made within seven flight legs.
|
12-01
MAIN GEAR DOORS
1)
Ground Opening Cables
C
2
0
(M) May be broken or missing.
31-00
Landing Gear Retraction System
B
1
0
(O) Except for ER operations, may be inoperative provided the airplane is operated with landing gear down in accordance with the AFM supplement for gear down flight.
31-01
Landing Gear Control And Interface Units (LGCIU)
A
2
1
(M)(O) LGCIU No. 2 may be inoperative provided:
a)
Both radio altimeter systems operate normally,
b)
Both FCU channels operate normally,
c)
All ELACs, SECs, ADIRs, SFCCs and FACs operate normally,
d)
Both thrust lever position sensors of engine No. 2 are operative,
e)
Flex takeoff is not used,
f)
Reverser No. 2 is considered inoperative, and
g)
Repairs are made within one flight day.
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:
32-2
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
32
LANDING GEAR
33-01
Landing Gear Gravity Extension System
B
1
0
(O) Except for ER operations, may be inoperative provided the airplane is operated with landing gear down in accordance with the AFM supplement for gear down flight.
41-01
Wheel Tie Bolts
A
-
-
(M) One bolt may be broken or missing provided:
a)
Affected wheel is removed, checked for broken parts or damage, and replaced if broken parts or damage is found,
　
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