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and C.G. calculations, and
b) ACT transfer valve is secured
closed.
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:
28-3
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
28 FUEL
12-01 Overpressure Protectors
(Continued)
(A321)
1) In Vent Surge Tank C 2 0 (M)(O) May be damaged or missing.
2) In Additional Center
Tank(s) (With ATC(s))
C - 0 (M)(O) May be open provided:
a) Manual transfer from ACT(s) to
center tank is verified to operate
normally, and
b) ACT(s) fuel quantity indications
(both FQI if both ACTs installed)
and center tank fuel quantity
indications are operative on
ECAM FUEL page.
C - 0 May be open provided there is no fuel in
any ACT.
C - 0 (M)(O) May be open provided:
a) Fuel in any ACT is considered
unusable and included in ZFW
and C.G. calculations, and
b) ACT transfer valve is secured
closed.
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:
28-4
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
28 FUEL
15-01 Outer to Inner TK
Transfer Valves
(A318/A319/A320)
|
|
A) LH Wing C 2 0 (O) May be inoperative open.
||
C 2 0 (O) Both may be inoperative closed
provided LH outer tank fuel is considered
unusable.
||||
C 2 1 (M)(O) One may be inoperative closed
provided the operative LH wing outer to
inner tank transfer valve is latched open
after each refueling.
||||
C 2 1 (O) One may be inoperative closed
provided the LH outer tank fuel
is considered as unusable for flight
planning.
||||
B) RH Wing C 2 0 (O) May be inoperative open.
||
C 2 0 (O) Both may be inoperative closed
provided RH outer tank fuel is
considered unusable.
||||
C 2 1 (M)(O) One may be inoperative closed
provided the operative RH wing outer to
inner tank transfer valve is latched open
after each refueling.
||||
C 2 1 (O) One may be inoperative closed
provided the RH outer tank fuel
is considered as unusable for flight
planning.
||||
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:
28-5
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
28 FUEL
20-01 Automatic Fuel Feed
System
|
1) A318/A319/A320
Feed System
with Mod. 37508
C 1 0 (O) May be inoperative provided
alternate procedures are established and
used.
|
2) A318/A319/A320
Feed System
(A318/A319/A320)
without Mod. 37508
C 1 0 (O) May be inoperative provided the
total FOB after refueling is less
than or equal to 12000kg (26500
lbs).
C 1 0 (O)May be inoperative provided:
a) The total FOB after refueling is
more than 12000 kg (26500 lb),
and
b) The fuel quantity in the center
tank is between2000 kg (4400 lb)
and 3000 kg (6600 lb).
21-01 Wing Tank Pumps
(Except those Aircraft
specified in Service
Bulletin A320-28-1102)
1) CFM Engines C 4 3 One pump may be inoperative provided
JP4/Jet B is not used.
C 4 3 (M) One pump 2 may be inoperative
when JP4/Jet B is used provided:
a) Prior to each flight, fuel return
valve is verified to operate
normally, and
b) Takeoff ECAM fuel temperature
is less than 30 degrees C.
|
2) IAE Engines C 4 3 One pump may be inoperative provided
JP4/Jet B is not used.
C 4 3 One pump 2 may be inoperative when
JP4/Jet B is used provided takeoff fuel
temperature is less than 30 degrees C.
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:
28-6
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
　
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