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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
1.
4. REMARKS AND EXCEPTIONS
28
FUEL
21-02
Center Tank Systems
1)
Pumps (A318/A319/A320) (Without ACT)
C
2
1
(O) One may be inoperative provided (when center tank fuel is required) a suitable alternate airport exists within range of wing tanks fuel loading.
C
2
0
(O) May be inoperative provided:
a)
Center tank pumps remain OFF, and
b)
Center tank remains empty.
||||
C
2
0
(O) May be inoperative provided fuel in center tank is considered unusable, and is included in ZFW and C.G. calculations.
|||
|
(A319/A320) (With ACT(s))
C
2
1
(O) One may be inoperative provided (when center tank fuel is required) a suitable alternate airport exists within range of wing tanks fuel loading.
C
2
0
(M)(O) May be inoperative provided:
a)
Center tank pumps remain OFF, and
b)
Center tank and ACT(s) remain empty.
|||||
C
2
0
(M)(O) May be inoperative provided fuel in center tank or ACT(s) is considered unusable and included in ZFW and C.G. calculations and the ACT transfer valve is secured closed.
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Airbus A318/A319/A320/A321 Master Minimum Equipment List(47)
