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A-318, A-319, A-320, A-321
REVISION NO:21
DATE: 06/17/2009
PAGE:
24-3
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
24
ELECTRICAL POWER
20-01
Engine Driven Generator Channel (IDG, GCU, Line Contactor) (Continued)
2)
IAE Engines
(Relief applies only to IDGs which incorporate Mods. 26929 or 30375/P/N 772292)
B
2
1
(M)(O) Except for ER operations, one may be inoperative provided:
a)
APU generator operates normally and is used throughout the flight
b)
Operator ensures that the APU oil quantity is adequate for the intended flight,
c)
All busses can be powered,
d)
All indications and warnings associated with the remaining engine and APU driven generator channels are verified to operate normally,
e)
Galley automatic shedding is verified to operate normally,
f)
Aircraft remains at or below FL330,
g)
Fuel recirculation system associated with the operative IDG is operative, and
h)
Approach minimums do not require its use.
(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:
24-4
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
24
ELECTRICAL POWER
20-01
Engine Driven Generator Channel (IDG, GCU, Line Contactor) (Continued)
|
3)
PW Engines Only
B
2
1
(M)(O) Except for ER operations, one may be inoperative provided:
a)
APU generator operates normally and is used throughout the flight,
b)
Operator ensures that the APU oil quantity is adequate for the intended flight,
c)
All busses can be powered,
d)
All indications and warnings associated with the remaining engine and APU driven generator channels are verified to operate normally,
e)
Galley automatic shedding is verified to operate normally,
f)
Aircraft remains at or below FL330,
g)
IDG cooler bypass valve is checked operative before each flight, and
h)
Approach minimums do not require its use.
(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:
24-5
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
24
ELECTRICAL POWER
20-02
APU Generator Channel
(pre-Mod. 24642 or AES APU pre-Mod. 24498 or 25568)
C
1
0
(M) May be inoperative provided:
a)
APU GEN p.b switch is set to OFF, and
b)
Both APU oil filters are not clogged.
C
1
0
Except for ER operations, may be inoperative provided APU is not used.
(post-Mod. 24642 and AES APU post-Mod. 24498 and 25568 or APIC APU or APU GTCP 131-9(A))
C
1
0
May be inoperative provided APU GEN p.b switch is set to OFF.
C
1
0
Except for ER operations, may be inoperative provided APU is not used.
NOTE: When GPCU and APU generator are both inoperative, engines cannot be started.
20-07
AC ESS Feed Control
1)
ALTN Feed Function
C
1
0
May be inoperative provided:
a)
AC ESS FEED p.b switch is set at NORM position, and
b)
TR 2 operates normally.
27-01
IDG FAULT Lights
C
2
1
One may be inoperative provided frequency and temperature indications are available on ECAM ELEC page and are monitored.
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:
24-6
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
24
ELECTRICAL POWER
27-02
GEN p.b Switch
1)
FAULT Lights
C
3
1
One GEN and/or the APU FAULT Light may be inoperative provided the associated indications are available on ECAM ELEC page.
2)
OFF Lights
C
3
0
27-03
AC ESS FEED FAULT/ALTN Light
C
1
0
May be inoperative provided AC ESS bus indication is available on ECAM ELEC page.
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Airbus A318/A319/A320/A321 Master Minimum Equipment List(28)
