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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.
27-04 GALLEY/GALY&CAB
p.b Switch
1) FAULT Light C 1 0 (O) May be inoperative provided:
a) AC load indication for each
generator channel is available
on ECAM ELEC page, and
b) Automatic shedding operates
normally.
2) OFF Light C 1 0
27-05 RAT and EMER GEN
FAULT Light
C 1 0 (O) May be inoperative provided
indications are available on associated
ECAM ELEC page.
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:
24-7
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL POWER
27-06 Indications On ECAM
ELEC Page
C - - (O) Indications related to AC generation
may be inoperative provided:
a) Load, voltage and frequency
indications of at least one engine
driven generator operate
normally,
b) Associated GEN FAULT caution
on ECAM operates normally,
and
c) Automatic shedding operates
normally.
a) APU GEN Parameters C - 0 Except for ER operations, may be
inoperative provided both Engine Driven
Generators are operative.
27-09
***
COMMERCIAL p.b
Switch
1) OFF Light
C 1 0
DC GENERATION
SYSTEM
30-01 Transformer/Rectifier
Units (TR)
A 3 2 (O) Except for ER operations, TR1 may
be inoperative provided:
a) Extract fan operates normally,
b) Battery voltage indicator
operates normally,
c) Both packs operate normally,
d) Repairs are made within two
flight days, and
e) 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:
24-8
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL POWER
30-01 Transformer/Rectifier
Units (TR) (Continued)
Without Mod. 27620 A 3 2 (O)Except for ER operations, TR2 may
be inoperative provided:
a) Extract fan operates normally,
b) Battery voltage indicator
operates normally,
c) Both packs operate normally,
d) Repairs are made within two
flight days,
e) AC ESS FEED control is
checked operative once each
day,
f) Standby Horizon operates
　
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