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AIRCRAFT:
A-318, A-319, A-320, A-321
REVISION NO: 21
DATE: 06/17/2009
PAGE:
73-3
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
73 ENGINE FUEL &
CONTROL
20-09 Aircraft 28V Power
Supply (IAE Engines
Only)
C 4 2 Channel B power supply may be
inoperative on one or both engines.
20-10
***
Engine Bump C 2 0 May be inoperative provided benefit of
bump is not utilized for determination
of takeoff performance.
30-02 Fuel Used
Indications
C 2 0 (M) May be inoperative provided:
a) Associated tank fuel quantity
indication system operates
normally, and
b) Fuel-On-Board indication
operates normally.
30-03 Fuel Filter Clog
Cautions on ECAM
E/WD (IAE Engines
and CFM Engines
with Mod. 28397 or
Mod. 28398)
C 2 1 (M) One may be inoperative provided
associated filter is changed once each
flight day.
|
|
(PW Engines) C 2 1 (M) One may be inoperative provided
associated filter is changed once each
flight day or every 15 flight hours
whichever occurs first.
|
|
30-04 Fuel Filter Clog
Indication on ECAM
System Display
C 2 0
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
A-318, A-319, A-320, A-321
REVISION NO: 20
DATE: 03/19/2008
PAGE:
74-1
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
74 IGNITION
31-01 Ignition Systems
1) CFM Engines
a) System A C 2 2 (M) NOTE: A and B input or output from
the exciter boxes may be
swapped in order to restore
System A operative.
b) System B (CFM 56-5A
Engines With Mod.
22333 or CFM 56-5B
Engines)
C 2 0 (O) May be inoperative provided
System A is operative.
c) System B (CFM 56-5A
Engines Without Mod.
22333)
C 2 0 (O) May be inoperative provided:
a) Engine relight envelope with
System B inoperative is
observed, and
b) System A operates normally.
2) IAE Engines & PW
Engines
a) System A C 2 1 (O) Except for ER operations, may be
inoperative on one engine only.
b) System B C 2 0 (O) May be inoperative provided system
A operates normally.
c) System A and B C 4 2 (O) Except for ER operations, two
igniters may be inoperative provided
they are not on the same engine.
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
A-318, A-319, A-320, A-321
REVISION NO: 20
DATE: 03/19/2008
PAGE:
74-2
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
74 IGNITION
31-01 Ignition Systems
(Continued)
2) IAE & PW Engines
(Continued)
NOTE: On IAE & PW engines, system
A must be considered
inoperative on both engines if
the common power supply line
from 401XP 115VAC ESS BUS
is inoperative as a result of
either a loss of electrical
continuity or a short circuit (C/B
Engine/1 AND 2 IGN/SYS A
(49VUA03) tripped).
31-02 ECAM Indications
(Lower Display)
1) Selected Igniter C 2 0 (M) May be inoperative provided IGN
FAULT warning operates normally on
ECAM.
31-03 IGN FAULT Caution
on ECAM
1) CFM Engines C 4 3 (M) One may be inoperative provided
associated ignition system is verified to
operate normally once each flight day.
C 4 2 (M) Two may be inoperative provided
associated ignition system is verified to
operate normally before each
departure.
2) IAE & PW Engines C 4 2 One or two may be inoperative
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:
75-1
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
75 BLEED AIR
21-01 HP Turbine Active
Clearance Control
System (CFM Engines
Only)
1) HPTC Valves Incorporated into 73-20-01.
2) Feedback Systems Incorporated into 73-20-01
.
3) HPTC Torque Motor
Wraps
Incorporated into 73-20-01.
4) HPTC Thermocouples Incorporated into 73-20-01.
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