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c)
Associated ENG OIL PRESS, OIL TEMP indications operate normally.
33-02
OIL LO PR Warning on ECAM (IAE or CFM Engines only)
C
2
1
||
C
2
0
May be inoperative provided RCDR GND CTL is verified ON after engines are started.
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:
79-3
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
79
ENGINE OIL
35-01
OIL FILTER CLOG Indications on ECAM Engine System Page
1)
CFM or IAE Engines Excluding Those With S/N’s V10600 To V11304 and V11315, V11330, V11335 (Not Including V11280, V11302)
C
2
1
2)
IAE Engines S/N’s V10600 To V11304 and V11315, V11330, V11335 (Not Including V11280, V11302) Without #3 FAG Bearing P/N 2A1165 Installed
C
2
1
3)
IAE Engines S/N V10600 To V11304 and V11315, V11330, V11335 (Not Including V11280 V11302) With #3 FAG Bearing P/N 2A1165 Installed
C
2
1
(M) One may be inoperative provided oil filter screen and chip detector on associated engine are checked and verified clear of contaminants once each flight day.
4)
PW Engines
C
2
1
(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:
79-4
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
79
ENGINE OIL
35-02
OIL FILTER CLOG Caution on ECAM E/WD
1)
CFM 56-5A Engines
C
2
1
(M) One may be inoperative provided:
a)
Associated filter is replaced once each flight day, and
b)
Chip detectors are inspected when the filter is replaced and do not reveal the presence of metal chips or other contaminants.
2)
CFM 56-5B Engines
C
2
1
(M) One may be inoperative provided:
a)
Associated filter is replaced once each flight day, and
b)
Visual indicator (pop-out) on the electrical master chip detector is inspected when the filter is replaced and does not reveal the presence of metal chips or other contaminants.
3)
PW Engines
C
2
1
(M) One may be inoperative provided:
a)
The associated filter is changed within the first day and every seven days, and
b)
The associated master chip detector is inspected when the filter is replaced and does not reveal the presence of magnetic chips.
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:
80-1
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
80
STARTING
11-01
Start Valve System
1)
Valves
(CFM/IAE Engines)
C
2
1
(M)(O) One may be inoperative provided:
a)
Valve is manually closed after engine start, and
b)
Associated igniter system operates normally.
(PW Engines)
C
2
1
(M)(O)One may be inoperative provided:
a)
Valve is manually closed after engine start,
b)
Associated igniter system operates normally, and
c)
Associated ENG 1 (2) START VALVE FAULT START VALVE NOT CLOSED caution is not displayed on ECAM E/WD after engine start.
2)
Solenoids
Incorporated into 73-20-01.
11-02
ENG MAN START Controls
C
2
0
11-03
FAULT light on ENGINE MASTER Panel
C
2
0
11-04
ECAM Start Valve Position Indicators (Lower Display)
C
2
0
(M) May be inoperative provided start valve is verified closed after engine start.
11-05
AUTOSTART Controls
C
2
0
(O) May be inoperative provided manual start procedures are used.
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Airbus A318/A319/A320/A321 Master Minimum Equipment List(89)
