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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.
Computer 30 PPiilloott MMaaggaazziinnee VV88II99 In the spring of 2001, Wilco
Publishing released 767 Pilot in
Command for FS2000, which turned
out to be one of the most highly acclaimed
MSFS add-ons ever. It proved that there
was a substantial (and largely untapped)
demand for simulations that strove
specifically to emulate the complexity of
an airliner’s flight deck. Even now, over
three years later, this product still has a
dedicated following.
In early 2003, Wilco followed up with a
new add-on product for FS2002, called A320
Pilot in Command. Although it was made
by a different group of developers, many
naturally associated it with 767 PIC and
great things were expected of it. Pre-release
marketing confirmed rumors that it would be
the first MSFS payware aircraft not to have
A320 Pilot In Command review...
a 2D cockpit at all. This was revolutionary.
Every switch, knob, and button would be
accessible by mouse from within the 3D
virtual cockpit environment. Remember that
　
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