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NUMBERS
1.
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
60-03 ECAM Wheel Page
Indications (Continued)
|
11) [Y] ALTN BRK (With
Mod. 31441)
C 2 0
12) ACCU PRESS/ACCU
ONLY (With Mod.
31441)
C 1 0
60-04 Fault(s) Indicated by
BRAKES N/WS MINOR
FAULT Caution on
ECAM E/WD (With Mod.
26925 and without Mod.
38973)
B - - (M)(O) May be displayed provided:
a) BSCU system 1 and system 2
operate normally, and
b) It is checked prior to each
departure that the following
CFDS failure messages related
to BRAKES N/WS MINOR
FAULT are not displayed:
- A fault on the Alternate
Braking Control Unit (ABCU),
- A fault on the Alternate
Braking Selector Valve,
- A fault on the Alternate
Braking Servo-valve, or
- A degraded pressure on an
Alternate Servo-valve.
||
(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:
32-11
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
60-04 Fault(s) Indicated by
BRAKES N/WS MINOR
FAULT Caution on
ECAM E/WD (With Mod.
26925 and without Mod.
38973)
(Continued)
B - - (M)(O) May be displayed provided:
a) BRAKES pressure indicators
operate normally,
b) Alternate braking system is
checked operative before the first
flight of each day, and
c) It is checked prior to each
departure that the following
CFDS failure messages related
to BRAKES N/WS MINOR
FAULT are not displayed:
- A fault on the Alternate
Braking Control Unit (ABCU),
- A fault on the Alternate
Braking Selector Valve,
- A fault on the Alternate
Braking Servo-valve,
- A fault on the Alternate
Pressure Transducer, or
- A degraded pressure on an
Alternate Servo-valve.
|||
60-04 Fault(s) Indicated by
BRAKES N/WS MINOR
FAULT Caution on
ECAM E/WD (With Mod.
26925 and with Mod.
38973)
B - - (M)(O) May be displayed provided
BSCU system 1 and system 2 operate
normally.
||
B - - (M)(O) May be displayed provided:
a) BRAKES pressure indicators
operate normally,
b) Alternate braking system is
checked operative before the first
flight of each day, and
c) It is checked prior to each
departure that the following
CFDS failure message related to
BRAKES N/WS MINOR FAULT
is not displayed:
- A fault on an Alternate
Pressure Transducer.
|
|
|
60-07
***
Integral Tire Pressure
Indicators
D - 0
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:
33-1
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
33 LIGHTS
10-01 Cockpit and Instrument
Panel Lighting System
C - - Individual lights may be inoperative
provided remaining lights are:
e) Sufficient to clearly illuminate all
required instruments, controls,
and other devices for which they
are provided,
f) Positioned so that direct rays are
shielded from flight crewmembers
eyes,
g) Lighting configuration and
intensity is acceptable to the flight
crew,
d) Both dome lights are operative,
and
e) Main panel flood light operates
normally.
|
NOTE: Dome lights are considered
operative with a minimum of three
bulbs illuminated in each
assembly.
||||
10-02 Annunciator Lights
1) Test Function B 1 0
2) Dim Function C 1 0
May be inoperative for day operations.
|
3) Bright Function C 1 0 May be inoperative:
a) For night operations, and.
b) Day operations are not
conducted.
||||
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:
33-2
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
33 LIGHTS
20-01 Cabin Light System
1) Passenger
　
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