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into known or forecast over-thetop
conditions.
22-02 Non-Stabilized Magnetic
Compass (Standby)
(Aircraft equipped with
Honeywell ADIRU’s or
aircraft equipped with
Litton ADIRUs P/N
465020-0303-316 and
Mod. 30630 or 30872)
B 1 0 (O) May be inoperative provided:
a) Three IRs operate normally, and
b) ATT/HDG, EIS DMS and
PFD/ND switching capabilities
operate normally.
(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:
34-9
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
22-02 Non-Stabilized Magnetic
Compass (Standby)
(Aircraft equipped with
Honeywell ADIRU’s or
aircraft equipped with
Litton ADIRUs P/N
465020-0303-316 and
Mod. 30630 or 30872)
(Continued)
B 1 0 (O) May be inoperative provided:
a) Three IRs operate normally, and
b) DDRMI operates normally.
B 1 0 (O) May be inoperative provided:
a) Any combination of two IRs are
operative, and
b) Airplane is operated with dual
independent navigation
capability and under positive
radar control by ATC on enroute
portion of flight.
1) Lighting (Aircraft
equipped with
Honeywell or Litton
ADIRU’s)
C 1 0
22-03 Integrated Standby
Instrument System
1) Horizon (Attitude)
Function
B 1 0 May be inoperative provided:
a) Operations are conducted in
Day VMC only, and
b) Operations are not conducted
into known or forecast over-thetop
conditions.
2) ILS Function D 1 0
3) Mach Number Function D 1 0
(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:
34-10
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
22-03 Integrated Standby
Instrument System
(Continued)
4) Bugs Function D 1 0
36-01 ILS Navigation Systems
C 2 - As required by FAR.
NOTE: GPWS Glideslope Deviation
Light(s) will be inoperative with
the loss of the ILS 1.
41-01 Weather Radar Systems D - - Any in excess of those required by FAR
may be inoperative.
42-01 Radio Altimeter (RA)
Systems
A 2 1 (O) One may be inoperative provided:
a) Approach minimums do not
require its use,
b) Both FCU channels operate
normally,
c) All ELACs, SECs, ADIRS,
SFCC, LGCIU, and FACs
operate normally, and
d) Repairs are made within two
flight days for RA 1 and within
three flight days for RA 2.
NOTE: Inoperative RA 1 renders
GPWS 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:
34-11
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
42-02 Automatic Call Out
System
C 1 0 May be inoperative provided approach
minimums do not require its use.
42-04 Altitude Alerting System A - 0 (O) May be inoperative provided:
a) Autopilot with altitude hold is
operative,
b) Enroute operations do not
require its use, and
c) Repairs are made within three
flight days.
C - 0 May be inoperative provided it is not
required by FAR.
43-01 Traffic Alert Collision
Avoidance System
(TCAS II)
B 1 0 (M) May be inoperative provided:
a) System is deactivated and
secured, and
b) Enroute or approach procedures
do not require its use.
C 1 0 (M) May be inoperative provided:
a) Not required by FAR,
b) System is deactivated and
secured, and
c) Enroute or approach procedures
do not require its use.
1) Combined Traffic Alert
(TA) and Resolution
Advisory (RA) Dual
Display System (s)
C 2 1 May be inoperative on the non-flying
pilot side provided:
a) TA and RA visual display is
operative on the flying pilot side,
and
b) TA and RA audio function is
operative on flying pilot side.
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION
　
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