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may be inoperative provided:
a) Slats, Flaps, and associated
monitoring and protection
systems operate normally on
SFCC 1,
b) Operation of SFCC 1 WTBs are
confirmed by tests before each
departure,
c) Electrical supply to SFCC 2 slat
channel is inhibited,
d) ELAC, SEC, ADIRS, LGCIU,
FAC and RA systems operate
normally, and
e) Takeoff in CONF 1+F is
prohibited.
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:
27-13
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
92-01 Speed Brake Control
System
C 1 0 (O) May be inoperative provided AFM
performance penalties associated with
all ground spoilers inoperative are
applied.
1) Speed Brake 2 or 3 and
4
C - - (O) May be inoperative provided AFM
performance penalties associated with
one pair or two pairs of ground spoilers
inoperative are applied.
|
92-02 Ground Spoiler Control
System
A 1 0 (M)(O) May be inoperative provided:
a) A check of the thrust reverser
system is performed before each
flight to ensure that both thrust
reversers operate normally,
b) Autobrake function is not used,
c) Approach minimums do not
require its use,
d) AFM takeoff and landing
performance penalties are
applied, and
e) Repairs are made within three
flight legs.
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|
|
|
1) Spoiler 5 C 2 0
2) Spoilers 1 and 2 or 3
and 4
C 8 4 (O) Spoilers 1 and 2 or 3 and 4 may be
inoperative provided AFM performance
penalties are applied.
92-03 Accelerometer Systems Incorporated into 27-27-00, sub item 1).
|
92-04 Sidestick Transducer
Systems
Deleted, REV 4.
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:
27-14
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
92-05 Spoiler/Speed-brake
Indications on ECAM
F/CTL and Wheel Page
C 10 - May be inoperative for an associated
inoperative spoiler.
C 10 0 (O) May be inoperative provided a
visual check of affected surface
movement is made before each
departure.
92-06
***
Side Stick Dual Input
Warning System
1) Flashing portion of
Sidestick dual input
function in lower half of
Sidestick priority green
light.
D 2 0 May be inoperative provided Sidestick
priority function is operative.
2) Aural Warning
D 1 0
92-07 Thrust Lever
Transducers
1) SEC 1
Incorporated into 27-92-02.
2) SEC 2
Incorporated into 27-27-00, sub item 1). |
3) SEC 3
Incorporated into 27-92-02.
92-08 SEC Tachometer Inputs
1) SEC 1
Incorporated into 27-92-02.
2) SEC 2
Incorporated into 27-27-00, sub item 1). |
3) SEC 3
Incorporated into 27-92-02.
92-09 Hydraulic Pressure
Switches
Incorporated into 27-27-00, sub item 1). |
92-10 Hydraulic Pressure
Transducers
Incorporated into 27-27-00, sub item 1). |
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:
27-15
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
92-11
***
STEEP APPR p.b
Switch
(With Mod.35542)
1) ON Light
C 1 0
2) FAULT Light
C 1 0
93-01 Elevator Aileron
Computers (ELAC)
(A320-200 without Mod.
26334 or 26335)
B 2 1 (M)(O) Except for ER operation, ELAC
1 or any ELAC 1 function may be
inoperative provided:
a) Both accelerometers
associated with ELAC 2
operate normally,
b) All Sidestick transducers
associated with ELAC 2 and the
three SECs operate normally,
c) ELAC 2, SECs, ADIRs, SFCCs,
LGCIUs, FACs, and RAs
operate normally,
d) TR 1 and TR 2 operate
normally,
e) DC TIE contactor 1 is verified
closed before each departure,
　
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