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DATE: 06/17/2009
PAGE:
36-11
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
36 PNEUMATIC
12-03 APU Bleed Check Valve C 1 0 (O) May be inoperative closed provided
APU bleed switch is selected OFF.
C 1 0 (O) May be inoperative open and APU
used provided:
a) Airplane remains at or below FL
200, and
b) X BLEED selector is selected
SHUT and ENG 1 bleed is
selected OFF if engine bleed is
used.
C 1 0 (O) May be inoperative open provided
APU is not used.
12-04 Cross Bleed Valve
1) Automatic Control C 1 0 (O) May be inoperative provided
manual control operates normally.
20-01 ENG BLEED p.b Switch
1) FAULT Lights C 2 0 May be inoperative provided alternate
procedures are established and used.
2) OFF Lights
C 2 0
20-02 APU BLEED p.b Switch
1) FAULT Light C 1 0
2) On Light C 1 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:
36-12
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
36 PNEUMATIC
20-03 ECAM BLEED Page
Indications
1) ENG BLEED Pressure C 2 0
2) ENG BLEED
Temperature
C 2 0
3) ENG BLEED Valve C 2 0
4) ENG HP Valve C 2 0
5) APU BLEED Valve C 1 0
6) X BLEED Valve C 1 0
22-15 Pylon Leak Detection
Loops
(A318/A319/A320/A321
aircraft fitted with Mod.
33844, or Mod. 33847,
or Mod. 33687)
C 2 1 (M) One may be inoperative provided:
a) The associated pylon leak
detection loop is deactivated,
b) The caution AIR ENG 1(2)
BLEED LEAK is confirmed to be
false by troubleshooting, and
c) The affected bleed air supply
system is considered
inoperative.
|||||||||
(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:
36-13
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
36 PNEUMATIC
22-15 Pylon Leak Detection
Loops (Continued)
(A318/A319/A320/A321
aircraft without Mod.
33844, or Mod. 33847,
or Mod. 33687)
(Continued)
C 2 1 (M)(O) Except for ER operations
beyond 120 minutes, one may be
inoperative provided:
a) The associated pylon leak
detection loop is deactivated,
b) The associated BLEED p.b-sw
is set to OFF,
c) The associated PACK p.b-sw is
set to OFF,
d) The X-BLEED selector is set to
SHUT,
e) The APU BLEED p.b-sw is set
to OFF if LH side is affected,
f) The aircraft is not operated in
known or forecast icing
conditions, and
g) Airplane remains at or below FL
310.
|||||||||||||||||
|
(A320/A321 aircraft
fitted with Mod. 31283
and without Mod. 33844,
or Mod. 33847)
C 2 1 (M)(O) Except for ER operations
beyond 120minutes, one may be
inoperative provided:
a) The associated pylon leak
detection loop is deactivated,
b) The associated BLEED p.b-sw
is set to OFF,
c) The associated PACK p.b-sw is
set to OFF,
d) The X-BLEED selector is set to
SHUT,
e) The APU BLEED p.b-sw is set
to OFF if LH side is affected,
f) The aircraft is not operated in
known or forecast icing
conditions, and
g) The speedbrakes are operative.
||||||||||||||||
|
(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:
36-14
2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM, &
SEQUENCE ITEM
NUMBERS
1.
4. REMARKS AND EXCEPTIONS
36 PNEUMATIC
22-15 Pylon Leak Detection
Loops
(Continued)
(A319 aircraft fitted with
Mod. 31283 and without
Mod. 33844, or Mod.
33847)
C 2 1 (M)(O) Except for ER operations, one
may be inoperative provided:
a) The associated pylon leak
detection loop is deactivated,
b) The associated BLEED p.b-sw is
set to OFF,
c) The associated PACK p.b-sw is
set to OFF,
　
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