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FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
47-1
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
47 INERT GAS SYSTEMS
-11-1
***
Nitrogen Generation System (NGS)
D
1
0
(M) May be inoperative provided NGS shutoff valve is deactivated closed.
|
|
1)
Nitrogen Generation
D
1
0
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
49-1
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
49 AIRBORNE AUXILIARY
POWER
-11-1
Auxiliary Power Unit (APU)
C
1
0
(O) APU may be inoperative provided:
a)
Other procedures do not require its use, and
b)
Flight remains within 180 minutes of landing at a suitable airport.
|
|
|
|
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-15-1
APU Air Inlet Door Actuation System
C
1
0
(O) May be inoperative with door in any position provided:
a)
Other procedures do not require the use of the APU,
b)
APU is not used, and
c)
Flight remains within 180 minutes of landing at a suitable airport.
|
|
C
1
0
(M)(O) May be inoperative provided door is deactivated in the full open position.
1)
APU Air Inlet Door Actuator Position Indication Switch
C
1
0
(M) May be inoperative provided:
a)
APU inlet door is verified to operate normally before each departure, and
b)
Both ELMS P310 panel channels operate normally.
-42-1
APU Starting System (Includes Electric Starter)
C
1
0
(O) May be dispatched with APU START SYS faults provided APU is started before departure and operated continuously throughout the flight.
C
1
0
(O) May be dispatched with APU START SYS faults provided:
a)
Other procedures do not require use of the APU, and
b)
Flight remains within 180 minutes of landing at a suitable airport.
|
|
|
|
-43-1
APU Air Turbine Starter
C
1
0
May be inoperative provided electric starter operates normally.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
49-2
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
49 AIRBORNE AUXILIARY
POWER
-52-1
APU Bleed Air System
C
1
0
(O) May be inoperative provided:
a)
Other procedures do not require use of the APU as a pneumatic source, and
b)
Flight remains within 180 minutes of landing at a suitable airport.
NOTE: The APU may be used as an electrical power source.
-52-2
APU Bleed Air Check Valve
C
1
0
(O) May be inoperative provided:
a)
APU bleed air switch remains OFF except for main engine start,
b)
Other procedures do not require use of the APU as a pneumatic source, and
c)
Flight remains within 180 minutes of landing at a suitable airport.
NOTE: The APU may be used for electrical power. Air Turbine Starter is not available with APU bleed air shutoff valve closed.
-61-1
APU Controller
C
1
0
May be dispatched with APU CONTROL faults.
|
-61-2
APU Ground Control Panel
C
1
0
-70-1
APU FAULT Light
C
1
0
-71-1
APU EGT Indication
C
1
0
-73-1
APU RPM Indication
C
1
0
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
49-3
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
49 AIRBORNE AUXILIARY
POWER
-94-1
APU OIL QTY Indication
C
1
0
(M) May be inoperative provided APU oil quantity is verified adequate once each flight day.
C
1
0
(O) May be inoperative provided:
a)
　
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