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AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
75-2
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
75 BLEED AIR
-24-2
Turbine Cooling Air Systems (PW)
C
2
1
(M) One may be inoperative provided associated Turbine Vane and Blade Cooling (TVBC) air shutoff valves are deactivated in the open position.
C
2
0
(M)(O) May be inoperative provided Turbine Vane and Blade Cooling (TVBC) air shutoff valves are deactivated in the open position.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 14 d
DATE: 02/26/2008
PAGE:
77-1
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
77 ENGINE INDICATING
-11-1
Engine Pressure Ratio Indicating Systems (PW and RR)
C
2
0
(O) May be inoperative provided:
a)
Both engines are operated in the alternate (ALTN) mode,
b)
For RR, N2 indication on affected engine operates normally, and
c)
Appropriate performance adjustments are applied.
-12-1
N2 Tachometer Systems (RR)
B
2
1
One may be inoperative provided EPR and Fuel Flow operate normally.
-21-1
Pyrometer Exhaust Gas Temperature (EGT) Indication System (GE Except GE90-100 Series)
C
2
0
(M) May be inoperative provided:
a)
Inoperative EGT pyrometer indication system is deactivated, and
b)
Associated engine EGT indications are verified to be normal.
-22-1
Engine Turbine Overheat Sensors (RR)
C
4
2
One per engine may be inoperative.
-31-1
Engine Vibration Monitor Systems
C
2
1
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
78-1
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
78 ENGINE EXHAUST
-31-1
Thrust Reversers
1)
All (Except
-200LR, 777F and
-300ER)
C
2
1
(M) One may be inoperative provided:
a)
Both sync locks are verified in the locked position,
b)
One locking actuator on each sleeve is verified in the locked position, and
c)
Inoperative reverser is secured in the forward thrust position.
|
|
2)
-200LR, 777F and
-300ER
C
2
1
(M)(O) One may be inoperative provided:
a)
Both sync locks are verified in the locked position,
b)
One locking actuator on each sleeve is verified in the locked position,
c)
Inoperative reverser is secured in the forward thrust position, and
d)
Appropriate performance adjustments are applied.
|
-34-1
Reverse Thrust Lever Interlocks
|
1)
-200/-200ER/-300
C
2
1
One may be inoperative released or retracted.
|
2)
-200LR/777F/-300ER
C
2
1
One may be inoperative released.
|
C
2
1
(O) One may be inoperative retracted provided appropriate performance adjustments are applied.
|
|
|
-36-1
Reverser Proximity Sensors
C
14
12
One per engine may be inoperative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
79-1
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
79 ENGINE OIL
-21-1
Engine Air/Oil Heat Exchanger Valves (RR)
C
2
0
(M)(O) May be inoperative provided:
a)
Associated valve is locked in the open position, and
b)
Appropriate minimum fuel temperature is maintained during flight.
-21-2
Engine Fuel/Oil Cooler Bypass Valves (PW)
C
2
0
May be inoperative in the closed position.
-31-1
Engine Oil Quantity Indicating Systems
A
2
1
(M) One may be inoperative provided:
a)
It is verified before each departure that the oil tank is filled to the recommended capacity,
b)
Oil consumption is within limits, and
　
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