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a)
Associated brake is deactivated with a deactivation assembly, and
b)
AFM performance decrements for brakes deactivated are applied.
C
12
10
(M)(O) One per each six wheel truck may be inoperative provided:
a)
Associated brake is deactivated by capping the brake line,
b)
After takeoff, gear remains down for two minutes before retraction,
c)
AFM performance decrements for brakes deactivated are applied, and
d)
Takeoff performance is based on landing gear extended.
C
12
10
(M)(O) One per each six wheel truck may be removed from the center axle only provided:
a)
Associated brake line is capped,
b)
After takeoff, gear remains down for two minutes before retraction,
c)
AFM performance decrements for brakes deactivated are applied, and
d)
Takeoff performance is based on landing gear extended.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
32-7
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR
-45-2
Wheel Tie Bolts
A
-
-
(M) One per wheel may be broken or missing provided:
a)
Affected wheel is removed, checked for broken parts or damage, and replaced if broken parts or damage is found,
b)
Associated brake is checked for broken parts or damage, and is replaced or deactivated if broken parts or damage is found,
c)
After each landing, wheel is inspected for additional broken or missing tie bolts, and
d)
Operations are limited to five departures before repairs are made.
-45-3
***
Integral Tire Pressure Indicators
D
-
0
-45-4
Nose Gear Spin Brake
C
2
0
(O) May be inoperative or missing provided after takeoff, gear remains down for two minutes before retraction.
NOTE: In the event of engine failure after V1, retract landing gear after takeoff.
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-46-1
Brake Temperature Indication System
C
1
0
(O) May be inoperative provided AFM Maximum Quick Turnaround Weight limitations are observed.
NOTE 1: Brake cooling fans (if installed) will be inoperative when all brake temperature indications are inoperative.
NOTE 2: Any portion of the system that operates normally may be used.
-47-1
***
Brake Cooling Fans
D
12
0
(M) May be inoperative provided associated fan shrouds are removed.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
32-8
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR
-49-1
***
Tire Pressure Indication System
C
1
0
May be inoperative provided alternate procedures are established and used.
NOTE: Any portion of the system that operates normally may be used.
D
1
0
May be inoperative provided procedures do not require its use.
-53-1
Main Gear Steering System (Including Indication)
C
1
0
(M) May be inoperative provided:
a)
Main gear steering actuators are verified locked in the center position, and
b)
Main gear steering system is deactivated.
-61-1
Landing Gear Position Indication Systems
B
2
0
(M)(O) May be inoperative provided:
a)
Landing gear are secured in the down position, and
b)
Airplane is dispatched in accordance with the appropriate AFM Gear Extended Appendix.
1)
Truck Tilt Sensors
C
4
0
(M)(O) May be inoperative provided the nose gear lock, nose gear down, main gear side brace and main gear drag brace sensors are verified to operate normally each flight day.
2)
Nose Gear Not Compressed Sensors
C
2
1
(M) One PSEU 2 nose gear not compressed sensor may be inoperative provided:
a)
Nose gear lock, nose gear down, main gear side brace and main gear drag brace sensors are verified to operate normally each flight day, and
b)
Left equipment cooling controller operates normally.
C
2
1
(M) One PSEU 1 nose gear not compressed sensor may be inoperative provided nose gear lock, nose gear down, main gear side brace and main gear drag brace sensors are verified to operate normally each flight day.
　
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