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1
0
May be inoperative provided flight deck brake accumulator pressure indicator 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:
32-4
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR
-41-2
Brake Accumulator Pressure Indicator (Flight Deck)
C
1
0
(M) May be inoperative provided brake accumulator charge is verified normal once each flight day.
-41-3
BRAKE SOURCE Indication System
A
1
0
(M)(O) May be inoperative provided:
a)
Flight deck brake accumulator pressure indicator operates normally,
b)
Normal and alternate brake systems are verified to operate normally,
c)
Brake accumulator isolation valve is verified to operate normally,
d)
Alternate procedures are established and used, and
e)
Repairs are made within three flight days.
1)
BRAKE SOURCE Light
C
1
0
May be inoperative provided the BRAKE SOURCE alerting message operates normally.
-42-1
Normal Antiskid Valves
C
12
10
(M)(O) One valve per each six wheel truck may be inoperative provided:
a)
Associated brake is deactivated using the deactivation assembly, and
b)
AFM performance decrements for brake(s) deactivated are applied.
C
12
10
(M)(O) One valve 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 brake(s) 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:
32-5
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR
-42-2
Antiskid Wheelspeed Transducers
C
12
10
(O) One transducer per each six wheel truck may be inoperative provided:
a)
AFM performance decrements for brake(s) deactivated are applied, and
b)
No other brakes are deactivated on that truck.
-42-3
Alternate Antiskid Valves
C
8
0
(M) May be inoperative provided manual braking capability on the alternate brake system is verified to operate normally.
-42-4
Autobrake System (Including Autobrake Solenoid Valve)
C
1
0
(M) May be inoperative provided:
a)
Autobrake solenoid valve is verified closed, and
b)
Autobrake selector remains in the OFF position.
C
1
0
(M) May be inoperative provided:
a)
Autobrake hydraulic control module is deactivated, and
b)
Autobrake selector remains in the OFF position.
-44-1
Brake Status Lights (On Nose Gear)
C
3
0
(O) May be inoperative provided alternate procedures are established and used.
D
3
0
May be inoperative provided procedures do not require their use.
-44-2
Gear Retraction Braking System
C
1
0
(O) Maybe inoperative provided:
a)
After takeoff, gear remains down for two minutes before retraction, and
b)
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:
32-6
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR
-44-3
Parking Brake Set Indication System (Flight Deck)
C
1
0
(M)(O) May be inoperative provided:
a)
Alternate procedures are established and used,
b)
Parking brake valve is verified to operate normally once each flight day,
c)
Parking brake and brake antiskid interface indication is verified to operate normally once each flight day, and
d)
Parking brake takeoff configuration warning system is verified to operate normally.
-45-1
Wheel Brakes
C
12
10
(M)(O) One per each six wheel truck may be inoperative provided:
　
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