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PSEU 1 transmission is verified on the right ARINC 629 systems bus,
b)
PSEU 2 transmission is verified on the left ARINC 629 systems bus,
c)
After takeoff, gear remains down for two minutes before retraction, and
d)
Takeoff performance is based on landing gear extended.
C
4
2
(M)(O) One may be inoperative in each PSEU provided:
a)
Landing gear are secured in the down position, and
b)
Airplane is dispatched in accordance with the appropriate AFM Gear Extended Appendix.
-09-1
Air/Ground System - Weight on Wheels
C
2
1
(M) Left system may be inoperative deactivated provided the right system cardfile power supply 1 operates normally.
C
2
1
(M) Right system may be inoperative deactivated provided all galley/lavatory water supply shutoff valves are closed.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
32-2
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR
-11-1
Nose Landing Gear Strut Upper Air Chamber Pressure Indicator (-300ER)
D
1
0
-30-1
Landing Gear Actuation System
B
1
0
(M)(O) May be inoperative provided:
a)
Inoperative components are properly secured by an accepted procedure,
b)
Landing gear is secured in the down position, and
c)
Airplane is dispatched in accordance with the appropriate AFM Gear Extended Appendix.
-30-2
Semi-Lever Gear (SLG) System
(-300ER)
C
1
0
(M)(O) May be inoperative provided:
a)
SLG system is deactivated, and
b)
Appropriate performance adjustments are applied.
-31-1
Landing Gear Lever Lock Solenoid
C
1
0
(O) May be inoperative provided solenoid is in the locked position.
-31-2
Landing Gear Selector Valve Electrical Control Circuits
C
2
1
(M) One UP/DOWN electrical control circuit may be inoperative provided the remaining UP/DOWN circuit is verified to operate normally each flight day.
-32-1
Main Gear Door Uplock Springs
B
4
3
(M)(O) One spring on one door uplock mechanism may be missing and gear retraction allowed provided the gear extended speed placard is not exceeded.
-32-2
Main Gear Uplock Springs
B
4
3
(M)(O) One spring on one main gear uplock mechanism may be missing and gear retraction allowed provided gear extended speed placard is not exceeded.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
BOEING B-777
REVISION NO: 15
DATE: 02/11/2009
PAGE:
32-3
1. 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
SYSTEM &
SEQUENCE
NUMBERS
ITEM
4. REMARKS OR EXCEPTIONS
32 LANDING GEAR
-32-3
Main Gear Side Brace Springs
(PRR 61350-34 Not Incorporated)
B
4
3
(M)(O) One main gear side brace spring may be missing provided airspeed is limited to 250 knots when extending landing gear using alternate gear extend system.
-35-1
Landing Gear Alternate Extend System
B
1
0
(M)(O) May be inoperative provided:
a)
Landing gear are secured in the down position,
b)
Alternate extend system is deactivated, and
c)
Airplane is dispatched in accordance with theappropriate AFM Gear Extended Appendix.
1)
Alternate Extend Hydraulic Pressure Switch
B
1
0
(M)(O) May be inoperative open provided:
a)
Landing gear doors are verified to open using the alternate extend system, and
b)
Alternate procedures are established, and used when required.
-35-2
Ground Door Release Control System
C
1
0
(M) May be inoperative provided:
a)
Both door open control switches are verified to be open,
b)
Landing gear doors are verified to open using the alternate extend system, and
c)
Landing gear doors are closed before each departure.
1)
Door Open Control Switches
B
2
0
(M)(O) May be inoperative closed provided:
a)
Landing gear are secured in the down position,
b)
Landing gear alternate extend system is deactivated, and
c)
Airplane is dispatched in accordance with the appropriate AFM Gear Extended Appendix.
-41-1
Brake Accumulator Pressure Indicator (Wheel Well)
D
　
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