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时间:2011-04-26 22:30来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

When you use the switches on the P40 panel, the nose landing gear doors close in approximately 5 seconds.
WARNING: MAKE SURE THE AREA AROUND THE DOORS FOR THE NOSE LANDING GEAR IS CLEAR OF PERSONS AND EQUIPMENT. THE DOORS CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
Once the door close operation starts, you can not stop the operation with the switches on the remote panels.
EFFECTIVITY BEJ ALL  32-35-00 
Page 40 
D633W101-BEJ  Sep 05/2002 

 

LANDING GEAR ALTERNATE EXTENSION SYSTEM -LANDING GEAR DOOR CLOSE OPERATION

EFFECTIVITY BEJ ALL  32-35-00 
Page 41 
D633W101-BEJ  Sep 05/2002 


LANDING GEAR ALTERNATE EXTENSION SYSTEM -BLEED VALVES

General
Four bleed valves let you bleed air from the alternate extension system. You need to bleed the alternate extension system when you replace some of the alternate extension system components.
Location
The bleed valves are near these components:
*
The NLG selector/bypass valve (NLG wheel well)

*
The NLG alternate uplock release actuator (NLG wheel well)

*
The left and right MLG alternate uplock release actuators (left and right MLG wheel wells).


Training Information Point
You operate the alternate extend power pack when you bleed the alternate extension system.
NOTE: The alternate extend power pack operates when you command the landing gear doors open with the ground door release system.
NOTE: The EICAS displays indicate non-normal sequencing during this test.
NOTE: The power pack remains ON until the LDG GR ALTN EXT CONTROL circuit breaker is opened. (The pressure switch that usually stops the power pack does not work since you are bleeding the system.)
CAUTION:  MAKE SURE YOU DO NOT RUN THE ALTERNATE EXTEND POWER PACK FOR MORE THAN FIVE MINUTES. IF YOU RUN THE POWER PACK FOR MORE THAN FIVE MINUTES, THE POWER PACK CAN GET TOO HOT. THIS CAN CAUSE DAMAGE TO THE EQUIPMENT.
EFFECTIVITY BEJ ALL  32-35-00 
Page 42 
D633W101-BEJ  Sep 05/2002 

 

LANDING GEAR ALTERNATE EXTENSION SYSTEM -BLEED VALVES

EFFECTIVITY BEJ ALL  32-35-00 
Page 43 
D633W101-BEJ  Sep 05/2002 


WHEELS AND BRAKES -INTRODUCTION

General  * decel -deceleration
*
ft -feet The wheels and brakes system includes: * fwd -forward

* gnd -ground

*
Wheels, brakes, and tires (SECTION 32-45) * gr -gear
*


*
Brake hydro-mechanical control system (SECTION 32-41) hyd -hydraulic
*


*
Parking brake system (SECTION 32-44)  ind -indication

*
Antiskid/autobrake systems (SECTION 32-42) * kts -knots
*


*
Tire pressure indication system (SECTION 32-49)  ldg -landing

*  
Brake temperature monitor system (BTMS) * LG -landing gear
(SECTION 32-46). * LRU -line replaceable unit


*
lt -left Abbreviations and Acronyms * mdl -module

* MD&T -master dim and test

*
A/B -autobrake

* MFD -multi-function display

*
ACMP -alternating current motor pump

* MLG -main landing gear

*
ADIRU -air data inertial reference unit

* mtrd -metered

*
AIMS -airplane information management system

* NLG -nose landing gear

*
AIV -accumulator isolation valve

* press -pressure

*
altn -alternate


PSEU -proximity sensor electronic unit
* ARINC -aeronautical radio, inc  * * psi -pounds per square inch * ASSV -alternate source selection valve * psig -pounds per square inch gage * A/S -antiskid * pwr -power * bat -battery * ref -reference
* BITE -built-in test equipment * rel -release
* brk -brake * rqst -request * BSCU -brake system control unit
* rt -right
* BTMS -brake temperature monitor system * RTO -rejected takeoff * BTMU -brake temperature monitor unit * sec -second
* capt -captain * sel -selector
* ctr -center * sig -signal * ctrl -control * sol -solenoid
* DC -direct current
EFFECTIVITY


32-40-00
BEJ ALL
Page 1 D633W101-BEJ Sep 05/2002

WHEELS AND BRAKES -INTRODUCTION

*
spd -speed

*
stby -standby

*
strg -steering

*
sw -switch

*
sys -system

*
temp -temperature

*
vlv -valve

*
whl -wheel

*
WIU -wheel interface unit

*
xdcr -transducer.


EFFECTIVITY BEJ ALL  32-40-00 
Page 2 
D633W101-BEJ  Jan 05/2002 


777 AIRCRAFT MAINTENANCE MANUAL
 
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