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时间:2011-04-13 07:45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

 (a)  
Do not lock the turnbuckles.

 (b)  
Make sure that rig pins NS-1, 2, 3, 4, 5, 6, and R-3 are loose.

 (c)  
Remove rig pins NS-1, 2, 3, 4, 5, 6 and R-3.

 (d)  
Make sure the nose gear ground door release handle is in the down and locked position.

 (e)  
Make sure the landing gear control handle is in the "DOWN" position.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-51-00
 ALL  ú ú 01 Page 510 ú Feb 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 865-116
 WARNING:_______ MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
 SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER.  AILERONS, RUDDERS,
 ELEVATORS, FLAPS,SPOILERS,LANDING GEAR, AND THRUST REVERSERS
 CAND MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER.  THIS CAN
 CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.

 (11)
 AIRPLANES WITH NEW CABLES; Provide system No. 1 hydraulic power (AMM 29-11-00/201).

 S 715-019

 (12)
 AIRPLANES WITH NEW CABLES; Cycle the left and right tillers through | 150 degrees for 15 strokes.

 S 865-020

 (13)
 AIRPLANES WITH NEW CALBES; Remove system No. 1 hydraulic power (AMM 29-11-00/201).

 (a)
Install rig pins NS-1, 2, 3, 4, 5, 6 and R-3.


 S 835-021
 (14)
 Rig the NWS1A/NWS1B cables per the data shown on sheet 3, Fig. 502.

 (a)
Do not lock the turnbuckles.


 S 835-117
 (15)
 Rig the NWS2A/NWS2B cables to 60 (| 10) pounds at all temperatures.

 S 715-022

 (16)
 Make sure that all rig pins are loose.

 S 095-023

 (17)
 Remove rig pins NS-1, 2, 3, 4, 5, 6 and R-3.


 S 865-118
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS, ELEVATORS, FLAPS,SPOILERS,LANDING GEAR, AND THRUST REVERSERS CAND MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (18)
 Provide system No. 1 hydraulic power (AMM 29-11-00/201).

 (19)
 Cycle both tillers through | 150 degrees for 3 strokes.

 (20)
 Remove system No. 1 hydraulic power (AMM 29-11-00/201).


 S 865-025
 S 865-027
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-51-00
 ALL  ú ú 01 Page 511 ú Feb 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A


 
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本文链接地址:747-400 AMM 飞机维护手册 起落架 LANDING GEAR 7(184)