S 024-006

 (2)  
Remove the bracket.

 TASK 32-09-10-404-007
 3.  Install the Target Support Bracket for the Tilt Sensor on the Main Landing__________________________________________________________________________ Gear (Fig. 401)____
 A.  Consumable Materials
 (1)  
A00246, Sealant, Chromate - BMS 5-95 Type I

 B.  
References

 (1)  
32-00-15/201, Landing Gear Door Ground Operations and Locking Procedure

 (2)  
32-09-07/201, Main Gear Truck Tilt Sensors

 C.  
Access

 (1)  
Location Zones
 731/741 Main Landing Gear (MLG)
 732/742 MLG Body Doors
 733/743 MLG Oleo Doors

 D.  
Install the Bracket

 S 844-008
 (1)  
Do the steps that follow to install the bracket:

 (a)  
Apply the sealant to the faying surfaces.

 (b)  
Put the sealant on the threads of the bolts.

 (c)  
Install the bracket with the nuts and the bolts.

 S 944-009
 CAUTION: USE THE PROCEDURE IN AMM 32-09-07/201 TO MAKE SURE THE
_______ SENSOR/TARGET DISTANCE IS CORRECT. IF THE SENSOR/TARGET DISTANCE IS NOT IN TOLERANCE, THE AIR/GROUND RELAY SYSTEM WILL NOT OPERATE CORRECTLY.
 (2)  Make sure that the sensor/target distance is correct (Ref 32-09-07).
 

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757 MAINTENANCE MANUAL
 E. Put the Airplane Back to Its Usual Condition
 S 094-011 WARNING: USE THE PROCEDURE IN AMM 32-00-15/201 TO REMOVE THE DOOR LOCKS.
_______ THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (1)  Remove the door locks from the landing gear doors and close the doors (Ref 32-00-15).
 

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757 MAINTENANCE MANUAL
 MAIN LANDING GEAR AND DOORS - DESCRIPTION AND OPERATION
_______________________________________________________
 1.  General_______
 A.  The main landing gear consists of two main gears (Ref 32-11-00) which absorb landing, taxiing, and take-off loads and support the airplane while on the ground. The gears are located on each side of the airplane and are mounted between the rear wing spar and the main landing gear beam. During flight, the gears retract inboard into the wing cavities and fuselage wheel wells and are covered by doors (Ref 32-12-00). The doors fair into the airplane body contour to reduce aerodynamic drag.
 

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757 FAULT ISOLATION/MAINT MANUAL
MAIN LANDING GEAR AND DOORS
COMPONENT  SHT 102 FIG.  QTY  ACCESS/AREA  REFERENCE 
BEARING - MAIN GEAR AFT TRUNNION  2  2  MAIN LANDING GEAR  32-11-01 
BEARING - MAIN GEAR FORWARD TRUNNION  2  2  MAIN LANDING GEAR  32-11-01 
DOOR - MAIN GEAR  2  2  GEAR WHEEL WELL OF THE MAIN LANDING  32-12-01 
DOOR - MAIN GEAR STRUT  1  2  MAIN LANDING GEAR  32-12-04 
DOOR - MAIN GEAR TRUNNION FAIRING  2  2  MAIN LANDING GEAR  32-12-10 
GEAR - MAIN  1 & 2  2  MAIN LANDING GEAR  32-11-01 
LINK - MAIN GEAR LOWER DOWNLOCK  1  2  MAIN LANDING GEAR  32-11-13 
　
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本文鏈接地址：757 AMM 飛機維護手冊 起落架 CHAPTER 32 - LANDING GEAR 1(73)