747-400 AMM 飞机维护手册 SERVICING 1(63)

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_______ OF THE MAIN LANDING GEAR AT THE SAME TIME. THE AIRPLANE CAN FALL TO THE SIDE IF YOU PRESSURIZE THEM INCORRECTLY.
 DO NOT PRESSURIZE THE MAIN LANDING GEAR TO MORE THAN 2000 PSI. TOO MUCH PRESSURE CAN CAUSE DAMAGE TO THE SEALS IN THE SHOCK STRUT.
 (a)  
Use the service manifold assembly or the strut inflation tool to pressurize the shock struts through the air valves.

 (b)  
Add gas (nitrogen or dry air) to each shock strut until dimension X is approximately 14.00 inches.

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 613-056
 (10) Adjust each shock strut until each pressure agrees with the servicing chart:
 (a)  
Measure dimension X.

 (b)  
Read the air pressure on the pressure gage.

 (c)  
Add or release gas until dimension X and the pressure are in the band on the servicing chart.

 S 433-009
 (11) Close the air charging valve.
 (a)  
Remove the hoses of the service manifold assembly from the air valves.

 (b)  
Tighten the swivel nut to 60-84 pound-inches.

 S 433-021
 (12)
 Install the pressure caps on the air valves of each main gear.

 S 613-010

 (13)
 After 5-10 landings, measure dimension X and read the pressure on the pressure gages of the wing landing gears.

 (a)  Add or release gas until dimension X and the pressure are in the band on the servicing chart.
 NOTE: It is not necessary to adjust the body landing gear and
____
 the nose landing gear again.

 S 093-029
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASKS BELOW TO REMOVE
_______ THE DOOR LOCKS ON THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT INSTALL THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (14) Do this task:  "Removal of the Door Locks from the Wing Landing Gear" (AMM 32-00-30/201).
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 12-15-03
 ALL  ú ú 03 Page 307 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 093-030
 (15) Do this task:  "Removal of the Door Locks from the Body Landing Gear" (AMM 32-00-30/201).
 TASK 12-15-03-603-012
 3.  Shock Strut Servicing Fast Check________________________________
 A. General
 (1)  
This task provides a fast check of the landing gear shock struts. This check will help you determine if the struts are serviceable for dispatch. It must be completed at or near dispatch weight. It is not accurate at or near empty weight.

 (2)  
This task also provides steps to do the minimum servicing necessary to allow the airplane to dispatch.

 B. Access
 (1)  Location Zone
 715 Nose Landing Gear
 735 Wing Landing Gear, LH
 745 Wing Landing Gear, RH
 755 Body Landing Gear, LH
 765 Body Landing Gear, RH

 C. Procedure (Fig. 301)
 S 223-024
 CAUTION: DO A FULL SERVICING TO THE LANDING GEAR ON ALL AIRPLANES WHICH
_______ DO NOT COMPLETE THIS FAST CHECK PROCEDURE CORRECTLY. DO NOT DO THE SERVICING WITH THE DIMENSIONS OF THE FAST CHECK AS AN ALTERNATIVE FOR A FULL SERVICING. A LANDING GEAR WHICH HAS INCORRECT SERVICING CAN HAVE A FAILURE DURING OPERATION.
 (1)  Do a fast check of the landing gear:
 (a)  
Make sure there is no evidence of major fluid leakage.

 (b)  
Make sure the differences between the extended lengths of each inner cylinder is not more than 2 inches.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú ú 03 Page 308 ú Oct 18/01
　
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