EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-21-04
 ALL  ú ú 01 Page 408 ú Jun 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 TASK 32-21-04-404-020
 3.  Nose Landing Gear Drag Strut Installation (Fig. 401)_________________________________________
 A. Special Tools and Equipment
 (1)  
20HME65B01462 Nose Landing Gear Drag Strut Hoisting Tool

 (2)  
PRE65B01202-1 Protective Equipment for Tripod Apex Pin

 B.
Consumable Materials

 (1)  
D00633 Grease - BMS 3-33 (preferred)

 (2)  
D00013 Grease - MIL-G-23827 (optional)

 (3)  
B00722 Solvent - PD-680 or Equivalent cleaning solvent

 C.
References

 (1)  
AMM 07-11-02/201, Jacking Airplane Nose

 (2)  
AMM 09-11-00/201, Towing

 (3)  
AMM 12-21-01/301, Landing Gear

 (4)  
AMM 32-00-30/201, Landing Gear Door Locks

 (5)  
AMM 32-21-05/601, Nose Gear Tripod Brace Assembly

 (6)  
AMM 32-34-00/501, Nose Gear and Door Extension and Retraction

 (7)  
AMM 32-34-02/601, Nose Gear Locking Mechanism

 (8)  
AMM 32-35-05/401, Nose Landing Gear Alternate Extension Drive Unit

 (9)  
AMM 32-61-03/201, Nose Gear Lock Sensor

 (10)
 AIPC 32-21-04 Fig. 1

 (11)
 AIPC 32-21-05 Fig. 1

 (12)
 AIPC 32-34-01 Fig. 2,

 (13)
 AIPC 32-34-02 Fig. 2

 (14)
 AIPC 32-35-62 Fig. 1

 D.
Access

 (1)  
Location Zone
 715 Nose Landing Gear

 E.
Prepare the Procedure

 (1)
Install the ground locks in all landing gear (AMM 09-11-00/201).

 S 494-041
 S 494-042
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO INSTALL
_______ 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.
 (2)  Do this task: "Installation of the Door Locks on the Nose Landing Gear" (AMM 32-00-30/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-21-04
 ALL  ú ú 01 Page 409 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 114-023
 (3)  
Clean all bolts, nuts, washers and all bearing surfaces with solvent.

 S 224-024

 (4)  
Examine the parts and the fittings for worn areas (AMM 32-21-05/601 and AMM 32-34-02/601).

 S 644-025

 (5)  
Lubricate all bolts, washers and bearing surfaces before you install the parts.

 NOTE: The torque in this procedure will be dry, unless the
____
 procedure will specify a different torque.

 F. Install the Drag Strut
 S 494-027
 (1)  
Use a drag strut sling to hold the strut in its position.

 S 424-028

 (2)  
Install the upper drag strut on the support fitting.

 (a)  
Install the pivot shaft (16) of the drag strut to attach the upper drag strut to support fittings.

 (b)  
Move the release shaft (13) of the emergency downlock into the downlock release shaft (14).

 (c)  
Set the two shafts into the pivot shaft (16) of the drag strut.

 (d)  
Install the actuator crank fitting (12) on the release shaft (13) of the emergency downlock.

 (e)  
Install the crank (12) with the lockbolt (19) and tighten the nut 30 - 40 pound-inches.

 (f)  
Install the downlock crank fitting (11) and the emergency downlock coupling (18) on the release shaft (13) of the emergency downlock.

 (g)  
Install the washer (21) and the castellated nut (22).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊(cè) 起落架 LANDING GEAR 3(139)