E.
Remove the Alternate Electric Motor

 S 032-051
 (1)  
Disconnect the electrical connector P203 (37) from the alternate electric motor (36).

 S 022-052

 (2)  
Remove the alternate electric motor (36) (Fig. 201):

 (a)  
Remove the three mounting bolts (35).

 (b)  
Pull the motor (36) axially to disengage the splines.

 (c)  
Remove the motor from the airplane.

 S 012-148
 (3)  
Remove the alternate electric motor seal (56) with the steps that follow (Fig. 201):

 (a)  
Use a screwdriver to remove the seal (56) from the housing.

 (b)  
Put a cover on the opening in the PDU.

 TASK 27-81-03-402-053
 5.  Alternate Electric Motor Installation_____________________________________
 A. Special Tools and Equipment
 (1)  
17MIT65B04017 Leading Edge Flap Drive Unit Lock

 B.
Consumable Materials

 (1)  
D00013 Grease - MIL-G-23827

 (2)  
C00432 Primer BMS 10-11, Type 1

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 C. Parts ~.............................................................................. | AMM | | AIPC | ................. ...........................| | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ...............................................................................| | 201 | 34 | Washer | 27-81-03 | 01 | 210 | | | 35 | Bolt | | | 200 | | | 35 | Bolt | | | 205 | | | 36 | Electric Motor (Alternate) | | | 195 | 2......…........…...................................…...........….....…........1
 D. References
 (1)  
AMM 24-22-00/201, Manual Control

 (2)  
AMM 27-81-00/201, Leading Edge Flap System

 (3)  
SSM 27-81-01, SSM 27-81-02, SSM 27-81-03, SSM 27-81-04

 (4)  
WDM 27-51-21, WDM 27-51-22, WDM 27-81-11, WDM 27-81-12, WDM 27-81-21, WDM 27-81-22, WDM 27-81-31, WDM 27-81-32

 E.
Access

 (1)  
Location Zone
 512 Krueger Flap Inboard, LH
 523 Variable Camber Flap, LH
 525 Variable Camber Flap, LH
 535 Variable Camber Flap, LH
 612 Krueger Flap Inboard, RH
 623 Variable Camber Flap, RH
 625 Variable Camber Flap, RH
 635 Variable Camber Flap, RH

 F.
Procedure

 S 422-193
 (1)  
Install the alternate electric motor seal (56) with the steps that follow (Fig. 201):

 (a)  
Apply a layer of the primer on the O/D of the seal (56).

 (b)  
Remove the cover from the PDU opening.

 (c)  
Use a guide tool to install the replacement seal (56)

 S 422-054
 (2)  
Install the alternate electric motor (Fig. 201):

 (a)  
Apply a thin layer of grease to the motor spline.

 (b)  
Engage the motor splines with the PDU.

 (c)  
Install the motor (36).

 (d)  
Install three mounting bolts (35) and washers (34).

 S 432-055
 (3)  Install the electrical connector P203 (37) (and clamp, if it is available).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 862-056
 (4)  
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P6 Main Power Distribution Panel
 1) 6L21 LE FLAP ELEC CONT GRP B DRIVE 1
 2) 6L22 LE FLAP ELEC CONT GRP A DRIVE 2
 3) 6L23 LE FLAP ELEC CONT GRP A DRIVE 3
 4) 6L24 LE FLAP ELEC CONT GRP A DRIVE 4

 (b)  
P7 Overhead Circuit Breaker Panel
　
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