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时间:2011-04-03 11:42来源:蓝天飞行翻译 作者:航空
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 (1)  Location Zone
 201 Radome

 D. Procedure (Fig. 401)
 S 114-005-B00
 (1)  
Clean the nose radome surface where you will install the director bar with aliphatic naphtha.

 S 374-006-B00

 (2)  
Apply one layer of the primer to the surface where you will install the director bar.

 S 114-007-B00

 (3)  
Clean the surface with the solvent.

 S 424-008-B00

 (4)  
Install the director bar.

 (a)  
Cut a 13-inch long strip of the aluminum foil tape.

 (b)  
Install the tape as shown in Fig. 401.

 (c)  
Push the tape correctly into its location.

 


 S 424-009-B00
 (5)  
Install the M1458 decal on the radome as shown in Fig. 401 if it is not installed.

 S 414-010-B00

 (6)  
Do this task to close the nose radome: "Install Nose Radome" (Ref/53-52-00/401).

 S 864-011-B00

 (7)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:


 (a)  P18 Load Control Center - Left
 1) WEATHER RADAR AC
 2) WEATHER RADAR DC

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 53-52-31
 ALL  ú ú B01 Page 403 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 TAIL CONE - REMOVAL/INSTALLATION
________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is one task for the removal and one task for the installation of the tail cone. The procedure has these parts:
 (1)  
The movement of the stabilizer

 (2)  
The removal of the access panels

 (3)  
The removal of the APU exhaust duct and the aft fairing

 (4)  
The removal of a stabilizer or the two elevators.

 (5)  
The removal of the tail cone

 (6)  
The installation of the tail cone

 (7)  
The installation of the APU exhaust duct and the aft fairing

 (8)  
The installation of the access panels.


 TASK 53-53-00-004-001-B00
 2.  Tail Cone Removal_________________
 A.  Standard Tools and Equipment
 (1)  Protective Plastic Shield
 B.  References
 (1)  
27-21-17/401, Rudder Index Plate

 (2)  
27-31-11/401, Elevator

 (3)  
27-31-81/401, Elevator Index Plate

 (4)  
27-41-11/401, Horizontal Stabilizer

 (5)  
49-81-11/401, Exhaust Duct Muffler

 (6)  
49-81-31/401, Aft Fairing Assembly


 C.  Access
 (1)  
Location Zone
 704 Tail Cone


 (2)  
Access Panels
 3801/3802 Tail Cone Access Doors

 

 D.  Prepare to Remove the Tail Cone
 S 864-002-B00
 (1)  Move the stabilizer to the leading edge down position and the elevators to the up position.
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 53-53-00
 ALL  ú ú B02 Page 401 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 494-027-B00
 (2)  
Install the plastic shield on the tail cone.

 S 864-004-B00

 (3)  
Open these circuit breakers and install DO-NOT-CLOSE tags:


 (a)  P18 Load Control Center Left
 1) ACC COMP LITS
 2) NAV LT (if applicable)

 S 014-005-B00
 (4)  
Remove the access panels 3801 and 3802.

 S 014-006-B00

 (5)  
Do this task: "Remove the Aft Fairing Assembly (With the APU in Position)" (Ref 49-81-31/401).

 S 014-007-B00

 (6)
Do this task: "Remove Exhaust Duct Muffler" (Ref 49-81-31/401).

 S 014-008-B00

 (7)  
 
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