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 (1)  Drill a hole in the wing tip navigation light window at all fastener locations (Fig. 401).
 NOTE:____Use a drill speed of 1200 to 1500 RPM. Cutters should be kept at a near room temperature when drilling successive holes.
 S 324-026-B00
 (2)  Use the file to make a chamfer at each fastener hole location (Fig. 401).
 TASK 57-21-11-404-013-B00
 4.  Wing Tip Installation (Fig. 401)_____________________
 A. Consumable Materials
 (1)  
A00136 Sealant - BMS 5-19, Class B

 (2)  
A00230 Coating Compound - BMS 5-37

 (3)  
A00247 Aerodynamic Smoother - BMS 5-95, Class B 1/2

 B. References
 (1)  
AMM 33-43-00/501, Steady Position (Navigation) Lights

 (2)  
AMM 33-43-11/201, Steady Position (Navigation) Lights - Maintenance Practices.

 (3)  
AIRPLANES WITH STROBE POSITION LIGHTS; AMM 33-45-11/201, Wingtip Strobe Postion Lights - Maintenance Practices

 (4)  
AIRPLANES WITH LOGO LIGHTS; AMM 33-49-00/201, Logo Lights - Maintenance Practices

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A
737-300/400/500MAINTENANCE MANUAL
 (5)  AMM 51-31-00/201, Seals and Sealing
 C. Access
 (1)  Location Zone
 301, 401 Wing Tip

 D. Procedure
 S 394-006-B00
 (1)  
Do this task: "Faying Surface Seal Application" (AMM 51-31-00/201).

 S 424-007-B00

 (2)  
Install the aft fairing.

 (a)  
Put the aft fairing in its position on the closure rib.

 (b)  
Install the fasteners to attach the aft fairing to the closure rib.

 (c)  
Install the wires into the wire tube for the tail light in the aft fairing.

 (d)  
Attach the navigation light bracket to the rib on the aft fairing.

 (e)  
Install the white steady position (navigation) lights.

 

 S 424-008-B00
 (3)  Install the middle fairing.
 (a)  
Put the middle fairing in its position on the closure rib and the splice.

 (b)  
Install the fasteners.

 S 424-017-B00
 (4)  
Install the access panel.

 S 424-009-B00

 (5)  
Install the forward fairing.

 (a)  
Put the forward fairing in its position on the closure rib.

 (b)  
Install the fasteners on the forward fairing.

 

 S 394-010-B00
 (6)  Do this task: "Aerodynamic Smoother Application"
 (AMM 51-31-00/201).

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A
737-300/400/500MAINTENANCE MANUAL
 S 864-018-B00
 (7)  
Remove the DO-NOT-CLOSE tags from the circuit breakers and close all of the circuit breakers for the lights in the wingtip (AMM 33-43-11/201, AMM 33-45-11/201, AMM 33-49-00/201).

 S 704-019-B00

 (8)  
Do a check of the lights in the wingtip as follows:

 (a)  
Do this task: "Steady Position (Navigation) Lights Test" (AMM 33-43-00/501).

 (b)  
Do this task: "Logo Lights Test" if installed
 (AMM 33-49-00/201).

 (c)  
Do this task: "Wingtip Strobe Position Lights Test", if installed (AMM 33-45-11/201).

 

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本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 機(jī)翼 WINGS(15)