737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 6(171)

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 12) S6 F EXT GAP FAR
 13) F1 EXT GAP NEAR
 14) F1 RET GAP FAR
 15) F2 EXT GAP NEAR
 16) F2 RET GAP FAR
 17) F3 EXT GAP NEAR
 18) F3 RET GAP FAR
 19) F4 EXT GAP NEAR
 20) F4 RET GAP FAR

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH POSITION INDICATION ú

 27-88-41
 MODULE WITH BUILT-IN-TEST EQUIMENT  ú ú 01 Page 507 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 E.  Position Indication Module Built-In-Test-Equipment (BITE) Test for Fault History
 S 865-025
 (1)  
Put the flap control lever to the full up detent position.

 (a)  
Make sure the leading edge indication shows the flaps and slats are up.

 S 745-029
 (2)  
Push the menu key until you find EXISTING FAULTS?.

 S 745-030

 (3)  
Push the down arrow key until you find FAULT HISTORY?.

 S 745-031

 (4)  
Push the YES button to enter menu selection.

 S 745-032

 (5)  
Push the YES button when you see LE FL/SL CYC 0?.

 S 745-035

 (6)  
Make sure the display shows NO FAULTS?.

 (a)  
If a fault is found, correct the problem then cycle the flaps and slats two times to clear the fault history.

 S 745-034
 (7)  
Push the ON/OFF key to stop the BITE test.

 F.  
Put the Airplane Back to Its Usual Condition

 (1)  
Release pressure from hydraulic system B (27-81-00/201).

 (2)  
Remove electrical power (AMM 24-22-00/201).

 S 865-001
 S 865-002
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH POSITION INDICATION ú

 27-88-41
 MODULE WITH BUILT-IN-TEST EQUIMENT  ú ú 01 Page 508 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.

 

 

　
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