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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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