S 865-595
(5)
If you will do no more tests, then do this task:
"Put the Airplane to its Usual Condition."
TASK 31-24-01-735-596
43. Leading Edge Flap Position Signals Test_______________________________________
A. Reference
(1) AMM 27-81-00/201, Leading Edge Flap and Slat
B. Access
(1) Location Zones
101 Control Cabin - Left
102 Control Cabin - Right
C. Procedure
S 865-597
(1)
Make sure you did the Prepare For Input Parameter Test task.
S 865-598
(2)
Make sure the flap system is serviceable (AMM 27-81-00/201).
S 735-599
CAUTION: MAKE SURE THE THRUST REVERSER COWLS (C-DUCTS) ARE IN THE CLOSED
_______ POSITION BEFORE YOU DO THIS TEST. YOU CAN CAUSE DAMAGE TO THE FLAPS AND COWLS IF THE COWLS ARE OPEN WHEN THE FLAPS EXTEND.
(3) Do this test of the signals from the leading edge flaps:
(a)
Move the flaps to get the conditions shown in the table.
(b)
Set the portable tester to the SUBFRAMEs and WORDs shown in the table.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. BEJ 113 ú
31-24-01
ú ú 13B Page 555 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(c) Make sure the conditions of the bit lights on the portable tester agree with the applicable values in the table.
~.................................................................... | FLAP | | | | FLAP LIGHT | BIT | BIT LIGHT | | NUMBER | S/F | WORD | FLAP LIGHT | STATE | LIGHT | STATE | ...................................................................... | 1 | 0 | 33 | IN TRANSIT | OFF | 1 | ON | | | | | IN TRANSIT | ON | | OFF | | | | 33 | FULL EXTEND | OFF | 2 | ON | | | | | FULL EXTEND | ON | | OFF | ...................................................................... | 2 | 0 | 38 | IN TRANSIT | OFF | 1 | ON | | | | | IN TRANSIT | ON | | OFF | | | | 35 | FULL EXTEND | OFF | 1 | ON | | | | | FULL EXTEND | ON | | OFF | ...................................................................... | 3 | 0 | 39 | IN TRANSIT | OFF | 2 | ON | | | | | IN TRANSIT | ON | | OFF | | | | 41 | FULL EXTEND | OFF | 2 | ON | | | | | FULL EXTEND | ON | | OFF | ...................................................................... | 4 | 0 | 39 | IN TRANSIT | OFF | 1 | ON | | | | | IN TRANSIT | ON | | OFF | | | | 41 | FULL EXTEND | OFF | 1 | ON | | | | | FULL EXTEND | ON | | OFF | 2........….....…......….............…............….......…...........1
S 865-600
(4) If you will do no more tests, then do this task: "Put the Airplane to its Usual Condition."
TASK 31-24-01-735-601
44. Leading Edge Slat Position Signals Test_______________________________________
A. References
(1)
AMM 27-81-00/201, Leading Edge Flap and Slat
(2)
AMM 29-00-00/201, Hydraulic Power
B. Access
(1) Location Zones
101 Control Cabin - Left
102 Control Cabin - Right
C. Procedure
S 865-602
(1) Make sure you did the Prepare For Input Parameter Test task.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. BEJ 113 ú
31-24-01
ú ú 22B Page 556 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 儀表 INSTRUMENTS(49)
