(h)
Make sure the applicable bit light on the portable tester goes out for the red landing gear lights. ~........................................ | WORD | S/F | BIT | LANDING GEAR LIGHTS | .......................................... | 29 | 0 | 7 | NOSE RED | .......................................... | 29 | 0 | 6 | RIGHT RED | .......................................... | 29 | 0 | 5 | LEFT RED | 2......….....….....….....................1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
BEJ 101-112, 114-999; ú 31-24-02
ú ú 10 Page 553 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 865-172
(4)
Put the landing gear in their usual condition.
S 865-605
(5)
If you will do no more tests, then do this task:
"Put the Airplane to its Usual Condition."
TASK 31-24-02-735-150
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 865-151
(1)
Make sure you did the Prepare For Input Parameter Test task.
S 865-152
(2)
Make sure the flap system is serviceable (AMM 27-81-00/201).
S 735-153
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.
(c)
Make sure the conditions of the bit lights on the portable tester agree with the applicable values in the table.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
BEJ 101-112, 114-999; ú 31-24-02
ú ú 10 Page 554 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
~.................................................................... | 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 | | | | 61 | 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 865-154
(4) If you will do no more tests, then do this task: "Put the Airplane to its Usual Condition."
TASK 31-24-02-735-155
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 865-156
(1) Make sure you did the Prepare For Input Parameter Test task.
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