TASK 76-11-01-844-001-C01
2. Thrust Lever Removal Preparation________________________________
A. Equipment
(1)
Assembly - Rig Pin, F70207-11, Component of Rig
Pin Kit F70207-93. Optional: MS20392-4C pin
(or equivalent 0.311 +0.000/-0.002-inch
diameter, 6-inch long rod or bolt)
(2)
Set - Thrust Lever Dowel, Control Stand,
F80195-1
B. References
(1)
AMM 12-31-11 201, Body Section 41 Access Doors and Panels
(2)
AMM 27-09-14/201, Flight Control Cables
(3)
AMM 29-15-00/201, Hydraulic Systems A, B, and Standby
(4)
AMM 76-11-04/201, Engine Control Cables
C. Access
(1)
Location Zones
101 Control Cabin - Left
102 Control Cabin - Right
202 Lower Nose Compartment
205 Electronic Compartment
(2)
Access Panel
1201 Electronic Equipment Access Door
D. Procedure
S 634-002-C01
(1)
Remove hydraulic power (AMM 29-15-00/201).
S 864-003-C01
(2)
Put the two thrust levers in the IDLE position and attach the cables with a clamp.
S 864-004-C01
(3)
Put the two start levers in the CUTOFF position and attach the cables with a clamp.
(4)
Open the access door of the nose compartment.
S 864-006-C01
(5)
Release the tension on the flap control cables, WFA and WFB:
S 014-005-C01
(a) Loosen the turnbuckles in the lower nose compartment (AMM 27-09-14/201 for turnbuckle location).
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76-11-01
STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 401 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 834-007-C01
(6)
Install a rig pin through the control drum of the forward speed brake into the structure (Fig. 401).
S 864-009-C01
(7)
In the lower nose compartment, adjust the forward and aft support links to lift the forward mechanism and to release the tension in the trim chain assembly (Fig. 402).
S 014-010-C01
(8)
Open the access door No. 1201 to the electronic equipment bay (AMM 12-31-11/201).
S 864-011-C01
(9)
Release the tension on the thrust control cables T1A, T1B, T2A, and T2B:
(a)
Loosen the turnbuckles in the electronic equipment compartment (AMM 76-11-04/201 for turnbuckle location).
(b)
Disconnect and tags the cables for the applicable thrust lever.
S 864-013-C01
(10) Loosen the turnbuckles in the forward cargo compartment to release the tension on the cables for engine start control ESS1A, ESS1B, ESS2A and ESS2B (AMM 76-11-04/201 for turnbuckle location).
TASK 76-11-01-004-014-C01
3. Thrust Lever Removal
____________________
A. Access
(1) Location Zones
101 Control Cabin - Left
102 Control Cabin
B. Procedure
S 034-015-C01
(1) Remove the tie rod nut (7) from the control wheel (6, Fig. 403).
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