(2)
Position feedback control lever so that rig pin hole in lever aligns with rig pin hole in support.
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May 01/03 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 78-32-201 Page 501
H29322
Thrust Reverser Linkage Adjustment 500
78-32-201 Figure 501 Aug 15/69
Page 502
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
(3)
Insert rig pin.
(4)
Adjust feedback control rod and control link rod ends until feedback control link rod end can be attached to lever. Bolt must be inserted freely.
(5)
Check to see that thread engagement of two rod ends is approximately equal and that rod ends are aligned with each other.
(6)
Check that rig pin can be removed and inserted without binding and remove pin.
(7)
Reactivate thrust reverser hydraulic system by removing ground locks from both thrust reverser isolation valves.
(8)
Operate thrust reverser through one cycle, and verify that rig pin can be inserted an d removed freely.
WARNING: PERSONNEL MUST STAY CLEAR OF THRUST REVERSER WHEN IT IS ACTUATED TO PREVENT BEING CAUGHT BY ROTATING DEFLECTOR DOORS.
G. Install feedback control access panel.
H. Check deflector door adjustment per 78-32-112.
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Nov 15/70 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 78-32-201 Page 503
TAILPIPE EXTENSION -REMOVAL/INSTALLATION
General
A. The tailpipe extension forward mounting flange is attached to the engine, the thrust reverser is attached to the tailpipe extension aft mounting flange. Forty two bolts are used at each flange. The reverser is normally removed and installed at the tailpipe extension aft mounting flange and the tailpipe extension then removed from the engine. However, the extension with reverser attached may be removed as a unit if desired.
2. Equipment and Materials
CAUTION: DO NOT USE CADMIUM-PLATED TOOLS ON TITANIUM COMPONENTS WHICH ARE SUBJECTED TO HIGH TEMPERATURES. CADMIUM REACTS WITH TITANIUM AT HIGH TEMPERATURES AND MAY CAUSE EMBRITTLEMENT AND CRACKS IN TITANIUM PARTS.
A. Antiseize Compound -Ease-Off 990, Texacone Corp., Dallas 8, Texas, or equivalent
B. Cart Assembly - F80101 or equivalent
C. Sling Assembly - F80110-1 or equivalent
D. Thrust Reverser Isolation Valve Ground Lock Cap and Pin Assembly - F80109-3 or F80109-9 or equivalent
3. Prepare for Removal
A. Check that thrust reverser deflector doors are stowed and locked.
B. Deactivate thrust reverser hydraulic system by installing ground locks on both thrust reverser isolation valves.
WARNING: SERIOUS INJURY CAN RESULT TO PERSONNEL IF GROUND LOCKS ARE NOT PROPERLY INSTALLED. ATTEMPT TO DEPLOY THRUST REVERSERS AFTER INSTALLING GROUND LOCKS. REVERSERS SHOULD NOT DEPLOY.
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May 01/03 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 78-32-211 Page 401
C. Remove engine side cowl panels per 71-11-11 and tailpipe fairings per 78-32-162.
D. Remove thrust reverser, if reverser and extension are not to be removed as a unit,
per 78-32-101.
4. Remove Tailpipe Extension
A. Disconnect push-pull cable at quick disconnect (Fig. 401).
B. Disconnect electrical connector on forward side of tailpipe extension bulkhead.
C. Provide support to hold unit in position when mounting bolts are removed. Tailpipe extension with thrust reverser attached weighs approximately 488 pounds. Extension alone weighs approximately 96 pounds.
D. Remove bolts attaching tailpipe extension to engine exhaust flange.
E. Carefully lower unit just enough to provide access to fittings and disconnect hydraulic lines at top side of fixed fairing. Cap disconnected lines.
F. Lower unit clear of engine.
Install Tailpipe Extension
A. Raise tailpipe extension to a position that will permit connection of hydraulic lines. Remove caps and connect lines at top side of fixed fairing (Fig. 401). Tighten fittings 250 to 300 pound-inches.
B. Raise unit to installed position and install bolts attaching tailpipe extension to engine exhaust flange. Tighten bolts 130 to 200 pound-inches.
C. Connect electrical connector on forward side of tailpipe extension bulkhead.
D. Connect push-pull cable at quick disconnect.
E. Install thrust reverser, if required, per 78-32-101.
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