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Boeing 767 - Subtask 72-35-00-418-096-G00; Subtask 72-35-00-948-097-G00; Subtask 72-35-00-868-098-G00; Subtask 72-35-00-848-099-G00

Boeing 767
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(b) Apply a thin layer of Esnalube 382 Lubricant, D50071 [C02-006] to the retainer screw
threads.
CAUTION
DO NOT USE A HAMMER OR MALLET TO PUT THE ACOUSTICAL LINER
SECTIONS IN THEIR POSITIONS. YOU CAN EASILY CAUSE DAMAGE
TO THE ACOUSTICAL LINER SECTIONS.
(c) Put the acoustical liner in position and engage the acoustical liner in the fan case.
1) Tighten the retainer screws to 55-70 pound-inches (6.2-7.9 Newton meters).
(d) Apply black silicone RTV Silicone Elastomer adhesive, A50311 [C01-006] to the areas
around the acoustical liner.
1) Make sure the adhesive is at the same height as the adjacent surfaces.
SUBTASK 72-35-00-418-096-G00
(6) Install the B1-0 borescope plug (Figure 803) as follows:
(a) Apply a light layer of antiseize compound on the threads and the pressure faces of the
plug.
(b) Install the borescope plug into the borescope port.
1) Tighten the plug to 40-60 pound-inches (4.5-6.8 Newton meters).
(c) Install lockwire.
SUBTASK 72-35-00-948-097-G00
(7) Remove the N2 rotor manual or pneumatic cranking system (PAGEBLOCK 72-00-00/201).
SUBTASK 72-35-00-868-098-G00
(8) Adjust the VSV system to the fully closed position (PAGEBLOCK 75-31-02/501).
SUBTASK 72-35-00-848-099-G00
(9) If no more work will be done at this time, do the task "Put the Airplane to its Usual Condition".
END OF TASK
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-35-00
NoC
Page 815
D633T1B7 Aug 22/2017
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ABX 001-007, 011, 012, 016-019, 021, 022, 025, 101,
109, 114, 115, 314-999

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