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Boeing 767 - Subtask 72-33-04-216-020-G00; Subtask 72-33-04-416-021-G00; Subtask 72-33-04-416-022-G00; Subtask 72-33-04-416-023-G00

Boeing 767
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Table 601/72-33-04-993-801-G00 (Continued)
Condition Maximum Serviceable Limits
Fretting and high metal Permitted, if the damage is less than 0.003 inch (0.08 mm) after you remove the
high metal. Blend the damage as close to the initial contour as it is possible.
Pylon mount nuts that are damaged Not permitted.
SUBTASK 72-33-04-216-020-G00
(13) Visually examine the fan stator case (4th stage) for the conditions that follow:
Condition Maximum Serviceable Limits
Teflon rub strip that is delaminated or
gone
Permitted. Cut away all the loose teflon material.
F. Put the Airplane to its Usual Condition
SUBTASK 72-33-04-416-021-G00
WARNING
OBEY THE INSTRUCTIONS IN THE PROCEDURE TO CLOSE THE THRUST
REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO
PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
(1) Close the thrust reverser (PAGEBLOCK 78-31-00/201).
SUBTASK 72-33-04-416-022-G00
(2) Close the core cowl panel (PAGEBLOCK 71-11-06/201).
SUBTASK 72-33-04-416-023-G00
(3) Close the fan cowl panel (PAGEBLOCK 71-11-04/201).
SUBTASK 72-33-04-446-024-G00
(4) Do the activation procedure for the thrust reverser (PAGEBLOCK 78-31-00/201).
END OF TASK
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-33-04
NoC
Page 608
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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