Condition Maximum Serviceable Limits
Cracks Not permitted.
Nicks, dents and scratches Permitted, if less than 0.035 inch (0.89 mm) in depth.
SUBTASK 72-62-01-216-002-G00
(2) Visuallly examine the housing studs for the conditions that follow:
Condition Maximum Serviceable Limits
Bent Not permitted.
Loose Not permitted.
SUBTASK 72-62-01-216-003-G00
(3) Visually examine the lube fittings and the plugs for the conditions that follow:
Condition Maximum Serviceable Limits
Leakage Not permitted. Tighten the fitting or replace the packing.
SUBTASK 72-62-01-216-004-G00
(4) Visually examine the fluid fitting insert at the lube supply for the conditions that follow:
Condition Maximum Serviceable Limits
Loose Not permitted.
Leakage Not permitted.
E. Put the Airplane to its Usual Condition
SUBTASK 72-62-01-416-009-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 reversers (PAGEBLOCK 78-31-00/201).
SUBTASK 72-62-01-416-010-G00
(2) Close the core cowl panels (PAGEBLOCK 71-11-06/201).
SUBTASK 72-62-01-446-011-G00
(3) Do the activatiion procedure for the thrust reverser (PAGEBLOCK 78-31-00/201).
SUBTASK 72-62-01-416-012-G00
(4) Close the fan cowl panel (PAGEBLOCK 71-11-04/201).
END OF TASK
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-62-01
NoC
Page 602
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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