ABX 001-007, 011, 012, 016-019, 021, 022, 025, 101, 109, 114, 115, 314-999 POST SB
CF6-80A-72-0438
SUBTASK 72-00-00-286-198-G00
(15) Examine the high pressure turbine rotor thermal shield for the condition that follows:
NOTE: Use the eddy-current equipment (Ref CF6-80A Non-Destructive Test Manual, GEK
72502).
Condition Maximum Serviceable Limit
Cracks Not permitted.
ABX 001-007, 011, 012, 016-019, 021, 022, 025, 101, 109, 114, 115, 314-999
SUBTASK 72-00-00-416-199-G00
(16) Install the ECS duct (Figure 601).
SUBTASK 72-00-00-416-200-G00
(17) If it is necessary, do the steps that follow to put the airplane to its usual condition:
NOTE: Do not do these steps if you will continue the inspection at this time.
(a) Remove the equipment that you used to turn the N2 rotor (PAGEBLOCK 72-00-00/201).
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.
(b) Close the thrust reversers (PAGEBLOCK 78-31-00/201).
(c) Close the core cowl panels (PAGEBLOCK 71-11-06/201).
(d) Do the activation procedure for the thrust reverser (PAGEBLOCK 78-31-00/201).
(e) Close the fan cowl panels (PAGEBLOCK 71-11-04/201).
END OF TASK
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-00-00
NoC
Page 698.2
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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