F. Put the Airplane to Its Usual Condition
SUBTASK 72-33-05-414-017-G00
(1) Install the fan blades (PAGEBLOCK 72-31-02/401).
SUBTASK 72-33-05-414-018-G00
(2) Install the fan rotor spinner (PAGEBLOCK 72-31-01/401).
SUBTASK 72-33-05-864-019-G00
(3) For the left engine, remove the safety tag and close this circuit breaker:
Circuit Breaker Panel, P11
Row Col Number Name
D 19 C01510 ENGINE START,LEFT CONT
SUBTASK 72-33-05-864-020-G00
(4) For the right engine, remove the safety tag and close this circuit breaker:
Circuit Breaker Panel, P11
Row Col Number Name
D 20 C01511 ENGINE START,RIGHT CONT
SUBTASK 72-33-05-944-021-G00
(5) Remove the protective mat, STD-6378 from the inlet cowl.
SUBTASK 72-33-05-414-022-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.
(6) Close the thrust reverser (PAGEBLOCK 78-31-00/201).
SUBTASK 72-33-05-414-023-G00
(7) Close the core cowl panel (PAGEBLOCK 71-11-06/201).
SUBTASK 72-33-05-414-024-G00
(8) Do the activation procedure for the thrust reverser (PAGEBLOCK 78-31-00/201).
SUBTASK 72-33-05-414-025-G00
(9) Close the fan cowl panels (PAGEBLOCK 71-11-04/201).
END OF TASK
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-33-05
NoC
Page 408
D633T1B7 Apr 22/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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