(b) Cure the repair at 135°-150°F (57°-66°C) for 1 hour.
(c) When the repair material is hard (before the cure time is over), use a razor blade or sharp
knife to trim the repair material.
1) Trim the repair material to 1/16 inch (0.6 mm) above (or the same level) the
adjacent area.
(d) After the cure time, file or sand the repair material to the same level as the adjacent area.
G. Put the Airplane to its Usual Condition
SUBTASK 72-33-05-948-012-G00
(1) Remove the protective mats from the inlet cowl.
SUBTASK 72-33-05-418-013-G00
(2) Install the fan rotor blades (PAGEBLOCK 72-31-02/401).
SUBTASK 72-33-05-418-014-G00
(3) Install the fan rotor spinner (PAGEBLOCK 72-31-01/401).
SUBTASK 72-33-05-868-015-G00
(4) 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 72-33-05-868-016-G00
(5) 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
END OF TASK
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-33-05
NoC
Page 804
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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