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Boeing 767 - Subtask 72-61-02-424-028-G00; Subtask 72-61-02-724-020-G00; Subtask 72-61-02-414-021-G00; Subtask 72-61-02-414-022-G00

Boeing 767
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(a) Apply a light layer of petroleum jelly, D50223 [C02-008] to the new packing.
(b) Install the packing on the groove on the outer diameter of the oil seal.
(c) Lubricate the inner diameter of the empty adapter pad with oil, D00068.
(d) Bend the oil seal three times to make it loose (and easy to install).
(e) Apply a light layer of oil, D00068 to the face of the oil seal and the face of the mating ring.
CAUTION
YOU MUST BE CAREFUL WITH THE PACKING WHEN YOU INSTALL IT.
THE PACKING IS EASILY CUT AND CAN GO OUT OF ITS POSITION
DURING INSTALLATION. IF THE PACKING IS NOT IN ITS POSITION OR
HAS DAMAGE, LEAKS WILL OCCUR.
(f) Align the oil seal with the gearbox studs.
(g) Carefully push the oil seal into the bore of the adapter pad.
(h) Apply pressure on the oil seal until it engages with the adapter pad.
(i) Install the nuts on the studs.
1) Tighten the nuts to 55-70 pound-inches (6.2-7.9 newton meters).
SUBTASK 72-61-02-424-028-G00
(3) Install the necessary component:
Component Reference
Fuel Pump PAGEBLOCK 73-11-01/401
Main Engine Control PAGEBLOCK 73-21-01/401
Starter PAGEBLOCK 80-11-01/401
Hydraulic Pump PAGEBLOCK 29-11-03/401 or PAGEBLOCK 29-11-03/
401 Config 3
IDG PAGEBLOCK 24-11-01/401 Config 3
SUBTASK 72-61-02-724-020-G00
(4) Do the lock test for the accessory gearbox (PAGEBLOCK 72-61-01/501).
SUBTASK 72-61-02-414-021-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.
(5) Close the thrust reversers (PAGEBLOCK 78-31-00/201).
SUBTASK 72-61-02-414-022-G00
(6) Close the core cowl panels (PAGEBLOCK 71-11-06/201).
SUBTASK 72-61-02-444-026-G00
(7) Do the activation procedure for the thrust reversers (PAGEBLOCK 78-31-00/201).
SUBTASK 72-61-02-414-024-G00
(8) Close the fan cowl panels (PAGEBLOCK 71-11-04/201).
END OF TASK
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-61-02
NoC
Page 407
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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