Boeing 767 - Subtask 72-00-00-986-207-G00; Subtask 72-00-00-016-208-G00; Subtask 72-00-00-016-209-G00; Subtask 72-00-00-016-210-G00

F. Procedure
SUBTASK 72-00-00-986-207-G00
(1) Turn the N2 rotor at the accessory gearbox (PAGEBLOCK 72-00-00/201).
NOTE: It is recommended that you turn the N2 rotor, then stop to do the inspection. Then, turn
the N2 rotor, and stop again to do the next inspection.
SUBTASK 72-00-00-016-208-G00
(2) If it is necessary, do the steps that follow to prepare for the borescope inspection:
WARNING
DO THE THRUST REVERSER DEACTIVATION PROCEDURE TO
PREVENT THE OPERATION OF THE THRUST REVERSER. THE
ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE
INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT.
(a) Do this procedure: Thrust Reverser Deactivation for Ground Maintenance
(PAGEBLOCK 78-31-00/201).
(b) Open the fan cowl panels (PAGEBLOCK 71-11-04/201).
(c) Open the core cowl panels (PAGEBLOCK 71-11-06/201).
SUBTASK 72-00-00-016-209-G00
CAUTION
PUT A LABEL ON THE BORESCOPE PLUGS. ENGINE DAMAGE CAN OCCUR
IF THE BORESCOPE PLUGS ARE NOT INSTALLED IN THE CORRECT
LOCATION.
(3) Remove the borescope plugs B2-1 through B2-5 (Figure 601).
(a) Put labels on the borescope plugs that you removed.
SUBTASK 72-00-00-016-210-G00
(4) Remove the ECS duct to get access to borescope plug B2-6 (Figure 601).
(a) Remove the borescope plug B2-6.
(b) Put a label on the borescope plug.
SUBTASK 72-00-00-296-211-G00
(5) Use the intrinsically safe borescope, COM-5661 to examine all the surfaces of the combustion
section for the conditions that follow (Figure 607):
Condition Maximum Serviceable Limit
Discoloration Permitted.
Collected carbon Permitted.
(a) Below is applicable equipment:
1) camera, STD-6732
2) VSV sight gage, SPL-6403
3) VSV sight gage, SPL-6404
4) VSV sight gage, SPL-6716
5) GE-FQAP-225 Inspection
(b) Below is list of lubricant that can be used:
1) sprayable air drying lubricant, D50194 [C02-004] or
2) lubricant, D00638 or
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-00-00
NoC
Page 686
D633T1B7 Aug 22/2017
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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109, 114, 115, 314-999