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Boeing 767 - Pageblock 72-63-01;601 - HORIZONTAL DRIVE SHAFT - INSPECTION;CHECK; Task 72-63-01-206-001-G00 - Examine the Horizontal Drive shaft Housing; Subtask 72-63-01-016-002-G00; Subtask 72-63-01-046-010-G00

Boeing 767
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HORIZONTAL DRIVE SHAFT - INSPECTION/CHECK
1. General
A. This procedure gives the instructions on how to examine the horizontal drive shaft. You will only
examine the external area of the drive shaft housing.
TASK 72-63-01-206-001-G00
2. Examine the Horizontal Drive shaft Housing
(Figure 601)
A. References
Reference Title
70-11-06 P/B 201 FLUORESCENT PENETRANT INSPECTION - MAINTENANCE
PRACTICES
71-11-00 P/B 001 ENGINE COWLING - DESCRIPTION AND OPERATION
71-11-04 P/B 201 FAN COWL PANELS - MAINTENANCE PRACTICES
(OPEN/CLOSE)
71-11-06 P/B 201 CORE COWL PANELS - MAINTENANCE PRACTICES
(OPENING/CLOSING)
78-31-00 P/B 201 THRUST REVERSER SYSTEM - MAINTENANCE PRACTICES
B. Location Zones
Zone Area
412 Left Powerplant Nose Cowl
422 Right Powerplant Nose Cowl
C. Procedure
SUBTASK 72-63-01-016-002-G00
(1) Open the fan cowl panels (PAGEBLOCK 71-11-00/001).
SUBTASK 72-63-01-046-010-G00
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.
(2) Do this procedure: Thrust Reverser Deactivation for Ground Maintenance
(PAGEBLOCK 78-31-00/201).
SUBTASK 72-63-01-016-004-G00
(3) Open the core cowl panels (PAGEBLOCK 71-11-06/201).
SUBTASK 72-63-01-016-012-G00
WARNING
OBEY THE INSTRUCTIONS IN THE PROCEDURE TO OPEN THE THRUST
REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO
PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
(4) Open the thrust reversers (PAGEBLOCK 78-31-00/201).
SUBTASK 72-63-01-216-005-G00
(5) Examine the external area of the drive shaft housing. If it is necessary, use the fluorescent
penetrant inspection (PAGEBLOCK 70-11-06/201) to see the cracks more clearly.
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-63-01
NoC
Page 601
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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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