TASK 72-61-02-404-016-G00
3. Install the Oil Seal
A. References
Reference Title
24-11-01 P/B 401 Config 3 INTEGRATED DRIVE GENERATOR -
REMOVAL/INSTALLATION
29-11-03 P/B 401 CENTER HYDRAULIC SYSTEM AIR DRIVEN PUMP (ADP) -
REMOVAL/INSTALLATION
29-11-03 P/B 401 Config 3 CENTER HYDRAULIC SYSTEM AIR DRIVEN PUMP (ADP) -
REMOVAL/INSTALLATION
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)
72-61-01 P/B 501 ACCESSORY GEARBOX - ADJUSTMENT/TEST
73-11-01 P/B 401 FUEL PUMP - REMOVAL/INSTALLATION
73-21-01 P/B 401 MAIN ENGINE CONTROL - REMOVAL/INSTALLATION
78-31-00 P/B 201 THRUST REVERSER SYSTEM - MAINTENANCE PRACTICES
80-11-01 P/B 401 STARTER - REMOVAL/INSTALLATION
FIXTURE
READY
FOR
INSTALLATION
FIXTURE
INSTALLED
PLASTIC
STOP
SCREW
OUTER
SLEEVE
PUSHER
PLATE
MATING
RING
73572 S00061423210_V1
Removal Fixture
Figure 402/72-61-02-990-802-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-61-02
NoC
Page 405
D633T1B7 Dec 22/2016
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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