Boeing 767 - Subject 72-61-03 - ADAPTER - GEARSHAFT PACKAGE; Pageblock 72-61-03;401 - GEARSHAFT PACKAGE ADAPTER - REMOVAL;INSTALLATION; Task 72-61-03-004-001-G00 - Remove the Adapter

GEARSHAFT PACKAGE ADAPTER - REMOVAL/INSTALLATION
1. General
A. In this procedure the gearshaft package adapter is referred to as the adapter.
TASK 72-61-03-004-001-G00
2. Remove the Adapter
A. Tool Information
(1) 2C14140 Bearing
(a) 9480M17G01 Puller
(b) 9480M17G02 Puller
(c) 9480M17G03 Puller
(d) 9480M17G04 Puller
B. References
Reference Title
24-11-01 P/B 401 Config 3 INTEGRATED DRIVE GENERATOR -
REMOVAL/INSTALLATION
29-11-05 P/B 401 Config 4 ENGINE-DRIVEN PUMP (EDP) - REMOVAL/INSTALLATION
71-11-06 P/B 201 CORE COWL PANELS - MAINTENANCE PRACTICES
(OPENING/CLOSING)
73-11-01 P/B 401 FUEL PUMP - REMOVAL/INSTALLATION
73-21-01 P/B 401 MAIN ENGINE CONTROL - REMOVAL/INSTALLATION
73-21-08 P/B 401 ELECTRONIC ENGINE CONTROL (POWER MANAGEMENT
CONTROL) GENERATOR - REMOVAL/INSTALLATION
78-31-00 P/B 001 Config 1 THRUST REVERSER SYSTEM - DESCRIPTION AND
OPERATION
78-31-00 P/B 001 Config 2 THRUST REVERSER SYSTEM - DESCRIPTION AND
OPERATION
79-21-03 P/B 401 LUBE AND SCAVENGE PUMP - REMOVAL/INSTALLATION
80-11-01 P/B 401 STARTER - REMOVAL/INSTALLATION
C. Tools/Equipment
Reference Description
STD-6422
Jackscrews - 1/4x28 UNF
STD-6554
Gun - Heat
D. Consumable Materials
Reference Description Specification
G50258 [C10-009] Paper - Greaseproof MIL-B-121 Type II Grade
A Class 2 (Kraft)
E. Location Zones
Zone Area
410 Left Powerplant
415 Left Powerplant Fan Reverser - Left
420 Right Powerplant
425 Right Powerplant Fan Reverser - Left
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-61-03
NoC
Page 401
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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