INTEGRATED DRIVE GENERATOR (IDG) - REMOVAL/INSTALLATION
1. General
A. This procedure has two tasks:
(1) The IDG Removal
(2) The IDG Installation.
TASK 24-11-11-000-801
2. Integrated Drive Generator (IDG) Removal
(Figure 401)
A. General
(1) The Integrated Drive Generator (IDG) is found on the accessory gearbox on the left side of the
engine fan case.
B. References
Reference Title
70-10-02-910-801-F00 General Precautions during the Removal and Installation of
Engine Components (P/B 201)
71-11-02-010-801-F00 Open the Fan Cowl Panels (P/B 201)
72-60-00-200-802-F00 Accessory Gearbox, Transfer Gearbox, and Horizontal Drive
Shaft - Oil Leakage Inspection (P/B 601)
C. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
COM-1443 Jack - Hydraulic, General Low Profile, Capacity: 2000 lbs, Lift: 10 to
44 Inches, or Equivalent Jack Capable of Lifting 300 lbs.
737-600, -700, -800
Part #: HW93718 Supplier: 28047
Opt Part #: W93718 Supplier: 36251
SPL-1626 Eye - Lifting, Generator
737-600, -700, -800
Part #: A49002-2 Supplier: 81205
SPL-1634 Jack Adapter - VSCF and IDG
737-600, -700, -800
Part #: C24002-77 Supplier: 81205
Part #: C24002-78 Supplier: 81205
STD-1055
Container - Oil Resistant, 5 Gallon (19 Liter)
D. Consumable Materials
Reference Description Specification
D00068 Oil - Aircraft Turbine Engine, Synthetic Base MIL-PRF-23699 Class
STD (Standard)
D00071 Oil - Aircraft Turbine Engine, Synthetic Base MIL-PRF-7808 Grade 3
G01048 Lockwire - MS20995C32, Corrosion Resistant
Steel - 0.032 Inch (0.8128 mm) Diameter
NASM20995
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
24-11-11
Page 401
D633A101-ILF Oct 15/2018
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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