HIGH PRESSURE COMPRESSOR - REPAIRS
1. General
A. This procedure contains sixteen tasks:
(1) Preparation for VSV Repairs
(2) Variable stator vane (VSV) lever arms (IGV - 5th stages) removal
(3) VSV lever arms installation
(4) VSV outer flanged bushing removal
(5) VSV outer flanged bushing installation
(6) VSV actuation levers removal
(7) VSV actuation levers installation
(8) HPC Stage 1 Blade Repair
(9) Slot loaded bearing ball removal
(10) Slot loaded bearing ball installation
(11) Repair of the slot loaded bearing with RTV sealant
(12) Borescope Blending Tool - Repair of the Stage 1-14 HPC Rotor Blades
(13) Loosen the Shingled HPC Stage 1 Blades
(14) Connecting Link Removal
(15) Connecting Link Installation
(16) Put the Airplane to its Usual Condition After VSV Repair
TASK 72-35-00-008-023-G00
2. Preparation for VSV Repairs
A. References
Reference Title
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
410 Left Powerplant
420 Right Powerplant
C. Procedure
SUBTASK 72-35-00-048-032-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.
(1) Do this procedure: Thrust Reverser Deactivation for Ground Maintenance
(PAGEBLOCK 78-31-00/201).
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-35-00
NoC
Page 801
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ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details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