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R = REVISED, A = ADDED OR D = DELETED CHAPTER 75 F = FOLDOUT PAGE EFFECTIVE PAGES 17 C PAGE 3 JUL 12/02 LAST PAGE
D6-37537 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. ////////////////////////A / / CFM56 ENGINES 737-300/400/500/ /MAINTENANCE MANUAL //////////////////////// CHAPTER 75 - AIR TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject ____ Effectivity _______ Page ___________ AIR 75-00-00 ___ Description and Operation 1 ALL General 1 Operation 1
Trouble Shooting 101 ALL ACCESSORY COOLING 75-20-00 _________________ Description and Operation 1 ALL General 1 Engine External Accessories 1
Cooling Engine Internal Cooling 1 High Pressure Turbine Clearance 1
Control System Turbine Case Cooling 1 ENGINE EXTERNAL ACCESSORIES 75-21-00 COOLING
Description and Operation 1 ALL General 1 Generator Cooling 1 Ignition Leads Cooling 1
HIGH PRESSURE TURBINE CLEARANCE 75-24-00 CONTROL SYSTEM
Description and Operation 1 ALL General 1 Valve - High Pressure Turbine 1
Clearance Control Operation 1 Adjustment/Test 501 ALL Do The Check For The HPTCC 501 Valve And Timer TIMER - HIGH PRESSURE TURBINE 75-24-02 CLEARANCE CONTROL Maintenance Practices 201
(Deactivation) General 201 HPTCC Timer Deactivation 201
(Electrical Deactivation Procedure) [*] ENGINES WITH THE HIGH PRESSURE TURBINE CLEARANCE CONTROL (HPTCC) TIMER
CBEJ Page 1 Jul 12/01 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. ////////////////////////A / / CFM56 ENGINES 737-300/400/500/ /MAINTENANCE MANUAL //////////////////////// CHAPTER 75 - AIR TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject ____ Effectivity _______ Page ___________ Removal/Installation 401 [*] [*] ENGINES WITH THE HIGH PRESSURE TURBINE CLEARANCE CONTROL (HPTCC) TIMER
VALVE - HIGH PRESSURE TURBINE 75-24-01 CLEARANCE CONTROL Removal/Installation 401 ALL Inspection/Check 601 ALL
COMPRESSOR CONTROL 75-30-00 __________________ VARIABLE STATOR VANE ACTUATION 75-31-00 SYSTEM Description and Operation 1 ALL General 1 Actuator - Variable Stator 1
Vane Bellcrank - Variable Stator 3 Vane, Assembly Cable - Feedback, Variable 4 Stator Vane Rings - Variable Stator Vane 4 Actuation Operation 4 Maintenance Practices 201 ALL Actuation Procedure - Engine 204 Motoring Actuation Procedure - External 201 Pressure Source Adjustment/Test 501 ALL
Alternate Variable Stator Vane 533 (VSV) Dynamic Rigging Procedure (With RMS Tool TEE62-2)
Alternate Variable Stator Vane 539 (VSV) Dynamic Rigging Procedure (With SPS Tool SA610)
VSV Dynamic Rigging Procedure 506 (With CFMI Tooling 856A2001 and 856A1214)
VSV Stage to Stage Rigging 501 Procedure
CBEJ Page 2 Jul 12/01 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. ////////////////////////A / / CFM56 ENGINES 737-300/400/500/ /MAINTENANCE MANUAL //////////////////////// CHAPTER 75 - AIR
TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject ____ Effectivity _______ Page ___________ ACTUATOR - VARIABLE STATOR VANE 75-31-01 Removal/Installation 401 ALL Inspection/Check 601 ALL BELLCRANK - VARIABLE STATOR 75-31-03 VANE, ASSEMBLY Removal/Installation 401 ALL CABLE - FEEDBACK, VARIABLE 75-31-02 STATOR VANE Removal/Installation 401 ALL Adjustment/Test 501 ALL Inspection/Check 601 ALL VARIABLE BLEED VALVE SYSTEM 75-32-00 Description and Operation 1 ALL General 1 Actuator - Bleed Valve and 7 Ballscrew Actuator - Bleed Valve and 7 Master Ballscrew Cable - Feedback, Variable 12
Bleed Valve Mechanism - Stop, Bleed Valve 4 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：737-300 400 500 AMM 飞机维护手册 空气 AIR
