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R = REVISED, A = ADDED OR D = DELETED CHAPTER 49 F = FOLDOUT PAGE EFFECTIVE PAGES 17 PAGE 7 JUL 12/02 LAST PAGE
D6-37537 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. CHAPTER 49 - AIRBORNE AUXILIARY POWER TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject_______ Page AIRBORNE AUXILIARY POWER 49-00-00 ________________________ Description and Operation 1 General 1 Air - APU 11 Air Inlet - APU 10 Airplanes with the Electronic 1 Temperature Control (ETC) Controls - APU 11 Engine - APU 10 Exhaust - APU 11 Fuel - APU 10 Ignition and Start System - APU 10 Indicating - APU 11 Indicating - APU Oil 12 Lubrication - APU 11 Mounts - APU 9 Power Plant - APU 9 Shroud - APU 9 Trouble Shooting 101 General 101 Control and Indicators - APU 101 Troubleshooting Tips 104 POWER PLANT 49-10-00 ___________ APU POWER PLANT 49-11-00 Description and Operation 1 General 1 APU Power Plant 1 Operation 1 Effectivity ALL ALL ALL 49-CONTENTS
BEJ Page 1 Nov 12/99 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. ////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES/MAINTENANCE MANUAL //////////////////////// CHAPTER 49 - AIRBORNE AUXILIARY POWER TABLE OF CONTENTS _________________ Chapter Section Subject Subject_______ _______ Page____ Maintenance Practices 201 General 201 Activation - APU System (The 226 APU Installed) Activation - APU System (The 240 APU Removed) Deactivation - APU System (The 225 APU Installed) Deactivation - APU System (The 227 APU Removed) Depreservation - APU 248 Dry Motor the APU 219 Inspection - APU (After An 256 Overtemperature During Start) Leak Check - Control Air 250 Preservation - APU (Less Than 244 180 Days) Preservation - APU (181 to 365 245 Days) Shutdown - APU Automatic 219 Shutdown - APU Fire 218 Shutdown - APU Usual 217 Start and Operation - APU 201 Wet Motor the APU 222 Removal/Installation 401 Adjustment/Test 501 General 501 Limits - APU Operation 501 Test - APU Operation 501 Test - Bleed Air Valve Opening 535 Rate Test - Engine Start, 510 Acceleration, Operation and Automatic Controls Test - Fuel Control Unit 530 Acceleration Limiter Valve Opening Pressure Test - Fuel Control Unit 522 Governor Speed
EffectivityALL ALLALL
BEJ Page 2 Mar 12/02 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. CHAPTER 49 - AIRBORNE AUXILIARY POWER
TABLE OF CONTENTS _________________ Chapter Section Subject_______ Subject ____ Effectivity_______ Page ___________ Inspection/Check 601 ALL General 601 Check - APU Condition 606 Monitoring Inspection - Auxiliary Power 601 Unit APU SHROUD 49-12-00
Description and Operation 1 ALL General 1 Drains - APU Shroud 1 Lower Shroud 1 Upper Shroud 1 LATCH - APU SHROUD 49-12-41 Adjustment/Test 501 ALL SEAL - UPPER SHROUD 49-12-51 Removal/Installation 401 ALL SHROUD - UPPER 49-12-31 Removal/Installation 401 ALL APU MOUNTS 49-13-00
Description and Operation 1 ALL General 1 Mounts - APU Engine 1 Mounts - Shroud 1 Rings - Shroud 1 MOUNTS - APU ENGINE 49-13-11 Removal/Installation 401 ALL Bracket Installation - APU 409 Engine Mount Bracket Installation -409 Shroud Mounting Bracket Removal - APU Engine 405 Mount Bracket Removal - Shroud 401 Mounting APU AIR INLET 49-15-00
Description and Operation 1 ALL General 1 Actuator - Air Inlet Door 3 Door - Air Inlet 1 Ducts - Air Inlet 1 Operation 3
BEJ Page 3 Mar 12/01 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. ////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES/MAINTENANCE MANUAL //////////////////////// CHAPTER 49 - AIRBORNE AUXILIARY POWER 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 AIRBORNE AUXILIARY POWER 1
