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BOEING 737 MAINTENANCE MANUAL
CHAPTER 75 TAB EFFECTIVE PAGES SEE LAST PAGE OF LIST FOR NUMBER OF PAGES CONTENTS 75 1 OCT 20/91 5202 FEB 20/87 5C8 75- 00 1 NOV 15/80 5152 JUN 20/85 515 75- 09-100 1 OCT 20/85 5C82 OCT 20/83 5A73 OCT 20/83 5C84 OCT 20/83 5C8 75- 09-100 101 OCT 20/85 5C8102 OCT 20/83 5C8 75- 09-100 501 OCT 20/85 5C8502 OCT 20/83 5C8503 OCT 20/83 5C8504 OCT 20/83 5C8 75- 09-111 401 OCT 20/85 5C8402 NOV 15/69 528 75- 11-0 1 MAY 15/72 5052 NOV 01/74 5113 AUG 15/69 5004 FEB 20/87 5E5 PAGE DATE CODE 75- 11- 21 (CONTINUED)402 NOV 15/67 500403 NOV 15/67 500404 BLANK 75- 11- 41 401 OCT 20/90 505402 JUN 20/87 505 75- 11- 51 401 OCT 20/91 500402 OCT 20/91 500403 OCT 20/91 500404 OCT 20/91 500 75- 11- 61 401 FEB 20/92 500402 FEB 20/92 500403 FEB 20/92 500404 BLANK 75- 21-0 1 MAY 15/68 5002 MAY 15/68 500 75- 31-0 1 OCT 20/83 5002 OCT 20/83 5003 OCT 20/83 5004 OCT 20/83 5005 OCT 20/83 5006 OCT 20/83 5007 OCT 20/83 5008 BLANK 75- 31-0 601 AUG 01/74 500602 MAY 01/00 500 75- 31- 01 401 FEB 20/87 500402 FEB 20/87 500 PAGE DATE CODE PAGE DATE CODE PAGE DATE CODE 75- 11-0 401 MAY 01/00 505402 OCT 20/90 500 75- 11-0 501 OCT 20/85 500502 BLANK 75- 11-0 601 MAY 15/78 500602 BLANK 75- 11- 11 401 FEB 20/91 505402 OCT 20/90 500403 FEB 20/91 500404 FEB 20/91 500 75- 31- 11 1 FEB 15/67 5002 BLANK 75- 31- 11 401 OCT 20/83 500402 OCT 20/83 500403 OCT 20/83 500404 OCT 20/83 500405 OCT 20/83 500406 MAY 01/99 500 75- 31- 12 401 JUN 20/83 501402 SEP 20/82 501 75- 11- 21 401 AUG 15/68 500
* = REVISED, ADDED OR DELETED PAGE F = FOLDOUT PAGE C8 CHAPTER 75 EFFECTIVE PAGES MAY 01/00 PAGE 1
CHAPTER 75 AIR TABLE OF CONTENTS Subject Subject No. AIR.................................................................................................................................. 75-00 Description and Operation ENGINE PROTECTION ENGINE GRAVELPROTECTION SYSTEM.........................................................*[1] 75-09-100
Description and Operation Engine Gravel Protection Boom Engine Gravel Protection Pressure Switch Engine Gravel Protection Valve
Trouble Shooting Adjustment/Test
Engine Gravel Protection Valve..........................................................................*[1] 75-09-111 Removal/Installation ENGINE ANTI-ICING ENGINE AND NOSE COWL ANTI-ICING .................................................................. 75-11-0
Description and Operation Engine Anti-Icing Air Valve Engine Anti-Icing Air Orifice Nose Cowl Anti-Icing Air Valve Nose Cowl Anti-Icing Thermostatic Valve
Removal/Installation Adjustment/Test Inspection/Check
Engine Anti-Icing Shutoff Valve ............................................................................... 75-11-11 Removal/Installation Nose Cowl Anti-Icing Shutoff Valve and Thermostatic Valve .................................. 75-11-21 Removal/Installation Anti-Icing Air Rear Tube........................................................................................... 75-11-41 Removal/Installation Anti-Icing Air Front Tube .......................................................................................... 75-11-51 Removal/Installation ACCESSORY COOLING GENERATOR COOLING............................................................................................ 75-21-0 Description and Operation 520 Oct 20/91 Contents 75 Page 1 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
Subject Subject No. COMPRESSOR CONTROL COMPRESSOR BLEED SYSTEM ............................................................................. Description and Operation Inspection/Check 75-31-0 Start Bleed Control Valve......................................................................................... Removal/Installation 75-31-01 Pressure Ratio Bleed Control .................................................................................. Description and Operation Removal/Installation 75-31-11 Pressure Ratio Bleed Control Metering Plug ........................................................... Removal/Installation 75-31-12 *[1] GJ ALL EXCEPT B-2509 and B-2510
5C8 Contents 75 Page 2 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Feb 20/87
AIR -DESCRIPTION AND OPERATION 1. General A. Engine compressor air is tapped for operating various engine accessories and airplane systems. Some bleed systems are basic with the engine as received from the engine manufacturer. Other engine bleed systems are installed by the airframe manufacturer. In addition to engine bleeds for accessory and system use, a compressor bleed system is incorporated to permit engine operational flexibility by allowing high compressor discharge air to bleed into the fan discharge duct. www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：737 AMM 飞机维护手册 点火 空气 AIR
