* = REVISED, ADDED OR DELETED PAGE F = FOLDOUT PAGE
EFFECTIVE PAGES CHAPTER 71 C8
PAGE 2 MAY 01/03
LAST PAGE

D6-37115

CHAPTER 71
POWER PLANT
TABLE OF CONTENTS
Subject Subject No.
POWER PLANT .............................................................................................................

Description and Operation
Trouble Shooting
Removal/Installation
Adjustment/Test
Inspection/Check
Cleaning/Painting
POWER PLANT OPERATING PROCEDURES ......................................................... 71-09-100 Engine Ground Safety Precautions Engine Oil Pressure Adjustment Engine Operation Preparations Engine Prestart Procedure Engine Shutdown Procedure Engine Start Procedure Engine Starting and Operating Limitations Motor Engine Procedure New Engine Fuel Control Bleeding and Depreserving New Engine Ignition Check New Engine Operating Procedure New Engine Post Run Procedure Return Airplane to Normal Configuration
Cold Weather Operating Procedures....................................................................... 71-09-111

POWER PLANT TRIM PROCEDURE ........................................................................ 71-09-200

Power Plant Trim Data............................................................................................. 71-09-210 Maintenance Practices
Trim Tables (JT8D-17) Barometric Pressure
20.9 to 22.4 Inches of Mercury Absolute.............................................................. 71-09-241

Trim Tables (JT8D-17) Barometric Pressure
22.5 to 24.0 Inches of Mercury Absolute.............................................................. 71-09-242

Trim Tables (JT8D-17) Barometric Pressure
24.1
to 25.6 Inches of Mercury Absolute.............................................................. 71-09-243

25.7
to 27.2 Inches of Mercury Absolute.............................................................. 71-09-244

Trim Tables (JT8D-17) Barometric Pressure
Trim Tables (JT8D-17) Barometric Pressure
27.3 to 28.8 Inches of Mercury Absolute.............................................................. 71-09-245

553 
Oct 20/87  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Contents 71 Page 1 

Subject Subject No.
Trim Tables (JT8D-17) Barometric Pressure
28.9 to 30.4 Inches of Mercury Absolute.............................................................. 71-09-246

Trim Tables (JT8D-17) Barometric Pressure
30.5 to 32.0 Inches of Mercury Absolute.............................................................. 71-09-247

Trim Tables (JT8D-17A) Barometric Pressure
20.9 to 22.4 Inches of Mercury Absolute.............................................................. 71-09-261

Trim Tables (JT8D-17A) Barometric Pressure
22.5 to 24.0 Inches of Mercury Absolute.............................................................. 71-09-262

Trim Tables (JT8D-17A) Barometric Pressure
24.1 to 25.6 Inches of Mercury Absolute.............................................................. 71-09-263

Trim Tables (JT8D-17A) Barometric Pressure
25.7 to 27.2 Inches of Mercury Absolute.............................................................. 71-09-264

Trim Tables (JT8D-17A) Barometric Pressure
27.3 to 28.8 Inches of Mercury Absolute.............................................................. 71-09-265

Trim Tables (JT8D-17A) Barometric Pressure
28.9 to 30.4 Inches of Mercury Absolute.............................................................. 71-09-266

Trim Tables (JT8D-17A) Barometric Pressure
30.5 to 32.0 Inches of Mercury Absolute.............................................................. 71-09-267

COWLING
ENGINE COWLING .................................................................................................... 71-11-0

Description and Operation
Engine Fixed Fairing
Engine Nose Cowl
Engine Removable Cowl Panels
Nose Dome

Removable Cowl Panels.......................................................................................... 71-11-11 Removal/Installation Adjustment/Test
Fixed Fairing ............................................................................................................ 71-11-21 Removal/Installation Subject Subject No.
553 
Contents 71 Page 2  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  May 20/82 

Engine Nose Cowl ................................................................................................... 71-11-31 Removal/Installation Engine Gravel Deflector Tube
Removal/Installation
Inspection/Check
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737 AMM 飛機維護手冊 動力裝置 POWER PLANT(2)