*
= REVISED, ADDED OR DELETED PAGE F = FOLDOUT PAGE
EFFECTIVE PAGES CHAPTER 34 C8
PAGE 4 MAY 01/03
CONTINUED
D6-37115
*
= REVISED, ADDED OR DELETED PAGE F = FOLDOUT PAGE
C8 CHAPTER 34 EFFECTIVE PAGES
MAY 01/03 PAGE 5
BOEING 737
MAINTENANCE MANUAL
34- 55- 02 101 OCT 20/84 505102 FEB 20/86 5C8 34- 55- 02 501 FEB 20/86 5C8502 FEB 20/86 5C8503 FEB 20/86 5C8504 BLANK 34- 55- 11 401 OCT 20/91 500402 MAY 15/80 500403 OCT 20/91 500404 BLANK 34- 55- 21 401 JUN 20/84 501402 BLANK 34- 57- 01 1 OCT 20/84 5352 NOV 15/79 5523 FEB 15/72 5154 JUN 20/88 5C85 JUN 20/88 5C86 JUN 20/88 5C87 OCT 20/83 5C88 AUG 15/79 5829 MAY 15/79 55710 OCT 20/83 5C811 OCT 20/83 5C812 OCT 20/83 5C813 OCT 20/83 5C814 BLANK 34- 57- 01 101 MAY 15/80 541102 FEB 15/72 515 PAGE DATE CODE 34- 59- 01 (CONTINUED)3 OCT 20/83 5544 MAY 15/81 5775 FEB 15/79 5546 JUN 20/85 5C86A JUN 20/85 5C86B BLANK 7 FEB 15/79 5548 JAN 20/82 577F 8A FEB 20/86 5C88B BLANK F 9 JUN 20/88 5C810 BLANK F 11 JUN 20/88 5C812 BLANK 13 SEP 20/81 59314 SEP 20/81 59315 SEP 20/81 59316 SEP 20/81 59317 SEP 20/81 59318 SEP 20/81 59319 JUN 20/85 5C820 SEP 20/81 59321 SEP 20/81 59322 BLANK 34- 59- 01 101 OCT 20/89 5C8102 JUN 20/85 5C8103 MAY 15/79 554104 JUN 20/85 5C8 34- 59- 01 501 OCT 20/89 5C8502 JUN 20/88 5C8503 JUN 20/85 5C8504 JUN 20/85 5C8505 JUN 20/88 5C8506 BLANK PAGE DATE CODE PAGE DATE CODE PAGE DATE CODE
34- 57- 01 501 OCT 20/83 5C8502 OCT 20/83 5C8503 OCT 20/83 5C8504 BLANK 34- 59- 11 401 NOV 15/78 566402 NOV 15/78 566
34- 57- 11 401 OCT 20/91 502402 NOV 15/69 502
34- 57- 21 401 AUG 15/79 517402 AUG 15/79 517403 AUG 15/79 517404 BLANK
34- 57- 31 401 JUN 20/88 500402 BLANK
34- 59- 01 1 JUN 20/88 5C82 OCT 20/90 5C7
LAST PAGE
D6-37115
CHAPTER 34
NAVIGATION
TABLE OF CONTENTS
Subject Subject No.
FLIGHT ENVIRONMENT DATA
PITOT STATIC SYSTEM............................................................................................ *[7] 34-11-0
Description and Operation *[8] 34-11-01 Pitot Static Probe Pitot System Static System
Maintenance Practices
Draining
Flushing
Adjustment/Test
Pitot Static Probe ..................................................................................................... 34-11-11 Removal/Installation Inspection/Check Cleaning/Painting
Alternate Static Port ................................................................................................. 34-11-21 Removal/Installation
PITOT SYSTEM, ELEVATOR FEEL COMPUTER (Ref 27-31-0)
AIR DATA PRESSURE INSTRUMENTS.................................................................... *[9] 34-12-0
Description and Operation *[10] 34-12-01 Airspeed/Mach Indicators Altimeters Digital Air Data Computer Instantaneous Vertical Speed/Rate of Climb Indicators Standby Airspeed/Altimeter Indicator *[10]
Adjustment/Test
Air Data Computer ................................................................................................... 34-12-11 Removal/Installation
Air Data Pressure Indicators.................................................................................... 34-12-21 Removal/Installation
AIR DATA TEMPERATURE INDICATING SYSTEM ................................................. 34-14-0
Description and Operation
Total Air Temperature Indication
Total Air Temperature Probe
Adjustment/Test Subject Subject No.
5C8
Feb 20/89 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. Contents 34 Page 1
Total Air Temperature Probe ................................................................................... 34-14-21 Removal/Installation Adjustment/Test Cleaning/Painting
MACH/AIRSPEED WARNING SYSTEM.................................................................... *[9] 34-15-0
Description and Operation *[10] 34-15-01 Mach/Airspeed Aural Warning Clacker Mach/Airspeed Warning Switch
Adjustment/Test
ALTITUDE ALERTING SYSTEM................................................................................ *[4] 34-17-0
Description and Operation *[3] 34-17-02 Altitude Alert Annunciators Altitude Alert Controller Audio Alerting Unit
Trouble Shooting
Adjustment/Test
PERFORMANCE DATA COMPUTER SYSTEM........................................................ 34-18-0
Description and Operation
Auto Throttle/Automatic Flight Control *[4]
Control Display Unit (CDU)
EPR Indicator
Fuel Summation Unit
Mach/Airspeed Indicator
Mode Annunciator
Performance Data Computer
Trouble Shooting
Adjustment/Test
Performance Data Computer................................................................................... 34-18-11 Removal/Installation 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：737 AMM 飛機維護手冊 導航 NAVIGATION 1(3)
