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时间:2011-03-20 12:12来源:蓝天飞行翻译 作者:admin
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_______ Page ___________
 Cable - Loop Antenna 1
 Transmission
 Corrector - Quadrantal Error 1
 Coupler - Sense Antenna 5
 Panel - Control 5
 Receiver 5
 Operation 5
 [*] AF 101-156; IB 405; LH 001-003; SN 301-302

 Description and Operation 1 CONFIG 2 [*]
 General 1
 Antenna - Loop 1
 Antenna - Sense 5
 Cable - Loop Antenna 1
 Transmission
 Corrector - Quadrantal Error 1
 Coupler - Sense Antenna 5
 Panel - Control 5
 Receiver 5
 Operation 6
 [*] AF 121, 122, 152-199; IB 406-499; LH 011-099; SN 303-399; AT, AZ, GN,
 MD AND VM ALL

 Trouble Shooting 101 CONFIG 1 [*]
 [*] AF 101-151; IB 405; LH 001-010; SN 301-302

 Trouble Shooting 101 CONFIG 2 [*]
 [*] AF 121, 122, 152-199; IB 406-499; LH 011-099; SN 303-399; AT, AZ, GN
 MD AND VM ALL

 Adjustment/Test 501 CONFIG 1 [*]
 Operational Test 501
 [*] AF 101-151; IB 405; LH 001-010; SN 301-302

 Adjustment/Test 501 CONFIG 2 [*]
 Operational Test 502
 [*] AF 121, 122, 152-999; IB 406-499; LH 011-099, SN 303-399; AT, AZ, GN,
 MD AND VM ALL

 COMPONENTS - ADF ANTENNA 34-57-01
 Removal/Installation 401 ALL
 PANEL - ADF CONTROL 34-57-02
 Removal/Installation 401 ALL

 34-CONTENTS
 ATG Page 22 Oct 25/97
 CHAPTER 34 - NAVIGATION

 TABLE OF CONTENTS
_________________
 Chapter Section
 Subject_______  Subject ____ Effectivity_______ Page ___________
 RECEIVER - ADF 34-57-03
 Removal/Installation 401 ALL

 POSITION COMPUTING  34-60-00
__________________ PERFORMANCE MANAGEMENT SYSTEM 34-62-00 Description and Operation 1 [*] General 1 Alerts - Panel Mounted 28 Annunciation - Descent Mode 27 Annunciators - PMS Mode and 57 Alert Control - Vertical Steering 14 and Speed Display - PMS Vertical Path 57 Deviation Distribution - PMS Power 58 Indicator - Attitude Director 30 Indicator - Engine Pressure 29 Ratio Indicator - Horizontal 30 Situation Indicator - Limit 23 Indicator - N1 Tachometer 29 Interface - PMS, Air Data 30 Interface - PMS, Airframe 30 Interface - PMS, Auto 57 Throttle, A/P-F/D Interface - PMS, Engine 30 Interface - PMS, INS 57 Navigation - Horizontal 11 Panel - Limit Select 22 Unit - Computer 23 Unit - Control Display 20 Unit - Engine Interface 27 Unit - Switching 27 Operation 58 [*] AIRPLANES WITH PMS
 Trouble Shooting 101 [*]
 [*] AIRPLANES WITH PMS

 Adjustment/Test 501 [*]
 Operational Test 501

 34-CONTENTS
 ATG Page 23 Oct 25/97
 CHAPTER 34 - NAVIGATION

 TABLE OF CONTENTS
_________________
 Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
 System Test 514
 [*] AIRPLANES WITH PMS

 INDICATOR - PMS LIMIT 34-62-03
 Removal/Installation 401 [*]
 [*] AIRPLANES WITH PMS

 Adjustment/Test 501 [*]
 [*] AIRPLANES WITH PMS

 PANEL - PMS LIMIT SELECT 34-62-02
 Servicing 301 [*]
 [*] AIRPLANES WITH PMS

 Removal/Installation 401 [*]
 [*] AIRPLANES WITH PMS

 Adjustment/Test 501 [*]
 [*] AIRPLANES WITH PMS

 UNIT - PMS COMPUTER 34-62-04
 Removal/Installation 401 [*]
 [*] AIRPLANES WITH PMS

 Adjustment/Test 501 [*]
 [*] AIRPLANES WITH PMS

 UNIT - PMS CONTROL DISPLAY 34-62-01
 Servicing 301 [*]
 [*] AIRPLANES WITH PMS

 Removal/Installation 401 [*]
 [*] AIRPLANES WITH PMS

 Adjustment/Test 501 [*]
 [*] AIRPLANES WITH PMS

 UNIT - PMS ENGINE INTERFACE 34-62-05
 Removal/Installation 401 [*]
 [*] AIRPLANES WITH PMS

 Adjustment/Test 501 [*]
 34-CONTENTS
 ATG Page 24 Oct 25/97
 CHAPTER 34 - NAVIGATION

 TABLE OF CONTENTS
_________________
 Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
 [*] AIRPLANES WITH PMS
 UNIT - PMS SWITCHING 34-62-06 Removal/Installation 401 [*] [*] AIRPLANES WITH PMS
 Adjustment/Test 501 [*] [*] AIRPLANES WITH PMS
 34-CONTENTS
 ATG Page 25 Oct 25/97
 NAVIGATION - DESCRIPTION AND OPERATION
______________________________________
 1.  General
_______
 A.  The navigation systems are those systems used to determine and display the attitude, altitude, and position of the airplane with respect to the earth's surface. The navigation systems fall in the following general catagories:
 
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