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2. Remove Install the Bendix\King KMA 24 Audio/Marker Receiver......................... 201
3. Connectors ............................................................................................................ 202
CHAPTER 34-50 DEPENDENT POSITION DETERMINING.................................................................. 1
1. General ...................................................................................................................... 1
2. Description and Operation......................................................................................... 3
Trouble Shooting....................................................................................................................... 101
1. General .................................................................................................................. 101
Maintenance Practices............................................................................................................... 201
1. General .................................................................................................................. 201
2. Remove Install the Bendix\King KX 125 NAV COMM........................................... 201
3. Remove Install the Bendix\King KX 155 NAV COMM........................................... 203
4. Remove Install the Bendix\King KLN 35A GPS Receiver ..................................... 205
5. Remove Install the Bendix\King KLX 135/135A GPS COMM............................... 207
6. Remove Install the Bendix\King KI 208/209 Indicator ........................................... 209
7. Remove Install the Bendix\King KT 76A Transponder.......................................... 211
8. Remove Install the GNS430W............................................................................... 213
9. Remove Install the Garmin GNS530W.................................................................. 215
10. Remove Install the GNS430W/GNS530W VOR, LOC, G/S Indicator................... 217
11. Antennas................................................................................................................ 218
12. Connectors ............................................................................................................ 218
DA20-C1 AMM
Navigation
Doc # DA 201-C1
Rev. 0 34-00-00 Page 1
19 Dec 1997
CHAPTER 34-00
NAVIGATION - GENERAL
1. General
This Chapter tells you about these navigation systems:
− Chapter 34-10. Pitot-static and outside air temperature (OAT).
− Chapter 34-20. Electrically powered gyros, stall warning and magnetic compass
− Chapter 34-30. Radio navigation instruments for landing such as the marker receiver.
− Chapter 34-50. Radio navigation instruments, which give position data such as the
transponder and GPS.
This Chapter gives you only the on-airplane data about the systems and components. See the
manufacturers handbooks for shop data.
Many different instruments and avionics can be installed as options. This Chapter tells you about
the standard installation.
2. Description
A. Flight Environment Data
(1) Pitot-Static System
The pitot-static system has these components:
− A combined pitot-static probe below the left wing.
− An airspeed indicator (ASI).
− An altimeter.
− A vertical speed indicator (VSI).
− A blind altitude encoder.
(2) OAT
The OAT indicator is a digital instrument with a solid-state sensor.
Navigation
DA20-C1 AMM
Page 2
19 Dec 1997 34-00-00 Doc # DA 201-C1
Rev. 0
B. Attitude and Direction
The attitude and direction system has these components:
− Turn coordinator.
− Directional gyro (DG).
− Attitude gyro.
− Magnetic compass.
− Stall warning.
C. Landing and Taxiing Aids
The audio control panel has an audio\marker receiver (dual VHF COMM installations only).
D. Dependent Position Determining
The dependent position determining system has these components:
− VHF radio navigation aids (VOR/LOC).
− NAV indicator/converter.
− Global positioning system (GPS).
− Transponder.
DA20-C1 AMM
Navigation
Doc # DA 201-C1
Rev. 15 34-10-00 Page 1
30 Apr 2009
CHAPTER 34-10
FLIGHT ENVIRONMENT DATA
1. General
This Chapter tells you about the pitot-static system and OAT indicating system in the airplane. See
the manufacturer’s handbook for shop data about an instrument or component.
2. Description
Figure 1 shows the pitot-static system schematic diagram. The pitot-static system component
locations are show on Figures 2 and 3.
A. Pitot-Static System
　
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