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(5) Remove the Stormscope antenna from the
% vertical stabilizer.
%
% B. Install the Stormscope Antenna
% Detail Steps/Work Items Key Items/References
(1) Put the Stormscope antenna in position in the
% vertical stabilizer.
%
(2) Install the screws which attach the Stormscope
% antenna to the mounting bracket.
%
(3) Connect the connector of the Stormscope
% antenna.
%
% (4) Close the 'Wx 500' circuit breaker.
% (5) Install the rudder. Refer to Section 55-40 of the AMM.
% (6) Do a test of the Stormscope system. Refer to Paragraph 6.
AIRCRAFT
Navigation
DA 40 Series
AMM
Page 204
20 Sep 2007 34-45-00 Doc # 6.02.01
Rev. 5
% 5. Remove/Install the DC-AC Inverter
% A. Remove the DC-AC Inverter
% Detail Steps/Work Items Key Items/References
% (1) Remove the passengers' seat. Refer to the AMM.
% (2) Open the 'Wx 500'- and 'DG'-circuit breakers.
% (3) Disconnect the electrical cables from the inverter.
%
(4) Remove the screws which attach the inverter to
% the baggage compartment frame.
% (5) Remove the inverter from the airplane.
% B. Install the DC-AC Inverter
% Detail Steps/Work Items Key Items/References
%
(1) Put the inverter in position on the baggage
% compartment frame.
%
(2) Tighten the screws which attach the inverter to
% the baggage compartment frame.
% (3) Connect the electrical cables of the inverter. Refer to Chapter 92 Wiring Diagrams.
% (4) Install the passengers' seat. Refer to the AMM.
(5) % Close the 'Wx 500'- and 'DG'-circuit breakers. %%
% (6) Do a test of the Stormscope system. Refer to Paragraph 6.
% 6. Test the Stormscope System
Do the installation checkout as outlined in Goodrich Stormscope WX-500 Installation Manual P/N 009-
11500-001, Chapter 3 'Installation Checkout'.
AIRCRAFT
DA 40 Series
AMM
Navigation
Doc # 6.02.01
Rev. 5 34-50-00 Page 1
20 Sep 2007
Section 34-50
Dependent Position Determining
1. General
This Section tells you about the equipment which shows dependent position determining.
Refer to these Sections for data about the systems:
Section 34-52 VHF Omnidirectional Range (VOR), Localizer (LOC), and Glideslope (GS).
Section 34-53 Automatic Direction Finder (ADF).
Section 34-54 Distance Measuring Equipment (DME).
Section 34-56 Transponder (XPDR).
Section 34-58 Global Positioning System (GPS).
AIRCRAFT
Navigation
DA 40 Series
AMM
Page 2
20 Sep 2007 34-50-00 Doc # 6.02.01
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AIRCRAFT
DA 40 Series
AMM
Navigation
Doc # 6.02.01
Rev. 5 34-52-00 Page 1
20 Sep 2007
Section 34-52
VOR/Localizer/Glideslope (VOR/LOC/GS)
1. General
This Section tells you about the VOR/LOC/GS (VHF omnidirectional range/localizer/glideslope) system
that can be installed in the DA 40. Refer to the manufacturer's manuals for more data about the
equipment.
The VOR/LOC/GS system consists of the following items:
) NAV receiver. The NAV receiver is part of the NAV/COM system. Refer to Section 23-10 for more
data about the NAV/COM system.
) Display or instrument:
) VOR and LOC information is displayed by the NAV/COM receiver. Refer to Section 23-10 for
more data about the NAV/COM receiver.
) VOR, LOC, and GS information can also be displayed by the course deviation indicator (CDI).
The CDI is optional equipment. It is described in this Section.
) VOR, LOC, and GS information can also be displayed by the horizontal situation indicator (HSI).
The HSI is optional equipment. Refer to Section 34-28 for more data about the HSI.
) NAV (VOR/LOC/GS) antenna. Refer to Section 23-10 for more data about the NAV antenna.
) NAV antenna coupler. Refer to Section 23-10 for more data about the NAV antenna coupler.
The audio panel controls the audio input from the NAV receiver (refer to Section 23-50).
2. Description and Operation
The VHF omnidirectional range (VOR) gives bearing information, ground station identification, and
reception of FSS reports in the VHF band.
Localizer (LOC) circuits are automatically energized when an ILS frequency is selected on the NAV.
Station identification and ATIS information can be received.
Glideslope (GS) circuits are automatically energized when an ILS frequency is selected on the NAV.
AIRCRAFT
Navigation
DA 40 Series
AMM
Page 2
20 Sep 2007 34-52-00 Doc # 6.02.01
Rev. 5
N
6
3
33
30
E
12
15
W
24
21
OBS S
VOR/LOC Pointer
VOR/LOC Flag
　
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