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3. Remove/Install the Stormscope Antenna A. Remove the Stormscope Antenna Detail Steps/Work Items Key Items/References (1) Remove the trim/cover from the front face of the baggage compartment frame. Pull the rear seat-backs forward. (2) Open the 'WX-500'-circuit breaker. (3) Disconnect the connector of the stormscope antenna. (4) Remove the screws which attach the stormscope antenna to the fuselage. Hold the antenna! (5) Remove the stormscope antenna from the fuselage.
B. Install the Stormscope Antenna Detail Steps/Work Items Key Items/References (1) Put the stormscope antenna in position on the fuselage. (2) Install the screws which attach the stormscope antenna to the fuselage. (3) Connect the connector of the stormscope antenna. (4) Close the 'WX-500' circuit breaker. (5) Install the trim/cover to the front face of the baggage compartment frame. (6) Do a test of the stormscope system. Refer to Paragraph 4.
4. 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'. Page 202 Doc # 6.02.01 09 Jan 2003 Rev. 4 34-45-00 Navigation AMM
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).
Doc # 6.02.01 Page 1 Rev. 4 09 Jan 2003
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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. Doc # 6.02.01 Page 1 Rev. 4 09 Jan 2003
OBS Selector Knob Reciprocal Course Indice Figure 1: Bendix/King KI 208 Course Deviation Indicator www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：钻石40飞机维护手册 DA 40 SERIES AMM 4
