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Doc # 6.02.01 Page 205
Rev. 4 09 Jan 2003
34-56-00
DA 40 Series
AMM
% This adjustment ensures that the altitude code generated from the SAE5-35 is within 125 feet of % the altitude displayed to the pilot. %
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% B. Adjust/Test the SAE5-35
Detail Steps/Work Items Key Items/References
(1) Connect the test equipment. Refer to the equipment manufacturers' manuals.
(2) Set the airplane altimeter to 1013.25 hPa (29.92 inHg).
(3) Monitor the altitude code. Decrease the pressure until the output code just changes to 20,000 ft.
(4) Make sure that the altimeter reading is within ± 125 ft of the encoder reading. If not, press the increase button (behind slot A) or decrease button (behind slot B) until the encoder reading is within 30 ft of the altimeter reading. Lightly tap the panel next to the altimeter to prevent errors due to friction.
(5) Increase the pressure until the output code just changes to 0 ft.
(6) Make sure that the altimeter reading is within ± 125 ft of the encoder reading. If not, press the increase button (behind slot A) or decrease button (behind slot B) until the encoder reading is within 30 ft of the altimeter reading. Lightly tap the panel next to the altimeter to prevent errors due to friction.
(7) Do steps 2 to 5 again until both 20,000 ft and 0 ft values are within the ± 125 ft tolerance.
(8) Operate the system through the range -1000 ft to 20,000 ft. Make sure that the altimeter and the encoder are within the ± 125 ft tolerance. Lightly tap the panel next to the altimeter to prevent errors due to friction.
(9) Disconnect the test equipment and remove it from the airplane.
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Page 206 Doc # 6.02.01 09 Jan 2003 Rev. 4
34-56-00
Navigation
AMM
% Section 34-58
% Global Positioning System (GPS)
% 1. General
% This Section tells you about the global positioning system (GPS) equipment that can be installed in
% the DA 40. Refer to the manufacturer's manuals for more data about the equipment. Refer to Chapter
% 92 for the wiring diagrams.
% Refer to Section 23-10 for more information about the NAV/COM system of the NAV/COM/GPS units.
% The GPS equipment consists of the following items:
%) GPS #1 receiver. One of the following GPS #1 receivers can be installed:
%) Bendix/King KLN 89B.
%) Bendix/King KLN 94.
%) Bendix/King KMD 150.
%) Garmin GNS 430.
%) Garmin GNS 530.
%) GPS #2 receiver. One of the following GPS #2 receivers can be installed:
%) Garmin GNS 430.
%) GPS annunciation control unit (optional).
%) GPS annunciation unit (optional).
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本文鏈接地址：鉆石40飛機維護手冊 DA 40 SERIES AMM 4(16)
