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base.
(3) Connect a digital millivolt meter to the slaving
control unit.
Connect the positive jack to the red jack
socket. Connect the common jack to
the black jack socket.
(4) Set all airplane electrical systems to ON.
(5) Set the gyro compass system ON. Allow it to
complete the start-up sequence.
(6) Align the airplane north. Use an approved external reference
compass.
(7) Set the slaving control to FREE.
(8) Use the CW/CCW switch to set the HSI compass
card to NORTH under the lubberline.
(9) Adjust the N/S potentiometer on the slaving
control unit to zero the external digital millivolt
meter.
Use a non-magnetic blade screwdriver.
(0 volts DC ± 50 millivolts).
(10) Align the airplane east. Use an approved external reference
compass.
(11) Use the CW/CCW switch to set the HSI compass
card to EAST under the lubberline.
(12) Adjust the E/W potentiometer on the slaving
control unit to zero the external digital millivolt
meter.
Use a non-magnetic blade screwdriver.
(0 volts DC ± 50 millivolts).
AIRCRAFT
DA 40 Series
AMM
Navigation
Detail Steps/Work Items Key Items/References
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(13) Align the airplane south. Use an approved external reference
compass.
(14) Use the CW/CCW switch to set the HSI compass
card to SOUTH under the lubberline.
(15) Adjust the N/S potentiometer on the slaving
control unit to zero the external digital millivolt
meter.
Use a non-magnetic blade screwdriver.
(0 volts DC ± 50 millivolts).
(16) Align the airplane west. Use an approved external reference
compass.
(17) Use the CW/CCW switch to set the HSI compass
card to WEST under the lubberline.
(18) Adjust the E/W potentiometer on the slaving
control unit to zero the external digital millivolt
meter.
Use a non-magnetic blade screwdriver.
(0 volts DC ± 50 millivolts).
(19) Set the slaving control to SLAVE.
(20) Align the airplane on each of the cardinal
headings in turn.
The error between the compass card on
the HSI and the external reference
compass must be less than ±2º.
(21) Set all airplane electrical systems to OFF.
(22) Remove the digital millivolt meter.
(23) Install the slaving control unit in the instrument
panel:
S Push the slaving control unit into position in
the panel.
S Install 2 attaching screws.
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DA 40 Series
AMM
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AMM
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Section 34-30
Landing and Taxiing Aids
1. General
This Section tells you about the landing and taxiing aids that can be installed in the DA 40.
Refer to the equipment manufacturers' manuals for more data about other options of landing and
taxiing aids.
2. Description
The DA 40 can have the following landing and taxiing aids:
) A localizer system which is part of the VOR/LOC/GS system. Refer to Section 34-52 for more data
about the VOR/LOC/GS system.
) A glideslope system which is part of the VOR/LOC/GS system. Refer to Section 34-52 for more
data about the VOR/LOC/GS system.
) A marker beacon receiver which is part of the audio integrating system. Refer to Section 23-50 for
more data about the marker beacon receiver functions of the audio integrating system.
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Navigation
DA 40 Series
AMM
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DA 40 Series
AMM
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Section 34-40
Independent Position Determining
1. General
This Section tells you about the independent position determining systems that can be installed in the
DA 40. Refer to these Sections for data about the systems:
Section 34-42 Strike Finder System
Section 34-45 Stormscope System
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DA 40 Series
AMM
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AMM
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Section 34-42
Strike Finder System
1. General
This Section tells you about the strike finder system that can be installed in the DA 40. Refer to the
manufacturer´s manual for more data about the equipment. Refer to Chapter 92 for the wiring
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