EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001
PAGE 152-226
REVISION D
© Copyright 2019 Aspen Avionics Inc.
10.4.7.3
PANEL ROLL ADJ
Panel Roll Adjust is used to align the roll reference mark of the EFD1000 to zero
degrees when the aircraft is wings level. With the aircraft wings level change the Panel
Roll Adjust adjustment to make the CORRECTED ROLL ATTITUDE equal to 0.0º. Should
more than 2º of correction be required the mechanical mounting of the EFD1000 for
level in the panel should be re-verified.
CAUTION: A RSM Calibration must be performed before first flight after changing either the PANEL
TILT PITCH ADJ or PANEL ROLL ADJ values.
10.4.7.4
ATTITUDE REF SYMBOL ADJ
This is used to make small changes to the pitch attitude reference mark on the
EFD1000 should the aircraft fly consistently slightly nose high or nose low in cruise
trim. It is not necessary to perform the RSM Calibration after making changes to this
setting.
10.4.8
NAV Setup Configuration
10.4.8.1
GPS/NAV#1 (ID#1)
Ranges from A to H as specified on the wiring diagrams of Section 9. See example
below.
Figure 10-6: GPS/NAV Example
10.4.8.2
COMPOSITE PHASE (VOR1, VOR2)
Most modern navigation receivers will be set to (0, 0) as VOR1 and VOR2 will have
VOR composite outputs with zero degree phase shift. For receivers with VOR
composite outputs that are 180º out of phase (i.e., ARC RT-385) set to 180 as
required.
10.4.9
ACU Configuration
10.4.9.1
ACU HSI TYPE
0= KI-525A, Emulates the KI-525A HSI
1= NSD-360A, Emulates the NSD-360A HSI
2= reserved
3= PN-101
Below is an example from Figure 9-16 showing a KI-525A Emulation with a Bendix
King autopilot. In this case you would set the ACU HSI TYPE =0:
ID#1
Description
G
H
H
ID#2
NONE
NONE
D
GPS1, No NAV1,
No NAV2
GPS1,NAV1,
No NAV2
GPS1, NAV1, NAV2
