EFD1000 Installation Manual
DOCUMENT # A-01-126-00 PAGE 211-225 Revision H
© Copyright 2009 Aspen Avionics Inc.
EFD1000 Installation Final Check Sheet
(page 3 of 4)
SECTION COMPLIANCE CHECK PASS FAIL
5.2 For aircraft not limited to VFR, a Standby Attitude indicator
must be installed in the pilot’ field of view
5.2 Standby Airspeed, Altimeter, Magnetic Compass must be
installed in the pilot’s field of view
5.2.8 For aircraft limited to VFR, a placard or equivalent
acceptable means, stating “Operation of This Aircraft is
Limited to VFR Only”, or similar phraseology acceptable to
the Administrator. See Section 5.2.8. Note: This placard
should be pre-existing under TC or STC. This step is to
verify that the placard is still present.
5.2.4 Backup Navigation Indicator (if required) connected to a
navigation source installed in pilot’s field of view. The
indicator must continue to function if the PFD and/or ACU
circuit breaker is pulled.
7.2 Circuit breaker installed for PFD and 1 ea. for each ACU
6.9.1 RSM location shows less than 2 degrees of needle deflection
on hand held compass within 18”x18” survey area.
10.3 PFD braided ground strap installed between unit and panel
with < .003 ohms to ground.
RSM ground wire attached to ground stud < .003 ohms.
RSM doubler plate bonded to airframe ground < .003 ohms.
ACU(s) chassis bonded to airframe ground < .003 ohms.
7.2 Wires, cables, and connectors clearly marked or stamped
7.2 If installed, PFD master switch must be easily accessible to
flight crew and clearly marked
MISCELLANEOUS
1.7 Update warranty records on Aspen Avionics website at
www.aspenavionics.com
/dealerramp
6.3 Log book entry stating aircraft has been modified in
accordance with EFD1000 AML-STC.
Misc Complete cover page of EFD1000 AFMS Aspen document #
A-01-175-00 (Pro & Pro Digital) or A-01-179-00 (Pilot)
and insert in Airplane Flight Manual.
Misc Complete wire routing diagram Figure D1in Appendix D
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