Aspen Avionics EFD1000 E5 - Page 189

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001 PAGE 189-226 REVISION D
© Copyright 2019 Aspen Avionics Inc.
SECTION
COMPLIANCE CHECK
PASS
FAIL
Misc
Complete wire routing diagram in the Instructions for Continued
Airworthiness. Complete circuit breaker and switch location
diagram Figure 3 in the ICA document.
Misc
Copy of Aspen Avionics document #900-00012-001 Rev Y or later,
Instructions for Continued Airworthiness with copy of wiring
diagrams (Section 9 or installer drafted), copy of Configuration
Pages Section 10.4.6, and copy of Pre-Modification Checklist Table
5-1 inserted. This data package is to be given to owner/operator
for inclusion in aircraft permanent records.
EA100 Adapter Installations Only:
Appendix E
“A/P AHRS FAIL” annunciator installed in the pilot primary field of
view.
Appendix E
“A/P AHRS FAIL” annunciator powered from the autopilot main
breaker so that the light is illuminated whenever the autopilot is
powered but the EA100 is not.
Appendix E
Insert the completed AFMS in the Airplane Flight Manual, which
must be furnished.
Appendix E
Post EA100 Operational Check resulted in similar or better
performance than the Pre EA100 Operational Check.
* Note – Item may not apply to installations with aircraft limited to VFR – See Figure 4-1A.
Inspected by: (print & sign)
_________________________________________________________________________ _______________________________
Installer / Inspector Date