EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001
PAGE 35-226
REVISION D
© Copyright 2019 Aspen Avionics Inc.
4
STC Specific Requirements and Limitations
4.1
EFD1000 E5 System Limitations
This section contains requirements that must be considered before installing the EFD1000 E5
system.
A turn and slip indicator (or backup attitude indicator) and an IFR GPS are always required for
airplanes certified for IFR operation. For airplanes restricted to VFR, see Section 4.5, Special
Consideration for Aircraft Limited to VFR.
The EFD1000 E5 is not approved for aircraft with a maximum takeoff weight (MTOW)
exceeding 6000lbs.
This installation is not authorized as a Flight Display for Category II Operations or RVSM
Operations.
4.2
EA100 Installation Limitations (EA100 is optional)
The EA100 must be installed in a temperature-controlled part of the aircraft.
The EA100 must not be installed on the firewall.
Maximum Ethernet cable length between the EFD and the EA100 is 30 feet.
An “A/P AHRS FAIL” light (amber) must be installed in the pilot primary field-of-view.
AFMS 900-00038-001 Rev ( ) or later FAA approved revision with the Configuration Matrix
in Section 1.2 completed must be inserted in the Airplane Flight Manual.
4.3
Authorized Configurations
The following are authorized configurations of the Aspen EFD1000 E5:
