EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001
PAGE 167-226
REVISION D
© Copyright 2019 Aspen Avionics Inc.
SYSTEM DESCRIPTION
POSITION
EFD1000 E5 System
Pass Fail
Using the cockpit intercom, verify interference free communications
between the crew while monitoring the effects of the Threat
equipment.
NAVIGATION
VOR / ILS
Verify the operation of each VHF Nav receiver in both VOR and ILS
modes (including glideslope) while monitoring the effects of the
Threat equipment. At a minimum, use of ground test equipment is
required. Use of ground stations should be accomplished if facilities
are available. Record the frequencies tested.
No 1
No 2
DME (If Installed)
Verify the operation of each DME while monitoring the effects of the
Threat equipment. Ground test equipment or the same local
frequencies used for VOR and ILS testing may be used for this test.
No 1
No 2
MARKER BEACON
Verify the operation of each Marker Beacon Receiver while monitoring
the effects of the Threat equipment.
No 1
No 2
ADF (If Installed)
Verify the operation of each ADF receiver while monitoring the effects
of the Threat equipment. Frequencies from each band should be
tested where possible. Public broadcast stations are acceptable for
conducting test.
GPS
Verify the operation of each GPS receiver while monitoring the effects
of the Threat equipment. GPS satellite signals should be stable and of
similar strength with the threat equipment on and off. The navigation
systems used to display GPS information should not have any
interference effects from the threat equipment. Record GPS satellite
and position data for each system.
No 1
No 2
FLIGHT CONTROL SYSTEMS AND DISPLAYS
DISPLAY
Verify the EFD1000 E5 display functions without interference while
monitoring the effects of the peripheral Threat equipment.
FLIGHT DIRECTOR (If Installed)
Operate the flight director system and verify it responds to commands
from the control panel while monitoring the effects of the Threat
equipment.