EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001
PAGE 187-226
REVISION D
© Copyright 2019 Aspen Avionics Inc.
Installation Final Check Sheet
SECTION
POST INSTALLATION TESTS
PASS
FAIL
Second Phase RSM Location Evaluation –
Aircraft “Z” component within NOAA determined Z range?
10.5.4
Heading Accuracy Check (from Page 1)
10.5.5
Heading Interference Test
Indicated Airspeed Test
Altitude Display Test
System Leak Test
AHRS (attitude solution) Test
GPS Sensor Test
NAV Receiver Sensor Test – NAV1 (if installed)
Back-up NAV Indicator Test (if installed)
Autopilot Sensor Test (if installed)
Ancillary Equipment Heading and Air Data (if connected)
List equipment interfaced:
Battery Capacity Check – Internal battery > 80% Charge
TAPES Configuration Check
EMI Test
Flight Control Interference Check
OBS Mode Check
SECTION
COMPLIANCE CHECK
PASS
FAIL
6.4
Weight and Balance performed
7.1
Electrical Load Analysis performed
A turn and slip (turn coordinator) or standby attitude indicator
must be installed in accordance with section 4.4
Existing Airspeed and Altimeter must be remain in “basic T” or
original certified configuration in accordance with section 4.4
If the airplane is certified for IFR operations and uses the EFD1000
as a backup: A placard must be installed near the EFD1000 E5
stating “ On BAT Dispatch Limit is 80% See EFD1000 E5 AFMS”
