Aspen Avionics EFD1000 E5 - Page 187

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
10.5.1.1
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
10.6.1
Indicated Airspeed Test
10.6.2
Altitude Display Test
10.6.3
System Leak Test
10.6.4
AHRS (attitude solution) Test
10.6.5
GPS Sensor Test
10.6.6
NAV Receiver Sensor Test – NAV1 (if installed)
10.6.7
Back-up NAV Indicator Test (if installed)
10.6.8
Autopilot Sensor Test (if installed)
10.6.9
10.6.10
Ancillary Equipment Heading and Air Data (if connected)
List equipment interfaced:
10.6.11
Battery Capacity Check – Internal battery > 80% Charge
10.6.12
TAPES Configuration Check
10.6.13
EMI Test
10.6.14
Flight Control Interference Check
10.6.15
OBS Mode Check
SECTION
COMPLIANCE CHECK
PASS
FAIL
6.4
Weight and Balance performed
7.1
Electrical Load Analysis performed
4.4*
A turn and slip (turn coordinator) or standby attitude indicator
must be installed in accordance with section 4.4
4.4*
Existing Airspeed and Altimeter must be remain in “basic T” or
original certified configuration in accordance with section 4.4
4.4.6*
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”