Aspen Avionics EFD1000 E5 - Environmental Qualification Form

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001 PAGE 226-226 REVISION D
© Copyright 2019 Aspen Avionics Inc.
Environmental Qualification Form
Nomenclature .................... EA100 Adapter
Part Number ...................... 910-00013-001
TSO Numbers .................... TSO-C4c, TSO-C113
Manufacturer ..................... Aspen Avionics, Inc.
Address ............................. 5001 Indian School Road NE, Albuquerque, NM 87110
DO-160 Revision ............... DO-160E
Date tested ........................ 7/2010
Condition
Section
Description of Tests Conducted
Temperature and Altitude
4.0
Equipment tested to Category D1
Low Temperature
4.5.1
High Temperature
4.5.2 & 4.5.3
Altitude
4.6.1
Decompression
4.6.2
Overpressure
4.6.3
Temperature Variation
5.0
Equipment tested to Category B
Humidity
6.0
Equipment tested to Category A
Operational Shocks and Crash Safety
7.0
Equipment tested to Category B
Vibration (Fixed Wing)
8.0
Equipment tested to Category S, aircraft Zone 2 for Fixed Wing Reciprocating
& Turboprop Engines, Multi Eng over 5700 KG (12,500 lbs.) (Using curve M),
Multi Eng Less than 5700 KG (12,500 lbs.) (Using curve M), Single Eng Less
than 5700 KG (12,500 lbs.) (using curve M)
Explosive Atmosphere
9.0
Equipment identified as Category X, no test performed
Waterproofness
10.0
Equipment identified as Category X, no test performed
Fluids Susceptibility
11.0
Equipment identified as Category X, no test performed
Sand and Dust
12.0
Equipment identified as Category X, no test performed
Fungus
13.0
Equipment identified as Category X, no test performed
Salt Fog Test
14.0
Equipment identified as Category X, no test performed
Magnetic Effect
15.0
Equipment is Category Z
Power Input
16.0
Equipment tested to Category B
Voltage Spike
17.0
Equipment tested to Category A
Audio Freq Conducted Susceptibility
18.0
Equipment tested to Category B
Induced Signal Susceptibility
19.0
Equipment tested to Category ZC
Radio Frequency Susceptibility
20.0
Equipment tested to Category TT
Radio Frequency Emission
21.0
Equipment tested to Category M, significant EM apertures, not in
direct view of radio receiver antenna (Equipment mounted in
cockpit or cabin area)
Lighting Induced Transient Susceptibility
22.0
Equipment tested to Category B3K33, Waveform Sets B and K are applicable
for equipment interconnected with wiring installed within any airframe or
airframe section when structural resistance is also a significant source of
induced transients, (i.e. carbon fiber composite structures). Level 3 is
intended for equipment and interconnecting wiring installed in a moderately
exposed environment.
Lightning Direct Effects
23.0
Equipment identified as Category X, no test performed
Icing
24.0
Equipment identified as Category X, no test performed
Electrostatic Discharge
25.0
Equipment tested to Category A
Fire, Flammability
26.0
Equipment identified as Category X, no test performed
Other Tests
Fire resistance conducted by analysis in accordance with Federal
Aviation Regulations Part 25, Appendix F.
Section 22.5.1 (Pin Injection): Communication between the EA100 and EFD1000 stopped. The EFD1000 remained operational,
and the EA100 successfully disengaged the autopilot relays.
END