EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001
PAGE 175-226
REVISION D
© Copyright 2019 Aspen Avionics Inc.
13
Environmental Qualification Forms
Nomenclature: ................ EFD1000 E5 Evolution Flight Display with Configuration Module
Part Number: .................. 910-00101-001 and CM: 910-00005-004
Manufacturer: ................. Aspen Avionics, Inc.
Address: ......................... 5001 Indian School Road NE, Albuquerque, NM 87110
DO-160 Revision: ........... DO-160E (DO-160G for Section 20 Category R)
Date Tested: ................... 2/2008 and 10/2018
Table 13-1: EFD1000 E5 Environmental Qualification Form
CONDITIONS
SECTI
ON
DESCRIPTION OF TESTS CONDUCTED
Temperature and Altitude
(Pressurized)
4.0
Equipment tested to Category A1, Decompress to 55,000”, Controlled temp and pressurized
to <15,000’
Temperature and Altitude
(Unpressurized)
4.0
Equipment tested to Category C1, Controlled temp and non-pressurized to 35,000’
Loss of Cooling
4.5.5
Equipment tested to Category Y, 300 minutes min.
Temperature Variation
5.0
Equipment tested to Category C
Humidity
6.0
Equipment tested to Category A, standard humidity environment
Operational Shock and Crash Safety
7.0
Equipment tested to Category B, standard operational shock and crash safety
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), Multi Eng Less than 5700 KG (12,500 lbs), and
Single Eng Less than 5700 KG (12,500 lbs) using vibration test 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 tested to Category Z, causes < 0.5 deg deflection to compass 0.3 meter away
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
RF Susceptibility
20.0
Equipment tested
in Accordance With PS-ACE-23-10
Additional Radio Frequency
Susceptibility (Conducted)
20.4
In addition, Conducted susceptibility per the Generic Conductive Curve- <25 meters
extrapolated the Env I per the applicable levels defined in RTCA/DO-160E section 20,
category A. Per FAA Policy PS-ACE-23-10
Additional Radio Frequency
Susceptibility (Radiated)
20.5
In addition, Radiated Susceptibility per Aircraft Generic Attenuation Curves applied to Env I.
0 dB: 100 MHz – 400 MHz
-6 dB: 400 MHz – 1 GHz
-12 dB: 1 GHz – 18 GHz
In accordance with FAA Policy PS-ACE-23-10.
RF Emissions
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
22.0
A3J33 and B3K33 for Refresh EFD1000 power pins, Refresh EFD1000 power bundle, RSM pins,
and RSM bundles, in accordance with FAA Policy PS-ACE-23-10.
A2J22 and B2K22 for all other Refresh EFD1000 pins and cables. Note: the main bundle was
tested at level 2 and level 3.
Lightning Direct Effects
23.0
Equipment identified as Category X, no test performed
Icing
24.0
Equipment identified as Category X, no test performed
ESD
25.0
Equipment tested to Category A
Fire, Flammability
26.0
Equipment identified as Category X, no test performed
Other Tests
Fire resistance was conducted by analysis in accordance with Federal Aviation Regulations Part
25, Appendix F.
