89000109-002 xVue Touch Installation Manual
Rev 2 Page 2-15
© Honeywell International Inc. Do not copy without express permission of Honeywell.
For Use in Non-Certified Aircraft
Table 2-13 KMG 7010 Environmental Qualification Form (EQF)
DO-160G
Section
Condition Category Notes
4.0 Temperature and Altitude A2F2 Ground Survival Low Temp: -55°C
Operating Low Temp: -55°C
Ground Survival High Temp: +85°C
Short-time Operating High Temp: +70°C
Operating High Temp: +70°C
Altitude certified to 55,000 feet
Decompression 8K to 55K ≤ 15 sec.
Overpressure 170 kPa
In-flight Loss of Cooling (Not Applicable)
5.0 Temperature Variation B 5°C/minute
6.0 Humidity B Severe Humidity Environment
7.0 Operational Shocks and Crash Safety B 3 shocks, 6g, each orientation
1 shock, 20g, each orientation
3 sec. minimum, 20g, each orientation
8.0 Vibration S (curves E, L, M &
T)
R (curve G)
(See Note 1)
Fixed Wing – Zone 5
Helicopter – Zone 1b.
9.0 Explosive Atmosphere E Environment II
Supplemental Analysis Performed – beyond
DO-160D:
DO-160G Section 9 analysis to meet Skydrol-
vapor Minimum Ignition Energy / HPN: 004-
02256-6232
10.0 Waterproofness W Drip Proof
11.0 Fluids Susceptibility X Not Tested
Supplemental Testing beyond DO-160D
DO-160G Section 11 Cat F / HPN: 004-02256-
6232
12.0 Sand and Dust X Not Tested
13.0 Fungus Resistance X Not Tested
14.0 Salt Fog X Not Tested
15.0 Magnetic Effect Z ≤ 1 degree deflection less than 0.3m
16.0 Power Input B From 10 VDC to 32.3 VDC.
Additional test of 200ms interrupt.
17.0 Voltage Spike A 600 Volt Spike
18.0 Audio Frequency Conducted Susceptibility BZ DC Powered equipment.
19.0 Induced Signal Susceptibility Z
(See Note 2)
Interference-Free Operation Required
20.0 Radio Frequency Susceptibility (Radiated
and Conducted)
RR
21.0 Emission or Radio Frequency Energy M
22.0 Lightning Induced Transient Susceptibility A4J33
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