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