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
