Appendix B Environmental Qualification Form; Environmental Qualification Form - L3 CP-2500 Installation Manual

Environmental Qualification Form

B.1 ENVIRONMENTAL QUALIFICATION FORM
PRODUCT DESCRIPTION:
MODEL:
PART NO.:
MANUFACTURER:
ADDRESS:
REVISION & CHANGE NUMBER OF DO-160: G
DESCRIPTION
Low Temperature
High Temperature
In-Flight Loss of
Cooling
Altitude
Decompression
Overpressure
Temperature Variation
Humidity
Operational Shocks
Crash Safety
Vibration
0040-17251-01
Revision D
CP-2500
Installation Manual
Appendix B
Control Panel
CP-2500
PS Engineering, 050-828-( )
ACSS, 9080-17250-( )
PS Engineering Inc.
9800 Martel Road, Lenoir City, TN37772
SECT.
NO. CAT.
-20° C Operating
4.5.1 -40° C Short Time Operating. Full performance except
4.5.2 optical performance is degraded
-55° C Ground Survival
+55° C Operating
4.5.3
A1F1
+70° C Short Time Operating
4.5.4
+85° C Ground Survival
Not Applicable, Not Tested.
4.5.5
External Cooling Not Required
4.6.1 Tested to 20,000 ft Maximum Operating Altitude
4.6.2 8,000 ft to 20,000 ft.
A1F1
A2F2
4.6.3 -15,000 ft.
5.3.1 B 5° C/min
6.3.1 B Standard Humidity Environment, 10 day test
3 shocks of 6g in both directions of the three
7.2 B
orthogonal axes.
One 20g Impulse shock in both directions
of each orthogonal axis.
Sustained Aircraft Type 5 (Helicopter and All Fixed-
7.3 B
Wing)
Test Type R (Random Orientation)
Fixed Wing Reciprocal and Turboprop – Single and
S
multi-engine (any weight)
Robust Fixed Wing, B/B1 – instrument panel – Fixed
8
R
Wing Turbojet
U2 Instrument panel and Fuselage Unknown Helicopter
Random Vibration
Appendix B
DESCRIPTION
March 15, 2018
Page B-1