GH-3100
Installation & Operation Manual
Page B-2
Appendix B
TP-559
March 30, 2017
Revision K
Conditions
Section
Description of Tests Conducted
Temperature and Altitude
4.0
Equipment tested to Category A2. Except as follows:
Low Temperature
4.5.1
Low operating temperature -40
°
C.
High Temperature
4.5.2 & 4.5.3
In-Flight Loss of Cooling
4.5.4
Not applicable, Not Tested, External Cooling Not
Required
Altitude
4.6.1
Normal max. Operating altitude of 25,000 ft.
Decompression
4.6.2
Max. Test (aircraft operating altitude of 55,000 ft.
Overpressure
4.6.3
Temperature Variation
5.0
Equipment tested to Category B.
Humidity
6.0
Equipment tested to Category A.
Operational Shocks, and
Crash Safety
7.0
Equipment tested to Category B. Except with operational
shocks of 10f/11mSec. Crash safety sustained test levels
specified for Aircraft/Test Type "5/F" shall apply.
Vibration
8.0
DO-160D change No. 1 used in lieu of Change No. 0.
Equipment Tested to Category R - for fixed-Wing Aircraft
(Random Test only) and Category U
(*remarks)
-for helicopters
with unknown frequencies.
Explosion Proofness
9.0
Equipment tested to Category E.
Waterproofness
10.0
Equipment tested to 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 Resistance
13.0
Equipment identified as Category F, no organic materials
used
Salt Spray
14.0
Equipment identified as Category X, no test performed.
Magnetic Effect
15.0
Equipment tested to Category Z.
Power Input
16.0
Equipment tested to Category BZ, - for 28 Vdc powered
units including emergency operation at 18.0 Vdc. For
temperatures>20
°
C, power interrupts
≤
250 mSec shall
not cause realignment but display may turn off.
Voltage Spike
17.0
Equipment tested to Category A.
Audio Frequency Conducted
Susceptibility
18.0
Equipment tested to Category Z.
Induced Signal Susceptibility
19.0
Equipment tested to Category Z.
