UAV-1004270-001
13
Rev A
5.7 Environmental Qualification Form
Conditions
DO-160G
Section
Description of Conducted Tests
Temperature and Altitude
4.0
Equipment tested to Category C4
Low temperature ground survival
4.5.1
-55°C
Low Temperature Short-Time
Operating
4.5.1
-45°C
Low Temperature Operating
4.5.2
-45°C
High Temperature Ground Survival
4.5.3
+85°C
High Temperature Short-Time
Operating
4.5.3
+70°C
High Temperature Operating
4.5.4
+70°C
Loss of Cooling
4.5.5
Cooling air not required (+70°C operating without
cooling)
Altitude
4.6.1
35,000 feet
Decompression
4.6.2
Equipment identified as Category C4
– no test
Overpressure
4.6.3
Equipment identified as Category C4
– no test
Temperature Variation
5.0
Equipment tested to Category A
Humidity
6.0
Equipment tested to Category C
Operation Shocks
7.0
Equipment tested to Category B
Crash Safety
7.0
Equipment tested to Category B Type 5
Vibration
8.0
Aircraft zone 1: Type 4/5 Category S Vibration Test
Curve M
Aircraft zone 7: Type 1 (Helicopter) to Category U2
Explosion
9.0
Equipment tested to Category H
Waterproofness
10.0
Equipment tested to Category S
Fluids Susceptibility
11.0
Equipment tested to Category F
Sand and Dust
12.0
Equipment tested to Category S
Fungus
13.0
Equipment identified as Category X
– no test
Salt Spray
14.0
Equipment tested to Category S
Magnetic Field
15.0
Equipment tested to Category A
Power Input
16.0
Equipment tested to Category BX
Voltage Spike
17.0
Equipment tested to Category B
AF Conducted Susceptibility
18.0
Equipment tested to Category B
Induced Signal Susceptibility
19.0
Equipment tested to Category AC
RF Susceptibility
20.0
Equipment tested to Category T
RF Emissions
21.0
Equipment tested to Category H
Lightning Induced Transient
Susceptibility
22.0
Equipment tested to Category A2XXXX
Lightning Direct Effects
23.0
Equipment identified as Category X
– no test
Icing
24.0
Equipment identified as Category X
– no test
Electrostatic Discharge
25.0
Equipment tested to Category A
Fire, Flammability
26.0
Equipment tested to Category C
