Configuration Module (SCM)
98-145168-A Appendix C: DO-160G specifications C-5
CCCC
C.3 Configuration Module (SCM)
Part Number: SCM-5055
Environmental variable
DO160 G section
(Unless otherwise specified)
Category and
requirements
Temperature and Altitude 4 -
Ground Survival Low Temperature Test -
55°C
4.5.1 A2
Short-Time Operating Low Temperature
Test -40°C
4.5.1 A2
Operating Low Temperature Test -40°C 4.5.2 A2
Ground Survival High Temperature Test
+85°C
4.5.3 A2
Short-Time Operating High Temperature
Test +70°C
4.5.3 A2
Operating High Temperature Test +70°C 4.5.4 A2
In Flight Loss of Cooling 4.5.5 X
Altitude Test +55.000ft 4.6.1 F2
Decompression Test 4.6.2 A2
Overpressure Test 4.6.3 A2
Temperature Variation (-40°C to +70°C) 5 B
Humidity 6 A
Operational Shocks and Crash Safety 7 -
Operational Shocks 7.2 B, E
Crash Safety (Impulse) 7.3.1 B, E
Crash Safety (Sustained) 7.3.3 Aircraft Type 5
(Helicopter and
All Fixed-Wing)
Orientation:
Random
Functional Test
before and after,
not during
Table C-2: Common environmental conditions and tests (DO160G) for SCM
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