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ATR500 Einbau und Bedienung
1.7 Umweltbedingungen
Characteristic DO–160D
Temperature / Altitude
Low ground survival temperature
Low operating temperature
High ground survival Temperature
High Short-time Operating
Temperature
High Operating Temperature
In –Flight Loss of Cooling
Altitude
Temperature Variation
Humidity
Shock
Vibration
Explosion Proofness
Water Proofness
Fluids Susceptibilities
Sand and Dust
Fungus Resistance
Salt Spray
Magnetic Effect
Power Input (DC)
Voltage Spike Conducted
Audio
Frequency
Susceptibility
Induced Signal Susceptibility
Radio Frequency Susceptibility
Emission of RF Energy
Lightning
Induced
Susceptibility
Lightning Direct Effects
Icing
Electrostatic Discharge (ESD)
Dokument-Nr.: 01.1251.010.71d / Revision: 1.04
Section Cat.
4.0
4.5.1
4.5.1
4.5.2
4.5.2
4.5.3
4.5.4
4.6.1
5.0
6.0
7.0
8.0
9.0
10.0
11.0
12.0
13.0
14.0
15.0
16.0
17.0
Conducted
18.0
19.0
20.0
21.0
Transient
22.0
23.0
24.0
25.0
Condition
-55° C
-20° C
C1
+85° C
+70° C
+55° C
Z
No auxiliary cooling required
C1
50,000 ft
2° C change rate minimum per
C
minute
A
6 G operational shocks
A
20 G Crash Safety
Test Type R in all 6 directions
S
Vibration Curve M
X
No test required
X
No test required
X
No test required
X
No test required
X
No test required
X
No test required
Z
< 0.3 m Compass Safe Distance
B
A
A
A
TT
M
B3F
3
X
No test required
X
No test required
A
9
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