Becker RT6201 - Environmental Conditions AR62 X1-(X1 X), RT62 X1-(X1 X)

Becker Avionics
General Description
Technical Data
DV14307.03 Issue 06 February 2021 Transceivers 6200 Series 31
Environmental Conditions AR62X1-(X1X), RT62X1-(X1X)
The test was done in accordance with EUROCAE/RTCA Document ED-14F/DO-160E under
consideration of the recorded environmental categories and conditions:
Environmental Conditions
Section
Cat.
Remarks
Temperature and Altitude
4
C4
Ground Survival Low Temperature
4.5.1
-55 °C
Short-Time Operating Low Temperature 4.5.1
-20 °C
-40 °C for RT62X1
Operating Low Temperature 4.5.2
-20 °C
-40 °C for RT62X1
Ground Survival High Temperature
4.5.3
+85 °C
Short-Time Operating High Temperature
4.5.3
+70 °C
Operating High Temperature
4.5.4
+55 °C
In-flight Loss of Cooling
4.5.5
X
No forced cooling required
Altitude
4.6.1
C4
35 000 ft
Decompression
4.6.2
No test done
Overpressure
4.6.3
No test done
Temperature Variation
5
B
5 °C per minute
Humidity
6
A
Standard
Shock and Crash Safety
7
B
-
Operational Shocks
7.2
6 g
Crash Safety
7.3
Fixed-wing and helicopter, standard
Vibration 8
S
U
Curve M for fixed-wing aircraft
Curve G for helicopters
Explosion Atmosphere
9
X
No test done
Waterproofness
10
Y
Condensation
Fluids Susceptibility
11
X
No test done
Sand and Dust
12
X
No test done
Fungus Resistance
13
X
No test done
Salt Fog
14
X
No test done
Magnetic Effect
15
Z
< 1° deflection at 0.3 m
Power Input
16
B
-
Voltage Spike
17
A
-
Audio Freq. Conducted Susceptibility
18
B
-
Induced Signal Susceptibility
19
AC
Primary power DC