MXS System Description and Installation Manual
UM06945
© Sagetech Avionics 2022 Proprietary Confidential
Page 13 of 56
2.9
Environmental Specifications
The MXS was designed and verified to perform its intended function while operating in the environments
listed in Table 2-1.
Table 2-1 List of Environmental Operating Conditions
Environment
DO-160G
Section
Category
Temperature and Altitude
Operating Low Temp
Operating High Temp
Short-Time Operating Low Temp
Short-Time Operating High Temp
Loss of Cooling
Ground Survival Low Temp
Ground Survival High Temp
Altitude
Decompression Test
Overpressure Test
4
B4F1
-40 °C
+70 °C
-40 °C
+70 °C
N/A
-55 °C
85 °C
55,000 Feet
N/A
N/A
Temperature Variation
5
S1
(1)
Humidity
6
B
Operational Shocks & Crash Safety
7
B
Vibration
8
S (Zone 1; Curve C)
U (Zone 1; Curve G)
Explosion Proofness
9
E
Magnetic Effect
15
Y
Power Input
16
BXI
(2)
Voltage Spike
17
B
Audio Frequency Conducted Susceptibility
–
Power Inputs
18
B
Induced Signal Susceptibility
19
ACX
Radio Frequency Susceptibility (Radiated and Conducted)
20
TT
Emission of Radio Frequency Energy
21
BB
Lightning Induced Transient Susceptibility
22
B2K3L3
*B2K1L1 for power lines
Electrostatic Discharge
25
A
Note: The Altitude Encoder is only calibrated to go up to 55kft. It can be calibrated to 85kft upon request.
