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
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
B4F1
-40 °C
+70 °C
-40 °C
+70 °C
N/A
-55 °C
85 °C
55,000 Feet
N/A
N/A
Operational Shocks & Crash Safety
S (Zone 1; Curve C)
U (Zone 1; Curve G)
Audio Frequency Conducted Susceptibility – Power Inputs
Induced Signal Susceptibility
Radio Frequency Susceptibility (Radiated and Conducted)
Emission of Radio Frequency Energy
Lightning Induced Transient Susceptibility
B2K3L3
*B2K1L1 for power lines
Note: The Altitude Encoder is only calibrated to go up to 55kft. It can be calibrated to 85kft upon request.