Rosen Aviation
MIP
Document Number: 109970
Page 10 of 12
Revision A
Date: 04/24/18
4.6.3
A1
Overpressure
5
Temperature Variation
5.3.1
C
(2C/min)
Temperature Variation
6
Humidity
6.3.1
A
Standard Humidity
7
Operational Shocks & Crash Safety
7.2.2
B
Operational Shocks
7.3.2
B
Crash Safety (Impulse)
7.3.3
B
Crash Safety (Sustained):
Fixed-Wing Transport Aircraft,
Random Orientation (9g /axis)
8
Vibration
8.5.2
S
(Curve B)
Random Vibration
– Fixed Wing Aircraft
9
-
Explosion Proofness
10
-
Waterproofness
11
-
Fluids Susceptibility
12
-
Sand and Dust
14
-
Salt Fog
15
Magnetic Effect
15.3
A
Magnetic Effect
16
Power Input
[DC, Designation Z(A)IX]
16.6.1
Normal Operating Conditions (DC)
16.6.1.1
Z
Average Value Voltage (DC)
16.6.1.2
Z
Ripple Voltage (DC)
16.6.1.3
Z
Momentary Power Interruptions (DC)
16.6.1.4
Z
Normal Surge Voltage (DC)
16.6.1.5
Z
Engine Starting Under Voltage Operation (DC)
16.6.2
Abnormal Operating Conditions
16.6.2.1
Z
Voltage Steady State (DC)
16.6.2.3
Z
Momentary Under Voltage (DC)
16.6.2.4
Z
Abnormal Surge Voltage (DC)
17
Voltage Spike
17.4
A
Voltage Spike
18
Audio Frequency Susceptibility
18.3.1
Z
AF Conducted Susceptibility- Power Inputs
19
Induced Signal Susceptibility
19.3.1
AC
Magnetic Fields Induced Into Equipment
19.3.3
AC
Magnetic Fields Induced Into Interconnecting Cables
19.3.4
AC
Electric Fields Induced Into Interconnecting Cables