Rosen Aviation 0603 Series : Rosenview MX - Manual (Page 18)

Rosen Aviation RosenView MX
Document Number: 106284 Revision: A
Date: 12/18/13
Template: 4.4.1.6FM2; Revision A; 12/06/12 Page 18 of 20
Description Section Category Comments
Operational Shocks & Crash Safety 7
Operational Shocks 7.2.1 B DO-160F
Crash Safety (Impulse) 7.3.2 B DO-160F
Crash Safety (Sustained) 7.3.3 B DO-160E
Vibration 8
Random Vibration – Fixed Wing Aircraft 8.5.2 S (Curve B) DO-160F
Magnetic Effect 15
Magnetic Effect 15.3 Z
Power Input 16
Normal Operating Conditions (DC) 16.6.1
Average Value Voltage (DC) 16.6.1.1 A
Ripple Voltage (DC) 16.6.1.2 Z
Momentary Power Interruptions (DC) 16.6.1.3 A
Normal Surge Voltage (DC) 16.6.1.4 A
Engine Starting Under Voltage Operation (DC) 16.6.1.5 B
Abnormal Operating Conditions 16.6.2
Voltage Steady State (DC) 16.6.2.1 A
Momentary Under Voltage (DC) 16.6.2.3 A
Abnormal Surge Voltage (DC) 16.6.2.4 B
Voltage Spike 17
Voltage Spike 17.4 B
Audio Frequency Conducted Susceptibility 18
AF Conducted Susceptibility- Power Inputs 18.3.1 Z
Induced Signal Susceptibility 19
Magnetic Fields Induced Into Equipment 19.3.1 AC
Magnetic Fields Induced Into Interconnecting
Cables
19.3.2 AC
Electric Fields Induced Into Interconnecting
Cables
19.3.3 AC
Spikes Induced Into Interconnecting Cables 19.3.4 AC
Radio Frequency Susceptibility 20
Conducted Susceptibility (CS) – 10 KHz to
400 MHz
20.4 T
Radiated Susceptibility (RS) – 100 MHz to
18 GHz
20.5 T