Rosen Aviation 19-55 : Remote electronics - Manual (Page 33)

Rosen Aviation Remote Display System
Document Number: 105478 Revision: F
Date: 06/23/14
Template: 4.4.1.6FM2; Revision A; 12/06/12 Page 33 of 38
Description Section Category Comments
Crash Safety (Sustained) 7.3.3 B
Vibration 8
Random Vibration – Fixed Wing Aircraft 8.5.2 S (Curve B)
Magnetic Effect 15
Magnetic Effect 15.3 B
Power Input 16
Normal Operating Conditions (DC) 16.6.1
Average Value Voltage (DC) 16.6.1.1 Z
Ripple Voltage (DC) 16.6.1.2 Z
Momentary Power Interruptions (DC) 16.6.1.3 Z (A)
A: for single power
interrupts up to 200 msec
Normal Surge Voltage (DC) 16.6.1.4 Z
Engine Starting Under Voltage Operation
(DC)
16.6.1.5 Z
Abnormal Operating Conditions 16.6.2
Voltage Steady State (DC) 16.6.2.1 Z
Low Voltage Conditions 16.6.2.2 – N/A (CAT B equip. only)
Momentary Under Voltage (DC) 16.6.2.3 Z
Abnormal Surge Voltage (DC) 16.6.2.4 Z
Voltage Spike 17
Voltage Spike 17.4 A
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) – 10kHz to
400MHz
20.4 T
Radiated Susceptibility (RS) – 100MHz to
18GHz
20.5 T