Specifications

Rosen Aviation Smart Remote Display System
Document Number: 106957
Revision: A
Date: 03/13/14
Template: 4.4.1.6FM2; Revision A; 12/06/12
Page 21 of 24
Description
Section
Category
Comments
Vibration
8
Random Vibration – Fixed Wing Aircraft
8.5.2
S (Curve B)
Magnetic Effect
15
Magnetic Effect
15.3
A
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
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) – 10 kHz to
400 MHz
20.4
T
Radiated Susceptibility (RS) – 100 MHz to
18GHz
20.5
T