Specifications

Rosen Aviation Remote Display System
Document Number: 105134
Revision: A
Date: 08/08/11
Template: 4.2.3-6-FM; Revision A; 16 May, 2005
Page 34 of 39
Description
Section
Category
Comments
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) – 10kHz to
400MHz
20.4
T
Radiated Susceptibility (RS) – 100MHz to
18GHz
20.5
T
Emission of Radio Frequency Energy
21
Conducted RF Emission
21.4
M
Radiated RF Emission
21.5
M
Electrostatic Discharge (ESD)
25
Electrostatic Discharge (ESD)
25.5
A
Flammability
26
N/A
Flammability testing in
accordance with 14 CFR
25.853 Appendix F
9.2.1. Other Certification Considerations for RDMs
Description
Comments
Static Abuse Load (300 lbs.)
Testing in accordance with DO 313 section 4.2(a), Glass
in the Cabin
Mechanical Strength (Ball Impact)
Testing in accordance with UL 61965
Inertia Loads
Testing in accordance with 14 CFR 25.561(b) (3)