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 33 of 39
9.2. RTCA DO-160F Qualifications for Displays
The table below shows the DO160 compliance of the remote display system, unless otherwise
noted. Omitted categories are not applicable to this product or its expected installation.
Table 4 DO 160 Level F test criteria
Description
Section
Category
Comments
Temperature and Altitude
4
Ground Survival/Short-Time Operating
Low Temp
4.5.1
A1
Operating Low Temperature
4.5.2
A1
Ground Survival/Short-Time Operating
High Temp
4.5.3
A1
Operating High Temperature
4.5.4
A1
In-flight Loss of Cooling
4.5.5
–
Not applicable
Altitude
4.6.1
A1
Decompression
4.6.2
A1
Overpressure
4.6.3
A1
Temperature Variation
5
Temperature Variation
5.3.1
C
Humidity
6
Humidity
6.3.1
A
Operational Shocks & Crash Safety
7
Operational Shocks
7.2.1
B
Crash Safety (Impulse)
7.3.2
B
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
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)
Normal Surge Voltage (DC)
16.6.1.4
Z
Engine Starting Under Voltage Operation
(DC)
16.6.1.5
Z