Specifications

Rosen Aviation 10.6” HD Widescreen Bulkhead Display
Document Number: 106282
Revision: D
Date: 03/20/14
Template: 4.4.1.6FM2; Revision A; 12/06/12
Page 26 of 30
7.3. RTCA DO-160F Qualifications for Displays
The table below shows the DO-160F compliance of the 1060-001, unless otherwise noted.
Omitted categories are not applicable to these products or their expected installations.
Table 4 The 10.6” display is compliant with the following DO-160F 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)
Seamless operation
through 200 msec, EUT
must self-recover for
interruptions longer than
200 msec.
Normal Surge Voltage (DC)
16.6.1.4
Z
Engine Starting Under Voltage Operation
(DC)
16.6.1.5
Z