Specifications

Rosen Aviation 19” HD Widescreen Display
Document Number: 104328
Revision: C
Date: 03/11/14
Template: 4.4.1.6FM2; Revision A; 12/06/12
Page 29 of 34
9.3. RTCA DO-160F Qualifications
The table below summarizes the basis for qualification of the 1900-001 and 1900-003 displays
by similarity to Rosen’s previously qualified 19” HD WS display (P/N 1900-002H), unless
otherwise noted.
Table 4 DO-160 Level F Test Criteria for the 1900-001 and 1900-003 displays
Description
Section
Category
Comments
Temperature and Altitude
4
Ground Survival/Short-Time Operating
Low Temp
4.5.1
A1
Tested
Operating Low Temperature
4.5.2
B4
Tested to 0C
Ground Survival/Short-Time Operating
High Temp
4.5.3
A1
Tested
Operating High Temperature
4.5.4
A1
Tested
In-flight Loss of Cooling
4.5.5
–
Not applicable
Altitude
4.6.1
B4
Qual by similarity to
1900-002H; tested to
25K ft
Decompression
4.6.2
A1
Qual by similarity to 1900-
002H; tested 6K–51K ft
Overpressure
4.6.3
A1
Qual by similarity to
1900-002H
Temperature Variation
5
Temperature Variation
5.3.1
C
Tested
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
Qual by similarity to
1900-002H; tested to
9.1g/axis
Vibration
8
Random Vibration – Fixed Wing Aircraft
8.5.2
S (Curve C)
Magnetic Effect
15
Magnetic Effect
15.3
Z
Tested
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