Electronics International MVP-50T, Руководство по установке

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Environmental Qualification Form
DO-160
Page 1 of 3
Electronics International Inc.
DO-160
Environmental Qualification Form
0210081
Rev. C
2/11/2011
Nomenclature: Multi Function Engine and Aircraft System Monitor
Models: MVP-50P-(X) MVP-50T-(X), EDC-33P-(X), EDC-33T-(X)
Note: (X) represents the instrument configuration for a specific aircraft,
helicopter or blimp make and model.
Accessories: The following accessories were tested with the MVP-50 systems:
PT-30ABS, PT-30ALT, PT-60ABS, PT-90ABS, PT-05Diff, PT-04H20, FFDM-1-MVP,
FM-VA-XX, DPIM-1, FFDM-1, FFAM-1, FM-FP-XX, FM-Gyro, CP-1, AL-1(x)
Specifications: Document # 0425052 (can be found in the MVP-50 Installation
Instructions)
Manufacturer: Electronics International Inc.
63296 Powell Butte Hwy
Bend, OR 97701
Test Requirements: DO-160E Changes: 1, 2 and 3
Conditions Section Description of Tests Conducted
Temperature and Altitude 4 Tested to Category D1:
Operating Temp: -20
0
C to +55
0
C
Short Time Low Temp: -40
0
C
Short Time High Temp: +70
0
C
Ground Survival Low Temp: -55
0
C
Ground Survival High Temp: +85
0
C
In-Flight Loss of Cooling: N/A
Altitude: 50,000 feet
Decompression: 8,000 to 50,000 feet
Overpressure: -15,000 feet
Temperature Variation 5 Tested to Category C: 2
0
C/min
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