JA95-091 Audio Controller - Dual ICS Input
Environmental Qualification Form Rev A
CONFIDENTIAL AND PROPRIETARY TO JUPITER AVIONICS CORPORATION.
Rev A
Page 1 of 3
Prepared:
KDV
Checked:
Approved:
CONDITIONS
SECTION
DESCRIPTION OF TESTS CONDUCTED
Temperature
4.5
Equipment tested to Category [C4]
Ground Survival Low Temperature
4.5.1
Equipment tested to Category C4, (-55 °C)
Short-Time Operating Low Temperature 4.5.1
Equipment tested to Category C4, (-45 °C)
Operating Low Temperature
4.5.2
Equipment tested to Category C4, (-45 °C)
Ground Survival High Temperature
4.5.3
Equipment tested to Category C4, (+85 °C)
Short-Time Operating High
Temperature
4.5.3
Equipment tested to Category C4, (+70 °C)
Operating High Temperature
4.5.4
Equipment tested to Category C4, (+70 °C)
In-Flight Loss of Cooling
4.5.5
Equipment identified as Category X, no test performed
Altitude
4.6
Equipment tested to Category [(A1)(D1)]
Altitude
4.6.1
Equipment tested to Category D1, (50,000 ft)
Decompression
4.6.2
Equipment tested to Category A1, (8,000 to 50,000 ft)
Overpressure
4.6.3
Equipment tested to Category A1, (-15,000 ft)
Temperature Variation
5.0
Equipment tested to Category B (5 °C/min)
Humidity
6.0
Equipment tested to Category A (48 hours)
Nomenclature
Audio Controller - Dual ICS Input
Type/Model/ Part No.:
JA95-091
TSO No.:
CAN-TSO-C139
Manufacturer’s Build Configuration:
JA95-091 Build Configuration Rev A
Manufacturer’s Test Report:
JA95-001 Test Report (Qualification - Final) Rev A
1
JA95-091 CAN-TSO Design Change Assessment Rev A
2
Manufacturer’s Specification
and/or Other Applicable Specification:
JA95-091 Derivative Declaration of Design and Performance Rev A
Manufacturer:
Jupiter Avionics Corporation
Address:
1959 Kirschner Road, Kelowna, BC, Canada, V1Y 4N7
Revision & Change No of DO-160:
Rev. F
dated December 6, 2007
Dates Tested:
Sept 28 - Dec 27, 2012
JAC
AH
03-26-20
JAC
KDV
03-26-20
