JA95-R03 Audio Controller
Environmental Qualification Form - BC Rev B
CONFIDENTIAL AND PROPRIETARY TO JUPITER AVIONICS CORPORATION.
Rev A
Page 3 of 3
CONDITIONS
SECTION DESCRIPTION OF TESTS CONDUCTED
Radio Frequency Susceptibility
Radiated
Conducted
(See remark 3)
20.0
Equipment tested to Category RR
R (20 V/m CW&SW) and (150 V/m PM)
R (30 mA)
Radio Frequency Emission
(See remark 3)
21.0
Equipment tested to Category H
Lightning Induced Transient Susceptibility
Pin Injection
Cable Bundle
(See remark 3)
22.0
Equipment tested to Category [A3J33]
Waveform Set A, Test Level 3
Waveform Set J, Test Levels 33
Lightning Direct Effects
23.0
Equipment identified as Category X, no test performed
Icing
24.0
Equipment identified as Category X, no test performed
Electrostatic Discharge
Equipment identified as Category X, no test performed
Fire, Flammability
26.0
Equipment identified as Category X, no test performed
Other Tests
N/A
N/A
REMARKS
1.
This product is a derivative of the JA95-001. All tests were performed on a JA95-001 and JA95-R03.
A similarity analysis between the two products is detailed in the Jupiter Avionics Corp. document:
JA95-R03 CAN-TSO Design Change Assessment (BC Rev B) Rev A
2.
Test information can be found in the Jupiter Avionics Corp. documents:
JA95-001 Test Report (Qualification - Final) Rev B
JA95-R03 Test Report (Environmental - Vibration - 20160629) Rev A
JA95-R03 Test Report (Environmental - Operational Shock & Crash Safety - 20160630) Rev A
3.
Testing of Radio Frequency Susceptibility, Radio Frequency Emission and Lightning Induced
Transient Susceptibility was conducted at CKC Laboratories in Bothell, WA, USA.
Reference Jupiter Avionics Corp. document:
JA95-001 Test Report (CKC Labs DO-160F Section 20,
21, 22
– 2012-11-26 to 30) Rev A
4.
During exposure to vibration test conditions the following critical resonances
changed frequency greater than 2.5%:
Orientation
Initial Freq.
Final Freq.
Side Mount, Vertical
1054 Hz
1016 Hz
