JA95-N22 Audio Controller
Environmental Qualification Form
CONFIDENTIAL AND PROPRIETARY TO JUPITER AVIONICS CORPORATION.
Rev A
Page 3 of 3
CONDITIONS
SECTION DESCRIPTION OF TESTS CONDUCTED
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
25.0
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 the JA95-001. A similarity
analysis between the two products is detailed in the Jupiter Avionics Corp. document:
JA95-N22 CAN-TSO Design Change Assessment (BC Rev B) Rev A
2.
Test information can be found in the Jupiter Avionics Corp. document:
JA95-001 Test Report (Qualification - Final) Rev B
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.
Horizontal
72.5 Hz
75.0 Hz
Vertical
338 Hz
329 Hz
203 Hz
208 Hz
Lateral
140 Hz
136 Hz
156 Hz
168 Hz
169 Hz
157 Hz
265 Hz
285 Hz
