![Jupiter Avionics JA95-091 Скачать руководство пользователя страница 46](http://html.mh-extra.com/html/jupiter-avionics/ja95-091/ja95-091_installation-and-operating-manual_2033794046.webp)
JA95-091 Audio Controller - Dual ICS Input
Environmental Qualification Form Rev A
CONFIDENTIAL AND PROPRIETARY TO JUPITER AVIONICS CORPORATION.
Rev A
Page 3 of 3
CONDITIONS
SECTION
DESCRIPTION OF TESTS CONDUCTED
Radio Frequency Susceptibility
4
Radiated
Conducted
20.0
Equipment tested to Category [RR]
R (20 V/m CW&SW) and (150 V/m PM)
R (30 mA)
Radio Frequency Emission
21.0
Equipment tested to Category H
Lightning Induced Transient Susceptibility
Pin Injection
Cable Bundle
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
Test information can be found in Jupiter Avionics document:
JA95-001 Test Report (Qualification - Final) Rev A
2
All tests were performed on the JA95-001 Build Configuration Rev D. A similarity analysis between the two
products is detailed in the Jupiter Avionics Corp. document:
JA95-091 CAN-TSO Design Change Assessment Rev A
3
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
4
Testing of Radio Frequency Susceptibility, Radio Frequency Emission and Lightning Induced Transient
Susceptibility was conducted at CKC Laboratories in Bothell, WA, USA.
Reference report:
JA95-001 Test Report (CKC Labs DO-160F Section 20, 21, 22
– 2012-11-26 to 30) Rev A