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AEROSPACE TESTING
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| Testing
is performed for: |
Compliance
Qualification |
Design Verification
Failure Analyses |
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| Testing
is performed on : |
| Military Parts |
Commercial Parts |
|
| Testing
in accordance with: |
|
Domestic Requirements
|
International Requirements
|
| ARINC |
ASTM |
FAA |
IEEE |
EUROCAE |
NATO |
| NASA |
RTCA |
SAE |
U.S. Military |
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U.S. Aircraft Test Environments
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MILITARY REQUIREMENT |
ENVIRONMENT DESCRIPTION |
COMMERCIAL REQUIREMENT |
|
Specification |
Method |
In
Alphabetical Order |
Specification |
Section |
|
MIL-STD-810F |
513.5 |
Acceleration |
RTCA/DO-160D |
7.3.2 |
|
MIL-STD-810F |
500.4 |
Altitude |
RTCA/DO-160D |
4.6.1 |
|
MIL-STD-704 |
|
Aircraft Electric Power Characteristics |
|
|
|
MIL-STD-810F |
510.4 |
Blowing Dust |
RTCA/DO-160D |
12.0 |
|
MIL-STD-810F |
510.4 |
Blowing Sand |
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MIL-STD-461E |
|
Power Inputs |
RTCA/DO-160D |
16.0 - 18.0 |
|
MIL-STD-810F |
500.4 |
Decompression |
RTCA/DO-160D |
4.6.2 |
|
MIL-STD-461E |
|
EMI |
RTCA/DO-160D |
19.0 - 21.0 |
| |
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ESD |
RTCA/DO-160D |
25.0 |
|
MIL-STD-810F |
|
Explosive Atmosphere
Explosion Proofness
|
RTCA/DO-160D |
9.0 |
|
MIL-STD-810F |
504 |
Fluids Susceptibility |
RTCA/DO-160D |
11.0 |
|
MIL-STD-810F |
508.5 |
Fungus Resistance |
RTCA/DO-160D |
13.0 |
|
MIL-STD-461E |
|
High Intensity Radiated Field
(HIRF) |
RTCA/DO-160D |
20.0 |
|
MIL-STD-810F |
507.4 |
Humidity |
RTCA/DO-160D |
6.0 |
|
MIL-STD-810F |
521.2 |
Icing |
RTCA/DO-160D |
24.0 |
|
MIL-STD-1757 |
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Lightning - Direct Effects |
RTCA/DO-160D |
23.0 |
|
MIL-STD-461E |
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Lightning - Indirect Effects |
RTCA/DO-160D |
22.0 |
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Magnetic Effect |
RTCA/DO-160D |
15.0 |
|
MIL-STD-810F |
516.5 |
Mechanical Shock |
RTCA/DO-160D |
7.2 |
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MIL-STD-740 |
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Noise |
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MIL-STD-810F |
509.4 |
Salt Fog |
RTCA/DO-160D |
14.0 |
|
MIL-STD-810F |
501.4 & 502.4 |
Temperature |
RTCA/DO-160D |
4.5 |
|
MIL-STD-810F |
514.5 |
Vibration |
RTCA/DO-160D |
8.0 |
|
MIL-STD-810F |
506.4 |
Waterproof |
RTCA/DO-160D |
10.0 |
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