RTCA/DO-160

Ref. Document RTCA/DO-160, D,E,F,G Advisory Circular [Download]

항공장비에 대한 표준환경 시험조건과 시험절차인 RTCA/DO-160 (or its precursor, RTCA/DO-138)은 1958년 부터 적용되어 왔습니다. 이 시험방법은 항공기 장비의 성능적 특성을 입증하기 위한 시험소에서의 시험방법을 제공합니다.  각 시험 조건은 다음과 같습니다.

1. RTCA/DO-160E/F Section 4: Temperature and Altitude
2. RTCA/DO-160E/F Section 5: Temperature Variation
3. RTCA/DO-160E/F Section 6: Humidity
4. RTCA/DO-160E/F Section 7: Operational Shock and Crash Safety
5. RTCA/DO-160E/F Section 8: Vibration
6. RTCA/DO-160E/F Section 9: Explosion Proofness
7. RTCA/DO-160E/F Section 10: Waterproofness
8. RTCA/DO-160E/F Section 11: Fluids Susceptibility
9. RTCA/DO-160E/F Section 12: Sand and Dust
10. RTCA/DO-160E/F Section 13: Fungus Resistance
11. RTCA/DO-160E/F Section 14: Salt Spray
12. RTCA/DO-160E/F Section 15: Magnetic Effect
13. RTCA/DO-160E/F Section 16: Power Input
14. RTCA/DO-160E/F Section 17: Voltage Spike
15. RTCA/DO-160E/F Section 18: Audio Frequency Conducted Susceptibility – Power Inputs
16. RTCA/DO-160E/F Section 19: Induced Signal Susceptibility
17. RTCA/DO-160E/F Section 20: Radio Frequency Susceptibility (Radiated and Conducted)
18. RTCA/DO-160E/F Section 21: Emission of Radio Frequency Energy
19. RTCA/DO-160E/F Section 22: Lightning Induced Transient Susceptibility
20. RTCA/DO-160E/F Section 24: Icing
21. RTCA/DO-160E/F Section 25: Electrostatic Discharge
22. RTCA/DO-160E/F Section 26: Fire, Flammability