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