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flight test aircraft
- Fonte1
- INTERNATIONAL CIVIL AVIATION ORGANIZATION. Airborne collision avoidance systems. Montreal, 1985. (Cir. 195 AN/118).
- Fonte2
- INTERNATIONAL CIVIL AVIATION ORGANIZATION. Manual on testing of radio navigation aids. 4th. ed. Montreal, 2000. (Doc. 8071).
- Fonte3
- INTERNATIONAL CIVIL AVIATION ORGANIZATION. Environmental technical manual: procedures for the noise certification of aircraft: volume 1. 2nd.ed. Montreal, 2015. (Doc. 9501 AN/929).
- Nota Adicional1
- If the test aircraft is unable to attain the reference value of the advancing blade tip Mach number or the agreed reference noise correlating parameter, then an extrapolation of the sensitivity curve is permitted, provided that the data cover a range of values of the noise correlating parameter between test and reference conditions as agreed by the certificating authority.
- Contexto
- have flown collision courses (with appropriate safety precautions) and followed the resolution advisories generated by the ACAS equipment.
- The flight test aircraft is used to perform a horizontal flight at approximately 1 500 m (5 000 ft) following a radial. The flight inspector records power density from the flight inspection system. Airspace procedures based on the use of DME are evaluated at the minimum flight altitude. The flight inspector verifies that the distance information is properly available in the aircraft at ATC reporting points, along air routes.
- Français
- aéronef de vérification en vol