Przeciągnięcie i korkociąg nagrane przez spadochroniarza
Beechcraft C90 King Air wpada w korkociąg po opuszczeniu go przez grupę spadochroniarzy. Samolot bezpiecznie wrócił na ziemię, nikomu nic się nie stało.
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Beechcraft C90 King Air wpada w korkociąg po opuszczeniu go przez grupę spadochroniarzy. Samolot bezpiecznie wrócił na ziemię, nikomu nic się nie stało.
Komentarze (43)
najlepsze
Chyba, że mówisz o tym co się dzieje w/na samolocie.
W ustalonym wcześniej z kierownikiem skoków punkcie zrzutu, włączył sygnalizację świetlną „wykonać skok”. W miarę przesuwania się skoczków do wyjścia trymował samolot z jednoczesnym oddawaniem wolantu, aby zapobiec
@t0rmentor: To pilot zrzucił "balast" xD
Aircraft Stall Captured by Skydiver
For the full video please visit: https://youtu.be/2XMESBk0dJw
Incident
1. The aircraft was inspected and is undamaged.
2. The jump run procedure entails setting flaps 60-80 and bringing back the left engine to flight idle. We also bring the left prop back to full coarse to minimize disking of the prop. This is to enable the jumpers to egress onto the outside step, which would otherwise be difficult due to the prop & thrust blast from the left engine. There is also the added danger of the blast pushing jumpers into the left elevator. Power is kept on the right engine to maintain altitude during the jump run, which typically takes 60 seconds. A fair amount of right rudder is required to fly a straight line in this configuration. Pilot to maintain 95-90 kts IAS.
3. The stall and subsequent spin happened when we allowed too many jumpers on the outside step, causing an aft center of gravity and excessive blocking of the airflow to the left horizontal stabilizer. The nose then pitched up beyond the controllability of the elevator.
4. I #!$%@? the stall when I hit the elevator stop. As the wing came over, I moved the right engine power and prop levers back to the flight idle position, thereby neutralizing the engine effect from both engines, centralized the ailerons and applied full right rudder (rudder was already in quite deep in at this point). The aircraft behaved very well, and the recovery was surprisingly easy. I pulled out as gently as possible as I did not want to stress the airframe. There was some additional instability when I pulled out of the dive and pushed the throttles forward to power up, as the one engine spooled up much quicker than the other and caused another asymmetrical moment. The flaps may have inadvertently helped to keep the airspeed low. AIS showed 140kts when I pulled out.
5. The incident was reported to CAA within 24 hours. They investigated (including a visit to our hangar) and they seem to be happy that the aircraft was operated and flown within its STC.