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FLIGHT ADVISORYGPS INTERFERENCE TESTINGDUGWAY PROVING GROUND UTAH(DPG) 26-09 05 – 10 MAYDugway
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HeliNews Headlines
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The FAA is seeking input on proposed updates to Part 141 pilot school regulations to support modern
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HeliNews Headlines
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There are strange aircraft, and then there is the Sud-Est Grognard. At first, the French prototype
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HeliNews Headlines
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Apr
30
2026
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Posted by Admin
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AIRCRAFT PREPARING TO LOAD PATIENT, CREW MEMBER LOST CONTROL OF THE STRETCHER AND ROLLED INTO THE TAIL ROTOR. PATIENT HAD NOT YET BEEN PLACED ON THE STRETCHER AT THE TIME OF THE INCIDENT, CHAPMANSBORO, TN.
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CHAPMANSBORO
FAA
FAA Accident Report
TN.
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Press Releases
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Apr
30
2026
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Posted by Admin
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AIRCRAFT LANDING ON A MOUNTAIN TOP AND TAIL ROTOR STRUCK A TREE, YOUNG, AZ.
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AZ
FAA
FAA Accident Report
YOUNG
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Press Releases
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Apr
30
2026
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Posted by Admin
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The pilot stated that he was flying the helicopter solo with the doors removed while scouting potential locations for an aerial photography flight scheduled for later that day. During cruise flight, he heard a loud“boom”and felt a slight airframe vibration. He subsequently lost tail rotor thrust and performed an autorotation to an area of snow-covered, mountainous terrain.
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NTSB Report
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Press Releases
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Apr
30
2026
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Posted by Admin
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The company’s chief flight instructor reported that during a hydraulic system training maneuver, the pilot receiving instruction established too high of a sink rate, and the helicopter bounced upon touchdown. The helicopter then yawed to the right and bounced a second time before starting a slide towards the edge of the runway. The pilot receiving instruction attempted to correct by pushing the collective full down, however, the flight instructor realized that the helicopter would not come to a stop before exiting the runway and attempted to lift the helicopter back into the air. Before the helicopter could lift off, the left skid contacted the grass, the helicopter rolled to the left, and the main rotor contacted the ground. The helicopter then rolled to the right and came to rest on its right side. The helicopter sustained substantial damage to the main rotor system, tail rotor system, and tail boom. The flight instructor reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation. The chief flight instructor reported the accident could have been prevented if the flight instructor would have recognized the excessive rate of descent and made the necessary control inputs.
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FORT WORTH
NTSB Report
TX
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Apr
30
2026
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Posted by Admin
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On July 26, 2024, at 10:40 Central Daylight Time, a Viking Aviation LLC, doing business as Survival Flight, Bell 407 helicopter, powered by a single Rolls-Royce Corporation model M250- C47B turboshaft engine, experienced an uncontained engine failure while traveling to refuel after dropping off a patient. The engine failure necessitated a forced landing in a field. The pilot reported the incident occurred during the third flight of the day while using night vision goggles (NVG) from Oklahoma City, Oklahoma (OK) to Okmulgee, OK with the autopilot engaged and the helicopter in level flight at 2,000 feet mean sea level (MSL), 1,400 feet above ground level (AGL). The pilot reported that the cockpit gauges indicated the engine torque to be 78%, the gas producer temperature (NGT) 707°C-710°C, and gas producer rotor speed (Ng also commonly referred to as N1) at 98.6%.
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NTSB Report
OK
Oktaha
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Press Releases