ERA24LA387
2024-09-19 · Canandaigua, New York, United States · Minor · 1 aircraft · Status: Completed
Airport IUA
Current FAA registration · N281MC
- Make / Model
- AGUSTAWESTLAND PHILADELPHIA CO AW119MKII
- Year of manufacture
- 2022 · 2 years old at event
- Engine
- P&W CANADA PT6B-37A (900 hp)
- Seats / Engines
- 8 seats · 1 engine
- Last airworthiness date
- 20220708
- ADS-B equipped
- Yes — Mode-S A2D2C8
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On September 19, 2024, about 2003 eastern daylight time, an Agustawestland Philadelphia Co. AW119MKII helicopter, N281MC, was substantially damaged when it was involved in an accident at Canandaigua Airport (IUA), Canandaigua, New York. The commercial pilot was not injured, and two medical crewmembers sustained minor injuries. The helicopter was operated as a Title 14 Code of Federal Regulations Part 135 air medical flight. The pilot reported that he had transported a patient to a local hospital and was returning to IUA at night using night vision goggles. The flight was uneventful until reaching the airport. On approach to the base ramp, obstacles were called out and the approach continued to a grass landing zone adjacent to the ramp. About 100 ft above the ground, the landing light was illuminated. When the helicopter was about 10 ft above the ground, it lunged rapidly forward and downward, and “rolled very slightly left.” The left skid impacted the ground, followed by the right skid, and the helicopter rapidly rotated to the left. There was a tail-down rocking movement, the tailboom separated, and the helicopter came to a stop. The engine continued to operate, and the pilot was able to shut the engine down with the assistance of the medical crewmember in the left cockpit seat. The pilot and two medical crewmembers exited the helicopter and were met by first responders. The helicopter came to rest upright in the grass. Initial examination of the helicopter by Federal Aviation Administration inspectors revealed substantial damage to the fuselage, main rotor, tailboom, and tail rotor. The helicopter was equipped with a Genesys Aerosystems avionics suite. Flight and systems data were recorded for the entire accident flight until the removal of battery power. The wreckage was retained for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Descent rate-Not attained/maintained
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
- — Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2024_ERA24LA387.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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