SEA95LA022
1994-11-28 · TWISP, Washington, United States · None · 1 aircraft · Status: Completed
Airport 2S0
Current FAA registration · N54594
- Make / Model
- HILLER UH-12C
- Engine
- FRANKLIN 6VS-335 SER (240 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19780616
- ADS-B equipped
- Yes — Mode-S A6EE2F
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
AN UNEXPLAINED LOSS OF POWER AND THE STUDENT PILOT'S DELAYED APPLICATION OF COLLECTIVE DURING THE LANDING FLARE.
Factual narrative
On November 28, 1994, approximately 1440 hours Pacific standard time (PST), a Hiller UH-12C helicopter, N54594, registered to and being flown by Ross C. Darling, a student pilot, was substantially damaged during a hard landing following a loss of power at the Twisp Municipal Airport, Twisp, Washington. The pilot was uninjured. Visual meteorological conditions existed and no flight plan had been filed. The flight, which was an instructional solo flight, was to have been operated under 14CFR91, and originated from the Twisp airport approximately 15 minutes before the accident. The student pilot reported that he was conducting a practice autorotation from approximately 1000 feet above ground commencing with a 300 RPM split between the engine/rotor tachometers. He reported applying carburetor heat and then reducing power to yield a 500-600 RPM split between the engine/rotor tachometers. Approaching 150 feet above ground, he began applying power with no effect. He transitioned into a full autorotation and between 50-75 feet above ground began his flare. He stated that he "began to apply collective but was (a) second slow fully levelling (the) helicopter." During the touchdown the tail boom was severed when it was struck by one of the rotor blades. FAA Inspector Doug Vaubel inspected the helicopter's Franklin engine subsequent to the accident and found no significant mechanical malfunctions. WHEN THE STUDENT PILOT APPLIED POWER DURING THE LANDING FLARE OF A PRACTICE AUTO ROTATION THE ENGINE DID NOT RESPOND. HE THEN TRANSITIONED TO A FULL AUTOROTATION BUT WAS LATE APPLYING COLLECTIVE TO FLARE BEFORE TOUCHDOWN AND A MAIN ROTOR BLADE IMPACTED THE TAILBOOM. NO MECHANICAL MALFUNCTION OF THE HELICOPTER'S POWERPLANT WAS DISCOVERED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_SEA95LA022.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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