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Atlas / NTSB / LAX94LA246

NTSB CAROL · Event

Event LAX94LA246

1994-06-11 WILLITS, California, United States Fatal 1 aircraft Status: Completed

Registry · N22GR

FAA Aircraft Registry record.

Make / Model

CESSNA 550

Year of manufacture

1999

Engine

P&W CANADA PW535A

Seats / Engines

8 seats · 2 engines

Last airworthiness date

19991130

ADS-B equipped

Yes — Mode-S A1DF4E

Registrant of record

M/V FORGER INC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

a loss of engine power for undetermined reasons.

Factual narrative

On June 11, 1994, at 0831 hours Pacific daylight time, a McCulloch Aircraft Corporation J-2 gyrocopter, N22GR, collided with terrain after takeoff from the Willits Municipal Airport, Willits, California. The gyrocopter was being operated as a personal flight by the pilot/owner. The gyrocopter was destroyed and the certificated commercial pilot received fatal injuries. The flight departed the Willits Municipal Airport about 0830 hours. Visual meteorological conditions prevailed for the local flight. The gyrocopter had just departed the airport at the time of the accident. A ground witness heard the aircraft depart and then heard the engine quit. The gyrocopter struck the terrain about 1/2 mile south of the airport and caught fire. The pilot stated to this person during the rescue that he "could not get the rotor blade up." The engine was examined on June 15, 1994, at Ukiah, California, under the supervision of an inspector from the Federal Aviation Administration (FAA). He reported that the No. 3 cylinder head had a crack approximately 3 inches in length. There were no exhaust or oil stains found in the cracked area to indicate problems prior to impact. The inspector noted nothing during the inspection of the engine that could have contributed to the power loss. The FAA inspector's report, and that of a local mechanic, is attached. SHORTLY AFTER TAKEOFF, A WITNESS HEARD THE ENGINE QUIT AND THEN OBSERVED SMOKE AND A LARGE FIRE OFF THE END OF THE RUNWAY. DURING THE RESCUE, THE PILOT TOLD THIS WITNESS THAT HE 'COULDN'T GET THE ROTOR BLADE UP.' EXAMINATION OF THE ENGINE FOUND NOTHING THAT WOULD HAVE CONTRIBUTED TO THE LOSS OF ENGINE POWER. HOWEVER, THE NO.3 CYLINDER WAS FOUND TO A 3-INCH CRACK THAT WAS ATTRIBUTED TO THE POSTCRASH FIRE. SUPPORTING THIS WAS THE ABSENCE OF EXHAUST SOOT OR OIL STAINS IN THE CRACKED AREA NORMALLY FOUND WITH A CYLINDER THAT FAILED IN FLIGHT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1994_LAX94LA246.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.