NTSB CAROL · Event
Event LAX94LA246
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 ↗.
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