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N6255N

Cancelled 2025
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Deregistered aircraft · 1968 Bell 206A · Allison 250 SER 250HP

Open in FAA registry

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Cancelled
September 15, 2025
Status when cancelled
Valid registration
Serial number
129
Year built
1968
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Restricted, agriculture and pest control, forest
Airworthiness date
June 8, 2004
Certificate issued
October 15, 2022
Last registry action
September 9, 2023
Mode S code
A82BE4
Owner when cancelled
Trinkle Aviation LLC
Location
Kingsburg, CA
Owner type
LLC
Airframe modelBell 206ATCDS H2SW · ADs, bulletins and aircraft registered nowEngine modelAllison 250 SER 250HPTurbo-shaft

From the FAA registry file of November 5, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 2

Matched to this aircraft by N6255N and the event date: up to this one’s cancellation.

NTSB WPR25LA078Accident · No injuriesClass 4 · LimitedFinal reportLemoore, CAThe pilot’s failure to maintain clearance from power lines while maneuvering at a low altitude.Jan 14, 2025 · DestroyedNTSB OAK69D0171Accident · No injuriesClosedHanapepe, HINov 2, 1968 · Substantial damage

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N6255N and the event date: up to this one’s cancellation.

Accident 20250114000129ADescent · Lemoore, CAOn January 14, 2025, while conducting agricultural operations, the helicopter hit a power line with its main rotor blade while flying at a low altitude en route to refill its hopper, resulting in a crash. The pilot was able to exit the aircraft, and no…Jan 14, 2025 · Destroyed

Service difficulty reports · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR SD72005F00000Fuel Control · failedPILOT REPORTED DECAY OF N2 RPM WHEN ATTEMPTING TO REAPPLY COLLECTIVE FOLLOWING GRADUAL DECENT IN LOW ALTITUDE CRUISE FLIGHT. PRECAUTIONARY LANDING ACCOMPLISHED. SUBSEQUENT GROUND RUNS SHOWED MAXIMUM ACHIEVABLE N2 RPM OF 80 PERCENT. TEMPORARY REPLACEMENT WITFeb 28, 2005 · N6255N · Bell 206A · Fuel Control/Turbine Engines