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N8844V

Cancelled 2004

Deregistered aircraft · 1971 Bellanca 17-30A · Continental IO-520 series

Open in FAA registry

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Cancelled: March 4, 2004
Status when cancelled: Triennial form not returned
Serial number: 30368
Year built: 1971
Type: Fixed wing single engine
Engine: Reciprocating
Airworthiness: Standard, normal
Airworthiness date: June 16, 1971
Certificate issued: January 25, 2001
Last registry action: January 20, 2004
Mode S code: AC2FA9
Owner when cancelled: Hankins Jon
Location: Semmes, AL
Owner type: Individual

Airframe modelBellanca 17-30ATCDS A18CE · ADs, bulletins and aircraft registered now Engine modelContinental IO-520 seriesTCDS E5CE · Reciprocating

From the FAA registry file of October 29, 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 N8844V and the event date: up to this one’s cancellation.

NTSB MIA01LA092Accident · No injuriesLimited investigationFinal reportSylacauga, ALThe pilot's failure to maintain directional control during landing rollout, and the subsequent runway excursion and collision with trees.Mar 4, 2001 · Substantial damage NTSB FTW74FRG99Accident · No injuriesClosedAustin, TXJun 24, 1974 · Substantial damage

FAA incident reports · 3

FAA accident and incident reports matched to this aircraft by N8844V and the event date: up to this one’s cancellation.

Accident 20010304003699ARoll-Out (Fixed Wing) · Sylacauga, AL(-23) Pilot departed mobile regional for Sylacauga, Alabama. The winds at the time of the accident were gusty. The pilot landed the a/c at higher than normal airspeed and started braking the a/c. the pilot slao tried to hold the a/c on the runway. All three…Mar 4, 2001 · Substantial damage Incident 19870508033629IRoll-Out (Fixed Wing) · Janesville, WIAircraft veered as nose wheel touched down. Struck a runway light before correction could be made.May 8, 1987 · Minor damage Accident 19740624019019ARoll-Out (Fixed Wing) · Austin, TXFailed to chg rudder input at t/d.nose whl not aligned with rwy.Jun 24, 1974 · Substantial damage