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N9296T

Cancelled 2008
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Deregistered aircraft · 1978 Piper PA-38-112 · Lycoming 0-235 series

Open in FAA registry

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Cancelled
March 18, 2008
Exported to
Canada
Status when cancelled
Triennial form not returned
Serial number
38-78A0335
Year built
1978
Type
Fixed wing single engine
Engine
4 cycle
Airworthiness
Standard, normal, utility
Airworthiness date
June 19, 1978
Certificate issued
September 24, 2003
Last registry action
September 19, 2006
Mode S code
ACE2D5
Owner when cancelled
Aero Flight School LLC
Location
Belgrade, MT
Owner type
Corporation
Airframe modelPiper PA-38-112TCDS A18SO · ADs, bulletins and aircraft registered nowEngine modelLycoming 0-235 seriesTCDS E-223 · 4 cycle

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 · 1

Matched to this aircraft by N9296T and the event date: up to this one’s cancellation.

NTSB CHI92LA217Accident · Serious injuriesLimited investigationFinal reportFaribault, MNThe pilot's improper starting procedures and the passenger's inattentiveness. A related factor is the pilot's lack of supervision.Nov 10, 1991 · No damage

FAA incident reports · 2

FAA accident and incident reports matched to this aircraft by N9296T and the event date: up to this one’s cancellation.

Incident 20021020026969IFcd/Prec Ldg From Cruise · Grandview, ID(-23) The private pilot and one passenger were on a pleasure flight from boise, Idaho to jerome, Idaho. At a point 35 nautical miles south of boise, Idaho at an altitude of 5,500 feet MSL the engine failed. The pilot initiated an emergency landing to an open…Oct 20, 2002 · Minor damageAccident 19911110063099AStarting Engines · Faribault, MNPassenger struck by propeller wheel removing jump start battery cables.Nov 10, 1991

Service difficulty reports · 1

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

SDR LER2002F00000Bolt · failedIN CRUISE FLIGHT. 6 HOURS AFTER ENGINE START WHEN PILOT NOTICED SLIGHT ROUGHNESS FOLLOWED BY LOSS OF OIL PRESSURE. FOLLOWED IMMEDIATELY BY EXTREME VIBRATION, SMOKE AND OIL FROM ENGINE COMPARTMENT AND ENGINE STOPPAGE. PILOT COMPLETED A SUCCESSFUL EMERGENCY LOct 22, 2002 · N9296T · Piper PA38112 · Reciprocating Engine Power Section