N9317M

CESSNA T207A · 1980 · Valid Registration

Registered owner: WESTWIND AVIATION INC, AZ (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
WESTWIND AVIATION, INC. (WIWA)Certificate holderMatched by certificate designator
WESTWIND AVIATION INC (W10A)Operator2025-02-06 – 2025-02-06Operator named in NTSB report

Accident & incident history

Acc · 2025-02-06 Operator named in NTSB report
CESSNA T207A None injury Part 91WESTWIND AVIATION INC
Source: NTSB case WPR25LA107
Accident · 2003-05-26 Matched by aircraft (N-number)
Cessna T207A None injuryWESTWIND AVIATION, INC.
Source: NTSB case LAX03LA164

Maintenance disclosures

K R Y · 2020-09-16 Matched by certificate designator
ATA 8550

THE PILOTS REPORTED THAT HE SET TAKEOFF POWER, ENGINE PARAMETERS READ NORMAL AND UPON REACHING 40 KNOTS HE SAW A ROLL BACK. HE EXECUTED AN ABORTED TAKEOFF AND HEARD SOME ENGINE SPUTTERING FOLLOWED BY THE ENGING SHUTTING OFF. MAINTENANCE FOUND NO ABNORMAL PROBLEMS ON THE FIRST FEW RUN UPS, BUT UPON FUTURE INSPECTION THEY DID FIND AN OIL LEAK APPEARING TO COME FROM THE TURBO CHARGER. HOWEVER, IT IS NOT CONFIRMED THAT THE TURBO CHARGER IS THE ISSUE. AT THIS TIME WE DO NOT KNOW THE CAUSE OF THIS ENGINE FAILURE.

Source: SDR WIWA2020F00000 · FAA SDRS
O · 1997-07-29 Matched by certificate designator
ATA 6114

PENETRANT INSPECTION DURING NORMAL OVERHAUL INDICATED A FINE LINEAR CRACK OR SCRATCH. SUBSEQUENT EDDY CURRENT TESTING USING PHASE PLANE ANALYSIS INSTRUMENTATION REVEALED A CRACK APPROXIMATELY 1.5 INCHES LONG, ESTIMATED OVER .040 INCH DEEP ON THE EXTERIOR SURFACE OF NR 3 BLADE SOCKET ON THE LEADING EDGE SIDE SLIGHTLY ABOVE CENTERLINE OF THE HUB. THIS CONDITION IS NOT COMMONLY FOUND IN THE 'THREADLESS' STYLE OF MCAULY HUBS AND MAY BE OVERLOOKED WITHOUT EDDY CURRENT TEST.

Source: SDR 97ZZZX3748 · FAA SDRS