This N-number isn't registered right now. Below is its last known registration, canceled Jul 7, 2023.
Safety record in brief:1 NTSB accident (substantial damage, Jan 1990)No ADs since 1998 matched3 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
THE LOSS OF THE FLIGHT CREW'S VISUAL PERCEPTION, DUE TO AN UNFORESEEN WHITEOUT CONDITION. A RELATED FACTOR WAS THE SNOWBANK.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA90LA037)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
IB OF RT NACELLE, BLEED AIR PIPE (PN 2784187019), CHAFED OR BURNED THROUGH THE ASBESTOS SLEEVE SURROUNDING THE STARTER RELAY WIRING, WHICH THEN ARCED A HOLE IN THE BLEED PIPE, WHICH THEN BURNED THE SHIELDING FROM THE STARTER RELAY WIRES, WHICH THEN ARCED A HOLE IN A HYDRAULIC LINE (PN 2781032403)…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A FLUORESCENT PENETRANT INSPECTION OF (CARGO DOOR FRAME LOWER END FORE AND AFT NEAR BAYONET PIN). (FC STUN-M00-2-1-1) A CRACK OF APPROXIMATELY 0.250 INCH WAS DETECTED. THE PROBABLE CAUSE IS SERVICE INDUCED FATIGUE CRACKING. AREA OF CONCERN HAS ALREADY BEEN REINFORCED WITH DOUBLER PLATE AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A 50 HOUR FLUORESCENT PENETRANT INSPECTION OF THE LT AND RT MAIN LANDING GEAR STRUT HOUSINGS, A CRACK WAS FOUND ON THE LT MLG HOUSING. THE CRACK IS .125 INCHES LONG AND IS LOCATED .125 INCHES FROM THE FORWARD EDGE ON THE OB SIDE. THE INSPECTION IS COVERED IN MFG SB 226-32-033. THE HOUSING…
From FAA Service Difficulty Reports; matched by N-number and serial number.