This N-number isn't registered right now. Below is its last known registration, canceled Jun 14, 2023.
Safety record in brief:1 NTSB accident (substantial damage, Jun 2021)No ADs since 1998 matched4 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 pilot’s failure to extend the landing gear before landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN21LA298)
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.
DURING A ROUTINE OIL CHANGE WHEN OIL FILTER WAS CUT OPEN FOR INSPECTION, A LARGE AMOUNT OF SILVER PARTICILES WERE FOUND. OIL SUMP SCREEN WAS REMOVED FOR INSPECTION AND LARGE PIECES OF SILVER MATERIAL WAS FOUND. ALL CYLINDERS WERE REMOVED FOR INTERNAL INSPECTION, FOUND NOTHING OBVIOUS, THE OIL SUMP…
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION BETWEEN PLATE AND CAST BEAM ALL FOUR SIDES. AREA BETWEEN PLATE AND BEAM CAN HOLD MOISTURE. CORROSION LOCATED UNDER PN 62003211 BLOCK. RECOMMEND REMOVE PLATES, CLEAN CORROSION, FILL WITH PRC AND REASSEMBLE. REPAIR WILL REQUIRE DER APPROVAL.
From FAA Service Difficulty Reports; matched by N-number and serial number.FOUND MOUNT CORROSION BETWEEN PLATE AND CAST BEAM ON ALL FOUR SIDES. AREA BETWEEN PLATE OF BEAM CAN HOLD MOISTURE. RECOMMEND REMOVE PLATES, CLEAN CORROSION, FILL WITH PRC, AND REASSEMBLE. REPAIR WILL REQUIRE DER.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING C/W SB 198A, PART I, CRACKS WERE FOUND RT FWD SCREW HOLE IN LEFT AND RIGHT RIBS ON BOTH TRIM TABS. FOUND NO OTHER DAMAGE AND RIBS WERE REPAIRED/MODIFIED PER SB 198A, PART II.
From FAA Service Difficulty Reports; matched by N-number and serial number.