N5409G

CESSNA 404 · Valid Registration

Registered owner: RICHLAND AVIATION INC, MT (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
RICHLAND AVIATION, INC. (HTKA)Certificate holderMatched by certificate designator
RICHLAND AVIATION, INC. (HTKA)Operator2021-09-18 – 2021-09-18Operator named in NTSB report

Accident & incident history

Acc · 2021-09-18 Operator named in NTSB report
CESSNA 404 None injury Part 135RICHLAND AVIATION, INC.
Source: NTSB case WPR21LA350

Maintenance disclosures

O · 2019-08-16 Matched by certificate designator
ATA 8500

ENGINE FAILED IN FLIGHT. NR 5 AND NR 6 CONNECTING ROD (CRANK END) PROTRUDING THROUGH TOP OF ENGINE CASE. HOLES IN BOTH SIDES OF CASE BELOW NR 5 AND NR 6 CYLINDERS ABOVE OIL PAN FLANGE. THE ENGINE HAS BEEN IN SERVICE SINCE 07/2016. IT IS A FACTORY REBUILT ENGINE.

Source: SDR HTKA2020010800001 · FAA SDRS
O · 1999-05-25 Matched by certificate designator
ATA 5320

FOUND BOTH LEFT AND RIGHT T CHANNELS CRACKED APPROX 8 INCHES. THESE CHANNELS ARE LOCATED ON THE FORWARD CORNERS OF THE NOSE WHEEL WELL BOX ASSY AND ACCESSED FROM THE NOSE BAGGAGE AREA. POSSIBLE CAUSE FOR CRACKING DUE TO EXCESSIVE SIDE LOADING WHILE TAXIING. (M)

Source: SDR 20000424AP035 · FAA SDRS
K · 1995-11-18 Matched by certificate designator
ATA 8530

FUEL STAINS WERE NOTED AROUND SEVERAL INTAKE TUBES. IN REMOVING THE COLLARS FROM THE CYLINDERS TO GAIN ACCESS TO THE INJECTORS, TWO OF THE INTAKE TUBES WERE FOUND CRACKED AROUND THE RADIUS OF THE FLANGE.

Source: SDR 96ZZZX4311 · FAA SDRS