N5409G

CESSNA 404 · Fixed-wing multi-engine · 2 engines · 8 seats · 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)Operatoron 2021-09-18Operator named in NTSB report

Accident & incident history

Accident · 2021-09-18 Operator named in NTSB report
CESSNA 404 No injuries Part 135Richland Aviation, Inc.

Operated by RICHLAND AVIATION INC (per NTSB report)

Source: NTSB case WPR21LA350

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

3 reports on file, 1995-11-18 – 2019-08-16.

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

Part: ENGINE — FAILED

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
OTHER · 1999-05-25 Matched by certificate designator
ATA 5320

Part: CHANNEL — CRACKED (NLG WW)

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
FLUID LOSS · 1995-11-18 Matched by certificate designator
ATA 8530

Part: INTAKE TUBE — CRACKED (FLANGE)

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