N98KC

BEECH 200 · 1976 · Fixed-wing multi-engine · 2 engines · 11 seats · Valid Registration

Registered owner: BELLES AVIATION LLC, MT (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Douglas E. ChappelleOperatoron 2008-08-11Operator named in NTSB report

Accident & incident history

Accident · 2008-08-11 Operator named in NTSB report
Cessna 210E Minor injury Part 91Douglas E. Chappelle

Operated by Douglas E. Chappelle (per NTSB report)

Source: NTSB case SEA08CA176

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.

2 reports on file, 2014-06-02 – 2015-01-13.

OTHER · 2015-01-13 Matched by certificate designator
ATA 5730

Part: SKIN — CRACKED (LT WING) · airframe 11,989 hrs · 13,544 cycles

DURING A PHASE 1 INSPECTION A SMALL CRACK APPROX 0.25 INCHES IN LENGTH ORIGINATING FROM A RIVET WAS DISCOVERED IN THE UPPER WING SKIN ON THE LT WING AT STATION 146.72 & 30% OF CHORD LINE.

Source: SDR QMLA2015011315003
OTHER · 2014-06-02 Matched by certificate designator
ATA 5720

Part: STIFFENER — CRACKED (RT WING) · airframe 11,898 hrs · 13,438 cycles

DURING AIRWORTHINESS INSPECTION AN ABNORMALITY NEAR A COUNTERSUNK RIVET WAS FOUND. THE LOCATION OF THE DEFECT FOUND IS ON THE WING CTR SECTION INBD OF THE NACELLE APPROXIMATELY 8 INCHES & FWD OF THE FLAP 6 INCHES. UPON FURTHER INSPECTION, THE ABNORMALITY WAS DETERMINED TO BE A CRACK APPROXIMATELY 1/2 INCH IN LENGTH IN THE ACFT SKIN. THE STIFFENER PN 50-10028-12 UNDER THE SKIN WAS ALSO DETERMINED TO BE CRACKED.

Source: SDR QMLA2014060214062