N998CK
Registered owner: KALITTA CHARTERS LLC, MI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Kalitta Charters LLC (KC8A) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
9 reports on file, 2005-09-29 – 2017-05-16.
Part: FRAME — CRACKED (FRM 33) · airframe 25,288 hrs · 20,120 cycles
DURING EDDY CURRENT INSPECTION, A CRACK WAS FOUND IN THE BEND BETWEEN THE VERTICAL FRAME WEB AND FRAME FLANGE ON OF FRAME 33, APPROXIMATELY 20 MM BELOW STRINGER 5L, APPROXIMATELY 21 MM LONG AND OVER 1.3 MM IN DEPTH. CRACK TO BE REPAIRED.
Part: SKIN — DAMAGED (ZONE 200) · airframe 25,122 hrs · 20,000 cycles
SMALL AREA OF SKIN WAS DAMAGED JUST FWD OF FUSELAGE FRAME 1, AND JUST ABOVE STRINGER 14R AT THE STATIC PORT NUT PLATE. THE DAMAGED SKIN IS TO BE REMOVED AND FLUSH PATCHED.
Part: SKIN — CORRODED (ZONE 100) · airframe 25,122 hrs · 20,000 cycles
EDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN FOUND CORROSION AT RT SIDE FUSELAGE FRAME 6-7, STRINGER 21-22R.
Part: SKIN — CORRODED (ZONE 100) · airframe 25,122 hrs · 20,000 cycles
EDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN FOUND CORROSION AT RT SIDE FUSELAGE FRAMES 29-33, STRINGER 18R-22R.
Part: SKIN — CORRODED (FUSELAGE) · airframe 25,122 hrs · 20,000 cycles
EDDY CURRENT INSPECTION OF SPOT WELDED FUSELAGE SKIN. FOUND CORROSION AT FRAME 17-19, STRINGERS 5L-19L.
Part: SKIN — CORRODED (ZONE 100) · airframe 25,122 hrs · 20,000 cycles
EDDY CURRENT INSPECTION OF SPOT WELDED ON FUSELAGE SKIN FOUND CORRODED AT FRAME 29-33, STRINGER 18L-22L.
Part: SKIN — CORRODED (WING TIP) · airframe 25,122 hrs · 20,000 cycles
VISUAL INSPECTION OF WING TIPS, FOUND CORROSION ON THE TOP AFT SKIN SECTIONS, UNDER THE STATIC WICK BASES, BETWEEN RIBS 19-20.
Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 25,036 hrs · 19,934 cycles
DURING THE AIRCRAFT SCHEDULED INSPECTION, THE VISUAL INSPECTION OF THE CARGO DOOR STRUCTURE REVEALED CRACKS IN THE LOWER FORMERS AT FRAMES 11, 12 AND 13. THE CRACKED FORMERS AND ATTACH CLIPS WHERE REPLACED. FAA FORM 337 COMPLETED FOR THIS REPAIR.
Part: ENGINE — FLAMED OUT (RIGHT)
RT ENGINE FLAMED OUT DUE TO TURBULANCE. ENGINE WAS RESTARTED AND CONTINUED TO ORIGINAL DESTINATION. CAPTAIN CONTACTED MAINTENANCE DEPARTMENT. ENGINE WAS INSPECTED IAW OPS MANUAL WITH NO DEFECTS NOTED. THE FLIGHT WAS CONTINUED WITH NO OTHER ABNORMAL ENGINE OPERATION. (K)