N237CK
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.
4 reports on file, 2011-07-29 – 2024-08-05.
Part: LINE — BROKEN (TAILCONE) · airframe 14,273 hrs · 11,937 cycles
AFTER THE CREW SELECTED GEAR DOWN FOR LANDING THEY DISCOVERED THEY HAD TWO GREEN AND THREE RED GEAR INDICATOR LIGHTS AND THE HYDRAULIC PRESSURE WAS INDICATING ZERO. THEY USED THE EMERGENCY GEAR SYSTEM TO OBTAIN THREE GREEN LIGHTS AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. TROUBLESHOOTING FOUND THE CAPILLARY LINE FOR HYDRAULIC PRESSURE WAS BROKEN. THE LINE WAS REPLACED WITH NEW, THE HYDRAULIC SYSTEM AND EMERGENCY SYSTEM WERE SERVICED, AND GEAR, FLAP AND SPOILER CHECKS ACCOMPLISHED IN ACCORDANCE WITH THE APPLICABLE PORTIONS FOR THE LEARJET 35/35A/36/36A MAINTENANCE MANUAL.
Part: COMPUTER — FAULTY (STALL WARNING) · airframe 13,006 hrs · 11,127 cycles
MOMENTARY PUSHER ACTIVATION WITH NO OTHER WARNINGS. REPLACED STALL WARNING COMPUTER WITH SERVICEABLE, REPAIRED COMPUTER. ALL WORK PERFORMED IN ACCORDANCE WITH THE MM-99, CHAPTER 27-31-00 PART 'D'.
Part: STICK SHAKER — FALSE ACTIVATION · airframe 13,006 hrs · 11,127 cycles
MOMENTARY PUSHER ACTIVATION WITH NO OTHER WARNINGS. AIRCRAFT IS STILL BEING TROUBLESHOT. OPEN
Part: PANEL — ARCED (COCKPIT) · airframe 10,409 hrs · 9,422 cycles
CO-PILOT NOTICED A FLASH ON HIS RIGHT SIDE AND HEARD A POPPING NOISE WITH NO SECONDARY INDICATIONS OR LOSS OF POWER. PILOT LOOKED AT HIS CIRCUIT BREAKER PANEL AND NOTICED SOME ARCING ON THE AC BUSS, TOP ROW CIRCUIT BREAKERS. CREW RETURNED TO BASE. MAINTENANCE FOUND THE TOP ROW AC BUSS ELECTROLUMINESENT PANEL ARCED. ALL OTHER PANELS ON THAT SYSTEM CONTROL WORKED NORMAL. ELECTROLUMINESENT PANEL WAS REMOVED, CIRCUIT BREAKERS WERE LABELED, AND CO-PILOTS ELECTROLUMINESENT LIGHTING WAS DEFERRED.