N95CK
Registered owner: C2 AVIATION LLC, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
8 reports on file, 1998-03-07 – 2002-06-19.
Part: HYDRAULIC LINE — CRACKED (HYD SYSTEM)
AIRCRAFT LOST HYDRAULIC PRESSURE AFTER CREW SELECTED THE GEAR DOWN. THE GEAR HAD 3 GREEN DOWN AND LOCKED INDICATIONS AND 2 RED UNSAFE INDICATIONS. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND HYDRAULIC LINE CRACKED UNDERNEATH ATTACHING ADEL CLAMP. HYDRAULIC LINE WAS REPLACED, HYDRAULICS WERE SERVICED, LANDING GEAR WAS CYCLED, AND EMERGENCY AIR WAS SERVICED USING PROCEDURES IN THE MFG MM.
Part: FILTER — DIRTY (CABIN PRESSURE)
CABIN WOULD NOT PRESSURIZE. CLEANED PRESSURIZATION JET PUMP FILTER. PERFORMED GROUND PRESSURIZATION CHECK PER MFG MM. AIRCRAF TEST FLOWN AND FOUND SATISFACTORY.
Part: CONNECTOR — LOOSE (PITCH TRIM)
PRIMARY PITCH TRIM WILL NOT PITCH UP. TIGHTENED LOOSE CONNECTOR PLUG AT TWO SPEED TRIM BOX AND RE-SAFTIED. FUNCTIONAL CHECK OF TRIM SYSTEM COMPLIED WITH PER MFG MM.
Part: FIRE LOOP — MALFUNCTIONED (NACELLE)
INTERMITTENT FIRE LIGHT RIGHT SIDE. RE-POSITIONED FIRE DETECT LOOP, WAS MAKING CONTACT WITH COWLING. DETECT SYSTEM OPERATIONALLY, CHECKS GOOD.
Part: RADIO — MALFUNCTIONED (E/E BAY)
REPLACED NR 1 COMM ANTENNA WITH NEW UNIT, PN VF10-347, SN 414. REPAIRED COAX END AT FRAME NR 5 FOR NR 2 COMM AND REPLACED NR 2 COMM WITH SERVICEABLE UNIT MODEL VHF20A, SN 14386. AIRCRAFT HAD LOST ALL COMMUNICATIONS UNTIL THEY WERE CLOSE TO THE STATION. COMM ANTENNA, P/N VJ10-347, S/N 3393.
Part: FILTER — CONTAMINATED (RT ENGINE)
WHILE EN ROUTE, FLIGHT CREW NOTICED RT OIL PRESSURE INCREASE FOLLOWED BY RPM FLUCTUATION. CREW DIVERTED TO MOR. MAINTENANCE FOUND OIL SERVICED TO PROPER LEVEL, HOWEVER, THE OIL FILTER WAS CONTAMINATED. ENGINE WAS REMOVED AND REPLACED.
Part: LINE — FAILED (WHEEL WELL)
WHILE EN ROUTE, HYDRAULIC PRESSURE INDICATION WENT TO ZERO. AIRCRAFT DIVERTED TO TYS FOR LONGER RUNWAYS, A NORMAL LANDING WAS MADE. INSPECTION REVEALED A BROKEN INDICATOR CAPILLARY LINE. LINE WAS REPLACED. HYDRAULIC SYSTEM WAS SERVICED AND INSPECTED.
Part: ENGINE — FAILED (RT ENGINE)
RIGHT ENGINE FLAMED OUT. ADJUSTED FUEL DENSITY. GROUND RUN SATISFACTORY. PERFORMED ALTITUDE ACCELERATION CHECK, ENGINE DID NOT PASS. REPLACED ENGINE WITH SERVICEABLE UNIT.