N24KM

CESSNA 310Q · Fixed-wing multi-engine · 2 engines · 6 seats · Valid Registration

Registered owner: NORTHERN JET INC, MI (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.

3 reports on file, 2002-05-14 – 2004-11-30.

OTHER · 2004-11-30 Matched by certificate designator
ATA 8120

Part: BRACKET — CRACKED (TURBOCHARGER) · airframe 8,756 hrs

A CRACK APPROXIMATELY 2.5 INCHES LONG WAS NOTICED IN THE UPPER PORTION OF THE TURBO CHARGER ATTACH BRACKET. UPON REMOVAL OF FROM THE ENGINE MOUNT NUMEROUS CRACKS WERE NOTED RUNNING ALONG WELDS AND THROUGHOUT THE ENTIRE ASSEMBLY. SUBSEQUENT REMOVAL OF THE TURBO MOUNTING ASSEMBLY ON THE RIGHT ENGINE REVEALED CRACKS IN MANY OF THE SAME AREAS. THE CRACKS ARE DIFFICULT TO DETECT UNLESS THE ASSEMBLY IS REMOVED FROM THE ENGINE MOUNT. BOTH UNITS HAVE 303.5 HOURS SINCE NEW. PICTURES OF THESE UNITS ARE AVAILABLE AT YOUR REQUEST.

Source: SDR H3AA1
OTHER · 2004-11-30 Matched by certificate designator
ATA 8120

Part: BRACKET — CRACKED (TURBOCHARGER) · airframe 8,756 hrs

A CRACK APPROXIMATELY 2.5 INCHES LONG WAS NOTICED IN THE UPPER PORTION OF THE TURBO CHARGER ATTACH BRACKET. UPON REMOVAL OF FROM THE ENGINE MOUNT NUMEROUS CRACKS WERE NOTED RUNNING ALONG WELDS AND THROUGHOUT THE ENTIRE ASSEMBLY. SUBSEQUENT REMOVAL OF THE TURBO MOUNTING ASSEMBLY ON THE RIGHT ENGINE REVEALED CRACKS IN MANY OF THE SAME AREAS. THE CRACKS ARE DIFFICULT TO DETECT UNLESS THE ASSEMBLY IS REMOVED FROM THE ENGINE MOUNT. BOTH UNITS HAVE 303.5 HOURS SINCE NEW. PICTURES OF THESE UNITS ARE AVAILABLE AT YOUR REQUEST.

Source: SDR 24KM1
FLT CONT AFFECTED · 2002-05-14 Unresolved
ATA 2731

Part: CONTROL CABLE — BROKEN (ELEVATOR TRIM) · airframe 8,150 hrs

ELEVATOR TRIM CABLE BROKE WHILE ON APPROACH. CABLE BROKE WHERE IT WRAPPED AROUND AN AUTOPILOT TRIM ACTUATOR THAT HAD BEEN DEACTIVATED. CORRECTIVE ACTION WAS TO REMOVE THE OLD TRIM ACTUATOR AND REPLACE ALL 4 ELEVATOR TRIM CABLES. AS A PRECAUTION ALSO REPLACED THE RUDDER TRIM CABLES.

Source: SDR 2002FA0000642