N260VP

No registry detail on file · not in current registry

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, 2004-05-14 – 2004-08-09.

VIBRATION/BUFFET · 2004-08-09 Unresolved
ATA 3240

Part: BRAKE — OUT OF ADJUST (MLG)

ON DEPARTURE FROM MKE, CREW NOTED A SHIMMY IN THE NOSE WHEEL AND ABORTED TAKEOFF. INSPECTION FOUND NOSE GEAR FRICTION BRAKE DRAG LOW. ADJUSTED FRICTION BRAKE PER CE650 MM. COMPLETED HIGH SPEED (100 KTS) TAXI CHECK WITH NO SHIMMY EVIDENT. RELEASED AIRCRAFT FOR SERVICE. (M)

Source: SDR 2004FA0000872
ENGINE STOPPAGE; WARNING INDICATION · 2004-06-14 Matched by certificate designator
ATA 7200

Part: ENGINE — FAILED (NR 1)

AFTER TAKEOFF, FLIGHT CREW NOTICED LOUD RUMBLE FOLLOWED BY NR 1 ENGINE SPOOLING DOWN. ITT INDICATED 1000 DEGREE CENTIGRADE WITH OVERTEMP LIGHT. FLIGHT CREW SECURED NR 1 ENGINE AND RETURNED LANDING WAS UNEVENTFUL. INITIAL VISUAL INSPECTION SHOWED NO SIGN OF FOD DAMAGE TO COMPRESSOR OR HIGH PRESSURE TURBINE. ENGINE REMOVED BY MFG SPI FOR TEARDOWN AND INSPECTION. FOLLOW-UP WILL BE SUBMITTED WHEN CAUSE OF SHUTDOWN IS DETERMINED, TO INCLUDE PN AND TIME/CYCLES ON FAILED PART.

Source: SDR DBCR122D
F.O.D.; WARNING INDICATION · 2004-05-14 Matched by certificate designator
ATA 7200

Part: ENGINE — FOD (NR 1)

AFTER TAKEOFF, FLIGHT CREW NOTICED LOUD RUMBLE FOLLOWED BY NR 1 ENGINE SPOOLING DOWN. ITT INDICATED 1000 DEGREE CENTIGRADE WITH OVERTEMP LIGHT. FLIGHT CREW SECURED NR 1 ENGINE AND RETURNED TO OMA. LANDING WAS UNEVENTFUL. INITIAL VISUAL INSPECTION SHOWED NO SIGN OF FOD DAMAGE TO COMPRESSOR OR HIGH PRESSURE TURBINE. ENGINE REMOVED BY MFG, SPI FOR TEARDOWN AND INSPECTION. FOLLOW-UP WILL BE SUBMITTED WHEN CAUSE OF SHUT-DOWN IS DETERMINED TO INCLUDE PN AND TIME/CYCLES ON FAILED PART.

Source: SDR DBCA122D3