N680AC
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.
6 reports on file, 1998-06-26 – 2019-08-07.
Part: STRINGER — CORRODED (FRAMES 31-32) · corrosion level 2 · airframe 18,959 hrs · 11,361 cycles
FORWARD PIT BILGE AREA SKIN AND STRINGER CORROSION FR 32-31, STR 39-43LT
Part: STRINGER SPLICE — CORRODED (FRAMES 31-32) · corrosion level 2 · airframe 18,959 hrs · 11,361 cycles
FORWARD PIT BILGE AREA SKIN AND STRINGER CORROSION FR 32-31, STR 39-43LT.
Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 18,959 hrs · 11,361 cycles
CORROSION AROUND 3EA FASTENER HOLES IN THE FWD MAIN CABIN FLOOR PNL ADJACENT TO THE L1 DOOR, FWD SIDE SURFACE.
Part: SUPPORT FRAME — CORRODED (FRAME 70) · corrosion level 2 · airframe 181,959 hrs · 11,361 cycles
AFT CABIN FLOOR 7" FWD OF FRAME70 LH SHEAR PLATE HAS CORROSION.
Part: SHEAR PLATE — CORRODED (FRAME 70) · corrosion level 2 · airframe 18,959 hrs · 11,361 cycles
AFT CABIN FLOOR 7" FWD OF FR70 SHEAR PLATE HAS CORROSION
Part: VALVE — FAILED (LT ENGINE)
BIL - PILOT REPORTED A LOSS OF MANIFOLD PRESSURE ON THE LT ENGINE IN CRUISE AND OIL LEAKING FROM LT ENGINE AFTER SHUT DOWN IN BILLINGS. AIRCRAFT LANDED WITHOUT INCIDENT, NO EMERGENCY DECLARED. LEFT ENGINE, NR 2 CYLINDER EXHAUST VALVE FAILED, DAMAGE CAUSED TO CYLINDER, PISTON AND CYLINDER SUBASSEMBLIES. ALL DAMAGED COMPONENTS WILL BE REPLACED WITH SERVICEABLE COMPONENTS AND OPERATIONALLY CHECKED.