N280L

CIRRUS DESIGN CORP SR22 · 2002 · Fixed-wing single-engine · 1 engine · 4 seats · Valid Registration

Registered owner: VAGIUNIC DAVID, NY (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.

2 reports on file, 2004-07-23 – 2024-04-07.

WARNING INDICATION; FLUID LOSS · 2024-04-07 Matched by certificate designator
ATA 7931

Part: OIL SYSTEM — LOW PRESSURE (RT ENGINE) · airframe 8,382 hrs · 6,647 cycles

DURING CLIMB OUT OF KFXE, R/H ENGINE OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE DROPPED TO ZERO. PILOT IMMEDIATELY SHUTDOWN ENGINE AND RETURNED TO HOMEBASE. AIRCRAFT RETURNED TO BASE LANDING 450 LBS OVER WEIGHT LIMITATIONS. POST FLIGHT INSPECTION REVEALED OIL STREAKS ON R/H ENGINE AND COWLING. TROUBLESHOOTING REVEALED CREW FROM PREVIOUS FLIGHT, AFTER SERVICING ENGINE OIL, DID NOT SECURE OIL CAP.

Source: SDR V6NA2024040801
OTHER · 2004-07-23 Unresolved
ATA 2497

Part: WIRE — CHAFED (ALT OUTPUT) · airframe 770 hrs

ALTERNATOR OUTPUT WIRE CHAFED ON THE RT FWD VALVE COVER AND BURNED A .2500 INCH HOLE IN THE VALVE COVER. WIRE AND BAFFLE ABOVE VALVE COVER NEED TO BE SECURED BETTER. SHORTING OF THE WIRE ALSO CAUSED DAMAGE TO COMPONENTS IN THE MCU AND SUBSEQUENT NR 1 ALTERNATOR FAILURE.

Source: SDR NF22004FCCC