N251FL

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.

8 reports on file, 2012-02-07 – 2014-06-24.

OTHER · 2014-06-24 Matched by certificate designator
ATA 5350

Part: FAIRING — DAMAGED (ZONE 100) · airframe 61,587 hrs · 37,860 cycles

FAIRING ADJACENT TO LEFT PACK COOLING DOOR DAMAGED.

Source: SDR VGCA20140624004
OTHER · 2013-05-28 Matched by certificate designator
ATA 5320

Part: SUPPORT FITTING — CORRODED (ZONE 500) · airframe 66,773 hrs · 37,349 cycles

CORROSION ON LT WING FUELAGE TERMINAL FITTING.

Source: SDR VGCA20130528001
OTHER · 2013-05-28 Matched by certificate designator
ATA 5343

Part: SUPPORT BEAM — CORRODED (ZONE 700) · airframe 66,773 hrs · 37,349 cycles

CORROSION ON LT MLG BEAM AT NR 4 FLAP TRACK ATTACH POINT AROUND BOLTS.

Source: SDR VGCA20130528005
OTHER · 2013-05-28 Matched by certificate designator
ATA 2810

Part: FUEL TANK — CORRODED (ZONE 600) · airframe 60,773 hrs · 37,349 cycles

RIGHT SIDE AFT UPPER SURFACE OF FUEL TANK AT FS 850 CORRODED.

Source: SDR VGCA20130528002
OTHER · 2013-05-28 Matched by certificate designator
ATA 5320

Part: SUPPORT FITTING — CORRODED (ZONE 500) · airframe 66,773 hrs · 37,349 cycles

CORROSION ON LT WING FUSELAGE TERMINAL FITTING.

Source: SDR VGCA20130528003
OTHER · 2013-05-28 Matched by certificate designator
ATA 5343

Part: SUPPORT BEAM — CORRODED (ZONE 700) · airframe 66,773 hrs · 37,349 cycles

CORROSION ON BOTTOM SIDE OF RT MLG SUPPORT BEAM AT NR 5 FLAP TRACK ATTACH POINT.

Source: SDR VGCA20130528004
OTHER · 2012-10-10 Matched by certificate designator
ATA 5330

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,496 hrs · 37,176 cycles

UPPER FUSELAGE SKIN DAMAGED.

Source: SDR VGCA20121010
OTHER · 2012-02-07 Matched by certificate designator
ATA 5310

Part: DOOR FRAME — CRACKED (BS 1090) · airframe 60,297 hrs · 37,060 cycles

THREE INCH CRACK FOUND ON NR 3 CARGO DOOR FWD FRAME AT S-26R ON FRAME 1090 WHILE COMPLYING WITH AD2006-13-01/SB 53A0169.

Source: SDR VGCA20120207