N583NK

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
SPIRIT AIRLINES, LLC (GTIA)Operatoron 2005-09-18Operator named in NTSB report

Accident & incident history

Accident · 2005-09-18 Operator named in NTSB report
Airbus A321-231 No injuries Part 121SPIRIT AIRLINES, LLC

Operated by SPIRIT AIRLINES INC (per NTSB report)

Source: NTSB case DCA05MA099

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.

11 reports on file, 2005-05-21 – 2007-08-17.

OTHER · 2007-08-17 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,490 hrs · 8,875 cycles

MAIN DECK FLOOR SUPPORT STRUCTURE (BEAM) CORRODED LT Y503.2 BETWEEN FR14 AND FR16. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW 51-42-11.

Source: SDR GTIA0800036
OTHER · 2006-05-02 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,022 hrs · 7,121 cycles

FOUND CORROSION ON FLOOR STRUCTURE FLOOR SUPPORT Y-129 AT FS 21. REMOVED CORROSION, REPAIRED.

Source: SDR GTIA200600028
OTHER · 2006-04-29 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,022 hrs · 7,121 cycles

FOUND CORROSION ON FLOOR STRUCTURE FLOOR SUPPORT Y503.2 AT FS 16. BLENDED CORROSION. REMOVED DAMAGED TOP STRAP. INSTALLED DOUBLER.

Source: SDR GTIA200600024
OTHER · 2006-04-29 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,022 hrs · 7,121 cycles

FOUND CORROSION ON FLOOR STRUCTURE FLOOR SUPPORT Y254 AT FR 16. REMOVED AND REPLACED FLOOR SUPPORT.

Source: SDR GTIA200600022
OTHER · 2006-04-29 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,022 hrs · 7,121 cycles

FOUND CORROSION ON FLOOR STRUCTURE FLOOR SUPPORT Y765 AT FS 16. REMOVED CORROSION, OUT OF LIMITS, REPAIRED.

Source: SDR GTIA200600025
OTHER · 2006-04-29 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,022 hrs · 7,121 cycles

FOUND CORROSION ON FLOOR STRUCTURE FLOOR SUPPORT Y254 AT FS 21. REMOVED AND REPLACED FLOOR SUPPORT.

Source: SDR GTIA200600021
OTHER · 2006-04-29 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,022 hrs · 7,121 cycles

FOUND CORROSION ON FLOOR STRUCTURE FLOOR SUPPORT Y-254 AT FS 20. CUT OUT DAMAGED AREA, REPAIRED.

Source: SDR GTIA200600026
OTHER · 2006-04-29 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,022 hrs · 7,121 cycles

FOUND CORROSION ON FLOOR STRUCTURE FLOOR SUPPORT Y503.2 FWD OF FS 16. REPLACED CORRODED AREA.

Source: SDR GTIA200600023
OTHER · 2006-04-29 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,022 hrs · 7,121 cycles

FOUND CORROSION ON FLOOR STRUCTURE FLOOR SUPPORT Y-254 AT FS 16. REMOVED CORROSION. FLOOR SUPPORT REPAIRED. PILOT DRIVED DOUBLERS.

Source: SDR GTIA200600027
OTHER · 2005-09-19 Matched by certificate designator
ATA 5330

Part: STRUCTURE — GROUND DAMAGE (FUSELAGE) · airframe 16,473 hrs · 6,451 cycles

PERFORMED HARD LANDING/ OVERWEIGHT LANDING INSPECTION, FOUND DAMAGE AT LOWER TAIL SECTION BETWEEN FR67-FR68 IAW AMM, NO ADDITIONAL DAMAGE NOTED. INSTALLED INTERM REPAIR IAW EA AND DWG, AIRCRAFT FERRIED FOR REPAIR. PERMANENT REPAIR ACCOMPLISHED, AIRCRAFT OK FOR CONTINUED SERVICE. (K)

Source: SDR GTIA050267
OTHER · 2005-05-21 Matched by certificate designator
ATA 3350

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

SEVERAL LIGHTS BURNED OUT IN EMERGENCY EXITS SIGNS ABOVE L1, R1 AND R4 DOORS, AIRCRAFT TAIL SWAP WITH N825NK. RELAMPED EMERGENCY EXIT SIGNS IN CABIN AS REQUIRED, OPS CHECK GOOD. (M)

Source: SDR GTIA050157