N585NK

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.

36 reports on file, 2005-07-20 – 2008-01-24.

NO TEST · 2008-01-24 Matched by certificate designator
ATA 5297

Part: CONNECTOR — DAMAGED (L4 DOOR) · airframe 22,079 hrs · 8,970 cycles

L4 DOOR CONNECTOR 13WL-A PIN "C" TO M FAILED CONTINUITY CHECK. CLEANED AND REINSTALLED WIRE TERMINAL AT 6924VN.

Source: SDR GTIA0800026
OTHER · 2008-01-15 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

CORROSION ON FLOORBEAM AT FRAME 20 AT Y-765, FABRICATED AND INSTALLED PART IAW SRM 53-00-14.

Source: SDR GTIA0800028
OTHER · 2008-01-15 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

Y 765 FLOOR SUPPORT 18-24 HAS CORROSION BEYOND LIMITS. REPLACED FLOOR SUPPORT Y 765.

Source: SDR GTIA0800029
OTHER · 2008-01-15 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

CORROSION ON FLOORBEAM AT Y-254 FRAME 20. FABRICATED AND INSTALLED PART IAW SRM 53-00-14.

Source: SDR GTIA0800027
NO TEST · 2008-01-14 Matched by certificate designator
ATA 5240

Part: MECHANISM — LACK OF LUBE (L4 DOOR) · airframe 22,079 hrs · 8,970 cycles

L4 DOOR FAILED STEP 4AS EMERGENCY CONTROL HANDLE CAN BE ARMED, LUBED AND RIGGED MECHANISM AND CHANGED SLIDE PACK.

Source: SDR GTIA0800025
OTHER · 2008-01-09 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

FOUND FLOORBEAM AT Y-468 AT FRAME 67.5 THRU 69 HAS CORROSION.

Source: SDR GTIA0800019
OTHER · 2008-01-09 Matched by certificate designator
ATA 2565

Part: LEVER — BROKEN (ESCAPE SLIDE) · airframe 22,079 hrs · 8,970 cycles

EMERGENCY EXIT DOOR R3 ESCAPE SLIDE RELEASE MECHANISM LEVER BROKEN IPC25-62-02 ITEM 50. REPLACED LEVER.

Source: SDR GTIA0800022
OTHER · 2008-01-09 Matched by certificate designator
ATA 5315

Part: SPLICE — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

Y-1292 AT FRAME 66 FLOORBEAM SPLICE HAS CORROSION. REPLACED FLOORBEAM SPLICE.

Source: SDR GTIA0800016
OTHER · 2008-01-09 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

FLOORBEAM AT FRAME 67-68, Y-765 CORRODED. REPLACED FLOORBEAM.

Source: SDR GTIA0800030
OTHER · 2008-01-09 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

FLOORBEAM CORRODED AT Y-189 FRAME 20. FABRICATED AND INSTALLED NEW PART IAW SRM 53-00-14.

Source: SDR GTIA0800021
OTHER · 2008-01-09 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

FLOOR SUPPORT AT Y765 AT FRAME 67-69 HAS CORROSION. REPLACED FLOOR SUPPORT.

Source: SDR GTIA0800017
OTHER · 2008-01-09 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

LEFT CORNER WEB CORRODED, FRAME 70 AND Y1292 AT FLOOR LINE. REPLACED LT CORNER WEB.

Source: SDR GTIA0800032
OTHER · 2008-01-09 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CORRODED (BS 4059) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

FS 4059 LT MOST OB INTERCOSTAL HAS CORROSION. REPLACED INTERCOSTAL.

Source: SDR GTIA0800020
OTHER · 2008-01-09 Matched by certificate designator
ATA 5220

Part: LEVER — BROKEN (L3 DOOR) · airframe 22,079 hrs · 8,970 cycles

EMERGENCY EXIT DOOR L3 ESCAPE SLIDE RELEASE MECHANISM LEVER BROKEN IPC25-62-02 ITEM 40. REPLACED LEVER.

Source: SDR GTIA0800023
OTHER · 2008-01-09 Matched by certificate designator
ATA 5315

Part: SPLICE — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

Y+1292 AND FRAME 66 FLOORBEAM SPLICE HAS CORROSION. REPLACED Y+1292 FRAME 66 FLOORBEAM SPLICE.

Source: SDR GTIA0800015
OTHER · 2008-01-09 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

FOUND Y 512 AT FRAME 66 CORRODED. REPLACE Y 512 AT FRAME 66.

Source: SDR GTIA0800018
OTHER · 2008-01-09 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

FLOORBEAM AT L4 DOOR THRESHOLD HAVE INTERGRANULAR CORROSION FROM FRAME 66.5 THRU 69.

Source: SDR GTIA0800014
OTHER · 2008-01-09 Matched by certificate designator
ATA 5220

Part: LEVER — BROKEN (EMERGENCY EXIT) · airframe 22,079 hrs · 8,970 cycles

EMERGENCY EXIT DOOR R2 ESCAPE SLIDE RELEASE MECHANISM LEVER BROKEN IPC25-62-02 ITEM 50. REPLACED LEVER.

Source: SDR GTIA0800024
OTHER · 2008-01-09 Matched by certificate designator
ATA 5310

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 22,079 hrs · 8,970 cycles

Y-1292 FRAME 18-24 HAS CORROSION BEYOND LIMITS. REPAIRED DAMAGED AREA 18-24 Y1292 IAW SRM 51-00-14.

Source: SDR GTIA0800031
OTHER · 2008-01-08 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,079 hrs · 8,970 cycles

FLOOR SUPPORT AT R4 DOOR THRESHOLD HAVE INTERGRANULAR CORROSION FROM FRAME 66.5 THRU 69 \ REPLACED FLOOR SUPPORT.

Source: SDR GTIA0800013
Earlier reports · 2005–2006 · 16 reports

2006

OTHER · 2006-05-28 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

AFT CARGO COMPARTMENT LT FLOOR SUPPORT TRACK FR 47.2 TO FR 48 STRINGER 39L HAS CORROSION. REPAIRED FLOOR SUPPORT TRACK.

Source: SDR GTIA200600064
OTHER · 2006-05-28 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

AFT CARGO COMPARTMENT RT SIDE FLOOR SUPPORT TRACK FR 47.2 TO FR 48 STRINGER 39R HAS CORROSION. REPAIRED FLOOR SUPPORT TRACK.

Source: SDR GTIA200600065
OTHER · 2006-05-27 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

FLOOR SUPPORT (INBOARD OF DOOR 4RT) FR 68 HAS CORROSION. REPLACED FLOOR SUPPORT.

Source: SDR GTIA200600063
OTHER · 2006-05-26 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE HAS CORROSION AT FR 20 AND RBL 53. REPLACED DAMAGED SECTION.

Source: SDR GTIA200600060
OTHER · 2006-05-26 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

AFT CABIN FR 68-69 BL 48 LEFT FLOOR SUPPORT BEAM CORRODED UNDER FLOOR PANEL 261EB. INSTALLED NEW FLOOR SUPPORT BEAM.

Source: SDR GTIA200600056
OTHER · 2006-05-26 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE HAS CORROSION AT FR 21 AND LBL 5. REPLACED DAMAGED AREA.

Source: SDR GTIA200600059
OTHER · 2006-05-26 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

MAIN CABIN FLOOR SUPPORT HAS CORROSION AT FR 16 AND RBL 9. REPLACED DAMAGED AREA.

Source: SDR GTIA200600062
OTHER · 2006-05-26 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE HAS CORROSION AT FR 20 AND RBL 7. REPLACED DAMAGED AREA.

Source: SDR GTIA200600058
OTHER · 2006-05-26 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

MAIN CABIN FLOOR SUPPORT STRUCTURE HAS CORROSION AT FR 21 AND RBL 5. REPLACED DAMAGED AREA.

Source: SDR GTIA200600061
OTHER · 2006-05-26 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

MAIN CABIN FLOOR SUPPORT HAS CORROSION AT FR 16 AND RBL 1. INSTALLED NEW FLOOR SUPPORT.

Source: SDR GTIA200600057
OTHER · 2006-05-26 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

AFT CABIN FR 69 TO FR 70 FLOOR SUPPORT WEB CORRODED AT BL 48 RIGHT. INSTALLED NEW SHEAR WEB.

Source: SDR GTIA200600067
OTHER · 2006-05-26 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

MAIN CABIN CORROSION SEAT TRACK FRAME 20 LBL 40. REPLACED DAMAGED AREA.

Source: SDR GTIA200600055
OTHER · 2006-05-26 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

MAIN CABIN CORROSION ON SEAT TRACK RBL 20 FR 20. REPLACED DAMAGE SECTION.

Source: SDR GTIA200600054
OTHER · 2006-05-26 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

MAIN CABIN FLOOR SUPPORT IS CORRODED BETWEEN FR 12 TO FR 16 AT LBL 21. INSTALLED NEW FLOOR SUPPORT.

Source: SDR GTIA200600053
OTHER · 2006-05-26 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,377 hrs · 6,718 cycles

AFT CABIN FR 69 TO FR 70 FLOOR SUPPORT WEB AT BL 48 LEFT CORRODED. INSTALLED NEW SHEAR WEB.

Source: SDR GTIA200600066

2005

OTHER · 2005-07-20 Matched by certificate designator
ATA 2565

Part: SLIDE — DEPLOYED (PAX DOOR)

FLT 507 - FLL - FOUND FORWARD SLIDE ACCIDENTALLY DEPLOYED AT THE GATE, SLIDE PACK DID NOT FULLY INFLATE DUE TO A RUPTURED LINE ON THE CHARGE BOTTLE. (M)

Source: SDR GTIA050216