N584NK
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.
9 reports on file, 2004-11-01 – 2007-09-04.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 19,380 hrs · 7,579 cycles
DURING SIMULATED LOSS OF 28VDC CHECK, THE EXIT LIGHTS OVER L1 AND R1 DOORS DO NOT ILLUMINATE. REPLACED BATTERY PACK ON EPSU 10WL.
Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 19,081 hrs · 7,457 cycles
14WL EMERGENCY LIGHTING SYSTEM POWER SUPPLY UNIT FAILED TEST. REPLACED SAME.
Part: ATTACH FITTING — CRACKED (NR 2 PYLON) · airframe 15,046 hrs · 5,831 cycles
NR 2 PYLON OUTBOARD SIDE HAS CRACK ON UPPER METAL STRIP FOR ATTACHMENT OF PANEL 424CR. INSTALLED REPAIR DOUBLER ON NR 2 PYLON OUTBOARD SIDE EXTRUSION PROFILE.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,046 hrs · 5,831 cycles
FLOORBEAM HAS CORROSION FROM FR 13 TO FR 16.
Part: POWER SUPPLY — UNSERVICEABLE (CABIN) · airframe 15,046 hrs · 5,831 cycles
EPSU BAD AT POSITION 15WL. REPLACED EPSU BATTERY PACK.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,046 hrs · 5,831 cycles
CABIN FLOOR AT FRAME 21 AT LBL 44 HAS CORROSION AT FLOOR SUPPORT SEAT TRACK FLANGE. INSTALLED NEW SEAT TRACK SECTION.
Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,046 hrs · 5,831 cycles
LEFT SIDE CABIN FLOOR SHEAR WEB CORROSION ON UPPER AND LOWER SURFACES. INSTALLED NEW SHEAR PLATE.
Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,046 hrs · 5,831 cycles
CABIN FLOOR SPLICE PLATE HAS CORROSION FR 68 RBL 12. REPLACED SPLICE PLATE.
Part: COMPRESSOR — STALLED (RT ENGINE)
LP NR 2907041; SHUTDOWN RT ENGINE, AIR RETURN. RT ENGINE COMPRESSOR STALL ON T/O AFTER V1, PULLED THROTTLE TO IDLE. TRIED ADVANCING POWER AGAIN ANOTER COMPRESSOR STALL AT ABOUT 1.3 EPR, FLEW SINGLE ENGINE APPROACH AND LANDING. REMOVED AND REPLACED RT ENGINE.