N558AX
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.
13 reports on file, 2009-05-23 – 2011-11-12.
Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 50,943 hrs · 14,575 cycles
CORROSION ON TOP FLANGE OF FLOORBEAM (TOP AND BOTTOM OF FLANGE) BS 1640. REPAIRED FLOORBEAM IAW MESSAGE FSA-OAE-11-0001-15B.
Part: FLOOR SUPPORT — CORRODED (BS 1640-1680) · corrosion level 2 · airframe 50,943 hrs · 14,575 cycles
CORROSION ON FLOOR SUPPORT AT BS 1640 TO 1680 LBL 54. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-30-01, 51-20-02, 51-20-01, 51-40-02 AND 53-60-51.
Part: FLOOR SUPPORT — CORRODED (BS 1640-1660) · corrosion level 2 · airframe 50,943 hrs · 14,575 cycles
CORROSION ON FLOOR PANEL SUPPORT BL 0, BS 1640 TO 1660. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-30-01, 53-60-51, 51-20-01 AND 51-40-02.
Part: SUPPORT ANGLE — CORRODED (BS 1679) · corrosion level 2 · airframe 50,943 hrs · 14,575 cycles
CORROSION ON SUPPORT ANGLE JUST INSIDE L4 DOOR BS 1679 LBL 52. FABRICATED AND INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-05, 51-20-02, 51-20-01, 51-40-02 AND 53-60-51.
Part: FLOORBEAM — CORRODED (BS 1660) · corrosion level 2 · airframe 50,943 hrs · 14,575 cycles
CORROSION ON FLOORBEAM BS 1660 LBL 52 TO RBL 52 . REPAIRED FLOORBEAM IAW MESSAGE NR FSA-OAE-11-0002-06B.
Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 50,943 hrs · 14,575 cycles
BOTTOM FLANGE OF FLOORBEAM BS 1681, LBL 47 CORRODED. REPAIRED FLOORBEAM IAW MESSAGE FSA-OAE-11-0003-01C.
Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 50,943 hrs · 14,575 cycles
DECK PLATE BETWEEN STA 1681 TO 1720 LBL 51.50 TO RBL 51.50 HAS AREA OF CORROSION. REPAIRED AS REQUIRED CUT OUT DAMAGED AREA FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-60-51, FIG 201 TREATED AND PRIMED AREA IN LIMITS.
Part: FLOOR PANEL — CORRODED (BS 1712) · corrosion level 2 · airframe 50,943 hrs · 14,575 cycles
CORROSION ON DECK PLATE STA 1912, RBL 47 OUT OF LIMITS. CUT OUT DAMAGED AREA FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-60-51, FIG 201, 51-20-01.
Part: FLOORBEAM — CORRODED (BS 335) · corrosion level 2 · airframe 50,943 hrs · 14,575 cycles
AREA OF CORROSION ON FLOORBEAM BS 335, RBL 24 TO RBL 36. FABRICATED NEW FLOORBEAM IAW SRM 53-10-51, FIG 1, 51-30-01 AND 51-20-01.
Part: FLOOR PANEL — CORRODED (BS 1685) · corrosion level 2 · airframe 50,943 hrs · 14,575 cycles
CORROSION ON DECK PLATE IN MAIN CABIN STA 1685 BL 0 IS OUT OF LIMITS. CUTOUT DAMAGE IAW SRM 53-60-51, FIG 201 FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR PARTS ON DECK PLATE STA 1685, BL 0 IAW SRM 53-60-51, FIG 201.
Part: SHEAR WEB — CORRODED (BS 1714-1720) · corrosion level 2 · airframe 50,943 hrs · 14,575 cycles
AFT GALLEY SHEAR WEB DOUBLER IS CORRODED AT LBL 24 TO RBL 24, STA 1714 TO 1720 BS 1681. R & R DOUBLER IAW SRM 53-60-51.
Part: DOUBLER — CORRODED (BS 1681) · corrosion level 2 · airframe 50,943 hrs · 14,575 cycles
AFT GALLEY SHEAR WEB DOUBLER IS CORRODED AT RBL 30 BS 1681. REMOVED AND FABRICATED NEW REPAIR OUT OF 2024-T3 .080 AND INSTALLED NEW REPAIR ON AFT GALLEY SHEAR WEB RBL 30 BS 1681 IAW SRM 53-60-51, FIG 201.
Earlier reports · 2009 · 1 report
2009
Part: UNKNOWN — ODOR (IFE UNIT) · airframe 45,662 hrs · 13,482 cycles
PASSENGER NOTICED ELECTRICAL ODOR AROUND ROW 12. IFE UNIT WAS TURNED OFF. ODOR DISSIPATED AND NEVER RETURNED. OPERATED PASSENGER IFE, OPERATED RECIRC FANS 1 HOUR THERE WERE NO ELECTRICAL ODOR. OK FOR SERVICE. NOTE ACFT HAS OPERATED 12 CYCLES AND 58 HOURS WITH NO REOCCURRENCE.