N608SY
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.
7 reports on file, 2012-05-14 – 2012-05-16.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
PASSENGER CABIN FLOOR SUPPORT INTERCOSTAL IS CRACKED BS 312 RBL 31. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE USING .050" 7075-T6AL AND INSTALLED REPAIR IAW B737-800 SRM 51-70-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,480 hrs · 17,584 cycles
FLOORBEAM CORRODED BS 947 LBL 8 TO RBL 11. REMOVED CORROSION BY BLENDING, MATERIAL LOSS IS OUT OF LIMITS IAW B737-800 SRM 53-70-51. REMOVED THE DAMAGED SECTION OF FLOORBEAM UPPER CHORD. FABRICATED REPAIR UPPER CHORD USING EXTRUSION BAC1505-100658, REPAIR ANGLES USING .100" 7075-T6AL, REPAIR STRAPS USING .125" 7075-T6AL AND SUPPORT CLIPS USING EXTRUSION PM606479. FLOURESCENT PENETRANT INSPECTED CUT EDGES AND REPAIR STRAP -NO DEFECTS NOTED. FLAP PEENED VERTICAL AND HORIZONTAL FLANGES OF T-CHORD. INSTALLED REPAIR PARTS IAW B737 SRM 737-800 53-70-51 REPAIR 5.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,480 hrs · 17,584 cycles
MAIN DECK FLOORBOARD SUPPORT CORRODED BS 944 RBL 36. REMOVED CORROSION FROM SUPPORT, MATERIAL LOSS OUT OF LIMITS IAW B737-800 SRM 53-70-51. REMOVED DAMAGED SUPPORT, FABRICATED REPLACEMENT USING EXTRUSION BAC1509-100505, HEAT TREATED TO CONDITION T73511 IAW BOEING DRAWING 147A5710 AND INSTALLED IAW B737-800 SRM 51-40-02.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,480 hrs · 17,584 cycles
MAIN DECK FLOORBOARD SUPPORT CORRODED BS 962 LBL 17. REMOVED CORROSION FROM SUPPORT, MATERIAL LOSS OUT OF LIMITS IAW B737-800 SRM 53-70-51. REMOVED DAMAGED SUPPORT, FABRICATED REPLACEMENT USING EXTRUSION BAC1506-43 IAW BOEING DRAWING 147A5676 SHIMMED USING .125" 7075-T6AL IAW B737-800 SRM 51-30-01 AND INSTALLED IAW B737-800 SRM 51-40-02.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,480 hrs · 17,584 cycles
AFT CARGO COMPARTMENT FLOOR SUPPORT CHAFED BS 772 LBL 3. REMOVED CORROSION FROM FLOOR SUPPORT, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53. REMOVED DAMAGED AREA OF FLOOR SUPPORT, ACCOMPLISHED HFEC, FABRICATED REPAIR PARTS FROM EXTRUSION BAC1510-1355, FLAP PEENED MACHINED EDGE OF FABRICATED SPLICE CHANNEL AND INSTALLED REPAIR PER AAR EA 14747.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,480 hrs · 17,584 cycles
AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED BS 772 RBL 3. REMOVED CORROSION FROM FLOOR SUPPORT, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53. REMOVED DAMAGED AREA OF FLOOR SUPPORT, ACCOMPLISHED HFEC, FABRICATED REPAIR PARTS FROM EXTRUSION BAC1510-1355, FLAP PEENED MACHINED EDGE OF FABRICATED SPLICE CHANNEL AND INSTALLED REPAIR PER AAR EA 14748.
Part: FLOOR SUPPORT — CHAFED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
AFT CARGO COMPARTMENT FLOOR SUPPORT CHAFED BS 727D+4 LBL 3. REMOVED CHAFING DAMAGE FROM FLOOR SUPPORT, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53. REMOVED DAMAGED AREA OF FLOOR SUPPORT, ACCOMPLISHED HFEC, FABRICATED REPAIR PARTS FROM EXTRUSION BAC1510-1355, FLAP PEENED MACHINED EDGE OF FABRICATED SPLICE CHANNEL AND INSTALLED REPAIR PER AAR EA 14747.