N806SY
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.
43 reports on file, 2003-07-14 – 2012-12-16.
Part: LENS — MISSING (CABIN) · airframe 49,055 hrs · 18,261 cycles
RIGHT FWD OVERWING EXIT LIGHT LENS MISSING. MAINTENANCE INSTALLED NEW EXIT LIGHT LENS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,328 hrs · 17,935 cycles
EMERGENCY EXIT LIGHT INOP AT 14A.
Part: PIN — UNSECURE (EVAC SLIDE) · airframe 48,024 hrs · 17,825 cycles
DURING WALKAROUND FOUND R-1 DOOR SLIDE PIN NOT SECURE INTO SLIDE CONTAINER. MAINTENANCE PERSONNEL REMOVED AND REPLACED R-1 DOOR SLIDE.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
FLOORBEAM CORRODED BS 986 LBL 48 TO RBL 48. REMOVED EXISTING UPPER T-CHORD REPAIR PARTS FROM LEFT AND RIGHT SIDES OF 986 BEAM. FABRICATED NEW REPAIR PARTS FOR THE LEFT SIDE USING EXTRUSION BAC1505-101474 T-CHORD, EXTRUSION BAC1490-2811 AND BAC1490-2885 FOR REPAIR ANGLES AND .080" 7075-T6AL FOR STRAP; RIGHT SIDE MATERIALS USED EXTRUSION BAC1490-101474 FOR T-CHORD, BAC14902865 AND BAC1490-2887 REPAIR ANGLES AND .080" 7075-T6AL STRAP IAW B737-800 SRM 53-70-51. FLAP PEENED THE T-CHORD AND REPAIR PARTS AND INSTALLED IAW B737-800 SRM 53-70-51 REPAIR 4.
Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
MAIN DECK FLOORBEAM CHAFED AT FASTENER HOLES. REMOVED DAMAGED AREA OF UPPER CHORD. FABRICATED REPAIR PARTS USING EXTRUSION BAC1505-101474 FOR T-CHORD, BAC1490-2811 AND BAC1490-2887 FOR REPAIR ANGLES AND .080" 7075-T6AL FOR REPAIR STRAPS. INSTALLED REPAIR PARTS IAW AAR EA 14752 AND SCA EA 53-8462.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,480 hrs · 17,584 cycles
MAIN DECK FLOOR PANEL 241XF UPPER SURFACE IS DELAMINATED. ACCOMPLISHED COMPOSITE REPAIR USING POTTING COMPOUND BMS 5-28, REPAIR FABRIC BMS 9-3, LAMINATING RESIN BMS 8-201 AND ADHESHIVE BMS 5-107.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,480 hrs · 17,584 cycles
MAIN DECK FLOOR PANEL 222BF HAS DELAMINATION DAMAGE. ACCOMPLISHED COMPOSITE REPAIR USING BMS 5-28 POTTING COMPOUND, BMS 9-3 FABRIC, BMS 5-107 ADHESIVE AND BMS 8-201 LAMINATING RESIN IAW B737-800 SRM 53-00-50 REPAIR 1.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,480 hrs · 17,584 cycles
MAIN DECK FLOOR PANEL 221DF HAS DELAMINATION DAMAGE. ACCOMPLISHED COMPOSITE REPAIR USING BMS 5-28 POTTING COMPOUND, BMS 9-3 FABRIC AND BMS 8-201 LAMINATING RESIN IAW B737-800 SRM 53-00-50 REPAIR 4.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,480 hrs · 17,584 cycles
MAIN DECK FLOOR PANEL 221GF HAS DELAMINATION DAMAGE. ACCOMPLISHED COMPOSITE REPAIR USING BMS 5-28 POTTING COMPOUND, BMS 9-3 FABRIC AND BMS 8-201 LAMINATING RESIN IAW B737-800 SRM 53-00-50 REPAIR 4.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,480 hrs · 17,584 cycles
MAIN DECK FLOOR PANEL 221BF HAS DELAMINATION DAMAGE. ACCOMPLISHED COMPOSITE REPAIR USING BMS 5-28 POTTING COMPOUND, BMS 9-3 FABRIC AND BMS 8-201 LAMINATING RESIN IAW B737-800 SRM 53-00-50 REPAIR 4.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
SHEAR TIE CRACKED AT FASTENER HOLE BS 727H STRINGER 27L. REMOVED DAMAGED SHEAR TIE AND REPLACED WITH SERVICEABLE PART IAW B737-800 SRM 51-40-02.
Part: FLOOR SUPPORT — GOUGED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
AFT CARGO FLOOR SUPPORT GOUGED BS 727E+17 LBL 8. REMOVED GOUGE BY BLENDING, FOUND MATERIAL LOSS TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53. REMOVED DAMAGED SECTION OF FLOOR SUPPORT, FABRICATED REPLACEMENT SECTION USING EXTRUSION BAC1509-100146 AND SPLICES USING EXTRUSION BAC1510-1355. INSTALLED REPAIR PARTS IAW B737-800 SRM 53-00-53 REPAIR 4.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
INTERCOSTAL CRACKED BS 500I STRINGER 26L. REMOVED DAMAGED INTERCOSTAL, FABRICATED REPLACEMENT USING .032" 7075-T6AL IAW BOEING DRAWING 143A7503. INSTALLED REPLACEMENT INTERCOSTAL IAW B737-800 SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
PASSENGER CABIN FLOOR PANEL SUPPORT (INTERCOSTAL) IS CRACKED BS 321 LBL 47. FABRICATED REPAIR FILLER USING .040" 7075-T6AL AND DOUBLER .050" 7075-T6AL. INSTALLED REPAIR PARTS IAW B737-800 SRM 51-70-11.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
LIGHTNING STRIKE DAMAGE ON INTERNAL FUSELAGE SKIN BS 727G TO 787 BETWEEN STRINGERS 27L AND 27R. ACCOMPLISHED HFEC INSPECTION ON BOTH SIDES OF SKIN AT DAMAGE LOCATIONS AND VISUAL INSPECTION OF UNDERLYING STRUCTURE - NO FURTHER DEFECTS NOTED. FABRICATED EXTERNAL REPAIR DOUBLER USING .071" 2024-T3AL AND INSTALLED IAW AAR EA 14755.
Part: SKIN — DENTED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
DENTED FUSELAGE SKIN BS 1064 BETWEEN STRINGERS 24R AND 25R. CUT OUT DAMAGED SECTION OF SKIN, ACCOMPLISHED HFEC INSPECTION OF CUTOUT, FABRICATED REPAIR DOUBLER USING .063" 2024-T3AL AND INSTALLED REPAIR IAW B737-800 SRM 53-00-01 REPAIR 3.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
PASSENGER CABIN FLOOR PANEL SUPPORT (INTERCOSTAL) IS CRACKED BS 335 LBL 48. FABRICATED REPAIR FILLER USING .040" 7075-T6AL AND DOUBLER .050" 7075-T6AL. INSTALLED REPAIR PARTS IAW B737-800 SRM 51-70-11.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,480 hrs · 17,584 cycles
FLOOR SUPPORT (INTERCOSTAL) CORRODED BS 952 LBL 51. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS IAW B737-800 SRM 53-70-51. REMOVED DAMAGED INTERCOSTAL, LOCATED AND DRILLED REPLACEMENT PART AND INSTALLED IAW B737-800 SRM 51-40-05.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,480 hrs · 17,584 cycles
AFT CARGO COMPARTMENT FLOOR INTERCOSTAL WEB CORRODED BS 767 - 787 RBL 6. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-01. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED IAW B737 SRM 51-70-13 REPAIR 1.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
CRACKED STRINGER CLIP AT BS 334 STR 25L. REMOVED DAMAGED CLIP. FABRICATED REPLACEMENT CLIP FROM EXTRUSION BAC1493-923 USING BOEING DRAWING 141A3534. INSTALLED REPLACEMENT STRINGER CLIP 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 CORRODED BS 772 RBL 8.1. 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 14749.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,480 hrs · 17,584 cycles
AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED BS 772 LBL 8.1. 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 14746.
Part: FLOOR SUPPORT — CHAFED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
AFT CARGO COMPARTMENT FLOOR SUPPORT HAS CHAFING DAMAGE BS 727 - 847 LBL 13. REMOVED CHAFING DAMAGE, FOUND TO OUT OF LIMITS AT BS 727G LBL 13 IAW B737-800 53-00-53 FIG 103. FABRICATED REPAIR PARTS FROM EXTRUSION BAC1509-1355 AND INSTALLED IAW B737-800 SRM 53-00-53 REPAIR 2.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,480 hrs · 17,584 cycles
AFT CARGO COMPARTMENT FLOOR SUPPORT TRACK CORRODED BS 772 LBL 17.24. 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 BAC1509-100688, FLAP PEENED MACHINED EDGE OF FABRICATED SPLICE CHANNEL AND INSTALLED REPAIR PER AAR EA 14745.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,480 hrs · 17,584 cycles
AFT CARGO COOR SILL PANEL CORRODED IN SEVERAL LOCATIONS. REMOVED CORROSION, FOUND OUT OF LIMITS IAW B737-800 SRM 53-00-01. REMOVED DAMAGED WEB, LOCATED AND DRILLED NEW PART AND INSTALLED IAW B737-800 SRM 51-40-02.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
MAIN DECK FLOOR PANEL SUPPORT CORRODED AT BS 994 LBL 40. REMOVED CORROSION, FOUND OUT OF LIMITS IAW B737-800 SRM 53-70-51. REMOVED DAMAGED FLOOR SUPPORT, FABRICATED REPLACEMENT SUPPORT FROM EXTRUSION BAC1509-100505 USING BOEING DRAWING 147A5710. INSTALLED REPLACEMENT FLOOR SUPPORT USING RIVETS NAS1097D5-4 IAW B737-800 SRM 51-40-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,480 hrs · 17,584 cycles
MAIN DECK FLOORBEAM UPPER CHORD HAS CORROSION AT CLIP NUT LOCATIONS BS 344 LBL 9 TO RBL 7. REMOVED CORROSION, FOUND OUT OF LIMITS IAW B737-800 SRM 53-10-51 FIG 105. FABRICATED FILLERS FROM 7075-T6 AND REPAIR ANGLES FROM EXTRUSION BAC1503-100135 AND FLAP PEENED MACHINED EDGES IAW B737-800 SRM 53-10-51 REPAIR 9. INSTALLED REPAIR PARTS IAW B737-800 SRM 53-10-51 FIG 202.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,480 hrs · 17,584 cycles
MAIN DECK FLOOR SUPPORT INTERCOSTAL CRACKED FROM BS 277 TO 294.5 BUTT LINE 0. REMOVED DAMAGED INTERCOSTAL. FABRICATED REPLACEMENT INTERCOSTAL FROM .040" 7075-T6 AL USING B737-800 SRM 53-10-51 AND INSTALLED IAW B737 SRM 51-40-01.
Earlier reports · 2003–2010 · 15 reports
2010
Part: CIRCUIT BREAKER — POPPED (CABIN) · airframe 42,742 hrs · 15,800 cycles
CABIN FLOOR EMERGENCY TRACK LIGHTING ILLUMINATED IN FLIGHT, PASSENGER CABIN. R AFT BREAKER OUT. RESET BREAKER, PERFORMED TEST PER AMM, NO DEFECTS NOTED.
2007
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 31,451 hrs · 11,302 cycles
DURING A FUNCTIONAL TEST OF THE EMERGENCY LIGHTS, MAINTENANCE FOUND LEFT REAR BIN EMERGENCY EXIT LIGHTS & L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT BATTERY PACK FAILS THE FUNCTIONAL TEST. MAINTENANCE REMOVED & REPLACED THE BATTERY PACK FOR THE LEFT AFT BIN EMERGENCY LIGHTS & L2 EXTERIOR DOOR.
Part: COVER — MISSING (CABIN) · airframe 29,404 hrs · 10,565 cycles
FLIGHT CREW FOUND ROW 12F EXIT SIGN COVER MISSING. MAINTENANCE THEN REPLACED THE COVER.
2006
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,310 hrs · 10,194 cycles
MAINTENANCE FOUND RIGHT FWD OVERWING EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE EMERGENCY LIGHTING BATTERY PACK.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,310 hrs · 10,194 cycles
MAINTENANCE FOUND L-2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT.
Part: HUB — BROKEN (MAIN WHEEL ASSY) · airframe 26,444 hrs · 9,502 cycles
PILOT REPORTED BRAKE/WHEEL DRAGGING AT THE GATE. MAINTENANCE INSPECTION FOUND NR 4 BRAKE HOTTER THAN NORMAL AND REMOVED AND REPLACED THE NR 4 BRAKE. UPON BRAKE REMOVAL, FOUND NR 4 MAIN WHEEL ASSY HUB BROKEN AND REMOVED AND REPLACED THE NR 4 MAIN WHEEL ASSY. INSPECTED AXLE ASSY NO TROUBLES FOUND IAW AMM 32-41-41.
2005
Part: OXYGEN MASK — DEPLOYED (LAVATORY) · airframe 23,889 hrs · 8,611 cycles
CREW REPORTED RIGHT AFT LAVATORY OXYGEN MASK DROPPED. MAINTENANCE RESET OXYGEN MASK DOOR LATCH AND OPERATIONALLY CHECKS GOOD.
Part: BOLT — SHEARED (TE FLAP) · airframe 22,871 hrs · 8,237 cycles
ON POST FLIGHT WALKAROUND, MAINTENANCE FOUND LT INBOARD AFT FLAP DROOPING WITH FLAPS RETRACTED. AFT FLAP ASSY BOLTS WERE SHEARED. MAINTENANCE REPLACED LT INBOARD AFT FLAP LINKAGE MOUNT BOLTS WITH BOLTS, WASHERS & NUTS.
2004
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,915 hrs · 6,808 cycles
CREW REPORTED R2 INTERIOR AND EXTERIOR EMERGENCY LIGHTS DIM. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD.
Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 18,915 hrs · 6,808 cycles
CREW REPORTED AFT RIGHT OVERWING AND MID SECTION OVERHEAD BIN EMERGENCY LIGHTS DIM. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK. OK FOR SERVICE.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 16,419 hrs · 5,848 cycles
FORWARD LEFT BATTERY PACK FOR EMERGENCY LIGHTS DEAD
2003
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 13,809 hrs · 4,713 cycles
EMERGENCY LIGHTS AT 17ABC OFF IN OVERHEAD & SEATS (17 THROUGH 23). REMOVED AND REPLACED POWER SUPPLY & BATTERY PACK AT 21 ABC & CKS GOOD.
Part: LIGHT — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,648 hrs · 4,645 cycles
EMERGENCY LIGHT AT SEAT 6C INOP. RELAMPED EMERGENCY LIGHT. OPS CHECKED GOOD
Part: LIGHT — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,648 hrs · 4,645 cycles
EXTERIOR EMERGENCY LIGHT BEHIND LT GEAR ON FUSELAGE INOPERATIVE. RELAMPED THE EMERGENCY LIGHT. OPS CHECKED GOOD
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,648 hrs · 4,645 cycles
EXTERIOR EMERGENCY OVERWING EXIT LIGHT BEHIND THE AFT LT OVERWING DOOR INOPERATIVE. RELAMPED THE EMERGENCY LIGHT, OPS CHECKED GOOD.