N805SY

Service difficulty reports · 190

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N805SY' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SCNA20210915080Frame Angle · crackedANGLE ON FWD SIDE OF FRAME IS CRACKED BS 500D LBL 25 CARGO FLOOR. CRACK ON ANGLE FWD OF FRAME 500D LBL 25 FOUND TO BE OUT OF LIMITS IAW 5RM53-00-53-1A-2 REV 73. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-06-0 REV 73, BOEING DWG 143A7505 REV A.Sep 15, 2021 · N805SY · Boeing 7378Q8 · Fuselage Main, FrameSDR SCNA20210915079Web · damagedE&E BAY DOOR CUTOUT L/H WEB IS DAMAGED. REMOVED DAMAGE E+E BAY DOOR CUTOUT WEB CBS 323-351 LBL 15 IAW SRM 737-800 51-40-02-0G FABRICATED WEB OUT OF 7075T6 .040 LOT # 5105057-1 ALODINE AND PRIMER NEW WEB IAW SRM 52-10-13-2A-3 REV 73 AND DRAWING PL141A8512 REV ESep 15, 2021 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20210914078Baffle · crackedBAFFLE CRACKED BETWEEN BS 500C AND 500D LBL25 STRINGER 26 L/H. CRACK BAFFLE 500C AND TO 500D LBL25 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REV. 73, REMOVED AND REPLACED BAFFLE IAW SRM 51-40-02-06-0 REV 73, BOEING DWG 143A7505 REV A.Sep 1, 2021 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20210927082None · noneCORROSION FLOOR TO SIDEWALL SUPPORT (ZEE CHANNEL) BS 500G +11 TO 500I RBL 25. CORROSION ON SIDEPLATE STA. 500G-500I RBL 25 FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLE IAW SRM 53-00-53-1A-2 DETAIL "D" REV 73. REMOVED AND REPLACED SIDEPLATE WITH Aug 28, 2021 · N805SY · Boeing 7378Q8 · Fuselage Structure (General)SDR SCNA2019101403204Web · crackedWEB FOUND TO BE CRACKED ON R/H WHEEL WELL WEB DURING AFT OUTBOARD WING TO BODY FAIRING MODIFICATION. REMOVED AND REPLACED WEB.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA2019101403197Scuff Plate · corrodedL1 DOOR CUT OUT WL 208.1 BTW STA 312 TO STA 339 SCUFF PLATE ATTACH POINT CORRODED ON MULTIPLE AREAS (DOT# AVG 004). ACCOMPLISHED REMOVAL AND INSTALLATION OF THE SCUFF PLATE ATTACH POINT.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA2019101403195Window Frame · crackedCRACK FOUND ON THE L/H #1 WINDOW FRAME. INSTALLED REPAIR IN ACCORDANCE WITH SB 737-53-1336.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Main, StructureSDR SCNA2019101403200Brace · corrodedPITTING FOUND ON L/H OUTBOARD BRACE FOR THE L/H WHEEL WELL RING SUPPORT ASSEMBLY. BLENDED DAMAGE PER SRM 51-10-02.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Main, StructureSDR SCNA2019101403203Repair · corrodedDURING CORROSION REMOVAL AN EXISTING INCOMING REPAIR HAD CORROSION ON TAPERED REPAIR REQUIRES REMOVAL AND REINSTALL OF NEW REPAIR. @ STA 967. REMOVED AD REPLACED UPPER CHORD REPAIR PER 737-800 SRM 53-70-51 REP 6 ON BS 967. LBL 47.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Structure (General)SDR SCNA2019101403202Floor Panel · damagedAFT CARGO PANEL 140CF DAMAGED. FABRICATED, LOCATED ANOL DRILLED NEW FLOOR PANEL IAW B-737-800 SRM 53-60-53 FIG2 TABLE 2 ITEM 1 ANOL SRM 51-40-05 FIG 2.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Floor PanelSDR SCNA2019101403201Mount · damagedBOTH REAR GALLEY MOUNTS OR FITTING ASSY HAVE HARDWARE STUCK IN THEM AND HEAVY CORROSION. FABRICATED GALLEY MOUNTS FITTING ASSY 40 IAW B737-800 DWG #415N4002-39 REV:B.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Main, Attach FittingsSDR SCNA2019101403199Scuff Plate · damagedAFT CARGO DOOR FWD SCUFF PLATE DAMAGED. LOCATED AND DRILLED NEW AFT LOGO FWD SCUFF PLATE ALL WORK DONE IAW B737-800 SRM 51-40-05 AND SRM 51-40-08.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Cargo/Baggage DoorsSDR SCNA2019101403198Door Sill · corrodedAFT CARGO DOOR LOWER SILL SUPPORT PLATE AND FASTENER HOLES CORRODED FROM STA 788 TO STA 847. BETWEEN APROX STR 24R TO 25R. REMOVED AND REPLACED WEB IN AFT CARGO DOOR LOWER SILL IAW B737-800 SRM 51-40-02.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA2019101403196Sleeve · crackedAPPROXIMATELY 3 INCHES CRACK AT #2 THRUST REVERSER SLEEVE SKIN JUST AFT OF INBOARD TORQUE BOX. (DOT NO. SKN 074). REMOVED AND REPLACED ENGINE #2 THRUST REVERSER SLEEVE SKIN FAIRING. ALL WORK DONE IAW B737-800 AMM 78-31-02 AND SRM 51-40-02.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Engine Thrust ReverserSDR SCNA2019101403194Crease Beam · corrodedCORROSION ON CREASE BEAM RBL48, W.L 208, BETWEEN B.S 328-B.S 294. REMOVED AND REPLACED CREASE BEAM RBL 48 WL208 BTW STA 328-294. ALL WORK DONE IAW B737-800 SRM 53-10-15, 51-40-02 AND 51-40-05.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Main, StructureSDR SCNA2019101403193Insert · corrodedCORRODED INSERT AT B.S 328 AT RBL 40, W.L 208. REMOVED AND REPLACED INSERT AT B.S 328 AT RBL 40, W.L 208 IAW B737 SRM 53-00-50 STEP 5 (S)(1,2).Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA2019101403192Insert · corrodedCORRODED INSERT AT RBL 7 FWD OF B.S 344 W.L 208. REMOVED AND REPLACED INSERT AT RBL 7 FWD OF B.S 344 W.L 208 IAW B737-800 SRM 53-00-50 STEP 5 (5) (1, 2).Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA2019101403191Crease Beam · corrodedCREASE BEAM CORRODED FROM B.S 344-B.S 312, LBL 48, W.L 208. REMOVED AND REPLACED LOOSE BEAM FROM STA. 312 TO STA. 344, LBL 48. ALL WORK DONE IAW B737-800 SRM 53-10-15, SRM 51-40-02, SRM 51-40-05.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Main, StructureSDR SCNA2019101403190Floorbeam · corrodedCORROSION ON FLOOR BEAM AT B.S. 328, RBL 48, W.L 208. REMOVED AND REPLACED ON FLOOR BEAM AT B.S. 328, RBL 48 W.L.208 ALL WORK DONE IAW B737-800 SRM 53-1051 STEP4 (C) 2, SRM 51-40-02 SRM 53-10-51 REPAIR 7. SRM 51-40-05, AMM 51-21-41 AMM 51-21-72, AMM 20-10-09 AOct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Main, Floor BeamSDR SCNA2019101403189Panel · wornPANEL 193AL WORN THROUGH OUTTER LAYERS TO HONEY COMB ON BACK SIDE OF PANEL. REPAIRED PANEL 193AL OUTER LAYERS TO HONEY COMB ON BACK SIDE OF PANEL IN REF. TO B737-800 SRM 53-40-70; B757-800 SRM 51-70-04.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Structure (General)SDR SCNA2019101403188Floor Support · corrodedCORROSION ON FLOOR SUPPORT WEB FROM STA 1006 TO STA 1015 , APROX. BL0. REMOVED AND REPLACED FLOOR SUPPORT STRAP FROM STA 1006 TO STA 1015 APPROX BL 0 IAW B737-800 SRM 51-40-02Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA2019101403187Fairing · damaged3 LH FLAP FAIRING AFT INBD HAS SCREWS RECESSED INTO SKIN. REMOVED, REPAIRED, AND INSTALLED #3 LH FLAP FAIRING IB; 113A9356 TAILCONE IN REF. TO B737-800 AMM 27-51-18 PG. 401 AND B737-800 AMM 27-51-18-010-003.Oct 3, 2019 · N805SY · Boeing 7378Q8 · Trailing Edge FlapsSDR SCNA2019101403186Floor Support · corrodedCORROSION ON FLOOR SUPPORT STRUCTURE FROM STA 1006 TO STA 1016 , LBL APROX. 20" AND AROUND FASTENER HOLES.REMOVED AND REPLACED FLOOR STRAP ON SUPPORT STRUCTURE FROM STA 1006 TO STA 1016 IAW B737-800 SRM-51-40-02Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA2019101403185Floor Support · corrodedCORROSION ON FLOOR SUPPORT ANGLE FROM STA 986.5 TO STA 1016 AND AROUND FASTENER HOLES. REMOVED AND REPLACED FLOOR SUPPORT STRAP FROM STA 986.5 TO STA1016 IAW B737-800 SRM 51-40-02Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA2019101403184Floorbeam · corrodedCORROSION AND BARE METAL ON FLOOR BEAM CAPAND AROUND FASTNER HOLES AT STA 986. REMOVED & REPLACED T-CUP @STA. 986.5 ALL WORK ACCOMPLISHED IAW B737-800 SRM 53-70-51 REPAIR 4., 51-40-02, 51-20-05Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Main, Floor BeamSDR SCNA2019101403178Floorbeam · corrodedAFT PAX. CABIN FLOORBEAM CAP AT BS 947.5 CORRODED AROUND FASTNER HOLES AT UPPER AND LOWER SURFACES. FABRICATED REPAIR STRAP FOR STA. 947.5 FLOOR ROOM. ALL WORK DONE IAW B737-800 SRM 51-10-02, SRM 53-70-51 REPAR 6 FIG 204, SRM 51-40-05, AMM 51-21-41 AND AMM 51Oct 3, 2019 · N805SY · Boeing 7378Q8 · Fuselage Main, Floor BeamSDR SCNA20190102001Battery Pack · dischargedROWS 7-11 ABC EMER LIGHTS INOP. R/R M1676 BATTERY PACK. OPS CHK GOOD.Jan 2, 2019 · N805SY · Boeing 7378Q8 · Emergency LightingSDR SCNA20180926115Antenna · damagedHF ANTENNA MISSING PAINT. HF ANTENNA FIBERGLASS IS DAMAGED BEYOND LIMITS. HF ANTENNA FIBERGLASS IS DAMAGED BEYOND LIMITS. NEW ANTENNA ON ORDER. REMOVED AND INSTALLED HF ANTENNA. VERTICAL FIN SIDE FASTENERS INSTAELLD. COUPLER SLEEVE AND FEEDER TUBE TO BE INSTASep 26, 2018 · N805SY · Boeing 7378Q8 · Vertical StabilizerSDR SCNA201809286114Skin · worn#4 SLAT UNDERSIDE INBD CORNER SKIN WORN THRU ALUMINUM DOWN TO COMPOSITE MATERIAL. STILL IN WORK. ADDITIONAL INFORMATION TO BE PROVIDED. #4 SLAT SKIN TOP UNDERSIDE ALUMINUM WORN TO COMPOSITE MATERIAL APPROX 3" LEGNTH AND GREATER THAN .625" IN WIDTH. #4 SLATSep 26, 2018 · N805SY · Boeing 7378Q8 · Leading Edge DevicesSDR SCNA20180926113Skin · damagedNUMBER 7 SLAT, BOTH ENDS, UNDERSIDE OTBD CORNERS HAVE WORN THRU ALUMINUM SKIN AND COMPOSITE IS EXPOSED. #7 SLAT UPPER CORNERS(INBD AND OUTBD) UNDERSIDE ALUMINUM SKIN WORN TO THE COMPOSITE MATERIAL IS GREATER THAN .625" IN WIDTH AND APPROX 3" IN LEGNTH EACH. Sep 26, 2018 · N805SY · Boeing 7378Q8 · Leading Edge DevicesSDR SCNA201809286112Skin · wornNUMBER 5 SLAT, INBD, AFT LOWER CORNER HAS WORN THREW ALUMINUM SKIN AND UNDERLYING COMPOSITE IS SHOWING. STILL IN WORK. ADDITIONAL INFORMATION TO BE PROVIDED.Sep 26, 2018 · N805SY · Boeing 7378Q8 · Leading Edge DevicesSDR SCNA201809286111Skin · cracked#5 SLAT SKIN CRACKED AT ACTUATOR ATTACH POINT. #5 SLAT SKIN CRACK END POINT MARKED AND VISUALLY MEASURED AT 7/16". #5 SLAT HAS BEEN REMOVED. COMPLETED INTERFACE INSPECTION ON #5 SLAT, OK TO INSTALL. INSTALLED #5 SLAT. N/R REMAINS OPEN FOR RIGGING. RII ACCOMPSep 26, 2018 · N805SY · Boeing 7378Q8 · Leading Edge DevicesSDR SCNA201809286110Skin · cracked#4 SLAT SKIN CRACKED AT ACTUATOR ATTACH POINT. #4 SLAT SKIN CRACK END POINT MEASURED VISUALLY APPROXIMATELY 1/4". #4 SLAT HAS BEEN REMOVED. RII ACCOMPLISHED ON INTERFACE INSPECTION. OK TO INSTALL #4 SLAT. INSTALLED #4 SLAT. NOTE INBOARD PRELOAD ADJUST BOLT RSep 26, 2018 · N805SY · Boeing 7378Q8 · Leading Edge DevicesSDR SCNA201809286109Skin · cracked#1 SLAT SKIN CRACKED AT ACTUATOR ATTACH POINT. STILL IN WORK. ADDITIONAL INFORMATION TO BE PROVIDED. MARKED END OF CRACK ON #1 SLAT SKIN VISUALLY AT 7/16". REMOVED #1 SLAT. RII ACCOMPLISHED ON INTERFACE INSPECTION. OK TO INSTALL #1 SLAT. INSTALLED #1 SLAT Sep 26, 2018 · N805SY · Boeing 7378Q8 · Leading Edge DevicesSDR SCNA201808098100Rib · corrodedLEFT WINGLET RIB WAS CORRODED ON THE OUTBOARD SIDE. REMOVED AND INSTALLED LEFT WINGLET. CHECKED GOOD AND SEALED.Aug 8, 2018 · N805SY · Boeing 7378Q8 · Wing Main, Frame StructureSDR SCNA2018080229099Battery Pack · dischargedEMER LIGHT BATTERY PACKS AT 13 ABC, 13 DEF INOP. REMOVED AND REPLACED BATTERY PACKS. OPS CHECK GOOD.Jul 29, 2018 · N805SY · Boeing 7378Q8 · Emergency LightingSDR SCNA20180209061Skin · wornNR 3 LE SLAT TRAILING EDGE WEDGE LOWER SKIN WEAR DAMAGE AT BOTH INBD AND OUTBD ENDS. TRIMMED OUT WEAR DAMAGE. FABRICATED AND INSTALLED 70756 REPAIR FILLER. TREATED, PRIMED AND APPLIED TOPCOAT.Feb 9, 2018 · N805SY · Boeing 7378Q8 · Leading Edge DevicesSDR SCNA20180209060Skin · crackedNR 6 SLAT SKIN CRACKED AT ACTUATOR. REMOVED NR 6 SLAT. INSTALLED NR 6 LEADING EDGE SLAT. OPS CHECKS GOOD, ALL SLAT PANELS REINSTALLED. RII ACCOMPLISHED.Feb 9, 2018 · N805SY · Boeing 7378Q8 · Leading Edge DevicesSDR SCNA20180209059Panel · delaminatedNR 1 ENG STRUT PANEL 434BL LOWER AFT CORNER HAS DELAMINATION AND EDGE EROSION. PERFORMED REPAIR TO PANEL 434BL. PANEL 434BL RE-INSTALLED.Feb 9, 2018 · N805SY · Boeing 7378Q8 · Nacelle/Pylon, Plate/SkinSDR SCNA20180209058Skin · crackedDURING REMOVAL OF NR 3 SLAT, S/N 000999 FOUND POSSIBLE CRACK AT THE LEADING EDGE SKIN AS MARKED. APPROX LOCATION OPPOSITE OF ACTUATOR LUG. GAINED ACCESS, CUT OUT DAMAGE. NEEDS HFEC FOR CUT-OUT, OPEN HOLE AND COUNTERSINKS. HFEC INSPECTIONS ACCOMPLISHED. NO CRACFeb 9, 2018 · N805SY · Boeing 7378Q8 · Leading Edge DevicesSDR SCNA20170922198Web · corrodedFOUND CORROSION ON WEB UNDER SCUFF PLATE FWD CARGO DOOR. REMOVED SCUFF PLATE IN FRONT OF FWD CARGO DOOR AND FWD AND AFT CORNER PIECES CARGO FLOOR FOR DOOR ALL PIECES IN CARGO PIT. REMOVED SUB FLOOR WEB, REMOVED NUT PLATES FROM OLD WEB, MANUFACTURED DRILL BUSHSep 22, 2017 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20170922197Structure · damagedHOLE IN FWD CARGO FLOOR AT APPROX STA 500B LBL 16. REPAIRED HOLE IN FWD CARGO FLOOR AT STA 500B LBL 16.Sep 22, 2017 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20170605088Battery Pack · no testFWD LT & RT, MID LT & RTH, AFT LT & RT EMERGENCY LIGHT BATTERIES FAILED A FUNCTIONAL CHECK. REMOVED AND REPLACED THE BATTERY PACKS. OPS CHECKED GOOD.Jun 5, 2017 · N805SY · Boeing 7378Q8 · Emergency LightingSDR SCNA20161023249Light · inoperativeSEAT 24DEF OVERHEAD BIN EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED M1672 EMERGENCY EXIT LIGHT BATTERY PACK AND POWER SUPPLY. OPS CHECKED GOOD. OK FOR SERVICE.Oct 23, 2016 · N805SY · Boeing 7378Q8 · Emergency LightingSDR SCNA20160614085Seat Track · damagedPASSENGER CABIN SEAT TRACK AT 727B + 1" FASTENER HEAD IS SHEARED OFF RBL 25. R & R FASTENERS.Jun 14, 2016 · N805SY · Boeing 7378Q8 · Fuselage, Seat/Cargo Attach FittingsSDR SCNA20160614084Stiffener · crackedLT HORIZONTAL STABILIZER, AT BS 101.90, FIRST VERTICAL STIFFENER FROM FWD SPAR IS CRACKED. REMOVED CRACK FROM VERTICAL STIFFENER AND WEB AT BS 101.9 OF LT STABILIZER ACCOMPLISHED HFEC OF REMOVED DAMAGE AREA. NO DEFECTS NOTED. FABRICATED, LOCATED & DRILLED Jun 14, 2016 · N805SY · Boeing 7378Q8 · Horizontal Stabilizer StructureSDR SCNA20160614083Crease Beam · corrodedCABIN, CREASEBEAM CORRODED STA 967 TO 990, IN AREA OF DOOR 2 LT. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CREASEBEAM. LOCATED DRILLED NEW CREASE BEAM TREAT PRIMED INSTALLED.Jun 14, 2016 · N805SY · Boeing 7378Q8 · Fuselage Main, StructureSDR SCNA20160614082Floor Support · crackedFORWARD CABIN, FLOOR INTERCOSTAL CRACKED IN RADIUS, BS 322, LBL 47". R & R INTERCOSTAL BS 322, LBL 47.Jun 14, 2016 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20160614081Floor Support · crackedFORWARD CABIN AREA, FLOOR INTERCOSTAL CRACKED AT BS 317, RBL 31. R & R INTERCOSTAL BS 317, RBL 31.Jun 14, 2016 · N805SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20160614080Floorbeam · corrodedAFT WET AREA FLOORBEAM BS 967, RBL 30 TO RBL 40 CORROSION AROUND 2 EA FLOORBOARD HOLES. AFT WET AREA FLOORBEAM BS 967, RBL 30 TO RBL 90 CORROSION AROUND 2 EA FLOOR BOARD HOLES. REMOVED DAMAGE DRILLED & FABRICATED TREATED PRIMED TOP COATED INSTALLED REPAIR.Jun 14, 2016 · N805SY · Boeing 7378Q8 · Fuselage Main, Floor Beam
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