N801SY

Service difficulty reports · 218

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 = 'N801SY' 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 SCNA20201007080Shield · corrodedCORROSION FOUND ON SHIELD AFT OF AFT CARGO COMPARTMENT DOOR STA 856 TO 867 RBL 21 WL 159. CORROSION ON AFT CARGO AFT SHIELD STA 856 TO 867 RBL 21 WL 159 FOUND TO BE OUT OF LIMITS, DUE TO NO LIMITS FOUND IN SRM 53-60-15-1A-1. REMOVED SHIELD, IAW SRM 51-40-02-Sep 11, 2020 · N801SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20201007079Attach Angle · corrodedFWD ENTRY INNER CHORD SCUFF PLATE ATTACH ANGLE STA 287 TO STA 335 LBL 59 WL 208 CORROSION DAMAGE. FWD ENTRY INNER CHORD SCUFF PLATE ATTACH ANGLE BS 287-335 LBL 59 FOUND TO BE OUT OF LIMITS, DUE TO NO ALLOWABLE LIMITS, IAW B737-800 SRM. REMOVED AND REPLACED ASep 10, 2020 · N801SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20201007078Seat Track · corrodedSEAT TRACK FLOOR STRUCTURE CORRODED AROUND HOLE BS 328 +5", LBL 43. CORROSION FOUND ON SEAT TRACK FLOOR STRUCTURE STA 328+5 LBL 43 FOUND TO BE OUT OF LIMITS, IAW SRM 51-10-02-0G-0 9C. REMOVED AND REPLACED FLOOR STRUCTURE WITH NEW, IAW SRM 51-40-02 AND DWG 14Sep 10, 2020 · N801SY · Boeing 7378Q8 · Fuselage, Seat/Cargo Attach FittingsSDR SCNA20201007077Floorbeam · corrodedFLOOR STRUCTURE AT BS 947 + 3" RBL 18 TO RBL 46 HAS CORROSION ON UPPER AND LOWER SURFACES OF TOP AROUND HOLES. REMOVED AND REPLACED FLOOR STRUCTURE AT BS 947+3 RBL 18 TO RBL 46 WITH NEW FLOOR STRUCTURE ITEM NR 147A5676U6 PO 801297, IAW SRM 51-40-02 AND DWG 14Sep 10, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Floor BeamSDR SCNA20201007076Stringer Clip · corrodedAFT CARGO BAY STRINGER CLIP STA 727D STR 22L HAS CORROSION ON SURFACE, MARKED. STRINGER CLIP AT BS 727D STR 22C FOUND TO BE OUT OF LIMITS, DUE TO NO ALLOWABLE LIMITS, IAW B737-800 SRM. REMOVED AND REPLACED STR CLIP, IAW B737-800 SRM 51-40-02-0G-0 AND BOEING Sep 10, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Attach FittingsSDR SCNA20201007075Channel · corrodedAFT CARGO BAY LEFT HAND Z CHANNEL HAS MULTIPLE AREAS OF CORROSION STATION 727B-827, MARKED. REMOVED AND REPLACED AFT CARGO LEFT HAND Z CHANNEL FROM BS 727B-827, IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 146A7502 REV. NOTE: CORROSION WAS FOUND TO BE OSep 10, 2020 · N801SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20201007074Stiffener · corrodedCORROSION FOUND WHERE TOP EDGE OF APU AIR INLET PLENUM ATTACHES TO FWD SIDE OF BULKHEAD STA 1088, MARKED. REMOVED AND REPLACED STIFF NEW AT BS 1088 AT PPU AIR INLET PLENUM ATTACH POINT, IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 148A0924 REV B.Sep 8, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, BulkheadSDR SCNA20201007073Floor Panel · corrodedFLIGHT DECK FLOOR PANEL 211AF HAS LIGHT SURFACE CORROSION AT OUTER EDGE AREA. FLIGHT DECK FLOOR PANEL 211AF HAS LIGHT SURFACE CORROSION AT OUTER EDGE AREA. BLENDED AREA W=1.0" X L=19" X D=.006" ORIGINAL .050" REMAINING .043 FOUND TO BE OUT OF LIMITS, IAW SRMSep 8, 2020 · N801SY · Boeing 7378Q8 · Fuselage Floor PanelSDR SCNA20201007072Floor Panel · damagedFWD WET AREA FLOOR PANEL P/N 141A5810-159 HAS 2 DAMAGED AREAS ON PANEL. REPAIRED 2 DAMAGED AREAS ON FWD WET AREA FLOOR PANEL P/N 141A5810-159, IAW 737 SRM 53-00-50-2R-0 AND SRM 53-00-50-2R-4 BOEING DWG 141A5810 ID: 0159.Sep 7, 2020 · N801SY · Boeing 7378Q8 · Fuselage Floor PanelSDR SCNA20201007071Floor Support · corrodedCORROSION FLOOR SUPPORT HAS CORROSION IN HOLES BS 312 TO BS 328 RBL 11. REMOVED DAMAGED FLOOR SUPPORT BS 312-328 RBL 11 AND INSTALLED NEW FLOOR SUPPORT P/N 141A5410U14 PO 801506, IAW SRM 51-40-02 DWG 141A5400. FINAL INSTALL TO BE ACCOMPLISHED ON CUSTOMER CARSep 6, 2020 · N801SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20201007070Support · corrodedCORROSION FOUND ON AFT CARGO COMPARTMENT AFT BULKHEAD LOWER CENTER SUPPORT STA 947 RBL 9.5 TO LBL 21 WL 157. CORROSION ON AFT CARGO AFT LOWER BULKHEAD SUPPORT OUT OF LIMITS, IAW SRM 51-10-02. REMOVED AND REPLACED AFT CARGO AFT LOWER BULKHEAD SUPPORT WITH NESep 6, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, BulkheadSDR SCNA20201007069Screw · corrodedAFT CARGO BAY TIE DOWN BRACKET CORRODED NEAR SCREW HOLES STA 792 STR 23-24L, MARKED. REMOVED AND REPLACED AFT CARGO BAY TIE DOWN BRACKETS AT STA 792 STR 23-24L, IAW SRM 51-40-02 AND DWG NR 146A7550 59568U 09/03/2020. CORROSION FOUND TO BE OUT OF LIMITS, DUE Sep 6, 2020 · N801SY · Boeing 7378Q8 · Fuselage, Seat/Cargo Attach FittingsSDR SCNA20201007068Attach Angle · crackedLT 663 UPPER ATTACH ANGLE CRACKED AT APPROXIMATELY LBL 8. REPAIRED LT 663 UPPER ATTACH ANGLE, IAW SRM 57-10-10-2R-5 LBL 8.Sep 5, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Attach FittingsSDR SCNA20201007067Floor Panel · damagedFWD WET AREA FLOOR PANEL P/N 141A5810-56 MISSING INSERT AND HAS A PUNCTURE. REPAIRED PUNCTURE, IAW SRM 53-00-50 REPAIR 6 + INSTALLED INSERT, IAW SRM 53-00-50 REPAIR GENERAL PARA 5S(1) ON FWD WET AREA FLOOR PANEL P/N 141A5810-56 80733U.Sep 4, 2020 · N801SY · Boeing 7378Q8 · Fuselage Floor PanelSDR SCNA20201007066Floor Support · corrodedAFT CARGO BAY FLOOR SUPPORT STATION 772 2" LEFT OF CENTERLINE HAS CORROSION NEAR BOLT HOLES, MARKED. CORROSION ON AFT CARGO BAY FLOOR SUPPORT FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-53-1A-1 FIG 103 DETAIL D. CORROSION FOUND AROUND FASTER HOLES. REMOVED FLOSep 4, 2020 · N801SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20201007065Floor Panel · delaminatedAFT WET AREA FLOOR PANEL P/N 147A5810-28 EDGE HAS DELAMINATION, DAMAGED INSERTS AND PUNCTURE. REPAIRED DELAMINATION AND PUNCTURE ON AFT WET AREA CABIN FLOOR PANEL 147A5810-28 AND REPLACED DAMAGED INSERTS, PER SRM 53-00-50-2R-1.Sep 3, 2020 · N801SY · Boeing 7378Q8 · Fuselage Floor PanelSDR SCNA20201007064Floor Support · damagedTOOLING MARK ON FLOOR STRUCTURE BS 270 TO 270 + 5", LBL 11. TOOLING MARK ON FLOOR STRUCTURE BS 270+6" LBL 11 FOUND TO BE OUT OF LIMITS, IAW NO SRM ALLOWABLE LIMITS. REMOVED AND REPLACED TEE, IAW SRM 51-40-02 AND BOEING DWG 141A5600 REV N 57828U.Sep 3, 2020 · N801SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20201007063Shield · corrodedCORROSION RT SHIELD FWD OF AFT CARGO DOOR FROM STA 767-794.5, RBL 25, WL 155. RT SHIELD FWD OF AFT CARGO DOOR FROM STA 767-794.5, RBL 25, WL 155. CORROSION ON RT SHIELD FWD OF AFT CARGO DOOR FOUND TO BE OUT OF LIMITS, DUE TO NO LIMITS FOUND IN SRM, IAW SRM 5Sep 3, 2020 · N801SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20201007062Bulkhead Web · crackedLT LOWER 663 VAPOR BARRIER CRACKED BY THE EXHAUST CUTOUT APPROXIMATELY LBL 14 BELOW THE HORIZONTAL STIFFENER. REPAIRED CRACKS BY EXHAUST CUTOUT APPROXIMATELY LBL 14 BELOW THE HORIZONTAL STIFFENER ON LT LOWER 663 VAPOR BARRIER, PER SRM 57-10-10-2R-2 PARA 1 NOTSep 3, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, BulkheadSDR SCNA20201007061Floorbeam · damagedTOOLING MARKS ON FLOOR BEAM BS 294.5, LBL 11 TO RBL 41. BLENDED ON UPPER SURFACE OF FLOOR BEAM 294.5 AT RBL 24.5 AREA 1.75" L X .7" W X .015" D. FOUND TO BE OUT OF LIMITS, IAW SRM 53-10-51-1A-1 DET C. ALL OTHER BLEND AREAS .012" OR LESS WITHIN LIMITS, IAW SSep 2, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Floor BeamSDR SCNA20201007060Floor Support · corrodedAFT CARGO BAY DOOR FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION, MARKED, STA 808-827 RBL 26.5 WL 160. AFT CARGO BAY DOOR FLOOR SILL PLATE FOUND TO BE OUT OF LIMITS, IAW SRM 53-60-15-1A-1. REMOVED FLOOR SILL PLATE, IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A13410Sep 1, 2020 · N801SY · Boeing 7378Q8 · Fuselage Miscellaneous StructureSDR SCNA20201007059Panel · erodedLEFT WING PANEL 521 QB HAS EROSION NEXT TO FASTENER HOLE. REPAIRED EROSION NEXT TO FASTENER HOLE ON LEFT WING PANEL 521QB, IAW 737 SRM 57-41-01-2R-1 AND SRM 51-70-05 REPAIR 8.Sep 1, 2020 · N801SY · Boeing 7378Q8 · Wing, Plate/SkinSDR SCNA20201007058Panel · erodedRT WING LEADING EDGE PANEL 621LB HAS EROSION AT DRAIN HOLE. REPAIRED EROSION AT DRAIN HOLE ON RT WING LEADING EDGE PANEL 621LB, IAW 737 SRM 57-41-01-2R-1 AND SRM 51-70-05 REPAIR 8.Sep 1, 2020 · N801SY · Boeing 7378Q8 · Wing, Plate/SkinSDR SCNA20201007057Panel · erodedRT WING LEADING EDGE PANEL 621EB HAS EROSION AT DRAIN HOLE. REPAIRED RT WING LEADING EDGE PANEL 621EB EROSION AT DRAIN HOLE, IAW 737 SRM 57-41-01-2R-1 AND SRM 51-70-05 REPAIR 8.Sep 1, 2020 · N801SY · Boeing 7378Q8 · Wing, Plate/SkinSDR SCNA20201007056Floor Panel · damagedAFT WET AREA FLOOR PANEL P/N 147A5810-23 HAS SEVERAL INSERTS DAMAGED. FABRICATED REPLACEMENT AFT WET AREA FLOOR PANEL P/N 147A5810-23, PER B737 SRM 53-00-50-2R-0 PARA 4A(1) TABLE 204 AND PARA 5A AND PER BOEING DRAWING 147A5810 REV A. BMS 4-17 TY6 LOT 5085150-Aug 31, 2020 · N801SY · Boeing 7378Q8 · Fuselage Floor PanelSDR SCNA20201007055Floorbeam · corrodedAFT CARGO BAY FLOOR SUPPORT TEE SPLICE STA 727I+5 HAS CORROSION AROUND MULTIPLE NUTPLATES. AFT CARGO BAY FLOOR SUPPORT TEE SPLICE STA 727I+5 HAS CORROSION AROUND MULTIPLE NUTPLATES. FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM. REMOVED AND REAug 27, 2020 · N801SY · Boeing 7378Q8 · Fuselage Main, Floor BeamSDR SCNA20180701094Battery Pack · dischargedEMERG LIGHTS AT ROWS 5, 6, 7, 9, AND 10 DO NOT WORK. REMOVED AND REPLACED LT AND RT BATTERY PACKS AT ROW 7AC/7FD. OPS CHECK NORMAL.Jul 1, 2018 · N801SY · Boeing 7378Q8 · Emergency LightingSDR SCNA201805221090Slat · crackedNR 6 SLAT HAD A SMALL CRACK AT A FASTENER HOLE FOR ACTUATOR ATTACH FITTING. REMOVED AND REPLACED THE NR 6 LEADING EDGE SLAT. OK FOR SERVICE.May 21, 2018 · N801SY · Boeing 7378Q8 · Leading Edge DevicesSDR SCNA20180519089Skin · crackedNR 8 LEADING EDGE SLAT HAS CRACK IN THE SKIN AT THE ACTUATOR ATTACH POINT. ACCCOMPLISHED AN INTERM REPAIR. REMOVED AND REPLACED THE NR 8 SLAT. PERFORMED A SLAT ADJUSTMENT. OK FOR SERVICE.May 19, 2018 · N801SY · Boeing 7378Q8 · Leading Edge DevicesSDR SCNA20180119006Plate · damagedFOUND WIGGLE PLATE ASSY DAMAGED AT T/E PANEL 651EB. REMOVED 5 EACH RIVETS COMMON TO WING PLANK AND WIGGLE PLATE. NEW PLATE DRILLED AND CLECO'D IN PLACE. READY TO INSTALL. INSTALLED FASTENERS IN WIGGLE PLATE.Jan 19, 2018 · N801SY · Boeing 7378Q8 · Wing Miscellaneous StructureSDR SCNA20180119003Beam · wornRIGHT WING LOWER INBD FIXED TE ATTACHED TO PANEL 651EB, FOUND A BEAM WORN AND ROD END MISSING. REMOVED PANEL 651EB. REMOVED THE WORN BEAM. INSTALLED A NEW BEAM.Jan 19, 2018 · N801SY · Boeing 7378Q8 · Wing Main, Frame StructureSDR SCNA20180119002Skin · puncturedFOUND A SMALL HOLE ON THE NR 1 OTBD NACELLE COWL. REPLACED WITH SERVICEABLE COWL.Jan 19, 2018 · N801SY · Boeing 7378Q8 · Nacelle/Pylon, Plate/SkinSDR SCNA20180119001Fuse · failedDURING AN EMERGENCY LIGHT SWITCH OPS TEST, FOUND THE L2 DOOR ESCAPE SLIDE LIGHT INOPERATIVE. REPLACED A BLOWN FUSE IN THE AFT POWER SUPPLY FOR THE L2 SLIDE LIGHT. OPS CHECKED GOOD.Jan 19, 2018 · N801SY · Boeing 7378Q8 · Emergency LightingSDR SCNA20180119005Link · wornNR 6 FLAP FAIRING AFT LINK ASSEMBLY UPPER ROD END BOLT AND SPACER WORN. REMOVED AFT CANOE FAIRING TIP 642EB. PART IN AREA. REMOVED AND REPLACED AFT LINK ASSEMBLY. FOUND UPPER ROD END BOLT AND SPACER WORN. ORDERED BOLT. NEW SPACER AND OLD BOLT REINSTALLED TILL Jan 19, 2018 · N801SY · Boeing 7378Q8 · Trailing Edge FlapsSDR SCNA20180119004Skin · damagedLEFT WING OUTBOARD MAIN FLAP INBOARD END TOP SIDE SKIN HAS WEAR DAMAGE. LEADING EDGE PANEL 113A3432-11 REMOVED FROM LT. FLAP FOUND WEAR OUT OF LIMITS. REPLACEMENT PANEL ORDERED FROM BOEING. FLAP PANEL # 113A3411-7 REMOVED DUE TO WEAR, FOUND TO BE WITHIN LIMITSJan 19, 2018 · N801SY · Boeing 7378Q8 · Trailing Edge FlapsSDR SCNA20170909164Flap Track · corrodedTHE AFT, LT, TE, OTBD FLAP, INBD FLAP TRACK HAS SIDE SCUFFING ON THE UPPER AND LOWER TRACK FLANGES FROM THE CARRIAGE RUB PLATES. ROLLER IS OUT OF LIMIT. BLENDED DAMAGE. NO CRACKS NOTED.Sep 9, 2017 · N801SY · Boeing 7378Q8 · Trailing Edge Flap Control SystemSDR SCNA20170909163Structure · missingLEFT OTBD FLAP PHENOLIC CHAFE MATERIAL MISSING FROM T/E OF FORE FLAP. REMOVED ALL OLD PHENOLIC AND ADHESIVE. CLEANED BOTTOM SIDE OF THE O/B FLAP. REPAIRED.Sep 9, 2017 · N801SY · Boeing 7378Q8 · Trailing Edge FlapsSDR SCNA20170909162Structure · missingRIGHT OTBD FLAP PHENOLIC CHAFE MATERIAL MISSING FROM T/E OF FORE FLAP. REPAIRED.Sep 9, 2017 · N801SY · Boeing 7378Q8 · Trailing Edge FlapsSDR SCNA20170530087Sensor · malfunctionedON APPROACH, AT FLAPS 1, THE LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED, NR 3 SLAT AMBER LIGHT ILLUMINATED. RAN QRH 9.14 STILL AT FLAP 1, LEADING FLAP TRANSIT LIGHT AND OVERHEAD AMBER LIGHT WENT OUT AFTER APPROXIMATELY 5 MINUTES AND LEADINGE EDGE FLAPS EXTEMay 30, 2017 · N801SY · Boeing 7378Q8 · Leading Edge Slat Control SystemSDR SCNA20170505056Slat · inoperativeWITH FLAPS EXTENDED TO 5 ON APPROACH. THE NR 3 SLAT ON THE LEFT WING FAILED TO EXTEND. REPLACED THE NR 3 LEADING EDGE EXTEND PROXIMITY SWITCH. R & R FSEU. OPS CHECKED GOOD. REPLACED THE LE FLAP/SLAT POSTION ANNUNCIATOR PANEL. OPS CHECKED GOOD. REMOVED AND RMay 5, 2017 · N801SY · Boeing 7378Q8 · Leading Edge Slat Control SystemSDR SCNA20161224378Slat System · malfunctionedNR 3 SLAT STAYED IN TRANSIT AFTER SELECTING FLAPS FIVE. ACP BITE OF FSEU WITH NO FAULTS FOUND. OPERATED FLAPS WITH NO FAULTS. OK FOR SERVICE. PERFORMED LEADING EDGE FLAP AND SLAT POSITION INDICATING SYSTEM TEST. NO FAULTS FOUND. PERFORMED FSEU BITE TEST. NODec 24, 2016 · N801SY · Boeing 7378Q8 · Leading Edge Slat Control SystemSDR SCNA20151120172Skin · looseRT WING, UPPER PANEL L/E INBD OF ENGINE HAS LOOSE, SMOKING RIVETS. REPLACED FASTENERS.Nov 20, 2015 · N801SY · Boeing 7378Q8 · Wing, Plate/SkinSDR SCNA20151120171Skin · looseLT WING, UPPER PANEL L/E INBD OF ENGINE HAS LOOSE, SMOKING RIVETS. REPLACED FASTENERS.Nov 20, 2015 · N801SY · Boeing 7378Q8 · Wing, Plate/SkinSDR SCNA20151112170Control Valve · failedFLAPS WOULD NOT MOVE FROM 25 POSITION DURING GO AROUND AT AIRPORT, WHEN FLAP LEVER WAS MOVED TO FLAPS 15 POSITION. R & R T/E FLAP CONTROL VALVE. R & R FLAP LEVER POSITION SWITCH. ALL TESTS REQUIRED PASSED NORMALLY.Nov 12, 2015 · N801SY · Boeing 7378Q8 · Trailing Edge Flap Control SystemSDR SCNA20151002136Battery Pack · failedEMERGENCY LIGHTS ON OVERHEAD BIN BULLNOSE BETWEEN SEATS 15 ABC AND 20 ABC AND LIGHT AFT OF LT AFT OVERWING EXIT DOOR FAILED BATTERY PACK CAPACITY FUNCTIONAL TEST. R & R POWER SUPPLY M1670, BATTERY PACK IAW AMM 33-51-06. OPS CHECKS GOOD.Oct 2, 2015 · N801SY · Boeing 7378Q8 · Emergency LightingSDR SCNA20151002135Battery Pack · failedEMERGENCY LIGHTS ON OVERHEAD BIN BULLNOSE BETWEEN SEATS 16 DEF AND 20 DEF AND LIGHT AFT OF RT AFT OVERWING EXIT DOOR FAILED BATTERY PACK CAPACITY FUNCTIONAL TEST. R & R POWER SUPPLY M1671 BATTERY PACK IAW AMM 33-51-06. OPS CHECKS GOOD.Oct 2, 2015 · N801SY · Boeing 7378Q8 · Emergency LightingSDR SCNA20150702117Battery Pack · inoperativeR2 EMERGENCY LIGHTS INOPERATIVE. R & R R2 EMERGENCY LIGHT CHARGER ASSY, AND BATTERY PACK.Jul 1, 2015 · N801SY · Boeing 7378Q8 · Emergency LightingSDR SCNA20141212214Wire · damagedR1 DOOR SLIDE EMERGENCY LIGHT INOPERATIVE AND KEEPS POPPING THE FUSE IN THE CHARGER. REPAIRED WIRING FROM CONNECTOR, D10748, PIN 12 TO CONNECTOR, D12052, PIN 2 AT ROW 1, SEAT AB.Dec 2, 2014 · N801SY · Boeing 7378Q8 · Light System WiringSDR SCNA20140922132Floorbeam · gougedFLOORBEAM BS 328 GOUGED DOWN THE AFT SIDE UNDER THE CUSP INSTALLATION ON THE RT SIDE, REPAIRED THE FLOORBEAM.Sep 20, 2014 · N801SY · Boeing 7378Q8 · Fuselage Main, Floor BeamSDR SCNA20140922130Floorbeam · corrodedPASSENGER CABIN FWD WET AREA BS 328 FLOORBEAM CORRODED AT SEVERAL SPOTS. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM.Sep 20, 2014 · N801SY · Boeing 7378Q8 · Fuselage Main, Floor Beam
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