JASC 5730
Service difficulty reports · 27,262
Reports filed under 5730 · Wing, Plate/Skin, 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 jasc_code = '5730' 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.
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 jasc_code = '5730' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201809112450Skin · crackedLT WING LEADING EDGE BOTTOM SURFACE AROUND STA XOS =787.5 FOUND CRACK. REPAIR CARRIED OUT AS PER EA 1-5730-T0342355 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR AALA201809121011Skin · corrodedCORROSION ON THE LEFT WING UPPER SURFACE SKIN NEAR THE OVERWING FILL PORT. REPAIRED THE SKIN IAW SRM 57-20-01, REPAIR 6, AND EA 283845.SDR AALA201809121003Skin · corrodedCORROSION WAS FOUND ON THE RIGHT WING UPPER SURFACE SKIN NEAR THE OVERWING FILL PORT. REPAIRED THE SKIN IAW SRM 57-20-01, REPAIR 6, AND EA 283832.SDR FDEA201809112451Skin · corrodedBONDING FUNCTIONAL TEST OF LEFT WING TANK OVERFILL PORT FAILED TEST. UPON EVALUATION, CORROSION FOUND ON SURFACE OF THE UPPER SKIN AT THE OVERWING FILL PORT. REPAIR CARRIED OUT IAW EA F-5730-T0341901.SDR J7SA20180910001Nut Plate · not seatedUPPER LEADING EDGE SCREW FOUND STRIPPED. STICKING UP ON POST FLIGHT. RIGHT MID-WING 7TH SCREW OUTBOARD FROM VORTLON. REMOVED RIGHT MIDDLE LEADING EDGE. RE-SEATED NUT PLATE IN UPPER GANG CHANNEL. REINSTALLED MIDDLE LEADING EDGE.SDR SWIA2018102545173Skin · dentedDENT ON RT WING LEADING EDGE. (C-CHECK) REPAIRED DENT ON RT WING, PER REO 601R-57-41-436.SDR FDEA201809102631Skin · crackedRT LWR WING ACCESS DOOR CUTOUT FASTENER ATTACH HOLE 1 EA HAS A CRACK INDICATION AT FWD EDGE HOLE. REPAIRED AREA PER EA. 8-5730-T0342637.SDR FDEA2018091882551Skin · corrodedRT WING UPPER SKIN CORROSION AT FASTENER STA XORS 400 20 INCH FWD OF AFT SPAR. REMOVED CORROSION PER SRM 57-10-00.SDR FDEA2018091882554Skin · corrodedRT WING UPPER SKIN SURFACE CORROSION AT ROW OF FASTENERS AFT O/B OF PYLON CENTERLINE STA XORS 346. REMOVED CORROSION PER SRM 57-10-00.SDR FDEA2018091882552Skin · corrodedRT WING UPPER SKIN AT FASTENERS SURFACE CORROSION STA XORS 360. REMOVED CORROSION PER SRM 57-10-00.SDR DALA2018090705491Fastener · missingFASTENERS MISSING FROM LT AILERON CLOSEOUT PANEL. INSTALLED FASTENERS. OK FOR SVC. SDR REPORTED DUE TO THE FACT THAT THE FASTENERS COULD HAVE DEPARTED THE AIRCRAFT DURING FLIGHT.SDR FDEA2018090532340Skin · crackedDURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING FIXED LEADING EDGE ACCESS DOOR CUTOUT CORNERS, FOUND 01 EACH CRACK AT CORNER 11 APPROXIMATELY 0.3 INCH IN LENGTH. ACCESS DOOR CUTOUT STA XOS 610 CARRIED OUT REPAIR AS PER SRM 57-SDR SWAA2022022380766Panel · delaminatedLH WING L/E PANEL 521 WB HAS DELAM / REPAIRED DELAM ON L/E PNL 521WB I.A.W B737 SRM 57-46-01-2R-1 AND 51-70-04-2R-10; REPAIRED ALUMINUM FOIL I.A.W SRM 51-70-14-2R-3 AND TOP COAT I.A.W AMM 51-21-99-300-801SDR FDEA2018090512333Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 CUTOUT BETWEEN 5TH AND 6TH RIBS, XOS 696 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 696 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR SDR FDEA2018090512332Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT INBOARD OF ACCESS PANEL 626FB CUTOUT FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR FDEA2018090512331Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 CUTOUT BETWEEN 4TH AND 5TH RIBS (COUNT OUTBOARD FROM SLAT TRACK NR 10) AT XOS 687 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 687 TRIMMED AND REPAIR CARRIED OUT AS PER SSDR FDEA2018090512330Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 CUTOUT BETWEEN 2ND AND 3RD RIBS (COUNT OUTBOARD FROM SLAT TRACK NR 10) AT XOS 677 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02SDR FDEA2018090512329Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 AT XOS 665 CUTOUT FOUND L/E PLATING BEADED DOUBLER CRACK . CRACKED BEADED DOUBLER AT XOS 665 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PESDR AALA2018090431008Skin · crackedRIGHT WING SKIN HAD A CRACK INDICATION AT DIAGONAL BRACE FASTENER HOLE NR 4. REPAIRED THE WING SKIN IAW EA 283659.SDR FDEA2018083102285Skin · corrodedRT WING OUTBD ISLAND AREA UPPER T/E SURFACE STA XORS 1070 FOUND CORROSION. CORRODED SKIN REPAIRED AS PER EA 1-5730-T0341923 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR JGVR20180830002Skin · corrodedFOUND AND BLENDED CORROSION N LT AND RT UPPER WING CENTER SPAR CAP FWD AND AFT SKIN SEAMS FROM WING ROOT TO APPROX. WS 85. PERFORMED NDT AND REPORTED FOR DISPOSITION. REPLACED FASTENERS AS REQUIRED USING NEW RIVETS, TREATED, PRIMED AND TOP COATED REPAIR AREA SDR FDEA201808292235Doubler · crackedLEFT WING LEADING EDGE COMPARTMENT AT XOS 528 ABOVE OUTBOARD SLAT DRIVE CYLINDER FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 528 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GSDR FDEA201808292234Doubler · crackedLEFT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 XOS 670 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 670 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.SDR FDEA201808292233Doubler · crackedLEFT WING LEADING EDGE COMPARTMENT OUTBOARD OF OUTBOARD REFUEL ADAPTER PORT XOS 646 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 646 TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR ASDR FDEA201808292232Doubler · crackedLEFT WING LEADING EDGE COMPARTMENT AT XOS 618 ABOVE INBOARD REFUEL ADAPTER PORT FOUND L/E PLATING BEADED DOUBLER CRACK, XOS 618. CRACKED BEADED DOUBLER AT XOS 618 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG203 REPAIR 15. REPAIR CLASSIFIED MAJOR ASDR FDEA201808292231Doubler · crackedLEFT WING LEADING EDGE COMPARTMENT INBOARD OF SLAT TRACK NR 14 AT XOS 885. FOUND L/E PLATING BEADED DOUBLER CRACK, XOS 885 LEFT WING LEADING EDGE COMPARTMENT INBOARD OF SLAT TRACK 14, CRACKED BEADED DOUBLER AT XOS 885 TRIMMED AND REPAIR CARRIED OUT AS PER SRM SDR DALA2018082905335Skin · dentedDURING A WALK AROUND, FOUND A DENT ON RT WING LE, BEHIND THE NR 2 SLAT. DENT MEASURES 1 1/8" X 1" DEPTH .155, DENT APPEARS TO HAVE A CRACK AT THE BOTTOM. REPAIRED IAW SRM 57-06-BD, TYPE II, FIG 11.SDR AALA2018100219021Access Panel · corrodedCORROSION ON THE ACCESS PANEL 640BB, RIGHT WING BETWEEN RIBS 5 TO 6. REPLACED THE ACCESS PANEL IAW AMM 57-27-11-400-002-A.SDR K11A2019031238Skin · corrodedRIGHT WING UPPER SKIN CORROSION 36" O/B OF WING ROOT WBL 107 & 12" AFT OF FRONT SPAR.SDR K11A2019031235Skin · corrodedRIGHT WING CORROSION OVERWING FILL PORT & ADAPTER.SDR DALA2018082305218Access Panel · corrodedCORROSION FOUND ON THE LT WING FUEL TANK ACCESS PANEL 520CT. UPPER WING ACCESS PANEL WAS REPLACED IAW AMM 28-00-00-420-801.SDR DALA2018082305217Access Panel · corrodedCORROSION FOUND ON THE RT WING FUEL TANK ACCESS PANEL 620CT UPPER WING ACCESS DOOR 520CT. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00-420-801, AND VERIFIED.SDR FDEA201808212135Doubler · chafedLT WING ANTI ICING TELESCOPIC DUCT DOOR CUTOUT REPAIR DOUBLER SURFACE CHAFED XOS 464. LT WING ANTI ICING TELESCOPIC DOOR CUTOUT WORN EXISTING REPAIR DOUBLER REMOVED PER SRM 51-31-01-0G AND REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 10 FIG 202. REPAIR CLASDR IPXA2018083103386Landing · crackedRIGHT WING FUEL TANK ACCESS PANEL 636AB LANDING HAD FIVE CRACKS, AT FASTENER HOLES BETWEEN XORS 683.40 - 713.65. REPAIRED THE ACCESS PANEL LANDING IAW SRM 57-20-02, REPAIR 5, FIG 201. MINOR.SDR IPXA2018083133420Landing · crackedLEFT WING LOWER FUEL ACCESS PANEL 536AB LANDING HAD SEVEN CRACKS, AT THE FASTENER HOLES BETWEEN XORS 683.4 TO 713.65. REPAIRED THE ACCESS PANEL LANDING IAW SRM 57-50-02, REPAIR 5, FIG 201. MINOR.SDR CA180822006Skin · corroded(CAN) DURING INSPECTION, CORROSION FOUND BEYOND LIMITS, SKIN TO BE REPLACED. (TC# 20180822006)SDR AALA201810019022Skin · corrodedCORROSION TO UPPER SURFACE EXTERNAL SKIN BETWEEN RIBS 4 TO 5, ON THE LT WING BETWEEN WING STA 2440 TO 2300. REPAIRED THE SKIN IAW EA 284511.SDR AALA2018091879032Skin · corrodedCORROSION FOUND ON THE UPPER SURFACE SKIN BETWEEN RIBS 5 TO 6, STRINGER 17R ON THE RIGHT WING. REPAIRED THE SKIN IAW SRM 51-21-11-283-014.SDR P5CA201808220211Panel · corrodedCORROSION INBD SPOILER UPPER CHORD OF RT WING INBD T/E UPPER FIXED PANEL WBL ISS AND WBL 162. CORROSION REMOVED IAW SRM 57-51-02-1A-1, FIG.101, SH8, REV 71. MEASURED REWORKED AREA ORGINAL THICKNESS = .112" REWORK AREA DEPTH =.017" THICKESS MORE THAN PERMITSDR FDEA2018082182100Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 642 WAS FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR TSAA20180818013Skin · corrodedREMOVED CORROSION ON UPPER SURFACE OF LEFT WING NEAR TIP IAW SRM 51-10-02, REV 117. FOUND TO BE BEYOND LIMITS IAW SRM 57-20-01. REPAIRED IAW ENGINEERING DRAWING R27905.1-057-006-001, REV A.SDR ASOA2018082385177Skin · damagedDISCOVERED SURFACE DAMAGE TO THE LEADING EDGE PANEL 622AR AT FASTENER HOLE BOTTOM INBD END OF THE PANEL. REPAIRED THE DAMAGE IAW EA 45-2018-127, AND EC/TC EA 45-2018-127.SDR IPXA2018082233095Skin · damagedLEFT WING TIP LOWER SURFACE WAS DENTED AND CRACKED AFT OF THE WING TIP. REPAIRED IAW SRM 57-30-11.SDR IPXA2018082733253Skin · crackedRIGHT WING FIXED L/E SKIN LOWER SURFACE WAS CRACKED AT THE NR 5 SLAT TRACK CUT-OUT, XOS. 775. REPAIRED THE FIXED L/E SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201. MAJOR.SDR CALA2018082001820Skin · corrodedRIGHT WING UPPER SURFACE, FROM RIBS 7 - 8, AND 4 INCHES FWD OF WING T /E WAS CORRODED. REPAIRED THE RT WING SKIN IAW ECRA 5725-01012, & REO L21513 REV IR.SDR ABXA2018082017087Skin · corrodedCORROSION FOUND ON THE RIGHT WING LOWER SKIN PANEL NR 1, RWS 918. THE AIRPLANE WAS GROUNDED. THE SKIN WAS REPAIRED.SDR ABXA2018082017086Skin · corrodedCORROSION FOUND ON THE RIGHT WING, LOWER SKIN, RWS 924.16. THE AIRPLANE WAS GROUNDED. THE SKIN WAS REPAIRED.SDR FDEA2018081762063Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 626 WAS FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2018081762062Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 665 WAS FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2018081762061Doubler · crackedRIGHT WING LEADING EDGE CAVITY, BEADED DOUBLER AT XOS 652 WAS FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.
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