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 = '5711' 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 = '5711' 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 EISA20010050Spar · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND CORROSION AT RIGHT WING CENTER SECTION, REAR SPAR LOWER CHORD AND WEB. FABRICATED AND INSTALLED WEB REPAIR AND SPACERS AT RIGHT WING CENTER SECTION REAR SPAR LOWER CHORD AND WEB, ALODINED AND PRIMED IAW SRM 51-10-2, 51-SDR AU010257Spar · corroded(AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED.SDR AU010258Spar · cracked(AUS) LT AND RT WING FORWARD AND AFT LOWER SPAR CAPS CRACKED IN AREABETWEEN RIBS NR 13 AND NR 18. CORROSION ALSO FOUND ON LOWER SKINS AT RIB BAYS NR 13 TO NR 18.SDR UPS01435350Spar Cap · corrodedINSPECTION TYPE:C, RIGHT WING FRONT SPAR LOWER CAP LOWER LEG IS CORRODED BEYOND LIMITS, 15 INCHES I/B OF STA FSSO, WS 1322. REPAIRED LOWER SPAR CAP IAW SRM 57-30-03 FIG 4.SDR C2XA01IA203Spar · crackedSJK - DURING C-CHECK INSPECTION, THE LEFT HAND AND RIGHT HAND SPAR CAPS WERE FOUND TO BE CRACKED AT RIB 17 USING EDDY CURRENT INSPECTION. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB-120 SRM 57-20-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN SDR SWAA010333Spar · crackedDURING SCHEDULED D-CHECK, FOUND 3 RT WING REAR SPAR UPPER CHORD CRACKS AT HOLE B24, RSS 222.14, HOLE C27, RSS 223.14 & HOLE D27, RSS 225.15. REPAIRED SPAR CHORD PER ER.SDR 20010326CW003Spar Cap · crackedDURING REPAIRS OF THE WING CENTER SECTION FOR CORROSION DAMAGE TO THE TRAILING EDGE SECTION OF THE WING AND DURING HIDDEN DAMAGE INSPECTION, FOUND .1250 INCH DEEP CRACK IN THE FORWARD LOWER SPAR CAP. THE CRACK RAN APPROX 24 INCHES INBOARD IN A SPANWISE DIRECTSDR UPS01434803Spar Cap · corrodedINSPECTION TYPE:IN PER EO-13738A REPAIR RT WING LWR SKIN FWD ANGLE ATTACH CHORD. *S/D* REPAIR ACCOMPLISHED PER EO -13738A.SDR 2002FA0000263Spar · crackedWINGS REMOVED FROM AC, THE REPAIR ON THE LT REAR SPAR STRUT ATTACH POINT. ALL FABRIC COVERING REMOVED, LT REAR SPAR HAD A 1 INCH X 16 INCHES LONG .1250 PLYWOOD STRIP GLUED TO THE TOP OF THE SPAR WHICH HID THE CRACK TO BUSHING HOLE. IT WOULD APPEAR THAT CRACKSDR 2002FA0000250Spar · crackedWOODEN SPARS, NAILS OUT OF LEADING EDGE RIBS, WOODEN SPACERS WERE LEFT OUT OF FIRST FOUR INBOARD LEADING EDGE RIBS. LEADING EDGE LOOSE, NAILS LOOSE. HAD BEEN PATCHED BEFORE, HAD PUT SCREWS INSTEAD OF NAILS ON LEADING EDGE SPARS AND RIBS. SOME RIBS CRACKED,SDR 20010417AP002Spar · damagedWOOD SPARS; NAILS OUT OF LEADING EDGE RIBS; WOODEN SPACERS WERE LEFTOUT OF FIRST FOUR IN-BOARD LEADINGEDGE RIBS; LEADING EDGE LOOSE; NAILSLOOSE; SOMEBODY HAD PATCHED UP BEFORE AND PUT SCREWS INSTEAD OF NAILS ON LEADING EDGE SPARS AND RIBS; SOME RIBS CRACKED; SDR UIEA01004Spar · corrodedDURING THE RECENT C-CHECK, THE REAR SPAR (OUTSIDE SURFACE) WAS FOUND CORRODED IN THE VICINITY OF THE NR 2 INBOARD FUELING VALVE MOUNT BOLT HOLES AT WS 562.50. FUELING EQUIPMENT AND MOUNT BOLT REMOVED. AREA REWORKED BY SPOT FACING CORRODED AREA, BLENDED, TREASDR UPS01834778Rib · crackedINSPECTION TYPE:C1&3, LEFT WING CENTER L/E UPPER RIBS ARE CRACKED AT XFS 347.75, XFS 354, XFS 372.75, XFS 379. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.SDR TSAA0157009Spar · corrodedIDENTIFIED CORROSION AT RT WING FRONT SPAR LOWER CHORD FSS 475. REPAIRED CONSISTS OF REMOVING DAMAGED AREA AT HORIZONTAL FLANGE AND INSTALLING A TAPERED FILLER, HFEC COMPLETED ON ALL FASTENER HOLES AND REWORKED AREA. NO DEFECTS NOTED. CLEAN AND TREATED ALL SDR DHL2001740C20Angle · corrodedLEFT WING FRONT SPAR LOWER CHORD ANGLE LOWER SECTION WHERE L/E PANELS ATTACH, CORROSION ON TWO SECTIONS APPROX BETWEEN WS 383.0 AND 477.0. FABRICATED AND INSTALLED REPAIR PLATE 18.375 X 2.875 INCHES. INSTALLED PER AVITAS EO AVHM-0186 RO-1FORM 337 FILED BY AVSDR 20010223CW001Spar · crackedDURING INSPECTION, CRACK FOUND ORIGINATING FROM RIB NAIL RUNNING HORIZONTAL. SPAR INSTALLED 5/17/59SDR QXEA0100069Spar · corrodedPDX- LEFT WING FRONT SPAR LOWER SURFACE HAS FRETTING CORROSION AT STATION YW210-220. REPAIRED IAW HORIZON AIR EA 9-57-548.SDR QXEA0100068Spar · corrodedPDX- LEFT WING FRONT SPAR, UPPER SURFACE HAS FRETTING CORROSION AROUND ATTACH HOLES FOR PANEL 511AL. REPAIRED IAW DHC-8 RD8-57-811 AND SRM 51-2011, AND HORIZON AIR EA 9-57-546.SDR QXEA0100070Spar · corrodedPDX- LEFT WING FRONT SPAR, LOWER SURFACE HAS FRETTING CORROSION AT STATION YW 48-82. REPAIRED IAW DHC-8 RD8-57-811 AND RD8-57-1150.SDR 20010412CW005Spar · corrodedINSPECTION REVEALED MISSING RIVET HEADS, RUST. CORROSSION ON REAR SPAR AT CENTER SECTION JUNCTION.SDR AT0100032R1Spar · corrodedFOUND RIGHT WING REAR SPAR TO HAVE INTERGRANULAR EXFOLIATED CORROSION INBOARD OF CENTER FLAP SUPPORT FITTING. REMOVED CORROSION AND FABRICATED AND INSTALLED SPLICES IAW REO-L00303.SDR AU010338Spar · cracked(AUS) LT UPPER WING MAIN SPAR CRACKED IN SEVERAL PLACES. FURTHER INSPECTION FOLLOWING FABRIC REMOVAL FOUND THAT THE SPAR HAD BEEN DRESSED WITH FILLER AND PAINT UNDER WHICH MORE CRACKS WERE FOUND.SDR AU010048Spar · corroded(AUS) LT AND RT WING FORWARD AND AFT SPARS CONTAINED PITTING CORROSIONIN AREAS OUTBOARD OF RIB NR 13. HEAVY STAINING FOUND IN WING TANKS SUSPECTED FROM CLADOSPORIUM RESINAE.SDR 2002FA0000241Spar · cracked1) RIGHT WING/ CRACKS PROPAGATING FROM BOLT HOLES ADJACENT TO FUSELAGE ATTACHMENT FROM AND REAR. 2) CRACK OUTBOARD OF REAR LIFT STRUT REAR SPAR (RIGHT WING) 3) LEFT WING REAR SPAR (ORIGINAL FACTORY SPAR) EDGE GLUED JOINT DELAMINATED FROM ATTACH FITTING OUT TSDR 2002FA0000240Spar · cracked1) RIGHT WING FRONT SPAR BETWEEN 3RD AND 4TH RIB ON FORWARD FACE OF SPAR A CRACK CROSSING 3 ANNUAL RINGS APPROXIMATELY 4 INCHES IN LENGTH. 2) LEFT WING LOOSE OR MISSING NAILS IN FRONT SPAR AS 3RD AND 4TH RIBS LOOSE OR MISSING NAILS IN FRONT AND REAR SPARS ADJSDR 20010525SG006Spar · defectiveSAW - DURING EDDY CURRENT ROTO TEST INSPECTION OF THE RIGHT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 2, THE FORWARD OUTBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. THE LEFT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 4SDR 20010530CW003Spar · crackedCRACKS FOUND IN WEB CUTOUTS. DURING INSPECTION CRACKS WERE FOUND. AIRCRAFT WILL BE FERRIED TO LOCATION TO BE REPAIRED.SDR AU001276Spar · corroded(AUS) LT AND RT WING FORWARD AND AFT SPARS CONTAINED SUSPECT INTERGRANNULAR CORROSION IN AREAS LOCATED OUTBOARD OF RIB NR 13.SDR ABXA010122Spar · corrodedTHE RIGHT WING SPAR AFT FACE AT UPPER DIHEDRAL HAD CORROSION EXTENDING DOWN FROM THE TOP OF AFT FACE TO BOTTOM OF THE REAR SPAR. MAINTENANCE INSPECTED AND REPLACED THE SPAR WEB.SDR CNMA200100011Spar · corrodedDURING C-CHECK, FOUND LEFT WING AFT SPAR T-CAP FASTENER HOLE CORRODED AT STA XORS 582. CORROSION WAS REMOVED BY SPOTFACING FASTENER HOLE FROM LOWER SIDE OF HOLE AND INSTALLING A FILLER AND DOUBLER USING 7075-T6 .125 THICKNESS. MAJOR REPAIR APPROVED BY 8110-3SDR QXEA0003291Spar · crackedPDX- LEFT HAND REAR SPAR WEB PLATE HAS CRACKS COMING OUT FROM TWO RIVETS. REPAIRED IAW HORIZON AIR EA 4-57-513, FOKKER SRM 57-13-05, 51-31-01 AND 28-11-0.SDR COOSDR000026Spar · corrodedLEFT WING INBOARD MID-FLAP, REAR SPAR LOWER CHORD, FORWARD FLANGE REPAIR FROM WBL 70.70 TO WBL 84.90. POSSIBLE CAUSE OF THE CORROSION WAS FATIGUE. (X)SDR 00FDEA00804Spar · corrodedDURING ROUTINE INSP, CORROSION DAMAGE FOUND AT SEVERAL FASTENERS IN THE WING CENTER SECTION REAR SPAR UPPER CHORD. REMOVED AND REPLACED PER P/N 65-18538-5 IAW FEDEX EA 7-5710-53851.SDR AU001115Spar Cap · cracked(AUS) LEFT SPAR CAP CRACKED IN AREA OF THE HOLE LOCATED 3 MM (0.118 INCHES) FORWARD ALONG THE BOTTOM FACE AND 8 MM (0.314 INCHES) UP THE HOLE. FOUND DURING MAGNETIC PARTICLE INSPECTION IAW AT/20 SL 197. (X)SDR DL72S002244Spar · wornRUB MARKS ON FWD I/B LWR END OF AUX SPAR NEAR MLG W/W. REPAIR PER M/M 57-43-0.SDR AT0000477Spar · corrodedDURING A SCHEDULED INSPECTION. FOUND INTERGRANNULAR CORROSION AT RIGHT WING LOWER SPAR LOWER SIDE INBOARD OF FUELING PANEL. CUT OUT CORROSION AND INSTALLED REPAIR IAW REO L-00304.SDR P2EA00406Spar · crackedSJO - DURING Q-CHECK, FOUND THE LEFT WING REAR SPAR SECTION AT RSS 205 TRAILING EDGE ANGLE CRACKED LENGTH .250 INCH WIDTH .005 INCH. REPLACED THE LEFT WING REAR SPAR SECTION AT RSS 205 TRAILING EDGE ANGLE IAW BOEING SRM 51-10-1 PAGE 8. (M)SDR P2EA00355Spar · crackedSJO - DURING Q-CHECK, FOUND THE LEFT WING REAR SPAR SECTION RSS 205 TRAILING EDGE ANGLE CRACKED. (M)SDR AU001079Spar · corroded(AUS) WING CENTER SECTION SPAR TO PN 0512124-35 AND PN 0512124-36 LT AND RT DOOR POST CHANNELS HAD ATTACHMENT RIVETS CORRODED WITH RIVET HEADS MISSING. (X)SDR QXEA0003076Spar Cap · scratchedYXX- SCRATCHES IN UPPER SPAR CAP OF RIGHT HAND WING AT STATION YW202.0, YW203.0, YW210.0, YW320.0, YW316.0, YW301.0, AND YW 285.0. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 1-8 AND RD8-57-1675.SDR AU001076Spar · cracked(AUS) RT UPPER WING FORWARD SPAR CRACKED FROM SLAT CABLE HOLE LOCATED OUTBOARD OF THE FORWARD INTERPLANE STRUT. FOUND DURING INSPECTION IAW AD/DH82/11 AMDT1.SDR AU001049Spar · cracked(AUS) LEFT AND RIGHT WING REAR SPAR WEBS CRACKED AT RELIEF HOLE FOR NR 3 FLAP HINGE BRACKET. (X)SDR QXEA0003075Spar Cap · scratchedYXX- SCRATCHES IN LOWER SPAR CAP OF RIGHT HAND WING AT STATION YW202.0 TO YW203.0. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36, PAGE 1-8 AND SRM 51-20-16, PAGE 5.SDR QXEA0003071Spar Cap · scratchedYXX- SCRATCH IN LOWER SPAR CAP OF LEFT HAND WING AT STATION YW315.0. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 1-8 AND RD8-57-1675.SDR QXEA0003070Spar Cap · scratchedYXX- SCRATCH IN UPPER SPAR CAP OF LEFT HAND WING AT STATION 239.0. REPAIRED IAW DHC-8 RD8-57-1675 AND SRM 51-20-36, PAGE 1-8.SDR 20010503CW001Spar Cap · corrodedFOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR. CORROSION WAS FOUND ON THE FORWARD FACE OF THE SPAR CAP AND WAS DISTRIBUTED ACROSS THE SPAR CAP. RECOMMEND THAT IMPROVED PAINT BE APPLIED TO THSDR AT0100032Spar · corrodedFOUND RIGHT WING REAR SPAR TO HAVE INTERGRANULAR EXFOLIATED CORROSION INBOARD OF CENTER FLAP SUPPORT FITTING. REMOVED CORROSION AND FABRICATED AND INSTALLED SPLICES IAW REO-L00303.SDR AT0000476Spar · corrodedDURING A SCHEDULED INSPECTION . FOUND RIGHT WING REAR SPAR CORRODED INBOARD OF CENTER FLAP SUPPORT FITTING. CUT AND REMOVED CORROSION. FABRICATED AND INSTALLED AFT AND FORWARD SPLICES IAW REO L-00303, REV A, PART 1A.SDR AU001275Spar · corroded(AUS) LT AND RT WING FORWARD AND AFT SPARS CONTAINED PITTING CORROSION IN AREA BETWEEN RIB NR 13 AND RIB NR 18.SDR MWEA001106Spar Cap · damagedLEFT WING LEADING EDGE AT STATION XFS 63.5, THE 3 INBOARD WING HEATER BLANKET ATTACH FASTENERS HOLE ARE OVERSIZED. REPAIRED ATTACH FASTENERS HOLES PER TELEX MWX-ORD-00-00447H.
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