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 UPS02438648Spar · corrodedINSPECTION TYPE:C, RT JETTISON PUMP ATT BONDING JUMPER ATT REAR SPAR BOLT HOLE SURFACE CORR AT WLG W/W STA 1241 RT AFT FACE RBL 91.8. CUTOUT RT WLG W/W BS 1241 REAR SPAR WEB JETTISON PUMP, CUTOUT ATT BONDING JUMPER ATT. FASTENER HOLE REPAIRED IAW RS R57-12-3SDR QXEA0200817Spar · chafedPDX - CHAFING ON FORWARD SPAR OF LT WING AT STATION YW202.000. REPAIRED IAW HORIZON AIR EA 2-57-163.SDR QXEA0200813Spar Cap · scratchedPDX - MULTIPLE SCRATCHES IN UPPER SPAR CAP ON FORWARD EDGES OF WING SKINS. REPAIRED IAW HORIZON AIR EA 2-57-265.SDR 200200251Spar · crackedA CRACK WAS FOUND COMMON TO THE UPPER CHORD OF THE RIGHT WING TRAILING EDGE AUXILIARY SPAR AT WBL 425. THIS DISCREPANCY WAS REPAIRED BY REMOVING THE DAMAGED SECTION OF CHORD AND SPLICING IN A NEW SECTION OF CHORD WITH REPAIR ANGLES PER EIA ECRA 470-57-141-02.SDR QXEA0200812Spar Cap · scratchedPDX - MULTIPLE SCRATCHES IN THE LOWER SPAR CAP AND ON THE FORWARD EDGE OF WING SKINS. RT WING LOWER FRONT SPAR CAP BETWEEN FUSELAGE AND NACELLE ADJACENT TO AFT EDGE OF LEADING EDGE. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-57-1150.SDR QXEA0200811Spar Cap · chafedPDX - FRONT SPAR CAP HAS BEEN CHAFED BY LEADING EDGE. RT WING INBOARD LEADING EDGE LOWER SPAR CAP AT STATION YW57. REPAIRED IAW RD 8-57-811.SDR QXEA0200809Spar Cap · scratchedPDX - VARIOUS SCRATCHES AND GOUGES IN THE LOWER SPAR CAP. RT WING FRONT SPAR LOWER CAP, FROM NACELLE TO STATION YW288. REPAIRED IAW RD 8-57-2054.SDR QXEA0200807Spar Cap · scratchedPDX - VARIOUS SCRATCHES AND GOUGES IN UPPER FRONT SPAR CAP, RT WING, LEADING EDGE AREA. FRONT SPAR UPPER CAP FROM NACELLE TO YW288. REPAIRED IAW RD 8-57-1675.SDR QXEA0200806Spar Cap · scratchedPDX - NUMEROUS SCRATCHES AND GOUGES IN THE LOWER SPAR CAP, RT WING FRONT SPAR LOWER CAP FROM NACELLE TO YW288. REPAIRED IAW RD 8-57-1675.SDR AUS20020431Attach Angle · cracked(AUS) FORWARD SPAR ATTACHMENT STRUCTURE LT AND RT SIDE CRACKED.SDR QXEA0200810Spar Cap · gougedPDX - SCRATCHES AND GOUGES IN UPPER FRONT SPAR CAP. RT WING LEADING EDGE AREA FRONT SPAR UPPER CAP FROM NACELLE TO STATION YW288. REPAIRED IAW RD 8-57-2054.SDR SIMA200212301Spar · corrodedDURING CPCP2 LEFT WING AFT SPAR UPPER ANGLE CORRODED BETWEEN INBOARD AND OUTBOARD AILERON HINGE POINTS. LEFT WING AFT SPAR REPAIR BY BLENDOUT IAW EO E1-57MR-107. (M)SDR 2002FA0000649Spar · crackedLEFT WING REAR SPAR COMPRESSION CRACK AT STRUT ATTACH POINT BETWEEN DOUBLER ON UPPER SURFACE.SDR ABXA010864Spar · crackedRIGHT WING FRONT SPAR OUTBOARD HOLES, HOLE NR 12, FROM TOP HAD A CRACK INDICATION WITH NDT. REAMED HOLE SIZE TO .387, NO CRACKS FOUND IAW B767 NDT MANUAL PT6 51-00-19. INSTALLED OVERSIZED FASTENERS IAW REA B657-43120MR.SDR ABXA010866Spar · crackedRIGHT WING, FRONT SPAR, OUTBOARD HOLES, HOLE NR 10 FROM TOP, HAD A CRACK INDICATION WITH NDT. REAMED HOLE SIZE TO .387, NO CRACKS FOUND IAW B767 NDT MANUAL PT6 51-00-19. INSTALLED OVERSIZED FASTENERS IAW REA B657-43120MR.SDR ABXA010865Spar · crackedRIGHT WING, FRONT SPAR, OUTBOARD HOLES, HOLE NR 4 FROM TOP, HAD A CRACK INDICATION WITH NDT. REAMED HOLE SIZE TO .387, NO CRACKS FOUND IAW B767 NDT MANUAL PT6 51-00-19. INSTALLED OVERSIZED FASTENERS IAW REA B657-43120MR.SDR CALA0200246Spar · crackedINSPECTION FOUND THE RT AND LT WING REAR SPARS HAD A 0.050 INCH CRACK INDICATION AT HOLE AT MLG BEAM ATTACH FITTINGS.SDR TSAA0253125Spar · corrodedFOUND CORROSION ON RIGHT WING FRONT SPAR, LOWER CHORD FORWARD HORIZONTAL FLANGE FORWARD LIP AT FSS 413. REMOVED CORROSION BY BLEND OUT. HFEC AREA TO ENSURE FREE OF CRACKS AND CORROSION. FABRICATED A REPAIR FILLER. INSTALLED REPAIR FILLER. REPAIR COMPLETEDSDR 474Spar · crackedC/W AD 00-25-02R1 FOUND CRACK AT BUTT OF MAIN SPAR JUST UNDER ATTACH FITTING TO FUSELAGE ON R/H WING TRAVELING SEVERAL INCHES LONGITUDINALLY AND PARALLEL- SEVERAL RIB NAILS LOOSE ON BOTH WINGS- AIRCRAFT HANGARED FOR SEVERAL YEARS (20)VERY LOW USEAGE- CAUSE UNKSDR CA020507019Spar Cap · corroded(CAN) INTERGRANULAR CORROSION FOUND ON TOP SPAR CAP (ANGLE) BOTH WINGS. REQUIRED REPLACEMENT (FOUND AT ANNUAL INSPECTION).SDR 2002FA0000637Spar · crackedIN COMPLYING WITH AD, FOUND CRACK AT BUTT OF MAIN SPAR JUST UNDER ATTACH FITTING TO FUSELAGE ON RIGHT WING TRAVELING SEVERAL INCHES LONGITUDINALLY. SEVERAL RIB NAILS LOOSE ON BOTH WINGS. AIRCRAFT HANGARED-CAUSE UNKNOWN, (HOURS ON WINGS 5000 TO 6000), REPAIR SDR QXEA0200714Spar · chafedPDX-LOWER RT INBOARD WING SPAR IS HEAVILY CHAFED AND TEFLON PAINT IS MISSING. REPAIRED IAW DHC-8 RD8-57-811 AND SRM 51-20-26.SDR UPS02838285Spar · crackedINSPECTION TYPE:C2 CRACK INDICATIONS FOUND BY NDT ON HOLE NR 11 LT. REAMED AND COINED HOLE, FABBED AND INSTALLED BUSHING IAW REO G08603.SDR UPS02838256Spar · crackedINSPECTION TYPE:C2 CRACK INDICATIONS FOUND BY NDT ON HOLE NR 9 LT. REAMED AND COINED HOLE, FABBED AND INSTALLED BUSHING IAW REO G08603.SDR UPS02838281Spar · crackedINSPECTION TYPE:C2 CRACK INDICATIONS FOUND BY NDT ON HOLE NR 9 LT. REAMED AND COINED HOLE, FABBED AND INSTALLED BUSHING IAW REO G08603.SDR QXEA0200653Spar · gougedPDX- PANEL MATTING SURFACES THROUGHOUT FORWARD SPAR ARE GOUGED AND SCRATCHED ON FORWARD TURTLE BACK AREA. REPAIRED IAW DHC-8 SRM 51-20-36, 51-20-16 AND RD 8-57-1441.SDR MWEA020250Cap · inadequateCOMPLY WITH CARRY OVER 2681. LOWER CAP REPAIR, LEFT WING, AT STATION 380 REQUIRES REMOVING TEMPORARY REPAIR AND INSTALLATION OF PERMANENT REPAIR. -- FABRICATED AND INSTALLED FILLERS AND REPAIR ANGLES.SDR QXEA0200681Spar · scratchedPDX- THERE IS A DEEP SCRATCH ON LEADING EDGE MATTING SURFACE OF LT WING FORWARD SPAR UPPER LIP FROM YW171.000 TO YW202.000. REPAIRED IAW RD 8-57-1119.SDR CALA0200192Spar · crackedINSPECTION FOUND A .125 INCH CRACK IN RT WING REAR SPAR UPPER CHORD AT MLG BEAM ATTACH FITTING. THE CRACKED AREA WAS REMOVED AND A FREEZE PLUG WAS INSTALLED.SDR CA020506005Spar · cracked(CAN) UPON CLOSE VISUAL INSPECTION A CRACK WAS FOUND IN THE CENTRE OF THE BUTT OF THE RIGHT FRONT SPAR. THE CRACK RUNS AT LEAST AS FAR AS THE BUSHING AT THE WING ATTACH BRACKET, BUT IS HIDDEN FROM THE FRONT AND BACK BY THE DOUBLER PLATE. WING TO BE REMOVED FORSDR QXEA0200593Spar · damagedPDX- REFERENCE HORIZON AIR EA 2-57-158 RIGHT HAND FRONT SPAR UPPER FLANGE DAMAGE.SDR QXEA0200594Spar · corrodedPDX- UPPER FLANGE OF REAR WING SPAR HAS LIGHT FRETTING CORROSION AT STATION X426.9. REPAIRED IAW DHC-8 RD 8-57-1434.SDR QXEA0200623Spar · corrodedPDX- SCRATCH AND FRETTING CORROSION ON RIGHT WING FORWARD SPAR AROUND SCREW HOLE FOR RIGHT LEADING EDGE 611 AT TOP INBOARD NEXT TO FUSELAGE. REPAIRED IAW DHC-8 SRM 51-00-06 AND HORIZON AIR EA 2-57-158.SDR QXEA0200622Spar · gougedPDX- GOUGES ON TOP OF RIGHT WING FORWARD SPAR AROUND TOP OUTBOARD SCREW HOLES. REPAIRED IAW HORIZON AIR EA 2-57-158.SDR QXEA0200616Spar · chafedPDX- UPPER FLANGE OF FORWARD WING SPAR HAS CHAFE DAMAGE AT FRAME 38.4/LBL 52.0 TO RBL 52.0. REPAIRED IAW DHC-8 RD 8-57-1441.SDR QXEA0200615Spar · corrodedPDX- UPPER FLANGE OF REAR WING SPAR IS CHAFED AND POSSIBLE FRETTING CORROSION. REPAIRED IAW DHC-8 SRM 51-20-11 AND RD 8-57-1434.SDR QXEA0200596Spar · corrodedPDX- UPPER FLANGE OF WING REAR SPAR HAS LIGHT FRETTING CORROSION AT STATION X426.9. REPAIRED IAW DHC-8 RD 8-57-1434.SDR 200200195Spar · corrodedCORROSION ON BS 1241 WCS REAR SPAR WEB AT LBL 80. THE CORROSION WAS BLENDED PER SRM.SDR 200200190Spar · corrodedREPAIR OF CORROSION ON WCS REAR SPAR WEB AT RBL 98.55. THE CORROSION WAS BLENDED PER B747 SRM 57-10-01.SDR UPS02837959Spar · crackedINSPECTION TYPE:N/A LEFT WING AFT SPAR UPPER CHORD CRACKED. DEFERRED PERMANENT REPAIR PER MM 28-10-01 PG 207 D234849 ASSIGNED.SDR 2002FA0000409Spar · corrodedREAR SPAR SEVERELY CORRODED UNDER STEEL ATTACH PLATES, P/N 66762-00. DAMAGE WAS FOUND WITH A FLASHLIGHT AND MIRROR, LOOKING AT THE FORWARD SIDE OF THE SPAR THROUGH THE INBOARD RIB LIGHTENING HOLES AND WAS SO FAR PROGRESSED THAT THE EXFOLITATION PROCESS HAD BULSDR 0200949602Spar Cap · crackedDuring Hck in ATL, the L/H wing spar revealed corrosion in the lower spar cap at the inbd and outbd attach holes for the flap hinge fitting. A .625 crack was found at the inboard hole. Repaired per EA 96-188409.SDR CA020327002Spar · corroded(CAN) PLATES TO BOTH THE LEFT & RIGHT ATTACHMENT OF AFT WING SPAR TO FUSELAGE FOUND BADLY CORRODED AND NECESSITATED REPLACEMENT.THIS WILL CAUSE DISSIMILAR METAL. THE PLATES ARE RIVETED TO THE AFT SPAR. NEW PLATES ORDERED. ATTACHED PHOTO SHOWS CONDITION. THE ALSDR 2002FA0000356Spar · damagedWHILE RECOVERING WINGS FOUND NUMEROUS LOOSE RIBS THAT HAD RUBBED GROVES IN THE SPARS. SOME SMALL CRACKS ORIGINATING FROM THE NAIL HOLES. AIRPLANE HAD BEEN USED IN AEROBATICS. REPLACED ALL FOUR WING SPARS.SDR CA020318001Spar · cracked(CAN) CRACKED RIGHT REAR LOWER SPAR CAP BEING REPLACED IN ACCORDANCE WITH CF92-26. FURTHER CRACKING DISCOVERED IN WING SPAR WEB AT RBL 50 DURING REPAIRS. THIS AREA IS OUTSIDE OF THE INSPECTION REQUIREMENTS OF THE AIRWORTHINESS DIRECTIVE.SDR CALA0200130Spar · crackedINSPECTION FOUND A 0.2" CRACK IN L/H WING UPPER SPAR AT #4 HOLE FROM THE I/B SIDE COMMOM TO THE SUPPORT FITTING. AN OVERSIZED BOLT WAS INSTALLED IAW ECRA 5743-01050. A DETAILED VISUAL INSPECTION OR HFEC INSPECTION WILL BE PERFORMED ON THE SPAR VERTICAL FLANGE SDR CA020313001Spar · cracked(CAN) LT WING SPAR CRACKS WERE FOUND. THE FRONT SPAR WAS CRACKED FROM THE STRUT ATTACHMENT OUTBOARD. THE REAR SPAR HAD A SEVERE COMMPRESSION CRACK STARTING 3 FEET FROM WINGTIP, PROGRESSING OUTBOARD.SDR 2002FA0000528Spar · crackedWHIN WAS INSPECTED PRIOR TO RECOVER. THIS INSPECTION SHOWED NO CRACKS. WING WAS RECOVERED AND STORED PRIOR TO SINTALLATION. THE WIND BLEW WING AND STORAGE RACK OVER. THE RACK FELL ONTO THE WING. AN INSPECTION WAS DONE. INSPECTION FOUND TWO CRACKS AT THE SDR QXEA0200486Spar Cap · corrodedPDX - FRETTING CORROSION AT MOST INBOARD BOLT HOLE, BOTTOM SPAR CAP, LT WING AT STATION YW57.0. REPAIRED IAW DHC-8 SRM 51-20-36, PAGE 6, PARAGRAPH F, STEPS 1 AND 2.SDR AUS20020158Spar · cracked(AUS) REAR SPAR WEB CRACKED ON RT SIDE AT WS 27.063. FOUND DURING INSPECTION IAW AD/SWSA226/86.
Back to JASC 5711