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 GUUA94557041611ASpar · corrodedDURING SCHEDULED ROUTINE X-RAY INSPECTION DISCOVERED CORROSION ON LEFT WING FORWARD SPAR AFT FLANGE WS 128.50. REMOVED CORROSION FROM FORWARD SPAR AFT FLANGE AND INSTALLED REINFORCEMENT DOUBLER STRAP.SDR FDEA201104121443Spar · corrodedLT WING REAR SPAR WEB AT IRSS 188 ABOVE FUEL BOOST PUMP UPPER BONDING JUMPER FOUND WITH CORROSION. CORROSION REPAIR CARRIED OUT ON LT WING REAR SPAR WEB IAW EA F-5710-146438. (LT WING REAR SPAR WEB CORROSION BLEND REPAIR). REPAIR IS CLASSIFIED AS MAJOR.SDR F3LA2011041300634Spar · dentedC-CHECK: NON ROUTINE NR30121; RT WING L/E STA 7792/RIB 14 IS DENTED WITH INTERNAL DAMAGE AT CLOSEOUT WEB. REPAIRED RIGHT WING L/E DAMANGE STATION 7792/RIB 14 REPAIRED IAW EA A9-57R-32036 INSTRUTIONS 1-4 AS WRITTEN. HFEC INSPECTED, NO CRACKS WERE FOUND.SDR KGBR110411338ASpar · corrodedRIGHT WING, REAR SPAR WEB HAS CORROSION, WS 5940 AFT SIDE AT BOTTOM SPAR CAP (MARKED).SDR CHQA201100131Spar · crackedDURING INSPECTION A CRACK WAS FOUND ON THE LEFT WING SPAR I TOP FLANGE CRACKED THRU AT RIB 19. THE CRACK WAS 2.745 INCHES LONG AND 0.001 INCHES WIDE THRU THE MATERIAL. THE DAMAGED AREA WAS REMOVED AND A REINFORCING PATCH WAS INSTALLED PER TI-145-11-095.SDR IPXA1M66276Spar · corrodedINSP TYPE:4C, CORROSION UNDER LT WING UPPER T/E PANEL NEAR STA XOS.795 REPAIRED LT WING REAR SPAR UPPER AFT FLANGE REF EO MD11-5710- 42417-A AND STA SA EA 011-5710-01-A3034 REV IR STA XORS 782-798.SDR 2011FA0000228Spar · corrodedCORROSION LOCATED ON RT WING SPAR AFT SIDE, WS 59-61, AT FUEL TANK FLEXIBLE ACCESS.SDR DALA1503459228Spar · crackedWING REAR SPAR CRACKED. REPAIRED IAW AA 5710-01119.SDR 2011FA0000210Spar · corrodedINSP OF WING CTR SECTION IAW AD 2002-26-02 INTER-GRANULAR CORROSION IN EXFOLIATION STAGE WAS DISCOVERED ON THE BOTTOM MAIN SPAR CAP, EXTREME REAR OTBD SECTIONS WHERE IT WAS MILLED TO ACCOMMODATE THE MLG TRUNNION AND JUST INBD. ALSO THE LT AND RT (WING WALK) ISDR DALA1502730982Spar · crackedWING REAR SPAR CRACKING AT XRS 164. REPAIRED IAW AA 5710-01110.SDR AALA20110324TUL05Spar · crackedHFEC SURFACE INSPECTION OF LEFT WING REAR SPAR CAP AT XRS 164.0 INDICATES A CRACK .250 AT 5 O`CLOCK POSITION OF THE LOWER INBOARD FLAP FAIRING ATTACH HOLE. REMOVED AND SPLICED IN NEW SECTION OF REAR SPAR PER EA MD80-57-015745.SDR DALA1404200976Spar · crackedWING REAR SPAR CRACKED AT XRS 164. REPAIRED IAW AA 5710-01110.SDR FOTR2102212307Spar · crackedNR 1 SLAT ACTUATOR OTBD MOUNT SUPPORT ON LT WING FRONT SPAR CRACKED. REMOVED CRACKED WEB FROM L/E LT WING SLAT STA 398.1 IAW SRM 51-30-2. FABRICATED NEW WEB FROM 7075T6 .063 PO 9009533 DIM 4.5" X 9" IAW SB 727-57-0130 FIG 1. INSTALLED REPAIR WEB IAW SB 727-SDR DALA1515590986Spar · crackedWING REAR SPAR CRACKING AT XRS 164 REPAIRED IAW AA 5710-01110.SDR AALA20110502TUL03Spar Cap · crackedRIGHT WING LOWER REAR SPAR CAP AT STATION XRS 164 HAS CRACK INDICATION APPROXIMATELY 1/4 INCH LONG CONFIRMED WITH HFEC SCAN. REPAIRED PER EA MD80-57-016677.SDR FDEA201103140966Rib · misrepairedRE-EVALUATION OF EXISTING REPAIR ON RT WING CTR FLAP BULLNOSE RIBS 19-20 LOCATION CARRIED OUT USING ORIGINAL NRC 0003346 AND SRM 57-50-00, FIG 208. REPAIR SUSPECTED TO HAVE 1 ROW OF SPLICE FASTENERS MISSING FROM THE OTBD SPLICE. REPAIR WAS REMOVED AND SKSDR GUUA95557031211ASpar · corrodedDURING SCHEDULED X-RAY INSP, DISCOVERED RT WING CORROSION ON MAIN SPAR 1.3 X 0.06 INCHES AT WS 124.25. REMOVED CORROSION FROM RIGHT WING LOWER FORWARD SPAR CAP COMPLIED WITH FLOURESCENT PENETRANT INSPECTION ON BLEND OUT AREA NO SIGNS OF CORROSION FOUND ALL ARESDR SWIA201125963Spar Cap · crackedLEFT WING FORWARD SPAR CAP INBOARD OF NACELLE CRACKED AT HI-LOK. (C-CHECK) REPAIRED LEFT WING AUX SPAR PER EMBRAER TECHNICAL DISPOSITION.SDR GLBA20110307GSpar · wornMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE LH WING REAR SPAR BOTTOM LEADING EDGE CHAFFED AT 2 LOCATIONS BY EXT PWR CABLE, OB CHAFF .4" IN LENGTH .1" DEEP, IB CHAFFR .3" IN LENGTH .05" DEEP. MAINTENANCE REPAIRED THE AFFECTED ARESDR CA110321004Spar · deteriorated(CAN) AILERON HINGE FLAP HINGE ATTACH POINT SPRUCE SPARS, WOOD DETERIORATED AT HINGE ATTACH POINT, FALSE SPARS REPLACED. DESCRIBED WITH DWG.SDR UALA2011030401069Spar · corrodedLT WING REAR SPAR WEB CORRODED AROUND FASTENERS BETWEEN IRSS 340 AND IRSS 350 WHERE A FUEL BOOST PUMP IS INSTALLED. REPAIRED IAW 777EN-57-0156.SDR DALA1505270985Spar · crackedWING REAR SPAR CRACKING AT XRS 164. REPAIRED IAW AA 5710-01110.SDR 2011FA0000608Spar · corrodedAT APPROX LT WING STA 56.0, THE UPPER OTBD QUADRANT OF AN ELECTRICAL WIRE PASS THROUGH HOLE IN THE WING SPAR WEB WAS FOUND TO HAVE EXFOLIATION CORROSION. THE PASS THROUGH HOLE, WHICH IS IN THE LANDING GEAR WHEEL WELL AREA, HAD A CATERPILLAR GROMMET INSTALLED TSDR FDEA201102200639Spar · damagedSPAR REF EO 6-5710-7-3305 PART 2, STEP 15 HOLE (I) DIAMETER OF HOLE EXCEEDED EO REQUIREMENT LIMIT. HOLE (I) DIAMETER = 0.572" (MAXIMUM DIAMETER ALLOWED = 0.531"). EO 6-5710-7-3305 PART 2, STEP 15 HOLE (I) DIAMETER REPAIR HAS EXISTING REPAIR RECORD AND PREVISDR IPXA11M65152Spar · corrodedINSPECTION TYPE:3C, SIGNFICANT MATERIAL LOSS DUE TO LATCH WEAR ON LT WING LOWER FWD SPAR FLANGE AT DOOR 526FB. AFTER REMOVAL OF LATCH WEAR PLATES FOUND SPAR FLANGE CORRODED UNDER EACH PLATE STA XFS910 & XFS924. REPAIRED SPAR FLANGE REF EO MD11- 5720-41719-A SDR FXGA20110217001Spar · crackedTHE CENTER SPAR WEB WAS FOUND CRACKED AT W/S 90R. REPAIRED PER EAC EO 1103 AND 8110-3 DATED 2/12/11SDR SWIA201125966Spar Cap · crackedLEFT WING INBOARD INTERNAL SPAR CAP IS CRACKED AT HI-LOK. (C-CHECK) REPAIRED LEFT INBOARD WING INTERNAL SPAR CAP PER EMBRAER TECHNICAL DISPOSITION.SDR SWAA110886Spar · crackedDURING SCHEDULED 20Y CHECK, FOUND LT WING CRACKED ON UPPER CHORD REAR SPAR RSS 223.14. REPAIRED SPAR PER EA.SDR IXXA11SMN048SSpar Cap · crackedDURING ROUTINE C-CHECK INSP FOUND RT WING FRONT SPAR L/E LOWER CAP CRACKED AT STA XFS 500.233. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSP, NO DISCREPANCY FOUND. FABRICATED SPLICE ANGLES, EXTERNAL DOUBLER, STRAP. CLEANED, TREATED, PRIMSDR QXEA2011021400150Spar · chafedC1 CHECK - AFT WING SPAR PANEL MONTING FLANGE FOR PANEL 262AT HAS FRETTING. BLENDED OUT CHAFE DAMAGE IAW RD 8/4-53-451. CONFIRMED CRACK FREE CONDITION AND FOUND WITHIN LIMITS IAW RD 8/4-53-451. REPAIR COMPLETED IAW RD 8/4-53-451.SDR QXEA2011021400149Spar · chafedC1 CHECK - AFT WING SPAR PANEL MOUNTING FLANGE UNDER PANEL 262FT HAS FRETTING. BLENDED OUT CHAFE DAMAGE IAW RD 8/4-53-451. CONFIRMED CRACK FREE CONDITION AND FOUND WITHIN LIMITS IAW RD 8/4-53-451. REPAIR COMPLETED IAW RD 8/4-53-451.SDR QXEA2011021400148Spar · chafedC1 CHECK - AFT WING SPAR PANEL MOUNTING FLANGE UNDER PANEL 262HT HAS FRETTING. BLENDED OUT CHAFE DAMAGE IAW RD 8/4-53-451. VERIFIED CRACK FREE CONDITION AND FOUND WITHIN LIMITS IAW RD 8/4-53-451. REPAIR COMPLETED IAW RD 8/4-53-451.SDR EE4Y20110094Anchor Fitting · corrodedLEFT OUTER WING REAR SPAR AFT FACE RETRACTION JACK ANCHORAGE FITTING CORRODED AROUND THE BORE UPPER AND LOWER AND IN THE BORE INNER SURFACE. DAMAGED PART IS GOING TO BE REPAIRED FOLLOWING REPAIR INSTRUCTIONS.SDR H5GR20110218001Spar · crackedDURING THE ANNUAL INSP, A CRACK IN THE RT FWD SPAR, FWD WEB BEND RADIUS WAS NOTICED DURING A VISUAL INSP OF THE AREA. A DYE PENETRANT INSP WAS PERFORMED AND CRACK VERIFIED. INSP WAS PERFORMED FOLLOWING MM, PN: 55-590000-13G, REV G2, SECTION 53-00-00, PAGE 202SDR FDEA201102010439Spar Cap · corrodedRT WING T/E UPPER AFT SPAR CAR TOP SURFACE FOUND CORRODED AT WING STA XORS 980. SPAR CAP CORROSION REPAIRED AS PER E.A. 1-5710-143520, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.SDR MU1Z2011020200001Spar · corrodedDURING HEAVY AND DELIVERY MAINTENANCE CHECK; RIGHT MAIN LANDING GEAR W/W AT CENTER WING REAR SPAR RBBL 74.57" AND 2 INCH DOWNWARD OF THE WL 178.02 CHORD WAS FOUND CORROSION (LEVEL 3).SDR CA110131010Aap · chafed(CAN) ACM LOUVERED EXHAUST PLENUM REMOVED TO CARRY OUT "F" CHECK PROCEDURE. NOTED AFTER REMOVAL OF LOUVERED PLENUM THAT THE PLENUM WAS CHAFING INTO THE LOWER MAIN SPAR CAP FORWARD FLANGE AT LWS 35-LWS 40. LWS 35 SPAR CAP FLANGE CHAFED TO 0.06 INCH AND DECREASESDR DALA1514330987Spar · crackedWING REAR SPAR CRACKED AT XRS 164 REPAIRED IAW AA 5710-01110.SDR FDEA201101250355Spar · crackedDURING HFEC OPEN HOLE INSPECTION CRACK INDICATION FOUND AT RT CTR WING BOX OF REAR SPAR HOLE (I) ON SECOND LAYER EDGE FROM FWD APPROX 0.5" (L2) LONG. THE THIRD LAYER CRACK IS NOT A CRACK AT ALL. INSTEAD IT IS A STRAIGHT LINE BUTT-JOINT BETWEEN THE REAR SPAR SDR FDEA201101210328Frame · crackedDURING HFEC OPEN HOLE INSP CRACK INDICATION FOUND AT LT CTR WING BOX OF REAR SPAR HOLE (N) ON SECOND LAYER EDGE FROM AFT APPROX 0.012" (L1) DEPTH AND 0.010" (L2) LENGTH. REPAIR CARRIED OUT IAW EO 6-5710-7-3305D PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100SDR FDEA201101210327Frame · crackedDURING HFEC OPEN HOLE INSP CRACK INDICATION FOUND AT LT CTR WING BOX OF REAR SPAR HOLE (M) ON SECOND LAYER EDGE FROM AFT APPROX 0.012" (L1) DEPTH AND 0.010" (L2). REPAIR CARRIED OUT IAW EO 6-5710-7-3305D, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REVSDR FDEA201101210326Frame · crackedDURING HFEC OPEN HOLE INSP CRACK INDICATION FOUND AT LT CTR WING BOX OF REAR SPAR HOLE (LT) ON SECOND LAYER EDGE FROM AFT APPROX 0.012" (L1) DEPTH AND 0.010" (L2) LENGTH. REPAIR CARRIED OUT IAW EO 6-5710-7-3305D, PART 1. REPAIR CLASSIFIED MAJOR GMM 6-2-100SDR FDEA201101170213Spar Cap · crackedLT WING AFT LWR SPAR CAP, FOUND 3 CRACKED HOLES ON THE OTBD ROW AND 1 CRACKED HOLE ON THE FWD MOST INBD LT WING AFT LOWER SPAR HAS BEEN REPAIRED AND COMPLIES WITH EA NR 8-5710-142566.SDR GUUA93757011711CSpar Cap · corrodedDURING SCHEDULED X-RAY INSP DISCOVERED LT WING CORROSION AT LOWER FWD SPAR CAP NEAR FUEL DRAIN WS 125.5. REMOVED CORROSION FROM LEFT WING AT LOWER FORWARD SPAR CAP NEAR FULE DRAIN WS 125.5 AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR GUUA93757011711BSpar Cap · corrodedDURING SCHEDULED X RAY INSP DISCOVERED RT WING CORROSION AT LOWER FWD SPAR CAP NEAR FUEL DRAIN. REMOVED CORROSION FROM RIGHT WING LOWER FORWARD SPAR CAP COMPLIED WITH FLOURESCENT INSPECTION ON BLEND OUT AREA NO SIGNS OF CORROSION FOUND,ALL AREAS WITHIN LIMITSSDR FDEA201101170214Spar · crackedLEFT WING REAR SPAR LOWER CHORD ANGLE AT STA.XORS 345 HAS A CRACK INDICATION THROUGH 3 FWD FWD HOLES AND CAN BE SEEN ON THE AFT SIDE EXTENDING OUT OF THE RADIUS APPROX.1" AFT AND UP THE VERTICAL LEG UNDER THE FITTING. (VERIFIED BY N.D.T) REPAIRED AND COMPLISDR FDEA201101160183Frame · crackedDURING HFEC OPEN HOLE INSP CRACK INDICATION FOUND AT LT CTR WING BOX OF REAR SPAR HOLE. REPAIRED IAW EO 6-5710-7-3305D PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV I 111.SDR VGQY2011011500009Spar Cap · corrodedRT MAIN LANDING GEAR WHEEL WELL - FOUND CORROSION AT OUTER WING REAR SPAR CAP, UPPER SIDE-BOTTOM SURFACE - STA XORS 118.200. COMPLIED WITH EA DC10-5730-1133.SDR VGQY2011011500007Spar · corrodedLT WING INNER REAR SPAR APPROX STA XORS 264 FOUND EXTRUSION CORRODED. COMPLIED WITH EA DC10-5710-1131.SDR VGQY2011011500006Spar Cap · corrodedLT WING INNER REAR SPAR APPROX STA XORS 197 FOUND EXTRUSION CORRODED. COMPLIED WITH EA DC10-5710-1132.
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