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 UIEA2025032800412Spar · crackedRHW I/B MID FLAP REAR SPAR WEB O/B EDGE FWD CRACK(<P>REAR SPAR WEB CRACK AREA REPAIRED AS PER RI-57-53-17514 REV A. NO FURTHER DEFECTS NOTED</P>)SDR DALA2025041502916Spar Cap · cracked-AD- CRACK WAS FOUND IN LOWER SPAR CAP NEAR XRS=164 DURING INSP OF LT WING REAR SPAR INSP AMDS 5720-01103-01A. "CONTACT LIAISON ENGINEERING FOR REPAIR PRIOR TO FURTHER FLIGHT" FC 5720-01103. COMPLIED WITH PRI 624256-14AD REVS 0, 1, 2, 3, 4, & 5. COMPARED PRI 6SDR KCSA202504051072Spar · crackedL/H WING T/E AUXILARY SPAR UPPER CHORD AT WBL 429.5 HAS POSSIBLE CRACKSDR IXXA202504030010Spar Cap · corrodedLH WING LOWER LE SPAR CAP IS CORRODED JUST OB OF PYLONSDR 9WGA2025100654523Spar · crackedDURING HEAVY CHECK TRANSFERRED FROM DMI# 26493 "PERMANENT REPAIR NEED WITHIN 60 DAYS ON CRACK IN AFT SIDE OF LH WING EXTENDING FROM #1 TANK XFER PUMP HOLE". PERMANENT REPAIR AT REAR SPAR ON AFT SIDE LH WING WAS PERFORMED I.A.W REP-11-545-259-WG AND BOEING REPSDR JGVR20250402001Spar · corrodedREPAIRED CORRODED AREA IN THE LH MLG WHEEL WELL ON THE AFT WING SPAR LOWER CLIP IN BAY 730DL, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR 2025FA0000228Spar · corrodedEXFOLIATION CORROSION WAS FOUND ON THE AFT SIDE OF THE UPPER SPAR ON THE LEFT WING AFTER THE WING HAD BEEN REMOVED FROM THE FUSELAGE. SEVERAL RIVED HEADS WERE FOUND TO BE SHEARED OFF ON THE SPAR WEBS IN BOTH LEFT AND RIGHT WINGS. THE WING WAS REMOVED IN EFFORTSDR JGVR20250331003Spar · corrodedREPAIRED TWO CORRODED AREAS IN THE RH MLG WHEEL WELL ON THE AFT WING SPAR LOWER CLIP, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20250331002Spar Web · corrodedREPAIRED CORRODED AREAS AT OF THE LH WING AFT SPAR WEB AFT FACE AT THE #4 SPEED BRAKE PANEL HYDRAULIC LINE CARRY-THRU FITTINGS, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR KCSA202503291046Spar · crackedDURING ULTRASOUND INSPECTION, CRACK INDICATION NOTED AT LOWER FASTENER HOLE ON RIGHT WING LEADING EDGE UPPER CHORD AT ILES STA 664.SDR CALA2025040103391Spar · corrodedLEFT WING REAR SPAR HAS CORROSION AT IB BOOST PUMP LWR GROUND ATTACH POINT. REF. AAR N/R:9942388 ACCOMPLISHED REPAIR AT R/H OUTER WING FRONT SPAR FUEL BOOST PUMP LOWER BONDING STRAP ATTACH AREA IN REF TO AAR ESR-WI 52-11818 REV IR AND UNITED EC/RA 5720-03508 ESDR DALA2025033102349Spar · cracked-AD- CRACK FOUND IN LWR AFT LEG OF LWR REAR SPAR JUST OB OF FLAP FITTING @ XRS170 DURING LT WING REAR SPAR INSP AMDS #5720-01103-01A. COMPLIED WITH PRI 623680-14AD REVS 0,1,2,3,4,5,6, & 7. COMPARED PRI 623680-14AD REVS 0,1,2,3,4,5,6, & 7 WITH ERA 623680-14AD RSDR CALA2025032803283Spar · corrodedRT WING FRONT SPAR WITH CORROSION AT FUEL BOOST PUMP UPPER BONDING STRAP ATTACH AREA. REF. AAR NR:9942346. ACCOMPLISHED REPAIR AT R/H OUTER WING FRONT SPAR FUEL BOOST PUMP UPPER BONDING STRAP ATTACH AREA IN REF TO AAR ESR-WI 52-11817 REV IR AND UNITED EC/RA #SDR CALA2025032803282Spar · corrodedRT WING FRONT SPAR WITH CORROSION AT FUEL BOOST PUMP LOWER BONDING STRAP ATTACH AREA. REF. AAR N/R:9942347 GENERATED BY: V919797 ACCOMPLISHED REPAIR AT R/H OUTER WING FRONT SPAR FUEL BOOST PUMP LOWER BONDING STRAP ATTACH AREA IN REF TO AAR ESR-WI 52-11818 REV SDR 2025FA0000214Spar · corrodedDURING WING AFT SPAR INSPECTION, FOUND CORROSION AROUND HYDRAULIC FITTINGS ON LH AFT SPAR. DURING BLENDING OF LH WING SPAR FOUND CORROSION UNDER ADDITIONAL FEED THROUGH. DURING ULTRASONIC THICKNESS INSPECTION OF A BLENDED AREA NEAR A FASTENER HOLE ON THE LH AFSDR 2025FA0000213Spar · corrodedDURING LH AND RH WING AFT SPAR INSPECTION FOUND CORROSION AROUND SPEED BRAKE HYDRAULIC FITTING AND SP HYDRAULIC FITTING ON RH WING. PERFORMED REPAIR TO RH WING SPAR WEB CORROSION. PER: NETJETS RFTS-112900 N341QS (680-0225) RH WING SPAR WEB CORROSION, REV.0 DATSDR IPXA2025062740712Spar · crackedCRACK - HOLE , RIGHT WING FRONT SPAR LOWER CHORD SKIN PANEL CRACK AT RIB 32 ( WSTA 1018.2 ), 1 EA. (REPAIR) 1. ACCOMPLISHED JOB I.A.W UPS EO-93536-REQ1 REV1 2. JOB COMPLETED. 3. PARTS PME RECORD UPLOAD.SDR SIMA20250325003Spar · crackedPOSSIBLE CRACK ON LH WING SPAR I END AT WING TIP ATTACHMENT POINT (MARKED) (MAJOR ALTERATION). COMPLETE:RAR LH WING OUTBOARD SPAR 1 IAW ENVOY EO EJ-57MA-024 PART "A" SEE TASKS AND WIPS BELOW FOR DETAILS.SDR IPXA2025041240712Spar · cracked*** SDR FILED OPEN *** FAULT - CRACK - HOLE , RIGHT WING FRONT SPAR LOWER CHORD SKIN PANEL CRACK AT RIB 32 ( WSTA 1018.2 ), 1 EA. (REPAIR) I.A.W AMM 27-81-32-904-001 REV.144 REMOVE RH WING NO.12 SLAT INBOARD SIDE AUXILIARY TRACK.SDR 2025F00075Spar · corrodedMECHANICALLY REMOVED 3 AREAS OF CORROSION LOCATED IN LH MLG WHEEL WELL, AFT SPAR, LOWER CLIP IAW C680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND C680 SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSION BLENDS IAW SDR 2025F00073Spar · corrodedMECHANICALLY REMOVED 2 AREAS OF CORROSION FROM RH WING AFT SPAR, FWD FACE IN RH MLG WHEEL WELL. EVALUATED AND FOUND BLENDED AREAS WERE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINAL THICKNESS. REPAIRED CORROSION BLENSDR HNAA2025051200309Spar · crackedF035242 THE LH WING SPAR I LOWER FLANGE AT RIB #9 IS CRACKED. PERFORMED CUTOUT, FABRICATED REPAIR DOUBLER, FILLER, SHIMS, AND SPACERS FOR LH WING SPAR I REPAIR AT RIB 9 IAW EMB 145 SRM 57-20-05 ITEM 2. AND INSTALLED IAW ETD2025-145-905692 REV B AND EO1-57-25-SDR DALA2025032102127Spar · corrodedCORROSION AT RIGHT WING CENTER SECTION (WCS) REAR SPAR WEB AND SIDE FRAME BULKHEAD FITTINGS. THE CORROSION ON WING CENTER SECTION REAR SPAR WEB AND REAR SPAR BULKHEAD FITTING REPAIRED PER PRI 624520-14 REV 0, PRI 624520-14 REV 1, AND PRI 624520-14 REV 2. COMPASDR 2025F00059Spar · corrodedMECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED ON RH GEARWELL AFT SPAR, FWD FACE, LOWER CLIP, INBD OF WS 37.00 IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND LIMITS IAW C680 SRM 51-70-02 LIMITATIONS EXCEEDING .002" OF MATERIAL REMOVED FROM NOMINALSDR 2025FA0000183Spar Web · corrodedLH WING AFT SPAR WEB CORROSION.SDR R61A2025030800134Spar · crackedDURING HEAVY CHECK FOUND RH WING FOUND CRACKED ON SPAR 1. REPLACED SPAR 1 IAW SB 57-73SDR JR2R20250305934Spar · crackedRH WING O/B SPAR 1 CRACKEDSDR JR2R20250305933Spar · crackedLH WING O/B SPAR 1 CRACKEDSDR JR2R20250226737Spar · damagedRH WING FWD O/B SPAR 1 DAMAGED ON LOWER O/B CORNERSDR COEA2025051305903Spar · corrodedWO 262165 NR 600012 HEAVY CHECK COE/MAJOR REPAIR: R/H UPPER WING RIB 13-21 REAR SPAR UPPER CHORD UPPER SURFACE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS S572K0045..25291 ISS A, DATED 4/18/2025.SDR DALA2025021001046Spar Cap · damaged-AD- AWR, AA, AD, IN REF TO AMDS 5720-01103-01B STEP 7: REPAIR IN PROGRESS AT RIGHT WING LOWER REAR SPAR CAP THATS INCLUDES LOWER WING SKIN AND DOUBLER BTW STA XRS 150 AND XRS 177. SUMMARY OF NRC 00918: THIS REPAIR PROVIDED WITH FAA AMOC APPROVAL AND INCLUDES SDR DALA2025020500884Spar · crackedTHE #13 FASTENER HOLE SHOWS A CRACK INDICATION WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/024 00024: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 31. (LP #0795830)SDR DALA2025020500879Spar · crackedTHE #12 FASTENER HOLE SHOWS A CRACK INDICATION WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/028 00028: NR TRANSFERRED TO H-CK PKG #P-384718220250123 - NR# 35. (LP #0795839)SDR DALA2025020500878Spar · crackedTHE #16 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR AND SKIN LAYERS. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/027 00027: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 34. (LP #0795837)SDR DALA2025020500877Spar · crackedTHE #15 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR AND SKIN LAYERS. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/026 00026: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 33. (LP #0795835)SDR DALA2025020500875Spar · crackedTHE #11 FASTENER HOLE SHOWS A CRACK INDICATION WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/023 00023: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 30. (LP #0795829)SDR DALA2025020500874Spar · crackedTHE #10 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/022 00022: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 29. (LP #0795826)SDR DALA2025020500873Spar Cap · cracked-AD- CRACK COMMON TO THE RH WING LOWER REAR SPAR CAP, COMMON TO THE RH WING REAR SPAR INST AT APPROXIMATELY 5.0" INBD OF XRS 164.000. THE MAIN CRACK MEASURES APPROXIMATELY 0.945" LONG, TERMINATING AT A FASTENER LOCATION. COMPLY WITH RH WING / LOWER REAR SPAR CSDR DALA2025020600917Spar Cap · damaged-AD- ON UPPER LEG OF LEFT WING AFT SPAR LOWER SPAR CAP XRS 164.00 FASTENER ABOVE INBOARD LOWER FLAP FITTING ATTACH BOLT IS LOOSE AND SPINNING. THIS FASTENER REPLACED WITH OVERSIZE FASTENER DURING LEFT WING SKIN DOUBLER RFEPAIR ON ER/A 622371-14AD, REV O. JOB CSDR DALA2025020300801Spar Cap · crackedCRACK ON RH WING LOWER REAR SPAR CAP AROUND SECOND FASTENER FROM FLAP HING FITTING STA XW=154 OUTBOARD TO INBOARD DIRECTION. SUMMARY OF NRC 00347: CRACK ON RH WING LOWER REAR SPAR CAP AROUND SECOND FASTENER FROM FLAP HING FITTING STA XW=154 OUTBOARD TO INBOARDSDR 2025FA0000077Spar · corrodedMECHANICALLY REMOVED 3 AREAS OF CORROSION WITH 1 ADDITIONAL AREA LOCATED ON THE LH AFT WING SPAR, AFT FACE AROUND THE CARRY THROUGH FITTINGS INSIDE FLAP WELL BAY 523AB. MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED AROUND SPOILER HYDRAULIC PRESSURE LINE CARSDR SWAA2025021089588Spar · damagedL/H I/B MAIN FLAP FWD SPAR HAS 2 EACH ELONGATED HOLES ON UPPER FLANGE BETWEEN 9' INCHES AND 12' INCHES FROM I/B SIDE.<[01] REPAIRED PER EA 25-157-00287;[02] REPAIRED PER EA 25-157-00287SDR P5CA2025012800005Spar · damagedWHILE ACCOMPLISHING RH SIDE FRONT SPAR LWR CHORD FASTENER REMOVAL IAW SB 777-57A0122 REV 0 FIG 109, FOUND 1 EACH INCOMING FASTENER WITH ELONGATION(<P>ELONGATED FASTENER HOLE ON RH SIDE FROM SPAR LWR CHORD AREA REPAIRED AS PER EN 006-25 REV 0. REPAIR CATEGORIZESDR JR2R20250126788Spar · crackedRH WING SPAR 1 CRACKED AT WINGTIP ATTACH LOCATIONSDR JR2R20250126370Spar · crackedLH WING SPAR 1 CRACKED AT WINGTIP ATTACH LOCATIONSDR JGVR20250123001Spar · corrodedMECHANICALLY REMOVED 3 AREAS OF CORROSION LOCATED IN LH MLG WHEEL WELL, AFT WING SPAR LOWER CLIP INBOARD OF BAY 730DL PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS PER TEXTRON REPAIR MEMO.SDR IPXA2025022365090Spar · corrodedFAULT - CORROSION - LOWER CHORD, RIGHT WING OUTBOARD FRONT SPAR AT FSSO / OLES 1510 (AGING A/C INSPECTION)PERFORMED REPAIR I.A.W EO-92809-REQ1 REV.1SDR DALA2025011600400Spar · damagedSHIP 3147 AN ELONGATED HOLE WAS FOUND IN THE MIDDLE REAR SPAR AT RIB 14 LEVEL. CORRECTIVE ACTION: COMPLIED WITH E/RA 622832-14. (0762553)SDR DALA2025011300272Spar Cap · cracked-AD- CRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP RADIUS. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT REF FC5720-01103. CRACK IS LOCATED INBD OF XRS 164 AT RIVET HEAD 1/2 INCH ABOVE LWR RADIUS. DISCREPANCY TRANSFERSDR IPXA2025021359559Spar Cap · crackedACCOMPLISH PERMANENT REPAIR PER T/C T3F18E002KT3R ON LT WING REAR LOWER SPAR CAP BETWEEN XORS=714 AND XORS=735. ACCOMPLISH EA#: 011-5710-01-B0319 REVISION P4 STEP: 18 OK TO INSTALL 2 EA REPAIR BUSHING AT LH WING REAR LWR SPAR CAP BETWEEN STA XORS=714 AND XOR
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