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 UHLA2013083000452Spar · crackedMAJOR REPAIR - LT WING HAT SPAR II RIB 10 NOT PERPENDICULAR TO SKIN. FABRICATED AND INSTALLED NEW BUSHING IN LT WING A3 HOLE AT SPAR II RIB 10 ETD 2013-170-03448, REV C.SDR FDEA201308302080Spar · crackedRT WING FRAME 47, VERTICAL HOLE G, REF EO 6-5710-7-3305PT4 HAS CRACK INDICATION HOLE DIA 0.515". REPAIRED IAW EA 6-5710-T0301726.SDR C77A20130828001Spar · crackedTWO CRACKS IN LT STUB WING SPAR III ,CRACK INDICATIONS AT THE 3 & 7 O`CLOCK, CRACKS START AT THE FWD SURFACE OF THE BLKHD EXTEND 0.125" INTO THE BORE WITH AN AMPLITUDE OF 100 PERCENT AND 60 PERCENT. PHASE ANGLE= 311, DEGREES L=0.300") WERE FOUND IN THE CRITISDR SIMA20130826024Spar · crackedLT SPAR 3 CRACKED BETWEEN RIB 3 AND 4. LT SPAR 3 CRACKED BETWEEN RIB 3 AND 4. REPAIRED IAW EO EM-57MR-711.SDR 2013FA0000640Spar Cap · corrodedFOUND CORROSION TO LOWER MAIN CARRY THROUGH SPAR BOX CHANNEL BS 109. DAMAGE EXTENDED FROM 7 INCHES LT OF CENTERLINE OF FUSELAGE, AND CONTINUED TO 20.5 INCHES LT OF FUSELAGE CENTERLINE. APPROXIMATELY 50 PERCENT OF THE THICKNESS OF THE FORWARD LIP OF THE LOWERSDR FDEA201308232017Spar · corrodedRT WING REAR SPAR BELOW RT FUEL PUMP HAS CORROSION. COMPLIED WITH EA F-5710-T0300819 STEPS 1, 2 WING -BASIC STRUCTURE-WING SPAR CORROSIONS AT AFT BOOST PUMPS MOUNT. MAJOR REPAIR.SDR ABXA201308185012Spar · corrodedLEFT WING REAR SPAR APPROX. W.S. 250 AT APU FUEL SHUTOFF VALVE MOUNTING BASE CORRODED. MARKED. REPAIRED REAR SPAR IAW REA B657-60671-MR. REAR WING SPAR, PN: 112T1007-7, SN: NSN, LOC: RSS-250.00, CORRODED; ACFT WAS GROUNDED.SDR GLBA2013081300293Spar Cap · chafedDURING A SCHEDULED INSP, FOUND CHAFING ON THE AFT SPAR LOWER CAP AT WS 85.50, APPROX .002 DEEP WITH A SMALL NICK IN THE CENTER OF THE CHAFE, NO OTHER DAMAGE IS NOTED, WIDTH OF THE DAMAGE IS 1.125". REPAIRED IAW EO 13-1900-57-015.SDR R61A201308120741Spar · crackedDURING HEAVY CHECK, LT WING UPPER SKIN CRACKED ABOUT .750 LONG AT SPAR 2 RIB 10. MX REPAIRED LT WING UPPER SKIN IAW ETD 2013-170-028510.SDR SIMA20130731007Spar · crackedCRACK ON LT WING SPAR, STARTING ON MLG WIRE HARNESS ACCESS HOLE GOING UPWARDS TO 1 O'CLOCK, CRACK APROX 2.4". ACCOMPLISHED EDDY CURRENT INSP IAW ETN-EM-51-113. FOUNDED LINEAR INDICATION ON DISPLAY UNIT.SDR DALA13036739247Spar · corrodedLEFT WING REAR SPAR AT APPROX STA XRS 160, REAR SPAR LOWER CHORD IS CORRODED. TASK 57-002-00. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR IAW SRM 51-10-03, 51-30-05 AND ERA 513402-14, REV O.SDR IPXA2016080206622Spar Cap · corrodedINSPECTION TYPE: 1C, LT WING REAR SPAR CAP HAS CORROSION BETWEEN XORS. 784.5 TO 829. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A6374 REV. I/R AND EO MD11-5710-61421-A.SDR 2013FA0000441Spar · crackedDURING INSPECTION OF WING IAW AD 2000-25-02R1, FOUND CRACK IN REAR SPAR ABOUT THREE INCHES LONG. ORIGINATES FROM FLAP SUPPORT BRACKET ATTACH POINT OUTWARD.SDR FDEA201307111545Spar · crackedRIGHT WING REAR LOWER SPAR HAS A CRACK AT XORS 402-452. REPAIRED IAW EA 8-5710-T03001500.SDR ERAA201307080049Spar Web · chafedRIGHT WING REAR SPAR HAS DEEP CHAFE SPOT CAUSED BY SPLIT FLAP SWITCH WIRE WS120.98 AND WS121.73. REPAIRED (BLENDED)CHAFING RT WING AFT SPAR WEB, WS 120 IAW FIELD REPAIR FR-CO-100695.SDR R61A201306290629Spar · damagedDURING HEAVY CHECK, FOUND LOOSE HYD LINE FITTING HAS CAUSED DAMAGE TO THE FWD SIDE OF AFT SPAR 3 ON RT WING INSIDE PANEL 622DB. MX REAMED HOLE TO 35 MM, FABRICATED REPAIR BUSHING IAW ETD 170-014321, REV B.SDR R61A201306290621Spar · damagedDURING HEAVY CHECK, FOUND HYD SYSTEM 1 PRESSURE LINE ON LT WING IS LOOSE AND CAUSING DAMAGE TO SPAR 3 FWD FACE. MX REAMED AFFECTED HOLE, FABRICATED AND INSTALLED REPAIR BUSHING IAW ETD 2013-170-014321, REV A AND B DATED 7-12-13SDR ABXA20130621472Spar · corrodedLEFT WING AT UPPER REAR SPAR WS 975 JUST AFT OF OTBD AILERON FOUND WITH CORROSION UNDER COMPOSITE PANEL JUST FWD OF OTBD AILERON, BLENDED CORRODED AREA FOUND TO BE OUT OF LIMITS. REPAIRED AREA IAW REA B657-60579-MR AND IAW SRM 51-40-02. ACFT WAS GROUNDED.SDR FDEA201306201357Spar · crackedNDT INSPECTION OF CENTER WING BOX, CENTER SPAR AT CUTOUT DOUBLER RUNOUT RT AT FR 44, CRACK FOUND AT RT UPPER HOLE 7 I, INDICATION 25 PERCENT FSH 10MM FROM AFT FACE AT APPROXIMATE VERTICAL POSITION. REPAIRED IAW EA 6-5710-167466.SDR UHLA2013061800249Spar · chafedRT WING HYD LINE FITTING FOR SYS NR 2 PUMP PRESSURE HAS WORN INTO SPAR III FEED THOUGH AFT OF MLG ACTUATOR. R & R FABRICATED REPAIR BUSHING IAW ETD 2013-170-012216. MAJOR REPAIR.SDR FDEA201306071221Spar · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION IAW EO 6-5710-7-3305, PART 4, STEP 11 OF HOLE 'C' AT RT WING REAR SPAR FOUND CRACK INDICATION AT 6 O'CLOCK TOWARDS AFT. REPAIRED IAW EA 6-5710-T0300640 REV A, P1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100SDR REXA2013053000682Spar · damagedDISCREPANT HOLE DRILLED INTO UPPER FLANGE OF RT WING L/E SPAR AT WS274 MEASURING .128" DIA. REPAIRED IAW EA CRJ257-01627 AND ASSOCIATED 8110-3.SDR QXEA2013052401040Spar · corrodedRIGHT WING L/E SPAR LOWER FLANGE HAS BARE METAL WITH CORROSION AT STA YW 193. REMOVED CORROSION IAW SRM (REV 12) 51-21-00-00-02. VERIFIED AFFECTED AREA TO BE CRACK FREE, REF NDTM PART 1, TASK 51-00-06-910-801, REV 9. BLENDS IN LIMITS IAW RD8/4-57-2109, ISDR QXEA2013052401039Spar · corrodedRT WING L/E SPAR UPPER FLANGE HAS BARE METAL WITH CORROSION FROM STA YW 225.263. REMOVED CORROSION IAW SRM 51-21-00-00-02, REV 12. VERIFIED AFFECTED AREA TO BE CRACK FREE, REF NDTM PART 1, TASK 51-00-06-910-801, REV 9. BLENDS WITHIN LIMITS IAW RD8/4-57-210SDR QXEA2013052401038Spar · corrodedRIGHT WING L/E SPAR LOWER FLANGE HAS BARE METAL WITH CORROSION FROM STA YW 225-263. REMOVED CORROSION IAW SRM 51-21-00-00-02. VERIFIED AFFECTED AREA TO BE CRACK FREE, REF NDTM PART 1 TASK 51-00-06-910-801. BLENDS IN LIMITS IAW RD8/4-57-2109 ISS 1.SDR QXEA2013052101037Spar · corrodedLEFT WING FRONT SPAR LOWER FLANGE HAS AREA OF BARE METAL WITH CORROSION AT BS YW 227.019. REMOVED CORROSION IAW SRM 51-21-00-00-02, REV 12. CONFIRMED BLENDED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1, REV 9. NO MATERIAL LOSS ALLOWED, FOUND TO BE OUT OFSDR QXEA2013052101036Spar · corrodedLEFT WING FRONT SPAR UPPER FLANGE HAS AREA OF BARE METAL WITH CORROSION FROM WING STA YW 191.200 TO 227.019. REMOVED CORROSION IAW SRM 51-21-00-00-02, REV 40. CONFIRMED AFFECTED AREAS CRACK FREE REF NTM 51-00-04-910-801, PT 1 AND 51-00-06-910-801, PT 1, REV SDR R61A201305190474Spar · crackedWHILE PERFORMING A LECK CHECK ON A RT WING FUEL LEAK. MX DISCOVERED A CRACK. INSPECTION VERIFIED CRACK PRESENT WITH EDDY CURRENT FROM THE A3 HOLE AFT SPAR AT RIB 10. REPAIRED IAW ETD2013-170-009240, REV B. MAJOR REPAIRSDR QXEA2013051701017Spar · corrodedRIGHT WING L/E SPAR UPPER FLANGE HAS BARE METAL WITH POSSIBLE CORROSION FROM STA YW 42 TO 155. REMOVED CORROSION ON SPAR UPPER FLANGE IAW SRM 51-21-00-00-02, REV 12. VERIFIED AFFECTED AREA TO BE CRACK FREE REF NDTM PART 1 TASK 51-00-06-910-801, REV 9. MECHANISDR QXEA2013051701016Spar · corrodedRIGHT WING L/E SPAR LOWER FLANGE HAS BARE METAL WITH POSSIBLE CORROSION FROM STA YW 42 TO 155. REMOVED CORROSION ON SPAR LOWER FLANGE IAW SRM 51-21-00-00-02, REV 12. VERIFIED AFFECTED AREA TO BE CRACK FREE REF NDTM PART 1, TASK 51-00-06-910-801, REV 9. FOUND SDR QXEA2013051701015Spar · corrodedLEFT WING FRONT SPAR LOWER FLANGE HAS BARE METAL WITH POSSIBLE FRETTING CORROSION FROM STA YW 42 TO 155. REMOVED CORROSION IAW SRM 51-21-00-00-02, REV 12. MIN THICKNESS NOTED .199" REF NTM 51-00-04-910-801, PT 1, REV 9. VERIFIED AFFECTED TO BE CRACK FREE REFSDR QXEA2013051701014Spar · corrodedLEFT WING FRONT SPAR UPPER FLANGE HAS BARE METAL WITH POSSIBLE FRETTING CORROSION FROM STA YW 42 TO 155. REMOVED CORROSION IAW SRM 51-21-00-00-02, REV 12. VERIFIED AFFECTED AREAS TO BE CRACK FREE REF NDTM PART 6, TASK 51-00-01-250-801. MECHANICALLY MEASURED SDR C77A20130517001Spar · crackedCRACK DAMAGE WAS FOUND DURING THE ACCOMPLISHMENT OF SB 170-57-0038 ON THE LT SPAR III, FASTENER HOLE. THE PERMANENT REPAIR WAS ACCOMPLISHED BY SPOTFACING OUT THE CRACK DAMAGE THROUGH SPAR III, FABRICATING AND INSTALLING A REPAIR BUSHING IAW EO E17X-57MA-004.5SDR CA130530005Bolt · failed(CAN) BOLTS ON SPAR WEB SPLICE PIPER P/N 40624-00 INSPECTED. TWO LOWEST BOLTS ON SPLICE ASSEMBLY BROKE WHEN TIGHTENED. BOLTS REPLACED. (TC# 20130530005)SDR CA130528006Spar · cracked(CAN) SEVERAL SMALL CRACKS (<1/2") AND ONE LARGE (1.5" APPROX) CRACK FOUND IN MAIN SPAR WEB. CRACKS ORIGINATE FROM RIVETS IN SPAR WEB AND SOME EXTEND TO BEHIND LOWER SPAR CAP. TWO BOLTS IN SPAR WEB JOINT FOUND SHEARED. AIRCRAFT REMOVED FROM SERVICE. OTHER AISDR AALA20130514007Spar · crackedRIGHT WING SPAR CRACKED AT OUTBOARD FLAP HINGE, LOWER INBOARD HOLE AT WING STATION XRS 164. ACCOMPLISHED REAR SPAR REPAIR PER EA MD80-57029767 AND BOEING DWG J060165.SDR REXA2013051100803Rib · damagedLEFT WING L/E WS (SS 15.50) RIB DAMAGED (BIRD STRIKE). REMOVED AND REPLACED RIB PER SRM 51-42-06.SDR C77A20130505017Spar · crackedRT WING STUB IN SPAR III FASTNER HOLE SHOWS CRACK INDICATIONS. HOLE DIA IS AT 0.314". REAMED SPAR III AND FITTING TO 0.350" SRM PART II 51-40-02, CRACK INDICATION STILL EXISTS. SPOT FACED SPAR III MATERIAL AT 0.500" NDT AND INSTALLED BUSHING.SDR GLBA2013042500234Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT WING AT BL 29.06 AND SPAR, INBD RIB ANGLE (FLANGE) AT WING SPAR, .75" IN LENGTH. REPAIRED IAW EO 13-1900-57-010. MAJOR REPAIR.SDR CA130422007Spar · corroded(CAN) LOCALIZED CORROSION FOUND DURING INSPECTION, EXFOLIATION OF FWD FACE UPPER REAR SPAR, BOOM, ANGLE.SDR FXGA201304221321Spar Cap · corrodedCORROSION ON LOWER CTR SPAR CAP AT RWS 177, REMOVED CORROSION. PERFORMED VISUAL & HFEC INSPECTIONS, NO CORROSION DETECTED. FOUND WITHIN LIMITS IAW TO 1C-118A-3-1 APPENDIX III FIGURE C-2. TREATED & PRIMED AREA FOR CORROSION PROTECTION. APPLIED SEALANT FOR AESDR FFFR201304240001Bolt · corrodedWHILE REMOVING RT WING FOR REPLACEMENT OF THE WING WALK SKIN FOR CRACKING OF A PREVIOUS REPAIR THE OTBD MAIN SPAR UPPER ATTACH BOLTS WERE FOUND TO BE CORRODED. ALL BOLTS WERE REPLACED USING NEW PN BOLTS LISTED IN THE CURRENT IPC. THE MM DID NOT INDICATE THE PSDR FDEA201304150783Spar · corrodedIAW EO F-2822-7-5009 PART 3, STEP B1. C (PAGE 16 OF 33). CORROSION AT RT AFT WING SPAR SURFACE. REMOVED AND SPAR WEB THICKNESS FOUND LESS THAN THE MINIMUM. IAW EO F-2822-7-5009, PART 3, STEP B1. C (PAGE 16 OF 33). CORROSION AT RT AFT WING SPAR SURFACE REMOVSDR SWIA201333402Spar Cap · crackedCRACKED FWD UPPER SPAR CAP AT RIGHT I/B LEADING EDGE BY NACELLE. (C-CHECK) INSTALLED DOUBLER AT RIGHT I/B LEADING EDGE SPAR CAP IAW ETD.SDR CA130422012Spar · damaged(CAN) ON A ROUTINE NDT WING FITTING INSPECTION (AS PER THE SIRM), IT WAS FOUND THAT THE FASTENERS THAT HOLD THE FITTING ON THE SPAR HAD WORKED LOOSE AND HAD BEEN "SMOKING". IN ORDER TOO INVESTIGATE FURTHER, THE WINGS HAD TO BE REMOVED AS WELL AS THE WING END RSDR QXEA2013040400758Spar · corrodedRT WING FRONT SPAR LOWER FLANGE HAS BARE METAL AND FRETTING CORROSION FROM STA YW 42 TO YW 155. REMOVED FRETTING CORROSION AND CLEANED BARE METAL AREAS FROM ST YW42 TO YW155 IAW Q400 SRM 51-21-00-00-02 REV 12 AND Q400 SRM 51-26-00-02-01 REV 12. MIN THICKNESS NSDR QXEA2013040400757Spar · corrodedRIGHT WING FRONT SPAR TOP FLANGE HAS BARE METAL AND FRETTING CORROSION FROM STA YW 42 TO YW 155. REMOVED FRETTING CORROSION AND CLEANED BARE METAL AREAS FROM ST YW42 TO YW155 IAW SRM 51-21-00-00-02, REV 12 AND SRM 51-26-00-02-01, REV 12. MIN THICKNESS NOTED .SDR QXEA2013040400756Spar · corrodedLEFT WING FRONT SPAR LOWER FLANGE HAS BARE METAL AND FRETTING CORROSION FROM STA YW42 TO YW 155. REMOVED CORROSION LT WING FRON SPAR LOWER FLANGE IAW SRM 51-21-00-00-02, REV 12 MIN THICKNESS NOTED .199" CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-SDR QXEA2013040400755Spar · corrodedLEFT WING FRONT SPAR TOP FLANGE HAS BARE METAL AND FRETTING CORROSION FROM STA YW42 TO YW 155. REMOVED CORROSION LT WING FRONT SPAR TOP FLANGE IAW SRM 51-21-00-00-02 REV 12 MIN THICKNESS NOTED .189", CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801SDR SWAA2013042415088Angle · crackedRIGHT WING FRONT SPAR ANGLE CRACKED AT WBL 71.24. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
Back to JASC 5711