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 = '5700' 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 = '5700' 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 SWIA202266460None · damagedFOUND DAMAGE TO THE LT WINGLET L/E SKIN (DWG CC670-15350 REF), WINGLET T/E WEDGE (DWG CC670-15309 REF), WINGLET LOWER FILLET FAIRING (DWG CC670-15305 REF), AND WINGLET OUTBD SKIN (DWG CC670-15114 REF), LHS, DUE TO IMPACT WITH THE CART. 1 SCRATCH:. 006€? MAX SDR CALA2022091402370Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 15.04 IS CRACKED SUPPORT TASK NSA EMX 00133SDR CALA2022091402369Fitting · crackedB737-4-1262 SHEAR FITTING AT STA 540 AND LBL 54.60 IS CRACKED SUPPORT TASK NSA EMX 00129SDR CALA2022091402368Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 15.04 IS CRACKED SUPPORT TASK NSA EMX 00127SDR CALA2022091402367Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 54.60 IS CRACKED SUPPORT TASK NSA EMX 00141SDR CALA2022091402366Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 32.40 IS CRACKED SUPPORT TASK NSA EMX 00128SDR CALA2022091402372Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 32.40 IS CRACKED SUPPORT TASK NSA EMX 00136SDR CALA2022091402371Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 6.14 IS CRACKED SUPPORT TASK NSA EMX 00130SDR CALA2022091402365Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 40.87 IS CRACKED SUPPORT TASK NSA EMX 00140SDR CALA2022091402364Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 6.14 IS CRACKED SUPPORT TASK NSA EMX 00126SDR COEA2022102508803Panel · corrodedWO 238881 NR 500023 HEAVY CHECK COE/MAJOR REPAIR: UPPER WING ACCESS DOOR CUTOUT FOR PANEL 522CT HAS FRETTING DAMAGE. CORRECTIVE ACTION: REPAIR PER ATR SRAS DO/TS-4828/10...6020 ISSUE F, DATED 10/20/2022.SDR COEA2022102507803Skin · corrodedWO 238881 NR 500022 HEAVY CHECK COE/MAJOR REPAIR: UPPER WING ACCESS DOOR CUTOUT FOR PANEL 521DT HAS FRETTING DAMAGE. CORRECTIVE ACTION: REPAIR PER ATR SRAS DO/TS-4828/10...6020 ISSUE F, DATED 10/20/2022.SDR SWIA202266467None · damagedTRANSFER FROM EAML 989654 : CATERING TRUCK BACKED INTO RIGHT SIDE WINGLET TRAILING EDGE (FLIGHT #3485 FILED CLOSED) PERFORMED PERMENANT REPAIR ON RH WINGLET TRAILING EDGE PER INSTRUCTIONS IN ETD 2022-170-028579. SEE CP 25484224-1 FOR RESTORATION OF ORIGINASDR UIEA2022082900916None · noneRH WLG W/W JETITION OVERRIDE PUMP ( M225 ) BONDING ATT POINT CORROSION(<P>CORROSION REOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 CHECKED WITHIN SRM 57-10-10 ALLOWABLE DAMAGE 2 FIG 101 LIMITS REV 95 20 JUN 2022</P>)SDR UIEA2022082900915None · noneLH WLG W/W JETITION OVERRIDE PUMP ( M224 ) BONDING ATT POINT CORROSION(<P>CORROSION REMOVE IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 CHECKED WITHIN SRM 57-00-00 ALLOWABLE DAMAGE 2 FIG 101 LIMITS REV 95 20 JUN 2022</P>)SDR UIEA2022081900877None · noneLHW I/B FORE FLAP UPPER SURFACE FOUND DENT(<P>PERFROMED REPAIR AT DENT AREA <SPAN>SRM 51-70-07 PAR.5A</SPAN></P>)SDR UIEA2022081700864None · noneRHW 2 EA HOLE FOUND CRACK AT RHW ILES 1014.95 AND 1048.25 RIB LAYER(<P>2EA RIBS CRACK HOLES REPAIRED AS PER RI NO : RI-57-41-15854 REV A</P>)SDR UIEA2022081700863None · noneRHW I/B FORE FLAP O/B UPPER SURFACE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.95 ,JUN20/2022</P>)SDR UIEA2022081000849None · noneRHW L/E OLES 1117 L/E D FAIRING LOWER SKIN SPLICE STRAP AND LOWER CHORD FOUND CRACKED.(<P>LOWER CHORD CRACK AREA REPAIRED AS PER RI NO : RI-57-41-15815 REV A</P>)SDR UIEA2022081000848None · noneRHW OLES 1202 L/E D FAIRING UPR CHORD CRACK(<P>CRACK AREA REPAIRED AS PER RI NO. RI-57-00-15825 REV A</P>)SDR UIEA2022081000847None · noneRHW OLES 1202 L/E D FAIRING AFT WEB CRACK(<P>CRACK AREA REPAIRED AS PER RI NO : RI-57-00-15825 REV A</P>)SDR UIEA2022081000846None · noneRHW ILES 1107 L/E D FAIRING ATT WEB UPR CHORD FOUND CRACKED(<P>CRACK AREA REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022081000845None · noneLHW ILES 1117 L/E 'D' FAIRING UPPER CHORD CRACK.(<P>CRACK AREA REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022080900844None · noneLHW ILES 1117 L/E 'D' FAIRING NOSE BEAM LWR CHORD CRACK(<P>LWR CHORD CRACK AREA REPAIRED AS PER RI NO : RI-57-41-15814 REV A</P>)SDR UIEA2022080900842None · noneRHW L/E ILES 1117 L/E 'D' FAIRING SKIN LOWER FASTENER HOLE ELONGATED(<P>L/E SKIN REPAIRED AS PER RI NO : RI-57-41-15852 REV A</P>)SDR UIEA2022080800834None · noneM/D STA 1140 RBL 30 - 33 WING CTR SECTION UPPER SKIN CORROSION(<P>SKIN CORROSION AREA REPAIRED AS PER RI NO : RI-57-00-15842 REV A</P>)SDR UIEA2022080200813None · noneLHW OB MID FLAP AFT UPPER SKIN FOUND 2EA SCREW HOLES ELONGATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5K</P>)SDR UIEA2022080200812None · noneLHW O/B T/E FORE FLAP L/E FAIRING AT MID EXTERIOR SURFACE DELAMINATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2022080200811None · noneRHW O/B T/E FORE FLAP L/E FAIRING AT MID EXTERIOR SURFACE DELAMINATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5C</P>)SDR UIEA2022090900945None · noneRH WING CENTER SECTION, LOWER SURFACE, SPLICE STRINGER L-6 AND BBL97.42 WITH LEAK FUEL(<P>FUEL LEAK WAS REPAIRED PER AMM 28-11-00-308-013 PARAGRAPH 2</P>)SDR UIEA2022090900947None · noneRH WING LOWER SURFACE, AT L-10 BETWEEN WS 284 AND WS 344 WITH FUEL LEAK(<P>FUEL LEAK WAS REPAIRED PER <SPAN> </SPAN><SPAN>AMM 28-11-00-308-013 PARAGRAPH 2</SPAN></P>)SDR UIEA2022090900948None · noneRH WING LOWER SURFACE, AT L-10 AND WS 486 WITH FUEL LEAK(<P>FUEL LEAK WAS REPAIRED PER AMM 28-11-00-308-013</P>)SDR SWIA202266805None · chafedRH WING PLANK AT REAR SPAR DATUM AND WS45.00 HAS CHAFING DAMAGE AS MARKED (C-CHECK RO 11/10/2022) REPAIRED CHAFE AT R/H WS45.00 AT REAR DATUM REF REO 601R-57-21-880 REV -D DATED 2017/03/06. CHECKS GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.SDR SWIA202266804None · chafedLH WING PLANK AT REAR SPAR DATUM AND WS45.00 HAS CHAFING DAMAGE AS MARKED (C-CHECK RO 11/10/2022) BLENDED CHAFING DAMAGE ON LH WING PLANK AT REAR SPAR DATUM & WS45.00 TO A SMOOTH CONTOUR. NOMINAL THICKNESS OF 0.300". REMAINING THICKNESS OF 0.283". MATSDR A6WA202209088333None · chafedR/H AILERON LOWER SHROUD L/E HAS WEAR DAMAGE AT WS 360. **************REMOVED AIRCRAFT FROM SERVICE************************* BLENDED DAMAGE AREA TO A SMOOTH CONTOUR WITH DIMENSIONS OF 2.0"L X 1.0"W X .037"D IAW ASAP EA #AWAC-CRJ257-01895 REV A DATED 09/30/2022SDR IXXA2022090701None · corrodedSEAL RETAINER CORRODEDSDR SWAA2022093050743Support Angle · brokenBROKEN SUPPORT ANGLE ON ACCES PANEL 551FB AT LT WING 2022-486098 /SDR IPXA2022092186472Support · crackedINSPECTION TYPE:3CR/H WING FIXED L/E SUPPORT STRUCTURE O/B END OF SLAT MECHANISM ACCESS DOOR IS CRACKED.REPLACED R/H FIXED L/E SUPPORT IAW SRM 51-35-01 (MINOR).SDR REXA2022110102348Panel · chafedRH AILERON ACCESS PANEL 699CB CHAFED. BLENDED CHAFE DIMENSIONS AS FOLLOWS 2.0" X .75" X .023" DEEP REMOVED AND REPLACED PANELSDR IXXA2022090103Slat · damaged#7 SLAT COMPOSITE DAMAGESDR JR2R20220831833Angle · crackedANGLE FWD OF LH MLG FWD BULKHEAD CRACKEDSDR SWIA202266439None · damagedREMOVED DAMAGED RIGHT WING WINGLET TRAILING EDGE RIB P/N 600-10381-20 LOCATED AT WS404.08 IN REFERENCE TO SRM 57-31-14. (FILED CLOSED) INSTALLED SERVICEABLE R/H WINGLET TRAILING EDGE RIB P/N 600-10381-20 LOCATED AT WS404.08 (ITEM #8 FIG1 SHEET 1 CRJ200 SRSDR UIEA2022082800910Fitting · delaminatedLHW O/B MID FLAP MID T/E LOWER SURFACE #7 AND #9 ARM FITTING (COUNT FROM O/B) FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5ASDR UIEA2022082400889Flap · delaminatedLHW O/B MID FLAP MID L/E FIXED PNL FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A</P>)SDR UIEA2022082400888Flap · delaminatedLHW O/B MID FLAP I/B L/E FIXED PNL FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A</P>)SDR UIEA2022082400887Flap · delaminatedLHW I/B AFT FLAP LOWER SURFACE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A</P>)SDR UIEA2022082400886Flap · delaminatedRHW I/B FORE FLAP O/B L/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A</P>)SDR UIEA2022082300885Flap · delaminatedRHW I/B FORE FLAP MID L/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A</P>)SDR UIEA2022082300884Flap · delaminatedRHW I/B AFT FLAP LOWER SURFACE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A</P>)SDR UIEA2022082300883Flap · delaminatedRHW O/B MID FLAP I/B L/E FOUND DELAMINATION(<P> PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR 5A</P>)
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