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 UIEA2022091200956None · noneLHW-L/H O/B MID FLAP L/E FOUND DELAMINATION (96" APPROX TO EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091200957None · noneLHW-L/H O/B AFT FLAP L/E FOUND DELAMINATION (96" APPROX TO I/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091200958None · noneLHW I/B AFT FLAP LOWER SURFACE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091200959None · noneLHW-LH O/B FORE FLAP L/E FOUND DELAMINATION (103" TO O/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091200960None · noneLHW-LH O/B FORE FLAP L/E FOUND DELAMINATION (40" TO O/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091200961None · noneLHW-LH O/B FORE FLAP L/E FOUND DELAMINATION (153" TO O/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091200962None · noneLHW-LH O/B FORE FLAP L/E FOUND DELAMINATION (56" TO O/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091200963None · noneLHW-LH O/B FORE FLAP L/E FOUND DELAMINATION (71" TO O/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091200964None · noneLHW-LH O/B FORE FLAP L/E FOUND DELAMINATION (108" TO I/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091300965None · noneLHW-LH O/B FORE FLAP L/E FOUND DELAMINATION (62" TO I/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091300966None · noneLHW-LH O/B FORE FLAP L/E FOUND DELAMINATION (36" TO I/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091300967None · noneLHW-LH O/B FORE FLAP L/E FOUND DELAMINATION (10" TO O/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091300968None · noneRHW L/E LOWER FIX PNL OLES 1380-1390 SUPPORT BEAM FOUND CORROSION(<P>RHW L/E LOWER FIX PNL OLES 1380-1390 SUPPORT BEAM CORROSION AREA REMOVED REPROTECTED IAW SRM 51-10-02 AND 51-20-01 CHECKED WITHIN SRM 57-41-13-1A-1 ADL 1 FIG 101 LIMIT</P>)SDR UIEA2022091300969None · noneLHW L/E LOWER FIX PNL OLES 1560 FOUND BULGE UP CORROSION(<P>LHW L/E LOWER FIX PNL OLES 1560 FOUND BULGE UP CORROSION AREA REMOVED REPROTECTED IAW SRM 51-10-02 AND 51-20-01 CHECKED WITHIN SRM 57-41-13-1A-1 ADL 1 FIG 101 LIMIT</P>)SDR UIEA2022091300970None · noneRH I/B AILERON UPPER SURFACE O/B AFT CORNER FOUND DELAM(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-06 PAR5G</P>)SDR UIEA2022091400971None · noneLHW L/E CAVITY OLES 1315 SKIN AT FORWARD OF FRONT SPAR FOUND CORROSION(<P>LHW L/E CAVITY OLES 1315 WING INTERSPAR UPPER SKIN CORROSION AREA REMOVED REPROTECTED IAW SRM 51-10-02 AND 51-20-01 CHECKED WITHIN SRM 57-20-01-1A-1 ADL 1 FIG 101 CHART II LIMIT</P>)SDR UIEA2022091400972None · noneLHW L/E UPPER FIX PNL OLES 1280 AT AFT STRAP FOUND BULGE UP CORROSION(<P>LHW L/E UPPER FIX PNL OLES 1280 AT AFT STRAP FOUND BULGE UP CORROSION AREA REMOVED REPROTECTED IAW SRM 51-10-02 AND 51-20-01 CHECKED WITHIN SRM 57-20-01-1A-1 ADL 1 FIG 101 CHART II LIMIT<SDR UIEA2022091400973None · noneRHW - O/B MID FLAP CENTRE L/E PANEL FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091400974None · noneRHW - O/B MID FLAP I/B L/E PANEL FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091400975None · noneRHW - O/B FORE FLAP L/E FAIRING FOUND DELAMINATION (153" FROM I/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091400976None · noneRHW - O/B FORE FLAP L/E FAIRING FOUND DELAMINATION (42" FROM I/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091400977None · noneRHW - O/B FORE FLAP L/E FAIRING FOUND DELAMINATION (154" FROM O/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091400978None · noneRHW - I/B FORE FLAP L/E FAIRING FOUND DELAMINATION (4" AND 15" FROM O/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091400979None · noneRHW - I/B FORE FLAP L/E FAIRING FOUND DELAMINATION (140" FROM O/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091400980None · noneRHW - I/B FORE FLAP L/E FAIRING FOUND DELAMINATION (46" FROM O/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091400981None · noneRHW - I/B FORE FLAP L/E FAIRING FOUND DELAMINATION (63" FROM O/B)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5A </P>)SDR UIEA2022091600984None · noneRHW L/E #25 VC FLAP CAVITY OLES 1440 LOWER FIX PNL SUPPORT BEAM FOUND CORROSION(<P>RHW L/E OLES 1440 PANEL SUPPORT BEAM P/N: 65D11862-30 CORROSION AREA REPAIRED IAW RI-57-41-15873 REV.A</P>)SDR UIEA2022091900992None · noneRH WING INBOARDS TRAILING EDGE FLAP HAS DENT LOCATED 25" (APROX) FROM AFT EDGE OF FLAP(<P>PERFORMED METAL HOTBOND REPAIR AS PER SRM51-70-10 REPAIR 2 AND F203</P>)SDR REXA2022110302412Hinge · damagedFOUND HINGE #2 AILERON WING FITTING NOMINAL OUTBOARD LUG TO BE DAMAGED. REPAIRED LEFT AILERON #2 WING HINGE FITTING IAW MHIRJ REO 690-57-51-276SDR WX0A1900010074283None · noneNRC 6000-0020: R/H WING FUEL TANK ACCESS PANEL 640HB CUTOUT HAS PITTING AROUND 6 HOLES./R/H WING FUEL TANK ACCESS PANEL 640HB CUTOUT, CORROSION REMOVED AROUND 6 HOLES AS PER SRM 51-74-00 REV 142 AND FOUND OUT OF LIMITS AS PER SRM 57-21-11-283-003 REV 142. DAMSDR REXA2022093002159Hinge Fitting · damagedFOUND HINGE #3 FITTING INBOARD AND OUTBOARD LUGS TO BE DAMAGED. REPAIRED RH WING AILERON HINGE FITTING NO.3SDR R61A2022102300665Wing · crackedCRACK LOWER SKIN ON RH WING RIB 4 AS MARKED. REPAIRED CRACK ON LOWER SKIN ON RH WING RIB 4 AS MARKED. REF ETD2022-170-029954. SEE
WIPS AND TASKS FOR WORK PERFORMED.SDR CALA2022092302439None · nonePANEL 511MB, 511NB, 511LB, 511KB, 511FB, 511DB, 611KB, 511AB, 611AB, 611FB, 511GB, 511EB, 611NB, 611MB, 611EB, 611DB, 511PB, 511QB, 611GB, NEEDS ALUMINUM FOILTAPE REPAIR IAW AMM TASK 51-27-01-340-801. IN COMPLIANCE WITH SRM 51-70-14-2R-3 AND RII. CLEAR TO INSTSDR CALA2022092302472None · noneLEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511AB CONDUCTIVE TAPE NEEDS REPAIR CLEARED TO APPLY CONDUCTIVE TAPE REPAIR IAW SRM 51-70-14-2R-3 INSPECTED PANEL TAPE AND INSTALLATION IAW SRM 51-70-14-2R-3.. STEP 6 CLEAR TO INSTALL. REMSDR IXXA2022092103None · wornFLAP COLLAR FITTING WORNSDR IXXA2022092101Skin · crackedLOWER LEFT WING SKIN CRACKEDSDR CALA2022091902420Slat · unserviceableTASKCARD 7678913 ACCOMPLISH UNITED EC/RA 5742-01111 REV E PART 3 PERMANENT REPAIR ON NUMBER 2 LEADING EDGE SLAT. REMOVED #2 LEADING EDGE SLAT, FOUND AND INSPECTED BY V895832. NO 2 SLAT TO BE UNSERVICEABLE IAW B737-800 SRM 57-42-01. NO 2 SLAT WILL BE REPLACED.SDR CALA2022091602388None · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 6.14 IS CRACKED SUPPORT TASK NSA EMX 00126 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 6.14 U354653, 09/13/2022. DATA TRANSCRIBED FROM NSA EMX N/R 00126 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A200SDR CALA2022091602387None · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 32.40 IS CRACKED SUPPORT TASK NSA EMX 00128 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 U354653, 09/13/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00128 IAW B737-800 SRM 51-40-02 AND BAC DWG 1SDR CALA2022091602386None · crackedB737-4-1262 SHEAR FITTING AT STA 540 AND LBL 54.60 IS CRACKED SUPPORT TASK NSA EMX 00129 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 54.60 U354653, 09/13/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00129 IAW B737-800 SRM 51-40-02 AND BAC DWG 111ASDR CALA2022091602385None · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 32.40 IS CRACKED SUPPORT TASK NSA EMX 00136 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 U354653, 09/13/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00136 IAW B737-800 SRM 51-40-02 AND BAC DWG 1SDR CALA2022091602384None · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 32.40 IS CRACKED SUPPORT TASK NSA EMX 00136 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 U354653, 09/13/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00136 IAW B737-800 SRM 51-40-02 AND BAC DWG 1SDR CALA2022091602383None · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 15.04 IS CRACKED SUPPORT TASK NSA EMX 00133 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 U354653 9/13/2022 DATA WAS TRANSCRIBED FROM NSA EMX N/R 00133 IAW B737-800 SRM 51-40-02 AND BA DWG 111A2SDR CALA2022091602382None · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 40.87 IS CRACKED SUPPORT TASK NSA EMX 00140 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 40.87 U354653, 09/13/2022. DATA WAS TRANSCRIBED FROM NSA EMX IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 RESDR CALA2022091602390None · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 54.60 IS CRACKED SUPPORT TASK NSA EMX 00141 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 ND RBL 54.60 U354653, 09/13/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000SDR CALA2022091602389None · crackedB737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 6.14 IS CRACKED SUPPORT TASK NSA EMX 00130 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 U354653, 09/13/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00130 IAW B737-800 SRM 51-40-02 AND BAC DWG 111SDR SWIA202266737None · crackedCOMPLY WITH: 170-57-0072 - WINGS - WING TIP - SPAR 1 REPLACEMENT REV 01 PART(S) 1, 2, 3, 4 (C-CHECK RO 11/4/2022) COMPLIED WITH: 170-57-0072 - WINGS - WING TIP - SPAR 1 REPLACEMENT REV 01 PART(S) 1, 2, 3, 4SDR R61A2022091900553Skin · crackedRH WING UPPER SKIN HAS 3 CRACKS OUTBD OF RIB 10, INBD OF # 3 SPOILER INBD HINGE AND AFT OF REAR SPAR FASTNER LINE ON TOP OF WING. REPAIRED IAW ETD2022-170-029017. ALSO REF VP-040130-2022 N/R 1&4 AND LP R1018658/1 & 3 FOR WORK PERFORMED.SDR SWIA202266595None · crackedL/H WING TIP SPAR 1 CRACKED, SB170-57-0072 ACCOMPLISHMENT REQUIRED IMMEDIATELY (C-CHECK RO 10/5/2022) / REMOVED AND REPLACED L/H WING TIP SPAR 1, REF SB170-57-0072 REFER TO CAMP # 25333256 FOR ALL WORK ACCOMPLISHEDSDR SWIA202266480None · damagedON PUSHBACK TUG PUSHED AIRCRAFT LEFT WING TIP INTO CART: DAMAGE TO THE LT WINGLET L/E SKIN, WINGLET T/E WEDGE, WINGLET LOWER FILLET FAIRING AND WINGLET OUTBD SKIN DUE TO IMPACT WITH THE CART / * THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M-337 IS R
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