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 2023FA0000119Wing · corrodedEXFOLIATION FOUND IN FOUR LOCATIONS ALONG THE REAR AFT SPAR OF THE LH & RH MLG. REQUIRES HI-LOK REMOVAL, CORROSION REMOVAL AND MAPPINGSDR FDEA202303080646Spoiler · delaminatedLH WING #6 SPOILER L/E CTR SECTION DELAMINATED. REMOVED L6 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L6 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, PAGE.211-213, FIG.206. "MAJOR REPAIR"SDR FDEA202303080626Skin · delaminatedLH WING #6 SPOILER L/E CTR SECTION DELAMINATED REMOVED L6 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L6 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, PAGE.211-213, FIG.206. "MAJOR REPAIR"SDR A6WA202303088527Unknown · dentedRH WING LEADING EDGE PANEL P/N 601R12016-6 HAS DENTS MEASURES P1 L= 2.100 X W= 1.300Ï¿½ P2 L= 2.500 X W= 1.500Ï¿½ P3 L= 2.400 X W= 1.650Ï¿½ P4 L= 2.100 X W= 0.500Ï¿½ ON LE INBOARD SECTION BETWEEN WS96.134-WS131.800 . *******AIRCRAFT REMOVED FROM SERVICE*****SDR UIEA2023031000241None · noneGOUGE - SKIN, RH WING INBD AILERON NOSE LE, WBL 502.5 - 514.25(<P>1. PERFORM REPAIR OF GOUGE DAMAGE FOUND ON RH WING INBD AILERON NOSE LE, WBL 502.5 - 514.25. PLEASE REFER TO THE JOB CARD ATTACHING SHEETS FOR DETAILED REWORKING INFORMATION. 2. CONDITION CHECK SDR UIEA2023031000240None · noneDISBOND - SKIN, #5 SPOILER UPPER SURFACE T/E FOUND DISBOND(<P>1. CUT OUT THE DISBOND AND CLEAN MEASURE THE CUTOUT (L = 5.5", W = 3", 32.5" FROM OUTBD EDGE AT T/E) INSTALL THE REPAIR CORE WITH COMPOUND, CURED AT 250 DEGREE FAHRENHEIT FOR 90 MINUTES WITH MINIMUMSDR FDEA202303070644Spoiler · delaminated1EA DELAMINATION WAS FOUND (2" X 1") AT LH SPOILER NO.5 UPPER SKIN. REMOVED L5 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L5 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, P.211~213, FIG.206. SDR FDEA202303070625Skin · delaminated1EA DELAMINATION WAS FOUND (2" X 1") AT LH SPOILER NO.5 UPPER SKIN REMOVED L5 SPLR, REPAIRED THE DELAMINATION AREA, REINSTALLED, ADJUSTED, AND PFMED TEST OF L5 SPLR IAW A300-600 AMM 27-61-53-04 AND A300-600F SRM 57-72-11-201, PARA.12, P.211~213, FIG.206. SDR SWAA2023041112744Panel · crackedCRACK ACCESS PANEL 661BB ON HOLES AT RT WING 2023-180655<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; DUE DATE: 20-DEC-23.;[02] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18175478; DUE DATE: 24/SEP/23;[03] TOOL USED SCALE PN: SPX621; SN: 8340225441;SDR SWAA2023041112745Panel · crackedCRACK ACCESS PANEL 621FB AT RT WING 2023-180659<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; DUE DATE: 20-DEC-23.;[02] TOOL USED: HOTBONDER: P/N:HCS9200B-AV S/N:18175478 DUE DATE:24-SEP-23;[03] TOOL USED SCALE PN: SPX621; SN: 8340225441; DUE DATE: SDR SWAA2023041112746Panel · crackedCRACK ACCESS PANEL 561BB ON HOLES AT LT WING 2023-180653<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; DUE DATE: 20-DEC-23.;[02] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18175478; DUE DATE: 24/SEP/23;[03] TOOL USED SCALE PN: SPX621; SN: 8340225441;SDR IPXA2023031591848Skin · unknownINSPECTION TYPE:C6*MAJOR REPAIR* FUSELAGE DRAIN HOLES ADDITION AND INSPECTION AFT OF STA 1725.5 BETWEEN S-36L AND S-36R.PERFORM UPS EO B767-2740-82173-C APPX B.SDR UIEA2023030200197None · noneRH WING, SPOILER #9, TRAILING EDGE LOWER SURFACE (OUTBOARD CORNER), CLOSE TO WSTA 616.2.(<P>IT WAS REPAIRED PER SRM 57-70-01-2R-1 AND SRM 51-70-04-0G-0.</P>)SDR CALA2023030300596Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 54.60 IS CRACKED SUPPORT TASK NSA EMX NR 00130 AND HANGER NR 7000935. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 54.60 /R 7000935 WORK ACCOMPLISHED BY V905004 AND INSPECTED BY V912634 IAW BAC DSDR CALA2023030300595Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX N/R 00129 AND HANGER N/R 7000924. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 /R 7000924 WORK ACCOMPLISHED BY V937791 AND INSPECTED BY V912634 IAW BAC SDR SWAA2023040511524Angle · corrodedCORROSION FUEL BOOST PUMP ANGLE LOCATED IRSS145 AFT POSITION AT LT WING 2023-142943<[01] REPLACED FUEL BOOST PUMP ANGLE LOCATED IRSS145 AFT POSITION AT LT WING IAW B737-700 SRM 51-10-02-0G-0<BR>SEE INDIVIDUAL SIGNOFF STEP BELOW;[02] TASK COMPLETED<BR><BR>SEE ISDR UIEA2023021500118None · noneRHW L/E OLES 1520 LWR FIXED PNL SUPPORT CHANNEL FOUND CORROSION.(<P>RHW L/E OLES 1520 TO OLES 15835 LWR FIXED PNL SUPPORT CHANNEL P/N: 65B11862-30 CORROSION DAMAGE AREA REPAIRED IAW RI-57-00-16071 REV.A</P>)SDR UIEA2023022200170None · noneRH O/B FORE FLAP FOUND DELAMINATION (50" TO O/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023022200171None · noneRH O/B MID FLAP NO.9 REAR SPAR SUPPORT LINK FASTENER HOLE ELONGATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5K</P>)SDR UIEA2023022200172None · noneRH O/B MID FLAP NO.6 REAR SPAR SUPPORT LINK FASTENER HOLE ELONGATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5K</P>)SDR UIEA2023022300191None · noneRHW - O/B AFT FLAP O/B UPPER ACCESS PANEL FOUND DEEP CHAFING MARK ABOVE AN OLD REPAIR(<P>PERFORMED METAL TO METAL HOTBOND REPAIR AS PER SRM 51 - 70 - 10 REPAIR 2</P>)SDR UIEA2023022300190None · noneRHW - O/B AFT FLAP O/B UPPER ACCESS PANEL FOUND DEEP CHAFING MARK(<P>PERFORMED METAL TO METAL HOTBOND REPAIR AS PER SRM 51 - 70 - 10 REPAIR 4</P>)SDR UIEA2023022300189None · noneRHW - O/B AFT FLAP O/B UPPER ACCESS PANEL EXISTING REPAIR DOUBLER HAS A DEEP CHAFING MARK(<P>PERFORMED METAL TO METAL HOTBOND REPAIR AS PER SRM 51 - 70 - 10 REPAIR 4</P>)SDR UIEA2023022200169None · noneLHW - AFT I/B FLAP O/B UPPER ACCESS PNL HAS CHAFING MARK.(<P>PERFORMED METAL TO METAL HOTBOND REPAIR AS PER SRM 51 - 70 - 10 REPAIR 2</P>)SDR UIEA2023022200168None · noneLHW - AFT I/B FLAP O/B SECTION LOWER SURFACE HAS A DENT MARK(<P>PERFORMED METAL TO METAL HOTBOND REPAIR AS PER SRM 51 - 70 - 10 REPAIR 2</P>)SDR UIEA2023022200167None · noneRHW O/B FORE FLAP O/B TOP PNL FOUND 1EA DENT(<P>PERFORMED METAL TO METAL HOTBOND REPAIR AS PER SRM 51 - 70 - 10 REPAIR 2</P>)SDR UIEA2023022200166None · noneRHW O/B FORE FLAP I/B TOP PNL NEAR I/B EDGE AREA FOUND PUNCTURED(<P>PERFORMED METAL TO METAL HOTBOND REPAIR AS PER SRM 51 - 70 - 10 REPAIR 4</P>)SDR UIEA2023022100163None · noneRHW - I/B FORE FLAP UPPER SURFACE FOUND DELAM (APPROX 140" FROM I/B AND 16"FROM T/E)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023022100158Shear Tie · noneRH STA 1000 FRONT SPAR SHEAR TIE RBL 33.99" 1EA CRACK WAS FOUND APPROX 1.5".(<P>CRACK SHEAR TIE REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO 4453C024 PART 8 AND RI NO. RI-53-43-16092 REV.A</P>)SDR UIEA2023022100151None · noneRHW - I/B T/E MID FLAP L/E FIXED FAIRING AT MID EXTERIOR SURFACE FOUND DELAM(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023022100150None · noneLHW - I/B FORE FLAP L/E FOUND DELAMINATION 128" APPROX FROM O/B EDGE(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023022100149None · noneLHW O/B T/E MID FLAP L/E FAIRING EXTERIOR SURFACE AT MID AREA DELAMINATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023022100148None · noneRHW - I/B FORE FLAP UPPER SURFACE FOUND DELAM (APPROX 50" FROM I/B 16" FROM T/E )(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023022100147None · noneRHW - O/B MID FLAP O/B SECTION UPPER FIXED PNL SUPPORT BRACKET ATT SCREW HOLE ELONGATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023021600122Shear Tie · noneLH STA 1000 FRONT SPAR SHEAR TIE LBL 57.5 1EA CRACK WAS FOUND APPROX 1.5".(<P>CRACK SHEAR TIE REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO: 4453C024 PART 5.</P>)SDR CALA2023030100576Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX N/R 00129 AND HANGER N/R 7000924.SDR CALA2023030100575Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 54.60 IS CRACKED SUPPORT TASK NSA EMX NR 00130 AND HANGER NR 7000935.SDR VNAA202302040024Access Panel · corrodedCORROSION ON ACCESS PANEL 622DZ, 542AZ, 642AZ, 542BZ AND 642BZSDR AALA202303025067Strut · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE FLAP INTERCONNECTING STRUT. MAINTENANCE REPLACED INTERCONNECTING STRUT PER TASK CARD 26C57057001.SDR AALA202303029418Strut · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE FLAP INTERCONNECTING STRUT. MAINTENANCE REPLACED INTERCONNECTING STRUT PER TASK CARD 26C67057001.SDR EE4Y2023022417281Skin Panel · corrodedDURING THE ACCOMPLISHMENT OF ALLEGIANT ZL-500-03-1-002_P1-OP-UP/0 EWIS TASK, IT WAS FOUND THE RH WING, EXTERNAL TOP SKIN PANEL 2 AT THE REAR SPAR BETWEEN RIB 4 AND RIB 5 SKIN WITH CORROSION.
DUE TO THERE IS NOT SRM AVAILABLE TO PERFORM PERMANENT REPAIR, AIRBSDR EE4Y2023022417276Skin Panel · corrodedDURING THE ACCOMPLISHMENT OF ALLEGIANT ZL-500-03-1-002_P1-OP-UP/0 EWIS TASK, IT WAS FOUND THE RH WING, EXTERNAL TOP SKIN PANEL 2 AT THE STG 15RH BETWEEN RIB 11 AND RIB 12 SKIN WITH CORROSION.
DUE TO THERE IS NOT SRM AVAILABLE TO PERFORM PERMANENT REPAIR, AIRSDR EE4Y2023022417275Skin Panel · corrodedDURING THE ACCOMPLISHMENT OF ALLEGIANT ZL-500-03-1-002_P1-OP-UP/0 EWIS TASK, IT WAS FOUND THE RH WING, EXTERNAL TOP SKIN PANEL 2, AT STG 16RH BETWEEN RIB 14 AND RIB 16 SKIN WITH CORROSION.
DUE TO THERE IS NOT SRM AVAILABLE TO PERFORM PERMANENT REPAIR, AIRBUSSDR EE4Y2023022417274Skin Panel · corrodedDURING THE ACCOMPLISHMENT OF ALLEGIANT ZL-500-03-1-002_P1-OP-UP/0 EWIS TASK, IT WAS FOUND THE RH WING, EXTERNAL TOP SKIN PANEL 2, AT THE STG 14RH BETWEEN RIB 12 AND RIB 13 SKIN WITH CORROSION.
DUE TO THERE IS NOT SRM AVAILABLE TO PERFORM PERMANENT REPAIR, AISDR EE4Y2023022417273Skin Panel · corrodedDURING THE ACCOMPLISHMENT OF ALLEGIANT ZL-500-03-1-002_P1-OP-UP/0 EWIS TASK, IT WAS FOUND THE RH WING, EXTERNAL TOP SKIN PANEL 2 AT THE STG 15RH BETWEEN RIB 11 AND RIB 12 SKIN WITH CORROSION.
DUE TO THERE IS NOT SRM AVAILABLE TO PERFORM PERMANENT REPAIR, AIRSDR EE4Y2023022417272Skin Panel · corrodedDURING THE ACCOMPLISHMENT OF ALLEGIANT ZL-500-03-1-002_P1-OP-UP/0 EWIS TASK, IT WAS FOUND THE RH WING, EXTERNAL TOP SKIN PANEL 2 AT THE STG 16RH BETWEEN RIB 11 AND RIB 12 SKIN WITH CORROSION.
DUE TO THERE IS NOT SRM AVAILABLE TO PERFORM PERMANENT REPAIR, AIRSDR EE4Y2023022417271Skin Panel · corrodedDURING THE ACCOMPLISHMENT OF ALLEGIANT ZL-500-03-1-002_P1-OP-UP/0 EWIS TASK, IT WAS FOUND THE RH WING, EXTERNAL TOP SKIN PANEL 2 FROM AT THE STG 14RH BETWEEN RIB 10 AND RIB 11 SKIN WITH CORROSION.
DUE TO THERE IS NOT SRM AVAILABLE TO PERFORM PERMANENT REPAIRSDR EE4Y2023022417266Skin Panel · corroded•DURING THE ACCOMPLISHMENT OF ALLEGIANT ZL-500-03-1-002_P1-OP-UP/0 EWIS TASK, IT WAS FOUND THE LH WING, EXTERNAL TOP SKIN PANEL 2 FROM BETWEEN RIB 24 AND RIB 25 ON TRAILING EDGE OVERHANG SKIN WITH CORROSION. DUE THIS CONDITION WAS REPORTED TO AIRBUS.
•AIRBUSDR EE4Y2023022417267Skin Panel · corrodedDURING THE ACCOMPLISHMENT OF ALLEGIANT ZL-500-03-1-002_P1-OP-UP/0 EWIS TASK, IT WAS FOUND THE LH WING, EXTERNAL TOP SKIN PANEL 2 FROM BETWEEN RIB 25 AND RIB 26 ON TRAILING EDGE OVERHANG SKIN WITH CORROSION. DUE THIS CONDITION WAS REPORTED TO AIRBUS.
AIRBUS PSDR EE4Y2023022417268Skin Panel · corrodedDURING THE ACCOMPLISHMENT OF ALLEGIANT ZL-500-03-1-002_P1-OP-UP/0 EWIS TASK, IT WAS FOUND THE LH WING, EXTERNAL TOP SKIN PANEL 2 FROM BETWEEN RIB 18 + 270MM ON FRONT SPAR SKIN WITH CORROSION. DUE THIS CONDITION WAS REPORTED TO AIRBUS.
AIRBUS PROVIDED REPAIR
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