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 DHL2007803500Frame · crackedRT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA XFS 660.000. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED ANGLES (2EA) DOUBLERS AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. ISDR DHL2007803502Frame · crackedRT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA 622.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED TWO ANGLES DOUBLERS (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLES IAW SRM 51-1-8B. INSTALLED ANGSDR 2007FA0000482Spar · corrodedRT WING REMOVED DUE TO DAMAGE. WING WAS SCRAPPED AND DEALER WANTED STEEL FITTINGS REMOVED. UPON REMOVAL OF REAR SPAR ATTACH PLATE, SEVERE CORROSION WAS FOUND ON THE SPAR UNDER THE PLATE. CONDITION WAS VERY SERIOUS AND COULD HAVE LEAD TO AN INFLIGHT FAILURE.SDR 2007FA0000480Spar Cap · corrodedFUEL TANK REMOVED DUE TO LEAKING VENT LINES. UPON REMOVAL, DISCOVERED RT WING UPPER SPAR CAP SEVERLY CORRODED. MAJOR EXFOLIATION TO THE SPAR CAP AT THE OB SECTION OF THE FUEL TANK OPENING.SDR ABXA070196Support Bracket · crackedLEFT WING AFT SPAR HAD CRACKED VERTICAL SUPPORT BRACKET NEAR INBOARD SPOILER ACTUATOR. REPLACED BRACKET IAW DC9 SRM.SDR 07FDEA01846Frame · crackedRIGHT WING LEADING EDGE FORMER CRACKED AT XOS625.5 STOP DRILLED CRACK AND INSTALLED REPAIR CLIP PER MD/DC 10-10 SRM 57-20-00 FIG 1 VOL I . FUEL CONTROL PANEL WAS REMOVED. REINSTALLED AND OPS CHECKED TO FACILITATE REPAIR IN REF TO MD10-10 MM 28-00-00-5. OPS SDR 07FDEA01838Spar Cap · corrodedRT WING HAS CORROSION ON AFT UPPER SPAR CAP STA.XORS 718 TO733. REMOVED CORROSION IAW DC/MD SRM 51-21-01 VOLII AND FEDEX EA 8-5710-109151, WINGS, RT WING SPAR CORROSION BETWEEN STA XORS 480-733. REPAIR, ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOLII.SDR 07FDEA01821Spar Cap · corrodedRIGHT WING HAS CORROSION ON AFT UPPER SPAR CAP AT XORS=718 TO XORS=733 ENTERED IN ERROR, SEE SDR NR 07-1838 N/R N00804 FOR CORRECTIVE ACTION.SDR 2007FA0000463Spar · crackedDELAMINATION OCCURRING AT WING STRUT ATTACH LOCATION. CRACK AT BOTTOM EDGE AT ROOT FITTING. POSSIBLE AGE OF SPAR CAUSING DELAMINATION. LONGITUDINAL CRACK AT WING ROOT POSSIBLE EARLIER DAMAGE REPLACE WITH NEW WOOD SPAR (PN 5146L). (K)SDR 07FDEA01776Spar · corrodedRIGHT WING, REAR SPAR UPPER CAP AT ABOUT STA XORS 1044 FOUND WITH CORROSION REFER TO SNRM NO.: N00247 (SDR TRACKING NO.: 07-1605). COMPLIED WITH FEDEX EA NR 1-5710-109869, WINGS, RIGHT REAR SPAR UPPER CAP CORROSION COMMON TO STATIONS XORS = 1039 THROUGH XOSDR 2007FA0000417Spar · delaminatedDELAMINATION OCCURRING AT LT FRONT WING SPAR / STRUT LOCATION. CRACK AT BOTTOM EDGE, AT WING ROOT FITTING. POSSIBLE AGE OF SPAR CAUSING DELAMINATION. LONGITUDINAL CRACK AT WING ROOT POSSIBLE EARLIER DAMAGE. REPLACED WITH NEW WOOD SPAR P/N 5146L.SDR AMWA06033BSpar Cap · corrodedBIO - CORROSION DAMAGE RT LOWER SPAR CAP AT WS 124. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-7 REV 1R.SDR AMWA06033ASpar Cap · corrodedBIO - CORROSION RT LOWER SPAR CAP AT WS 124. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-7 REV 1R.SDR NWAA071779988Spar Cap · crackedDURING H-CHECK FOUND CRACK IN RIGHT WING AFT UPPER SPAR CAP AT STA XCWS 58.5. REPAIRED PER EA 99-208494.SDR 07FDEA01742Spar Cap · corrodedLEFT WING UPPER REAR SPAR CAP HAS CORROSION ON AFT UPPER SURFACE AT XORS 480-490. [SUP 05-16-07] REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW FEDEX E.A. 8-57-109150 STEP 2 (LT WING CORROSION BETWEEN XORS=480-800)ALODINED AND PRIMED DC10 SRM 51-21-01 VOL ISDR 07FDEA01741Spar Cap · corrodedLEFT WING REAR SPAR CAP HAS CORROSION MIGRATING UNDER WING SKIN AT ST XORS 600-606. [SUP 05-16-07] REMOVED CORROSION IAW DC10 SRM 51-21-01 VOLII ,ORIG THICKNESS .300 REMAINING .290 FOUND TO BE WITHIN LIMITS IAW 57-20-00 VOLII.REMOVED AND REPLACED FASTENSDR 07FDEA01740Spar Cap · corrodedLEFT WING UPPER SPAR CAP HAS CORROSION MIGRATING UNDER SKIN PLATE AT XORS 645-671. [SUP 05-16-07] REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW FEDEX E.A 8-5710-109150 STEP 3 (LT WING CORROSION BETWEEN XORS=412-800- REPAIR). ALODINED AND PRIMED IAW DCSDR UPS07549838Fitting · corrodedINSPECTION TYPE:SPV LEFT FWD TRUNNION BEARING LWR I/B ATTACH POINT, WHERE LWR I/B FUSE PIN IS, SPAR FITTING I/B FACE HAS CORROSION AROUND BUSHING HOLE. REPAIRED PER GOODRICH ER REPAIR O7-2294.SDR UPS07549837Fitting · corrodedINSPECTION TYPE:SPV LEFT FWD TRUNNION BEARING LWR OUTBOARD ATTACH POINT, WHERE LWR OUTBOARD FUSE PIN IS, SPAR FITTING OUTBOARD FACE HAS CORROSION AROUND BUSHING HOLE. REPAIRED PER GOODRICH ER REPAIR 07-2294.SDR 07FDEA01711Spar Cap · crackedRT WING UPPER SURFACE AT SPOILER PANEL NR 11 AREA SPAR CAP HAS CRACK AROUND 3RD HINGE FITTING. NDT NOTED NO CRACKED PER NTM 51-00-00 PT6 (AFTER STOP DRILL). STOP DRILLED 0.025" HOLE AT THE END OF CRACKED IAW SRM 57-30-4 FIG10 SHEET 1/3. TREATED AND PRIMED ISDR 07FDEA01710Spar Cap · corrodedRIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1042. [SUP 05-22-07] REPAIRED AS PER FEDEX EA 1-5710-111099.SDR SWIA200718442Shear Tie · crackedRIGHT WING IS LEAKING OUTBOARD OF NACELLE, DISCOVERED AT C-CHECK. REPLACED CRACKED SHEAR CLIP AT RIB NR 16 PER EMB SRM 51-40-02. NO LEAKS NOTED.SDR K11A2008112672206Attach Angle · crackedFEW SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK.SDR QXEA200700763Spar · chafedC4 PDX - RIGHT HAND WING INBOARD LOWER SPAR FLANGE CHAFED OUTBOARD EDGE. REPAIRED IAW SRM 51-21-00 AND RD8/4-57-796.SDR QXEA200700762Spar · chafedC4 PDX - RIGHT WING INBOARD LOWER SPAR FLANGE CHAFED INBOARD EDGE. REPAIRED IAW SRM 51-21-00 AND RD8/4-57-796.SDR S2YA07004Spar Cap · crackedON 04/29/07 DURING INSPECTION REQUIRED BY AD 2006-18-51 SKYWAY MAINTENANCE FOUND A CRACK ON RIGHT WING AFT SPAR, LOWER SPAR CAP AFT FLANGE AT WING STATION 117 INCHES. THE CRACK RAN FROM THE AFT EDGE TO A RIVET HOLE. THE DAMAGE WAS REPAIRED IAW RAYTHEON AIRCRSDR 2007FA0000858Spar · deterioratedREPORT IAW AD 200-25-02R1 PARAGRAPH D (4) LOOSE, MISSING AND RUSTED NAILS IN RIBS ALLOWING RUSTY MOISTURE INTO SPAR, FRETTING ON TOP CAP GREATER THAN .0625 INCH ON LOOSE RIBS, CRACKS AT AILERON BELLCRANK BRACKET, CAUSED FROM OVER TORQUING OF BOLTS, PREVIOUS WISDR 07FDEA01608Spar · corrodedLEFT WING, REAR SPAR UPPER CAP SURFACE AT ABOUT STA XORS 1046 FOUND WITH CORROSION. [SUP 05-14-07] REPAIRED AS PER FEDEX EA 1-5710-109868, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01607Spar · corrodedRIGHT WING, REAR SPAR LOWER CAP AT ABOUT STA XORS 1046-1050 FOUND WITH CORROSION. [SUP 05-14-07] REMOVED AS PER SRM 51-21-01 VOLUME II. MATERIAL REMOVED= 0.064", ORIGINAL THICKNESS= 0.108", REMAINING THICKNESS= 0.044", AND EXCEEDED LIMITS AS PER SRM 57SDR 07FDEA01605Spar · corrodedRIGHT WING, REAR SPAR UPPER CAP AT ABOUT STA XORS 1042 FOUND WITH CORROSION. [SUP 05-14-07] REMOVED AS PER SRM 57-21-01 VOLUME II. MATERIAL REMOVED =0.043" ORIGINAL THICKNESS =0.136", REMAINING THICKNESS =0.093" AND FOUND EXCEEDED LIMITS AS PER 57- 20SDR K11A2008112872215Attach Angle · crackedFWD SPAR ATTACH ANGLE CRACKED ( RT WING ).SDR K11A2008112872214Attach Angle · crackedFWD SPAR ATTACH ANGLE CRACKED ( RT WING).SDR K11A2008112872213Attach Angle · crackedFWD SPAR ATTACH ANGLE CRACKED ( RT WING ).SDR CPCP20070038Frame · corrodedAILERON CONTROL QUADRANT CORRODED RT FRAME 27 AND 28 WING RIB 1 AND 2. REPLACED QUADRANT ASSY ON AUTO-PILOT ROLL CONTROL SYSTEM IAW AMM JIC 27-11-23 RAI 10000.SDR SWAA072042Spar · crackedDURING SCHEDULED 22Y CHECK, FOUND RT WING AFT SPAR CASTING CRACKED AT STA 228. REMOVED AND REPLACED AFT SPAR CASTING PER SRM.SDR UPS07849763Bracket · crackedINSPECTION TYPE:C1 LOWER FRONT SPAR CAP BRACKET IS CRACKED IN 2 PLACES BETWEEN XRS 463-428 NR 1 ALT. REMOVED, FABRICATED AND INSTALLED BRACKET IN NR 1 ALT TANK IAW SRM 51-01-20D, 51-03-02, AND DWG 76335150001.SDR DHL2007806586Frame · crackedRT WING INBD L/E FORMER WITH CRACKS 1" AND 1.500" (MAJOR REPAIR) STA XCW 69.000. PERFORMED MAJOR REPAIR IAW SRM 57-3-3 FIG 1. REMOVED CRACKED FORMER IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED FORMER (AL7075"0" 0.090") IAW SRM 57-3-3 FIG 1, SRM 51-1-4. HESDR S9BA00407Spar Cap · corrodedFOUND CORROSION ON RT WING LOWER MAIN WING SPAR CAP BETWEEN STATION 35.2 AND STATION 74. REPAIRED IAW RD-57-24 AND INSTALLED SKIN PATCH IAW SRM 57-30-00 FROM STA 47 TO STATION 60.SDR K11A2008112872212Attach Angle · crackedFWD SPAR ATTACH ANGLE CRACKED. ( RT WING )SDR K11A2008112872211Attach Angle · crackedFWD SPAR ATTACH ANGLE CRACKED. ( RT WING )SDR K11A2008112872210Attach Angle · crackedFWD SPAR ATTACH ANGLE CRACKED. ( RT WING )SDR UPS07849791Spar Cap · crackedINSPECTION TYPE:C1 CRACK ON LWR CENTER SPAR CAP FLANGE NEAR XRS 172 NR 2 MAIN TANK. REPAIRED WING CENTER LWR CAP AND WEB AT STA XRS 168 NR 2 MAIN TANK IAW SAA EA 008-5710-01-A0808, UPS EO DC8-5710-26734-A, SRO8570015, AND FAA FORM 8100-9.SDR AWXA200700617Spar · crackedMCN - MAJOR REPAIR - LEFT WING REAR SPAR UPPER CHORD CRACKED, RSS 221. REPAIRED LEFT WING REAR SPAR UPPER CHORD, RSS 221 IAW AWA ER 03-5722-07128-SS1.SDR DHL2007743506Spar · crackedDISCOVERED WHILE IN "A" CHECK A/C 743DH AT MCO, THEN FERRIED TO VQQ REF ASTAR NR 078282 AND NR 078290. LT WING AFT FALSE SPAR ANGLE JUST FWD OF NR 7 SPOILER FITTING CRACKED IN ANGLE APPROX 2 1/2" LONG STARTING FROM INBD AND RUNNING BELOW FASTENERS. CUT OUT DSDR DHL2007806529Frame · brokenFOUND RT WING CTR L/E INTERIOR FORMER BROKEN STA XFS 510.222. REMOVED FASTENERS IAW SRM 51-1-20D. FABRICATED ANGLE DOUBLER (AL7075-0 0.063") IAW SRM 57-2-0 PG 9-10, SRM 57-3-3 FIG 4. HEAT TREATED ANGLE DOUBLER FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-1SDR EIA2007067Spar · corrodedRT WING FWD SPAR O/B LOWER CHORD CORRODED FROM 1467-1475. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER ECRA 479-57-218-2 REV A.SDR EIA2007065Spar · crackedRT WING FORWARD SPAR I/B LOWER CHORD CRACKED AT FSSO 1446 ON VERTICAL AND HORIZONTAL FLANGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 479-57-218-2 REV A.SDR 07FDEA01229Spar Cap · corrodedLT WING, REAR SPAR LOWER CAP UPPER SURFACE XORS 1050 FOUND WITH CORROSION. [SUP 4-20-07] COMPLIED WITH FEDEX EA 1-5710-109848. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA01222Spar Cap · damagedLT WING, REAR SPAR UPPER CAP XORS 680 HOLE FOUND ELONGATED. [SUP 4-20-07] COMPLIED WITH FEDEX E.A. 1-5710-109851 CLASSIFIED AS MAJOR. REPAIRED IAW FEDEX GMM 6-2-100.SDR AWXA200700431Spar · crackedMCN - LEFT WING REAR SPAR UPPER CHORD CRACKED, RSS 221. REPAIRED LEFT WING REAR SPAR UPPER CHORD, RSS 221 IAW AWA ER 03-5722-07086-SS4.
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