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 DHL2004803550Fitting · crackedLOWER AUX SPAR CAP, FITTING CRACKED 2.000 P/N 4778052-1 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, EA 5320-014, DWG 4778052. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. FABRICATED NEW FITTING (7075-T6 51) IAW EA 5320-014, DWG 4778052. SDR UPS04842539Spar · crackedINSPECTION TYPE:C-2, RIGHT WING FWD SPAR AT XFS 520.00 HAS 500 HOLE WITH CRACK INDICATED. REPAIRED RIGHT WING FWD IAW DWG J060232-532 CONF AND REO GO9802SDR CA040512005Spar · chafed(CAN) ON METAL-SPAR WINGS RETROFITTED TO THIS AC THE AFT SPARS HAVE THREE FOOT STIFFENERS RIVETED TO THEM AT AFT STRUT ATTACH POINT. CLEARANCE BETWEEN FABRIC AND STIFFENER IS MINIMAL, AND INSPECTION HOLE COVER CLIPS CAN CONTACT STIFFENER AND CHAFE GROOVES INTOSDR USAA040205Spar Cap · crackedSPAR CAP CRACKED (.2187 INCH CRACK) WBL 157 LT WING UPPER SKIN AT AFT SPAR.SDR 2004FA0000537Spar · crackedSPAR INSPECTED IAW 00-25-02R1. FOUND 2 CRACKS IN BUTT END, DOUBLER PLATES APPEAR TO BE LOOSENING. CRACKS ARE HORIZONTAL ACROSS THE END GRAIN.SDR AUS20040321Support Angle · cracked(AUS) WING SPAR STRAP SUPPORT FORWARD AND AFT ANGLES CRACKED ALONG RIVET LINE.SDR IXXA0400094SSpar · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND LT WING REAR SPAR DOUBLER UPPER SIDE HAS CRACK DAMAGE AT STA XCW 69.500. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS, ALONG WITH THE DAMAGED AREA IAW DC8 SRM 51-1-20D PG 21 AND DC8 SRM 57-2-6 FIG 15. FABRICATED FILSDR USAA040162Spar · crackedPIT - FOUND UPPER SPAR CRACKED .21875 INCH, RSS 222.5 REAR SPAR UPPER CHORD FITTING AT MLB BEAM. OVERSIZED FASTENER HOLE TO REMOVE CRACK AND INSTALLED FREEZE PLUG PER EA 78361. (M)SDR CA040430001Rib · corroded(CAN) DURING INSPECTION TO COMPLY WITH AD 2003-21-01 SEVERE CORROSION FOUND ON FORWARD END OF RIB, AFT OF REAR SPAR, IN THE RT CENTER SECTION, BETWEEN THE FUSELAGE AND WING. THE CORROSION WAS NOT READILY NOTICEABLE UNTIL INSTALLATION OF INSPECTION PANELS SK 80SDR UIEA200400063Spar · crackedFOUND LEFT WING UPPER MID SPAR WEB SURFACE FROM MSS 446.41 TO MSS 475.62 FOUND 2 CRACKS OF 5MM AND 16MM IN LENGTH REF TO NDT REPORT NR 276/03. CARRIED OUT HFEC INSPECTION ON THE CUTOUT SURFACE WEB AS PER NTM PART 6 51-00-00 FIG 4. NIL CRACK INDICATED. CRACKSDR 04FDEA01008Spar Cap · corrodedCOMPLY WITH FEDEX EA 8-5710-77344 WINGS BASIC LEFT WINGS, LOWER AFT SPAR CAP REPAIR. COMPLIED WITH EA 8-5710-77344 WINGS - BASIC LEFT WING, LOWER AFT SPAR CAP REPAIR.SDR 04FDEA001008Spar Cap · corrodedCOMPLY WITH FEDEX EA 8-5710-77344 WINGS BASIC LT WINGS, LOWER AFT SPAR CAP REPAIR. COMPLIED WITH EA 8-5710-77344 WINGS BASIC LT WING, LOWER AFT SPAR CAP REPAIR.SDR DL73G040309Spar · fatiguedTHE LEFT WING REAR SPAR CHORD WAS FOUND TO BE CRACKED AT APPROX RSS 223. THE SUBJECT HOLE IS COMMON TO THE MLG BEAM ATTACH FITTING. DAMAGE WAS REMOVED AND REWORKED PER ERA 386257-14.SDR SROM200400047Spar · elongatedDURING D CHECK RT WING UPPER SPAR AND SPAR WEB HAS ELONGATED HOLES. REAMED HOLES, TRIMMED UPPER FOOTPRINT IAW ASA EA 5720-01241 AND AAR EA 10336.SDR DHL2004740005Spar · damagedPER DER RECOMMENDATION, INSTALLED DOUBLER REPAIR'S AS REQ AT LWS 198, FWD SPAR, LOWER CHORD PLATE IAW AERONAUTICAL SOLUTIONS REPORT 04-004IK. FABRICATED REPAIR DOUBLER & TRIPLER, TREATED & PRIMED, AND INSTALLED PER AERONAUTICAL SOLUTIONS REPORT 04-004IR, DATESDR DHL2004740003Spar · corrodedSMALL AREA OF EXFOLIATION CORROSION AT FORWARD SPAR WING WELL STA 198 TO 210 LEFT-HAND WING. REMOVED CORROSION AT LEFT WING FORWARD LOWER CHORD. TREATED AND PRIMED PER B-727 SRM 51-10-6 & 51-10-2, MATERIAL REMOVED LESS THAN .080 CROSS SECTIONAL AREA REDUCED SDR UIA9311Spar · corrodedDURING C 05 CHECK OF DATUM A/C: FOUND CORROSION ON UPPER SURFACE OF FRONT SPAR OF RT WING AT STA XRS 531. FOUND CORROSION ON UPPER SURFACES OF LOWER SKIN P/N:5935822-50 AND REAR SPAR LOWER CAP OF RT WING AT STA XRS=546. PERMANENT REPAIR ON FUSELAGE SKIN P/SDR DHL2004803517Frame · crackedLT INNER WING CTR L/E FORMER CRACKED 0.250, XFS 427.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE ON CRACK END AND FABRICATED DOUBLER (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLEDSDR 04FDEA01859Spar Cap · crackedCRACK FOUND IN THE LT WING UPPER CAP AT RIB STATION XORS 402. THE CRACK IS ALL WAY THRU THE CAP AND IS LOCATED IMMEDIATELY FORWARD OF STRINGER 15. CRACKS ROUTED AND EXTRUDED REPAIR ANGLE INSTALLED IAW FEDEX EA 8-5710-75730 (REF FEDEX NRC N0625).SDR ABXA040123Spar Cap · crackedTOP SIDE OF CENTER WING BOX, STA 857, LEFT BUTT LINE 24, UPPER SPAR CAP HAD A 3 INCH CRACK. REPAIRED AREA IAW DC-8 SRM 51-1-24, 51-1-20D AND 31-3-1.SDR AUS20040202Spar · corroded(AUS) WING SPAR CORRODED. FOUND FOLLOWING REMOVAL OF FUEL TANK FOR STRUCTURAL DEFECT REPAIR. CORROSION WAS SEVERE ENOUGH TO HAVE COMPROMISED STRUCTURAL INTEGRITY.SDR DHL2004809004Spar · crackedLT MLG WHEEL WELL FUSELAGE STA 931 FALSE SPAR STA 1.50 THE UPPER END OF CHANNEL HAS A .375 INCH CRACK IN RADIUS OF VERT LONG. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. ENTER AS DMI 1604SDR 04FDEA00643Spar · damagedRIGHT WING - DURING ACCOMPLISHMENT OF OUTBOARD TRAILING EDGE FLAP INBOARD HINGE TENSION STRAP SUPPORT REPLACEMENT, FOUND 2 EACH EXISTING HOLES OVERSIZED. REPAIR CARRIED AT RIGHT WING 2 EA EXISTING OVERSIZED HOLES OF OUTBOARD TRAILING EDGE FLAP INBOARD HINGESDR UPS04442045Strap · corrodedINSPECTION TYPE: C, BS 1241 LEFT WING REAR SPAR LOWER SPLICE FOUND CORROSION AT HOLE -A- ALL LAYERS APPROX 12 O/C POSITION AND APPROX 0.030 INCH DEEP. CORROSION REMOVED AND BOLT HOLE FINAL OVERSIZE TO 0.907 INCH PER EO B747-5710-12138-G, HFEC INSPECTED RESULSDR UPS04442048Fitting · crackedINSPECTION TYPE:C LLEFT WING REAR SPAR LOWER KICK FITTING HOLE -C- FOUND CRACKED APPROX 0.040 INCH. LOWER KICK FITTING HOLE -C- OVERSIZED TO 1.000 INCH TO REMOVE CRACK. HFEC INSPECTED CONFIRM CRACK FREE. FASTENER HOLE BUSHING REPAIRED PER RS R-57-12-35122. SDR UPS04442047Fitting · crackedINSPECTION TYPE:C RIGHT WING REAR SPAR LOWER KICK FITTING HOLE -C- FOUND CRACKED APPROX 0.040 INCH. KICK FITTING HOLE -C- OVERSIZED TO 0.937 INCH TO REMOVE CRACK. HFEC INSPECTED CONFIRM CRACK FREE FASTENER HOLE BUSHING REPAIRED AND BOLT BACB30US14K45X INSTALSDR DHL2004750038Frame · crackedDURING -C- CHECK, LT WING L/E CAVITY WBL 92 INT FRAME STIFFENER 2ND FROM SPAR HAS UPPER END CRACKED. CUT OUT DAMAGED AREA AND FABRICATED FILLER FROM 2024 T3 .032 PO 900534 DIM 3.75 X 2.5 INCH REPAIR ANGLE FROM 7075 T3 040 PO 900226 DIM 7 X 3.5 INCH IAW B727 SSDR ABXA040099Spar · corrodedANGLE EXFOLIATED AND BULGED UPPER AFT FLANGE OF REAR SPAR UPPER TEE JUST OUTBOARD OF TRUNNION. REPLACED TEE ANGLE XRS 111.00 LEFT WING IAW DC-9 SRM.SDR UPS04442000Spar · corrodedINSPECTION TYPE:C BS 1241 WING REAR SPAR LEFT UPPER CHORD FOUND CORROSION AT HOLE NR 9 APPROX 0.030 INCH DEPTH. BS 1241 WING REAR SPAR LEFT UPPER CHORD BOLT HOLE NR 9 CORROSION REMOVED NDT INSPECTED RESULT CORROSION FREE. BOLT HOLE BUSHING REPAIRED AS PER ESDR CALA0400173Spar · crackedINSPECTION FOUND THE RT WING REAR SPAR UPPER CHORD CRACKED AT RSS 288. THE SPAR CHORD WAS REPAIRED IAW ECRA 5711-01055.SDR UIA9306Spar · corrodedDURING S90M CHECK OF DATUM A/C, FOUND CORROSION, UPPER SURFACE OF FRONT SPAR LOWER CHORD OF LT WING AT STA XRS 509.2. LT WING (STA. XRS 115-601) AND RT WING (STA. XRS 73-477) UPPER SKIN. T/E ALUMINUM STRIP OF RUDDER THAT HAD PENETRATED THROUGH THE ENTIRE THICSDR MALA040250Spar · gougedRIGHT O/B LEADING SPAR HAS GOUGES BETWEEN WS 2976 AND WS 3142. MX FABRICATED AND INSTALLED REPAIR ANGLE AND FILLERS IAW TIMCO REQ-L00725. A/C RELEASE DATE 3/8/2004.SDR UIA9305Spar Cap · corrodedDURING S90M CHECK FOUND TWO CORROSION SITES ON AFT EDGE OF RT WING UPPER SKIN AND TWO CORROSION NR 1-NR 4 ON LOWER P/N5935822-506 AND REAR SPAR CAP P/N 5911301-1 UPPER SURFACE OF RT WING NEAR STA XRS=546. PFM THE REPAIR TO CORROSION BLEADOUTS AND TEMPOARY RESDR AUS20040076Spar · debonded(AUS) LT WING SPAR WEB DISBONDED IN AREA LOCATED AT CWS 57.SDR AUS20040133Spar Cap · cracked(AUS) REAR WING SPAR BOTTOM SPAR CAP CRACKED IN AREA OF LT SIDE WING ATTACHMENT. CRACK LENGTH 6MM (0.236IN). FOUND DURING EDDY CURRENT INSPECTION.SDR 04FDEA00336Spar · corrodedRT WING, UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 506 TO XORS 538. RT WING, UPPER SURFACE IN SPAR AREA BETWEEN XORS 506 TO XORS 538 CORROSION REPAIRED AS PER SRM 51-21-01 VOL.IISDR 04FDEA00337Spar · corrodedRT WING- UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 562 TO XORS 623. RT WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 562 TO XORS 623 CORROSION REMOVED AND REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL. II.SDR 04FDEA00338Spar · corrodedRT WING UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 538 TO XORS 582. RT WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 538 TO XORS 562 CORROSION REMOVED AND REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL. II.SDR 04FDEA00339Spar · corrodedRT WING UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 455 TO XORS 506. RT WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 455 TO XORS 506 CORROSION REMOVED AND REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL. II.SDR 04FDEA00321Spar · corrodedRT WING - UPPER SURFACE IN SPAR AREA BETWEEN XORS 264 TO XORS 298 FOUND WITH CORROSION. CORROSION ON RH WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 264 TO XORS 298, STR 12 TO STR 13 REMOVED AS PER SRM 51-21-01 VOL. II AND FOUND WITHIN LIMITS AS PER SRM 57-SDR ABXA040057Spar · crackedRIGHT WING REAR SPAR XRS 139 JACKPAD TO REAR SPAR FITTING CRACKED. REPAIRED AREA IAW REA D857-48845MR.SDR UPS04241791Spar · crackedINSPECTION TYPE: C, RIGHT WING REAR SPAR UPPER CHORD HAS CRACK INDICATION BETWEEN WS 288L TO WS 285. SPAR REPAIRED IAW UPS ENGINEERING AUTHORIZATION 727-57-20108.SDR 2004FA0000142Spar · crackedAD 200-25-02-R1, INSPECTION OF WING SPARS WAS SIGNED OFF AS COMPLIANCE WITH, ON 19 AUG O1 AS A NON-REOCCURRING INSP. DURING ANNUAL INSPECTION IN JAN 04, BOTH MAIN SPARS WERE FOUND TO BE CRACKED AT THE ROOT END.SDR AUS20040105Spar · cracked(AUS) RT WING FRONT AND REAR SPARS CRACKED. CRACKS APPEAR TO ALIGN WITH THE ATTACHMENT FITTING BOLT HOLES. SPARS ARE CONSTRUCTED FROM TIMBER. FOUND DURING INSPECTION IAW AD/CHA/23 AMDT4.SDR 2004FA0000080Spar · corrodedAD 2002-26-02 CORROSION INSPECTION: REMOVED BOTH WINGS AND BOTH FUEL TANKS. INSPECTED ENTIRE CENTER SECTION AND FOUND FOUR QUARTER SIZED AREAS OF LIGHT CORROSION ON FWD SIDE OF FRONT CENTER SECTION SPAR. CORROSION AREAS WERE SANDED WITH 240 GRIT SANDPAPER AND SDR JRP2004F00000Fitting · crackedLATERAL CRACK BETWEEN RIVETS IN VERTICAL LEG OF FITTING AT WS 40 AND AT WS 47.5 FITTING IS PART OF FORWARD WING ATTACHMENT ASSEMBLY. NOTE: PART NAME IS FRONT SPAR CAP ADAPTOR FITTING.SDR DHL2004806524Frame · crackedRIGHT STUB WING FORMER CRACK 0.250, STA XFS 548.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (ALCLAD 2024T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B PG 16, 17. INSTALLED ANGSDR DHL2004806526Frame · crackedRT OUTER WING OUTBOARD L/E FORMER 0.250 INCH CRACK, STA XFS 785.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGSDR DHL2004806525Frame · crackedRIGHT INNER WING CTR L/E FORMER 1.000 INCH CRACK, STA XFS 385.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (2024T3 0.040) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED RSDR DHL2004806522Frame · crackedRIGHT OUTER WING OUTBOARD L/E FORMER CRACK 0.250, STA XFS 785.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED AN
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