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 ABXA010779Spar · crackedLEFT WHEEL WELL, JUST OUTBOARD OF STATION ZERO, CENTER TANK ON REAR SPAR, UPPER INBOARD CORNER, HAD A CRACK. REPAIRED AREA IAW DC-9 SRM 51-30-5 AND 57-09.SDR CALA0200122Spar Cap · crackedINSPECTION FOUND A 1/2" CRACK AT HOLE IN SPAR CAP AT R/H WING MLG BEAM ATTACH FITTING. REPAIRED IAW ECRA 5740-02000. THE ITEM WAS PLACED ON DIP TO PERFORM AN HFEC INSPECTION ON THE R/H WING REAR SPAR AT MLG BEAM ATTACH FITTING AT THE LOCATION REFERENCED IN ECRSDR AUS20020168Spar · delaminated(AUS) LT AND RT AFT SPAR WEBS DELAMINATED.SDR AUS20020195Spar · delaminated(AUS) LT WING REAR SPAR WEB DELAMINATED IN THREE AREAS.SDR AUS20020167Spar · delaminated(AUS) LT AND RT AFT SPAR WEBS DELAMINATED.SDR 2002FA0000351Spar · corrodedDURING ANNUAL INSPECTION OF THE CARRY THROUGH SPARS, INTER GRANULAR CORROSION WAS FOUND IN THE BOTTOM WEB OF THE AFT SPAR, NONE FOUND IN THE FORWARD SPAR. PROBABLE CAUSE WAS IN MANUFACTURING. RECOMMEND CONTINUED INSPECTION OF OLD SPARS.SDR 2002FA0000254Spar · crackedDURING THIS ANNUAL INSPECTION FOUND COMPRESSION CRACKS ON THE RIGHT WING REAR SPAR AT TOP LOCATION ON TOP SIDE OF SPAR. THIS COMPRESSION CRACK WAS HIDDEN UNDER OLD SPAR VARNISH AND WOULD HAVE BEEN MISSED IF TOP INSPECTION HOLES WERE NOT INSTALLED ALSO MANY OTSDR CA020221002Spar Cap · cracked(CAN) CRACK WAS DICOVERED WHILE PERFORMING NDT IN ACCORDANCE WITH AIRWORTHINESS DIRECTIVE CF93-07. WHILE CARRYING OUT REPAIR, ADDITIONAL CRACKING WAS FOUND IN AREA OUTSIDE OF THE INSPECTION PARAMETERS OF AD CF93-07 AT RBL 53 AND RBL 58.SDR DHL2002364500Spar · corrodedLEFT WING REAR SPAR BETWEEN RIB 19 AND 22 HAS LIGHT CORROSION ON AFT FACE SPAR. REMOVED CORROSION IAW A300SRM 51-40-11.SDR 02FDEA00133Spar · bulgedLT WING UPPER FIXED T/E PANEL BULGED AT BS XOR 674 (CTR OF NR 4 SPOILER). REMOVED AND REPLACED OUTER WING REAR SPAR/TRAILING EDGE PER EA 1-5720-60680.SDR 02FDEA00132Spar · corrodedLT WING UPPER FIXED T/E PANEL BULGE AT BS XOR 772.5 (O/B OF NR 5 SPOILER). REMOVED AND REPLACED OUTER WING REAR SPAR/TRAILING EDGE PER EA 1-5720-60680.SDR ARWA20020205Spar · crackedDURING C-CHECK, LEFT WING STA XW 60 AUXILIARY SPAR LUG WITH CRACK, ADJACENT TO MLG TRUNNION FITTING. REMOVED AND REPLACED AUXILIARY SPAR IAW DRAWING 5616128.SDR UIEA02007Spar · corrodedDURING CURRENT C-CHECK AT KLM/AMS, FOUND LEVEL 1 CORROSION ON THE L/W VERTICAL FLANGE OF THE LOWER FRONT SPAR CHORD BETWEEN ILES 630.72 AND 638 (INBOARD OF NR 2 PYLON). TAPER LOCK FASTENERS IN THE AFFECTED AREA WERE REMOVED. CORROSION BLENDED AND FASTENER HOSDR ABXA010734Spar · crackedLEFT UPPER FORWARD SPAR WAS CRACKED AT THE INBOARD LEADING EDGE ATTACH HOLE. REPAIRED SPAR IAW DC-9 REA D957-43288MR.SDR IXXA0200017SSpar · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING LOWER SPAR INBOARD OF THE #4 ENGINE PYLON FORWARD SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 57-DC8-1837.SDR 200200175Spar · corrodedCENTER WING REAR SPAR WEB CORROSION. THIS REPAIR IS ACCOMPLISHED BY BLENDING OUT CORROSION AREAS. SECTION OF THE SLOPING PRESSURE DECK ANGLE WHICH WAS REMOVED TO GAIN ACCESS TO CORRODED AREAS IS ALSO REPLACED. THIS IS ACCOMPLISHED USING TWO SPLICE ANGLES. SDR QXEA0201418Spar · gougedCKB - RIGHT HAND WING FORWARD SPAR TOP FLANGE OUTBOARD OF NR 2 NACELLE AT 24 INCHES HAS GOUGES. REPAIRED IAW DHC-8 SRM 51-20-11, PAGE 3, METHOD 2.SDR 2002F00205Spar · crackedDURING CURRENT C-CHECK AT SIAC INSPECTION OF THE RT L/E NR 15 KRUEGER FLAP, A CRACK WAS DISCOVERED IN THE FRONT SPAR INBOARD END OF THE DEVICE (65B39252-2). (M)SDR UPS02837653Doubler · brokenINSPECTION TYPE:C2 LT WING LOWER SPAR CAP DOUBLER BROKEN, PIECE MISSING AT XS520. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 57-2-1 FIG 14 A.SDR EIAA2002012Spar · corrodedMZJ-EAC - FOUND STATION 1241 REAR SPAR WEB, LEFT SIDE WAS FOUND TO HAVE 2 LOCATIONS OF CORROSION BEHIND FITTING. CORROSION REMOVED AND REPAIRED PER SB 747-57-2263 R2, EO 57-747-1544-99A AND ECRA 482-57-141-2. (M)SDR 2002FA0000261Spar · crackedCRACK ON BOTTOM SURFACE OF SPAR LEFT SIDE REAR. FOUND PRIOR TO CRACK INSPECTION AS PER AD, OWNER DISCONTINUED ANNUAL INSPECTION PRIOR TO FULL INSPECTION.SDR 2002FA0000249Spar · crackedDURING INSPECTION OF AD INSPECTION. FOUND LEFT WING FORWARD SPAR CRACKED AT UNDER SIDE OF SPAR OUT BOUND OF LIFT STRUT ATTACH POINT. OWNER WAS CALLED TO INFORM HIM THIS WING WILL BE REPAIRED WITH NEW SPAR INSTALLED.SDR TVM2002F00000Spar · crackedWHILE COMPLYING WITH AD, A LONGITUDINAL CRACK IN THE RIGHT FORWARD WOODEN WING SPAR APPROXIMATELY 30 INCHES LONG.SDR AUS20020071Spar Cap · corroded(AUS) WING SPAR CAP CONTAINED EXFOLIATION CORROSION.SDR AUS20020249Spar · corroded(AUS) LT REAR WING SPAR UPPER AND LOWER CHORDS CORRODED IN AREA LOCATED BEHIND THE VERTICAL STIFFENER. CORROSION LOCATED AT ZONE 6-72, WS 437 TO WS 438 LT.SDR HO1R15248Spar · corrodedDURING ANNUAL INSPECTION THE RIGHT WING AFT ATTACH FITTING OUTBOARD OF THE FUSELAGE AND AFT WING SPAR WERE FOUND TO EXHIBIT DISSIMILAR METAL CORROSION BETWEEN THE STEEL ATTACH FITTING AND THE REAR SPAR. THE AFT SPAR WAS CORRODED TO THE POINT WHERE A CRACK HADSDR 2002F00194Spar · corrodedFOUND CORROSION ON RIGHT WING UPPER SPAR CHORD ALONG EDGE BETWEEN SPLICE PLATE AND CHORD STATION 663 OUTBOARD OF BBL 70.85 APPROXIMATELY 3.5 INCHES LONG. (M)SDR 2002FA0000234Spar · crackedRIGHT REAR SPAR CRACKED ON TOP AT OUTBOARD END OF STRUT ATTACHMENT DUBBLER. TIP OF SPAR HAS DUBBLER PLATES. SPAR HAS BEEN DAMAGED BEFORE.SDR CA020104020Spar Cap · chafed(CAN) DURING "C" CHECK AND CORROSION INSPECTION THE LT REAR SPAR CAP AND SPAR AREA ABOVE THE SPAR CAP WAS FOUND CHAFED. THE CHAFING WAS CAUSED BY SPIRAL WRAP WOUND AROUND A WIRE BUNDLE THAT RUNS ACROSS THE FACE OF THE REAR SPAR.SDR AUS20020002Spar · corroded(AUS) FORWARD SPAR ASSEMBLY CONTAINED SEVERE EXFOLIATION CORROSIONBETWEEN THE SPAR PNO 0523014-2 AND THE ATTACHMENT PLATE PNO 0523016-1. THE THICKNESS OF THE ASSEMBLY WAS REDUCED BY APPROXIMATELY 50% DUE TO THE CORROSION. THE RIVETS HOLDING THEASSEMBLY TOGETHESDR 2003F00335Spar · corrodedLEFT WING FRONT SPAR UPPER CAP, LOWER LEG, HAS CORROSION AT WS 222.0 AND 224.5. CORROSION FOUND OUT OF LIMITS. REPAIRED SPAR PER DRAWING RFB275710-122601. (M)SDR CA020702001Spar · corroded(CAN) CORROSION FOUND ON FRONT AND REAR SPAR CAP IN AUXILIARY FUEL BAY RIGHT HAND SIDE. CORROSION FOUND ON SPAR CAP IN AUXILIARY FUEL BAY LEFT HAND SIDE.SDR AUS20011457Spar · corroded(AUS) LH AND RH WING REAR SPAR ATTACHMENT POINTS CORRODED AS DESCRIBEDIN AD/PA28/40. INSPECTION WAS CARRIED OUT IAW AD/PA28/40 WHICHWAS NOT DUE FOR ANOTHER TWO YEARS.SDR UPS02237543Spar · corrodedINSPECTION TYPE:C+SI WING CENTER SECTION FRONT SPAR UPPER CHORD HAS CORROSION AT RT END OF CHORD AT RBL 55 APPROX. FOUND TO BE EXFOLIATED.SDR LAB2002F00000Spar · crackedCRACK IN A SPOT THAT IS NOT VISIBLE TO BORESCOPE WHEN COMPLYING WITH AD. 730 HOURS SINCE EFFECTIVE DATE OF AD. 1000 HOURS ALLOWED FROM EFFECTIVE DATE.SDR KZH2002F00000Spar Cap · crackedWHILE PERFORMING AN EDDY CURRENT INSPECTION OF THE .3750 DIAMETER BOLT HOLES ON THE LOWER SPAR CAP, 3 SMALL CRACKS WERE INDICATED. AD HAS BEEN ISSUED ADDRESSING THE ABOVE PROBLEM, HOWEVER IT DOES NOT ADDRESS AIRCRAFT OF THIS MODEL BELOW 4000 TT. I AM CONCERNSDR GTIA012191Splice · corrodedFTW - FOUND LEFT WING LEADING EDGE UPPER FRONT SPAR PREVIOUS REPAIR HAS CORROSION FROM XFS 550-XFS 77. REMOVED CORROSION. SPLICE PLATE FOUND TO BE OUT OF LIMITS. FABRICATED SPLICE PLATE. INSTALLED SPLICE PLATE IAW MD80 SRM 51-30-5. (M)SDR TSAA0253012Spar · corrodedDISCOVERED CORROSION AT RIGHT WING WBL 304.5 FORWARD SPAR LOWER CHORD. REMOVED CORROSION PER SRM 737-100/200, 57-30-1 FIGURE 1. HFEC INSPECTED BLENDOUT AREA TO ENSURE NO CRACKS AND CORROSION REMOVED. RESTORED AIRCRAFT TO NORMAL IAW ECO 2135. AIRCRAFT OK FOSDR ASOA01264Spar Cap · crackedDURING SCHEDULED MAINTENANCE IN MCN, A CRACK WAS FOUND ON THE RIGHT SIDE LOWER SPAR CAP. MAINTENANCE REPAIRED THE CRACKED SPAR CAP IAW ASA EO 120-57-0117. THE EO REF SRM 57-20-05, FIGURE 201 AND SRM 51. AIRCRAFT OK FOR SERVICE. (M)SDR ABXA010607Spar · crackedLEFT UPPER REAR SPAR HAD A HORIZONTAL CRACK IN THE UPPER INBOARD CORNER FROM LEFT BUTT LINE 5 TO BUTT LINE 0. REPAIRED AREA IAW DC-9 SRM 57.SDR UPS01437282Spar · crackedINSPECTION TYPE:SP RIGHT WING REAR SPAR HAS A 1.5 INCH CRACK IN AFT WING SPAR WEB AT STA 1238 REF DMI D-226421. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-10-05 FIG 2.SDR GTIA012262Doubler · crackedFTW - FOUND LEFT WING LEFT REAR SPAR DOUBLER CRACKED IMMEDIATELY OUTBOARD OF THE STATION XCW=58.688 TRAPEZOIDAL PANEL TO REAR SPAR ATTACH FITTING. REMOVED DAMAGE AREA. REPAIR DOUBLER FABRICATE. INSTALLED REPAIR DOUBLER IAW DC9. (M)SDR AUS20011174Spar · cracked(AUS) WING RH FORWARD SPAR WEB CRACKED AROUND BEND RADIUS AND FORWARD FACE. FOUND DURING INSPECTION IAW BEECH SB 2269 REV1 ANDAD/BEECH55/62 AMDT4.SDR 2001FA0000500Spar Cap · corrodedDURING ANNUAL INSPECTION, WING CARRY THROUGH SPAR WAS FOUND TO HAVE EXFOLIATION CORROSION ON TOP SPAR CAP.SDR 01FDEA00916Spar · crackedRIGHT WING I/B MIDFLAP, AFT FLAP CONTROL ROD CUT OUT IN THE LWR SPAR CHORD CRACKED. REMOVED AND REPLACED CHORD PER SRM 51-40-4, 51-30-2.SDR 2002FA0000236Spar · crackedFOUND A CRACK AT THE SPAR BUTT ON THE RIGHT FORWARD SPAR WHILE COMPLYING WITH AD. THE CRACK WAS CLOSE TO THE WING ATTACH FITTING WHICH LIMITED THE ABILITY TO FULLY INSPECT THE CRACK WITHOUT MAJOR DISASSEMBLY. A PIECE OF .020 INCH SAFETY WIRE WAS ABLE TO GO ISDR AUS20011108Spar Cap · debonded(AUS) LT AND RT WING SPAR CAPS DEBONDED AND CORRODED. FOUND DURING ULTRASONIC INSPECTION IAW JWP/2531/01 AND JWP/2503/01.SDR 2001UALA02106Spar · damagedRIGHT HAND WING REAR SPAR LOWER CHORD DAMAGED AT WS 590 TO WS 605. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, MANUFACTURED CHORD ANGLE AND INSTALLED.SDR 2001UALA02105Spar · damagedRIGHT HAND WING REAR SPAR WEB DAMAGED FROM WS 585 TO 605. MAJOR REPAIR ACCOMPLISHED. SPLICED AND REPAIRED WEB.SDR 0103549759Spar Cap · corrodedDURING H CHECK IN ATL, CORROSION WAS FOUND ON RT WING REAR SPAR UPPER CAP AROUND THE HOLE FOR NR 3 FLAP HINGE STUD. THE HOLE WAS CLEANED UP WITH A DEPTH OF .040 INCH AND DIAMETER OF 1.26 INCH EXTRUSION 4911204, PER EA 97-185168.
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