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 99ZZZX1057Spar · wornDURING ANNUAL INSPECTION, FOUND FRETTING AT LEFT AND RIGHT MAIN GEAR LEGS (PN 35644-04 AND PN 35644-05) TO WING LOWER SPAR CAP ATTACH POINTS. INSPECTION REVEALED THAT LOWER ATTACH BOLTS (AN4-11A) WERE LOW ON TORQUE AND ATTACH HOLES IN GEAR LEGS AND SPAR CAPS SDR TWAA9902304Spar · crackedDURING OP 15 MAINT CHECK, FOUND RT WING WITH APPROXIMATELY .625 INCH CRACK IN REAR SPAR UPPER CAP AT UPPER INBD HOLE AT CENTER HINGE INBD ATTACH BOLT, APPROXIMATELY 10 TO 12 O'CLOCK POSITION. STOP DRILLED CRACK AND INSTALLED DOUBLER AND FILLER PER ARA 16062.SDR TWAA9902303Spar · crackedDURING OP 15 MAINT CHECK, FOUND RT WING WITH .375 INCH LONG CRACK IN REAR SPAR UPPER CAP AT UPPER OTBD HOLE AT CENTER FLAP HINGE OTBD ATTACH BOLT AT APPROX 1130 TO 1230 O'CLOCK POSITION. BLENDED AREA PER SRM 57-01, FIG 1. INSTALLED DOUBLER AND FILLER PER ARASDR CA990318032Spar Cap · cracked(CAN) WHILE C/W AD CF 92-26, A CRACK WAS DISCOVERED VISUALLY IN THE LOWER FORWARD SPAR CAP. A SECOND CRACK APPROXIMATELY 1.1250 INCH WAS FOUND IN THE RADIUS OF SHEAR ANGLE. INSPECTION WAS C/W PRE AD REQUIREMENT. AD CALLS FOR ULTRASONIC TESTING.SDR MWEA99061Spar · damagedFOUND DAMAGED HOLE AT RIGHT WING STATION 109.0 AFT SPAR. MTC INSTALLED TEMPORARY REPAIR STRAP.SDR DL72K990245Spar · damagedFOUR FASTENER HOLES WERE MISDRILLED DURING ACCOMPLISHMENT OF EO 4-72440-3AD. HOLES WERE OVERSIZED TO 0.312 DIA. REPAIRED PER ERA 332757-14AD.SDR AU990113Spar · cracked(AUS) LT UPPER MAIN PLANE FRONT SPAR (P/N H34737) AND REAR SPAR (P/N H34356) CRACKED AND SPLIT HORIZONTALLY FROM WING ROOTS TO WING TIPS. FOUND DURING INSPECTION IAW AD/DH82/11 AMDT1 (BRITISH AEROSPACE T.N.S. CT(MOTH) NR 32 ISSUE 2). PART TC: 2,549.SDR AU990082Spar · cracked(AUS) LEFT UPPER MAIN PLANE FRONT SPAR P/N H34737 AND REAR SPAR P/N H34356 CONTAINED HORIZONTAL CRACKING AND SPLITS FROM THE ROOTS TO THE TIPS. FOUND DURING INSPECTION IAW AD/DH82/11 AMDT1 (BRITISH AEROSPACE T.N.S. CT(MOTH) NR 32 ISSUE 2). PART TC: 2,549.SDR AALA990143Spar · corrodedTUL - FORWARD LOWER SPAR CHORD VERTICAL LEG HAS CORROSION BELOW NR 7 SLAT ACTUATOR. REPAIRED PER ESO 11697 DATED 1-25-99. (M)SDR 99FDEA00032Spar Web · crackedNR 129 - RT WING REAR SPAR WEB HAS CRACK EMANATING INBD FROM RADIUS OF APU FUEL PUMP HOLE. CRACK APPROX 2.5 INCHES IN LENGTH VER BY NDT. STOP DRILLED CRACK AND PLUG HOLE IAW SRM 51-00-02 AND 53-00-01 WEB DOUBLER INSTALL PER EA 8-5710-40417.SDR AU990088Spar · cracked(AUS) FORWARD WING SPAR CARRY THOUGH STRUCTURE CRACKED ON THE RT SIDE IN BOTH THE FORWARD AND AFT AREAS AS DESCRIBED IN BEECHCRAFT SERVICE BULLETIN NR 2269 REV 1 (NOT APPLICABLE TO THIS AIRCRAFT). PART TC: 81,801.SDR CALA9900082Spar Cap · crackedINSPECTION FOUND A 1.875 INCH CRACK IN RT WING LOWER SPAR CAP, UNDER THE I/B FLAP HINGE FITTING AT STA XRS 164.0. A REPAIR WAS INSTALLED IAW DOUGLAS DRAWING NR 506271.SDR CA990210017Cap · cracked(CAN) INSPECTION PER SB 215-A454 FOUND A HAIR LINE CRACK AT THE LOWER SPAR CAP AT WS 51-650 LT. INSPECTION PERFORMED BY NDT USING ULTRASONIC, EDDY CURRENT AND DYE PENETRANT. REPAIR WILL BE IAW PSP 297 CH. 57-15-06.SDR RRXA991053Spar · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, WING, LT I/B FLAP REAR SPAR UPPER CAP AT STA XW 97. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT SECTION OF SPAR, REPAIR ANGLES, ANDSDR UPS99228477Front Spar · corrodedINSPECTION TYPE-SI, CORROSION (C57-571-01.05-01) ON LEFT WING FRONT SPAR FUEL TANK ACCESS CUT OUT 7340 AFT SURFACE. REMOVED CORROSION AND REPAIRED PER EO 99-5020.SDR P5CA9900042Spar · corrodedLEVEL 1 CORROSION FOUND ON LEFT WING UPPER SURFACE OF REAR SPAR WS 410 TO 1390. REPAIRED PER SRM 51-10-01, 57-30-01 AND MM 51-14-07.SDR DL72W990142Spar Chord · crackedTHE FRONT SPAR CHORD WAS FOUND WITH CRACKS IN THE FWD FLANGE AT A FASTENER HOLE AT APPROX WS 333. REPAIRED PER ERA 332687-14.SDR TSAA9957042Spar · corrodedLEFT WING FRONT SPAR LOWER CHORD AT NR 2 SLAT ACTUATOR HAS EXFOLIATION CORROSION. CLEANED AND TREATED PER SRM 51-10-6. REPAIRED PER ECO 2135R2. TAT: 47,785.0 HOURS. TAC: 63,219. (X)SDR 99FDEA00017Spar · corrodedUPON REMOVAL OF CTR WING SECTION AFT BULKHEAD WEB FOUND VERTICAL FLANGE OF LWR 870 SPAR CHORD TO BE CORRODED FROM LBL 60-RBL 35.SDR AU990019Spar · cracked(AUS) WING FRONT SPAR SPLICE RIGHT OUTBOARD HOLE HAS A SMALL CRACK AT THE INBOARD LOWER CORNER OF THE SPAR SECTION RUNNING UP THE BOLT HOLE. CRACK LENGTH APPROXIMATELY 3.175 MM (0.125 INCH). FOUND DURING NDT INSPECTION IAW AD/ACSNOW/24 AMDT1.SDR UPS99828586Frame · crackedINSPECTION TYPE-123D, LT WING O/B LEADING EDGE STA 495 FRAME CRACKED AT PNEU DUCT SUPPORT. FABRICATED DOUBLER IAW DC8 SRM 57-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.SDR CALA9900101Spar · crackedINSPECTION FOUND A .25 INCH CRACK IN RT WING AFT SPAR AT I/B ACTUATOR HINGE FORWARD FORGING FROM I/B LOWER BOLT AREA, APPROXIMATELY XRS 164. THE FASTENERS WERE REMOVED AND THE CRACKED SECTION OF SPAR WAS CUT OUT. A NEW SPAR SECTION WAS INSTALLED USING SPLICESDR MZZA99012Spar Web · crackedTNN - DURING S-CHECK INSPECTION AT AIR ASIA, CRACK WAS FOUND ON WING CENTER SECTION REAR SPAR WEB AT WL 185 FROM RBBL 2 TO RBBL 4. THE WING CENTER SECTION REAR SPAR WEB CRACK END WAS STOP DRILLED AND REPAIRED PER EA 5750-01843 OP 3. (M)SDR MWEA981182Spar · misdrilledRIGHT WING AUXILLARY SPAR UPPER ATTACH HOLE IS MISDRILLED. CLEANED UP HOLE FABRICATED AND INSTALLED REPAIR BUSHINGSSDR 99ZZZX148Spar · crackedDURING REPAIR OF RT AND LT WINGS, CRACKS WERE DISCOVERED IN LOWER SPAR CAP OF BOTH WINGS NEAR THE 2ND MOST INBD WING ATTACH BOLT HOLE. CRACK APPEARED TO START WHERE THE SPAR DOUBLER, P/N 2-1610-081, INTERSECTS A ROUTED AREA OF INBD END OF THE LOWER SPAR CAP. SDR AU981681Spar · cracked(AUS) DURING INSPECTION, A CRACK WAS FOUND IN THE SPAR ASSEMBLY EXTENDING FROM STRINGER NR 13.SDR 9810909916Spar Cap · crackedDURING PERIODIC CHECK, FOUND RIGHT WING LOWER SPAR CAP WITH ONE INCH CRACK AT FS 353 BELOW LOWER OUTBOARD MOUNTING HOLE AT NR 4 HINGE FITTING. INSTALLED INTERIM REPAIR PER EA 99-159428.SDR CA990119001Fitting · cracked(CAN) MPI OF SPAR FITTING REVEALED A CRACK IN THE CENTER OF THE WELD STARTING AT THE END AND GOING AFT. UNABLE TO DETERMINE HOW FAR BACK THE CRACK GOES. FITTING REQUIRES COMPLETE REMOVAL. MANUFACTURER NOTIFIED.SDR CKSA98748Spar · corrodedLOCATED AT LEFT WING LOWER L/E CAVITY, FRONT SPAR, LOWER CHORD AT OSLE 1440 AND OSLE 1460 FOUND SMALL AREA OF LEVEL 2 LOCAL CORROSION. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPAIR FACILITY, IN HONG KONG (VHKG). SDR AALA982158Spar · corrodedTUL - FOUND CORROSION ON FORWARD SPAR LOWER CHORD PLATE FS 514. INSTALLED REPAIR STRAP OVER BLENDOUT PER AARD 57-30-00-2 PAGE 1-3. (M)SDR CA981216004Spar · cracked(CAN) SPAR INSPECTION AS DETAILED IN SL 406A FOUND WITH A 2 INCH CRACK. WOOD SPAR HAD BEEN INVOLVED IN A FLIP OVER PREVIOUSLY.SDR ABXA9801179Spar Cap · crackedNR 3 MAIN TANK ACCESS PANEL NR 506A, LOWER CENTER SPAR IS CRACKED BETWEEN FUEL TRANSFER SLOTS AND FASTENERS AT STATION XRS 26. REPAIRED IAW ABX REA D857-24357MR, REV F.SDR VJ9800665Spar Chord · corrodedSCHEDULED INSPECTION, THE RIGHT HAND LOWER WING CHORD HAS MATERIAL MISSING AND CORROSION AT FUELING PANEL AT FS 365. MECHANICALLY REMOVED CORROSION, MATERIAL THICKNESS .170, MATERIAL LOSS .100 REMAINING THICKNESS .070. FABRICATED REPAIR DOUBLER IAW AIRTRAN RSDR SWAA983036Spar · crackedDURING SCHEDULED D-CHECK, FOUND LEFT WING CENTER FUEL CELL UPPER REAR SPAR SEAL CUP CRACKED. REPAIRED PER TRAMCO EWO 98-1085.SDR 98ZZZX4775Spar · corrodedAIRCRAFT WAS METALIZED IN 1960'S. NO INSPECTION PROVISIONS IN WINGS. FRONT SPAR ON RT WING WAS/IS SEVERELY CORRODED FROM STA 40 TO STA 80. CORROSION IS ON LEADING EDGE SIDE OF SPAR. FOUR LEADING EDGE FORMERS ALSO SEVERELY CORRODED.SDR DHL9872060DSpar · wornAT D CHECK, NR 4 SLAT WHERE NR 12 RIB FROM O/B END ATTACHED TO SPAR WEB HOLES ARE LARGE AND ELONGATED. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 57-30-3, 7 BY 4, N/R 1958.SDR ARWA981119Spar · crackedC-CHECK, CENTER WING REAR SPAR LOWER CAP CRACKED BETWEEN FASTENERS STA 857 LBL 37, 51, 61 LT W/W. STOP DRILLED CRACKS AND INSTALLED DOUBLERS PER DRAWING NR 98-013 ON 8110-3 DATED SEPT 22, 1998 UNDER WORK ORDER NR 1300.SDR ARWA981118Spar · crackedC-CHECK, WING REAR SPAR LOWER CAP CRACKED BETWEEN FASTENERS 33 TO 35 RIGHT OF CENTER LINE AND 53 TO 54 STA 857 RT W/W. STOP DRILLED AND INSTALLED DOUBLERS PER DRAWING NR 98-015 ON 8110-3, DATED SEPT 30, 1998 UNDER WORK ORDER NR 1300.SDR RRXA98576Spar · misdrilledDURING MAINTENANCE VISIT, FOUND LT WING LOWER FRONT SPAR FORWARD FLANGE WITH MISDRILLED HOLES BETWEEN WS XFS 417 AND XFS 424. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05566 AND TREATED AREA IAW DC-8 SRM 51-1-8.SDR MWEA981086Spar Cap · mismanufacturedFRONT SPAR SECTION MACHINED INCORRECTLY AT XS 560. FABBED FILLERS AND DOUBLER, ALODINED AND PRIMED. ALSO, INSTALLED DOME, SEALED REPAIR FASTENERS. LEAK CHECK NOT REQ, REPAIR IN VENT BOX.SDR MWEA981085Spar Cap · mismanufacturedFRONT SPAR SECTION MACHINED INCORRECT AT XS 560. MTC FABRICATED AND INSTALLED FILLERS AND DOUBLERS.SDR DHL9872093DFrame · crackedAT D CHECK, RIGHT WHEEL WELL AFT OF UPLOCK FITTING BS 915 CRACKED FRAME 12 BELOW PRESSURE FLOOR. STOP DRILLED, HFEC, INSTALLED ANGLE PER SRM 57-40-3, 4 BY 8, N/R 2916.SDR AU981540Web · cracked(AUS) CENTER SPAR WEB CRACKED. FOUND DURING INSPECTION IAW SA226/ST-UN-M002.SDR MZZA98294Spar · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT WING T/E INBOARD MID FLAP REAR SPAR LOWER CHORD HORIZONTAL FORWARD FLANGE AT WBL 2105. THE CORRODED REAR SPAR LOWER CHORD HORIZONTAL FORWARD FLANGE WAS CLEAN UP AND REPAISDR QXEA9801690Spar · delaminatedLEFT-HAND WING FRONT SPAR LOWER MOUNTING FLANGE FOR INBOARD END OF PANEL 61C AT STATION 4700 HAS ONE LAYER DELAMINATING. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B (2).SDR P2EA98245Spar · corrodedSJO - RIGHT WING FRONT SPAR UPPER CHORD CORRODED AT FSS 430. REPAIRED RIGHT WING FRONT SPAR UPPER CHORD BETWEEN FSS 401.95 AND FSS 460 PER COOPESA EO COO-3-57-597 DATED OCT 30, 1998 AND BOEING INSTRUCTION LIST OF DATA INCLUDED ON FAA FORM 8110-3. (M)SDR DHL9980192CSpar · crackedAT C-CHECK, LEFT WING L/E SPAR AREA AT XW 408 UPPER SURFACE CRACK ON FIXED L/E SECTION OF UPPER FLANGE. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER AND INSTALLED PER SRM 51-1-8 AND EO 18R5761051.SDR CA981207008Spar · cracked(CAN) MAINTENANCE CARRIED OUT THE INSPECTION REQUIRED BY AIRFRAME AIRWORTHINESS LIMITATIONS MANUAL ST-UN-M001 ATA 5710, FIG. 10-1, REV C DATE APRIL 17,1998 - AND FOUND THE MAIN SPAR CENTER WEB CRACKED AT BOTH STRINGER NR 13 CUT-OUTS. AIRCRAFT FERRIED TO CALGASDR P2EA98201Spar · wornSJO - RIGHT WING FRONT SPAR LOWER CHORD WORN AT WSL 475, DEFECT SIZE LENGTH 2.625 INCH, WIDTH .812 INCH DEPTH .055 INCH. REPAIRED FRONT SPAR LOWER CHORD AT WS 475 PER COOPESA EO C00-SJO-57-567-98 DATED OCT 15, 1998 AND BOEING FAX COO-SJO-98-0755RR DATED OCT 9SDR DL72S982149Frame · crackedCRACK WAS FOUND IN THE VERT FLANGE OF THE WING TO FUSE UPPER ATTACH CHORD, LWR FRAME HOLE RBL 70.85, FS 760. REPAIRED PER ERA 332283-14AD.
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