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 = '5541' 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 = '5541' 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 IPXA2016040901867Rib · corrodedINSPECTION TYPE:3C, CORRODED RIB, AMC7292-33 INSIDE UPPER FWD RUDDER L/E AT BS ZFR450. REMOVED FABRICATED AND INSTALLED REPLACEMENT RIB IAW DWG AMC7292 AND SRM 51-35-01.SDR QXEA2016022500151Spar · gougedTRAILING RUDDER FRONT SPAR AT LOWER MAIN HINGE HAS GOUGED. REPAIRED IAW RD 8/4-55-1221, ISSUE 2. NO DEFECTS NOTED.SDR SIMA20151231003Rib · bentRUDDER 1 HAS 2 BENT RIBS. 1 NEAR THE UPPER CTR HINGE POINT & 1 BY THE LOWER CTR HINGE POINT. INSTALLED RIB IAW SRM 51-40-02.SDR JJBA20150621011Rib · damagedDAMAGE ON LOWER AFT END OF TRAILING RUDDER. R & R DAMAGED AREA, LOWER CLOSING RIB & DAMAGED SKIN ON LEFT LOWER TRAILING IAW RD 8-55-078 & RD 8-55-2862.SDR UHLA2014090600642Rib · crackedCRACK FOUND ON RUDDER VERTICAL SPAR BETWEEN RIBS 9 AND 10. TRIMMED AFFECTED RIB FLANGES AND FABRICATED REPAIR DOUBLERS IAW ETD2014-170-075408, REV 1. INSTALLED REPAIR IAW ETD2014-170-075408, REV 1ABD SRM 51-41-01, 51-41-02.SDR HN6R2014FA0000431Spar · damagedFRONT SPAR OF RUDDER DAMAGED AT RUDDER STATION 165.074. DAMAGE APPROXIMATELY 2"X 2".SDR SIMA20140628027Rib · crackedFORWARD RIB BY UPPER MIDDLE HINGE POINT ON RUDDER 1 HAS A 1/8 INCH CRACK. R & R IAW SRM 51-40-02.SDR R61A201407300940Rib · dentedRUDDER MIDDLE SKIN RIB 28 WAS FOUND DAMAGED. MAINTENANCE R & R RIB IAW SRM 51-42-05-02-01.SDR CA140730012Spar · cracked(CAN) 4 CRACKS WERE FOUND ON THE FORE RUDDER FRONT SPAR FLANGE AT THE CENTER HINGE RIGHT HAND SIDE.SDR CA140128012Rib · damaged(CAN) DURING A STRUCTURAL INSPECTION, MAINTENANCE NOTICED THERE WERE MISSING/SHEARED RIVETS ADJACENT TO WHERE THE RUDDER TORQUE TUBE ASSY ATTACHES TO THE RIB CLOSURE AND DOUBLER DUE TO THE NATURE OF THE DEFECT A FLEET WIDE INSPECTION WAS COMPLETED ON AN ADDITSDR CA130927008Spar · cracked(CAN) A TOTAL OF 4 CRACKS WERE FOUND ORIGINATING FROM THE 1" HOLE IN THE SPAR AS DESCRIBED IN MFG SEB94-3. THE DEFECTIVE SPAR WAS R & R WITH A NEW PART THAT IS NO LONGER MFG WITH THE 1" HOLE.SDR USAA2013090500013Spar · crackedQ3 CHECK, CRACK ON RUDDER LT FRONT SPAR TAB BETWEEN RUDDER STATION 10.8 TO 20. REPAIRED RUDDER LT FRONT SPAR TAB BETWEEN RUDDER IAW EA 105064.SDR UALA2013070304655Spar · gougedRUDDER HINGE (FITTING ON FRONT RUDDER SPAR) IS GOUGED. BLENDED GOUGES IAW ECRA 5530-01705 AND EA 130685. ACCOMPLISHED HFEC IAW NTM 51-00-19, PT 6, NO DEFECTS NOTED.SDR CA130213002Spar · cracked(CAN) RUDDER SPAR CRACKED THROUGH THE UPPER LIGHTENING HOLE AT UPPER RUDDER MOUNTING HINGE. IT WAS NOTED AS CRACKED WHILE CARRYING OUT SID NR 22.SDR CA130201009Rib · cracked(CAN) DEFECT-1097637, THE FORE RUDDER UPPER CLOSING RIB HAS A 4" LONG IRREGULAR CRACK. RESOLVED ON W/O: 370263 TASKCARD: NR-00007, CLOSING RIB ASSY ORDERED AOG, PN 85540027-001. REMOVED DAMGED UPPER CLOSING RIB AND FIT AND DRILLED NEW UPPER RIB ASSY, PN 855400SDR CWQR20121011051Rib · crackedDURING A SCHEDULED INSPECTION, FOUND THE RUDDER ASSY LOWER CLOSE-OUT RIB TO BE CRACKED ON RT SIDE ABOUT 2" LONG. REPLACED CLOSE-OUT RIB.SDR USAA2012070200030Frame · corrodedQ4 CHECK - RUDDER RIGHT SIDE CONDUCTIVE FRAME CORRODED AT RUDDER STA 234.89. REMOVED FRAME, FABRICATED AND INSTALLED NEW FRAME IAW BOEING DRAWING 65C31496 AND EA 104047.SDR FDEA201109304229Rudder · damagedSUSPECT WATER INDICATIONS ON RUDDER FOUND DURING THERMOGRAPHY INSP REPAIR CARRIED OUT TO T/E SCREW NR 37 RT IAW EA 6-5540-154307, PART 1, SRM 55-41-12, MAJOR REPAIR ULTRASONIC INSP OF AREAS IN FIG 2 THRU 8 TO BE CARRIED OUT AT 6 YEAR INTERVALS IAW MRBR IAW ESDR USAA2011040191316Rib · corrodedCLT - Q2 - CRACK ON RUDDER CLOSE OUT RIB AT STA 1127. REPLACED RUDDER CLOSE OUT RIB AT STA 1127 IAW B737 SRM 51-40-02 & EA 102809.SDR DHLA201100022Rib · damagedRT RUDDER RIB BROKEN AT STA ZR 217.188 AFT OF SPAR PERFORMED MAJOR REPAIR IAW JC EC-02401-001 WO 9960, DWG 5654863, MS NR SEU-SEU-11-0007-02B DATED 01-25-11. REMOVED DAMAGED RIB IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED RIB IAW DWG 5654863, HEAT TREATED IAW SRSDR 2010FA0000934Spar · crackedRUDDER SPAR CRACKED AT UPPER HINGE FITTING.SDR 2010FA0000933Spar · crackedRUDDER SPAR CRACKED AT UPPER HINGE FITTING.SDR DALA1022540193Spar · delaminatedRUDDER FRONT SPAR EXTERNAL SURFACE AT RUDDER STA 144, RT L/E FLANGE FOUND DELAMINATED. REPAIR WITH RESIN CARRIED OUT AT DELAMINATED AREA IAW ER/A 482281-14.SDR CA100525022Spar · crackedFOUND 1 IN CRACK IN SPAR BEHIND TOP RUDDER HINGE, AT THE EDGE OF THE HINGE, RUNNING VERTICALLY. RUDDER HAD BEEN REMOVED, AND HINGES REMOVED TO LOOK FOR THIS CONDITION. SPAR HAS SUBSEQUENTLY BEEN REPLACED.SDR ASAA1047937Spar · delaminatedRUDDER FRONT IS DELAMINATED AT RUDDER STA 17.25. CUT OUT DAMAGED AREA AND BONDED REPAIR.SDR 2010FA0000093Spar · crackedTOP RUDDER ATTACH BRACKET CRACKED OUT OF REAR SPAR ON THE VERTICAL FIN. NOTICED CRACK AT ANNUAL INSP. THE RUDDER BEARINGS ARE ALL FREE AND OK. POSSIBLY INSTALL A HEAVIER REAR SPAR.SDR 2010FA0000008Tube · crackedINNER PORTION OF RUDDER HORN TUBE (PN 63547-000) CRACKED AT WELD ASSY (PN 63546-000) ON UNDERSIDE OF WELD BEAD. AREA IN QUESTION EXHIBITED SIGNS OF EXCESSIVE WELD PENETRATION ALONG WITH PROJECTING GLOBULES. PROBABLE CAUSE OF CRACK OCCURRED DUE TO WEAKENING OSDR RU3A0919Rib · gougedDEEP GOUGE FOUND ON UPPER BONDED FLOOR RIB OF RUDDER TRIM TAB PUSH/PULL ROD TUNNEL.SDR CA090910002Spar · crackedAPPROX 2 INCH VERTICAL CRACK IN UPPER END OF SPAR WEB AT UPPER HINGE FITTING. UPPER FITTING LOOSE ON RIB - HINGE PIN LOOSE IN FITTING. CRACK IN SPAR NOT READILY VISIBLE UNTIL RUDDER IS REMOVED. PROBABLY A RESULT OF HIGHER AIRSPEEDS WITH TURBINE POWERED OTTER.SDR CA090310005Spar · cracked(CAN) LOWER FWD RUDDER SPAR FOUND CRACKED. CRACKS FOUND STEMMING FROM THE 2 RIVETS USED TO ATTACH RUDDER HORN.SDR ASAA0944234Spar · delaminatedRUDDER LE SPAR DELAMINATED. REPAIRED RUDDER LE SPAR.SDR 2008FA0000743Spar · crackedSPAR IS CRACKED AND BROKEN OUT AT UPPER HINGE ATTACH POINT. THIS SPAR WAS REPLACED WITH NEW 1-1-99 FOR SAME CONDITION. THIS CONDITION WAS FOUND BY CLOSE EXAMINATION OF AREA DURING ANNUAL INSPECTION. WE ARE IN RECEIPT OF INFORMATION OF SAME FAILED CONDITION OSDR CA080620004Spar · cracked(CAN) FRONT SPAR WAS FOUND CRACKED AFTER THE RUDDER WAS REMOVED FOR REPLACEMENT OF UPPER HINGE BEARING. FRETTING WAS NOTICED AT BEARING BLOCK TO SPAR MOUNTING SURFACE/BEARING BLOCK WAS REMOVED AND CRACKS FROM THE (2) ATTACH HOLES WERE FOUND. 3 CRACKS FROM ONE SDR 2008FA0000379Spar · corrodedFOUND EXTERNAL CORROSION ON RUDDER MAIN TUBULAR SPAR APPROXIMATELY (2) INCHES ABOVE RUDDER CONTROL HORN. POST WAS SEVERELY CORRODED WITH HOLES THRU TUBE. AD 78-08-09 ADDRESSES THIS PROBLEM BUT NOT FOR THIS MODEL AIRCRAFT. (K)SDR UPS08851607Rib · crackedINSPECTION TYPE:C2 NR 5 RIB FROM BOTTOM OF RUDDER IS CRACKED THROUGH PREVIOUS REPAIR AT RT SIDE AT FRONT SPAR. RUDDER REPLACED ON N/R 123801.SDR UPS08851606Rib · crackedINSPECTION TYPE:C2 9TH RIB FROM BOTTOM OF RUDDER IS CRACKED ON LT SIDE AT FRONT SPAR. RUDDER REPLACED ON N/R 123801.SDR UPS08851603Rib · crackedINSPECTION TYPE:C2 17TH RIB FROM BOTTOM OF RUDDER ON LE CAVITY CRACKED. RUDDER REPLACED ON N/R 123801.SDR UPS08851602Rib · crackedINSPECTION TYPE:C2 16TH RIB FROM BOTTOM OF RUDDER ON LE CAVITY CRACKED. RUDDER REPLACED ON N/R 123801.SDR FDKA200712389Frame · damagedFDM 6088 RDU (2225 PHX LCL) - RUDDER CABLES DAMAGED FRAME. MX CURRENTLY TROUBLESHOOTING.SDR 07FDEA04115Rib · corrodedFOUND CORRODED RIB 54 ON RUDDER. REPLACEMENT OF RIB 54 IAW SRM 55-41-19.SDR UPS07849618Rib · crackedINSPECTION TYPE:C2 12TH RIB FROM BOTTOM OF RUDDER ON L/E IS CRACKED. STOP DRILLED CRACK ON 12TH RIB ON RUDDER L/E IAW SRM 55-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON 12TH RIB ON RUDDER L/E IAW SRM 55-2-0 FIG 2 SHEET 2.SDR UPS07849617Rib · crackedINSPECTION TYPE:C2 18TH RIB FROM BOTTOM OF RUDDER ON L/E CRACKED. STOP DRILLED CRACK ON 18TH RIB FROM BOTTOM OF L/E IAW SRM 55-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON 18TH RIB IAW SRM 55-06-00 FIG 028.SDR CA061201003Spar · cracked(CAN) DURING THE COMPANY 12 YEAR STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), A CRACK WAS FOUND ON THE RUDDER SPAR ON THE OUTER LT EDGE OF THE UPPER HINGE ATTACH POINT. (TC NR 20061201003)SDR CA061201002Spar · cracked(CAN) DURING THE COMPANY 12 YEAR STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), A CRACK WAS FOUND IN ON RUDDER SPAR ON THE OUTER LT EDGE OF THE UPPER HINGE ATTACH POINT. LPI INSPECTION WAS USED TO VERIFY THE CRACK (TC NR 20061201002)SDR 06FDEA03988Spar · corrodedUPPER FWD RUDDER REAR SPAR STRUCTURE, SEVERE CORROSION WITH EXFOLIATION ON WEB. REMOVED HINGE TO GAIN ACCESS AND REPAIRED DAMAGED WEB IAW SRM 55-00-01 FIG 9 VOL 1 AND REINSTALLED. REMOVED HINGE PER SRM 51-31-01 PAGE 36/41. FAB PART IAW DETAIL PART TRAVELERSSDR MWEA060138Doubler · delaminatedSIX RUDDER TRIM TAB TRAILING EDGE IS DELAMINATED, NEAR THE CENTER OF THE TAB. FABRICATED AND INSTALLED DOUBLER.SDR 2006FA0000573Rib · crackedRIB, CRACKED AT VERTICAL HINGE LINE JUNCTURE. STRESS FROM COUNTER WEIGHT AND NORMAL WEAR. AGE OF THE PART AND THE WIND. SUBMITTER RECOMMENDS CLOSE INSPECTION AND REPLACEMENT OF PART IF DAMAGED. (K)SDR IXXA06SMN148SSpar Cap · corrodedDURING ROUTINE C CHECK INSPECTION, RUDDER LEFT HAND CAP CORRODED AT HINGE SUPPORT AT STATION ZR 103.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIGURE 2, SHEET 1, AND 3, DOUGLAS DRAWING 5655068. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17, 18. FOUND OUTSDR IXXA06SMN166SSpar Cap · corrodedDURING ROUTINE C CHECK INSPECTION, RUDDER RIGHT HAND CAP CORRODED NEXT TO SUPPORT HINGE HOUSING AT STATION ZR 103.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 55-6-1 FIG. 2, DOUGLAS DRAWING NUMBER 5655068. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17, 18. FOUNDSDR SIMA200614501Rib · damagedDURING HMBV, FOUND RUDDER 1 LIGHTNING HOLE FLANGE DAMAGED. REMOVED AND REPLACED RIB IAW SRM 57-40-03. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
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