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 = '5751' 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 = '5751' 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 MALA060394Skin · damagedLEFT AILERON SUSTAINED HAIL DAMAGE WS 307, 11.75 INCHES FROM TRAILING EDGE. REPAIRED IAW EOS51031.SDR MALA060393Skin · damagedLEFT AILERON SUSTAINED HAIL DAMAGE WS 299.5, 11.55 INCHES FROM TRAILING EDGE. REPAIRED IAW EOS51031.SDR MALA060396Skin · damagedLEFT AILERON SUSTAINED HAIL DAMAGE WS 328.75, 9 INCHES FROM TRAILING EDGE. REPAIRED IAW EOS51031.SDR MALA060387Skin · damagedRIGHT AILERON SUSTAINED DAMAGE WS 407 2.5 INCHES FROM TRAILING EDGE. REPAIRED IAW EOS51031.SDR MALA060386Skin · damagedRIGHT AILERON SUSTAINED HAIL DAMAGE WS 395 8.5 INCHES FROM TRAILING EDGE. REPAIRED IAW EOS51031.SDR MALA060385Skin · damagedRIGHT AILERON SUSTAINED HAIL DAMAGE WS 367.5, 6 INCHES FROM TRAILING EDGE. REPAIRED IAW EOS51031.SDR MALA060384Skin · damagedRIGHT AILERON SUSTAINED HAIL DAMAGE WS 339, 9.5 INCHES FROM TRAILING EDGE. REPAIRED IAW MESABA EOS51031.SDR MALA060382Skin · damagedRIGHT AILERON SUSTAINED HAIL DAMAGE WS 686.5, 5 INCHES FROM TRAILING EDGE. REPAIRED IAW MESABA EOS51031.SDR MALA060383Skin · damagedRIGHT AILERON SUSTAINED HAIL DAMAGE WS 404, 1.75 INCH FROM TRAILING EDGE. REPAIRED IAW MESABA EOS51031.SDR MALA060381Skin · damagedRIGHT AILERON SUSTAINED HAIL DAMAGE WS 406.5 6.75 INCHES FROM TRAILING EDGE. REPAIRED IAW MESABA EOS51031.SDR MALA060376Skin · damagedRIGHT AILERON SUSTAINED HAIL DAMAGE WS 397, 3.25 INCHES FROM TRAILING EDGE. REPAIRED IAW EOS51031.SDR MALA060380Skin · damagedRIGHT AILERON SUSTAINED HAIL DAMAGE WS 367.5 6 INCHES FROM TRAILING EDGE. REPAIRED IAW MESABA EOS51031.SDR MALA060379Skin · damagedRIGHT AILERON SUSTAINED HAIL DAMAGE WS 362.5 7.5 INCHES FROM TRAILING EDGE. REPAIRED IAW MESABA EOS51031.SDR MALA060378Skin · damagedRIGHT AILERON SUSTAINED HAIL DAMAGE WS 318 7.75 INCHES FROM TRAILING EDGE. REPAIRED IAW MESABA EOS51031.SDR MALA060377Skin · damagedRIGHT AILERON SUSTAINED HAIL DAMAGE WS 686.5 5 INCHES FROM TRAILING EDGE. REPAIRED IAW MESABA EOS51031.SDR IXXA06SMN167SSkin · crackedDURING C CHECK, FOUND LEFT WING L/E SKIN CRACKED ON INBOARD AILERON, AT STATION XA 480.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-8-1 FIG 1. REMOVED DAMAGED SKIN IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21. FAB`D NEW SKIN IAW DC-8 SRM 57-8-1 FIG 1 ITEM E.SDR 2006FA0000526Aileron · crackedDURING A PHASE 1,2,3,4 INSPECTION THE RT AILERON WAS FOUND TO BE CRACKED AT THE LEADING EDGE IN THE AREA OF ATTACHMENT POINTS FOR THE WEIGHTS. THE SKIN WAS REMOVED AND REPLACED. HAD SEVERAL CRACKED AILERONS IN OUR OTHER AIRCRAFT BOTH LT AND RT CRACK IN THIS ARSDR IXXA06SMN151SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD AILERON LEADING EDGE SKIN DENTED, AND CRACKED AT STATION XA 475.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-8-1 FIG 1. REMOVED DAMAGED SKIN IAW DC-8 SRM 57-1-0 PAGE 1, DC-8 SRM 51-1-21. FABRICATED SDR MALA060332Skin · damagedHAIL CONTACT DAMAGE ON LT AILERON 33 1/4" OB ON LEADING EDGE 2" AFT OF LEADING EDGE AND ALSO AT STA 390.82, 2" FROM AILERON TRAILING EDGE. DAMAGE REPAIRED IAW EOS#51031.SDR MALA060341Skin · damagedRIGHT AILERON SUSTAINED DAMAGE FROM HAIL. TWO DENTS REQUIRED REPAIRS. FIRST DENT DAMAGE MEASURES 1.0 INCH IN DIAMETER AND .006 INCH IN DEPTH, LOCATED 5 3/4 INCH FROM TRAILING EDGE AND AT STATION 352.64. SECOND DENT DAMAGE MEASURE 1/2 INCH IN DIAMETER AND .0SDR MALA060345Skin · damagedLEFT AILERON SUSTAINED DAMAGE FROM HAIL. TWO DENTS REQUIRED REPAIRS. FIRST DENT DAMAGE MEASURES 5/8 INCH IN DIAMETER AND .008 INCH IN DEPTH LOCATED 7 3/4 INCH FROM TRAILING EDGE AND AT STATION 409.7. SECOND DENT DAMAGE MEASURES 5/8 INCH IN DIAMETER AND .005SDR MALA060327Skin · dentedHAIL CONTACT DAMAGE ON RIGHT AILERON CAUSED DENT IN UPPER COMPOSITE SKIN. DENT WAS .75 IN DIA AND .75 IN LENGTH AND .007 DEEP. LOCATED 67.625 INCHES FROM I/B AILERON EDGE AND 5.375 INCHES FROM TRAILING EDGE. DAMAGE REPAIRED WITH A COLD BOND WET LAYUP IAW SASDR MALA060323Skin · damagedDURING 4K CHECK IN BNA FOUND RT AILERON LEAKING EDGE 651DB HAS MINOR COMPOSITE DAMAGE AND HAS BEEN REPAIRED IAW MESABA EO S51031.SDR AWXA200600840Support Fitting · damagedSAL - DURING C5 CHECK DISCOVERED ELONGATE HOLE ON THE FRAME SUPPORT FITTING OF THE LT AILERON AT RIB 23. MAINTENANCE REMOVED AND INSTALLED NEW FRAME SUPPORT FITTING ON THE LT AILERON AT RIB 23 IAW AIRBUS 320 SRM 51-72-11.SDR AWXA200600839Channel · crackedSAL - DURING C5 CHECK DISCOVERED CRACK ON TRAILING EDGE (T/E) CHANNEL ON THE LT WING, T/E AILERON. MAINTENANCE REMOVED AND INSTALLED NEW T/E CHANNEL ON THE LT WING, T/E AILERON IAW AIRBUS 320 SRM 51-72-11.SDR QXEA200601307Skin · dentedYYC - C4 LEFT HAND AILERON, TOP SKIN DENTED, MID AREA AT STATION YW 457. REPAIRED IAW SRM 57-60-21 AND SRM 57-60-71.SDR QXEA200601242Skin · chafedPDX - C3 CHAFFING ON LOWER RIGHT AILERON LEADING EDGE. REPAIRED IAW SRM 57-61-01 AND SRM 51-21-11.SDR MALA060275Skin · dentedRT AILERON, P/N 7257610-622, S/N 0245, LOWER OUTBOARD SKIN IS DENTED AND HAS BEEN REPAIRED IAW MESABA EO#S51031. REF: EAMS WORK ORDER 213767 TASK 6504.SDR SWIA200616584Bushing · wornON DESCENT FROM FL250 WITH TORQUE AT 61 PERCENT A VIBRATION WAS FELT. REPLACED LEFT AILERON HINGE AND BUSHING IAW MM 57-00-00, REMOVED AND REPLACED RIGHT AILERON TRIM TAB IAW EMB 120 MM 27-72-02.SDR DHL2006764516Skin · dentedNR 016062 LT WING IB AILERON UPPER SKIN HAS NUMEROUS DENTS. REMOVED AND REINSTALLED LH IB AILERON AND TAB IAW MM 27-10-01 AND MM 27-10-11. FABRICATED NEW SKIN USING MAT 2024T3 .040 PO NR 9003189 DIM 41 .2500 X 22.2500 INCH IAW SRM 57-50-2 FIG7 AND SRM 51-30-5SDR DU4R2006368Aileron · dentedS/O 304001) N/R 24581, RT WING IB AILERON NUMEROUS DENTS. REMOVED DENTED SKIN. FABRICATED AND INSTALLED REPAIR SKIN DOUBLER 5.5 INCH X 5.5 INCH FROM 2024-T3 .016 AND 2 EA. SKIN REPAIR DOUBLER 24 INCH X 54 INCH FROM 2024-T3 .040 IAW SRM 51-10-2 AND 51-30-2.SDR 06FDEA1351Skin · delaminatedLEFT WING OUTBOARD AILERON TRAILING EDGE INBOARD UPPER SURFACE FOUND DELAMINATED. LEFT WING OUTBOARD AILERON TRAILING EDGE INBOARD UPPER SURFACE REPAIRED AS PER FEDEX EA NR 1-5790-95674, TITLE: WINGS, OUTBOARD AILERON, REPAIR LEFT OUTBOARD AILERON DELAMINASDR MALA060240Skin · delaminatedDURING 2 YEAR CHECK IN BNA FOUND LT AILERON P/N 7257610-621, S/N 0260, IS DELAMINATED ON LOWER SURFACE, 38" FROM INBOARD END AND 2.5" FORWARD OF TRIM TAB. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO#S57115. REF: EAMS WORK ORDER 213710 TASK 5505.SDR CA060406009Arm · looseMASS BALANCE ARM EXHIBITED LOOSENESS, AND WAS MOVING IN EXCESS OF 1/2 INCH AT THE END WHEN MOVED WITH MINIMAL HAND PRESSURE. AILERON DISASSEMBLED, FASTENERS REPLACED AND RETURNED TO SAFE AND FIT CONDITION IAW TYPE DESIGN.SDR 2006FA0000394Spar · corrodedAILERON SPARS FOUND EXCESSIVE CORROSION UNDER ALL 3 HINGES. NEEDED TO REPLACE SPAR ON BOTH LT AND RT AILERONS BEFORE RECOVERING AILERONS. (K)SDR 06FDEA1241Skin · dentedDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: LT WING, INBOARD AILERON, LOWER SIDE, STA XIA = 347-341: 3EA DENT IN AREA 3.4 X 3.7 INCH, MAX DEPTH .190 INCH. NO DAMAGE FOUND AT RIB LOCATION. ACCOMPLISHED LT INBOARD LOWER SKIN REPAIR IAW SRM 57-10-0SDR IXXA06SMN102SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, LT WING OUTBOARD AILERON L/E DENTED, XA 662.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-8-1 FIG 4. PERFORMED NDT INSPECTION DETECT CRACK IAW DC-8 NDT SPM PART 06-10-01-001. CRACK FOUND 0.250 LENGTH ENCLOSED SMN FORM 242-2.SDR DHL2006750521Skin · gougedFOUND L WING I/B AILERON UPPER SKIN IS GOUGED AT WS 410. CUT OUT DAMAGED AREA DIM 2X2 AND FABBED REPAIR DOUBLER FROM MAT USE 2024 T3 .04 PO 9003055 AND DIM 5 1/3 BY 4 IAW B727 SRM 57-50-2 FIG NR 7 AND 57-50-5 FIG 5. TREATED AND PRIMED IAW B727 SRM 51-10-2. SDR QXEA200600732Structure · wornYYC - C4 LEFT HAND AILERON INPUT ROD AFT ATTACHMENT POINT TO AILERON IS WORN. REPAIRED IAW RD 8-57-087, ISSUE 2, DHC-8-200 SRM 57-60-71, DHC-8-200 AMM 27-12-00-330-801, PARAGRAPH 3.SDR ABXA060150Support · crackedRIGHT INBOARD AILERON MANUAL REVERSION MECHANISM CRACKED AT UPPER MOUNT HOLE. REMOVED AND REPLACED SUPPORT ASSEMBLY ON AILERON MANUAL REVERSION MECHANISM IAW DC8 OHM 27-6-2.SDR 2006UALA00468Attach Fitting · misdrilledRIGHT WING INBOARD AILERON, INBOARD SECTION LEADING EDGE ATTACH FITTING MISDRILLED. S/D* THE SUBJECT FITTING WAS MISDRILLED DURING INSTALLATION. REPAIRED PER TIMCO REO-G11452.SDR QXEA200600767Spar · damagedYYC C4, LEFT HAND AILERON AFT SPAR, ATTACH POINT BRACKET FITTINGS FOR SPRING TAB ATTACH ARE ELONGATED. REPAIRED IAW RD 8-57-048, ISSUE 1, PAGE 2, NOTE 3.SDR UPS06846527Fitting · crackedR/WING TE STA XW5 FITTING FOR SPOILER ATTACHMENT CRACKED. FABRICATED REPLACEMENT FITTING IAW SAA EA NR 008-5730-01-A0107 AND UPS RA DC8-57-20157.SDR 06FDEA0868Finger Doubler · corrodedLT OUTBOARD AILERON, I/B UPPER SKIN FINGER DOUBLERS DELAMINATED WITH CORROSION. FABRICATED AND INSTALLED NEW SKIN IAW DC 10 SRM 51-35-01 VOL II AND DAC DWG ARC1110, AND EA 8-5710-92633 WINGS - LT AILERON SKIN CORRODED.SDR MALA060058Structure · damagedRT WING AILERON SUSTAINED DAMAGE BY CONTACT WITH A GROUND SUPPORT VEHICLE. CONTACT DAMAGE STARTED JUST OUTBOARD OF THE TRAILING EDGE STATIC WICK, DEFORMATION OF THE AILERON STRUCTURE EXTENDED APPROXIMATELY 8 INCHES FORWARD FROM THIS POINT. RIVET HEADS ON THESDR ARWA20060217Skin · corrodedDURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND; I/B AILERON BETWEEN XA 565 AND SA 542 LOWER SKIN WITH CORROSION. REMOVED SKIN AND BONDED DOUBLER AND REPLACED BY SOLID SKIN BETWEEN XA 542 AND XW 563 IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-07/05. ISSSDR ARWA20060212Skin · damagedDURING "C" CHECK INSPECTION, LT O/B AILERON BETWEEN XA 678 AND XA 685 LOWER SKIN RIVETS SHEARED. REMOVED LT O/B AILERON PLATING BETWEEN XA 662 & XA 724 AND REPLACED WITH SOLID SKIN IN ACCORDANCE WITH DRAWING NR AIPSAC-N784AL-09/05, ISSUED FAA FORM 8110-3 APPRSDR CALA0600028Beam · crackedTHE LT AILERON BEAM WAS FOUND CRACKED AT WS 538, THE CRACK WAS STOP DRILLED PER ECRA 5752-01230. A DIP WAS ISSUED TO REINSPECT THE AREA AT 50 FLIGHT HOUR INTERVALS UNTIL A PERMANENT REPAIR IS PERFORMED PER ECRA 5752-01230.SDR DHL2006763501Fitting · brokenS/O 284007 N/R 031639 - LT OUTBD AILERON TAB HAS EXCESSIVE PLAY. OPEN LT OUTBD AILERON SKIN, FOUND INTERNAL TAB MOUNT FITTING BROKEN. REMOVED AND REPLACED FITTING, BALANCED IAW B727 SRM 51-80-4 AND 51-30-2.SDR QXEA200600313Structure · wornYYC - C3 RIGHT AILERON OUTBOARD TOP LEADING EDGE WORN BY SEAL, UNDER PANEL 698CT. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.
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