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 QXEA0101122Bearing · loosePDX - RIGHT-HAND AILERON INBOARD HINGE BEARING HAS RADIAL PLAY. REPLACED IAW DHC-8 MM 20-21-52 AND TASK CARD 9200001, 1-4.SDR P2EA01109Skin · delaminatedSJO - DURING C-CHECK, FOUND LEFT WING AILERON UPPER SKIN WITH DENTS AND LOWER SKIN WITH DELAMINATION AT WBL 480. REPAIRED LEFT WING AILERON P/N 65-46454-23A, S/N 555 DUE TO DELAMINATION BETWEEN WBL STATION 471 AND 486 IAW COOPESA EO NR COO-CMP-3-57-259-01 DATSDR P2EA01098Skin · delaminatedSJO - DURING C-CHECK, FOUND LEFT WING AILERON UPPER SKIN WITH DENTS AND LOWER SKIN WITH DELAMINATION AT WBL 480. (M)SDR AUS20010837Doubler · cracked(AUS) RT AILERON DOUBLER CRACKED.SDR CA010625013Doubler · cracked(CAN) DURING ANNUAL INSPECTION CRACKS WERE NOTED ALONG THE BEND RADIUS OF PARTS (REFER PHOTOS ATTACHED). SUSPECT DAMAGE WAS CAUSED FROM CONTROLS NOT BEING PROPERLY SECURED ALLOWING AILERONS TO WORK UP ANDDOWN DURING WINDY CONDITION S._P/N'S 66767-00 & 66767-01SDR CA010625016Hinge Bracket · misinstalled(CAN) PILOT FOUND AILERON SECURED ONLY BY OUTBOARD HINGE AND PUSHROD DURING WALK AROUND INSPECTION. THE SCREWS FOR THE INBOARD AND MIDDLE HINGE BRACKETS WERE IN PLACE, BUT NOT THROUGH THE BRACKETS. THE AILERON WAS REMOVED IN NOV 98 FOR PAINT. THE A/C WENT THROSDR ABXA010245Angle · crackedRIGHT INBOARD AILERON ON OUTBOARD TRAILING EDGE CRACKED. REPAIRED AREA IAW DAC DWG 5705334, DC8 SRM 51-1-8, 51-1-24, AND 51-1-21.SDR MWEA010771Skin · dentedLEFT AILERON UPPER SURFACE HAS DENT. EVALUATE AND REPAIR.SDR MWEA010770Skin · dentedLEFT AILERON UPPER SURFACE HAS DENT. EVALUATE AND REPAIR.SDR MWEA010769Skin · dentedRIGHT AILERON UPPER SURFACE HAS DENT. EVALUATE AND REPAIR.SDR GTIA010395Aileron · crackedFLL - FLT 1181 - RIGHT AILERON T/E BETWEEN BOTH TRIM TABS HAS 3 INCH CRACK IN FAIRING. CLEANED AREA AND APPLIED SPEED TAPE PER MD-80 SRM 51-02 PAGE 1 PARA A ITEM ON CARRY OVER REFERENCE CONTROL NR 002000-2. REMOVED AND REPLACED RT WING AILERON TRAILING EDGE SDR GTIA010930Attach Angle · crackedFTW - RIGHT AILERON INBOARD LOWER FLANGE CRACKED. REMOVED NOSE CAP ATTACHING ANGLE IAW SRM MD-80 51-30-2. FABRICATED ATTACH ANGLE IAW MD80 SRM 51-10-2. (M)SDR UPS01835876Skin · corrodedINSPECTION TYPE:C1,3 LT I/B AILERON FWD UPPER SKIN CUTOUT AT XA 458 IS CORRODED BEYOND LIMITS. REPAIRED SKINSDR 2001F00046Skin · crackedDURING A SCHEDULED PHASE INSPECTION THE LEFT AILERON WAS REMOVED. UPON REMOVAL THE LEADING EDGE SKIN AT THE WEIGHT ATTACHMENT SCREWS WAS FOUND CRACKED. THIS HAD ALLOWED THE SKIN TO CRACK ABOVE AND BELOW A SCREW APPROX. .5000. THE RIGHT AILERON WAS ALSO REMOSDR SDRS2001001Skin · crackedDURING SCHEDULED INSPECTION, TOP OF THE AILERON JUST OUTBOARD OF THE INNERMOST HINGE POINT ALONG THE LAP JOINT WAS FOUND TO BE CRACKED. CRACK WAS APPROX 4.5 INCHES LONG AND HAD BEEN CONCEALED UNDER THE PAINT. REPLACED THE AILERON WITH A SERVICEABLE PART.SDR USAA010495Hinge Fitting · crackedCLT - FOUND HINGE CASTING CRACKED .5 INCH, RT AILERON, NR 2 HINGE SUPPORT CASTING, LOWER OUTBOARD PANEL. REMOVED AND REPLACED CASTING PER BOEING DRAWING NR 65-63445-1. (M)SDR F3LA200100056Aileron · delaminatedPRIOR TO DEPARTURE, MAINTENANCE REPORTED OTBD SIDE OF RT AILERON DELAMINATED. REPLACED AILERONS IN LT AND RT POSITIONS PER MM 27-11-11, RIGGED AILERONS, AND PERFORMED OPERATIONAL CHECK PER MM 27-11-11.SDR UPS01235791Support · corrodedINSPECTION TYPE:C, O/B AILERON LT WING, ALL HINGE SUPPORTS ON REAR SPAR OF AILERON SHOW EVIDENCE OF CORROSION. LT O/B AILERON REMOVED IAW MM 27-10-31, NEW AILERON INSTALLED IAW MM 27-10-31.SDR USAA010549Aileron · crackedPIT - FOUND RIGHT AILERON CRACKED .5 INCH BY .5 INCH, AILERON FRONT SPAR UPPER FLANGE AT NR 1 HINGE ACCESS. INSTALLED WET LAYUP WITH A 230 CURE WITH ONE EXTRA PLY PER SRM 51-70-17, EA 70844. (M)SDR SWIA972509Fairing · departedIN FLIGHT, FELT STRANGE VIBRATION FOR A FEW SECONDS. UPON CONDUCTING POST FLIGHT INSPECTION, FOUND A SECTION OF UPPER AILERON FAIRING MISSING. REMOVED DAMAGED LEFT AILERON UPPER FAIRING AND REPLACED WITH SERVICEABLE UNIT.SDR ZW0A0100604Skin · crackedHAIL DAMAGE CAUSED H-SHAPE CRACK IN RT AILERON, 17 INCHES FROM OTBD EDGE AND 3.5 IN FROM THE T/E CRACKS ARE .75 IN LONG. RT AILERON CRACK REPAIRED PER SRM 51-70-1A, NUMBER 11. CHECK-C 2-5-01 JFK.SDR ZW0A0100603Skin · crackedDENTS DUE TO HAIL DAMAGE WERE FOUND ON LT AILERON UPPER SURFACE, FWD OF THE INBD TAB, HAD CRACK 1 INCH LONG. REPAIRED PER SRM 57-00-00 FIG 201, AND COMPUTER BALANCE ACCOMPLISHED. NO CHECK-C.SDR 20010517CW001Bearing · defectiveDURING A RESENT MAINTENANCE CHECK, AIRCRAFT PAINT AND REFURBISH, BOTH AILERONS WERE REMOVED FOR PAINT/BALANCE CHECK. THE BEARINGS WERE FOUND DEFECTIVE. PROBABLE CAUSE: BEARINGS WERE DRY AND WERE VERY DIFFICULT TO MOVE, DUE TO LACK OF LUBRICATION.SDR SWAA011018Skin · delaminatedON WALKAROUND, FOUND LT WING AILERON SKIN DELAMINATED ON UPPER AND LOWER SURFACE, OUTBD END. REMOVED AND REPLACED AILERON PER MM.SDR DHL2001806591Rib · crackedC-CHECK - LT WING AILERON INTERIOR LATERAL RIB ACCESS DOOR FRAME CRACKED 4 INCHES, STA XA 425. REMOVED LATERAL RIB ACCESS DOOR FRAME IAW SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AILERON INTERIOR LATERAL RIB ACCESS DOOR FRAME AT STA XA 425 IAW SRM 51-1SDR P5CA0100517Balance Weight · corrodedLEVEL 1 CORROSION FOUND ON BALANCE WEIGHT ONE LEFT OUTBOARD AILERON NR 3 POSITION. REPAIRED PER S/L 747-55-07.SDR DHL2001740002Doubler · looseNR 19. LT WING TOP AILERON REPAIR IS COMING LOOSE FWD. AND INBD NR 7 SPOILER(DOT) RII CORRECTIVE ACTION: ACOMPLISHED REPAIR IAW AERONAUTICAL SOLUTIONS REPORT 00-003 IR 03-26-01 AND SRM 51-30-02.SEE ITEM 9M FOR REPLACEMENT INSTRUCTIONS. INTERIM REPAIR INSTALLEDSDR C2XA01TY055Attach Fitting · gougedTYS DURING A SCHEDULED INSPECTION THE RIGHT HAND AILERON TO PCA ATTACH FITTING WAS FOUND GOUGED AND CHAFED. MAINTENANCE REMOVED AND REPLACED THE ATTACH FITTING IAW EMB GST-0903/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OSDR C2XA01TY046Bracket · gougedTYS DURING A SCHEDULED INSPECTION THE LEFT HAND AILERON ATTACHMENT BRACKET WAS FOUND TO BE GOUGED. MAINTENANCE REPAIRED THE BRACKET IAW EMB GST-085/01, THE REPAIR WAS FOUND SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR 20010417CW013Skin · crackedDURING PHASE 2 INSPECTION, FOUND 6 INCH CRACK AT TOP AILERON SKIN. SKIN WAS CLOSE TO FAILURE.SDR QXEA0100384Skin · delaminatedYYC-LEFT HAND AILERON TRAILING EDGE HAS 5 DISBONDS FROM OUTBOARD END AT EXITING DOUBLER ON TOP SKIN. REPAIRED IAW FOKKER SRM 51-70-00, PAGE 13 AND SRM 57-50-41, PAGE 1.SDR QXEA0100383Skin · delaminatedYYC-LEFT HAND AILERON TRAILING EDGE HAS DELAMINATION FROM OUTBOARD END AT EXITING DOUBLER. REPAIRED IAW FOKKER SRM 51-70-00, PAGE 14 AND SRM 57-50-41, PAGE 1.SDR CA010313028Skin · cracked(CAN) WHEN CHECKING SB 57-3148 IT WAS NOTICED THAT THIS AILERON WAS ALSO CRACKED AS PER SB 57-3148. KIT 109-4011-1 INSTALLED.SDR CA010313027Skin · cracked(CAN) ON INSPECTION IT WAS NOTICED THAT THE UPPER SKIN INBOARD WAS CRACKED UNDER THE LAP 1.50 INCH LONG. THE SKIN WAS REMOVED AND NEW BEECH SKIN INSTALLED. LT AILERON.SDR DHL2001806625Skin · dentedC-CHECK - RT OUTBD AILERON UPPER SKIN SURFACE DENTED BETWEEN STA XRS 640-660. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. REMOVED DAMAGED SKIN IAW DHL EO O10313, EO 2411, EO 2001078. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN (ALCSDR CA010323008Skin · cracked(CAN) WHEN CHECKING SB 57-3148 IT WAS NOTICED THAT THIS AILERON WAS ALSO CRACKED AS PER SB 57-3148. KIT 109-4011-1 INSTALLED.SDR 2001UALA00200Skin · damagedTHE AILERON SKIN IS DAMAGED AND STRETCHED. REPLACED UPPER AND LOWER AILERON SKIN PER BAC DWG 65-21766 AND SRM 51-30-2. REBALANCED SURFACE PER SRM 51-80-04.SDR RAIA00102006Fairing · damaged5391-EWR- DURING TAXI OUT CREW REPORTED RIGHT AILERON TIP FAIRING DAMAGED. CREW RETURNED TO GATE. MAINTENANCE INSPECTED, PERFORMED HIDDEN DAMAGE INSPECTION, AILERON TRAVEL/DEFLECTION CHECK. MAINTENANCE REPLACED RIGHT AILERON TIP FAIRING.SDR 20010328CW007Hinge Bracket · wrong partFOUND ON INSPECTION, OUTBOARD RIGHT AILERON NOT STREAMLINED WITH TRAILING EDGE OF WING (APPROX .2500 HIGH) INVESTIGATION REVEALED INCORRECT OUTBOARD HINGE BRACKET INSTALLED DURING PREVIOUS WING REPAIR CAUSED BY INCORRECT PRINT IN 414 PARTS CATALOG. THE HINGESDR ABXA010057Aileron · corrodedLEFT AILERON WAS CORRODED. MAINTENANCE INSPECTED AND REPLACED THE AILERON IAW DC-9 MAINTENANCE MANUAL.SDR QXEA01000257Skin · tornPDX-LEFT HAND AILERON HAS LOWER SKIN TEAR AT TRAILING EDGE OF INBOARD TRIM TAB ATTACH POINT. REPAIRED IAW DHC-8 RD8-27-005.SDR ASAA0110077Skin · crackedPHX - DURING SCHEDULED D-CHECK, FOUND LEADING EDGE OF LEFT AILERON CRACKED. REPAIRED PER EA. (M)SDR DHL2001712519Structure · crackedC-CHECK, LT WING TRIM TAB L/E PART FROM EXTERNAL AILERON SHOWS CRACK .25 INCH. REMOVED LEADING EDGE FROM TRIM TAB IAW SRM 51-10-2, PAGE 1 AND 2. FABRICATED NEW LEADING EDGE WITH ALCLAD 2024, T3, 0.020 INCH IAW SRM 57-20-03, FIG 2. TREATED AND PRIMED IAW SRMSDR 20010409SG003Skin · delaminatedRIGHT AILERON UPPER SURFACE DELAMINATED 40 INCHES INBOARD OF OUTBOARD END 6 INCHES FORWARD OF TRAILING EDGE. REPAIRED IAW SRM. (M)SDR UPS01234802Skin · crackedINSPECTION TYPE:N/A, LT OUTBOARD AILERON HAS DELAMINATION AND .25 INCH CRACK AILERON REMOVED WD 66470 INSTALLED LT OUTBOARD AILERON TO STEP D (4) MM 27-10-31. OK FOR SERVICE.SDR MWEA010124Skin · corrodedRIGHT AILERON UPPER OUTBOARD SKIN JUST FORWARD OF STATIC WICK HAS A SPOT OF CORROSION. FABRICATED AND INSTALLED DOUBLER.SDR HNAA0100007Housing · crackedCRACK FOUND IN AILERON QUADRANT MOUNTING BRACKET/HOUSING ON LOWER OUTBOARD CORNER RUNNING TO THE FIRST RIVET THEN .25 INCHES INBOARD OF RIVET TOWARDS THE NEXT RIVET. CRACK IS TO BE EDDY CURRENT INSPECTED EVERY 70 HOURS AND REPAIRED WITH IN 500 HOURS PER PIEDMSDR TWAA0101127Skin · delaminatedDURING CHECK-C MAINT THE RT WING OUTBOARD AILERON AT OUTBOARD END, BOTTOM 4 INCH BY 6 INCH AREA DELAMINATED. CLEANED AND BONDED FWD EDGE OF CONDUCTIVE FRAME WITH BMS 5-95 PER MM 57-51-03.SDR ASAA0040150Fitting · gougedSEA - DURING C-CHECK INSPECTION, FOUND RIGHT AILERON INBOARD HINGE FITTING IS GOUGED FROM CONTACT WITH SUPPORT FITTING ON AIRCRAFT. REPAIRED IAW ASA EA 2710-01056. (M)SDR CA010102006Aileron · damaged(CAN) ON THE RAMP IN ATL, NOTICED THAT THE RIGHT AILERON LOWER SURFACE LEADING EDGE HAD CONTACTED THE WING LOWER SKIN TRAILING EDGE, CAUSING DAMAGE TO THE AILERON LOWER ACCESS PANELS AND WING TRAILING EDGE SKIN REMOVABLE PANEL. IT SHOULD BE NOTED HERE THAT NO
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