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 = '5700' 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 = '5700' 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 06FDEA0562Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT NR 1 LEADING EDGE SLAT , LOWER AFT SURFACE WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-50-3 FIG.1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPASDR CA060228014Wing · misinstalledDURING INSPECTION, FOUND INBD EDGES OF BOTH LT AND RT FLAP ASSEMBLIES WERE TOUCHING FUSELAGE IN FULL UP POSITION. MX DEPART COMPLETED INSPECTIONS OF FOLLOWING AREAS FLAP ATTACHMENT, FLAP RIGGING, FLAP STRUCTURE FOR BENDING OR WARPING, STRUCTURE OF WINGS FOR BSDR 06FDEA0530Repair · misinstalledFOUND REPAIR LOCATED ON LT INBD FLAP, LT WS 277 - WS 289. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOSDR 06FDEA0531Repair · unknownFOUND REPAIR LOCATED ON RT INBD FLAP, RT WS 359-409. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX EA 6-5710-95695 AND RAS/DABRE/700SDR 2006UALA00220Structure · pilot errorLEFT WING STRUCK PARKED AC DURING TAXI OUT. WHILE TAXIING OUT, THE SUBJECT AIRCRAFT'S LEFT WING TIP STRUCK THE HORIZONTAL STABILIZER OF A PARKED 767 AIRCRAFT. THE COLLISION DAMAGED THE SUBJECT AIRCRAFT'S WINGLET, THE UPPER FIXED LE SKIN, THE FRONT SPAR UPPER SDR CA060321014Bar · corrodedDURING A VISUAL INSPECTION OF THE OTTER TIE BAR ASSEMBLY A LARGE COLLECTION OF DEAD FLY CARCASSES WERE FOUND CRAMMED INTO THE "U" CHANNEL SECTION OF THE TIE BAR. ON FURTHER INVESTIGATION WITH THE BUG BIOMASS IT BECAME EVIDENT THAT THE BAR HAD STARTED TO EXFOLSDR 06FDEA0335Repair · misinstalledREPAIR LOCATED AT LEFT OUTBOARD AILERON OUTBOARD END T/E WEDGE REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED OLD REPAIR NOT WITHIN FAA APPROVED DATA. FABRICATED NEW WEDGE SECTION AND ZEE IAWSDR 06FDEA0332Repair · misinstalledFOUND REPAIR LOCATED LT WS270-280. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-42-11 FSDR 06FDEA0331Repair · unknownFOUND REPAIR LOCATED LT WS222-232. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS REMOVED FOUND SMALL DENT PERFORMED NDT INSPECTION , NO CRACKS FOUND DENT WAS FILLED AS PER SSDR QXEA200600425Panel · misdrilledON LT WING AT OUTER END OF PANEL 522BT THE WING LANDING HAS THE MOST FWD HOLE COUNTERSUNK ON EDGES. MAINTENANCE REPAIRED IAW EA 6-57-429, RD 8/4-57-611 AND NDTM PART 6, 51-00-02.SDR 06FDEA0295Repair · noneLT HORIZONTAL STAB INBOARD ELEVATOR UPPER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION REPAIR IAW SRM 55-10-00 FIG 8 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.SDR USAA060073Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, I/B END LWR SURFACE. SDA UPDATED AS REQUIRED IAW TR 57-50-26A, DEFECT SIZE: UNKNOWN.SDR USAA060074Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR I/B END UPPER SURFACE. UPDATED SDA AS REQUIRED IAW TR 57050-26A, DEFECT SIZE: 10 BY 4.SDR USAA060075Repair · unknownFOUND SLAT SKIN WITH PREVIOUS REPAIR LWR SURFACE AT I/B AUX TRACK. SDA UPDATED AS REQUIRED IAW TR 54-43-01, DEFECT SIZE: 12" BY 4".SDR USAA060042Repair · unknownPREVIOUS REPAIR UPPER IB T/E. UPDATED SDA AS REQUIRED IAW TR 57-42-02 DEFECT SIZE: 5" BY 5".SDR DHL2006572512Slat · crackedDISCREPANCY FOUND NR 111075; NR 2 SLAT RIB NR1 AT SLAT STA 234.0 IS CRACKED. REMOVED DAMAGED PART IAW SRM 51-30-2 AND FABBED NEW RIB AREA NR 2 SLAT RIB NR 1 SLAT 180 DIM 16 X 5 MAT USE 7075.0 0.40 PO 9001602 IAW SRM 57-50-2 FIG NR 2 AND 51-20-1 PART TREATEDSDR 06FDEA0098Repair · unknownFOUND LT WING SLAT NR 2 INT SKIN FOUND A FLUSH REPAIR DIM 5" BY 4.75" BY 5" XORS 264. REMOVED SLAT NR 2 LT, AND EXISTING REPAIRS, TRIMMED OUT PORTION OF INNER SKIN. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161061-3/N01061-3, F161061-5/N01061-5, F161061-7/SDR 06FDEA0080Repair · unknownFOUND PREVIOUSLY 2 REPAIRS INSTALLED ON LT WING TIP LOWER SURFACE WAS ACCOMPLISHED IAW SRM 57-20-5 FIG 1, BASED ON EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP ASDR 06FDEA0079Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT UPPER SURFACE OF LT WING TIP WAS ACCOMPLISHED IAW SRM 57-20-1 FIG 2, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBER AND SPACING, GENERAL WORKMANSHSDR 2006UALA00046Unknown · peelingLT WING NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE DAMAGED, PNL ON TOP OF WING JUST AFT OF NR 5 SLAT ALSO DAMAGED. ENGINEERING IS CONDUCTING ADDITIONAL INVESTIGATIONS FOR CAUSES OF THIS TYPE OF FAILURE. FAILURE OF THE LAMINATE ON WING. LE SLATS IS A SYSTEMICSDR 06FDEA00055Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT RT WING OB OF LANDING LIGHT WAS ACCOMPLISHED IAW SRM 57-30-4, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENERS NUMBER AND SPACING, GENERAL WORKMANSHIP ANDSDR 06FDEA00039Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT NR 2 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57- 50-3, FIG. 3, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, TYPE, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBER AND SPACING, GENERAL WORKMANSHIP,SDR 06FDEA00026Repair · unknownDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND: 1EA EXISTING REPAIR ON RT WING, STA 1159 BTW STR 28-29. REPAIR IS CONFORM TO SRM 57-20-00 FIG 6 SH 3 FOLLOWING EO 8-5100-7-5001 PT 2 CRITERIA.SDR 05FDEA04344Repair · unknownFOUND PREVIOUS REPAIR ON UPPER LEADING EDGE OF LEFT WING AT NR 3 LEADING EDGE SLAT WAS ACCOMPLISHED IAW SRM 57-30-4, FIG 1. BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL SDR 05FDEA04343Repair · unknownFOUND PREVIOUSLY REPAIR ON LT INBOARD FORE FLAP LEADING EDGE WAS ACCOMPLISHED IAS SRM 57-50-4, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS SDR 05FDEA04342Repair · unknownFOUND PREVIOUS REPAIR ON LT OUTBOARD FOREFLAP LEADING EDGE WAS ACCOMPLISHED IAW SRM 57-50-4, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENERS NUMBER AND SPACING AND GENERAL WORKMANSHIP, REPAIR SDR 05FDEA04341Repair · unknownFOUND PREVIOUS REPAIR ON LOWER SURFACE OF RIGHT INBOARD AFT FLAP WAS ACCOMPLISHED IAW SRM 57-50-4 FIG 5, PAGE 12, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPASDR 05FDEA04340Repair · unknownFOUND PREVIOUS REPAIR ON RIGHT WING NR 7 L/E SLAT WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 1 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR CLASSIFIED AS MAJOR PESDR 05FDEA04339Repair · unknownFOUND PREVIOUS REPAIR ON LEFT WING NR 1 KRUEGER FLAP FWD SURFACE WAS ACCOMPLISHED IAW SRM 57-50-3, FIG 2 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENERS SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR CLASSSDR 05FDEA04337Repair · unknownFOUND PREVIOUSLY REPAIR AT NR 5 KRUEGER FLAP WS 265.0 WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 3, BASED ON EXTERNAL EVALUATION CONSISTED OF LOCATION, SIZE, SHAPE, NUMBER OF FASTENERS AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS SDR 05FDEA04311Repair · unknownRT WING SLAT NR 2 FOUND DOUBLER REPAIR ON UPPER SKIN T/E OB SIDE DIM 3 INCHES BY 3 INCHES. REMOVED REPAIR IAW SRM 51-35-01 PAGE 13 AND SRM 51-33-01 PAGE 34/47. CLEANED AREAS AND REMOVED PART IAW SRM 51-41-01 VOL 2. PERFORMED INSPECTION IAW NDI SPM08. FOUNDSDR 2006FA0000009Strip · unserviceableDURING ANNUAL INSPECTION, WHILE INSPECTING THE AILERON CABLES, FOUND A FLAT SPOT ON THE LT AILERON CROSSOVER CABLE AT THE AILERON CABLE ABRASION STRIP ATTACHED TO A RIB ASSY LOCATED AT WING STA 71.19. FURTHER INVESTIGATION FOUND THE CABLE BEGINING TO FRAY. SDR 05FDEA04289Repair · noneRIGHT WING SLAT NR 6 STA XOS 860 HEATED AREA HAS AN EXTERNAL DOUBLER REPAIR DIM 10 X 6 INCHES. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 57-10-00 FIG 12 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 05FDEA04288Repair · unknownRT WING OUTBOARD FLAP LOWER SURFACE HAS A DOUBLER REPAIR ON TWO RIBS AT T/E PANEL BETWEEN STA XOF 580 AND XOF 588 DIM 13" BY 8". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 57-10-00 FIG 85 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-500SDR 05FDEA04286Repair · unknownFOUND LEFT WING NR 1 SLAT HAS AN EXTERNAL DOUBLER REPAIR AT THE LOWER AFT EDGE OF THE OUTER SKIN DIM. 8.5" BY 5". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 57-10-00 FIG 84 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2.SDR VNAA0512001Structure · lightning strikeEVIDENCE OF LIGHTNING DAMAGE WAS FOUND ON THE LT WINGLET TIP TRAILING EDGE DURING THE 50 HOUR SERVICE CHECK. MAINTENANCE COMPLIED WITH A LIGHTNING STRIKE INSPECTION. NO FURTHER DAMAGE WAS FOUND. A TEMPORARY REPAIR WAS PERFORMED ON THE LT WINGLET TIP TRAILINSDR CA051122001Nut · mismanufacturedTHE CREW WENT TO INSTALL A WING BOLT RETAINING NUT ON THE AIRCRAFT. IT WAS NOTICED THAT THE NUT WAS MISSING ONE OF THE TWO PLASTIC LOCKING DEVICES. IT APPEARS THE PLASTIC WAS NEVER INSTALLED IN ONE HOLE. THIS IS THE SECOND NUT THAT WAS FOUND WITH PROBLEMS. SDR DEBA401PP1Unknown · unknownAIRCRAFT WOULD NOT PASS THE BIT CHECK ON PREFLIGHT. CONTACTED NEAREST AUTHORIZED RAYTHEON SERVICE CENTER FOR SERVICE OF THE NITROGEN BOTTLE, BOTTLE WAS JUST AT THE BOTTOM OF THE GREEN. THE THOUGHT WAS THAT IT CAUSED A LOW PRESSURE INDICATION AND MADE THE BITSDR IXXA05SMN236SSkin · improperDURING C CHECK INSPECTION, RT OTBD FLAP UPPER SKIN HAS NON STANDARD REPAIR, STA XF 210.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4, TR#57-94, EO SEMAN # 20051288 DATED 09-28-05. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1SDR ASAA0570038Seal · chafedPAE - DURING C-CHECK, FOUND LOWER SKIN CHAFED AT NR 1 ENGINE PYLON AFT FAIRING UPPER BLADE SEAL JUST AFT OF FUEL CELL PANEL 532BB. REPAIRED IAW EA 5720-01272. (M)SDR ASAA0570040Seal · chafedPAE - DURING C-CHECK, FOUND LEFT WING LOWER SKIN CHAFED AT NR 1 ENGINE PYLON AFT FAIRING UPPER BLADE SEAL JUST FORWARD OF FUEL CELL PANEL 532 BB. REPAIRED IAW EA 5720-01272. (M)SDR ASAA0570039Seal · chafedPAE - DURING C-CHECK, FOUND RT WING LOWER SKIN CHAFED AT NR 2 ENGINE AFT PYLON FAIRING UPPER BLADE SEAL JUST FORWARD OF FUEL CELL PANEL 632BB. REPAIRED IAW EA 5720-01272. (M)SDR EIA2004142Skin · corrodedBS 1200, LBL 98.5, UPPER SKIN CENTER TANK HAS CORROSION. REMOVE DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-57-270-2.SDR EIA2004140Skin · corrodedSKIN AT BS 1140, LBL 98.58, LBL 110 AT BUTT JOINT OVER MID SPAR HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-57-269-2.SDR ARWA20040703Unknown · unknownAFTER APP TAKEOFF POWER HEARD BANG ON LEFT HAND SIDE WING. INSPECTED LEFT HAND WING IN ACCORDANCE WITH MM 57-00; NO OBVIOUS DEFECTS NOTED. ALSO INSPECTED LEFT HAND MAIN LANDING GEAR AND DOORS IN ACCORDANCE WITH MM 32-10-0, NO OBVIOUS DEFECTS NOTED. PERFORMESDR IXXA060444SFitting · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF219. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA0400047SVane · corrodedDURING ROUTINE C-CHECK INSPECTION FOUND RT WING L/E OB VANE CORRODED, ELONGATED HOLES AROUND STA. XOLDS 6.224. REPAIRS WERE ACCOMPLISHED IAW DWG V22-RO6, REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 21, REMOVED CORROSION IAW SRM 51-1-8 PAGE 11 1SDR 2004FA0000009Flying Wire · brokenUPPER LT FLYING WIRE TAIL BROKE ABOUT 6 INCHES FROM TOP ATTACH POINT. WHILE FLYING, FLAT TYPE WIRE.SDR 2003F00442Attach Angle · crackedAT C-CHECK, FOUND CRACK AT NLG WHEEL WELL AFT BULKHEAD CENTER TOP RIGHT STIFFENER BRACKET. REMOVED CRACK ANGLE. FABRICATED ANGLE. TREATED AND PRIMED. INSTALLED ANGLE AT NOSE LANDING GEAR WHEEL WELL AFT BULKHEAD CENTER RIGHT TOP. (M)SDR ABXA030113Flange · shearedFLAP INBOARD FIXED VANE CENTER TWO CAM ATTACH FITTINGS ON FLAP LEADING EDGE WERE SHEARED. REPLACED FITTINGS (9957536-13 AND 9957536-7) IAW DC-9 SRM 51-30-2.
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