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 SWIA201743522Hinge · gougedRIGHT BUTTE DOOR 694LB HAS A SMALL GOUGE AT INBOARD FIRST HINGE LUG. BLENDED OUT DAMAGE, NO DAMAGE ALLOWED ON HINGE FOUND TO BE OUT OF LIMITS. REPLACED HINGE IAW SRM 51-42-06SDR GTIA2017061701977Not Reported · corrodedLEFT WING CORROSION UPPER WING BETWEEN RIB 15 - 16. REPAIRED IAW EO 5721-1718.SDR GTIA2017061701996Not Reported · corrodedRT WING CORRODED UPPER WING BETWEEN FIB 14 - 15. REPAIRED IAW EO 5721-1719.SDR JGVR20170615001Tube · chafedLEFT WING LEADING EDGE RAM AIR TUBING IS CHAFED INTO FUSELAGE SKIN. FOUND DURING WING HEATED LEADING EDGE AND PLUMBING INSPECTION TASK 30-14-00-210 ON THE PHASE 5. BLENDED LEFT FUSELAGE FEED THRU DOUBLER AT THE LEFT WING ROOT AND INSTALLED FABRICATED FEED THRUSDR UIEA2017042600650Structure · crackedJ8 JUNCTION BOX ON LT WING LANDING GEAR CRACKED. CLEANED, PREPPED, REPAIRED, & REFINISHED J8 JUNCTION BOX IAW SRM 51-20-06, 51-70-06, AND AMM 51-24-22.SDR DALA2017060804559Fork · corrodedDURING C CHECK, CORROSION WAS NOTED UNDER THE FORK FITTING. COMPLIED WITH ERA 555745-14SDR 2017FA0000186Valve · intermittentWING LOW PRESSURE LIGHT ILLUMINATED INTERMITTENTLY AT LOW POWER SETTING. REMOVED AND REPLACED HP VALVE NR 2.SDR HYIA20170821001Rib · crackedDURING A ROUTINE INSPECTION, A CRACK WAS LOCATED AT RIB RT WS. 106.79. THE CRACK WAS 1.5 INCHES IN LENGTH, REPLACED THE RIB IAW MM.SDR UIEA2017020100137Structure · damagedRT WING TIP OTBD AFT EDGE CORNER FOUND BURNED. REPAIRED IAW RI-57-30-11689 REV A.SDR HYIA20170822001Rib · crackedDURING A ROUTINE INSPECTION, A CRACK WAS LOCATED AT RIB AT RT WS 106.79. THE CRACK ORIGINATED FROM A LOCK FASTENER. REPAIRED IAW MAINTENANCE MANUAL.SDR A6WA2016113044603Bracket · crackedBRACKET FOR FUEL FILL RECEPTACLE IS CRACKEDSDR 2016FA0000547Skin · corrodedCORROSION FOUND ON TOP OF THE LEFT AND RIGHT WINGS. BLENDED AREAS OF CORROSION IAW W.O. CS481707, AND DRAWINGS 1159WM40003 AND 1159SB40574. ULTRASONIC THICKNESS INSPECTIONS PERFORMED IAW WORK ORDERS 9161078, AND 10161107. NO FURTHER CORROSION NOTED.SDR DALA2016080305746Panel · damagedFOUND RIGHT MAIN LANDING GEAR FLAP CLOSEOUT SPRING PANEL DAMAGED. REMOVED AND REPLACED INBOARD BUTE DOOR AND BEAM ASSEMBLY IAW DWG 5936844.SDR COEA2016070819917Spar · corrodedRIGHT WING LOWER SPAR STRIP SLAT INBOARD OF LEADING EDGE 611 HAS FRETTING CORRODED. REPAIR IAW CETS-3309/16.SDR SCNA20160516049Fitting · crackedWHILE REMOVING LT T/E WEB, FOUND SEAL END FITTING TO BE CRACKED. LOCATED AND DRILLED NEW FITTING AND ASSEMBLED TO BULB SEAL.SDR R61A201605070369Bearing Race · damagedDURING HEAVY CHECK, TWO EACH FWD BEARING RACES PITTED ON FAIRING 523BB. MAINTENANCE R & R 2 EACH FWD BEARING RACES IAW SRM 51-43-02.SDR AXSA03/04/2016Structure · damagedTHE ACFT WAS SUBJECTED TO SEVERE TURBULENCE ON APPROACH. AFTER THE TURBULENCE EXCESSIVE AILERON TRIM WAS REQUIRED. VISUAL INSPECTION REVEALED WRINKLING OF BOTH INNER WINGS BETWEEN THE FUSELAGE & THE NACELLE.SDR SWIA201641956Panel · chafedPANEL 584EB CHAFED. REPLACED OUT OF LIMITS PANEL 584EB IAW SRM.SDR Q2SA20160214242Unknown · smokeON TAKEOFF ROLL, TOWER CALLED SMOKE FROM LT WING REJECTED TO AT 122 KTS. FIRE RESCUE INSPECTION REPORT, NO SMOKE FUEL FROM LT WING. BRAKE ENERGY WAS IN CAUTION RANGE.SDR DALA2015121007643Not Reported · crackedCRACKS EXISTING IN HOLES AFTER OVERSIZING TO .288 REPAIR C/W.SDR DALA2015120507391Duct · wornWEAR AT FUEL VENT DUCT, RT WING. EDGE OF CUTOUT ON Y=1211 AND LONGERON 23 TO 24 RT WAS REPAIRED IAW SRM 53-05, FIG 155, OPTION 1.SDR DALA2015120207336Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACESS PANEL 620CT. FOUND TO BE OUT OF LIMITS. REPLACED FUEL ACCESS PANEL IAW SRM 57-00-04.SDR 4M2S2015FA0000544Nut Plate · damagedRIGHT MLG FORWARD TRUNNION ASSY MOUNTING BOLTS LOOSE, 3 OF 4 BOLTS HAD VISIBLE GAPS BETWEEN BOLT HEADS AND TRUNNION ASSY. SIGNS OF FRETTING APPARENT BETWEEN TRUNNION ASSY AND MAIN SPAR WEB WERE ACCOMPANIED BY A SLIGHT GAP BETWEEN THE TRUNNION ASSY AND SPAR. SDR REXA2015100600940Panel · chafedPANEL 599AB HAS A DEEP GOUGE ON THE INBD EDGE OF THE PANEL. RECEIVED NEW PANEL 599AB, REFER TO MASTER PANEL BOOK M-212 PG 74 FOR REMOVAL & INSTALLATION. LOCATED, DRILLED & COUNTERSUNK NEW PANEL 599AB, PN 601R13440-1 IAW SRM 51-40-11-001-001-A01.SDR ASOA2015090813867Link · deterioratedLT AND RT REAR SPAR LINK TILTED/CONTRACTING CONDITION IAW EC/TC REO 670-53-41-177, ITEM 5. COMPLIED WITH ECTC REO 670-53-41-17701 PERMANENT DISPOSITION. LT AND RT REAR SPAR LINKS R & R IAW SB670BA-57-016. REFERENCE ECTC REO 670-53-41-177-01 FOR PERMANMENT DSDR DALA2015071304324Not Reported · damagedDENT AND TOOL DAMAGE ON RT WING L/E, XOS 248. THE WING L/E WAS REPAIR IAW SRM 57-06A, PARA 9. HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001.SDR DALA2015061403948Not Reported · crackedGROUP A, HOLE NR 1 HAS CRACK INDICATION AT .288, REWORKED.SDR DALA2015061403947Not Reported · crackedGROUP A, HOLE NR 1 HAS CRACK INDICATION AT .288, REWORKED ON AMDS 5724-01010-06.SDR CA150320003Screw · wrong part(CAN) CHECKING SB 57-4144, ALL THE SCREWS WERE REMOVED AND FOUND MANY WERE NOT THE CORRECT LENGTH. ALL SCREWS WERE REPLACED WITH NEW ONES IAW SB 57-4144.SDR UHLA2015021800135Structure · crackedRT WING STUB AT CENTER FUSELAGE II PRESSURE BULKHEAD TO SPAR III FASTENER HOLE CRACKED. HOLE REAMED TO .372" TO REMOVE CRACK, FAB AND INSTALLED OVERSIZED BUSHINGS EAW ETD2015-170-015818, REV A.SDR GTIA2014112501456Structure · damagedCREW REPORTED A LIGHTNING STRIKE AFTER DEPARTURE. DIVERTED, DECLARED EMERGENCY. EXTENSIVE DAMAGE FOUND ON ACFT. LSDR 3FMR20140903003Skin · corrodedRIGHT WING LOWER SKIN WAS FOUND CORRODED AROUND FRONT SPAR ATTACH FASTENERS LOCATED AT WING STA 509 - 519. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS. REPAIRED IAW DWG AMJN598AJ 3/14.SDR ASOA2014081511085Unknown · damagedWHILE PERFORMING SB 670BA-57-015 01 ON RT SIDE GO-NO-GO GAUGE GOES ALL THE WAY IN TOP AND BOTTOM HOLE LOCATIONS. REPAIRED IAW REO 670-57-21-721.SDR ASAA2013112596532Unknown · arcedPAX REPORTED ARCING ON RT WING AT CRUISE. VISUALLY INSPECTED AND CONCURRED. ARC IS BETWEEN GROUND SPOILER AND WING. ACFT GROUNDED. DETERMINED THE ANOMALY WAS AT THE OTBD AFT CORNERD THE RT INBD GROUND SPOILER. VISUALLY INSPECTED BONDING JUMPERS ON SPOILER SDR UVVR2013101500027Bolt · fracturedBOLT HEAD MISSING FROM UPPER FWD WING SPLICE PLATE. BOLT SHANK AND NUT WERE FOUND INTACT.SDR C77A20130929003Panel · damagedRACK, 2, SHELF (B)- (9009)- ELONGATED HOLE ON PANEL 516DB. ACCOMPLISHED PERMANENT REPAIR TO LT WING PANEL 516DB DAMAGED FASTENER HOLE IAW EA E175-57-170.SDR HNAA2013092500515Plate · crackedFWD INBD CORNER OF STRESS PANEL LADDER PLATE IS CRACKED AT PANEL 622AT. REMOVED DAMAGE AND REPLACED WITH NEW PART FABRICATED IAW RD 8-57-2287. COMPLIED WITH BOND TEST AND HFEC INSPECTION. NO OTHER CRACKS NOTED.SDR ECLA201309234337Unknown · unknownBIRDSTRIKE ON OTBD PORTION OF THE LT WING.SDR REXA2013090101645Panel · chafedPANEL 584AB IS CHAFED. REMOVED CHAFE IAW SRM 51-12-00. PANEL FOUND TO BE IN LIMITS IAW REO 680-57-52-157.SDR REXA2013083101641Panel · chafedPANEL 684EB IS CHAFED. REMOVED CHAFE FROM PANEL 684EB IAW REO 690-57-52-156. PANEL FOUND TO BE IN LIMITS IAW REO 690-57-52-156.SDR REXA2013083101640Panel · chafedPANEL 684LB IS CHAFED. REMOVED CHAFE FROM PANEL 684LB IAW SRM 51-12-00, FOUND TO BE IN LIMITS IAW REO 690-57-52-156.SDR REXA2013083101639Panel · chafedPANEL 684HT CHAFED. FABRICATED NEW PANEL IAW SRM 51-24-28.SDR ASAA2013083095913Rib · puncturedRT SEAL RIB HAS A PUNCTURE. R & R SEAL RIB.SDR REXA2013082101644Panel · chafedPANEL 584EB IS CHAFED. LOCATED AND DRILLED NEW PANEL IAW SRM 51-40-11.SDR REXA2013082101643Panel · chafedPANEL 584GB IS CHAFED. REPLACED PANEL 584GB IAW SRM 51-40-11.SDR CALA2013072990042Fastener · missingWALKAROUND MULTIPLE FASTENERS LOOSE, MISSING UNDERWING PANELS BOTH SIDES, OTBD EA MLG STRUT. INSTALLED NEW FASTENERS ON UNDERWING PANELS.SDR ASMF201308008Fairing · damagedDURING TRANSIT CHECK, A BIRD STRIKE WAS DETECTED IN RT ENGINE. BIRD STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-18, DETECTING 6 FAIRING DAMAGES AND 2 PANELS WITH 4 IMPACT, BEING WITHIN LIMITS OF OPERATION IAW AMM 71-00-00. PANELS WERE REPAIRED ISDR A6WA2013071041054Panel · chafedVISOR PANEL NR 326 BL DISTORTED (BENT) CHAFED BEYOND LIMITS. REPLACED WITH SERVICEABLE VISOR PANEL.SDR 2013FA0000146Bolt · crackedFOUND RIGHT WING LOWER FORWARD WING BOLT CRACKED DURING DYE PENETRANT INSPECTION, CRACK WAS JUST BELOW THE BOLT HEAD RADIUS, INSTALLED NEW BOLTSDR SWIA201332827Unknown · dirty1/2 OF LEFT AILERON TRAVEL NEEDED WITH FLAPS AT 45° FOR A/C TO FLY STRAIGHT. (SERVICE) CLEANED FLAPS, FLAP WELLS AND WINGS IAW AMM. OPERATED FLAPS AND FOUND NO FAULTS.
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