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 = '1430' 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 = '1430' 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 QXEA200400361Nut Plate · loosePDX - AFT LEFT AND FORWARD LEFT NUT PLATES HAS COME LOOSE FROM THE RED LOCATOR BEACON. REPAIRED IAW SRM 51-43-05.SDR RX8R2004001Bolt · shearedWHILE TAXIING AFTER LANDING, THE PILOT DISCOVERED THE AIRCRAFT WOULD NOT TURN TIGHT. AFTER EXAMINATION, IT WAS FOUND THE (3) AN-3 BOLTS THAT SECURE THE NOSE STEERING LINKAGE TO THE TOP OF THE NOSE LANDING GEAR STRUT HAD SHEARED. FOUR OTHER AIRCRAFT WERE EXAMSDR QXEA200400339Nut Plate · brokenPDX- FORWARD LT AND RT NUTPLATES ARE BROKEN ON UPPER RED ANTI-COLLISION LIGHT ASSEMBLY ATTACH HARDWARE. REMOVED FORWARD ANGLE, REPLACED NUTPLATES AND REINSTALLED ANGLE IAW Q400 SRM 51-42-75.SDR QXEA200400352Rivet · burnedPDX - ABOVE PILOT AND CO-PILOT WINDSHIELD HAS RIVET HEADS BURNED APPROXIMATELY X-74 AND Z173.000. ALSO HAS SKIN DAMAGE. REPAIRED IAW HORIZON AIR EA 6-53-354 -A-.SDR QXEA200400334Rivet · burnedPDX - ABOVE PILOT AND CO-PILOT WINDSHIELD HAS RIVET HEAD BURNED. REPAIRED IAW HORIZON AIR EA 6-53-354.SDR QXEA200400341Nut Plate · damagedPDX- PANEL 121BL HAS A BAD NUTPLATE ON LOWER ROW. DOME SEALED NUT PLATE IAW DHC-8 SRM 51-23-00.SDR QXEA200400340Nut Plate · damagedPDX- RT FORWARD FUSELAGE PANEL 122AR HAS TWO BAD NUTPLATES. DOME SEALED NUTPLATES IAW DHC-8 SRM 51-23-00.SDR SWAA041408Fastener · looseDURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE HOOK FASTENERS PER MM.SDR QXEA200400326Nut Plate · strippedPDX- FOUR NUTPLATES ON PANEL 121AL ARE STRIPPED OUT. REMOVED AND REPLACED NUTPLATE IAW DHC-8 SRM 51-40-11.SDR AUS20040413Bolt · separated(AUS) GOVERNOR LINKAGE BOLT SEPARATED. LOSS OF ENGINE CONTROL RESULTED IN AUTO ROTATION AND HEAVY LANDING WITH SOME MINOR DAMAGE TO THE AIRCRAFT.SDR H2U2004F00001Bolt · brokenLT IB MLG BOLT AND NUT THAT ATTACHES IB MLG TO AIRCRAFT FRAME CAME LOOSE AND FELL OUT. NUT IS (LOCKNUT PN AN365-720) (BOLT PN AN7-23A). WHEN BOLT CAME OUT IB MLG BROKE BOTTOM SKIN AND MLG PLASTIC FARRING. LOWER SKIN PANEL $80, FARRING $70 NO OTHER DAMAGE OSDR H2U2004F00000Nut · brokenLT IB MLG BOLT AND NUT THAT ATTACHES IB MLG TO AIRCRAFT FRAME CAME LOOSE AND FELL OUT. NUT IS LOCKNUT (PN AN365-720) (BOLT PN AN7-23A). WHEN BOLT CAME OUT IB MLG BROKE BOTTOM SKIN AND MLG PLASTIC FARRING. LOWER SKIN PANEL $80 , FARRING $70 NO OTHER DAMAGE SDR 61334Screw · looseAT DFW AIRSTAIR DOOR WILL NOT CLOSE SECURE. NO FURTHER INCIDENT. RESECURED LOOSE SCREWS ON COVER PLATES.SDR 2004FA0000572Bolt · corrodedPILOT DECLARED AN EMERGENCY WHEN HE HAD A GEAR UNSAFE LIGHT AFTER THE GEAR EXTENDED. (AC EVENTUALLY LANDED SAFELY). GEAR DOWNLOCK DID NOT GO ALL THE WAY TO THE LOCK POSITION AND ACTIVATE THE SWITCH. (DOWNLOCK WAS FOUND CORRODED TO THE BOLT) MM , PUT A FEW DSDR KBM2004F00186Bolt · undertorquedENGINE TO MGB POWER SHAFT FORWARD COUPLING BOLT TO PULLEY FAIL TORQUE LOAD CHECK, COUPLING REJECTION MANDATORY. REMOVED AND REPLACED.SDR AUS20040390Bolt · incorrect(AUS) LT WING LANDING GEAR TO LANDING GEAR DOOR TIE ROD BOLTS INCORRECTLY FITTED. BOLTS WERE FITTED UPSIDE DOWN. PERSONNEL/MAINTENANCE ERROR.SDR AUS20040345Bolt · corroded(AUS) FORWARD OUTER ATTACHMENT SPECIAL BOLT SHAFT CORRODED AND PLATING MISSING. CORROSION WAS LOCATED APPROXIMATELY 12.7MM (0.5IN) DOWN FROM THE BOLT HEAD. AREA OF CORROSION 25.4MM (1IN) IN LENGTH BY 9.39MM (0.370IN) IN WIDTH BY0.127MM (0.005IN) DEPTH.BOLTS ASDR RO32004F00002Screw · chafed24TH SCREW IB OF RIB 20 ON LT WING IS CHAFFING ON OB SLAT HYDRAULIC LINE. DOORS, UPPER FIXED STRUCTURE BOX, RIB 7 TO RIB 13.SDR C2XA04CL050Screw · wrong partDURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT WOULD NOT OPEN. MAINTENANCE INSPECTED AND FOUND THE WRONG GRIP LENGTH SCREW INSTALLED ON THE DOOR SURROUND LINER. THE SCREW WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD OF THE DOOR.SDR DEL2004F00000Bolt · crackedDURING ENGINE REMOVAL, FOUND RT ENGINE AFT MOUNT BOLT CRACKED (PN26520023).SDR 2004FA0000375Bolt · shearedDURING FLIGHT, THE PILOT REPORTED THAT THE GEAR UNSAFE LIGHT WAS ILLUMINATED DURING GEAR RETRACTION. THE GEAR WAS EXTENDED AND 3 GREEN LIGHTS WERE OBSERVED. DURING THE SUBSEQUENT INSPECTION, THE BOLT IDENTIFIED BELOW WAS FOUND SHEARED AND THE PORTION OF THE BOSDR 04FDEA01118Fastener · shearedRIGHT WING LOWER SURFACE, ONE FASTENER HEAD FOUND SHEARED OFF FORWARD OF O/B FLAP I/B HINGE. RIGHT WING LOWER SURFACE - ONE FASTENER FORWARD OF O/B FLAP I/B HINGE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.SDR 04FDEA01119Fastener · shearedRIGHT WING LOWER SURFACE, ONE FASTENER HEAD FOUND SHEARED OFF FORWARD OF PANEL 641KB. RIGHT WING LOWER SURFACE, ONE FASTENER FORWARD OF PANEL 641KB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2.SDR 04FDEA01117Fastener · shearedLT WING LOWER SURFACE I/B AREA, ONE FASTENER HEAD FOUND SHEARED OFF. LT WING LOWER SURFACE I/B AREA, ONE FASTENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2.SDR AUS20040318Bolt · cracked(AUS) PROPELLER COUNTERWEIGHT TO BLADE CLAMP ATTACHMENT BOLTS (2OFF10) CRACKED.SDR 0400679954Screw · shearedDUIRING DESCENT FOR LANDING, THE CREW NOTICED THE LOSS OF ALL OF THE LEFT HYDRAULIC SYSTEM FLUID. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HOUSING SCREWS SHEARED ON THE ALTERNATE GEAR PUMP AND REPLACED THE PUSDR SWAA041209Fastener · missingL2 DOOR EVAC SLIDE DOOR GIRT BAR HOOK MISSING FASTENER. INSTALLED FASTENER IN R2 DOOR EVAC SLIDE HOOK PER MM.SDR UPS04842308Screw · corrodedTWENTY SCREWS & NUTPLATES CORRODED OUT OF BOTTOM OF LEFT REAR L1 TYPE DOOR. REPAIRED LEFT REAR TYPE 1 EXIT DOOR PER DC8 EO DC8-5220-19783F.SDR AUS20040312Bolt · separated(AUS) PASSENGER SEAT SUPPORT BEAM TO AISLE SIDE LEG STRUCTURE BOLTS SEPARATED AND FOUND UNDER SEAT 12 DEF.SDR QXEA200400290Dome Nut · damagedMAINTENANCE FOUND A BAD DOME NUT ON PANEL 122BR. THE DOME NUT WAS REMOVED AND REPLACED IAW Q400SRM 51-42-05.SDR DL764040369Bolt · failedLEADING EDGE SLAT ASYM EICAS MESSAGE DURING FLAP EXT FOR TAKEOFF. BITE TESTED PSEU. FAULTED TARGET 303 ON 9 SLAT INBOARD END. FOUND TARGET AND BOLT MISSING. REPLACED MISSING PARTS. CLEARED PS CYCLED FLAPS AND SLATS. NO MESSAGES APPEARED. SYSTEM CHECKS GSDR QXEA200400288Screw · looseMAIN CABIN DOOR CATCHES ON OPENING. APPEARS TO BE CATCHING ON LOOSE HINGE SCREW. MAINTENANCE TIGHTENED SCREW ON MAIN CABIN DOOR HANDLES. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR AUS20040307Bolt · missing(AUS) CRANKCASE BOLT MISSING. OIL LEAKING FROM CRANKCASE. ENGINE HAD JUST BEEN FITTED AND AIRCRAFT WAS ON TEST FLIGHT. PERSONNEL/MAINTENANCE ERROR.SDR CA040423011Rivet · burned(CAN) UPON DESCENT AIRCRAFT WAS STRUCK BY LIGHTNING ON LT SIDE OF NOSE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE COMPLETED LIGHTNING STRIKE INSPECTION IAW AMM 05-51-05. INSPECTION OF AIRCRAFT STRUCTURE FOUND 25 RIVETS BURNED ALONG THE LENGTH OF THE LTSDR 2004FA0000384Nut · missingUPON LANDING AIRCRAFT VEERED OFF THE RUNWAY. UPON INSPECTION IT WAS FOUND THAT THE NUT, (PN 5PA-108) HAD FALLEN OFF ALLOWING THE LINK (PN 32358) TO SEPARATE.SDR AUS20040296Bolt · faulty(AUS) LT AND RT VERTICAL FIN FORWARD ATTACHMENT BOLTS FAILED TORQUE TEST.SDR SWAA041080Rivet · shearedR2 DOOR EVAC SLIDE GIRT BAR FWD FITTING HAS SHEARED RIVET. REMOVED AND REPLACED R2 DOOR EVAC SLIDE GIRT BAR RIVET PER MM.SDR 513NA0005Bolt · missingTHREE TIE BOLTS MISSING ON THE NR 5 MAIN WHEEL ASSEMBLY. REPLACED LEFT OUTBOARD TIRE ASSEMBLY PER MM 32-45-01.SDR AWXA200400450Bolt · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON RT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT BS 1016, STR 2 RT. MAINTENANCE REMOVED AND REPLACED RT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT IAW T/C I6B5502.SDR AWXA200400446Bolt · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON THE LT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT BS 1016, STR 2 LT. MAINTENANCE REMOVED AND REPLACED L/H VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT IAW T/C I6B55002.SDR AWXA200400451Bolt · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON RT AFT INBOARD VERTICAL STABILIZER ATTACH BOLT BS 1085, STR 2 RT. MAINTENANCE REMOVED AND REPLACED RT AFT INBOARD VERTICAL STABILIZER ATTACH BOLT IAW T/C I6B55002.SDR SIMA200409901Connector · looseEMERGENCY FLOOR LIGHTING STRIP INOPERATIVE AT SEAT 16A, ISSUED MEL 33-27. FOUND CONNECTION OF STRIP LIGHTING LOOSE. RE-SECURED AS REQUIRED IAW EMB AMM, MEL RESTORED. AIRCRAFT RETURNED TO SERVICE. (M)SDR MCI2004F00000Attach Bolt · damagedPERFORMED INSPECTION ON HORIZONTAL STABILIZER ATTACH FITTINGS AND FOUND BOLT HEAD MISSING ON ONE BOLT ON LT AFT ATTACH POINT. REMOVED BOLT AND FOUND IT TO BE WORN AND CORRODED. REPLACED LT AND RT AFT ATTACH BOLTS, BOTH WERE WORN AND CORRODED. BOLT HEAD SHOWSDR CA040427010Screw · galled(CAN) DURING INCORPORATION OF SERVICE BULLETIN THE SERVICE CENTER TECHNICIAN FOUND GALLING ON THE ACME SCREW AND A SMALL PIECE OF THE SCREW THREAD WAS MISSING. THE PITCH TRIM ACTUATOR WAS REMOVED FROM THE AIRCRAFT AND SHIPPED TO THE VENDOR FOR INVESTIGATION. NSDR 040604Bolt · damagedTHE ENGINE WAS SPLIT AT THE (C) FLANGE. AFTER REMOVAL OF THE C.T. DISC, IT WAS NOTED THAT 2 BOLTS HOLDING THE INNER EXIT DUCT TO THE ENGINE HAD SHEARED OFF AND WERE LODGED IN THE AREA, WITH THE REMAINDER OF THE BOLT SHANKS LEFT IN THE BOLT HOLES. DAMAGE WAS SDR ASAA0480246Fastener · corrodedFOUND RUSTED FASTENERS ON LONGERON 29R STATION 1231-1250. REMOVED DAMAGED LONGERON, ORDERED AND INSTALLED NEW LONGERON IAW MD80 SRM 51-30-5. (M)SDR CA040512007Bolt · worn(CAN) DURING SERVICEABILITY CHECK, THE AME FOUND THE ELEVATOR SYSTEM SEEMED LOOSE. HE ALSO FOUND THAT HE COULD MOVE BOTH ELEVATORS IN THE OPPOSITE DIRECTION SLIGHTLY. FURTHER TROUBLESHOOTING REVEALED THAT THE UPPER CONTROL TUBE TO BELL CRANK BOLT WAS INSUFFICSDR ASAA0480203Fastener · corrodedOKC - FOUND DURING HV CHECK, CORROSION AROUND FASTENER INSIDE LONGERON 30 AT STATION 655 IN MID PIT. REMOVED CORROSION, INSTALLED U-CHANNEL REPAIR PER SRM 53-02. (M)SDR QXEA200400256Nut Plate · strippedPDX - PANELS 121AL, 121BL, 122BR, AND 122AR HAVE STRIPPED NUT PLATES. MAINTENANCE REPLACED THE NUT PLATES AS REQUIRED IAW D-8-200 SRM 51-40-11.SDR AUS20040247Bolt · broken(AUS) RT MAIN LANDING GEAR UPLOCK ROLLER BOLT BROKEN.
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