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 aircraft_model_key = '120' 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 aircraft_model_key = '120' 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 DXTA2022082968970None · noneMAIN DOOR PRECATCH: MAIN CABIN DOOR PRECATCH WILL NOT RELEASE DOOR WITH APU OPERATING.SDR DXTR2022082602Galley · scratchedDESCRIPTION: 1. 5" SCRATCHES AFT SIDE OF GALLEY DOORS - 2. TABLE BETWEEN SEAT 7 AND 9 LAMINATE GOUGED - 3. GALLEY COFFEE DOOR FACE HAS DENT IN WOOD.
1- REPAIRED & REFINISHED GALLEY DOORS TO A HIGH GLOSS USING;
A. IC&S POLYESTER - SEE FAA 8110SDR DXTR20220826Panel · elongatedVERTICAL STABILIZER HAS AN ELONGATED FASTENER HOLE AT THE 341CL PANEL (LH SIDE). RESOUTION: ACCOMPLISHED MAJOR REPAIR IAW AQRD ERO-106773 DATED 8/17/22SDR DXTA2022082668910None · noneMAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE WITH BOTH APU ON AND OFF. DURING THE LAST THIRD OF HANDLE MOVEMENT BOTH OPENING AND CLOSING DOOR YOU CAN FEEL AND HEAR SOMETHING BINDING. // SIGNOFF// PERFORMED A GVI OF MED LOCKING PIN RECEPTACLES AND FOUND LARGE AMSDR DXTA2022082668930Battery Pack · defectiveWITH THE EMER LIGHT SWITCH IN THE ARMED POSITION (AND THE SEAT BELT SIGN OFF) THE EXIT SIGN OVER THE LAV, SEAT 7, AFT DROP AISLE LIGHTING AND RING WING EMERGENCY LIGHTS ARE ALL ON. THE EXIT SIGN OVER THE MAIN CABIN DOOR AND FORWARD DROP AISLE LIGHTS ARE OFF. WSDR DXTA2022082668880None · noneCABIN EMERG LIGHT: WITH ALL POWER OFF AIRCRAFT, AND EMER LIGHT SWITH OFF, THE WING INSPECTION LIGHTS, CABIN MAIN ENTRY EXIT LIGHT, LIGHT OVER SEAT 3, AND FLOOR LIGHT UNDER SEAT 3 ARE ALL ON. BEING POWERED BY EMER BATTERIES. // SIGNOFF// TROUBLE SHOT SYSTEM ASDR DXTA2022082468780Light · inoperativeRIGHT EXTERIOR EMERG LIGHT: RIGHT SIDE FURTHEST AFT EMERGENCY LIGHT INOP. LIGHT BELOW EMERGENCY EXIT DOOR. // SIGNOFF// REMOVED INOP AFT WING EMERGENCY LED LIGHT ASSY AND REPLACED WITH A NEW LED LIGHT ASSY IAW CE-560XLS AMM 33-50-04. OPERATIONAL CHECK GOOD WITSDR 2022F00341None · looseUPON CLIMB OUT FROM KSDL THE PILOT SAW A LH GEAR UNSAFE LIGHT. HE THEN CYCLED THE LANDING GEAR AND APPROX. 4 MINUTES LATER HE SAW THE RED GEAR UNSAFE LIGHT AGAIN. HE CYCLED THE LANDING GEAR ONCE MORE AND THE CREW RETURNED TO BASE. - MAINTENANCE TROUBLESHOT TSDR DXTA2022082268640None · noneCABIN EMERG LIGHT: AFTER DE-POWERING AIRPLANE EMERGENCY LIGHTS REMAIN ON.SDR DXTA2022082268660Acm · inoperativeACM O'TEMP AMBER CAS: ACM O'TEMP MSG ILLUMINATED AT 45,000'. CHECKLIST ACCOMPLISHED.SDR 2022F00334None · noneON TAKEOFF THE CREW SAW THE MAIN CABIN DOOR CAS MESSAGE ILLUMINATE AS WELL AS THE CABIN VENT DOOR CAS MESSAGE. BOTH CAME ON AT 11,000 FEET WHILE DEPARTING ASPEN. THEY RETURNED TO ASPEN AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE INTERIOR CABIN DOOR HSDR DXTA2022081668120None · noneSPEED BRAKES AMBER CAS: THE SPOILERS TESTED CORRECTLY DURING THE AFTER START FLOW. ON TAXI THE AMBER AUTO TEST FAIL CAS MESSAGE LLUMINATED. THE TEST WAS REPEATED MANUALLY WITH THE SAME RESULT. AFTER THE CAS MESSAGE ILLUMINATED THE LEFT OUTBOARD SPOILER WOULD NSDR DXTA2022080467330Engine · defectiveENGINE FLAMEOUT: CLIMBING THROUGH FLIGHT LEVEL 280 THE NUMBER 2 ENGINE FLAMED OUT. LOUD BANG AND THEN INSTANT ROLL BACK QRH PROCEDURES ACCOMPLISHED. DECLARED AN EMERGENY TO INCLUDE ROLLING THR TRUCKS. AND RETURNED TO KLAS // SIGNOFF// REMOVED AND REPLACED SDR DXTA2022072566520None · defectiveGEAR DISAGREE L AMBER CAS: LANDING GEAR DID NOT EXTEND WHEN THE GEAR HANDLE WAS SELECTED DOWN. WE CYCLED THE LEVER AND IT STILL DIDNT EXTEND. THEN THE AMBER GEAR DISAGREE L/R/N ILLUMINATED. AFTER GOING AROUND, WE COMPLIED WITH THE QRH AND MANUALLY BLEW DOWN THSDR DXTA2022071165690None · noneMAIN DOOR: CAS MESSAGE "CABIN DOOR OPEN" CAN NOT GET AMBER LIGHT TO EXTINGUISH. FOLLOWED QRC GUIDANCE. // SIGNOFF// CHECKED SYSTEM DIAGNOSTICS WHILE OPENING AND CLOSING DOOR. FOUND THAT PAWL SWITCH S6 (SC007 IN AMM) WAS NOT CHANGING STATE. GAINED ACCESS TO S6SDR 2022F00263None · noneRIGHT ENGINE PYLON PANEL (P/N 7412311-4 MISMATCH). ACCOMPLISHED TEXTRON AVIATION LETTER DQ35192M1 DATED JUNE 15, 2022; 680A-0063 (N525QS) RIGHT ENGINE PYLON PANEL (P/N 7412311-4 MISMATCH).SDR 2022F00259None · noneLEFT ENGINE PYLON SKIN DAMAGE (WAVY). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ35118M1 DATED JUNE 10, 2022; 680A-0063 (N525QS) LEFT ENGINE PYLON SKIN DAMAGE (WAVY).SDR DXTA2022061563940Pin · looseEMERG EXIT SIGN/LIGHT: FORWARD FACING EMERGENCY EXIT SIGN LIGHT ON BULKHEAD ABOVE SEAT 9 HEADREST IS INOPERATIVE.// SIGNOFF// UPON INSPECTION, FOUND THE PIN ON ONE OF THE PIN SPLICES TO THE EMERGENCY EXIT SIGN ON THE FWD FACING LH LAV PARTITION TO BE LOOSE, CASDR 2022F00258None · noneWHILE IN CRUISE, FLIGHT CREW OBSERVED COCKPIT PAC O'TEMP CAUTION CAS MESSAGE (PAC AUTOMATICALLY SHUT DOWN). CREW PERFORMED CHECKLIST ITEMS, CAS MESSAGE DISAPPEARED AND APPROXIMATELY 2 MINUTES LATER, SAME MESSAGE APPEARED. WHILE REFERRING TO CHECKLIST AGAIN, CASDR 2022FA0000323Ejector · cloggedAFTER SUCCESSFUL ENGINE START, ENGINE SHUT-DOWN "UN-COMMANDED". REMOVED FUEL HEADER TANK ACCESS PANEL AND VISUALLY OBSERVED A SMALL SCREW IN INLET SCREEN OF FUEL JET / EJECTOR PUMP.SDR DXTA2022051962150None · defectiveAFT EMERGENCY LIGHT WILL NOT ILLUMINATE USING THE EMERGENCY LIGHTS BATTERY. THEY DO WORK WITH MAIN DC POWER. // SIGNOFF// VERIFIED AFT EXIT SIGNS AT DIVIDER AND OVER LAVATORY DO NOT ILLUMINATE ON EMERGENCY POWER ALONE, ALSO NOTED EXTERIOR OVER-WING LIGHTS DO NSDR 2022F00241None · chafedCHAFE DAMAGE ON THE LEFT MLG SIDE-BRACE FITTING. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34792 DATED MAY 16, 2022; 680A-0153, N596QS REPAIR RECOMMENDATION.SDR 2022F00240None · chafedRIGHT MAIN LANDING GEAR SIDE BRACE ACTUATOR (INBOARD FITTING) CHAFE DAMAGE. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34793M1 REV A DATED MAY 17, 2022; 680A-0153 (N596QS) RIGHT MAIN LANDING GEAR SIDE BRACE ACTUATOR (INBOARD FITTING) CHAFE DAMASDR 2022F00239Axle · chippedRIGHT MAIN LANDING GEAR AXLE PLATING DAMAGE (CHIPPED). ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34811M1 DATED MAY 17, 2022; 680A-0153 (N596QS) RIGHT MAIN LANDING GEAR AXLE PLATING DAMAGE (CHIPPED).SDR DXTA2022051962140None · defectiveLEFT FUEL TRANSFER: DURING LEVEL FLIGHT, FUEL TRANSFER SWITCH SELECTED TO RIGHT TANK, AT WHICH TIME AMBER FUEL TRANSFER FAIL CAS MESSAGE DISPLAYED. SWITCH WAS RETURNED TO OFF POSITION AND CAS MESSAGE EXTINGUISHED. FUEL TRANSFER SWITCH WAS SELECTED TO LEFT TANKSDR DXTA2022051761910Switch · intermittentCABIN EMERG LIGHT: EMERGENCY LIGHTING SYSTEM FAILS TO TEST PROPERLY ON PREFLIGHT. ALTHOUGH THEY INITIALLY ALL ILLUMINATE PROPERLY WHEN SELECTING THEM TO "ARM" WITH MAIN SHIP BATTERIES "OFF", THEY REMAIN ILLUMINATED ONCE MAIN SHIP BATTERIES ARE "ON" AND ALSO WISDR DXTA2022051661790Battery · abnormalCABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS FLICKER AND EXTINGUISH WHEN TESTING. ONCE SHIPS POWER IS APPLIED EMERGENCY LIGHTS WORK FINE. ONCE SHIPS BATTERIES ARE TURNED THE OFF , LIGHTS FLICKER AND THEN EXTINGUISH WITH EMERGENCY LIGHTS SWITCH IN THE ON POSITION.SDR 2022F00234Screen · corruptedDURING CRUISE FLIGHT, CREW EXPERIENCED LH PFD SCREEN FREEZING INTERMITTENTLY. FOLLOWED BY MULTIPLE AVIONICS FAILURES SUCH AS AUTO-PILOT FAIL, AUTO-THROTTLE FAIL, TRANSPONDER FAIL, SPOILER FAIL, GEAR DISAGREE, WINDSHIELD HEAT FAIL, GROUND PROX FAIL, TERRAIN FAISDR DXTA2022041260200Switch · activatedEMERGENCY LIGHTING: 5G RESET BUTTON LOCATED UNDER THE LEFT PILOTS SEAT SET OFF EMERGENCY LIGHTS. SWITCH IS BROKEN AND WILL NOT RESET. EMERGENCY LIGHTS WILL NOT GO OUT. // SIGNOFF// POWERED ON AIRCRAFT AND NOTED EMERGENCY LIGHTS ON. ATTEMPTED TO RESET LH PILOTSDR 2022FA0000580None · nonePILOT EXPERIENCED A SUDDEN POWER LOSS FOLLOWED BY A DROP IN OIL PRESSURE ON CLIMB OUT. THE PILOT WAS ABLE TO GET THE PLANE UNDER PARTIAL POWER BACK TO THE AIRPORT AND LAND SAFELY. PILOT REPORTED THAT THE OIL PRESSURE NEVER DROPPED BELOW THE BOTTOM OF THE GREENSDR 2022F00054Doubler · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL SDR 2022F00053Fairing · chippedLIGHTNING STRIKE DAMAGE OF THE VERTICAL FIN TIP FAIRING AND UPPER AFT RUDDER CAP. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ33675 DATED FEB. 20, 2022; 680A-0087, N537QS REPAIR RECOMMENDATION OF THE VERTICAL FIN TIP FAIRING AND UPPER AFT RUDDER CAP.SDR 2022F00083None · corrodedHORIZONTAL STABILIZER (LEFT SIDE) UPPER SKIN CORROSION. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ33582M1 DATED FEB/15/2022; 680A-0113 (N563QS) HORIZONTAL STABILIZER (LEFT SIDE) UPPER SKIN CORROSION.SDR 2022F00085Skin · corrodedLEFT WING UPPER SKIN (WHEEL WELL TOP/TRAILING EDGE SKIN) CORROSION. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ33529M1 DATED FEB/11/2022; 680A-0113 (N563QS) LEFT WING UPPER SKIN (WHEEL WELL TOP/TRAILING EDGE SKIN) CORROSION.SDR 2022F00069Cowl Door · noneRIGHT ENGINE UPPER COWL DOOR DAMAGE. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ33101M1 DATED JANUARY 10, 2022; 680A-0063 (N525QS) RIGHT ENGINE UPPER COWL DOOR DAMAGE.SDR 2022FA0000313None · failed* SUPPLEMENTAL INFORMATION TO THE INITIAL REPORT SUBMITTED ON CONTROL NUMBER AWKA202201050001 FILES ON DECEMBER 28, 2021 * TECHNICIANS INSPECTED THE FLAP SYSTEM AND FOUND THE INBOARD, LEFT FLAP PANEL TIGHT AND THE FLAP POWER DRIVE UNIT FAULTY. THE OUTBOARD FLASDR DXTA2021122754120None · noneCABIN EMERG LIGHT: OVERHEAD CABIN EMERGENCY LIGHTS ARE INOP. // SIGNOFF// PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHTS AND IS GOOD IRW CE-700 AMM 33-50-00.SDR 2021FA0000419None · noneL/H AND R/H MLG SIDE BRACE FITTING GOUGE.SDR 2022FA0000035Rocker · damagedPUSH ROD DROVE ACROSS ROCKER (HOLE) ENGINE VIBRATION AND LOSS OF POWER FALLOWEDSDR 2021FA0000371None · noneCOIL CORD INSULATION FAILED AFTER BEING INSTALLED 2 YEARS.SDR 2022FA0000607None · crackedAS OF THIS DATE THE ENGINE HAS 380 HOURS SINCE A MAJOR OVERHAUL. AIRCRAFT WAS IN A NORMAL CRUISE CONFIGURATION. ENGINE STARTED TO RUN ROUGH, PILOT RETURNED TO THE AIRPORT WITH NO FURTHER ISSUES. UPOND TEAR DOWN THE EXHAUST PUSH ROD HAD PUNCHED THROUGH THE ROCKSDR 2022F00016None · chippedCHIPPED PLATING ON RIGHT MAIN LANDING GEAR AXLE P/N 6741032-5. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ32727M1 REV. B DATED DECEMBER 6, 2021; 680A-0227 (N696QS) RIGHT MAIN LANDING GEAR AXLE PLATING DAMAGE (CHIPPED).SDR 2021FA0000321None · corrodedCORROSION ON LH WING UPPER SKIN ON SEAM FWD OF I/B FLAP. REFERENCE TEXTRON ENGINEERING MEMO DQ32434M1 DATED 11/16/2021.SDR 2021FA0000383None · inoperativePILOT REPORTS FUEL INDICATION IS HIGH. OPS TESTED AND FOUND FUEL FLOW TRANSMITTER AT FAULT. COMPLIED WITH R&R OF FUEL FLOW TRANSMITTER. AIRCRAFT OK FOR RTS.SDR 2020FA0000109Shaft · brokenALTERNATOR WAS INSTALLED ON ENGINE. ENGINE INSTALLED IN ACFT ON 3/1/2017 ACFT TT 5410.1 SHAFT IN ALTERNATOR BROKEN, REMOVED 6/12/2019 ACFT TT5740.9 TIME IN SERVICE 330.8 HOURS.SDR DXTA2018051000938None · noneCORRECTION TO SDR AS PER FAA REQUEST. REPEAT WRITE UP. RIGHT BRAKE FAILED (NO COCKPIT WARNINGS) LEFT LOCKED. NOSE ENDED UP IN GRASS OF TAXIWAY "CORRECTIVE ACTION: REPLACED THE PARKING BRAKE VALVE, ANTISKID CONTROL SERVO VALVE AND THE POWER BRAKE VALVE
IAW CESDR OSW201609260386Tire · departedSOLID RUBBER TIRE HAD DEPARTED THE TAIL WHEEL HUB ASSEMBLY DURING LANDING.SDR 2009FA0000870Rod End · corrodedA MAJOR PORTION OF THE ROD END IS CORRODED. THE TOP OF THE SPHERICAL END OF THE BALL (ROD END) IS AGAINST THE BOTTOM OF THE WING SKIN. THE ROD END IS VERY DIFFICULT IF NOT IMPOSSIBLE TO INSPECT WITHOUT REMOVING THE WING STRUT AND PERFORMING A GOOD VISUAL INSPESDR CA070717009Bracket · broken(CAN) V-BRACKET OF SPINNER BROKE ON ONE SIDE, THAT CAUSED OFFSET OF SPINNER WHICH CAUSED VIBRATION AND DECIDED TO CONDUCT A PRECAUTIONARY LANDING ON A FARMERS FIELD. NO FURTHER DAMAGE. (TC NR 20070717009)SDR CA040312003Cylinder Head · misaligned(CAN) ENGINE WAS SENT TO ENGINE SHOP FOR PROP STRIKE INSPECTION. UPON REINSTALLATION OF NR 1 CYLINDER, IT WAS DISCOVERED THAT THE BARREL AND HEAD WERE MISALIGNED BY APPROX. 5 DEGREES (UNIT WAS REPLACED). ENGINE SHOP ADVISES THIS IS A DEFECT OCCURING DURING O
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