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 = '402C' 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 = '402C' 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 HYIA20151203002Gasket · defectivePILOT REPORTED STRONG SMELL OF FUEL, WHEN COCKPIT WITH THE HEATER RUNNING. R & R THE HEATER FUEL FILTER GASKET & PUMP OUTLET FITTING. OPERATIONALLY CHECKED GOOD.SDR HYIA20151203003Pump · defectivePILOT REPORTED FUEL SMELL WITH HEATER RUNNING IN FLIGHT. R & R THE HEATER FUEL PUMP & HEATER FUEL LINE. OPERATIONAL CHECKED GOOD.SDR HYIA20151124003Flap · out of rigPILOT REPORTED ACFT ROLLS TO THE RT WHEN FLAPS ARE 15 DEGREES EXTENDED. INSPECTED & FOUND AN ASYMMETRICAL CONDITION WITH FLAPS. RIGGED FLAPS IAW MM CHAPTER 27.SDR HYIA20151124002Fuel Line · leakingPILOT REPORTED STRONG FUEL ODOR IN CABIN. INSPECTED THE HEATER FUEL SYS & FUEL LINES, FOUND THE RT HEATER FUEL LINE LEAKING. TORQUED HEATER FUEL LINES & LEAK CHECKED WITH NO FURTHER DEFECTS NOTED.SDR HYIA20151124001Unknown · odorPILOT REPORTED STRONG FUEL SMELL IN CABIN WITH HEATER ON. INSPECTED HEATER FUEL LINES WITH NO LEAKS NOTED. AS PRECAUTION, CLEANED HEATER SPARK PLUG & FUEL NOZZLE. OPERATIONALLY CHECKED GOOD.SDR HYIA20151117001Unknown · smokePILOT REPORTED BURNING INSULATION SMELL IN COCKPIT. INSPECTED LT SIDE CONSOLE, CB PANEL, BEHIND INSTRUMENT PANEL, FOUND NO SIGN OF OVERHEATED OR BURNT WIRES & NO POPPED CB.SDR HYIA11072015001Beam · crackedDURING SCHEDULED INSPECTION THE LT NACELLE CROSSOVER BEAM ASSEMBLY WAS FOUND TO BE CRACKED AT OTBD LOWER U CHANNEL. REMOVAL OF CROSSOVER BEAM ASSEMBLY, DETAILED VISUAL INSPECTION OF SURROUNDING STRUCTURE FOR ADDITIONAL DEFECTS & INSTALLATION OF NEW BEAM ASSEMSDR HYIA20151107001Push-Pull Rod · bentWHEN EXTENDING FLAPS 15 DEGREES, ACFT ROLLS RT UNCOMMANDED. REST OF FLAP DEPLOYMENT AFTER TRIM INITIATED FEELS NORMAL. INSPECTED & FOUND THE RT INBD & OTBD FLAP RODS BENT. R & R RIT INBD & OTBD FLAP PUSH & PULL RODS & RE-RIGGED FLAP CABLES.SDR HYIA20151029002Fuel Line · loosePILOT REPORTED A STRONG FUEL SMELL IN CABIN, NOTING THAT THE HEATER WAS OFF DURING FLIGHT. PERFORMED AN OPERATIONAL CHECK OF THE HEATER, INSPECTED THE FUEL LINES & COMPONENTS, NO FUEL LEAKS OR SMELLS NOTED AT THIS TIME. APPLIED TDMI OF RT WING FUEL PANEL SEESDR HYIA20151026001Line · loosePILOT REPORTED A FUEL ODOR IN COCKPIT. INSPECTED FUEL SYS & TIGHTENED A RT FUEL SELECTOR LINE, WITH NO FURTHER DEFECTS NOTED.SDR HYIA20151019001Rod · severedPILOT REPORTED ON APPROACH, WHEN FLAPS DEPLOYED TO 30 DEGREES THE ACFT ROLLED AGGRESSIVELY TO THE RIGHT. INSPECTED & FOUND THE RT FLAP OTBD FLAP ROD SEVERED. R & R THE FLAP ROD, OPERATIONALLY CHECKED GOOD.SDR 8PCR20151027001Nut · fracturedDURING ROUTINE INSPECTION, TWO THROUGH BOLT NUTS, TWELVE POINT PN 652541, WERE FOUND FRACTURED & LAYING IN THE BOTTOM OF THE ENG COWLING. THE ENG HAS BEEN REMOVED TO BE DISASSEMBLED, INSPECTED & OVERHAULED. THE NUTS WERE RETURNED TO THE ENG MFG FOR FURTHER ESDR GULA20151013001Pump · faultedAFTER COMPLETION OF A PHASE INSPECTION, FOUND THE LT FUEL BOOST PUMP WAS NOT OPERATING. REPLACEMENT RECEIVED & INSTALLED, THE OUTPUT PRESS FAILED TO REGISTER ON THE FLIGHT DECK INDICATOR. CONTACTED THE VENDOR FOR A RMA & RECEIVED ANOTHER FUEL BOOST PUMP. AGSDR HYIA20151006001Caliper · leakingTHE RT BRAKE INOPERATIVE. INSPECTED THE RT BRAKE & FOUND THE CALIPER LEAKING. R & R THE RT CALIPER & BLED RT BRAKE SYS. OPERATIONAL & LEAK CHECKED GOOD.SDR HYIA20151007001Housing · defectivePILOT REPORTED FUEL SMELL IN THE CABIN. R & R THE RT FUEL BOWL HOUSING, LEAK CHECKED GOOD.SDR N3BA2015100200113Cylinder · detachedNUMBER 4 CYLINDER SEPARATED FROM ENGINE CASE.SDR 8PCR20151001003Nut · fracturedDURING ROUTINE INSPECTION, A THRU-BOLT NUT, TWELVE POINT PN 65254, WAS FOUND FRACTURED & LAYING IN THE BOTTOM OF THE ENG COWLING. THERE WERE NO SIGNS OF CORROSION ON THE NUT. THE ENG WAS REMOVED TO BE DISASSEMBLED, INSPECTED & OVERHAULED. THE NUT WAS RETURNSDR 8PCR20151001002Nut · fracturedDURING ROUTINE INSPECTION, A THRU-BOLT NUT, TWELVE POINT PN 652541, WAS FOUND FRACTURED & LAYING IN THE BOTTOM OF THE ENG COWLING. THERE WERE NO SIGNS OF CORROSION ON THE NUT. THE ENG WAS REMOVED TO BE DISASSEMBLED, INSPECTED & OVERHAULED. THE NUT WAS RETURSDR 8PCR20151001001Connecting Rod · out of limitsDURING REPLACEMENT OF THE NR 2 CYLINDER, THE CONNECTING ROD BUSHING, PN 530658, HAD MOVED FROM THE CONNECTING ROD BORE IN A REARWARD DIRECTION & EXHIBITED MISSING MATERIAL FROM CONTACT WITH THE PISTON PIN BORE BOSS. THE ENG WAS COMPLETELY DISASSEMBLED FOR FURSDR HYIA20151002001Governor · defectivePILOT REPORTED RT PROPELLER OVERSPEED INDICATION ON CLIMB OUT, THEN DIFFICULTY CONTROLLING THE PROPELLER AT A STEADY RPM AFTER THAT POINT. R & R THE RT ENG PROPELLER GOVERNOR, OPERATIONAL & LEAK CHECKED GOOD WITH NO FURTHER DEFECTS AT THAT TIME.SDR HYIA20150928001Wire · brokenPILOT REPORTED THE NOSE GEAR WOULD NOT INDICATE DOWN DURING NORMAL OR EMER EXTENSION. INSPECTED NOSE GEAR EXTENSION & RETRACTION SYS & FOUND NLG ACTUATOR GND WIRE BROKEN AT RING TERMINAL. ATTACHED NEW RING TERMINAL TO NLG ACTUATOR GND WIRE IAW 402C WDM CH 20SDR N3BA2016100500003Nut · brokenNR 4 CYLINDER'S CONNECTING ROD END CAP SEPARATED FROM CONNECTING ROD. INSPECTION OF ENGINE REVEALED THAT 1 OF THE 2 ATTACHMENT NUTS THAT SECURES END CAP TO CONNECTING ROD CRACKED INTO 4 PIECES ALLOWING END CAP TO STOP SECURING CONNECTING ROD TO CRANKSHAFT. COSDR HYIA20150918003Engine · damagedRIGHT ENG OIL PRESS DROPPED TO ZERO IN FLIGHT. DIVERTED & ON SHORT FINAL APPROACH RT ENG STOPPED RUNNING. PROPELLER DID NOT FEATHER. POST LANDING INSPECTION REVEALED OIL LEAKING FROM TOP & BOTTOM OF ENG COWLING. PRELIMINARY EXAMINATION REVEALS TOP OF CRANKSDR HYIA20150918002Door · openPILOT REPORTED THE LT WING LOCKER OPENED DURING FLIGHT. INSPECTED THE LT WING LOCKER DOOR & LATCH ASSEMBLY WITH NO DEFECT NOTED. OPERATIONS CHECKED GOOD.SDR HYIA20150921001Engine · making metalJUST AFTER LIFTOFF, STILL AT TAKEOFF POWER, RT MANIFOLD PRESS WAS 36" RPM NORMAL & ROUGH RUNNING. INSPECTED THE ENG & FOUND EVIDENCE OF METAL CONTAMINATION. THE RT ENG WAS REMOVED & REPLACED, SENT FOR TEARDOWN ANALYSIS.SDR HYIA20150918001Door · openPILOT REPORTED THE LT WING LOCKER OPENED DURING FLIGHT. INSPECTED THE DOOR WITH NO DISCREPANCIES FOUND.SDR HYIA20150914001Axle · brokenON TAXI OUT, PILOT REPORTED THE RT MAIN WHEEL BROKEN. PERFORMED VISUAL INSPECTION ON RT MLG & FOUND THE RT MLG AXLE BROKEN & MAIN TIRE WITH DAMAGE. R & R THE RT MLG LOWER BARREL IAW MM CHAPTER 32-10-00. OPERATIONS CHECKED GOOD. R & R RT MLG WHEEL ASSEMBLY SDR 8PCR20150910001Bolt · shearedCRANKSHAFT CLUSTER GEAR BOLTS, PN 536379, HAD SHEARED ALLOWING THE DISENGAGEMENT OF THE LARGE GEAR THAT COUPLES WITH THE STARTER ADAPTER SHAFT-GEAR. THE ENG WAS NOT IN COMPLIANCE WITH SERVICE BULLETINS SIL06-3 & SB13-6, WHICH RECOMMEND REPLACEMENT OF THE GEARSDR HYIA20150903002Governor · defectivePILOT REPORTED LT ENG PROP FEATHERS BEFORE DETENT. LUBRICATED THE PROP GOVERNOR CABLE, R & R LT ENG PROP GOVERNOR. OPERATIONAL & LEAK CHECK GOOD.SDR HYIA20150903001Unknown · odorPILOT REPORTED FUEL SMELL IN CABIN. INSPECTED LT & RT WING FUEL LINES, CABIN FUEL LINE, HEATER FUEL LINES & ENG LT & RT FUEL LINES, NO LEAKS NOTED.SDR HYIA20150827003O-Ring · damagedPILOT REPORTED LT BRAKE FAILED UPON LANDING. R & R O RING ON PISTON IN LT MASTER CYLINDER, SERVICED WITH HYD FLUID. OPERATIONAL & LEAK CHECKED GOOD.SDR HYIA20150827002Master Cylinder · lowPILOT REPORTED RT BRAKE SOFT & NO BRAKING ACTION. INSPECTED THE RT BRAKE SYS. SERVICED RT BRAKE MASTER CYLINDER WITH HYD FLUID. OPERATIONALLY CHECKED GOOD.SDR HYIA20150827001Door · openPILOT REPORTED CREW DOOR IN FLIGHT UNLATCHED & CAME OPEN. INSPECTED THE DOOR LATCH MECHANISM WITH NO DEFECTS NOTED. DAMAGE NOTED AT FWD HINGE & REPAIRED AS NECESSARY. CREW WAS UNABLE TO VERIFY IF THE DOOR WARNING LIGHT HAD ILLUMINATED DURING FLIGHT.SDR HYIA20150911001Bolt · severedON PREFLIGHT, PILOT REPORTED THE RT NACELLE, LG, FLAP & WING WERE OIL SOAKED & PUDDLES OF OIL UNDER THE WING. INSPECTED & FOUND THE SCAVENGE PUMP DRIVE GEAR BOLTS SEVERED. REPLACED THE RT ENG WITH NO FURTHER DEFECT NOTED. ENG WAS SENT OUT FOR TEAR DOWN.SDR HYIA20150820001Liner · defectivePILOT REPORTED RT BRAKE DROPPED TO FLOOR AFTER LANDING & A VERY MUSHY FEEL. R & R THE RT BRAKE LINING ASSEMBLY & SERVICED THE HYD SYS IAW CHAPTER 32-40-00. OPERATIONS CHECKED SATISFACTORY AT THAT TIME.SDR HYIA20150817001Engine · failedPILOT REPORTED RT ENG FAILED INFLIGHT. R & R THE ENG, OPERATIONAL & LEAK CHECKED GOOD. ENG HAS BEEN SENT FOR TEAR DOWN ANALYSIS.SDR HYIA20150813001Balance Tube · defectivePILOT REPORTED FUEL SMELL IN FLIGHT. R & R THE LT ENG BALANCE TUBE & FWD DRAIN. LEAK CHECKED GOOD WITH NO DEFECT NOTED. ADDITIONALLY CAS ORDERED THAT ALL FUEL LINES & FUSELAGES BE INSPECTED, AS WELL AS RE-INSPECTING THE BALANCE TUBE & FUEL DRAIN FOR POSSIBLSDR HYIA20150804002Fluid · lowLEFT FOOT BRAKE, NO PRESS ON LT SIDE, NO BRAKING ACTION LT SIDE. INSPECTED LT BRAKE LININGS, CHECKED FOR LEAKS, NO DEFECTS NOTED. SERVICED MASTER CYLINDER WITH FLUID. OPERATIONS CHECKED GOOD.SDR HYIA20150804001Fluid · lowLOST BRAKING FOR A FEW SECONDS ON LANDING ROLLOUT. FIRST ON CO-PILOT SIDE THEN ON PILOT SIDE. INSPECTED BRAKE LINING & PADS ON LT & RT SIDE. INSPECTED FOR LEAKS, NO DEFECTS NOTED, SERVICED BOTH BRAKE MASTER CYLINDERS WITH FLUID. OPERATIONS CHECKED GOOD.SDR HYIA20150729003Control Cable · disconnectedPILOT REPORTED NO PROPELLER RPM CONTROL THROUGH LEFT PROPELLER LEVER. FOUND LEFT PROPELLER CONTROL CABLE DISCONNECTED AT GOVERNOR. CONNECTED WITH PROPER HARDWARE IAW MM 61-20-00. OPS CHECKED GOOD.SDR HYIA20150729004Relay · failedPILOT REPORTED LEFT ENGINE STARTER LIGHT ILLUMINATED. THE FLIGHT DIVERTED FROM ITS ORIGINAL DESTINATION. INSPECTED & FOUND LEFT STARTER RELAY INTERMITTENT. R & R LEFT STARTER RELAY, THE STARTER REMAINED INOPERATIVE. R & R THE LEFT ENGINE STARTER & OPERATIOSDR HYIA20150729002O-Ring · leakingPILOT REPORTED FUEL ODOR IN CABIN. FOUND THE FUEL SUMP ON LEFT WING LEAKING. R & R O-RING ON SUMP. OPERATIONAL & LEAK CHECK GOOD.SDR HYIA20150729001O-Ring · leakingPILOT REPORTED FUEL ODOR IN COCKPIT. R & R THE RIGHT FUEL BOWL O-RING, NO FURTHER DEFECTS NOTED.SDR HYIA20150723002Caliper · failedPILOT REPORTED LT BRAKES INOPERATIVE. R & R THE LT BRAKE CALIPER & BLED BRAKES. OPERATIONAL & LEAK CHECKED GOOD.SDR HYIA20150720001Sealant · unknownPILOT REPORTED FUEL SMELL IN CABIN. ENCAPSULATED & FILLET SEALED RT WING TE AFT SPAR WEB RIVETS. LEAK CHECKED GOOD IAW AMM CH 28-10.SDR HYIA2015072020150Master Cylinder · lowPILOT REPORTED ON LANDING, RT BRAKE PEDAL WENT TO THE FLOOR & APPLIED NO BRAKE PRESS. INSPECTED RT BRAKE SYS WITH NO DEFECTS OR LEAKS NOTED. SERVICED RT BRAKE MASTER CYLINDER WITH HYD FLUID IAW MM CH 32-40-00. OPERATIONALLY CHECKED GOOD.SDR HYIA2015072015Alternator · failedPILOT REPORTED LT & RT ALTERNATOR LIGHTS ILLUMINATED IN FLIGHT. R & R THE RT ALTERNATOR & RT VOLTAGE REGULATOR. PERFORMED PARALLELING. OPERATIONAL & LEAK CHECKED GOOD IAW MM CH 24-30-01.SDR HYIA20150723001Structure · leakingPILOT REPORTED FUEL SMELL IN CABIN. FOUND A LEAK IN THE LT OTBD FLAP RIB AREA. SEALED INSIDE FUEL TANK WITH PRC. LEAK CHECKED GOOD.SDR HYIA07092015001Beam · crackedDURING SCHEDULED INSPECTION, THE LWR U CHANNEL OF RT NACELLE CROSSOVER BEAM, 5654104-12, WAS FOUND TO BE CRACKED, TRANSVERSE TO LENGTH OF CHANNEL THROUGH EACH RADIUS. CORRECTIVE ACTION WILL BE A COMPLETE REPLACEMENT OF BEAM, FOLLOWING A DETAILED INSPECTION OFSDR 2015F00089Filter Adapter · crackedENGINE RECEIVED FOR OVERHAUL, 5317.1 HOURS SFRM. TOTAL TIME ON PART UNKNOWN. OIL FILTER ADAPTER PN 653491, CASTING PN CA641608A, WAS FOUND TO BE CRACKED DURING ROUTINE INSPECTION AT ENG OVERHAUL. THE CRACK WAS LOCATED AT LOWER LT MOUNTING STUD BORE SPOT FAC
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