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 = '400A' 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 = '400A' 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 2011F00204Tire · separatedFLIGHT CREW NOTED ABNORMAL BRAKING AND CONTROL ON LANDING, ACFT CLEARED RUNWAY AND STOPPED ON RAMP WITH NO INCIDENT. FOUND LT MAIN TIRE FLAT WITH TREAD MISSING, NO OTHER ACFT DAMAGE NOTED. MX INSPECTED ACFT, AND REPLACED TIRE AND WHEEL ASSY. MX FOUND TREAD SDR 2011F00201Engine · making metalDURING ENGINE MINOR INSP, SENT OIL FILTER TO LAB FOR ROUTINE ANALYSIS, LAB REPORTED METAL IN OIL. CONTACTED MFG FOR EVALUATION, MFG INSTRUCTED TO INSTALL NEW OIL AND FILTER, PERFORM GROUND RUN FOR 1 HOUR, AND SEND FILTER OUT FOR REPEAT ANALYSIS. SECOND ANALYSSDR CVGA112501Engine · power lossDESCENDING THROUGH 16,000FT WITH 68% N1/SIDE AND ENGINE ANIT-ICE ON, THE RIGHT ENGINE ROLLED BACK TO 42% N1. HEARD BANGING FROM THE RIGHT ENGINE THAT LASTED 3 OR 4 SECONDS WITH ABOUT 5 BANGS. THEN THE ENGINE RETURNED TO THE ORIGINAL POWER SETTING.SDR DJFA20110905001Oil System · leakingFLIGHT CREW NOTED A BURNING SMELL AFTER TAKEOFF, FOLLOWED BY VISIBLE SMOKE IN THE AFT PASSENGER CABIN (NO PASSENGERS WERE ONBOARD). ACFT RETURNED TO THE DEPARTURE AIRPORT AND LANDED SAFELY. MAINTENANCE TECHNICIANS CONFIRMED OIL SMELL COMING FROM THE RT ENGISDR DXTA2011082304706Brake Sys · malfunctionedMOMENTARY BRAKE RELEASE WHEN APPLYING BRAKES PRIOR TO EXITING THE RUNWAY. PERFORMED BRAKE BLEED & TAXI CHECK, UNABLE TO DUPLICATE DISCREPANCY, PERFORMED ANTI-SKID RESPONSE CHECK, NO DEFECTS NOTED. ALL WORK DONE IAW MM 32-40-00.SDR E81RJT2309420BDuct · crackedDURING SCHEDULED INSPECTION, FOUND LT ENGINE NACELLE ANTI-ICE CROSSOVER BLEED AIR DUCT CRACKED AT BELLOWS, STAINLESS STEEL BRAIDING FRAYED AND BLOWN-OUT. MX HISTORY UNKNOWN. MAY POSSIBLY HAVE BEEN CAUSED BY PARTIAL MIS-ALIGNMENT STRESS. RECOMMEND MFG INVESTISDR E81RJT2309420ADuct · crackedDURING SCHEDULED INSP, FOUND LT ENGINE INBD SIDE ENGINE PAD TO "Y" DUCT BLEED AIR ANTI-ICING DUCT CRACKED AT BELLOWS, STAINLESS STEEL BRAIDING BLOWN-OUT AND FRAYED. MX HISTORY UNKNOWN, POSSIBLY CAUSED BY MIS-ALIGNMENT. RECOMMEND MFG INVESTIGATE WHETHER THIS ISDR DJFA2011040Motor · seizedPRIOR TO ENGINE START, CREW NOTED SMOKE FROM A VENT ON THE TAIL OF THE ACFT AND SMELLED A STRONG ELECTRICAL ODOR. MX FOUND THE VAPOR CYCLE MACHINE MOTOR BURNED UP. MOTOR WAS REPLACED.SDR DJFA2011038Frame · crackedDURING SCHEDULED INSP, MX TECH FOUND THE BLEED AIR TUBE SUPPORT BRACKET ATTACHED TO FRAME 329.9 PULLED AWAY AND DAMAGED THE FRAME. THE FASTENERS WERE PULLED THROUGH THE FRAME AND THE FRAME CRACKED AT THE FASTENER HOLES. FRAME WAS REPAIRED IAW DER APPROVED SDR CVGA111961Unknown · malfunctionedON TAKEOFF ROLL, LOST ALL N1 INDICATION (DIGITAL AND ANALOG) ON THE RT ENGINE.SDR DJFA2011037Bracket · crackedDURING A SCHEDULED MX VISIT, WHILE PERFORMING A HORIZ STABILIZER ROLLER INSP OF THE HORIZ STABILIZER INBD RIB AND BRACKET ASSEMBLIES, THE LT AFT ROLLER BRACKET WAS FOUND CRACKED. ROLLER BRACKET WAS REPLACED.SDR DJFA2011036Bracket · crackedDURING A SCHEDULED MX VISIT WHILE PERFORMING A HORIZ STABILIZER ROLLER INSPECTION OF THE HORIZ STABILIZER INBD RIB AND BRACKET ASSEMBLIES, THE RT AFT ROLLER BRACKET WAS FOUND CRACKED. ROLLER BRACKET WAS REPLACED.SDR DXTA2011070804652Control Cable · out of rigFLAP ASYMMETRY ANNUNCIATOR ILLUMINATED ON APPROACH, JUST AFTER FLAPS SELECTED TO 10 DEGREES. FLAPS EXTENDED A FEW DEGREES BEFORE FREEZING IN PLACE. FLAP HANDLE RETURNED TO ZERO DEGREES TO MATCH CONDITION OF INDICATOR WITH NO MOVEMENT OR RETRACTION NOTED. NOSDR 9JLA1869Computer · defectiveTHE CREW REPORTED THE LT STALL SYSTEM TEST WOULD NOT MOVE THE NEEDLE ON AOA GAUGE, TROUBLESHOT THE STALL SYSTEM AND FOUND THE STALL WARNING COMPUTER TO BE DEFECTIVE. REMOVED S/N 22886 AND INSTALLED AN INSPECTED STALL COMPUTER P/N 0020BG1 S/N 22957. FUNCTIONASDR DXTA2011061704618Control Cable · out of rigINITIATED A 15 DEGREES LEFT TURN & HAD A BINDING IN SPOILER SYS. NO PROBLEMS ROLLING RT. AT 0-10 NORMAL 10-15 DEGREES BINDING BEGINS & AROUND 15, PRESSURE POPS OFF TO LESS THAN NORMAL. AT 18, NORMAL PRESSURE & CONTROL. OBSERVED ON BOTH CONTROL COLUMNS AT MUSDR DJFA2011022Frame · crackedDURING SCHEDULED INSPECTION, MAINTENANCE TECHNICIANS FOUND THE BLEED AIR TUBE SUPPORT BRACKET ATTACHED TO FRAME 329.9 PULLED AWAY AND DAMAGED THE FRAME. THE FASTENERS WERE PULLED THROUGH THE FRAME AND THE FRAME CRACKED AT THE FASTENER HOLES. THE FRAME WAS RSDR E81RJT230313Circuit Card · faultyFLIGHT CREW REPORTED RECEIVING A RED "AP PITCH TRIM FAIL" INDICATION ON CLIMBOUT. VERIFIED FAULT IN NR 1 AUTOPILOT SYS FCC-4007 FLIGHT CONTROL COMPUTER CARD. REPLACED FCC-4007 CARD WITH AN O/H CARD, AUTOPILOT/ FLIGHT DIRECTOR, AND PITCH TRIM OPS CHECK NORMALSDR CA110711009Warning Light · illuminated(CAN) ABORTED T/O, ON T/O ROLL AT APPROXIMATELY 25 KTS, THE ENGINE ELECTRONIC FUEL CONTROL, EFC, LIGHT CAME ON AT APPROX 97 PERCENT N1. THE PILOT ABORTED T/O. TROUBLESHOOTING IS ON-GOING.SDR DJFA2011023Frame · crackedDURING SCHEDULED INSPECTION, MAINTENANCE TECHNICIANS FOUND THE BLEED AIR TUBE SUPPORT BRACKET ATTACHED TO FRAME 329.9 PULLED AWAY AND DAMAGED THE FRAME. THE FASTENERS WERE PULLED THROUGH THE FRAME AND THE FRAME CRACKED AT THE FASTENER HOLES. FRAME WAS REPAISDR DXTA201105120479A/C Pack · noisyBLOWER AND FREON AIR SYSTEM MAKES A NOTICABLE GRINDING/ BUZZING SOUND ACCOMPANIED BY A FRICTION/BURNING ODOR. IT IS MOST APPARENT AT THE AIR EXHAUST. THIS WORSENS THE LONGER IT RUNS.SDR DXTA2011050404573Hinge · vibrationTHERE IS AN INTERMITTENT VIBRATION IN THE CONTROL YOKE. THE VIBRATION IS BOTH TACTILE AND AUDIBLE. IT OCCURS INTERMITTENTLY IN FLIGHT AT ALL ALTITUDES AND AIRSPEEDS. REPLACED IND HINGE ASSY AND ECCENTRIC ON LT OTBD SPOILER. OPS CHECKED SATISFACTORY. ALL WSDR DJFA2011017Master Cylinder · failedDURING TAXI, CREW REPORTED BRAKES SPONGY AND PEDALS SLOWLY LOSING PRESSURE. MX FOUND THE RT BRAKE MIXING VALVE AND PILOT RT BRAKE MASTER CYLINDER FAILED. BOTH COMPONENTS WERE REPLACED.SDR DJFA2011016Torque Tube · twistedDURING A C-CHECK INSPECTION, MAINTENANCE TECHNICIANS FOUND THE LT AND RT ELEVATORS WOULD NOT LINE UP IN THE NEUTRAL POSITION. UPON FURTHER INVESTIGATION, IT WAS DETERMINED THAT BOTH THE LEFT AND RIGHT TORQUE TUBES WERE TWISTED SUCH THAT ALIGNMENT OF THE ELEVASDR 9JLA2093Actuator · defectiveTHE HORIZ STABILIZER ACTUATOR FAILED 3.5 HOURS AFTER INSTALLATION. THE CREW REPORTED THAT DURING PREFLIGHT PREPARATIONS THE EMERGENCY/AUTOPILOT MODE OF THE HORIZONTAL STABILIZER ACTUATOR FAILED. THIS ACTUATOR PN 45AS61023-143, SN ET0050 WAS INSTALLED AFTER FASDR UVCA20110418002Seal · leakingNOSE STRUT WOULD NOT EXTEND, FOUND SEAL LEAKED PRESSURE OUT.SDR 9JLA2091Actuator · defectiveTHE HORIZ STABILIZER ACTUATOR WAS DUE FOR O/H AND WAS REPLACED WITH AN O/H HORIZ STABILIZER ACTUATOR OF A DIFFERENT SN (ET0049). THE UNIT WAS INSTALLED BY A REPAIR STATION. GROUND FUNTIONAL/OPS AND THE OPS CHECK FLIGHT CHECKS WERE SATISFACTORY. DURING THE FIRSDR DJFA2011012Valve · inoperativeDURING TAXI, AFTER LANDING, CREW NOTED LOSS OF BRAKING ACTION FROM THE PILOTS AND COPILOTS RT BRAKE PEDAL. BRAKING ACTION WAS RETURNED AFTER REPEATED PUMPING OF THE PEDAL. MX FOUND POWER BRAKE ANTI-SKID CONTROL VALVE FAILED. THE UNIT WAS REPLACED.SDR 9JLA20110308001Position Switch · defectiveCREW REPORTED THE SPEED BRAKES WERE INOP IN FLIGHT. TROUBLESHOT AND FOUND THE RT FLAP FOLLOW-UP SWITCH TO BE DEFECTIVE. REMOVED THE DEFECTIVE UNIT S/N 38A6. INSTALLED AN OVERHAULED UNIT. FT OK.SDR T17A20110217001Bonding Jumper · brokenSHORTLY AFTER TAKEOFF THE PILOT NOTICED A SLIPPAGE IN THE THE CONTROL PRESSURE WHEN A LT ROLL WAS INPUT ON THE YOKE. AFTER 15 DEGREES OF YOKE TRAVEL, CONTROL PRESSURE RELEASED AND THEN CAUGHT WITH CONTINUED INPUT. CONTROL PRESSURE BEYOND THAT POINT WAS NORMASDR E81RJW304203Pcb · intermittentINVESTIGATED FLIGHT CREW REPORT OF ROLL TRIM NOT RESPONDING TO SELECTED INPUTS AFTER 10 DEGRESS FLAPS SELECTED ON APPROACH. ROLL TRIM OPERATING NORMAL AFTER LANDING. FOUND INTERMITTENT OPERATION OF A194 ROLL TRIM PC BOARD ASSY. REPLACED A194 PC BOARD WITH NSDR DXTA2011021004463Landing Gear · malfunctionedRED GEAR HANDLE LIGHT REMAINED ILLUMINATED IN THE GEAR UP POSITION. VISUALLY INSPECTED LANDING GEAR. PERFORMED GEAR SWING. FOUND MLG INBD DOORS NOT CLOSING DURING RETRACTION CLEANED LT AND RT NLG UPLOCK SWITCHES. OPS CHECKED NORMAL. PERFORMED OPS CHECK OSDR DJFA2011009Power Supply · failedDURING FLIGHT, CREW REPORTED SMOKE AND FUMES IN THE COCKPIT. ACFT DIVERTED AND, AFTER LANDING, CREW REPORTED SMOKE DISSIPATED WHEN CTR PEDESTAL LIGHTS WERE EXTINGUISHED. MAINTENANCE FOUND THE INSTRUMENT PANEL DIMMER OUTPUT INCORRECT AND THE ALTITUDE AWARENESDR E81RJW304162Transmitter · out of adjustFLIGHT CREW REPORTED FLAP ASSYMETRY ANNUNCIATOR LIGHT INDICATION AND SLIGHT RT ROLL ON APPROACH, WHEN FLAPS EXTENDED TO 20 DEGREE POSITION. FOUND LT FLAP FOLLOW-UP SWITCH ASSY. S517 AND LT FLAP POSITION TRANSMITTER MT111 ADJUSTMENTS OUT OF SERVICE LIMITS ANDSDR E81RJW304141Door · out of rigAFTER DEPARTURE, FLIGHT CREW NOTED RED WARNING LIGHT IN LANDING GEAR CONTROL HANDLE REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. FLIGHT CREW RETURNED TO DEPARTURE, LANDING NORMAL. DURING TROUBLESHOOTING OF RETRACTION/EXTENSION SYS, AT REDUCED (950 PSISDR DXTA2011020304448Door · out of rigAFTER TAKEOFF, GEAR HANDLE "RED" LIGHT WOULD NOT EXTINGUISH. REDUCED HYD PRESS TO 950 PSI IAW MM 32-00-00. FOUND NLG DOORS RIGGED TOO TIGHT. ADJUSTED DOORS IAW MM 32-20-00. LANDING GEAR OPS CHECKED GOOD IAW MM 32-00-00.SDR DXTA2011020104439Switch · malfunctionedON FINAL, EXTENDED LANDING GEAR. SOUNDED NORMAL BUT NO GREEN INDICATION. MISSED APPROACH AND ENTERED CLOSED TRAFFIC. CYCLED GEAR UP AND GOT NORMAL INDICATIONS. ON FINAL AGAIN EXTENDED GEAR AND GOT NORMAL INDICATIONS. LANDED UNEVENTFULLY. TROUBLESHOT LANDSDR R71A20110126001Drain · openPILOT REPORTED FUEL LEAKING FROM RIGHT WING TIP WHILE EN ROUTE. INSPECTION OF THE WING TIP REVEALED OUTBOARD VENT SURGE TANK "SUMP DRAIN" WAS LOCKED IN THE OPEN POSITION. AIRCRAFT STARTED LEAKING FUEL AT THE WING TIP AFTER FLIGHT CONFIGURATIONS ALLOWED FUEL SDR E81RJT229291Switch · shortedINVESTIGATED FLIGHT CREW REPORT OF THE SPEEDBRAKE CNTRL SYS CIRCUIT BREAKER TRIPPING AND NOT RESETTING. DURING TROUBLESHOOTING FOUND AN INTERNAL SHORT IN THE RT FLAP FOLLOW-UP SWITCH ASSY. REPLACED THE RT FOLLOW-UP SWITCH ASSY WITH AN O/H REPLACEMENT EXCHANGSDR ISYA20110106Engine · failedDURING CLIMBOUT, NOTICED A MASTER CAUTION LIGHT FLASH. THEN A FEW SECONDS LATER IT DID IT AGAIN, LOOKED ALL AROUND AND SAW NOTHING. THEN IT CAME ON AND STAYED ON AND IT WAS THE RT OIL PRESSURE LIGHT. LOOKED AT THE GAUGE AND THE NEEDLE WAS IN THE RED. WENT TOSDR DJFA2011001Bracket · crackedDURING A SCHEDULED MX VISIT, WHILE PERFORMING A HORIZ STABILIZER ROLLER INSP OF THE HORIZ STABILIZER INBD RIB AND BRACKET ASSEMBLIES, THE RT BRACKET WAS FOUND CRACKED. THE BRACKET WAS REPLACED.SDR DBCA201101020001Starter Gen · failedWHEN PREPARING TO DEPART BZN NR 1 ENGINE WOULD NOT SPOOL. TROUBLESHOOTING BY MAINTENANCE FOUND STARTER/GENERATOR HAD FAILED. REPLACED STARTER/GENERATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR DXTA2011010304387Control Cable · contaminatedLT THRUST LEVER BINDING; UNABLE TO MOVE. WORKED NORMALLY ON TAXI OUT, TAKEOFF, AND CLIMBOUT. ONCE LEVELED OUT AT ALTITUDE IT WAS EXTREMELY DIFFICULT TO REDUCE POWER. WERE ABLE TO MOVE LEVER TO CUTOFF ONCE PARKED. FOUND MOISTURE INGRESSION PRESENT IN LT AFT SDR DXTA2011010304394Indicator · inoperativeLANDING GEAR, DOWN LIGHTS DID NOT ILLUMINATE WHEN GEAR WAS SELECTED DOWN OR WHEN LIGHTS WERE TESTED VIA ROTARY TEST. THE GEAR WAS NOT BLOWN DOWN. INSTALLED & SAFETIED A NEW LIGHT ASSEMBLY IAW DWG 32-01-01-02, REV 01 - DEC 1, 2007 IAW; AMM 32-00-00-301. LIGHTSDR E81RJT22919Wire · broken(E81R) DURING DESCENT "A/C FAIL" ANNUNUNCIATOR LIGHT ILLUMINATED AND EMERGENCY PRESSURIZATION SYS ACTIVATED. DURING TROUBLESHOOTING FOUND WIRE E067-P0108B-22 WIRE BROKEN AT BLEED AIR OVERPRESSURE SWITCH CONNECTOR P0108. REPAIRED WIRING AT CONNECTOR AND REPLACSDR DBCA2010122100030Wire · brokenON DESCENT "AIR CONDITIONING FAIL" ANNUNCIATOR ILLUMINATED & EMERGENCY PRESSURIZATION ACTIVATED. PER ACFT CHECKLIST DESCENDED TO 10,000 FT & CLOSED BLEED AIR SOURCES. LANDING WAS UNEVENTFUL. TROUBLESHOT AND FOUND WIRE BROKEN IN AIR CYCLE TURBINE OVER PRESSUSDR DJFA2010037Control Cable · severedDURING CRUISE FLIGHT, THE CREW NOTED THE FLAP ASSYMETRY LIGHT AND MASTER CAUTION LIGHT ILLUMINATED. DURING TROUBLESHOOTING MX FOUND THE LT AND RT FWD FLAP CABLES SEVERELY CORRODED AND SEVERED AT THE MID BELL CRANK FERRULE. MX REPLACED BOTH CABLES.SDR DJFA2010036Power Supply · failedACFT DIVERTED, DUE TO SMOKE SMELL IN COCKPIT. EMERGENCY WAS DECLARED. MX EVALUATED AND CONFIRMED "BURNED ELECTRICAL" ODOR FROM ALTITUDE AWARENESS PANEL. ALSO FOUND INSTRUMENT LIGHT POWER SUPPLY OUTPUT AT 118VAC. R & R THE INSTRUMENT LIGHT POWER SUPPLY AND SDR 9JLA20111107001Rccb · defectiveTHE CREW REPORTED THE LT BUS TIE CIRCUIT BREAKER TRIPPED DURING THE PREFLIGHT CHECKS. TROUBLESHOOTING FOUND THAT THE LEFT BUS TIE RCCB P/N 45AS88810-003 S/N 001194 TO BE DEFECTIVE. INSTALLED A NEW RCCB, FUNCTIONAL CHECKS SATISFACTORY (RCCB = REMOTE CONTROLLESDR DJFA2010035Seal · looseDURING CLIMB, CREW NOTED A LOUD SQUEAL FOLLOWED BY A POP AND A STEADY LOSS OF CABIN PRESSURE (ABOUT 2000 FPM). EMERGENCY PROCEDURES WERE EXECUTED AND EMERGENCY WAS DECLARED. ACFT LANDED SAFELY. MX INSPECTED THE ACFT AND FOUND THE MAIN ENTRY DOOR SEAL HAD COSDR DJFA2010034Aap · odorMX TECH NOTED A BURNING SMELL IN THE COCKPIT WHILE TROUBLESHOOTING A LIGHTING PROBLEM ON THE PILOT'S AUDIO PANEL. THE ODOR APPEARS TO HAVE COME FROM THE ALTITUDE AWARENESS PANEL (AAP). NO FIRE OR SMOKE WAS NOTED BUT THE AAP PRODUCED A STRONG ELECTRICAL BURNI
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