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 6CBA2017072717169Lens · missingDURING INSPECTION THE TAIL BEACON LENS WAS FOUND MISSING. REMOVED BEACON ASSEMBLY AND INSTALLED A NEW ONE IAW 33-40-00 AND ENGINEERING ORDER NT-EO-0717-07_REV IR, OPS CHECKED NORMAL.SDR 9JLA2017071215775Wheel · defectiveDURING AN AIRCRAFT POSTFLIGHT INSPECTION. THE MAINTENANCE TECH WAS COMPLETING A CHECK OF THE AFT EQUIPMENT BAY HEARD A BANG. THE TECH INVESTIGATED INTO THE CAUSE OF THE NOISE AND FOUND THAT THE RT MAIN LANDING GEAR WHEEL ASSY. WAS MISSING THE NUT END OF ONE OFSDR YQKA201706140001Indicator · no indicationONLY TWO GREEN LIGHTS AFTER SELECTING GEAR DOWN. RIGHT MAIN GEAR NO INDICATION.SDR 2017F00121Anti-Skid Sys · malfunctionedUNEVENTFUL DEPARTURE. THE ANTI-SKID CHECK WAS CONDUCTED. NO ABNORMALITIES OBSERVED WITH THE ANTI-SKID AT THIS TIME. ON ARRIVAL, SET UP FOR THE VISUAL APPROACH. ON TOUCHDOWN NOTICED DID NOT HAVE NORMAL BRAKING AVAILABLE AND DECIDED TO TURN THE ANTI-SKID OFF TSDR YQKA2017061400002Warning Light · illuminatedCABIN PRESSURE LOW LIGHT ILLUMINATED.SDR E81R2017041130512Bolt · misinstalledDURING REINSTALLATION OF THE RT MLG SIDE STRUT ASSY. FOLLOWING SCHEDULED OVERHAUL, NOTED CENTER PIVOT BOLT INSTALLED IN REVERSE IAW MM 32-13-00 AND SB 2649 R1, CAUSING INTERFERENCE WITH ADJACENT COMPONENTS. REINSTALLED IAW CMM 32-13-00, OPS NORMAL.SDR FCPR201704196692Contactor · burnedINSPECTION REVEALED RIGHT TAIL DEICE MOSFET CONTACTOR BOX LOCATED IN EMPENNAGE OF AIRCRAFT, FAILED INTERNALLY AND CAUGHT FIRE. RESULTING FIRE DAMAGED OTHER COMPONENTS LOCATED IN THE VICINITY.SDR PAIR20170308S3720Engine · making metalDURING PRE-PURCHASE SURVEY, INSPECTED ENGINE OIL FILTER AND FOUND LARGE AMOUNT OF METAL DEBRIS. ENGINE REMOVED FROM SERVICE AND SENT TO OVERHAUL FACILITY FOR REPAIR OR OVERHAUL.SDR 9JLA2017030611001Indicator · failedTHE RIGHT ITT GAUGE WAS REPLACED WITH AN OVERHAULED UNIT. THIS INDICATOR FAILED 11 HRS AFTER INSTALLATION.SDR FJTA2016112200091O-Ring · cutDURING DECENT, CREW NOTICED LOW LT AND RT HYDRAULIC PUMP PRESSURE ANNUNCIATORS ILLUMINATED. CREW EXTENDED GEAR AND FLAPS AND DECLARED EMERGENCY BEFORE LANDING. CREW USED NITROGEN BOTTLE FOR BRAKING. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUSDR 9JLA2016111810525Switch · defectiveTHE FLIGHT CREW REPORTED THAT THE NR 2 ENGINE STARTED NORMALLY, THEY THEN MOVED THE START SELECT SWITCH INTO THE NR 1 POSITION, THE NR 1 STARTER AUTOMATICALLY ENGAGED WITHOUT ENGAGING THE START SWITCH. TROUBLESHOOTING IDENTIFIED START SWITCH TO BE DEFECTIVE. TSDR WC72201609001Fastener · brokenIT WAS NOTED THAT THERE WERE THREE RIVET HEADS MISSING FROM THE RT INLET LIPSDR 9JLA201611187890Motor · overheatedCREW REPORTED AFTER THE AIRCRAFT WAS SHUT DOWN AND OPENING THE BAGGAGE DOOR, THE PILOT NOTED PRESENTS OF SMOKE IN THE TAILCONE WITH THE AIR CONDITIONING SYSTEM OPERATING. THE AIRCRAFT WAS SHUT-DOWN AND INVESTIGATED THE SOURCE OF THE SMOKE. CONFIRMED NO FIRE. FSDR 9JLA2017071412189Wheel · damagedDURING A POST MAINTENANCE CHECKS IT WAS NOTED THAT THE RT MAIN LANDING GEAR WHEEL HAD A BROKEN THRU-BOLT. THIS WHEEL ASSY. WAS OVERHAULED THREE MONTHS PRIOR, IT HAD 121.0 HRS AND 88 LANDINGS ON THE WHEEL ASSY BEFORE THE BOLT FAILED. THE DEFECTIVE WHEEL WAS RESDR 9JLA2016093012189Bolt · brokenDURING A WALK-A-ROUND FOLLOWING A SCHEDULED MX INSPECTION EVENT IN JUNE, A BOLT FOR THE RT MLG WHEEL ASSY WAS FOUND BROKEN. A/C WAS IMMEDIATELY REMOVED FROM SERVICE FOR REPAIRS. THE WHEEL WAS REMOVED FROM THE AIRCRAFT WHERE IT WAS DISCOVERED THE REMAINING BRSDR 9JLA201610209322Pcb · failedCREW REPORTED THAT DURING FLIGHT THE "RUDDER BOOST FAIL" ANNUNCIATOR ILLUMINATED AND REMAINED ON. MAINTENANCE TROUBLESHOT THE DISCREPANCY AND VERIFIED THE REPORT AND FOUND THAT THE NO. 2 FLIGHT CONTROL COMPUTER (FCC) FAILED. AN OVERHAULED FCC WAS INSTALLED ANDSDR 2016FA0000136Starter Gen · failedRIGHT STARTER GENERATOR FAILED IN FLIGHT, ACFT RETURNED TO BASE REMOVED RT STARTER GENERATOR AND FOUND THE FORWARD BEARING NEXT TO THE COOLING FAN FAILED.SDR DJFA20160314001Unknown · malfunctionedON LANDING, CREW REPORTED LOSS OF BRAKES. ACFT EXITED THE END OF THE RUNWAY & WAS DAMAGED. THIS SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.SDR V7PA2016F00078Cabin Pressure · malfunctionedAFTER DEPARTING HPN AND CLIMBING THROUGH APPROXIMATELY 9000-10000 FT THE CREW INDICATED THAT THEY FELT PRESSURE CHANGES IN THEIR EARS. THE CABIN PRESSURE VSI WAS FLUCTUATING, SHORTLY THEREAFTER IT INDICATED A FULL-RATE CABIN CLIMB, TOTAL DEPRESSURIZATION. THSDR DJFA20160202001Seal · leakingSTRAIGHT LEVEL FLIGHT AT FL270 CREW RECEIVED AMBER AIR CONDITIONING FAIL LIGHT FOLLOWED BY A RAPID DECOMPRESSION. O2 MASK DEPLOYED, THEN RECEIVED CABIN LOW PRESS LIGHT. ACCOMPLISHED CHECKLIST PROCEDURES & DID NOT RESOLVE THE ISSUE. ACFT LANDED SAFELY AT THESDR DJFA20151214001Unknown · leakingCREW EXPERIENCED A SMOKEY SMELL ON CLIMB OUT WITH ANTI-ICE ON. THE SMELL DISSIPATED WHEN ANTI-ICE WAS TURNED OFF. MX FOUND THE SPIRAL WRAP FROM THE ANTI-ICE DUCTING. THE BLEED LEAK WAS ISOLATED & REPAIRED. THE SPIRAL WRAP WAS REPLACED & LEAK OPERATIONS CHESDR WC7220151204001Fitting · crackedA HIGH FREQUENCY EDDY CURRENT INSPECTION OF THE HORIZONTAL STABILIZER REAR SPAR FITTING LUGS WAS PERFORMED BY IAW MM 55-50-00-601 AND MM 20-80-03-201. THIS INSPECTION INCLUDES THE CROSS HATCHED AREAS OF THE LUGS WITH A MINIMUM RADIUS OF 0.5" OUT FROM EACH RASDR MGOR20151014001Rib · crackedDURING A D CHECK INSPECTION, FOUND HORIZONTAL STABILIZER RIBS CRACKED AT HSS 350. PERFORMED A BORESCOPE INSPECTION OF THE HORIZONTAL STABILIZER RIBS IAW CHAPTER 55-10-00 IN THE MODEL 400 & 400A MM. FOUND A TOTAL OF 7 RIBS WITH CRACKS, 2 45A2112-0005, 2 45A21SDR 9JLA201512097875Oxygen Mask · defectiveREPORTED THAT DURING THE POST FLIGHT CHECKS, THAT THEY WERE UNABLE TO EXHALE THROUGH THE PILOT'S OXYGEN MASK. THE DEFECTIVE MASK WAS R & R WITH AN OVERHAULED UNIT. OPERATIONS CHECKED OK.SDR BTVR2015092901Anti-Skid Sys · faultyAFTER LANDING, TAXING INTO THE GATE, NORMAL BREAKING ACTION WAS LOST. UPON TURNING THE ANTI-SKID SWITCH TO THE OFF POSITION BRAKING CONTROL WAS RETURNED. THE ANTI-SKID SYS WAS DEFERRED & THE FLIGHT WAS CONTINUED. SYS WILL REQUIRE FURTHER TROUBLESHOOTING TO SDR IKMA20151001001Light · inoperativeDURING APPROACH, FOR SCHEDULE FUEL STOP THE NLG DOWN & LOCKED INDICATING LAMP FAILED TO PROVIDE A POSITIVE INDICATION. PILOTS FOLLOWED THE CHECKLIST BY CYCLING THE GEAR UP THEN DOWN AGAIN WITHOUT GETTING A POSITIVE INDICATION FOR DOWN & LOCKED. PILOTS THEN FSDR 2015FA0000382Computer · intermittentYAW DAMP DISENGAGED SEVERAL TIMES DURING LANDING DECENT.SDR 2015FA0000323Door · crackedFOUND LT MLG DOOR CRACKED AT THE FORWARD HINGE AREA.SDR UG8A2015070602Former · crackedLEFT INBD MLG DOOR FWD FORMER CRACKED. CRACK IS 1" LONG IN THE INSIDE RADIUS STARTING AT OTBD EDGE OF DOOR & TRAVELING INBD.SDR UG8A2015070601Former · crackedNUMBER 2 THRUST REVERSER FAN NOZZLE AFT FORMER RING CRACKED.SDR MGOR20150706001Rib · crackedSUBMITTING THIS SDR DUE TO THE LOW ACFT TOTAL TIME & INITIAL INSPECTION REQUIREMENTS CONTAINED IN AD 2014-15-15. DURING AN A CHECK INSPECTION, THE CUSTOMER REQUESTED EARLY COMPLIANCE WITH AD 2014-15-15, INSPECTION OF THE HORIZONTAL STABILIZER RIBS FOR FATIGUESDR CIER201506190001Engine · flamed outWHILE ENROUTE, THE NR 2 ENGINE FLAMED OUT AT APPROXIMATELY FL380. THE ACFT, DIVERTING FOR A LARGE CELL DEPICTED ON THE RADAR, THE CELL WAS DEPICTED OVER DESTINATION. THE ACFT HAD EXPERIENCED 3 TO 4 SUSPECTED LIGHTNING STRIKES AND WAS DESCENDING THROUGH FL380SDR 2015F00082Switch · defectiveCREW REPORTED THAT THE RIGHT ENGINE WOULD NOT START. MAINTENANCE VERIFIED AND TROUBLESHOT DISCREPANCY TO THE DISENGAGE SWITCH. THE SWITCH WAS REMOVED AND REPLACED, WITH SAME PART NUMBER, AND OPERATION CHECKED SATISFACTORY. THE AIRCRAFT WAS APPROVED FOR RETURN SDR 9JLA201506027869Fire Loop · out of positionTHE CREW REPORTED THAT AFTER TAKEOFF & CLIMBING OUT THROUGH 2000 FT MSL THE LT ENG FIRE WARNING SYS ACTIVATED. THE LT ENG WAS BROUGHT BACK TO IDLE IAW THE CHECKLIST & AFTER 3 - 4 SECONDS THE FIRE WARNING EXTINGUISHED. THE CREW COMPLETED THE CHECKLIST ITEMS & SDR DJFA20150528001Warning System · false activationDURING LANDING, CREW COULD NOT GET A LANDING NOSE GEAR DOWN GREEN LIGHT. TEST WOULD NOT LIGHT BULB EITHER. DECLARED EMER & CONDUCTED FLY-BY OF TOWER, FOR VISUAL CONFIRMATION OF GEAR DOWN. UPON LANDING THE NOSE GEAR LIGHT ILLUMINATED. LANDING & TAXI WITHOUT SDR DJFA20150525001Door Seal · failedTHE MAIN DOOR SEAL FAILED IN FLIGHT & THE PAX OXYGEN MASKS DROPPED. PAXS DONNED OXYGEN MASKS WHILE CREW PROCEEDED TO DIVERT FLIGHT & DESCEND BELOW FL 120. AN EMER LANDING WAS DECLARED & THE ACFT LANDED WITHOUT FURTHER INCIDENT. R & R THE DOOR SEAL. LEAKS &SDR 9JLA201506248079Uplock Switch · intermittentON SEVERAL OCCASIONS THE CREW HAD REPORTED AN INTERMITTENT , LG UNLOCK ANNUNCIATOR, ILLUMINATING IN FLIGHT. TROUBLESHOOTING DETERMINED THAT THE NLG UPLOCK & DOWNLOCK WERE DEFECTIVE. THE SWITCHES WERE REPLACED WITH NEW PN MS24331-1 & RIGGED IAW THE AMM 32-20-SDR VIB42015FA0000091Pcb · deactivatedIGNITER WOULD NOT FUNCTION, NO POWER TO UNIT. NO POWER TO UNIT IN IGNITER ON OR STANDBY POSITION OR DURING START. ENGINE LIP HEAT VALVE NOT POWERED WITH BATTERY ON. POWERS CLOSES VALVE BATTERY ON. OPENS ON ACTIVATION BY REMOVING POWER. DISCOVERED SOMEONE HASDR 1KSA2015FA0000087Cabin Pressure · leakingCREW REPORTED THEY STARTED LOOSING CABIN PRESSURE AT FL 24, DECENT TO LOWER FLIGHT LEVEL WAS INITIATED AT WHICH TIME THE CREW REPORTED THEY HEARD A LOUD WHISTLE AT THE MAIN ENTRY DOOR.SDR 9JLA201502267983Oxygen Mask · leakingDURING THE POST FLIGHT INSPECTIONS THE PILOTS OXYGEN MASK WAS LEAKING OXYGEN FROM THE SUPPLY HOSE AT THE FLOW INDICATOR. THE DEFECTIVE MASK ASSEMBLY PN 174262-12, SN 15072 WAS REMOVED & THE MASK WAS REPLACED WITH A LOANER MASK.SDR 9JLA2015022604035Strut · leakingAFTER TAKEOFF THE CREW REPORTED THAT AFTER THE LG WAS RETRACTED THAT THE NLG DEPLOYED TO THE DOWN POSITION. TROUBLESHOOTING & INSPECTION FOUND THAT THE NLG HAD AN INTERNAL LEAK. THE INTERNAL LEAK IN THE STRUT WAS PREVENTING THE STRUT FROM FULLY EXTENDING AFTSDR 9JLA2015012811961Wire Harness · defectiveDURING CLIMB AFTER TAKEOFF, IT WAS REPORTED THAT THE LT ENG ITT GAUGE FAILED. TROUBLESHOOTING FOUND THE LT ENG T1 WIRING HARNESS ASSEMBLY DEFECTIVE & REQUIRED REPLACEMENT PN 3119094-1. THE DEFECTIVE WIRING HARNESS WAS R & R WITH A NEW CONDITION HARNESS. OPESDR 9JLA2015012807298Pressure Switch · faultyFLIGHT CREW REPORTED THAT THE NR 1 ENG OIL BYPASS LIGHT ILLUMINATED DURING FLIGHT WITH NO SECONDARY INDICATIONS. TROUBLESHOOTING CHECKED THE ENG OIL FILTER FOR BLOCKAGE, NO BLOCKAGE FOUND. FURTHER TROUBLESHOOTING REVEALED THAT THE OIL BYPASS PRESS SWITCH WAS SDR ZKFR2014041201Bolt · looseLEFT MAIN TIRE FOUND FLAT AFTER PARKING. TECH REPORTED 5 OUT OF 7 WHEEL HALF THROUGH BOLTS LOOSE CAUSED WHEEL HALF O-RING TO SQUEEZE OUT AND TIRE WENT FLAT. THE TIRE THAT WENT FLAT WAS INSTALLED 11/26/2014 AS AN ASSEMBLY OVERHAULED BY A VENDOR WITH TIRE INSTASDR 9JLA2014122604978Controller · defectiveCOULD NOT CONTROL THE TEMPERATURE FOR THE FLIGHT DECK OR CABIN. TROUBLESHOOTING FOUND THE LOW LIMIT SENSOR CONTROLLER & THE LOW LIMIT PROPORTIONING VLV BOTH TO BE DEFECTIVE, UNITS REPLACED. OPERATIONS CHECKED OK.SDR 9JLA2014123104021Radar · interferenceINTERMITTENT ISSUE WITH COMM STATIC. EXTENSIVE TROUBLESHOOTING WAS COMPLETED. THIS RADIO STATIC ISSUE HAD EVERYONE STUMPED. EVENTUALLY THE SOURCE OF THE STATIC WAS TRACKED DOWN TO A RF INTERFERENCE COMING FROM THE RADAR UNIT. NO CREW REPORTS ON ANY FAULTS SDR 9JLA2014122604062Radar · defectiveTHE CREW REPORTED THE WEATHER RADAR AS INOPERATIVE. TROUBLESHOOTING FOUND THE RADAR UNIT DEFECTIVE. PN 622-8440-003 SN 2091. TOTAL TIME & CYCLES IN SERVICE OF RADAR, 58.1 TT & 42 TC AFTER AN OVERHAUL DATED JULY 01 2014.SDR DJFA20141019001Control Valve · faultyAIRCRAFT DIVERTED FOR UNCONTROLLABLE HEAT, WITH VISIBLE SMOKE IN COCKPIT. THE COCKPIT TEMP CONTROL VALVE WAS REPLACED. IT WAS ALSO NOTICED THAT THE TEMP CONTROL VALVE LINES WERE SWAPPED. LINES WERE ALSO INSTALLED IN CORRECT POSITION. OPS CHECKS WERE GOOD ASDR 9JLA201410134977Motor · overheatedTHE VAPOR CYCLE AC SYS WAS INOPERATIVE. TROUBLESHOOTING FOUND THE AC COMPRESSOR DRIVE MOTOR HAD OVERHEATED BY EVIDENCE OF PEELING PAINT ON UNIT. THIS DRIVE MOTOR WAS INSTALLED A MONTH & A HALF PRIOR & FAILED WITH 55 HOURS OF OPERATION. THE DRIVE MOTOR PN 11SDR 9JLA2014122905065Step · failedDURING PAX DEPARTURE FROM ACFT THAT THE LOWER STEP OF THE MAIN ENTRY STAIRS FAILED. THE LOWER STEP & SUPPORT CONTROLLER WAS REPLACED WITH NEW.
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