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 = '750' 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 = '750' 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 DXTA2013042905363Elevator System · malfunctionedON LT BASE TO FINAL WITH GEAR AND FLAPS 35 AND 145KTS WITH AUTOPILOT OFF. ELEVATOR PRESSURE STUCK WHEN APPLYING DOWNWARD PRESSURE. IT TOOK EXCESSIVE FORCE TO PULL YOKE FWD AND AFT AND LANDING WAS MADE MOSTLY WITH TRIM.SDR DJFA20130423002Bracket · crackedCREW REPORTED OF A NOTICEABLE "SLACK" IN THE YOKE CAUSING A DELAY OF INPUT FOR A TURN. NOTED AT ALTITUDE WITH THE AUTOPILOT ON THE WINGS WOULD SLOWLY ROLL AND THEN A MECHANICAL "BUMP" COULD BE FELT CORRECTING, THIS WOULD CYCLE ABOUT EVERY 10-15 SECONDS. MX SDR DXTA2013040105346Warning Message · illuminatedPITCH FEEL FAIL AMBER MESSAGE ILLUMINATED ON CLIMB OUT WITH AUTOPILOT ON. DISCONNECTED AUTO PILOT AND PITCH FELT HEAVY ON BOTH CONTROLS. MESSAGE EXTINGUISHED BEFORE LANDING BUT CONTROLS REMAINED HEAVY. OPS CHECKED SYS SEVERAL TIMES WITHOUT FAULT. REPLACED SDR DXTA2013040105345Flap System · malfunctionedSELECTING FLAPS 5 TO 15 HAD FLAPS FAIL CAS MESSAGE. WOULD NOT RESET FOLLOWED CHECKLIST AND LANDED. FOLLOWING ACFT RESTART FOR TAXI REPO. NO FLAP FAULTS PRESENT. NO DISCREPANCIES NOTED. WORKED IAW MM 27-50-00.SDR DJFA20130326001Acm · seizedCREW REPORTED THAT THE COCKPIT A/C PACK EMMITTED SMOKE AND THE AIR TEMPERATURE WAS UNCONTROLLABLE. MX FOUND THE ACM HAD FAILED AND REPLACED THE UNIT.SDR DXTA2013032805341Fuel Sys · ventingACFT HAD JUST LEVELED OFF AT FL250, AMBER CAS MESSAGE, WING TANK OVER FULL RT, ILLUMINATED. FUEL OBSERVED VENTING OUT OF RT WING TIP. CTR WING TRANSFER SWITCHES WERE IN NORM, RT WING FUEL TANK HAD 3300 LB OF FUEL, & APPROX 300 LB OF FUEL IN CENTER TANK. CASDR DXTA2013032505334Bulb · inoperativeON FINAL WHEN GEAR SELECTED DOWN BOTH LT MAIN GREEN LIGHTS WERE INOPERATIVE. PERFORMED FLYBY OF TOWER CONFIRMED ALL GEAR DOWN. RAN GEAR WOULD NOT EXTEND CHECKLIST AND BLEW GEAR DOWN. ALSO RAN ROTORY TEST AND HAD NO GEAR HORN. LANDED WITH NO FURTHER PROBLEMSDR DXTA2013032505333Uplock Switch · out of adjustIMMEDIATELY AFTER TAKEOFF, WHEN GEAR HANDLE WAS SELECTED TO UP POSITION, GEAR UNLOCK LIGHT FLASHED 5 OR 6 TIMES AS NOSE GEAR REPEATED TO MAKE LOUD BANGING NOISES BEFORE FINALLY LOCKING IN UP POSITION WITH NORMAL INDICATIONS. INSPECTED AND FOUND THAT THE NOSE SDR 2013FA0000200Seal · leakingDURING CRUISE, FLIGHT LEVEL 41.0, FLIGHT CREW BEGAN TO SMELL SMOKE AND NOTICED THE COCKPIT PAC WAS RUNNING HOT AND UNCONTROLLABLE. RAN CHECKLIST AND SHUTDOWN PAC. APPROXIMATELY FIVE MINUTES LATER, NOTICED THE CABIN PAC WAS ALSO RUNNING HOT AND UNCONTROLLABLE. SDR AWKA20130404001Connector · unsecureFIGHT CREW REPORTED THAT ON LIFT OFF, PILOT RECEIVED A STICK SHAKER AND RED AIRSPEED TAPE STALL INDICATION THAT LASTED 2-3 MINUTES. LEVELED OFF AT 2,500 - 3,000 FT AND DECLARED AN EMERGENCY. RETURNED AND LANDED UNEVENTFULLY. FUTHER INVESTIGATION FOUND THE NSDR DXTA2013032005326Acm · failedWHILE IN TAKEOFF POWER AND ON CLIMBOUT, BLUE SMOKE WAS OBSERVED TO BE VENTING INTO THE FLIGHT DECK. SMOKE WAS EVIDENT UNTIL SUCH TIME AS POWER REDUCTION OCCURRED, THEN THE SMOKE BEGAN TO DISSAPATE. RAN APU WITH NORMAL BLEED AIR AND MAX BLEED AIR. ISOLATION VSDR DXTA2013031905323Wheel · vibratesTAKEOFF ABORTED PRIOR TO 80 KTS DUE TO NOSE WHEEL SHIMMY & EICAS MESSAGE. R & R BOTH NOSE WHEEL ASSEMBLIES DUE TO VIBRATION ON TAKEOFF ROLL. ALL WORK IAW MM 32-41-01.SDR DXTA2013031905321Control Valve · malfunctionedAMBER "CABIN ALTITUDE" CAS MESSAGE ILLUMINATED IN FLIGHT APPROX 10 MINUTES INTO LEVEL FLIGHT AT FL 400. CABIN BEGAN TO DEPRESSURIZE. IMMEDIATELY DESCENDED TO 10,000 FT AND LANDED. R & R THE MANUAL CONTROL VALVE IAW MM 21-30-00. OPS CHECKED GOOD.SDR XCGA20130321001Windshield · crackedTHE RIGHT WINDSHIELD CRACKED WHILE CLIMBING THROUGH FL 200. THE WINDHIELD HEAT HAD BEEN ON CONTINUOUSLY SINCE TAKEOFF FROM KAGC. THE PILOT STATED HE HEARD A LOUD POPPING NOISE JUST PRIOR TO THE WINDSHIELD CRACKING. THE PILOT FLYING DECLARED AN EMERGENCY TO SDR DJFA20130318001Brake · dirtyCREW REPORTED DURING LANDING ROLLOUT WHEN THE LT BRAKE IS APPLIED NOTHING HAPPENS INITIALLY, THEN AFTER CONSIDERABLE PRESSURE IS APPLIED THE LT BRAKE, GRABS PRETTY HARD AND PLANE YAWS TO THE LT. MAINTENANCE INSPECTED THE BRAKE SYS AND TAXI CHECKED THE ACFT, TSDR DXTA2013031805319Acm · failedBURNING ODOR COMING FROM COCKPIT. TURNED COCKPIT PACK OFF AND ODOR DISSIPATED. R & R AFT ACM IAW MM 21-51-00. ACM OPS & LEAK CHECKS GOOD.SDR XCGA20130311001Actuator · failedPILOT WRITE UP "PITCH FEEL FAIL AMBER CAS MESSAGE ILLUMINATED IN FLIGHT. ABNORMAL AMOUNT OF AFT ELEVATOR REQUIRED DURING LANDING". FAULT OCCURED SHORTLY AFTER TAKEOFF FROM KAGC, PILOT RETURNED TO KAGC. TROUBLESHOOTING REVEALED THE RIGHT ELEVATOR PITCH FEEL SDR DXTA2013030805311Unknown · malfunctionedDURING CLIMBOUT, CYAN YAW DAMPER FAIL UPPER A MESSAGE APPEARED. PFD WAS SELECTED TO RT SIDE AND UPPER RUDDER B WAS ILLUMINATED. MESSAGE STAYED ON FOR REMAINDER OF FLIGHT AND TAXI IN. COULD NOT DUPLICATE DISCREPANCY ON GROUND. PERFORMED YSAC SYS OPS CHECKSSDR DXTA2013030405305Compressor · failedAFTER ENGINE SHUTDOWN WITH THE APU RUNNING AND BOTH COCKPIT AND CABIN PACKS ON, THE ACFT STARTED HAVING SMOKE IN THE CABIN COMING OUT OF THE OVERHEAD WEMACS. THE CABIN PACK WAS TURNED OFF AND THE SMOKE SUBSIDED. INSPECTED PAC FOR CABIN (FWD) NO SIGNS OF EXTESDR DXTA2013021905293Wheel · wornVIOLENT NOSEWHEEL SHIMMY ON TAKEOFF ROLL. BEGAN RT AFTER TAKEOFF POWER APPLIED AND ABORTED AT APPROX 30 KTS. REMOVED BOTH NOSE WHEELS AND TIRE ASSEMBLIES AND INSTALLED TWO OVERHAULED WHEELS WITH NEW TIRES REF AMM 32-41-01. TAXI CHECKED GOOD.SDR DXTA2013021805294Control Handle · malfunctionedCLIMBING THROUGH APPROX FL210 AT APPROX 310 KTS WITH AUTOPILOT ENGAGED THE SLATS EXTENDED UNCOMMANDED. FIRST INDICATION WAS THE "RUMBLE" THEY MAKE WHEN EXTENDED. WE COULD VISUALLY SEE THEM EXTENDED AND THE FLIGHT CONTROL SYNOPTIC ALSO INDICATED SLATS EXTENDED.SDR 2013FA0000106Display · failedTHREE MINUTES INTO FLIGHT DU5 (PFD2) WENT BLANK FOR 1 SECOND. 5 SECONDS LATER TUBE WENT BLACK. A FEW SECONDS LATER BURNING INSULATION WAS SMELLED AND SAW SMOKE FROM PFD OR RT SIDE. DECLARED EMERGENCY LANDING. SMOKE CLEARED WITHIN SECONDS AND LANDED IN 10 MISDR DXTA2013021505289Downlock Switch · intermittentWHEN GEAR HANDLE WAS SELECTED TO THE DOWN POSITION FOR LANDING, MAIN GEAR INDICATIONS WERE GREEN, NOSE GEAR DID NOT INDICATE GREEN. UNLOCK LIGHT WAS NOT ILLUMINATED. FOLLOWED THE CHECKLIST PROCEDURE WHICH DIRECTED US TO BLOW THE GEAR DOWN AND PULL THE NOSE GEASDR DXTA201302145286Engine · sparksAFTER ENGINE START, LINEMAN ADVISED HE NOTICED SPARKS AND BLACK SMOKE OCCASIONALLY COMING FROM APU EXHAUST. SHUTDOWN APU.SDR DXTR20130214001Cable · bindingRIGHT BRAKE IS BINDING AND AT HIGH SPEED IT IS ALMOST UNUSABLE. FOUND RT BRAKE TELEFLEX CABLE BINDING WITH A RATCHETING EFFECT THAT IS FELT IN BOTH RT BRAKE PEDALS(CAPTAINS AND F/O'S) AND TRANSMITTED TO BRAKE METERING VALVE. R & R DEFECTIVE RT (CO-PILOT) TELSDR DJFA20130207001Metering Valve · stuckCREW REPORTED BRAKE ACTION WAS DELAYED AFTER APPLICATION OF BRAKES FOLLOWED BUT AN ABRUPT GRAB, MOST NOTICEABLE DURING THE LANDING ROLLOUT. MX REPLACED THE POWER BRAKE METERING VALVE.SDR DXTA2013020805279Metering Valve · malfunctionedON LANDING ROLLOUT, PLANE PULLS TO THE RIGHT WITHOUT BRAKES APPLIED. ON DOWNHILL TAXIWAY, POWER HAD TO BE ADDED TO TAXI THE PLANE. BRAKE ON RT INBD MAIN WHEEL IS SMOKING HOT AND RT OTBD WHEEL IS WARM. REMOVED POWER BRAKE METERING VALVE AND INSTALLED O/H POSDR DXTA2013021105281Access Panel · corrodedLT WING FUEL PANEL CORRODED.SDR DXTA2013012905265Compressor · inoperativeCOCKPIT PAC TEMPERATURE WAS UNCONTROLLABLE WHILE ON THE GROUND. COCKPIT FILLED WITH BLUEISH WHITE SMOKE BEFORE COCKPIT PAC WAS SECURED. COCKPIT SUPPLY TEMP INDICATED 234 BEFORE PAC WAS SECURED. INSPECTION OF PAC OIL SIGHT CUP INDICATES BLACK OIL. INSPECTESDR DXTA2013012405261Flap System · malfunctionedON APPROACH FLAPS FAILED AT 5 DEGREES/SLATS EXTENDED. COMPLIED WITH FLAPS FAIL CHECKLIST AND DIVERTED. FLAP FAULT CODE IS 467. UNABLE TO DUPLICATE DISCREPANCY. CONFIRMED BITE 4, 6, 7. CONTACTED TEAM 10. HELD EACH FLAP PANEL UP WHILE EXTENDING FLAPS. NO DEFSDR DXTA2013012405260Turbocharger · inoperativeON INITIAL START UP OF APU A STRONG BURNING ODOR WAS OBSERVED FOLLOWED BY A VISABLE MIST IN THE COCKPIT ONLY. THIS OCCURED AS THE ISOLATION VALVE WAS OPENED. PERFORMED APU RUN DUPLICATED DISCREPANCY. NOTED BURNING SMELL FROM COCKPIT WEMAC. RELOCATED ACFT TOSDR DXTA2013012205255Light · odorELECTRICAL ODOR IN LAVATORY AREA, UNABLE TO ISOLATE CAUSE OF ODOR. TROUBLESHOT TO LAVATORY ACCENT LIGHT, BURNED PLASTIC COVER & LIGHT BULB CAUSING ELECTRICAL BURNING ODOR. R & R IAW CMM. WORK DONE IAW MM 25-98-00. DRAWING 4698140. OPS CHECKED NORMAL.SDR DXTA2013012105252Coalescer Bag · odorSMOKEY OIL ODOR COMING THROUGH AIR VENTS. REMOVED AND CLEANED COOLESCER SOCKS WITH MILD DETERGENT. INSPECTED ALL DUCT WORK AND BORESCORED THE APU. RAN APU WITH TEMP CONTROLLER ON HOT & COLD. SHUT DOWN APU REPLACED COOLESCER SOCKS WITH NEW AND PACKING. OPS CHSDR DXTA2013011705246Connector · damagedTHE LANDING GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION AFTER TAKEOFF. RETURNED TO DEPARTURE WITH 3 GREEN SAFE LIGHTS. FOUND CONNECTOR JG019 FOR THE NLG SQUAT SWITCH WIRE HARNESS PULLED APART. PIN LOCK ON THE CONNECTOR BROKEN. NO DAMAGE TO WIRES OR PISDR DXTA2013010405229Inverter · failedAFTER SHUTDOWN DETECTED A VERY STRONG ELECTRICAL BURNING ODOR FROM THE AFT CLOSET INSIDE THE ELECTRICAL BOX. NO FIRE. TROUBLESHOT ELECTRICAL BURNING ODOR TO THE 110V AC INVERTER IN AFT CLOSET. R & R INVERTER WITH AN OVERHAULED UNIT IAW MM 25-40-03. OPS CHECKSDR DXTA2013010305228Lamp · inoperativeDURING GEAR EXTENSION DID NOT RECEIVE A GREEN LIGHT FOR THE LT MAIN GEAR. CONFIRMED WITH TOWER THAT IT WAS DOWN. BLEW GEAR DOWN BOTTLE. RAN ROTORY TEST WHEEL TO LANDING GEAR AND RECEIVED NO HORN. LANDED WITHOUT INCIDENT. FOUND BOTH LT GEAR INDICATOR LIGHTSDR DXTA2012123105221Line · leakingAFTER TAKEOFF, HYDRAULIC VOLUME LOW, AMBER CAS ILLUMINATED DURING GEAR RETRACTION. HYD QTY INDICATED 0 PERCENT. ACFT INSPECTED, RT MLG FOUND RETRACT LINE LEAKING. REMOVED LINE IAW MM 32-30-04. INSTALLED RT GEAR RETRACT LINE IAW MM 32-30-00. PERFORMED SDR DXTA2012122605217Unknown · unknownSELECTED MLG DOWN, NOSE GEAR WOULD NOT INDICATE GREEN. ABNORMAL PROCEDURES FOLLOWED, INCLUDING NG UPLOCK RING PULLED, RECEIVED THREE GREEN INDICATIONS. LANDED WITHOUT FURTHER INCIDENT. ACFT. SERVICED AND RESET GEAR BLOWDOWN BOTTLE. RESET OVERRIDE VALVE ONSDR DXTA2013010405233Acm · defectiveNOTICED A POPPING SOUND COMING FROM THE BACK OF ACFT. BURNED RUBBER ODOR WAS THEN NOTICED. COCKPIT SUPPLY TEMP WAS THEN OBSERVED RISING IN AUTO MODE. ON TROUBLESHOOTING OBSERVED SMOKE IN THE COCKPIT UPON WHICH THE APU WAS SHUTDOWN. GAIN ACCESS, TROUBLESHOT, FSDR DXTA2012121805208Battery · overtempBATTERY OVERTEMP IN FLIGHT. AT FL350, MASTER WARNING WITH RED CAS MESSAGE: BATTERY 2 OVERTEMP. CHECKLIST COMPLIED WITH. OBSERVED TEMP BETWEEN 35C-100C. R & R LT AND RT MAIN BATTERIES IAW MM 24-34-00. OPS CHECKED GOOD.SDR DXTA2012121005203Computer · inoperativeTAKEOFF REJECTED AT 50 KTS DUE TO FAILURE OF DU 1, 2 AND 3, AS WELL AS FMS 1 AND RMU 1. ALL AVIONICS REPOWERED WITHIN 15 SECONDS. THE FOLLOWING AMBER CAS MSG. REMAINED: FADEC REV ADC R, YD OFF LOWER, FADEC FAULT R A, FADEC FAULT L A. TROUBLESHOT TO DEFECTISDR I5EA20121205001Skin · corrodedCORROSION WAS FOUND AT A WING FUEL HOLE COVER PANEL LANDING AREA. THE CORROSION WAS REMOVED, CAUSING THE AREA TO BE OUT OF LIMITS. CESSNA OBTAINED AN 8100-9 REPAIR APPROVAL AND MADE THE REPAIRS.SDR DXTA2012121705207Hinge Bracket · crackedLT INBD ELEVATOR HINGE FITTING BRACKET DUE TO CRACK. REMOVE EXISTING ANGLES AND BRACKETS FOR ACCESS, FABRICATE LOCATING TEMPLATE, REMOVE EXISTING HINGE BRACKET, LOCATE DRILL AND INSTALL NEW HINGE ASSY. R & R LT ELEVATOR INBD HINGE FITTING BRACKET INBD HALFSDR DXTA2012113005198Generator · failedAPU GENERATOR FAILED ON GROUND. COULD NOT RESET. FOUND THE APU GENERATOR AND ITS MOUNTAING PAD TO BE DAMAGED FROM EXCESSIVE HEAT. FOUND APU GENERATOR CATASTROPHICALLY FAILED AND DEPARTED FROM APU GEARBOX. REMOVED APU. INSTALLED APU GEN MOUNTING PLATE & GESDR DJFA20121127001Charger · failedCREW REPORTED ELECTRICAL BURNING ODOR DURING FLIGHT COMING FROM OUTLET FOR EFB. AFTER NOTICING ODOR, IT WAS NOTED THE EFB WAS NO LONGER SHOWING A CHARGE. MX FOUND THE POWER ADAPTOR FOR THE EFB FAILED AND REPLACED IT.SDR DXTA2012112605196Acm · seizedCABIN ACM IS MAKING A LOUD BEARING NOISE WHEN RUNNING. STRONG OIL ODOR ASSOCIATED IN THE CABIN WITH CABIN PACKS OPERATING. OIL ODOR IS STILL PRESENT AFTER PACKS HAS BEEN SHUTOFF FOR 10 MINUTES. BEARING NOISE STOPS WHEN CABIN PACK IS SHUTOFF. TROUBLESHOT, FOSDR DXTA2012112605195O-Ring · leakingDURING DECENT, CREW RECEIVED AN AMBER CAS MESSAGE: HYD LEVEL LOW A, HYD SHOWED 16 PERCENT. FOLLOWED EMERGENCY CHECKLIST AND MADE A SAFE LANDING, STOPPING THE ACFT ON THE RUNWAY USING THE EMERGENCY BRAKE. DURING POST FLIGHT INSPECTION, FOUND FRESH HYD FLUIDSDR DXTA2012112605194Module · malfunctionedAT TOUCH DOWN A STRONG ODOR DETECTED IN COCKPIT AND GOT STRONGER WHEN APU BLEED AIR WAS PLACED IN HIGH. AT THE SAME TIME AURAL WARNING TONES 1 AND 2 CONTINUOUSLY SOUNDED AND DID NOT GO OUT UNTIL AVIONICS WAS TURNED OFF. TROUBLESHOT AND FOUND NR 1 AURAL ANNSDR DJFA20121114001Acm · failedCREW REPORTED SMELLING SMOKE AND OIL IN THE CABIN WITH THE APU RUNNING. MX FOUND THE FORWARD ACM FAILED AND REPACED IT.SDR DXTA2012110505169Unknown · odorFOUL OILY, MUSTY ODOR COMING FROM BOTH PACS.
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