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 = '650' 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 = '650' 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 2001FA0000272Landing Light · damagedRECEIVED THIS PART FROM CESSNA WITH UNDAMAGED PACKING. THE GROUND LUG WAS BENT, LOOSE AND HAD DAMAGED THREADS. THIS PART WAS PROPERLY PACKED WITH SPRAYED IN FOAM. THIS PART WAS DAMAGED PRIOR TO BEING PLACED IN THE BOX.SDR 2001FA0000271Motor · defectiveUNIT RECEIVED AND INSTALLED. WHEN LIGHT IS RETRACTED, UNIT CONTINUES TO RUN WITH A GRINDING NOISE AND MOTOR WILL NOT SHUT OFF. UNIT WAS NOT ADJUSTED ON INSTALLATION. UNIT WAS PURCHASED THRU CESSNA AS AN OVERHAULED PART BY AN OUTSIDE VENDOR. THE UNIT HAS A SDR 2001FA0000270Motor · failedUNIT RECEIVED AND INSTALLED. OPERATED UNIT 3 CYCLES AND ON 4 EXTENSION UNIT WOULD NOT EXTEND AND MOTOR SEIZED AND SMELLED OF BURNING ELECTRICAL WIRING. UNIT WAS PURCHASED THRU CESSNA AS AN OVERHAULED PART BY AN OUTSIDE VENDOR. THE UNIT HAS A HISTORY OF EARSDR UG82001F00003Printed Ckt Board · defectiveNR 2 COMM INOPERATIVE. REPLACED STRAPPING PC CARD ON NR 2 COMM UNIT, OPERATION NORMAL CHECKED 1 & 2 TRANSPONDERS.SDR UG82001F00004Relay · stuckRIGHT ENGINE STARTER WOULD NOT DISENGAGE. STUCK START RELAY. REMOVED AND REPLACED START RELAY.SDR 2001F00325Transceiver · malfunctionedNR 2 COMM RADIO FAILED EN ROUTE, WILL NOT HOLD A FREQUENCY. UNABLE TO DUPLICATE AFTER SIX HOURS OF GROUND OPERATION. PERFORMED BIT AND SELF TEST. CHECKED POWER INPUTS AND GROUNDS AT PT538 AND SECURITY OF PA502. (M)SDR 20010511CW011Blower · defectiveON TAXI OUT CREW NOTICED SMOKE IN CABIN AND SMELLED SMOKE. AIRCRAFT WAS TAKEN TO REPAIR STATION AND THEY FOUND THE BLOWER TO BE INOPERATIVE AND SMELLING STRONGLY OF BURNED WIRING. THEY INSTALLED AN OVERHAULED SYSTEM, OPS CHECKED OK. DUE TO NORMAL WEAR.SDR 20010529CW013Fuel Control · malfunctionedENGINE LOST POWER IN FLIGHT. PILOT REPORTED THAT FUEL FLOW WAS ERRATIC AND THAT NR 1 BECAME LIMITED TO 40 PERCENT. WHEN TROUBLESHOT, THE FAULT WAS TRACED TO THE FUNCTION OF THE FUEL CONTROL UNIT. A REPLACEMENT FUEL CONTROL UNIT WAS INSTALLED AND THE DEFECTISDR 20010612CW008Impeller · disintegratedWRITE-UP, WEMAC BOOST INOPERATIVE, PART ON ORDER. FOUND FAN CASE IMPELLER HAD DISINTEGRATED.SDR 20010413CW001Sensor · defectiveTEMPERATURE SENSOR CONNECTOR PINS FOUND TO BE RECESSED EXCESSIVELY. DEFECT FOUND DURING INSPECTION OF BATTERY. THIS CONDITION PROVIDES ONLY MINIMAL CONTACT BETWEEN MATING PINS.SDR CA010214012Seal · frozen(CAN) AFTER OR DURING CLIMB TO CRUISE ALTITUDE, DOOR SEAL ANNUNCIATOR LIGHT CAME ON AND PASSENGER DOOR SEAL STARTED WHISTLING.PILOT RETURNED TO YUL WITH NO PROBLEM.AFTER INVESTIGATION, SUSPECT THAT DOOR SEAL WAS FROZEN, FOUND LOT OF SNOW AND ICE AROUND DOOR FRSDR 20010129CW012Wire · chafedPILOT REPORTED THAT IN FLIGHT, THE NOSE WHEEL STEERING SYSTEM DISARMS WHEN THE YAW DAMPER SYSTEM IS DISENGAGED USING THE AUTOPILOT/ NWS DISCONNECT SWITCH ON THE PILOT OR COPILOTS CONTROL WHEEL. THE TECH FOUND A CHAFFED STEERING SYSTEM WIRE SHORTING TO GROUND SDR 20010205CW018Actuator · failedLANDING APPROACH, THE FLAPS WERE SELECTED TO 20 DEGREE. AC BEGAN UNCOMMANDED ROLL TO THE RIGHT AND HAD TO BE COUNTERED USING AILERON INPUT. AFTER LANDING, FLAPS WERE RAISED TO 0 DEGREE. SHORTLY AFTER FLAP FAILED, ANNUNCIATOR LIGHT ILLUMINATED. INSPECTION OF SDR 20001227SH014Valve · failedPILOT REPORTED THE EMERGENCY PRESSURIZATION WAS COMING ON WHEN THE WING DEICE WAS SWITCHED ON. NO INDICATION ON ANNUNCIATOR PANEL TO INDICATE EITHER OF THE EMERGENCY PRESS SYSTEMS BEING ACTIVATED. DISCOVERED THE RT EMERG PRESSURIZATION VALVE WAS LEAKING BY ASDR 20010124CW001Rod End · brokenLOWER DOOR ROD END BROKEN IN TWO PARTS. CAUSE WAS IMPROPER OPERATION BY PEOPLE OPERATING DOOR.SDR 20001129SH009Fire Loop · failedFIRE LOOP SHOWED FAILED ON DEPT FROM SSI. RECEIVED FERRY PERMIT FROM FAA. FOUND FIRE LOOP FAILED, PN 9914092-1. REMOVED AND REPLACED WITH NEW PN 9914092-1. (X)SDR 20001013SH018Seal · failedWHEN FUELING AIRCRAFT, PILOT NOTED NR 1 STRUT ASSY LOW. TROUBLESHOT TO FAILED STRUT SEALS. REPLACED STRUT ASSY P/N G241115-4, SN WTC157 OFF, RENTAL STRUT PN 6241209-2, SN B316S ON. (X)SDR 20001012SH020Tire · failedUPON POST-FLIGHT INSPECTION, PILOT NOTED NR 1 TIRE SHREDDED. REPLACED WHEEL ASSY, PN 3-1399-3, SN 2293, OFF. INSTALLED LOANER WHEEL ASSY, PN 3-1399-3, SN 1152, AND TIRE, P/N 226K08-4. LANDINGS: 211 (X)SDR 20001017SH027Actuator · brokenAFTER LANDING, HYD FLUID FOUND LEAKING FROM RT MLG DOOR, RT INBD WING. INVEST REVEALED THE OTBD RT MLG RETRACT/EXTEND ACTUATOR HAD BROKEN AT WING ATTACH FITTING , INBD (RETRACT) HYD FITTING BENT. ACT HOUSING WAS DAMAGED AT FITTING PORT DUE TO MOVEMENT OF ACTSDR 20000808SH013Wire · brokenFLIGHT CREW REPORTED LOOSE WHEEL STEERING, COULD NOT BE DISENGAGED. FOUND WIRE, GPN1-7APNS, BROKEN BETWEEN CONNECTOR PN1 AND PN5. WIRE BUNDLE WAS WELL PROTECTED WITH SPIRAL WRAP AND CLOTH COVERING. WIRE BUNDLE SHOWED NO SIGN OF EXTERIOR DAMAGE AND WAS SUPPOSDR 20000613SH010Valve · failedDURING CENTER POINT FUELING, ENCOUNTERED INTERMITTENT FUEL VENTING FROM RIGHT WING TIP. DISCOVERED RIGHT FUEL PRE-CHECK WOULD NOT SHUT OFF FUEL TO RT WING. SUBMITTER STATED THIS CONDITION HAD BEEN AN ONGOING INTERMITTENT PROBLEM. REPLACED RT WING DE-FUEL SDR 20000817SH027Brake · damagedDURING AN INSPECTION, FOUND A 3 INCH AND A 2 INCH SECTION OF FRICTION MATERIAL MISSING FROM THE SAME DISC. ALL OTHER DISCS WERE SERVICEABLE AND THE BRAKE ASSY HAD NORMAL WEAR. SUBMITTER RECOMMENDED BETTER MATERIALS OF PROCEDURES FOR BONDING OF FRICTION MATERSDR 20000623SH006Seal · leakingUPON TAKEOFF, LANDING GEAR WOULD NOT RETRACT BECAUSE SQUAT SWITCH WAS NOT MADE FOR AIR MODE. ADDITIONALLY, NOSE WHEEL WAS DEFLECTED TO THE LEFT. CAUSE WAS DETERMINED TO BE OLEO STRUT NOT EXTENDING COMPLETELY WHICH PREVENTED THE NOSE WHEEL FROM CENTERING, NOTSDR 2000ZZZX417Seal · leakingUPON TAKEOFF, LANDING GEAR WOULD NOT RETRACT BECAUSE SQUAT SWITCH WAS NOT MADE FOR AIR MODE. ADDITIONALLY, NOSE WHEEL WAS DEFLECTED TO THE LEFT. CAUSE WAS DETERMINED TO BE OLEO STRUT NOT EXTENDING COMPLETELY WHICH PREVENTED THE NOSE WHEEL FROM CENTERING, THESDR 2000ZZZX266Housing · failedPILOT NOTED LOW OIL PRESSURE INDICATION ON NR 1 ENGINE. PILOT LANDED AT LNK WITHOUT INCIDENT. TROUBLESHOT TO CRACK IN OIL FILTER HOUSING. REMOVED OIL FILTER HOUSING P/N 3072231-1 AND INSTALLED P/N 3072231-4 PER GARRETT SB 72-3635. SOAP SAMPLE TAKEN. GROUNSDR 2000ZZZX107Deice Element · mismanufacturedHORIZONTAL STABILIZER ANTI-ICE LEADING EDGE. THIRD NEW LEADING EDGE RECEIVED FROM CESSNA KS. HAS ONE TEMPERATURE SWITCH BROKEN LOOSE FROM MOUNTING POINT. DEFECT FOUND DURING RECEIVING INSPECTION. SUBMITTER RECOMMENDED NEW TYPE OF BONDING OF TEMPERATURE SWISDR 2000ZZZX108Deice Element · mismanufacturedHORIZONTAL STABILIZER ANTI-ICE LEADING EDGE. SECOND NEW L/E RECEIVED FROM CESSNA KS. HAS TWO HEATING ELEMENT DEFECTS, ONE 26 INCHES FROM OUTBOARD EDGE AND ONE 15 INCHES FROM OUTBOARD EDGE. DEFECTS FOUND DURING RECEIVING INSPECTION.SDR 2000ZZZX106Deice Element · mismanufacturedHORIZONTAL STABILIZER ANTI-ICE LEADING EDGE. NEW FROM CESSNA KS HAD ONE TEMP SWITCH LOOSE IN MOUNTING, AND ONE TEMP SWITCH BROKEN OUT OF MOUNTING POINT. LEADING EDGE IS ELECTRICALLY HEATED. LOSS OF TEMPERATURE CONTROL WILL RESULT AND ALSO LOSS OF ANTI-ICE PRSDR 99ZZZX3766Uplock · looseDURING INSPECTION, FOUND LT MLG UPLOCK ASSY LOOSE IN AIRCRAFT STRUCTURE. ALL 4 BOLTS (AN4-7A) WERE LOOSE. NO SAFETY DEVICE OTHER THAN THAN SELF-LOCKING NUTPLATE (MS21069L4). TORQUED BOLTS AND APPLIED LOCTITE 271 THREAD LOCKER. FOUND RT UPLOCK ASSY SECURE, SDR 99ZZZX3765Uplock · looseDURING INSPECTION, FOUND LT MLG UPLOCK ASSY LOOSE IN AIRCRAFT STRUCTURE. ALL 4 BOLTS (AN4-7A) WERE LOOSE. NO SAFETY DEVICE OTHER THAN SELF-LOCKING NUTPLATE (MS21069L4). TORQUED BOLTS AND APPLIED LOCTITE 271 THREAD LOCKER. FOUND RT UPLOCK ASSY SECURE, BUT BSDR 99ZZZX4231Drain Heater · failedNEW GALLEY DRAIN, PN 105881, WAS INSTALLED. WHEN ELECTRICAL POWER WAS APPLIED, THE HEATER/DRAIN BURNED OUT. IT SEEMS THE HEATER WAS SHORTED OUT INTERNALLY.SDR 99ZZZX2960Switch · out of adjustAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. PILOT FLEW TO HOME BASE WITHOUT INCIDENT. RAN GEAR RETRACT TEST. ADJUSTED NOSE GEAR CENTERING SWITCH. FLIGHT TEST OK.SDR 99ZZZX3393Filter · failedDURING SMIP INSPECTION, OPERATION 10, ITEM 27-20, INSPECTION REVEALED FILTER SEPARATED FROM MOUNTING FLANGE IN THE END OF ELBOW FITTING PERMITTING FILTER TO SLIDE BACK AND FORTH WITHIN THE FITTING. REPLACED WITH NEW UNIT. FILTER NOW HAS 3,600 HOUR LIFE-LIMITSDR 99ZZZX2778Blower · malfunctionedIN-FLIGHT, BLOWER MOTOR FAILED, CAUSED COCKPIT TO FILL WITH SMOKE. PILOTS HAD TO PUT ON SMOKE GOGGLES AND OXYGEN MASKS AND DECLARE AN EMERGENCY TO LAND AT ACY AT APPROXIMATELY 15:45 7-7-99. AFTER LANDING, OPS CHECKED BLOWER, IT RAN FOR ABOUT 3 SECONDS AND STSDR 99ZZZX2552Oxygen Mask · defectiveINSPECTED AIRCRAFT FOR COMPLIANCE OF AD 99-08-21 PURITAN BENNETT PASSENGER OXYGEN MASKS. OXYGEN MASK INSTALLED IN AIRCRAFT WERE NOT FULLED LISTED.SDR 99ZZZX2551Oxygen Mask · misinstalledDURING INSPECTION OF PASSENGER OXYGEN MASKS FOR AD 99-08-21, FOUND 2 SCOTT PASSENGER OXYGEN MASKS IN A PURITAN BENNETT CONTAINER ASSY. CE650 IPC STATES PURITAN BENNETT MASK ASSEMBLIES ARE TO BE USED ONLY WITH PURITAN BENNETT CONTAINER ASSEMBLY.SDR 99ZZZX2230Pump · crackedPILOT NOTED HYDRAULIC LEAK ON TAIL. TROUBLESHOT TO LEAKING AUXILIARY HYDRAULIC PUMP. REPLACED PUMP P/N 9914119-3, S/N 124 OFF, S/N 0037 ON. OPERATIONS CHECKED OK.SDR 99ZZZX2262Line · chafedFUEL LINE IS CHAFING ON WIRING HARNESS THAT RUNS JUST AFT OF THE TRANSFER GEARBOX ON BOTH ENGINES. INSTALL SPIRAL WRAP AROUND FUEL LINE OR SEPARATE WIRES AND LINE WITH ADEL CLAMPS.SDR 99ZZZX2048Steering Unit · failedAIRCRAFT EXPERIENCED A HARD LEFT YAW AT V1, FOLLOWED BY POSITIVE AIRCRAFT CONTROL TO ROTATION. GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AFTER TAKEOFF. DIVERTED AIRCRAFT TO CESSNA NY SERVICE CENTER. APPROACH AND LANDING WAS NORMAL, HOWEVER, NOSE TIRE WAS SDR 99ZZZX2047Chip Light · illuminatedPILOT NOTED A CHIP DETECTOR LIGHT IN-FLIGHT. PILOT LANDED IN BUFFALO, NY WITHOUT INCIDENT. CLEANED CHIP DETECTOR AND GROUND RAN. OPERATIONS CHECK OK. PILOT RESUMED TRIP TO MILWAUKEE WITHOUT INCIDENT. SOAP SAMPLE TAKEN AND SENT TO GARRETT-SPRINGFIELD FOR ASDR 99ZZZX1867Seal · failedPILOT DETECTED SMOKE IN CABIN. TROUBLESHOT TO NR 4 AND NR 5 LABRYNTH SEALS IN LEFT ENGINE, SN 87270. REMOVED ENGINE SN 87270 AND INSTALLED LOANER ENGINE SN P-87267. NOTE: REPAIRED AT GARRETT SPRINGFIELD W.O. NR 73041.SDR 99ZZZX1828Windshield · crackedRIGHT WINDSHIELD CRACKED AT FL 39,000 FEET. PPG NOW HAS IMPROVED WINDSHIELD P/N 991438-10 WHICH WAS INSTALLED.SDR 99ZZZX2107Cap · seizedWHILE PERFOMRING OPERATION 8 INSPECTION WHEN REMOVING ANTI-ICE FILTER CAP, FOUND CAP FROZEN OR GALLED AND ON OTHER ANTI-ICE VALVE, THE CAP FROZE OR GALLED UPON RE-INSTALLING CAP AFTER CLEANING AND INSPECTING FILTER. RECOMMEND PROPER COMPOUND BE APPLIED BY OVESDR 99ZZZX2106Cap · seizedWHILE PERFORMING OPERATION 8 INSPECTION WHEN REMOVING ANTI-ICE FILTER CAP, FOUND CAP FROZEN OR GALLED AND ON OTHER ANTI-ICE VALVE, THE CAP FROZE OR GALLED UPON RE-INSTALLING CAP AFTER CLEANING AND INSPECTING FILTER. RECOMMEND PROPER COMPOUND BE APPLIED BY OVESDR 99ZZZX2169Bypass Valve · failedTHE LANDING BYPASS VALVE FAILED AND CAUSED AN EMERGENCY LANDING.SDR 99ZZZX806Squat Switch · malfunctionedGEAR HANDLE WOULD NOT GO UP. TROUBLESHOT TO NOSE GEAR SQUAT SWITCH. REMOVED AND REPLACED SWITCH P/N 41EN45-6. OPERATIONS CHECKED OK.SDR 99ZZZX1424Labels · looseLINE LABELS IN FUEL CELLS COMING LOOSE. LABEL MIGRATED TO SUMP AREAS FOULING SCREENS, FLAPPER VALVES, AND JET PUMPS. TWO SEPARATE AIRCRAFT HAD FUEL PRESSURE PROBLEM RELATED TO THIS PROBLEM. LOOSE LABELS SHOULD BE REMOVED AT PHASE 5 INSPECTION.SDR 99ZZZX790Steering Unit · malfunctionedAIRCRAFT HAD A PROBLEM WITH NOSE WHEEL SHIMMY AFTER A NOSE TIRE CHANGE. THE TIRE WAS REPLACED WITH A NEW NOSE TIRE. AFTER THIS, COUPLE OF INSTANCES WHERE THE LANDING GEAR WOULD NOT RETRACT. UNABLE TO DUPLICATE LANDING GEAR NOT RETRACTING PROBLEM ALTHOUGH SUSDR 20000713SH013Diode · openRIGHT THRUST REVERSER WOULD NOT STOW IN NORMAL OR EMERGENCY RE-STOW. FOUND NO POWER TO ISOLATION VALVE WHEN STOW WAS COMMANDED IN NORMAL OR EMERGENCY STOW. FOUND DIODE D91 OPEN ON PC BOARD 62184165. SUBMITTER RECOMMENDED MAKING THE EMERGENCY STOW A FULLY RESDR 99ZZZX15Uplock · failedRIGHT MAIN GEAR WOULD NOT LOCK UP. FOUND BAD UPLOCK SWITCH. REMOVED AND REPLACED SWITCH. NEW P/N 6217102-2.
Back to Cessna 650