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 FCPR20070006Ballscrew · failedFLAP ACTUATOR DRIVE CARRIAGE BALLSCREW NUT FAILED. FLAPS WOULD NOT MOVE.SDR 2007FA0000368Doubler · fatiguedTHE 6213011-139 LT DOUBLER AND THE 6213011-140 RT DOUBLER FATIGUE CRACKING ON BOTH. THE 6213011-139 LT DOUBLER AND THE 6213011-140 RT DOUBLER, ON MODEL 650 IS PART OF THE NOSE WHEEL WELL ASSY, HAS BEEN FOUND WITH FATIGUE CRACKING ON MULTIPLE SN. CURRENTLY THSDR 2007FA0000367Doubler · fatiguedTHE 6213011139 LT DOUBLER AND THE 6213011140 RT DOUBLER FATIGUE CRACKING ON BOTH. THE 6213011139 LT DOUBLER AND THE 6213011140 RT DOUBLER, ON MODEL 650 IS PART OF THE NOSE WHEEL WELL ASSY, HAS BEEN FOUND WITH FATIGUE CRACKING ON MULTIPLE SN. CURRENTLY THE PASDR BTA2007F00000Unknown · malfunctionedRT ENGINE FIRE LIGHT CAME ON DURING CLIMBOUT, RETARDED THROTTLE LIGHT WENT OUT, ADVANCED THROTTLE LIGHT CAME BACK ON AND LANDED. PERFORMED LEAK CHECKS WITH COWLING OPEN, RAN AT FULL POWER FOR 10 MINUTES, COULD NOT DUPLICATE PROBLEM. FLEW AIRCRAFT BACK TO HOMSDR DXTA200702072Engine · malfunctionedLEFT ENG ROLLED BACK TO 91% N1 ON T/O ROLL (APROX 80 KNOTS). T/O ABORTED. INSP EEC FOR FAULTS NONE NOTED. RAN A/C AT ALL POWER SETTINGS IN AUTO & MANUAL MODES. NO ROLL BACK NOTED SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME ALL WORK DONE IAW CE 650 M/M 76-10-0SDR 03192007650ZHose · crackedLT UPPER ACTUATOR LINE WAS FOUND TO HAVE A CRACK IN THE ELBOW, CAUSING A HYDRAULIC FLUID LEAK. MATERIAL IN THE ELBOW OF THE HOSE LOOKS GRAINY AS IS STRESSED WHILE FORMING.SDR DXTA200702018Switch · out of adjustLANDING GEAR WOULD NOT RETRACT. AFTER TAKEOFF. GEAR HANDLE WOULD NOT MOVE. TROUBLESHOT TO NOSE CENTERING SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH IAW 650 MM 32-60-00. OPS CHECK GOOD IAW SAME.SDR DXTA200702000Strut · underservicedLANDING GEAR WOULD NOT RETRACT (HANDLE WOULD NOT COME UP) AFTER TAKEOFF. TROUBLESHOT NOSE LANDING GEAR - FOUND NOSE STRUT NOT FULLY SERVICED - SERVICED STRUT WITH FLUID AND NITROGEN IAW CESSNA M/M 12-10-38 FUNCTIONALLY TESTED GEAR - NO DEFECTS NOTED AT THIS TISDR DXTA200701975Unknown · smokeDISTINCT SMELL OF ELECTRICAL SMOKE IN CABIN AND COCKPIT AND A NOTICEABLE HAZE OF SMOKE VISIBLE. OPERATED GROUND TEST APU TWICE FOR APPROX 20-25 MIN IAW 650 MM 49-10-00. NO NOTICEABLE SIGNS OF SMOKE IN CABIN. RAN CABIN TEMP TO FULL HOT AND COLD. BITE CHECKED SDR DXTA200701933Wire · brokenRT ENGINE FIRE DETECT ANUNCIATOR ILLUMINATED AFTER COCKPIT PREP WAS COMPLETED. T/S TO BROKEN RT FIRE LOOP ON ENG. REMOVED & REPLACED FIRE LOOP. BLEED T/R'S, SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE 650 M/M 26-10-01SDR DXTA200701867Control Module · inoperativeLANDING GEAR WOULD NOT RETRACT, AFTER T.O. OUT OF SFO. FINALLY 2-3 SECONDS LATER THE GEAR CAME UP. REMOVED AND REPLACED THE LANDING GEAR CONTROL PERFORMED 10 GEAR SWINGS OSP CHECKS GOOD ALL WORK DONE IAW CE-650 M.M. 32-30-01SDR A8J2007F00001Circuit Board · faultyON 1/10-07 AT 1900, AIRCRAFT EXPERIENCED AN AILERON BOOST FAILURE. PILOT DECLEARED AN EMERGENCY AND LANDED AT ITS SCHEDULE DETINATION WITHOUT ANY COMPLICATIONS. AILERON BOOST CIRCUIT BOARD WAS REPLACED AND THE SYSTEM CHECKED GOOD. (K)SDR 01082007650ZUnknown · unknownDISCREPANCY (PRIMARY TRIM INDICATOR DOES NOT MOVE FULL RANGE.) DURING FLIGHT, FLIGHT CREW OBSERVED INTERMITTENT FAILURE OF THE HORIZONTAL STABILIZER PRIMARY TRIM (CLACKER). UPON ARRIVAL, FLIGHT CREW PERFORMED ALL PRE AND POST TAKEOFF OPERATIONAL CHECKS AND OBSSDR DXTA200701837Unknown · unknownAIRCRAFT EXPERIENCED UNCOMMANDED HARD LT YAW CAUSED BY YAW DAMPER. OPERATION CHECK OF A AND B YAW DAMPER SYSTEMS GOOD, SPZ-8000 DIAG. TEST GOOD. RUDDER SERVO OPERATION CHECK GOOD, FLIGHT GUIDANCE, FGC'S, AND AHRS SYSTEMS CHECK GOOD IAW MFG SPZ-8000 AFCD MM SECSDR DJFA2007002Computer · odorKLUK-KTUL TRIP 1124319 THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT AREA WITH NO SMOKE PRESENT. THEY WERE UNABLE TO ISOLATE IN FLIGHT. MAINTENANCE TROUBLESHOT THE ELECTRICAL SMELL AND ISOLATED IT TO THE STALL WARNING COMPUTER. THE STALLSDR 2007F00001Control Unit · defectivePRIMARY TRIM ANNUNCIATOR COMES ON INFLIGHT. SECONDARY TRIM FAIL LIGHT ILLUMINATES ALSO AND STAB TRIM WILL NOT MOVE. TROUBLESHOT STABILIZER SYSTEM; FOUND HORIZONTAL STABILIZER ACTUATOR CONTROL UNIT DEFECTIVE. REPLACED AS REQUIRED; PERFORMED FUNCTIONAL CHECK FLISDR ZLWA0603Cabin Pressure · uncontrollableCABIN DEPRESSURIZED AT 20,000 FEET, 8500 FT LIGHT ILLUMINATED AND MADE AN EMERGENCY DESCENT. MAINTENANCE INSPECTED SYSTEM COMPONENTS WITH NO DEFECTS NOTED. UNABLE TO DUPLICATE DISCREPANCY.SDR DXTA200601777Control Module · inoperativeGEAR WOULD NOT RETRACT AFTER TAKE OFF , GEAR HANDLE STUCK IN THE DOWN POSITION. RETURNED TO AIRPORT. REMOVED AND REPLACED LANDING GEAR CONTROL IAW CE 650 M/M CHP 32-30-01, OPS CHECKED AND CYCLED X 10. CHECKS GOODSDR DXTA200601645Annunciator · inoperativeUPON ADVANCING POWER FOR T/O, ENGINE OIL PRESSURE WARNING LIGHT CAME ON. TAPES FOR TEMP AND PRESSURE INDICATED NORMAL. INSTALLED REPAIRED ANNUNCIATOR PANEL IAW CESSNA 650 MM CHAP 31-10-01, OPS CHECK GOOD.SDR DXTA200601615Link · wornAFTER TAKEOFF GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. CHECKED SYSTEM FOR PROPER OPERATION, COULD NOT DUPLICATE. CHECKED NOSE SQUAT SWITCH FOUND NOSE CENTERING LINK ASSY NOT GRABBING CENTERING SWITCH TO ACTUATE PROPERLY. REMOVED AND REPLACED NOSE CENTSDR ZLWA0602Cabin Pressure · failedCLIMBING THROUGH FL230, CABIN LOST PRESSURE CONTROL. CABIN WENT TO 20,000, MASK DROPPED. AIRCRAFT WAS INSPECTED AND NUMEROUS TEST RUNS PERFORMED ON AIRCRAFT. ALL SYSTEMS WERE CHECKED AND THE PRESSURIZATION SYSTEM CHECKED GOOD. NO SYSTEM OR COMPONENT FOUND FAULSDR CA060822001Bolt · broken(CAN) ON DAILY INSPECTION, FOUND (1) BOLT BROKEN ON NR 4 MAIN WHEEL ASSY. (TC NR 20060822001)SDR 2006FA0000767Wire Harness · damagedDUAL TRANSPONDER FAILURE IN HEAVY PRECIPITATION. NO FAILURE INDICATION ON SPZ8000 SYSTEM. CENTER REQUESTED RESET OF TRANSPONDER, AND DIRECTED OUT OF RVSM AIRSPACE WHEN UNSUCCESSFUL. HANGAR TESTS OF POWER OUTPUT SHOWED 40WATTS BEFORE CABLES REPLACED, AND 400 WSDR 2006FA0000766Wire Harness · damagedDUAL TRANSPONDER FAILURE IN HEAVY PRECIPITATION. NO FAILURE INDICATION ON SPZ8000 SYSTEM. CENTER REQUESTED RESET OF TRANSPONDER, AND DIRECTED OUT OF RVSM AIRSPACE WHEN UNSUCCESSFUL. HANGAR TESTS OF POWER OUTPUT SHOWED 40WATTS BEFORE CABLES REPLACED, AND 400 SDR 2006FA0000868Switch · mismanufacturedAFTER ARRIVAL, FOUND FUEL LEAK NEAR IB END OF RT WING. INVESTIGATION SHOWED THE LOW LEVEL FUEL LIMIT SWITCH WAS NOT ASSEMBLED. THE FLOAT, PN L15F2, WAS NOT ATTACHED TO THE MOUNT ASSY PN 62266503. THIS ALLOWED FUEL TO LEAK FROM THE WING. SWITCH WAS ASSEMBLESDR IJ02006F00000Actuator · crackedAFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A LOSS OF HYDRAULIC PRESSURE, DURING LANDING GEAR RETRACTION. THE CREW RETURNED THE GEAR TO THE EXTENDED POSITION AND DECLARED AN EMERGENCY WITH ATC. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INVESTIGATION REVSDR DXTA200601472Acm · leakingDURING FLIGHT FROM GSO TO LUK, REAR ACM LEAKING OIL WITH STRONG ODOR IN CABIN. AIRCRAFT CONTINUED AND LANDED AT LUK. REMOVED AND REPLACED REAR ACM, INSTALLED AN OVHD UNIT OF THE SAME P/N WORK DONE IAW HAMILTON STANDARD MM 21-50-03. SERVICED TO PROPER LIMITS.SDR 2006FA0000910Shutoff Valve · misinstalledDETERMINED THE PRESSURE REGULATOR SHUTOFF VALVE WAS LEAKING. FOUND THE REGULATOR HAD BEEN INSTALLED WITHOUT GASKETS. THE PARTS MANUAL DOES NOT CLEARLY IDENTIFY THAT GASKETS ARE REQUIRED TO BE INSTALLED WITH THIS SPECIFIC PN OF VALVE. CONTACTED AND CONFIRMEDSDR DXTA200601382Actuator · inoperativePRIMARY AND SECONDARY STAB TRIMS FAILED IN CRUISE FLIGHT (ALTITUDE WAS FL 300 AT MACH .77). REMOVED AND REPLACED HORIZONTAL STABILIZER PRIMARY TRIM ACTUATOR IAW CESSNA 650 MM 27-40-01 AND PERFORMED APPLICABLE CHECKS. OPS CHECKED GOOD.SDR DXTA200601366Controller · inoperativePRIMARY TRIM FAIL ENUNCIATOR ILLUMINATED IN FLT. FOLLOWED EMERGENCY CHECKLIST. SECONDARY TRIM FAILED TO MOVE STABILIZER. SEC. TRIM FAULT ENUNCIATOR WAS NOT ILLUMINATED AND NO TRIM CLACKER HEARD. - REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR CONTROLLSDR LMM2006F00000Switch · defectiveDURING LANDING GEAR RETRACTION, AFTER TAKEOFF. BOTH MAIN GEAR RETRACTED NORMALLY (GREEN LIGHTS OUT). RED TRANSIENT LIGHT REMAINED ON. NOSE GEAR GREEN LIGHT WENT OUT, MOMENTARILY AND THEN CAME BACK ON. (K)SDR DXTA200601352Control Unit · inoperativeGEAR HANDLE WOULD NOT MOVE THEREFORE THAT LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED LANDING GEAR CONTROL DUE TO FAULTY DOWN LOCK SOLENOID, INSTALLED CONTROL. CONTROL AND GEAR OPERATIONAL CHECK NORMAL. WORK PERFORMED IAW THE MM CHAPTER 32-30-01.SDR DXTA200601336Control Arm · dirtyLANDING GEAR WOULD NOT RETRACT AFTER DEPARTURE. CLEANED NOSE GEAR CENTERING ARM AND LUBED DUE TO BINDING IAW THE 650 MM CHAPTER 32-20-00. PERFORMED GEAR RETRACTION OPS CHECK. OPS CHECK NORMAL.SDR DXTA200601292Disconnect Unit · corrodedBRAKES FADED ON ROLLOUT, TURNED ANTI-SKID OFF BRAKES WORKED NORMAL. BRAKES WOULD NOT HOLD DURING STATIC THRUST CK ABOVE 61 PERCENT N1, WITH ANTI SKID ON. ANTI SKID OFF BRAKES ARE NORMAL. REMOVED AND REPLACED CORRODED RT WHEEL WELL CONNECTOR JW18 IAW 650 WM SDR 2006FA0000214Windshield · crackedPILOT'S GLASS WINDSHIELD SHOWED SIGNS OF OVERHEATING AT UPPER CENTER EDGE CAUSING COMPLETE CRACKING OF WINDSHIELD IN A SPIDER WEB FASHION. THE WINDSHIELD REMAINED STRUCTURALLY SOUND AND THE AIRCRAFT WAS ABLE TO LAND WITHOUT INCIDENT.SDR CA060224008Turnbuckle · chafedDURING A SCHEDULED PHASE 5 INSPECTION ON CESSNA 650 C-FIMO, THE TECHNICIAN DISCOVERED THAT THE LT AND RT AILERON OUTBOARD AFT CABLE CHAFED THROUGH THE LOKCLAD AND THE TURNBUCKLE WAS DAMAGED.SDR DXTA200601245Gearbox · frozenFLAPS INOP, WOULD NOT EXTEND. FLAP INOP LIGHT ILLUM, WOULD NOT RESET. CHK`D FLAP CONTROLLER. NONE FOUND GAINED ACCESS TO FLAP PDU. DISCONNECTED RT FLAP DRIVE CABLE FROM PDU. UPON REMOVAL, DRIVESHAFT OF FLEX CABLE REMAINED IN PDU & CABLE SEPARATED FROM PDU.SDR 2006FA0000159Water Separator · separatedEXPERIENCED AN ABRUPT CABIN PRESS FLUCTUATION DURING FLT. FLT CREW REPORTED, ABLE TO MAINTAIN CABIN ALT WITHIN LIMITS AFTER NOTICED PROBLEM. AFTER THIS A/C LANDED MX PERSONNEL DISCOVERED ONE OF THE ENVIRONMENTAL CONTROL SYS WATER SEPARATOR UNITS HAD SEPARATESDR ZN3R556712Stator · separatedENGINE 4TH LPC STATOR HAD INNER RING FRACTURE, LEADING TO A SINGLE VANE SEPARATING FROM THE STATOR ASSEMBLY. THE VANE CAUSED DAMAGE TO THE HPC AREA OF THE ENGINE. AIRCRAFT DID NOT EXPERIENCE ANY PROBLEMS WITH ENGINE DURING FLIGHT, AND PERFORMED SCHEDULED LANSDR DXTA200601182Squat Switch · intermittentDURING ROLL OUT (AT APPROXIMATELY 20 - 30 KNOTS) THE BRAKES RELEASED EVEN THOUGH THE BRAKING PRESSURE WAS NOT REDUCED. THE AIRPLANE CONTINUED ROLLING FOR APPROXIMATELY 15-30 YARDS THEN THE BRAKES KICKED BACK IN AGAIN. TROUBLESHOT BRAKE CONTROL SYSTEM, FOUND SDR DXTA200501126Coalescer Bag · contaminatedHOT OIL SMELL CAME INTO CABIN DURING CLIMB. INDICATED AIRSPEED 215 KNOTS, CLIMBING 100 FT PER MINUTE THRU 41,700 FT. ALL INDICATIONS NORMAL (OIL, HYDRAULIC AND ELECTRICAL). INSPECTED ENGINE, APU, AND ACM OIL LEVELS. ALL INDICATE FULL. REMOVED PLUMBING FROSDR DXTA200501100Control Panel · hotAT FL390 RIGHT REAR PASSENGER AUDIO & LIGHTING PANELS WERE VERY HOT TO THE TOUCH. PANELS COOLED OFF ONCE AIRCRAFT WAS ON THE GROUND. BURNING WIRING ODOR IN A/C REAR, NO SMOKE OBSERVED. ITEM IS UNDER INVESTIGATION.SDR DXTA200501099Position Switch · out of adjustCAB DOOR UNLOCK LIGHT WAS FLICKERING ON TAKEOFF ROLL, AFTER THE ABORT THE ANNUNCIATOR EXTINGUISHED. REPEAT WRITE UP. ADJUSTED UPPER FWD DOOR PIN SWITCH, OPERATIONAL CHECKS SATISFACTORY. ALL WORK IAW CE-650 M/M CHPT 52-70-00.SDR DJFA2005163Spar · corrodedDURING AN UNSCHEDULED MAINTENANCE VISIT, WHILE INVESTIGATING A FUEL LEAK, CORROSION WAS DISCOVERED ON BOTH FORWARD AND BOTH AFT WING SPAR SPLICES ON THE UNDERSIDE OF THE WING DIRECTLY ABOVE THE SKID RAILS.SDR CA051018001Turnbuckle · chafedDURING PHASE 1-5 INSPECTION ON AIRCRAFT, TECHNICIANS DISCOVERED THAT THE LT AND RT AILERON CABLES WERE FOULING. THE RESULT WAS THAT THE LT TURNBUCKLE WAS CHAFED AND THE RT SIDE THE SAFETY CLIP WAS GONE AND THE TURNBUCKLE WAS ALSO CHAFED.SDR DXTA200501018Control Panel · hotBURNT WIRING SMELL WAS NOTICED AFTER ENGINE SHUTDOWN. HEADING AD SELECTION CONTROL PANEL WAS EXTREMELY HOT SO COMPLETE SHUTDOWN WAS INITIATED. - TROUBLESHOT TO BAD REMOTE INSTRUMENT CONTROLLER, REPLACED BAD R.I.C. IAJ CE 650MM CH 34-21-00 + OPS CHECK GOOD.SDR DJFA2005148Line · leakingCREW REPORTED THAT RT ENGINE OIL LOW PRESSURE ANNUNCIATOR HAD ILLUMINATED WHILE IN CRUISE FLIGHT APPROX AN HOUR AND A HALF AFTER TAKE OFF. RT ENGINE OIL PRESSURE INDICATED BETWEEN 38 - 25 PSI. POWER TO RT ENGINE WAS REDUCED TO FLIGHT IDLE, AND AN EMERGENCY WSDR JDW2005F00000Pin · looseRT MAIN GEAR OLEO STRUT WOULD NOT COMPRESS AFTER LANDING, MORE THAN 50 PERCENT OF NORMAL. AC WAS JACKED, SERVICE OF THE STRUT WAS CHECKED NORMALLY. NEX LANDING, STRUT WOULD AGAIN NOT COMPRESS. OLEO WAS REMOVED FROM AC AND DISASSEMBLED. METERING PIN INSIDE SDR DXTA200500988Smoke Detector · faultyDURING THE TAKEOFF ROLL, THE RED "SMOKE DETECT" LIGHT CAME ON TRIGGING THE MASTER WARNING, DURING THE TAXI BACK TO THE FBO THE LIGHT AND MASTER WARNING KEPT ON ILLUMINATING AND FLASHING. TROUBLESHOT SYSTEM AND FOUND SMOKE DETECTOR BOX FAULTY. REMOVED DEFECTISDR DXTA200500973Fire Detector · malfunctionedAPU FIRELIGHT CAME ON IN FLIGHT, PUSH THE LIGHT AND BLEW THE BOTTLE AS PER CHECKLIST, INSPECTED APU AND SURROUNDING AREA NO DAMAGE NOTED, MEL PER CE-650 NJA MEL MANUAL. ITEM IS UNDER INVESTIGATION.
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