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 99ZZZX134Control Cable · out of rigDURING ROUTINE DAILY CHECK, AILERON WING CABLE TENSION WAS FOUND TO BE SO LOW THAT THE CABLES WERE DRAGGING ON THE LOWER SURFACE OF THE WING TRAILING EDGE. TENSION CHECKED 15 POUNDS. MAINTENANCE MANUAL CHAPT 27-10-00 PG 501 SPECS TENSION AT 35 PLUS OR MINUS SDR 99ZZZX133Control Cable · out of rigDURING ROUTINE DAILY CHECK, AILERON WING CABLE TENSION WAS FOUND TO BE SO LOW THAT THE CABLES WERE DRAGGING ON THE LOWER SURFACE OF THE WING TRAILING EDGE. TENSION CHECKED 19 POUNDS. MAINTENANCE MANUAL CHAPTER 27-10-00 PG 501 SPECS TENSION AT 35 PLUS OR MINUSDR 99ZZZX131Control Cable · out of rigDURING ROUTINE DAILY CHECK, AILERON WING CABLE TENSION WAS FOUND SO LOW THE CABLES WERE DRAGGING ON THE LOWER SURFACE OF THE WING TRAILING EDGE. TENSION CHECKED 18 POUNDS. MAINTENANCE MANUAL CHAPT 27-10-00 PG 501 SPECS TENSION AT 35 PLUS OR MINUS 5 POUNDS ATSDR 99ZZZX219Lamp · failedSPRING CONTACT IN LAMP 18 ASSY SEPARATED CAUSING A SHORT CREATING CURRENT OVERLOAD TO COMPONENT U217. U217 BURNED. CAUSE UNKNOWN. SUBMITTER SUSPECTS MISALIGNED OR MISGUIDED CONTACTS ON BULB CHANGE OR WEAK SPRING CONTACTS. PRODUCT HISTORY REVIEWED WITH NO CSDR 98ZZZX4687Actuator · leakingEXTERNAL LEAKAGE INTO WING TRAILING EDGE CAVITY. REPLACED ACTUATOR.SDR 98ZZZX4686Fan · leakingPOST-FLIGHT INSPECTION REVEALED STREAKING ON AFT FUSELAGE HYDRAULIC FAN AFT EXHAUST DUCT AREA. REPLACED HYDRAULIC FAN ASSEMBLY.SDR 99ZZZX875Annunciator Pnl · failedON DESCENT INTO HOME BASE AIRPORT, FLIGHT CREW SMELLED ELECTRICAL ODOR IN COCKPIT FOLLOWED BY ALL ANNUNCIATOR LIGHTS ILLUMINATED. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED FAULT IN ANNUNCIATOR PANEL. CESSNA REQUESTED PANESDR 98ZZZX4359Line · chafedPILOT NOTED LEFT OIL PRESSURE DROPPING IN-FLIGHT AND THAT IT WOULD FOLLOW THROTTLE MOVEMENT. PILOT SHUT LEFT ENGINE DOWN AND LANDED 15 MINUTES LATER NORMALLY. INVESTIGATION REVEALED NR 6 BEARING PRESSURE OIL LINE CHAFED THROUGH FROM CONTACT WITH CESSNA BLEEDSDR 98ZZZX3251Skin · crackedAT 6 O'CLOCK POSITION, A CRACK WAS VISIBLE COMING OFF THE T/E OF THE OUTER SKIN AT ES 239.49 WHERE THE THRUST REVERSER MEETS THE OUTER SKIN OF THE AFT BODY (WHEN THE THRUST REVERSER IS IN THE STOWED POSITION). UPON INVESTIGATING, DETERMINED THE OUTER SKIN PANSDR 98ZZZX3250Skin · crackedBOTH AFT BODIES HAD A KEVLAR CRACK AND DELAMINATION AT THE 12 O'CLOCK POSITION. BOTH DEFECTS CAUSED BY A METAL BRACKET RIVETED TO COMPOSITE STRUCTURE AFT OF FWD ATTACH FLANGE. 2 RIVETS GOING DOWN THRU OUTSIDE SKIN INTO BRACKET ARE FLATTENING OUTSIDE CURVE OFSDR 98ZZZX3249Skin · crackedAT ES 239.49 IS LOCATED A RIB BONDED AND RIVETED TO THE INTERNAL AND EXTERNAL SKINS. ON THE OUTSIDE SKIN THERE ARE AREAS OF FATIGUE THAT TAP TESTED BAD AND HAD PAINT CRACKS ORIGINATING AT THE LAST RIVET HEAD ON THE UPPER AND LOWER ENDS OF THE RIB. THE CRACKSSDR 98ZZZX1869Connection · loosePILOT REPORTED AFT J-BOX CB ANNUNCIATOR ILLUMINATED IN-FLIGHT. FOUND BAGGAGE HEAT AND APU AUX HYD PUMP CONTROL CB'S LOCATED IN AUX DC J-BOX TRIPPED. USED AN INSP MIRROR AND FOUND NO OBVIOUS WIRING DEFECTS. AFTER SEVERAL HRS OF SYS T/S AFT J-BOX CB ANNUNCIATSDR 98ZZZX1527Door Rod · failedTHIS IS THE THIRD SECONDARY DOOR ROD INSTALLED ON THIS AIRCRAFT. SUBMITTER SUGGESTED THERE ARE TWO SUSPECT CAUSES FOR THESE FAILURES. ROD DIAMETER IS TOO SMALL FOR THE LOADS ENCOUNTERED OR DEFECTIVE RODS.SDR 98ZZZX4611Current Limiter · failedON MARCH 27, 1998, AT 1330 ON APPROACH TO ASPEN, COLORADO, THE PILOTS GOT AN INOPERATIVE INDICATION FOR THE FLAP MOTOR. ABORTED LANDING AND DIVERTED TO DENVER. REPLACED THE FLAP MOTOR. CURRENT LIMITER CHECKED OKAY. RETURNED TO SERVICE. REF: CESSNA 650 WISDR CA980331012Pump · low pressure(CAN) AFTER TAKEOFF, THE LEFT HAND HYDRAULIC LOW PRESSURE LIGHT CAME ON. LT HYDRAULIC PUMP CHANGED AND GROUND RUN OK. LT UNLOADING VALVE TO BE CHANGED WHEN PARTS AVAILABLE. PARTS TC: 1,962.SDR 98ZZZX1103Current Limiter · failedDURING NORMAL APPROACH WHEN FLAPS WERE SELECTED FROM SEVEN DEGREE POSITION TO TWENTY DEGREES, FLAPS STARTED DOWN THEN STOPPED. NO ADVERSE EFFECTS FELT ON THE AIRCRAFT AND NORMAL LANDING MADE. TOLEDO CITATION SERVICE CENTER HELP WAS REQUESTED AND THEY CAME TOSDR 98ZZZX1069Rod · failedTHE MLG UPPER DOOR ROD P/N NAS 354-4-240 HAS BROKEN 2 TIMES. SUSPECT DUE TO EXCESSIVE AIR LOAD FOR THE ROD SIZE OR DEFECTIVE RODS. TAT: 1661. LANDING: 1,055.SDR 98ZZZX1245Switch · failedBLOWER BECAME NOISY. FOUND 5 EACH FAN BLADES MISSING (P/N 2100900-25). REMOVED BLOWER FROM AUX HEATER (P/N 6214434-53). FOUND BLADES IN AUX HEATER, ALSO FOUND AIRFLOW SWITCH VANE. SUSPECTED THE VANE CAME OFF THE AIRFLOW SWITCH ASSY CAUSING THE BLADES TO BRESDR 98ZZZX859Resistor · failedRESISTOR HAD OVERHEATED CAUSING HEAT DAMAGE TO THE CASE AND PC BOARD. THE DECAL ON THE OUTSIDE OF THE CASE WAS DISCOLORED. ACCORDING TO THE AIRCRAFT RECORDS, THE LAST ELT OF THIS TYPE WAS ALSO REPLACED BECAUSE OF INTERNAL HEAT DAMAGE. SUBMITT ER STATED A DIFFSDR 98ZZZX806O-Ring · mismanufacturedON MAINTENANCE POST-FLIGHT, DISCOVERED RIGHT ENGINE HYDRAULIC MAIN FILTER WET WITH HYDRAULIC FLUID. INVESTIGATION SHOWED LEAKAGE FROM FILTER BOWL SEAL AND TEFLON CHEVRON AREA. INSPECTION OF O-RING SEAL AND BACK-UP TEFLON RINGS SHOWED BEVEL DEFECT ON BACK-UP SDR 98ZZZX479Backup Ring · mismanufacturedON MAINTENANCE POST-FLIGHT, DISCOVERED RT ENGINE HYDRAULIC MAIN FILTER WET WITH HYDRAULIC FLUID. INVESTIGATION SHOWED LEAKAGE FROM FILTER BOWL SEAL AND TEFLON CHEVRON AREA. INSPECTION OF O-RING SEAL AND BACK-UP TEFLON RINGS SHOWED BEVEL DEFECT ON BACK-UP RINSDR 98ZZZX705Control Cable · wornRIGHT WING AILERON CABLE (OUTBOARD, AFT) WORN THROUGH CLAD. FOUND DURING OPERATION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE CHANGE, ALL PRIMARY CONTROL SURFACES.SDR 98ZZZX704Control Cable · frayedRIGHT WING AILERON CABLE, (INBOARD, FORWARD) HAS BROKEN WIRES IN SEVERAL STRANDS AT CABLE PULLEYS WS 88.00. FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE HCANGE, ALL PRIMARY CONTROL SSDR 98ZZZX703Control Cable · frayedRIGHT WING AILERON CABLE (INBOARD FORWARD), HAS BROKEN WIRES IN ONE STRAND AT CABLE PULLEYS WS 88.00. FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE CHANGE, ALL PRIMARY CONTROL SURFACESDR 98ZZZX702Control Cable · frayedRIGHT WING AILERON CABLE, (OUTBOARD, FORWARD), HAS BROKEN WIRES IN STRAND AT CABLE PULLEY WS 175.63 (PLUS OR MINUS). FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE CHANGE, ALL PRIMARYSDR 98ZZZX701Control Cable · frayedRIGHT WING AILERON CABLE, (OUTBOARD, AFT) HAS BROKEN WIRES IN STRAND AT CABLE PULLEY WS 175.63 (PLUS OR MINUS). FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE CHANGE, ALL PRIMARY CONTRSDR 98ZZZX700Control Cable · frayedRIGHT AILERON CABLE, (OUTBOARD FORWARD) AT CABLE PULLEYS WS 175.63 (PLUS OR MINUS) HAS BROKEN WIRES IN STRAND. FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HR CABLE CHANGE, ALL PRIMARY CONTROL SDR 98ZZZX699Control Cable · frayedRIGHT AILERON CABLE (INBOARD FOWARD) AT CABLE PULLEYS WS 88.00. BROKEN WIRES IN THREE STRANDS. FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800 HOUR CABLE CHANGE, ALL PRIMARY SURFACES.SDR 98ZZZX698Control Cable · frayedRIGHT WING AILERON CABLE, OUTBOARD, AFT HAS BROKEN WIRES IN STRAND AT CABLE PULLEY WS 175.63 (PLUS OR MINUS). FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE CHANGE, ALL PRIMARY CONTROLSDR 98ZZZX91Hose · leakingCREW COMPLAINED OF FUEL ODOR IN AFT BAGGAGE COMPT. INVEST REVEALED A FUEL HOSE LEAKING THRU OUTER JACKET. HOSE IS APPROX 16 INCHES LONG AND LOCATED ABOVE RT FWD CEILING OF AFT BAGGAGE COMPT BETWEEN APU FUEL SHUT-OFF VALVE AND A UNION. THE OTHER SIDE IS ATTSDR 98ZZZX174Switch · failedDURING SCHEDULED CALIBRATION (OPERATION 12) INSPECTION, CABIN OVERHEAT SWITCH FAILED TEST DUE TO OUT OF TOLERANCE. REPLACED SWITCH WITH SERVICEABLE ASSEMBLY. NEW SWITCH WAS VERIFIED IN TOLERANCE PRIOR TO INSTALLATION.SDR 97ZZZX5095Actuator Control · failedAIRCRAFT PRIMARY PITCH TRIM INOPERABLE. IF NOSE UP OR DOWN WAS SELECTED, PITCH TRIM WOULD NOT MOVE AND PITCH TRIM FAIL ANNUNCIATOR WOULD COME ON. TROUBLESHOT DOWN TO ACTUATOR CONTROL UNIT. ORDERED AND INSTALLED REPLACEMENT UNIT. TURNED AIRCRAFT POWER ON, PSDR 97ZZZX5081Loran · malfunctionedLORAN GIVES CONSTANT BATTERY WARNING MESSAGE. REMOVED AND REPLACED.SDR 97ZZZX4855Pressurization · malfunctionedAIRCRAFT DID NOT PRESSURIZE DURING FLIGHT TO PHOENIX FROM PARKER, AZ. CHECKED GEAR SQUAT SWITCHES AND WIRING. PERFORMED GROUND PRESSURIZATION OF AIRCRAFT WITH APU. APPROVED AIRCRAFT FOR RETURN TO SERVICE. MAINTENANCE CHECK FLIGHT PERFORMED. AIRCRAFT FUNCTSDR 97ZZZX4857Bolt · failedNOSE GEAR CHECKED FOR BENT ROD ON GEAR DOOR REPORTED BY LINE SERVICE. ALL GEAR DOOR RODS WERE CORRECT SHAPES FOR LOCATIONS. DURING CHECK, LEFT ROD TO SPADE DOOR ATTACH BOLT FAILED. BOLT WAS BROKEN AT HEAD WITH SHANK LEFT IN GEAR HOUSING BODY. REMOVED AND RSDR 97ZZZX4856Light · breaker trippedRIGHT LANDING LIGHT IN NOSE WOULD NOT RETRACT AFTER LANDING AT MDW. FOUND CIRCUIT BREAKER UPSET AND RESET. UNIT FUNCTIONAL CHECKED. EXTENDED AND RETRACTED WITH AND WITHOUT LOAD. LANDINGS, 4,874.SDR 97ZZZX4285Actuator · malfunctionDURING PREFLIGHT, DISCOVERED THE SECONDARY TRIM OPERATED BACKWARDS. THE OVERHAULED ACTUATOR WAS INSTALLED 5 HOURS PREVIOUSLY. SUBMITTER STATED REVIEW OVERHAUL, FUNCTIONAL TEST AND QUALITY CONTROL PROCEDURES AT ELECTROMECH TECHNOLOGIES. FOLLOW MM PROCEDURES SDR BTVR82997Heat Barrier · corrodedEXHAUST OUTLET WAS REMOVED FOR WELD REPAIR. FUSELAGE DOUBLER WAS CORRODED THROUGH (2 PLACES) WITH SUBSEQUENT CORROSION ON AIRCRAFT SKIN. REPAIRED IAW CESSNA REPORT S650-0033/01RD WHICH REPLACED HEAT BARRIER WITH HIGH TEMP (RED) RTV 106. THIS WILL PREVENT INGSDR 97ZZZX5082Controller · malfunctionedUNIT REPORTED TO CAUSE AN INTERMITTENT TRIM FAIL ANNUNCIATOR LIGHT.SDR 97ZZZX3729Sense Probe · plug looseNR 2 ENGINE SURGED TWICE DURING CLIMB-OUT. INDICATIONS WERE OBSERVED ON BOTH FAN AND FUEL FLOW. AIRCRAFT ALSO YAWED. FOUND NR 2 ENGINE PT2 LENS PROBE PLUG LOOSE, ALSO, DIRTY WITH RUST-LIKE MATERIAL. CLEANED PROBE AND PLUG. SWAPPED PT2 PROBE LT TO RT PER INSDR 97ZZZX3174Support Bracket · failedNOSE GEAR REMAINED IN UP POSITION WHEN GEAR SELECTED TO DOWN POSITION. EMERGENCY EXTENSION PERFORMED AND GEAR EXTENDED AND SHOWED GEAR SAFE LIGHTS. UNEVENTFUL LANDING AND TAXI TO RAMP. INSPECTION FOUND DAMAGED UPLOCK SUPPORT BRACKET. CITATION 650 SB 650-53SDR 97ZZZX3079Servo · failedDURING APPROACH, CREW NOTICED RUDDER OPERATION WAS EXTREMELY STIFF IN BOTH DIRECTIONS. MAINT INVESTIGATION VERIFIED RUDDER TRAVEL WAS FULL, BUT VERY STIFF WITH OR WITHOUT ELECTRIC POWER. OCCASIONALLY, STIFFNESS WOULD BREAK FREE, THEN RE-ENGAGE. THE RUDDER SSDR 97ZZZX3049Housing · crackedAFTER LANDING DURING THE CREWS TRANSIENT WALK-AROUND, FOUND THE LT ENGINE OIL QUANTITY ONE AND ONE-HALF QUARTS LOW. THE OIL WAS FULL BEFORE THE 2-1/2 HOUR FLIGHT. FURTHER INVESTIGATION REVEALED A CRACKED OIL FILTER HOUSING PN 3072231-1. ALSO, FOUND A CRACKEDSDR 97ZZZX3090Filter · failedDURING SMIP INSPECTION OPERATION 10, ITEM 27-20, INSPECTION REVEALED FILTER SEPARATED FROM MOUNTING FLANGE IN THE END OF THE ELBOW FITTING PERMITTING FILTER TO SLIDE BACK AND FORTH WITHIN THE FITTING. SUBMITTER STATED THIS NEGATES FILTERING CAPABILITY. REPLASDR 97ZZZX2544Hydraulic Motor · defectivePILOT REPORTED LOW HYDRAULIC PRESSURE WITH ONE ENGINE RUNNING AND AT IDLE. DISCOVERED THE HYDRAULIC FLUID FLOW RATE THROUGH THE RAM AIR HYDRAULIC FAN TO BE EXCESSIVE. REPLACED ASSEMBLY WITH REPAIRED UNIT AND RETESTED FLOW RATE AND FOUND TO BE WITHIN TOLERANCSDR 97ZZZX1648Motor · leakageACFT PARKING BRAKE WAS SET AND BOTH ENGINES WERE STARTED, ACFT STARTED DRIFTING FWD. THE PILOT RESET PARKING BRAKE, THEN NOTICED BOTH HYD FLUID LEVEL AND HYD PRESSURE GAUGES FALLING RAPIDLY. ENG WERE SHUT DOWN IMMEIDATELY. HYD FLUID WAS FOUND RUNNING DOWN TSDR 97ZZZX1623Overlay · shortedUPON REINSTALLATION OF THE PILOT'S SIDE MAIN CIRCUIT BREAKER PANEL OVERLAY, THE ATTACHING SCREW INSTALLED IN THE AFT CENTER MOUNT HOLE CONTACTED THE VERTICAL LEG OF A BUSS BAR. THE BUSS BAR IS LOCATED DIRECTLY BEHIND (OUTBOARD OF THE MOUNTING NUTPLATE. THE SSDR 97ZZZX1406Supply Tube · crackedDURING AN INSPECTION REQUIRING WING LEADING EDGE PANEL REMOVAL, THE OUTBOARD CENTER LEADING EDGE SECTION ANTI-ICING SUPPLY TUBE WAS FOUND CRACKED AND NOT CONNECTED. THIS WAS DUE TO MISALIGNMENT WHEN INSTALLED NEW AT THE FACTORY.SDR 97ZZZX1626Outflow Valve · defectiveKTEB/KBWI - FLT 8038 - AIRCRAFT WAS NOT PRESSURIZING, CABIN WAS CLIMBING WITH AIRCRAFT. FOUND DEFECTIVE OUTFLOW VALVE.SDR 97ZZZX768Blower Motor · seizedBLOWER MOTOR SEIZED CAUSING EXCESSIVE CURRENT DRAW. THE 15-AMP CIRCUIT BREAKER PROTECTING THE CIRCUIT FAILED TO OPEN. THIS CAUSED THE WIRING FOR THE BLOWER MOTOR TO GET HOT AND EMIT SMOKE AND FOUL ODOR. THE COCKPIT AUX HEATER THEN CIRCULATED THE SMOKE INTO T
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