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 = '414A' 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 = '414A' 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 97ZZZX5107Cylinder · crackedOIL LEAKED FROM THE CRACKED CYLINDER WHICH FLOWED ONTO THE EXHAUST SYSTEM AND CAUSED SOME SMOKE TO BE FORCED INTO THE CABIN. THE PILOT DID A PRECAUTIONARY SHUT DOWN AND LANDED AT RAPID CITY WITHOUT ANY FURTHER INCIDENT.SDR 97ZZZX4626Exhaust Elbow · crackedDURING MAINTENANCE CHECK, EXHAUST STAIN NOTED ALONG A WELD ON THE ELBOW FROM THE EXH WYE TO THE EXH WASTEGATE. CLOSER EXAMINATION SHOWED THE ELBOW CRACKED ALONG EDGE OF THE WELD ON BOTH SIDES. ON THIS PARTICULAR PART, WHICH IS IDENTIFIED AS A PMA REPLACEMENTSDR 97ZZZX4580Manifold Assy · defectivePILOT REPORTED THE 'HYDRAULIC PRESSURE' LIGHT WOULD NOT EXTINGUISH WHEN THE LANDING GEAR WAS RETRACTED. RED TRANSIT LIGHT EXTINGUISHED. GEAR CYCLED 5 TIMES IN THE AIR WITH NO CHANGE. AIRCRAFT RETURNED TO STATION. AIRCRAFT PLACED ON JACKS. GEAR CYCLED 5 TISDR CA971015060Camshaft · spalled(CAN) OIL FILTER INSPECTION FOUND METAL CONTAMINATION. ENGINE WAS SENT FOR INVESTIGATION AND REPAIR. DISASSEMBLY FOUND WEAR/SPALLING ON THE CAMSHAFT LOBES AND THE CAM FOLLOWERS FACE. THE CAMSHAFT AND FOLLOWERS WERE REPLACED. THE ENGINE WAS CLEANED, REASSEMBLEDSDR 97ZZZX4255Control Cable · brokenPILOT REPORTED LOUD BANG WHEN FLAPS SELECTED DOWN. LEFT FLAP JAMMED AND RIGHT FLAP WAS UNCONTROLLABLE. PILOT MANAGED A SAFE LANDING. INSPECTION REVEALED THE RIGHT FLAP EXTEND CABLE HAD BROKEN WHERE THE CABLE WRAPS AROUND THE FIRST SET OF PULLEYS OUTBOARD OFSDR CA970909018Pressure Switch · failed(CAN) ON GEAR RETRACTION AFTER TAKEOFF, THE HYDRAULIC PRESSURE LIGHT REMAINED ILLUMINATED. LANDING GEAR EXTENDED, LIGHT REMAINED ON. MAINTENANCE INVESTIGATION FOUND AN INOPERATIVE PRESSURE SWITCH. THE SWITCH WAS REPLACED AND RETRACTION TESTS CARRIED OUT, SESDR 97ZZZX3833Lever Assy · detachedRIGHT PROPELLER GOVERNOR CONTROL ARM CAME LOOSE FROM GOVERNOR JUST AFTER TAKEOFF CAUSING PROPELLER TO START GOING TO FEATHER AND A LOSS IN POWER. SUBMITTER RECOMMENDATION, CHECK TORQUE ON CLAMP SCREW EVERY 100 HOURS. OVERHAULED BY ROCKY MOUNTAIN PROPELLERS.SDR 97ZZZX3834Cylinder · crackedTHE TWO REPORTED ENGINES EXHIBITED FUEL STAINS ADJACENT TO THE ENGINE FUEL INJ ECTORS ON 9 OF A POSSIBLE 12 CYLINDERS. FURTHER EXAMINATION REVEALED CYLINDER HEAD CRACKS UNDER CYLINDER FINS (AT THE INTAKE PORTS) AND THROUGH THE SPARK PLUG BOSSES ON EACH OF THE SDR 97ZZZX3692Engine · rpm lossPILOT REPORTED RIGHT ENGINE FLUCTUATED IN-FLIGHT. WHEN PROPELLER LEVER WAS MOVED, RPM DECREASED. TROUBLESHOT SYSTEM. ADJUSTED IDLE MIXTURE AND SPEED. ADJUSTED FOR 30 RPM RISE AND 600 RPM IDLE PER MM. GROUND CHECK OK. UPON FURTHER INVESTIGATION, FOUND LOW SDR 97ZZZX3018Hook · crackedOLD UPLOCK HOOK CRACKED IN HOOK AREA. NEW UNPLOCK HOOK ASSY PN 5141312-10 IS MUCH HEAVIER. SUSPECT CAUSE WAS TIME AND NUMBER OF GEAR CYCLES.SDR 97ZZZX3482Stud · brokenTHE LEFT ENGINE NR 1 CYLINDER HAD 5 BROKEN HOLD-DOWN STUDS (ALL 3 ON THE BOTTOM AND 2 FORWARD ON TOP) WHICH CAUSED A VIBRATION AND RPM REDUCTION AT FULL POWER. ALL THE STUDS WERE BROKEN JUST UNDER THE HOLD-DOWN NUTS. REPLACEMENT OF ALL STUDS ON THAT CYLINDERSDR 97ZZZX3486Bearing · wrong partPULLED STRUTS TO RESEAL. DISCOVERED UPPER BEARING BLOCKS, AD 90-02-13, REQUIRES MAGNAFLUX EACH 1,000 HOURS, BUT SERIAL NUMBER DOES NOT APPLY TO 414A AFTER 0340. THESE WERE NOT BROKEN, BUT HAVE FOUND SEVERAL ON EARLIER AIRCRAFT COVERED BY THE AD BROKEN.SDR 97ZZZX1982Pump · leakingPILOT REPORTED BOTH LEFT AND RIGHT HYDRAULIC FLOW LIGHTS ON THE CAUTION PANEL WERE ILLUMINATED. LANDING GEAR WAS EXTENDED USING THE EMERGENCY EXTENSION PROCEDURE. AIRPLANE LANDING WITHOUT INCIDENT. FLUID DISCOVERED LEAKING FROM RIGHT ENGINE NACELLE DRAIN. SDR 97ZZZX1219Line · corrodedALUMINUM LINE THAT ATTACHES TO GEAR BLOW-DOWN BOTTLE HAS A HOLE CORRODED IN TUBE 7.5 INCHES DOWN FROM BLOW-DOWN BOTTLE WHERE IT LAYED AGAINST THE CROSS-OVER HEAT DUCT INSULATION. SUBMITTER SUGGESTED LINE BE BENT OUT ENOUGH TO RELIEVE PRESSURE AND CHAFING PROBSDR CA970325001Cylinder Assy · cracked(CAN) DURING INSPECTION FUEL STAINS WERE FOUND AT THE COOLING FIN AREA ON ONE OF THE CYLINDERS. THE CYLINDER WAS REMOVED. FURTHER INVESTIGATION REVEALED A CRACK STARTING ABOVE THE VALVE SEAT UP AND TOWARD THE INTAKE PORT. THE CYLINDER WAS REPLACED.SDR 97ZZZX1185Hook Assy · malfunctionPILOT REPORTED THAT AFTER GEAR RETRACTION ON TAKEOFF, THE GEAR UNLOCK RED LIGHT AND THE HYDRAULIC PRESSURE MASTER CAUTION LIGHT REMAINED ILLUMINATED. ACFT LANDED WITHOUT INCIDENT. AIRCRAFT PLACED ON JACKS AND GEAR OPERATIONAL CHECK ACCOMPLISHED. DISCREPANCYSDR 97ZZZX1183Hose Elbow · blownENG INDUCTION HOSE BLOWN OUT CAUSING INDUCTION LEAKAGE AND ENG PERFORMANCE DEGRADATION IN ALL PWR MODES. RECOMMEND CHANGING THE MATERIAL HOSES ARE MADE FROM. THIS IS THE THIRD OCCURENCE IN LESS THAN 600 HRS.SDR 97ZZZX1188Elbow · tornPILOT REPORTED THAT THE RIGHT ENGINE WOULD NOT MAINTAIN POWER. MANIFOLD PRESSURE DECREASED DURING FLIGHT. TAKEOFF POWER OKAY ON BOTH ENGINES. DURING CLIMB, THE RIGHT ENGINE ONLY DEVELOPED 27 IN HG. IT WAS DISCOVERED THAT THE INBOARD INDUCTION ELBOW RAM P/NSDR 97ZZZX1104Control Cable · frayedBASED ON PREVIOUS INSPECTIONS, REMOVED FLAP CABLES FOR CLOSE INSPECTION BY TWISTING AND BENDING. FOUND MANY INTERNAL STRANDS BROKEN. SUBMITTER STATED MAY NEED TO HAVE LIFE LIMIT. THIS IS THE THIRD OCCURRENCE OUT OF FOUR, 400 SERIES INSPECTED IN PAST SIX MONSDR 97ZZZX797Packing · cutPILOT REPORTED THAT BOTH LEFT AND RIGHT HYDRAULIC PRESSURE CAUTION LIGHTS WERE ILLUMINATED. LANDING GEAR WOULD NOT EXTEND. LANDING GEAR WAS EXTENDED USING THE EMERGENCY EXTENSION PROCEDURE. AIRPLANE WAS JACKED AND THE LANDING GEAR OPERATIONAL CHECK WAS PERFSDR 97ZZZX1050Control Cable · wornEXTREME CABLE WEAR (FLAP EXTEND) AT PULLEY ASSY JUST OUTBOARD OF THE FLAP MOTOR AND TRANSMISSION ASSY. PULLEYS MUST BE REMOVED IN ORDER TO SEE THIS TYPE OF WEAR. SUBMITTER RECOMMENDED 100 PERCENT INSPECTION OF FLAP CABLES (BY REMOVAL AND REPLACEMENT) AT 4,00SDR 96ZZZX5721Pump · seal failedLT AND RT HYD LOW FLOW LITES CAME ON IN FLIGHT. LANDING GEAR HAD TO BE EXTENDED USING THE LANDING GEAR EMERGENCY PROCEDURE. ACFT LANDED WITHOUT INCIDENT. RIGHT HYD PUMP NOSE SEAL LEAKED HYDRAULIC FLUID OVERBOARD THROUGH THE NOSE CASE DRAIN. PUMP REPLACED. SDR 96ZZZX5646Control · wornA SPLIT FLAP CONDITION OCCURRED ON FINAL APPROACH. THE OUTER HOUSING OF THE PRE-SELECT CONTROL IS BADLY WORN WHERE IT MOUNTS TO BULKHEAD AT STA 166. FLAP CABLE AND PRE-SELECT ARE NOT RUNNING PARALLEL WITH EACH OTHER. SUBMITTER STATED A STRONGER MOUNTING MIGSDR 96ZZZX5645Cable Assy · frayedA SPLIT FLAP CONDITION OCCURRED ON FINAL APPROACH. AFTER CHECKING SYSTEM, ALL CABLES WERE REMOVED FROM AIRCRAFT FOR REPLACEMENT. INTERNAL CABLE WEAR WAS FOUND AT ALL PULLEY LOCATIONS. HIGH CABLE SYSTEM TENSION IS REQUIRED ON THESE CABLES. SUBMITTER SUGGESTSDR 96ZZZX5644Cable Assy · brokeA SPLIT FLAP CONDITION OCCURRED ON FINAL APPROACH. FLAP EXTEND CABLE WAS FOUND BROKEN ON INBOARD SIDE OF PRE-SELECT CONTROL ATTACH CLAMP. PRE-SELECT CABLE IS NOT RUNNING PARALLEL TO FLAP CABLE. THIS EXTEND CABLE WAS ALSO FOUND TO HAVE INTERNAL WEAR AT PULLESDR 96ZZZX5600Tube · stem failedON LANDING ROLL-OUT, NOSE TIRE DEFLATED. FENDER P/N 5042022-9 WAS TORN FROM THE NOSE GEAR ASSEMBLY. IT WAS DISCOVERED THE VALVE STEM WAS MISSING FROM THE NOSE TIRE. NOSE TIRE P/N 600-6-8-330 HAD BEEN REPLACED 8-10-95. THE TOTAL TIME ON THE TIRE SINCE REPLASDR CA961025007Check Valve · failed(CAN) DURING GROUND RETRACTION TESTS, THE GEAR FAILED TO RETRACT. HYDRAULIC PRESSURE CLIMBED SUFFICIENTLY TO TRIP PNEUMATIC BLOWDOWN SYSTEM. PROBLEM TRACED TO CHECK VALVE WHICH ALLOWED HYDRAULIC PRESSURE TO BE APPLIED TO GEAR UP, GEAR DOWN AND PNEUMATIC BLOWDOSDR CA961025006Sight Tube · melted(CAN) THE NOSE GEAR FAILED TO LOCK IN THE UP POSITION AFTER TAKEOFF PREVENTING THE HYDRAULIC SYSTEM FROM CYCLING TO 'OPEN CENTRE' OPERATION. CONTINUED HYDRAULIC PRESSURE RAISED FLUID TEMPERATURE TO MELT PLASTIC RESERVOIR SIGHT TUBE AND SUBSEQUENT LOSS OF HYDRASDR 96ZZZX5404Crankcase · crackedAFTER REMOVAL OF CYLINDER NR 4 DUE TO A LEAKING EXHAUST VALVE, A 4 INCH CRACK WAS FOUND STARTING AT THE NR 2 MAIN JOURNAL. THIS CRACK STARTED AT THE BEARING SURFACE AND PROGRESSED TO THE INSIDE OF THE CASE BETWEEN CYLINDERS NR 2 AND 4. NO EVIDENCE OF A CRACKSDR 96ZZZX5413Nitrogen Line · rupturedFOUND CORROSION ON THE NITROGEN LINE FROM THE EMERGENCY GEAR BLOW DOWN BOTTLE WHERE IT WAS IN CONTACT WITH BLACK HEAT DUCT. THERE WAS NO CORROSION FOUND ON THE LINE EXCEPT WHERE IT MADE CONTACT WITH THE HEAT DUCT. WHEN THE EMERGENCY GEAR DOWN BOTTLE ACTIVATESDR 96ZZZX5412Structure · corrodedCORROSION FOUND AROUND THE HOLES (WHEELWELL-NOSE) AREA WHERE THE BLACK HEAT DUCT TUBING THAT RUNS THROUGH STRUCTURE MAKES CONTACT WITH THE ALUMINUM. FOUND THIS ON A 1981 CESSNA 414A WITH A TOTAL TIME OF 4900 HRS AND ALSO 1981 CESSNA 425 WITH 6203 HRS.SDR 96ZZZX5443Switch · looseLANDING GEAR FAILED TO RETRACT. AIRCRAFT LANDED WITHOUT INCIDENT. IT WAS DISCOVERED THE WIRING HARNESS HAD TORN LOOSE FROM THE MICROSWITCH. HYD ACTUATOR WAS REPLACED. OPERATIONAL CHECK PERFORMED AND IS OKAY.SDR 96ZZZX5118Support · crackedSUPPORT CRACKED/SPLIT FROM THE AFT BOLT HOLE TO FORWARD BOLT HOLE AND OUT THE FRONT. LANDING GEAR UPLOCK HAS MOVED UPWARD ALLOWING LANDING GEAR STRUT TO CONTACT UPPER WING SKIN. WING SKIN DENTED SLIGHTLY OVER MAIN WHEEL AXLE. SUPPORT IS LATE STYLE WITH LARGSDR EY2R9600987Nut · corrodedNUT CORRODED.SDR EY2R9600986Dowel · corrodedDOWEL CORRODED.SDR EY2R9600985Cylinder Pin · corrodedCYLINDER PIN FOUND CORRODED.SDR 96ZZZX4753Uplock Hook · crackedUPLOCK HOOK FOUND CRACKED AFTER GEAR WOULD NOT RETRACT AND REMAIN IN UPLOCK. ALSO, FOUND P/N 5141204-3, CRACKED AT FORWARD BLOCK ATTACH HOLE. HOOK CRACKED AT RADIUS OF MLG RETAINING CUT OUT. UNABLE TO DETERMINE IF DAMAGE OCCURRED UPON LAST EXTENSION OR RETRSDR AU961084Rheostat · burnt(AUS) PILOTS PANEL LIGHTING RHEOSTAT SHORT CIRCUITEDSDR 96ZZZX5252Pump · shaft shearedFOLLOWING PUMP REMOVAL FOR FAILURE, FOUND DRIVE SHAFT SHEARED. THIS IS A VACUUM TYPE SYSTEM.SDR 96ZZZX5251Pump · shaft shearedFOLLOWING PUMP REMOVAL FOR FAILURE, FOUND DRIVE SHAFT SHEARED. THIS IS A VACUUM TYPE SYSTEM.SDR 96ZZZX4800Tire · rubs plateDURING INSPECTION, BOTH GOODYEAR 6:50 X 10 8-PLY FLT CUSTOMER II TUBE TYPE TIRES FOUND DAMAGED BY BRAKE ASSY BACK PLATES. AFTER WORN PARTS OF BRAKE ASSY WERE REPLACED, NEW TIRES WERE INSTALLED. (SAME MAKE, GOODYEAR.) TIRES STILL RUBBED. INSPECTED TWO OTHERSDR 96ZZZX4069Fitting · crackedDURING ANNUAL INSPECTION, A CRACK WAS DISCOVERED IN THE RT ELEVATOR TORQUE TUBE ATTACH FITTING. CRACK RADIATED FROM TAPERED HOLE. NEW FITTING DELIVERED FROM CESSNA WAS OF DIFFERENT DESIGN AND REQUIRED NEW HOLE DRILLED IN TORQUE TUBE FOR TAPERED PIN INSTALLATSDR 96ZZZX4068Rib · crackedDURING ANNUAL INSPECTION, A CRACK WAS DISCOVERED IN RT OUTBOARD WING RIB WHERE AILERON HINGE BEARING BLOCK ATTACHES. CRACK IS HARD TO DETECT WITH AILERON INSTALLED. SUSPECT CAUSE IS THOUGHT TO BE FLYING IN TURBULENT AIR ABOVE MANEUVERING SPEED.SDR 96ZZZX3923Elbow · blown outAIRCRAFT RETURNED FROM FLIGHT ON SHORT FINAL. ENGINE RPM COULD NOT BE REDUCED BELOW 1,400 RPM. SECURED ENGINE WITH MIXTURE TO PREVENT ASYMMETRIC THRUST CONDITION. UPON INSPECTION BY MECHANIC, FOUND BLOWN OUT INDUCTION ELBOW. SECOND OCCURRENCE IN 6 MONTHS. SDR CA960711014Line Assembly · chafed(CAN) WASTE GATE OIL SUPPLY LINE FOUND CHAFED ON ENGINE MOUNT BEAM FLANGE. P/N MS21919WCH4 CLAMP AND ASSOCIATED MOUNT BOLT, SPACER, WASHER AND NUT ALSO MISSING WHICH ALLOWED LINE TO DROP DOWN ONTO MOUNT BEAM FLANGE. SUBMITTER STATES AREA IS INCONVENIENT TO INSSDR 96ZZZX5250Pump · shaft shearedFOLLOWING PUMP REMOVAL FOR FAILURE, FOUND DRIVE SHAFT SHEARED. THIS IS A VACUUM TYPE SYSTEM.SDR 96ZZZX3874Regulator · failedREGULATOR FAILED IN-FLIGHT. REGULATOR REPLACED AND ADJUSTMENTS MADE IAW CESSNA SM.SDR 96ZZZX3224Switch · wire burnedPILOT REPORTED ALL MLG GREEN LIGHTS ILLUMINATED AND GEAR UNSAFE LIGHT ILLUMINATED IN-FLIGHT. EMERGENCY EXTENSION PERFORMED, NO CHANGE IN INDICATOR STATUS. AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOOTING REVEALED HIGH RESISTANCE IN THE NLG UPLOCK CIRCUITRYSDR CA960513015Fuel Line · chafed(CAN) FUEL LINE CHAFED ON EDGE OF THE HOLE WHERE IT PASSES THROUGH THE MAIN WING SPAR LT SIDE. LINE INSPECTED AND FOUND WITHIN CHAFE LIMITS OF CESSNA SB MEB 87-7. LINE REPOSITIONED TO PROVIDE CLEARANCE. MANUFACTURER INSTALLED SPIRAL CHAFE STRIP TO PROVIDE PSDR 96ZZZX2766Spring Clutch · failedTWENTY-SIX HOURS AFTER INSTALLING A TCM OVERHAULED ENGINE, STARTER ADAPTER FAILED. INSPECTION SHOWED THAT SPRING CLUTCH FAILED AND WAS UNCOILING INTO ENGINE ACC CASE.
Back to Cessna 414A