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 = '550' 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 = '550' 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 CA061109001Tube · cracked(CAN) DURING COMPLIENCE WITH CAMPAIGN NOTICE 851-27-20-035 (RUDDER AND ELEVATOR CABLE GUARDS) BOTH ELEVATOR CABLE GUARDS WERE FOUND TO BE UNSERVICEABLE. ALL (4) CLAMPS WERE DISTORTED AND CAUSED DISTORSION TO THE TUBES WHEN CLAMPED CAUSING CRACKS IN THE TUBES. SDR 2006FA0001148Seat Frame · crackedUPPER CHAIR BASE ASSY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. CHAIR WAS REPAIRED IAW STCC ST01042W STRUCTURAL SEAT REPAIR. (K)SDR Z3S2006F00000Line · obstructed(REF NR SO13001) AT CRUISE ALTITUDE (34,000 FT) THE FLIGHT CREW HEARD A LOUD RUSHING AIR NOISE FOLLOWED IMMEDIATELY BY AN OBSERVED RAPID CLIMB IN CABIN PRESSURE. OXYGEN MASKS WERE DONNED BY FLIGHT CREW AND PASSENGER MASKS WERE DROPPED FLIGHT CREW FOLLOWED EMSDR CA061103016Engine · flamed out(CAN) THE ENGINE FLAMED OUT IN FLIGHT FOLLOWING A COMMANDED REDUCTION IN POWER TO IDLE. PWC WILL MONITOR INVESTIGATION OF THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC# 20061103016)SDR 2006FA0001016Structure · crackedDURING A PHASE NR 5 A CRACH WAS FOUND IN THE LT & RT WHEEL WELL AREA ADJACENT TO THE INSIDE CORNER OF THE OPENING AT THE WHEEL WELL. A REPAIR WAS DONE AS PER SERRIA INDUSTRIES WING SKIN REPAIR ENGINEERING REPORT NR 3521-36 AND A DER 8110-3. THIS REPAIR HAS BEESDR CA061103015Turbine Blades · fractured(CAN) IN CRUISE THE ENGINE EXPERIENCED VIBRATIONS FOLLOWED BY A LOUD NOISE AND WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED FRACTURED TURBINE BLADES. P&WC WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC# 20061103015)SDR CA060905003Fan Blade · failed(CAN) WHEN PILOTS WERE USING FLOOD COOLING ON THE GROUND THEY HEARED A NOISE AND HAD A VIBRATION THEY SHUT THE SYSTEM DOWN . AFTER MAINTENANCE REMOVED THE FLOOD COOLING FAN MOTOR ASSY THEY FOUND A BROKEN FAN BLADE . THEY REPLACED FLOOD COOLING FAN MOTOR ASSY SDR RQ22006F00000Starter Gen · failedDURING FLIGHT, THE CREW NOTICED A VIBRATION COMING FROM THE NR 2 ENGINE FOLLOWED BY NR 2 ENGINE GENERATOR FAIL ANNUNCIATION ILLUMINATING ON THE PANEL. THE CREW ELECTED TO DIVERT. ON APPROACH, VIBRATION BECAME WORSE, SO THE CREW DECIDED TO SHUTDOWN THE NR 2 ESDR 0809200644AS2Web · crackedNOSE LANDING GEAR WHEEL WELL, FOUND WHEEL WELL TOP SKIN CRACKED.SDR 0809200644ASSkin · bentCABIN DOOR SKIN LOWER EDGE IS BENT AND TORN IN SEVERAL AREAS ACROSS THE BOTTOM OF THE DOOR.SDR 0809200644AS1Doubler · gougedA SINGLE GOUGE WAS NOTED IN THE DOUBLER P/N 6511032-18, COMMON TO THE RT STUBWING LOWER SKIN ASSEMBLY.SDR CA060905013Fuel Control · failed(CAN) THE ENGINE FLAMED OUT DURING DESCENT. SUBSEQUENT INSPECTION REVEALED METAL PARTICLES IN THE FUEL SYSTEM DOWNSTREAM OF THE FUEL CONTROL UNIT. THE FUEL SYSTEM COMPONENTS WERE REPLACED. MFG WILL MONITOR INVESTIGATION OF THE FCU AND ADVISE OF ROOT CAUSE ONCSDR CA060731005Indicator · shorted(CAN) DURING TROUBLESHOOTING OF A POSSIBLE N2 OVERSPEED OF BOTH ENGINES, THE N2 GAGE WAS TESTED BY SIMULATING SPEEDS WITH VOLTAGE AT SEVERAL FREQUENCIES. WHEN VALUES WERE BROUGHT AT LEVELS TO ILLUMINATE THE RED OVERSPEED WARNING LIGHT, IT WAS NOTED THAT THE INSDR CA060731001Guard · delaminated(CAN) WHEN MOVING THE RUDDER WITH HAND PRESSURE OF APPROXIMATELY 10 DEGREES EITHER SIDE OF CENTER A NOISE ALONG WITH A ROUGH SNAGGING FEEL NOTICED. TRACING THE NOISE DOWN THROUGH THE TAIL INTO THE CABIN BETWEEN FLIGHT STATION 166 TO 180. THE CABLE GUARD PN 6SDR CA060726007Brushes · worn(CAN) DURING BASE INSPECTION, LT ENGINE COWL WAS COVERED WITH BLACK DUST. UPON FURTHER INSPECTION THE STARTER/GEN WAS REMOVED AND THE BRUSHES INSPECTED TO BE WORN OVER HALF LIFE. STARTER/GEN HAD ONLY 2.7 HRS SINCE OVERHAUL. STARTER/GEN SENT FOR WARRANTY AND TESDR CA060719003Potentiometer · separated(CAN) VISUAL INSPECTION CARRIED OUT ON ELEVATOR FDR SYSTEM DUE TO A FAILURE OF THE FDR CORRELATION FLIGHT TEST. FLIGHT TEST RECORDER SHOWED ELAVATOR SYSTEM NO RESPONSE TO SIGNAL. VISUAL INSPECTION REVEALED FAILED POTENTIOMETER SHAFT. REPLACED WITH NEW PART IAWSDR 072006N332CS1Fuel Control · malfunctionedWHILE PERFORMING ENGINE ACCELERATION TEST , ENGINE FAILED TO RESPOND TO THROTTLE MOVEMENT AND HUNG AT 56.4 PERCENT N1.CREW DECLARED AN EMERGENCY AND DIVERTED BACK TO TOL. AIRCRAFT LANDED UNEVENTFULLY. FUEL CONTROL WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR CA060712006Wheel · corroded(CAN) AFTER ONLY ONE TIRE CHANGE AND 9 MONTHS IN SERVICE THE NOSE WHEEL WAS REMOVED AND FOUND EXCESSIVE CORROSION THE BOLT HOLES AND SURFACE CORROSION ON THE INNER WHEEL HALVES. (TC NR20060712006)SDR CA060731008Fuel Control · unserviceable(CAN) THE ENGINE WAS REPORTED TO FLAME OUT ON APPROACH. THE FUEL CONTROL UNIT WAS SUBSEQUENTLY REPLACED. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20060731008)SDR 70506N304CS1Fuel Control · failedRT ENGINE EXPERIENCED UNCOMMANDED SHUTDOWN WHILE TURNING BASE, AFTER A STEEP IDLE DESCENT WITH ENGINE ANTI-ICE ON. AC WAS STABILIZED AND IN GOOD POSITION TO LAND SO CREW CONTINUED APPROACH, DECLARED AN EMERGENCY AND LANDED AC WITHOUT INCIDENT. FIELD SERVICE SDR CA060629003Flange · debonded(CAN) WELDED TUBE ASSEMBLY REMOVED FROM AIRCRAFT TO GAIN ACCESS FOR INSPECTION. WELDED TUBE ASSEMBLY INSPECTED - FLANGE ATTACHED APPEARED TO BE BONDED TO TUBE. UPON INSTALLATION ON AIRCRAFT - WHEN CLAMP ATTACHING WELDED TUBE ASSEMBLY TO CABIN VENTILATION JUNSDR 2006FA0000680Seat Frame · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. CHAIR WAS REPAIRED IAW STRUCTURAL SEAT REPAIR. (K)SDR STARTRELAYRelay · stickingAFTER STARTING RT ENGINE THE START BUTTON LIGHT COULD NOT BE EXTINGUISHED. AFTER SHUTDOWN THE RT ENGINE REMAINED SPOOLING AS THE STARTER WAS STILL ENGAGED AND THE BATTERY HAD TO BE DISCONNECTED TO TERMINATE THE STARTER. THE RT START RELAY WAS REPLACED AND OPSDR CA060608010Channel · brokenPILOTS REPORTED THAT WHEN THE RUDDER PEDALS ARE BOTH PUSHED, THE CO-PILOT'S INSTRUMENT LIGHTS DIM. INVESTIGATION REVEALED THAT THE PILOT'S RUDDER SUPPORT BRACKET WAS BROKEN AT THE TOP OF THE ATTACH CHANNEL. THE CO-PILOTS INSTRUMENT LIGHT RHEOSTAT WAS ALSO DASDR CA060529010Servo · malfunctionedDURING LANDING, ANTI-SKID INOP ANNUNCIATOR ILLUMINATE THEN EXTINGUISH. ROLLOUT WAS UNEVENTFUL AND DUE LONG RUNWAY, NO BRAKE APPLICATION AT ALL BUT AT END OF RUNWAY RT TURN TO TAXIWAY, BRAKES WERE NON-RESPONSIVE BUT PEDALS WERE EXTREMELY HARD. MX FOUND PRESS SSDR 2006FA0000537Channel · damagedTHE STRIKER PLATE HAD COME LOSE AT THE TOP LATCH POINT FOR THE ESCAPE HATCH ALLOWING THE LOCK PIN TO ELONGATE OUT THE HOLE. THIS REQUIRED THE REPLACEMENT OF 5511162-12 CHANNEL AND 5511162-48 ZEE CHANNEL.SDR 2006FA0000526Aileron · crackedDURING A PHASE 1,2,3,4 INSPECTION THE RT AILERON WAS FOUND TO BE CRACKED AT THE LEADING EDGE IN THE AREA OF ATTACHMENT POINTS FOR THE WEIGHTS. THE SKIN WAS REMOVED AND REPLACED. HAD SEVERAL CRACKED AILERONS IN OUR OTHER AIRCRAFT BOTH LT AND RT CRACK IN THIS ARSDR 2006FA0000525Elevator · maint errorAFTER A REPAIR AT ANOTHER FACILITY THIS ELEVATOR WAS IN A BIND AND NOT ABLE TO STREAMILINE WITH THE STABILIZER (COULD NOT RIG). IT APPEARS THAT THIS CONTROL WAS NOT INSTALLED CORRECTLY IN A JIG FIXTURE. WHILE REPLACING THE UPPER AND LOWER SKINS IT WAS ALSO FOUSDR 2006FA0000523Skin · corrodedAFTER A PHASE 1,2,3,4,49&59 CORROSION AND DELAMINATION WAS FOUND ON TOP AND BOTTOM SKINS LT AND RT SIDES OF THE HORIZONTAL STABILIZER, LT SKIN OF THE VERTICAL STABILIZER. TAIL SKINS 5512010-9 AND 6512010-20 (SKINS UNDER VERT. STAB.) AS WELL AS THE AFT BULKHEADSDR 51406N339CS1Warning Light · defectiveON APPROACH, CREW REPORTED NO RT MLG GEAR DOWN AND LOCK INDICATION. THERE WAS NO HYDRAULIC PRESSURE ON LIGHT AND NO GEAR UNSAFE LIGHT. PERFORMED ROTARY TEST FOR GEAR LIGHT TEST WITH SAME RESULTS. DIVERTED DESTINATION FROM CRG TO MCO. PRIOR TO LANDING, EXECSDR 314901Wheel · crackedFINDING FATIGUE CRACKS FORMING AT THE INTERSECTION OF THREADED HOLE AND DRILLED PASSAGE OF FUSE PLUG HOLE AND VALVE STEM HOLE.SDR CA060425020Hmu · malfunctionedON TAKEOFF ROLL, ENGINE POWER ROLLED BACK MARGINALLY AND WAS CORRECTED BY A THROTTLE ADJUSTMENT. POWER FLUCTUATIONS WERE REPORTED DURING CLIMB. IN CRUISE, POWER ROLLED BACK UNCOMMANDED AND THE ENGINE WAS FOUND NOT TO RESPOND TO THROTTLE INPUT. THE AIRCRAFT SDR B3OR20060111Terminal · misinstalledWIRE TERMINAL WAS IMPROPERLY CRIMPED ONTO WIRE INSULATION WITH STRIPPED END OF WIRE STRANDS CONTACTING TERMINAL SCREW AT VOLTAGE METER CIRCUIT BREAKER. THIS DISCREPANCY CAUSED AN INTERMITTENT VOLTAGE METER READING FAILURE.SDR 41506N304CS1Bulb · burned outDURING APPROACH THE LANDING GEAR WAS EXTENDED AND THERE WAS NO NOSE AND RIGHT MAIN DOWN AND LOCKED INDICATIONS. HYDRAULIC POWER LIGHT AND UNSAFE LIGHT WENT OUT, PILOT FOLLOWED CHECKLIST PROCEDURES WHICH REQUIRE EMERGENCY GEAR BLOWDOWN TO CONFIRM DOWN CONDITIOSDR CA060224011Battery Pack · corrodedDURING A PHASE INSPECTION, EMERGENCY LIGHT OPERATIONAL CHECK, THE LIGHTS FAILED TO TURN ON. FURTHER INVESTIGATION REVEALED THAT THE EMERGENCY LIGHT POWER SUPPLY WAS DAMAGED. ALL BATTERIES CELLS WERE CORRODED AND THE BATTERY BOX MELTED. THE BATTERY PACK 2 AMSDR CA060227022Engine · failedTHE ENGINE EXPERIENCED AN UNCOMMANDED IN-FLIGHT SHUT DOWN AFTER TAKEOFF. SUBSEQUENT INSPECTION REVEALED DEBRIS IN THE ENGINE EXHAUST. P&WC WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE DETERMINED.SDR CA060227017Fuel Control · malfunctionedDURING DESCENT, THE ENGINE WAS FOUND TO NOT RESPOND TO THROTTLE LEVER INPUT AND WAS SHUT DOWN IN FLIGHT. THE ENGINE FUEL CONTROL UNIT AND FLOW DIVIDER VALVE WERE SUBSEQUENTLY REPLACED.SDR CA060227020Engine · power lossON DESCENT, THE ENGINE WAS REPORTED TO EMIT A GRINDING NOISE ACCOMPANIED BY AN UNCOMMANDED POWER LOSS. THE ENGINE WAS SHUT DOWN IN FLIGHT AND A SINGLE-ENGINE LANDING ACCOMPLISHED AT POINT OF DESTINATION. GROUND INSPECTION REVEALED INTERNAL ENGINE DAMAGE. P&SDR CA060214001Tube · melted(CAN) DURING UNSCHEDULED MAINT FOR AN UNRELATED MAINTENANCE ISSUE, THE POLYFLOW LINE PROVIDING ATMOSPHERIC REFERENCE PRESSURE TO THE RT OUTFLOW VALVE WAS FOUND MELTED AND OPEN TO CABIN PRESSURE. THE POLYFLOW LINE WAS TOO LONG AND WAS POSITIONED IN SUCH A WAY ASDR CA060227014Engine · flamed outTHE ENGINE FLAMED OUT DURING TAXI. SUBSEQUENT INVESTIGATION COULD NOT DUPLICATE THE PROBLEM. THE ENGINE FUEL FILTER WAS REPLACED, THE AIRFRAME RIGGING CHECKED AND THE AIRCRAFT RETURNED TO SERVICE.SDR 2006FA0000138Motor · failedTHE FLAP MOTOR EXPERIENCED AN OUT OF BOX FAILURE IMMEDIATELY AFTER INSTALL. THE MOTOR`S INTERNAL BRAKE MECHANISM MALFUNCTIONED IN A WAY TO NOT ALLOW IT TO RELEASE. THE PART WAS IN NO WAY AIRWORTHY AND MALFUNCTION SHOULD HAVE BEEN NOTICED AT THE REPAIR STATIOSDR 2006F00007Tach Generator · failedDURING CRUISE FLIGHT THE LT ENGINE N1(FAN) INDICATOR WENT TO ZERO, ALL OTHER ENGINE INDICATIONS WERE NORMAL. INVESTIGATION REVEALED THAT THE N1 TACH GENERATOR DRIVE SHAFT HAD SHEARED. REPLACED WITH OVERHAULED UNIT AND OPERATIONALLY CHECKED OK. CAUSE WAS EVIDENSDR CA060209001Hose · burst(CAN) LANDING THE CREW DEPLOYED THE THRUST REVERSERS AND GOT 6 LIGHTS FOLLOWED BY (HYD LOW LEVEL) AND (HYD LOW FLOW) LIGHTS. MAINTENANCE FOUND ONE LINE P/N CM3574D460B000S ON THE LT SIDE HAD BURST. REPLACED LINE WITH NEW. INSPECTED BOTH PRESSURE FILTERS AND NOSDR CA060129009Fuel Control · faulty(CAN) ON APPROACH, THE ENGINE DID NOT RESPOND TO THROTTLE INPUT. AN EMERGENCY WAS DECLARED AND A LANDING ACCOMPLISHED WITH THE THROTTLE IN THE IDLE DETENT. SUBSEQUENT INSPECTION REVEALED A FAULTY FUEL CONTROL UNIT. MFG WILL INVESTIGATE THE EVENT AND ADVISE SDR ZES2006F00000Fcu · unserviceableAFTER DECENDING FROM ALTITUDE, LT ENGINE WOULD NOT ACCELERATE AND REMAINED AT IDLE. PILOTS LANDED THE AIRCRAFT WITHOUT INCIDENT. REMOVED AND REPLACED THE FUEL CONTROL UNIT. OPS CHECKED, OK. (EA03200603629) (K)SDR 122105N317CS1Reservoir · unknownAFTER T/O ATTEMPTED TO RETRACT MLG, HEARD A LOUD NOISE & HAD CAUTION LIGHTS ILLUMINATE. GEAR UNSAFE, HYD PRESSURE , & LOW FLUID LIGHTS CAME ON. SELECTED GEAR DOWN & PULLED EMERGENCY BLOWDOWN HANDLE. GEAR WENT INTO DOWN & LOCKED POSITION & GEAR INDICATORS NOSDR CA051220001Seal · leakingON LANDING, OBSERVED NO BRAKING ACTION EVEN THOUGH BRAKE PEDALS HARD. EMERG BRAKING UTILIZED & A/C CLEAR OF RUNWAY, NORMAL BRAKING ACTION RETURNED. NO FAULT LIGHTS INDICATING ANTI-SKID FAILURE. MX NOTICED UPON REMOVING LT WHEEL BEARING CAP, ANTI-SKID DRIVSDR DJFA2005178Brake Assy · failedTHE CREW REPORTED THAT WHILE THEY WERE ON A VISUAL APPROACH THE ANTI-SKID AND POWER BRAKE PRESSURE LOW LIGHTS ILLUMINATED. THE ANTI-SKID CIRCUIT BREAKER WAS RECYCLED AND THE CREW WERE PREPARING TO USE THE EMERGENCY BRAKING SYSTEM, BUT LATER FOUND THAT THE BRASDR 121405N332CS1Downlock Switch · shortedON FINAL, MLG WOULDN`T EXTEND NORMAL. ONLY NLG EXTENDED AND C/B WOULD POP. NLG RETRACTED & A/C DIVERTED. ON APPROACH, MLG LEVER SELECTED DOWN & NLG EXTENDED AND C/B AGAIN POPPED. PULLED EMERG EXTEND HANDLE, DISCOVERED HANDLE WOULD NOT COME OUT & MLG STILL SDR L3WSAControl Cable · frayedWE HAVE FOUND THE ELEVATOR AUTOPILOT SERVO LT CABLE WITH BROKEN STRANDS ON 3 SUCCESSIVE AIRCRAFT THAT WERE UNDERGOING A PHASE 5 INSPECTION. ON CABLE HAD 50 PERCENT FRAYING. THE FRAYING WAS FOUND WHERE THE CABLE PASSES THROUGH A DOUBLE CABLE JOGGLE AT FUSELAGE
Back to Cessna 550