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 99ZZZX1135Valve · malfunctionedNEW FLAPPER TYPE CHECK VALVE WAS INSTALLED AND AIRCRAFT WAS PRESSURIZED WITH TEST UNIT. EXCESSIVE CABIN LEAK RATE WAS TRACED TO FAILED CHECK VALVE. THE RUBBER LINER STARTED COMING LOOSE FROM THE FLAPPER PART OF THE VALVE AND FOLDED PREVENTING IT FROM CLOSINGSDR 99ZZZX873Igniter · damagedIGNITERS WERE REMOVED FOR INSPECTION AND CENTER ELECTRODE APPEARED TO BE MISSING ON ONE OF THE IGNITERS. FURTHER INVESTIGATION SHOWED THAT WHEN LEAD WAS REMOVED FROM IGNITER, THE CENTER ELECTRODE WAS LOOSE INSIDE THE IGNITER AND PULLED PARTIALLY OUT CAUSING TSDR 99ZZZX548Indicator · malfunctionedDURING SLOW RATE OF TURNS, THE ATTITUDE FLAG APPEARS AND ADI SPHERE STUCK. ADI STUCK SEVERAL TIMES ON BOTH LEFT AND RIGHT BANKS AND ATTITUDE FLAG COMES IN VIEW.SDR 99ZZZX1056Valve · leakingON TAKEOFF, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT LANDED UNEVENTFULLY. TROUBLESHOOTING REVEALED VALVE ON EMERGENCY PNEUMATIC RESERVOIR (BLOW DOWN BOTTLE) LEAKED, PRESSURIZING DOWN SIDE OF LANDING GEAR RETRACTION SYSTEM. ASSEMBLY WAS REMOVED AND SHIPPED OSDR CA990111034Tube · chafed(CAN) ON DESCENT, THE LEFT ENGINE ANTI-ICE ANNUNCIATION WOULD NOT EXTINGUISH WITHIN 2 MINUTES AFTER SELECTED PER OPERATING MANUAL. TWO CONTACTS OF TEMP LO SWITCH P/N S105 WHICH ARE ON INSIDE OF THE LEFT HEATED LEADING EDGE WERE FOUND SHORTING ACROSS AN ALUMINUSDR CA981230028Sprocket · sheared(CAN) GEARBOX OUTPUT SPROCKET SHEARED WHEN ISOLATED FROM SECOND GEARBOX AND COMMANDED FLAPS TO MOVE. PART TC: 653.SDR 99ZZZX360Spring · brokePILOT REPORTED HE HEARD A 'POP' DURING ENGINE SHUT DOWN AND LEFT THROTTLE TRIGGER LOST TENSION. FOUND SPRING BROKEN AND REPLACED UNIT. FAILURE OF THIS SPRING COULD ALLOW THROTTLE TO MAKE A 'CUT-OFF' INADVERTENTLY INSTEAD AT IDLE.SDR 99ZZZX263Valve · malfunctionedDURING FLIGHT, THE RT HAND ANTI-ICE APPEARED TO WORK NORMALLY FOR 6 MINUTES, LIGHT FLICKERED FOR 3 MINUTES, THEN REMAINED STEADY. AMMETER FOR BOTH LT AND RT GENERATORS MATCHED. LIGHT FLICKERED AT LOW AMPERAGE. TROUBLESHOOTING OF ANTI-ICE SYSTEM REVEALED STASDR 99ZZZX136Line · chafedREF CESSNA IPC 28-20-01 FIG 1 ITEM NR 1. DURING RECENT PHASE 5J AND 5K INSPECTIONS, PRESSURE LINE TO EJECTOR TRANSFER PUMP (ITEM NR 40) WAS FOUND CHAFING AGAINST THE WIGGINS COUPLING (ITEM NR 6) ON THE T-CONNECTION BETWEEN MANUAL SHUT OFF (ITEM NR 1) AND FUELSDR 98ZZZX4720Valve · failedAIRCRAFT UNDERGOING IN-FLIGHT PRESS TEST AND IT FAILED CABIN LEAKAGE RATE CHECK WHEN PRESSURE SOURCES WERE SHUT OFF. WHEN PRESSURIZED ON THE GROUND, AIR FLOW WAS HEARD INTO THE CABIN ACM. DUCT FROM ACM TO REAR PRESS BULKHEAD REMOVED AND FLAPPER TYPE CHECK VASDR CA981028008Motor · failed(CAN) ON APPROACH, PILOT FAILED TO GET POWER BRAKE PRESSURE AND ANTI-SKID BREAKER TRIPPED. FURTHER INVESTIGATION FOUND A NEW POWER BRAKE MOTOR HAD FAILED.SDR 98ZZZX4044Transducer · inoperableANTI-SKID SYSTEM INOPERABLE WHICH ALLOWED THE LT WHEEL TO LOCK-UP ON LANDING. AIRCRAFT SKIDDED THROUGH THE TIRE WHICH WENT FLAT. TROUBLESHOOTING REVEALED LT WHEEL SPEED TRANSDUCER INOPERABLE. REPLACING TRANSDUCER CORRECTED THE PROBLEM AT WHEEL SKID.SDR AU981346Bracket · misinstalled(AUS) RIGHT AILERON HINGE BRACKET INCORRECTLY RE-FITTED FOLLOWING REPAIR. PART TC: 9,832.SDR AU981345Bracket · misinstalled(AUS) LEFT AILERON HINGE BRACKET INCORRECTLY RE-FITTED FOLLOWING REPAIR. PART TC: 9,382.SDR 98ZZZX4059Channel · chafedDURING PHASE INSP, A CHAFED SPOT WAS NOTICED ON THE INBD UPPER ACCESS DOOR ON ENGINE COWL. INVEST REVEALED IT HAD BEEN IN CONTACT WITH ENG MOUNT CHANNEL ON THE FWD SIDE. FOUND DAMAGE TO BOTH SIDES WHICH NECESSITATED REPLACING BOTH FWD CHANNELS. UPON INSP OFSDR 98ZZZX4058Channel · chafedDURING PHASE INSP, A CHAFED SPOT WAS NOTICED ON THE INBD UPPER ACCESS DOOR ON ENGINE COWL. INVEST REVEALED IT HAD BEEN IN CONTACT WITH ENG MOUNT CHANNEL ON THE FWD SIDE. FOUND DAMAGE TO BOTH SIDES WHICH NECESSITATED REPLACING BOTH FWD CHANNELS. UPON INSP OFSDR AU981386Rod · broke(AUS) RIGHT FLAP INBOARD ACTUATING ROD FORWARD ROD END BROKEN THROUGH THE THREADED SECTION IN THE AREA OF THE LOCKNUT. SUBMITTER SUSPECTED CAUSE AS OVERTORQUING OF THE LOCK NUT WITH THE FLAPS BEING OUT OF ADJUSTMENT AS A CONTRIBUTING FACTOR.SDR AU981309Rod · broke(AUS) RIGHT FLAP INBOARD ACTUATING ROD FORWARD ROD END BROKEN THROUGH THREADED SECTION IN AREA OF LOCKNUT. SUBMITTER SUSPECTED CAUSED BY OVERTORQUE OF THE LOCKNUT AND/OR FLAPS SLIGHTLY OUT OF RIG.SDR 98ZZZX4547Seal · failedAIRACRAFT LOST PRESSURIZATION DURING CRUISE AT FL 37 DUE TO A COLLAPSED CABIN DOOR SEAL. FLIGHT CREW EXECUTED THE EMERGENCY DESCENT AT THE NEAREST AIRPORT - EL PASO, TEXASSDR CA980930020Cables · crossed(CAN) ON TEST FLIGHT AFTER PHASE V INSPECTION, PILOT NOTICED THAT NOSE DOWN TRIM CORRECTION RESULTED IN NOSE PITCHING UP. INSPECTION FOUND CROSSED ELEVATOR TRIM CABLES.SDR 98ZZZX3696Tire · out of balanceTHE INTERNAL BALANCE WEIGHT/PATCH BECAME LOOSE FROM THE NOSE TIRE CAUSING AN UNBALANCED CONDITION OF THE TIRE/WHEEL ASSEMBLY.SDR 98ZZZX4193Engine · malfunctionedPILOT REPORTED HOT OIL SMELL COMING FROM OVERHEAD VENTS DURING POSITIONING FLIGHT FOR MAINTENANCE. TROUBLESHOOTING SHOWED SMELL COMING FROM RIGHT ENGINE.SDR CA981014013Brake · overheated(CAN) FOLLOWING A REJECTED TAKEOFF, THE PILOT THOUGHT HIS TIRES WERE FLAT. IT WAS CONFIRMED THAT BOTH SIDES WERE FLAT AND THE BRAKES WERE BURNING. FIRE EXTINGUISHED. INSPECTION FOUND BOTH BRAKES AND WHEEL ASSEMBLIES WERE OVERHEATED CAUSING THE TIRES TO DEFLSDR CA980909002Light · inoperative(CAN) NAVIGATION LIGHT CIRCUIT BREAKER TRIPPED IN-FLIGHT. FOUND TAIL POSITION LIGHT ASSY GROUNDED INTERNALLY. CONTACTS MELTED AND BULB SOLDER PLUG MELTED CAUSING A SHORT.SDR 98ZZZX3439Line · chafedDURING PHASE 5K INPSECTION OF FUEL SYSTEM IN RT WING ROOT, A .023 INCH CHAFE WAS FOUND ON THE PRESS LINE TO THE EJECTOR TRANSFER PUMP. REF: CESSNA IPC 28-20-01 FIG 01 SHET 01 ITEM 40. CHAFED LINE (ITEM 40) IS LOCATED IN THE 'Y' (ITEM 28) OFF THE MAIN FUEL SDR 99ZZZX51Gearbox · failedRIGHT ENGINE SHUT DOWN IN CRUISE FLIGHT AT 24,000 FEET. PRECAUTIONARY LANDING. POSSIBLE ENGINE GEARBOX PROBLEM STILL UNDER INVESTIGATION. FAILURE OF LOCK WASHER ON UPPER TOWER SHAFT DUPLEX BEARING. OVERHAUL OCCURRED 2,236 HOURS AGO.SDR 98ZZZX3220Control Box · failedRECEIVED AN 'EXHANGE' ANTI-SKID CONTROL BOX FROM SERVICE CENTER. UPON INITIAL INSTALLATION INTO THE AIRCRAFT WHEN THE ANTI-SKID SWITCH WAS SELECTED 'ON', THE ANTI-SKID FAIL 'AMBER' LIGHT REMAINED ILLUMINATED. INVESTIGATED PROBLEM AND DETERMINED THE 'EXCHANGESDR 98ZZZX3230Indicator · shortedPIN APEARS TO BE GROUNDED TO CHASSIS. UNIT OPERATES ON BENCH, BUT WHEN INSTALLED INSTRUMENT PANEL, IT TRIPS THE CIRCUIT BREAKER.SDR 98ZZZX3221Inverter · burnedAT FL 31, SMOKE REPORTED IN CABIN. EMERGENCY LANDING REQUEST MADE. AIRCRAFT LANDED UNEVENTFULLY, AIRCRAFT INSPECTED FOR FERRY FLIGHT TO SWF WITH INDIRECT LIGHTING POWER INVERTERS DISABLED. INSPECTION REVEALED BURNED INVERTER, NO INDICATION OF CAUSE. SUSPECSDR 98ZZZX3325Wheel · out of balanceAIRCRAFT EXPERIENCED VIBRATION ON ROTATION. AIRCRAFT RETURNED TO BASE AND FOUND LOOSE BALANCE PATCH IN NOSE TIRE. SEE PAGE 4 OF AUGUST '98 ALERTS FOR SIMILAR INCIDENTS.SDR CA980721018Motor · overheated(CAN) DURING TAXI AFTER LANDING, THERE WAS A RAPID ACCUMULATION OF SMOKE IN THE COCKPIT. BLOWER MOTOR WINDINGS HAD OVERHEATED.SDR CA980720016Solenoid · sticking(CAN) AFTER LANDING AND RT THRUST REVERSER FULLY DEPLOYED, THE PILOT COULD NOT INCREASE POWER FOR REVERSE USING THE TR CONTROL LEVER. THE DEPLOY INTERLOCK SOLENOID PLUNGER REMAINED IN THE LOCK-OUT POSITION, PREVENTING LEVER FROM MOVING TO THE POWER UP POSITIOSDR CA980629012Switch · failed(CAN) ON DESCENT, WHEN THE ENGINES WERE THROTTLED BACK, THE 'FUEL PRESS LOW RT' AND THE 'BOOST PUMP ON RT' ILLUMINATED. CREW SELECTED THE RIGHT BOOST SWITCH FROM 'NORM' TO 'ON' AND LANDED WITHOUT INCIDENT. ENGINE PARAMETERS OK. AFTER LANDING , THE BOOST PUMPSDR CA980706033Switch · failed(CAN) IN DESCENT THROUGH APPROX FL 320, CABIN ALTITUDE CLIMBED UP TO 6,000 FPM THEN REDUCED. CABIN ALTITUDE HELD AT 13,000 FEET DESCENDING THROUGH 13,000 FEET, CABIN DESCENDED AT SAME RATE AS AIRCRAFT. AFTER LANDING, AIRCRAFT WAS INSPECTED AND FOUND THAT THESDR CA980622007Disk · broken(CAN) BOTH SETS OF BRAKE ROTATOR DISC ASSEMBLIES FOUND BROKEN. BOTH WERE IN VERY POOR SHAPE WITH SEVERE WEAR.SDR AU980639Tire · failed(AUS) NOSE WHEEL TIRE BLEW OUT WHILE BEING INFLATED TO APPROXIMATELY 60 PSI.SDR CA980615003Control Cable · kinked(CAN) AFTER AIRCRAFT HAD BEEN PARKED OUTSIDE ON RAMP FOR AFTERNOON WITH CONTROL LOCKS ON, CONTROL LOCKS COULD NOT BE SELECTED OFF. IT WAS DISCOVERED THAT THE INNER CABLE HAD BULGED OUT OF ITS CASING AND JAMMED. PART TC: 3,035.SDR CA980610018Controller · failed(CAN) ON TAKEOFF, CABIN RATE NEEDLE STAYED AT ZERO AND CABIN ALTITUDE STAYED AT GROUND LEVEL. DIFFERENTIAL INCREASED AT FL 220 AND DIFFERENTIAL REACHED 8.5 CABIN ALTITUDE BEGAN INCREASING TO 6,000 WHEN AIRCRAFT REACHED FL 370, STARTED DESCENT AT 1,000 FPM. CASDR CA980603002Hinge · cracked(CAN) CABIN DOOR WOULD NOT CLOSE. INSPECTION REVEALED A CRACK DUE TO CORROSION ON THE UPPER ATTACHMENT LUG ARM. SUBMITTER SUSPECTS DISSIMILAR METAL CORROSION DUE TO PREVIOUS REPLACMENT OF WRONG TYPE OF RIVETS.SDR CA980525001Oleo · failed(CAN) RIGHT HAND OLEO ASSY COLLAPSED WHILE AIRCRAFT WAS IN THE HANGAR FOR MAINTENANCE. PART TC: 562.SDR 98ZZZX2192Hose · leakingPILOT REPORTED HYDRAULIC LOW LEVEL LIGHT CAME ON IN-FLIGHT. AIRPLANE MADE LANDING AT NEAREST AIRPORT. LANDING GEAR EXTENSION WAS NORMAL, SPEED BRAKES AND THRUST REVERSERS DEPLOYED NORMALLY. UPON REMOVING COWLING, THE LEFT HYDRAULIC PRESSURE HOSE WAS FOUND SDR 98ZZZX2545Wire · detachedDURING A FAR 135 FLIGHT, THE FLAPS WERE SELECTED UP AFTER TAKEOFF AND WOULD NOT RETRACT ALL THE WAY UP. STEP 2 ABNORMAL CHECK LIST WAS PERFORMED (FLAPS INOPERATIVE). PARTIAL FLAP LANDING WAS PERFORMED. INVESTIGATION REVEALED THE WIRE FROM THE FLAP RELAY K44SDR 98ZZZX1543Hinge Assy · corrodedCABIN DOOR REMOVED TO CHANGE BEARING ASSYS IN DOOR HINGE AND CORROSION DAMAGE WAS DISCOVERED IN HINGE. THIS IS MADE OF MAGNESIUM AND THE CORROSION DAMAGE WOULD NOT BE REMOVED WITHOUT COMPROMISING THE HINGE INTEGRITY. REASON FOR CORROSION WAS LACK OF LUBRICATISDR 98ZZZX1692Stud · failedIN PERFORMING 10,000-HOUR MLG INSPECTION AND UPON INSTALLING NUT ON STUD, STUD SHEERED IN HALF AT BASE OF THREADED AREA ALLOWING ACTUATOR TO SEPARATE FROM LANDING GEAR. AIRCRAFT WAS ON JACKS. UPON INSPECTION OF STUD, DETERMINED IT WAS CRACKED AND CORRODED.SDR CA980421001Switch · intermittent(CAN) WHEN GEAR SELECTED DOWN NO GREEN LIGHT FOR NOSE GEAR DOWNLOCK. ALSO, THERE WAS NO RED UNSAFE LIGHT OR ANY HYD ON ANNUNCIATOR LIGHT. GEAR RECYCLED, STILL THE SAME AND BULBS OK. GEAR BLOWN DOWN. AIRCRAFT LANDED OK. FOUR HOURS LATER THE GREEN LIGHT WASSDR CA980407023Stator · cracked(CAN) AIRCRAFT LANDED NORMALLY BUT WHILE TURNING AROUND AFTER TAXIING, THE LT WHEEL LOCKED UP. BRAKING WAS NORMAL DURING LANDING. WHEN MAINTEANCE REMOVED BRAKE, THE DISK-STATOR (P/N 133-893-2) WAS FOUND CRACKED IN THE AREA OF A KEY SLOT IN THE STATOR. BOTH SDR CA980225014Blower · failed(CAN) ON DESCENT, THE PILOT'S NOTED A FAINT BURNING ODOR AND GETTING STRONGER. OXYGEN MASKS AND SMOKE GOGGLES PUT ON. SMOKE THEN APPARENT AND AN EMERGENCY DESCENT LANDING CARRIED OUT. THE DEFOG FAN FOUND SEIZED AND THE 20-AMP CIRCUIT BREAKER HAD NOT TRIPPED.SDR 98ZZZX849Fuel System · leakDURING RELEASING AIRCRAFT FOR WORK ALREADY DONE, NOTED EXCESSIVE FUEL LEAKING (CLASS D, TYPE 4) UNDER LEFT WING, INBOARD OF WHEEL AND BEHIND LEFT WING HEATED LEADING EDGE. ALSO, NOTED THE NOSE TIRE WAS CUT TO THE CORD AND REPLACEMENT IS REQUIRED. CUSTOMER WASDR 98ZZZX1095Valve · failedRECEIVED RECENTLY OVERHAULED VALVE FROM SUPPLY. INSTALLED VALVE, VALVE WOULD NOT PASS OPERATIONAL TEST IN AIRCRAFT. FOUND VALVE TO BE FAULTY. (INTERNALLY BYPASSING PNEUMATIC PRESSURE). PART WAS OVERHAULED 5-23-97 BY ALLIED SIGNAL AEROSPACE EQUIPMENT SYSTEMSDR 98ZZZX614Relay · intermittentUPON REMOVAL OF THIS RELAY FOR REPLACEMENT, LOOSE HARDWARE WAS HEARD RATTLING AROUND INSIDE. SUBMITTER STATED THIS IS A CONTINUING PROBLEM WITH THIS TYPE AND PART NUMBER RELAY AND HAS BEEN FOUND ON SEVERAL OTHER OCCASIONS. THE RELAY WOULD NOT HAVE FAILED HAD
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