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 96ZZZX149Wheel · brokenELEVATOR TRIM WHEEL 'GROOVES' FOR TRIM INDICATOR ARE BROKEN. SUBMITTER STATED THIS IS DANGEROUS AS IT GIVES A 'FALSE' TRIM READING. PART SHOULD BE MADE FROM ALUMINUM.SDR CA951228006Lockout Cable · broken rod end(CAN)DUE TO THE SEPARATION OF THE THROTTLE LOCKOUT CABLE ROD END, THE ENGINES CAN BE STARTED AND OPERATED THROUGHOUT THEIR FULL RANGE WHILE THE FLIGHT CONTROLS WERE IN THE LOCKED POSITION.SDR 96ZZZX6073Seal · failed22.5 HOURS AFTER INSTALLATION OF OVERHAULED ENGINE, OIL PRESSURE LIGHT ILLUMINATED ON MASTER CAUTION PANEL AND OIL PRESSURE INDICATED 35 PSI. ENGINE WAS SHUT DOWN AND A PRECAUTIONARY LANDING WAS MADE AT NEAREST AIRPORT. DURING TROUBLESHOOTING, OIL LEAK WAS FSDR 96ZZZX202Fork · crackedPERFORMED UNSCHEDULED LIQUID DYE PENETRANT EXAMINATION IAW CESSNA NDT MANUAL, PART 7, CHAPTER 32-20-01, NOTED TWO CRACKS IN THE LT AND RT CORNER RADII OF THE NLG FORK. BOTH CRACKS EXCEED LIMITS IAW CESSNA CMM MANUAL, CHAPTER 32-20-00. INITIAL INSPECTION OF TSDR 96ZZZX576Brake Assy · rotor crackedBRAKES REPLACED DUE TO WEAR INDICATOR 'BRAKES WORN TO LIMITS'. UPON DISASSEMBLY, FOUND ONE ROTOR CRACKED THROUGH ENTIRE LENGTH. FOUND TWO ROTORS WITH SAME DEFECT ON RIGHT BRAKE ASSEMBLY. THESE BRAKE ASSEMBLIES HAVE 502.3 HOURS SINCE OVERHAUL AND 480 LANDINGSDR 96ZZZX271Gear · teeth shearedPILOT INDICATED THE FLAPS WOULD NOT FULLY EXTEND AT THE UPPER AIRSPEED LIMITS. INSPECTION REVEALED THE LEFT FLAP GEARBOX WAS BAD. GEARBOX WAS DISASSEMBLED AND IT WAS FOUND TO HAVE SHEARED GEAR TEETH. INSTALLED EXCHANGE GEARBOX.SDR CA951122027Wire · damaged(CAN)WHILE TROUBLESHOOTING SNAG, TECHNICIAN FOUND WIRE GOING AROUND L/H THRUST REVERSER SWITCH WAS BEING DAMAGED BY A COTTER PIN. WIRE REPAIRED.SDR CA951122026Switch · broken wire(CAN)WHILE CONDUCTING GROUND TEST, L/H THRUST REVERSER DID NOT DEPLOY. TECHNICIAN FOUND WIRE #K106C20 BROKEN AT THE MICROSWITCH P/N V3 15.SDR CA951120008Switch · broken wiring(CAN)AFTER LANDING,THRUST REV LIGHTS SHOWED NORMAL DEPLOYMENT,BUT AFTER SELECTING STOW,THEY REMAINED DEPLOYED & THE UNLOCK LIGHTS REMAINED ON.SELECTING THE EMERGENCY STOW SWITCH STOWED THE THRUST REV. TROUBLESHOOTING, FOUND THAT SWITCHES S153 & S161, IN THE PSDR CA951108022Cable Assembly · worn(CAN)DURING A DAILY INSPECTION, THE R/H AILERON WAS MOVED AT THE WING WHERE A RUBBING SOUND WAS HEARD. UPON INVESTIGATION, IT WAS DISCOVERED SEVERAL CABLE PASS THROUGH HOLES IN THE WING RIB WERE RUBBED BY THE CABLE. VERY LITTLE WEAR COULD BE SEEN ON THE CABLESDR 95ZZZX6192Joint · crackedINSPECTION REVEALED BLEED AIR JOINT WITH A CRACK APPROX 1 INCH BEYOND LIMITS. POSSIBLY CAUSED BY UNINTENTIONAL FORCE APPLIED TO AIR JOINT.SDR 95ZZZX6031Filter Assy · separatedFILTER BOWL AND FILTER SEPARATED FROM FILTER HEAD/ASSEMBLY. THE HEILCOIL IN THE HEAD CASTING PULLED FROM HEAD. FUEL PRESSURE WAS LOST TO THE ASSOCIATED ENGINE. UPON FURTHER INSPECTION, THE OTHER FUEL FILTER ASSEMBLY WAS STARTING TO FAIL IN A SIMILAR WAY. SSDR 95ZZZX6835Access Door · departedLEFT ENGINE OIL ACCESS DOOR (APPROXMATELY 6 INCHES BY 8 INCHES) DEPARTED THE AIRCRAFT STRIKING THE LT HORIZONTAL STABILIZER, CUTTING A SMALL HOLE IN THE DEICE BOOT AND DENTING THE LEADING EDGE SKIN. INSPECTION OF THE HINGE REMAINING ON THE COWLING REVEALED THSDR 95ZZZX6193Line · bogusREMOVED RUBBER HOSE (GARDEN HOSE) FROM THE FUEL VENT LINE AND INSTALLED PROPER PLUMBING PER CITATION PARTS MANUAL.SDR 95ZZZX6027Switch · failedDURING DEFUEL, FOUND ANOTHER BAD LOW LEVEL SWITCH. EITHER THE WARNING LIGHT FAILS TO ILLUMINATE, OR IT STAYS LIT AFTER REFUELING. UPON REMOVAL, SWITCH USUALLY FEELS NORMAL, THAT IS, FREE MOVEMENT. RECORDS SHOWS 8 EACH CHANGED SWITCHES OVER THE PAST 2 YEARS.SDR 95ZZZX6044Regulator · gasket failedAT ALMOST EVERY PHASE INSPECTION, FIND THE 23 PSI PNEU REGULATOR LEAKING BLEED AIR DUE TO BLOWN GASKET. REGULATOR IS LOCATED NEXT TO THE AFT PRESSURE BULKHEAD AND PROVIDES PNEUMATIC PRESSURE FOR DE-ICE BOOTS, INSTRUMENTS, AND PRESSURIZATION CONTROL. ALSO, FOSDR 95ZZZX6030Adaptor · mismanufacturedFOUND FUEL FILTER INLET FITTING O-RING EXTRUDED FROM FITTING. THERE WAS NO EVIDENCE OF FUEL LEAKING. DISCOVERED IMPROPERLY MACHINED LAND ON FITTING WOULD NOT ALLOW SEAL TO PROPERLY MATE WITH SEAL RECESS IN HOUSING. REPLACED FITTINGS WITH NEW PARTS WHICH DIDSDR 95ZZZX4608Altitude Switch · defectiveDURING PHASE 5 INSPECTION, OXYGEN SYSTEM FAILED FUNCTIONAL CHECK. OXYGEN MASK DEPLOYED AT 12,400 FEET WHEN THEY SHOULD DEPLOY AT 13,500 FEET, PLUS OR MINUS 600 FEET. DEFECTIVE BAROMETRIC ALTITUDE SWITCH CAUSED DISCREPANCY. INTERNAL FAILURE OF WEAKNESS OF SWSDR 95ZZZX4604Blade · damagedDURING PHASE 25/HOT SECTON INSPECTION, IMPACT DAMAGE WAS FOUND ON 2ND STAGE LOW TURBINE. THIS WAS CAUSED BY FAILURE OF DEFLECTOR RING. UNIT WAS SENT TO P & WC, DISASSEMBLED, BLENDED AND REASSEMBLED. NO COCKPIT INDICATIONS OF DAMAGE WERE NOTED PRIOR TO HOT SSDR 95ZZZX4603Shroud Segment · gougedDURING PHASE 25/HOT SECTION INSPECTION, ALL HIGH PRESSURE TURBINE SHROUD SEGMENT WIRE FOUND GOUGED. DAMAGE WAS CAUSED BY FAILURE OF DEFLECTOR RING AND RESULTING HIGH TURBINE BLADE DAMAGE. ALL SHROUD SEGMENTS WERE REPLACED.SDR 95ZZZX4602Blade · damagedDURING PHASE 25/HOT SECTION INSPECTION, ALL 71 HIGH TURBINE BLADES WERE FOUND NICKED, DENTED AND BROKEN BY IMPACT DAMAGE FROM DEFLECTOR - RING FAILURE. NUMEROUS BLADES WERE MISSING FORWARD ONE-QUARTER OF OUTBOARD LEADING EDGE. NO COCKPIT INDICATION WAS NOTEDSDR 95ZZZX4601Ring Support · brokenDURING PHASE 25/HOT SECTION INSPECTION, IMPACT DAMAGE WAS NOTED ON THE NR 2 TURBINE BLADES. FURTHER DISASSEMBLY REVEALED 2 SECTIONS OF THE DEFLECTOR RING HAD BROKEN OFF. THESE SECTIONS WERE APPROXIMATELY 1.50 INCHES LONG AND LOCATED AT TEN O'CLOCK AND 1:30 OSDR 95ZZZX4544Outflow Valve · poppet crackedTHIS VALVE WAS WORKING PROPERLY WHEN REMOVED FOR SB 550-21-41. FURTHER INSPECTION FOUND CRACK IN POPPET AREA. IF IT HAD CRACKED MORE, IT IS POSSIBLE THAT THE CABIN WOULD HAVE DEPRESSURIZED. SUBMITTER STATES IF THIS SB APPLIES TO AIRCRAFT, C/W AS SOON AS POSSDR 95ZZZX4465Tube · chafedDURING TROUBLESHOOTING OF FUEL LEVEL LOW LIGHT, LEFT SIDE, FOUND BOOST PUMP WIRE HARNESS HAD CHAFED THROUGH APPROXIMATELY 20-25 PERCENT OF WALL THICKNESS OF ALUMINUM TUBE, PN 6526355-37 (FIG. 01, ITEM 10, CHAPTER 28-20-00 IPB), AND INSULATION OF HARNESS WORN TSDR 95ZZZX5971Brake Assy · defectiveINSTALLED THE BF GOODRICH WHEEL BRAKES ON CESSNA 550 APPROXIMATELY ONE YEAR AGO TO TAKE ADVANTAGE OF THE GUARANTEED PRORATED 1,000 LANDING LIFE OF THIS WHEEL BRAKE ASSYS. THE PROBLEM IS THAT THE WHEEL BRAKES ARE ONLY LASTING APPROX 300-400 LANDINGS BEFORE THESDR 95ZZZX3578Gear · failedDURING FINAL APPROACH, FLAPS WERE SELECTED TO FULL DOWN FROM APPROACH POSITION. PILOT HEARD A LOUD BANG AND AIRCRAFT 'SETTLED'. A GO-AROUND WAS PERFORMED. PILOT NOTICED THE FLAP POSITION INDICATOR SHOWED FLAPS UP WITH SELECTOR IN THE FULL DOWN POSITION. A SDR 95ZZZX3577Gear · failedDURING FINAL APPROACH, FLAPS WERE SELECTED TO FULL DOWN FROM APPROACH POSITION. PILOT HEARD A LOUD BANG AND AIRCRAFT 'SETTLED'. A GO-AROUND WAS PERFORMED. PILOT NOTICED THE FLAP POSITION INDICATOR SHOWED FLAPS UP WITH SELECTOR IN THE FULL DOWN POSITION. A SDR 95ZZZX3305Hinge · crackedWHILE CHECKING A DOOR SEAL PROBLEM, THE PAINT WAS FOUND CRACKED ON THE LOWER CABIN DOOR HINGE LEG. IT WAS FOUND TO BE A CRACK THAT EXTENDS APPROXIMATELY 65 PERCENT IN LENGTH OF LOWER PART LEG. REMOVED AND INSTALLED NEW HINGE ASSEMBLY. THE LOWER LEG RECEIVEDSDR 95ZZZX5362Gear Piston · mismanufacturedDURING ROUTINE INSPECTION OF RT MLG, THE SAFETY WIRE ON THE WHEEL HEAT SHIELD WAS FOUND BROKEN. FURTHER INSPECTION FOUND THE DISTANCE BETWEEN THE WHEEL KEYWAY LINERS AND THE MAIN GEAR SCISSOR LOWER ATTACH POINT WAS VERY CLOSE AND RUBBING ON LANDING AND HIGH SSDR 95ZZZX1721Valve · leakingNOTED HYD FLUID ON HYD PANEL. TROUBLESHOT SYSTEM, FOUND HYD PRESSURE RELIEF VALVE LEAKING AT AREA WHERE THE TWO HALVES OF THE VALVE CONNECT. THERE IS NO PROCEDURE IN THE MM TO RESEAL UNIT. HAD TO REPLACE UNIT WITH EXCHANGE PART.SDR 95ZZZX1720Blower Assy · motor failedPILOT REPORTED NO AIR FLOWING FROM OVERHEAD VENTS. WITH ENGINES RUNNING, LOW AIR FLOW THROUGH VENTS. TROUBLESHOT SYSTEM, FOUND BLOWER MOTOR INOP. REPLACED MOTOR AND VENTS WORE NORMAL. CAUSE OF MOTOR FAILURE UNKNOWN. MOTOR PN ME38A-1.SDR 95ZZZX1175Tire · defectiveWHILE MOVING AIRCRAFT INTO HANGAR, NOSE TIRE MADE ODD NOISE. DISASSEMBLY REVEALED BALANCE PATCH INSIDE TIRE HAD COME LOOSE. PATCH WAS FREE TO CHANGE POSITION. SUBMITTER SUSPECTS POOR QUALITY OF ADHESIVE. MANUFACTURER WAS NOTIFIED OF PROBLEM. LANDINGS, 41.SDR 95ZZZX1136Motor · burnedON CLIMB OUT THROUGH 14,000 FEET, SMELLED SMOKE IN COCKPIT. SMELL IS EVIDENT THROUGHOUT THE CABIN. FOUND ELECTRIC MOTOR ON COCKPIT DEFOG BLOWER HAD BURNED OUT.SDR 95ZZZX1146Oil Pump · failedTHE ENGINE WAS DISASSEMBLED TO DETERMINE THE REASON FOR THE REPORTED PROBLEMS. DISASSEMBLY OF THE OIL PUMP ASSEMBLY REVEALED THE POST SB 7185 PLATE HAD BECOME WELDED TO THE SCAVENGE ELEMENT CAUSING IT TO SHEAR THE SHAFT DRIVE PIN. THIS FAILURE CAUSED FLOODINSDR 95ZZZX789Step Assy · block brokeUPON STOWING OF STEP ASSY, DETENT BLOCK SUPPORT BROKE. FOUND EXCESSIVE WEAR ON DETENT BLOCK CATCHES AND BLOCK. SUBMITTER SUGGESTS MORE FREQUENT LUBE OF CATCHES AND BETTER DEFINITION OF ALLOWABLE WEAR.SDR 95ZZZX787Handle · brokeWHEN PILOT CLOSED DOOR, DOOR HANDLE BROKE OFF (OUTSIDE HANDLE OF DOOR).SDR 95ZZZX975Mount Pad · corrodedFOUND CORROSION ON ENGINE MOUNT BOSS AND AREA ON ENGINE, DURING SCHEDULED INSPECTION. PRATT AND WHITNEY WAS INFORMED, GAVE OKAY TO CLEAN, TREAT, AND REINSTALL ENGINE MOUNTS.SDR 95ZZZX258Transmitter · failedLEFT ENGINE LOW OIL PRESSURE TRANSMITTER FAILED WHILE EN ROUTE. REPLACED TRANSMITTER. RETURNED TO SERVICE.
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