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 = '425' 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 = '425' 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 O05R2004117Blade · scratchedSCRATCH IN SHOTPEEN ON SHANK. AMMENDED SERIAL NO IN BOX 5 (D) BF024SDR O05R200400118Blade · scratchedSCRATCH IN SHOTPEEN ON SHANK.SDR O05R200400117Blade · scratchedPROPELLER BLADE HAS A SCRATCH IN SHOTPEEN ON SHANK.SDR O05R200400116Hub · crackedPROPELLER HUB CRACKED.SDR EWG2004F00000Skin · wrinkledIAW REQUIREMENTS OF FAR 145.63, SUBMITS THIS 8010-4. IN THE PROCESS OF PERFORMING A PHASE 2 AND 3 INSPECTION, DIAGONAL WRINKLES WERE DISCOVERED ON THE TOP LT WING PANEL BETWEEN THE AUX AND AFT SPARS IB OF THE NACELLE. AFTER CONTACT WITH AND REVIEW BY MFG ENGSDR 2003FA0000519Structure · debondedTHE AILERON IS AN ALL ALUMINUM BONDED ASSEMBLY. THE AILERON WAS REPAIRED BY REPLACING THE AFT SKIN, USING DER APPROVED DATA AND WAS RETURNED TO SERVICE 11-15-2002. ON 05-08-2003 A BOND LINE SEPARATION WAS DISCOVERED ON A SKIN EDGE. REVIEW OF THE REPAIR PROCSDR CA020530004Spring · failed(CAN) RFR: GEAR WOULD NOT GO DOWN.FINDINGS: FAULTY (OPEN) SOLENOID ASSEMBLY AND BROKEN SPRING.SDR 2002FA0000503Hose · failedHOSE WAS INSTALLED ON 10-15-99 1869.1TT. CURRENT AIRCRAFT TIME 2234.8 HRS. THIS HOSE LASTED 365.7 HRS. THIS HAS BEEN AN ON GOING PROBLEM WITH THIS AIRCRAFT. CESSNA SUPERSEEDED THE ORIGNAL HOSE P/N AS705976-1 TO THE AE7013002K024 WHICH IS SLIGHTLY LONGER,IN HOPSDR 2002FA0000407Tube · meltedRIGHT INSTRUMENT AIR PRESSURE WAS AT ZERO ON THE GROUND AND WOULD INCREASE AS CABIN PRESSURE INCREASED IN FLIGHT. FOUND PNEUMATIC SUPPLY LINE FROM COMMON TEE TO FORWARD PRESSURE BULKHEAD MELTED. REPLACED TUBING WITH SUPERSEDED (PN P610051) TWICE. BOTH TIMESSDR 2002FA0000406Tube · meltedRIGHT INSTRUMENT AIR PRESSURE WAS AT ZERO ON THE GROUND AND WOULD INCREASE AS CABIN PRESSURE INCREASED IN FLIGHT. FOUND PNEUMATIC SUPPLY LINE FROM COMMON TEE TO FORWARD PRESSURE BULKHEAD MELTED. REPLACED TUBING.SDR 2002FA0000405Tube · meltedRIGHT INSTRUMENT AIR PRESSURE WAS AT ZERO ON THE GROUND AND WOULD INCREASE AS CABIN PRESSURE INCREASED IN FLIGHT. FOUND PNEUMATIC SUPPLY LINE FROM COMMON TEE TO FORWARD PRESSURE BULKHEAD MELTED. REPLACED TUBING.SDR 2002FA0000364Window · crackedWINDOW, LOCATED IN UPPER CABIN DOOR, WAS FOUND TO HAVE 4 CONSECUTIVE MOUNTING HOLES BROKEN ALONG LOWER EDGE. A RETAINING RING, CALLED OUT IN PARTS BOOK, WAS NOT INSTALLED ON THIS WINDOW. THE INSTALLATION APPEARS TO HAVE BEEN DONE AT THE FACTORY, DUE TO DATESDR 2001FA0000617Fan · failedAIRCRAFT RETURNED FROM FLIGHT WITH CABIN BLOWER OPERATING BUT NOT MOVING ANY AIR. GAINED ACCESS TO BLOWER ASSEMBLY UNDER CO-PILOT FLOOR. FOUND ALL FAN BLADES TO BE BROKEN OFF. THIS IS THE SECOND TIME THIS HAS HAPPENED IN LESS THAN TWO MONTHS. CHECKED MOTORSDR WC72001F00000Link · corrodedTHE TRAILING LINK ASSEMBLY ON LEFT AND RIGHT MAIN LANDING GEAR HAD CORROSION AND PITTING PRESENT IN THE LIGHTENING BORE AT THE FORWARD OR UPPER END. PITTING IN AREAS WAS APPROXIMATELY .025. AFTER BLENDING AND REMAINING THICKNESS DETERMINED WITH UT THE PART WSDR 2001FA0000320Line · deterioratedLEFT SIDE WALL WAS REMOVED TO INSTALL RADIO EQUIPMENT. THE VERTICAL DUCT FOR AIR TO OVERHEAD WEMAC SHOWED DEFINITE SIGNS OF BURNING AND SEVERE DETERIORATION. UPON FURTHER EXAMINATION, THE OXYGEN LINE CROSSING DUCT HAD SEVERE CORROSION WHERE CONTACT BETWEEN TSDR 20010511CW009Hose · rupturedHOSE PN 156F001-12D0196 MANUFACTURED IQ99 INSTALLED 3, 00 RUPTURED IN FLIGHT DUMPING OIL ON LEFT ENGINE.SDR 20010423CW008Link · corrodedDURING PAHSE INSPECTION CORROSION WAS FOUND INSIDE THE LIGHTENING BORE OF THE AXLE LINK ASSEMBLY ON BOTH MAIN GEAR AT THE UPPER END (KNEE). CORROSION WAS REMOVED AND AFTER MEASURING REMAINING THICKNESS THE PARTS WERE FOUND WITHIN PRODUCTION TOLERANCES. THE SDR 20010423CW007Link · corrodedDURING PHASE INSPECTION CORROSION WAS FOUND INSIDE THE LIGHTENING BORE OF THE AXLE LINK ASSEMBLY ON BOTH MAIN GEAR AT THE UPPER END.(KNEE). CORROSION WAS REMOVED AND AFTER MEASURING REMAINING THICKNESS THE PARTS WERE FOUND WITHIN PRODUCTION TOLERANCES. THE BSDR 20010323CW012Angle · crackedWHILE INSPECTING FOR FUEL LEAKS A CRACK APPROXIMATELY 2.5 INCHES IN LENGTH WAS FOUND IN THE LEFT CANTED RIB, JUST AFT OF THE FORWARD SPAR, BELOW THE TOP SKIN. RECOMMEND REPLACEMENT OF THE ANGLE.SDR 20001227SH001Trunnion · groovedFOUND TWO SMALL GROOVES WORN INTO THE NOSE GEAR UPPER TRUNNION WHERE THE DRAG BRACE ATTACH LINK CONNECTS TO THE UPPER TRUNNION. THE FORWARD END OF THE ATTACH LINK WAS MAKING CONTACT WITH THE UPPER TRUNNION DURING NORMAL OPERATION. FOUND BEARING IN ATTACH LINSDR CA001016009Door Frame · cracked(CAN) A CRACK WAS FOUND IN THE LOWER MAIN CABIN DOOR. THE CRACK WAS LOCATED ON THE FRAME ASSEMBLY IN THE RADIUS TO THE FLANGE WHERE THE SEAL RETAINER STRIP IS ATTACHED AROUND THE FRAME. (SEE ATTACHED PC REFERENCE). THE FRAME PART NUMBER IS 5711145-4. THE CRACKSDR 20000914SH016Fan Blade · brokenDURING FLIGHT, CREW SMELLED BURNING PLASTIC. UPON INVESTIGATION BY MAINTENANCE, FOUND THAT ALL OF THE FAN BLADES HAD BROKEN OFF AND WERE LAYING IN THE AUXILIARY HEATER ASSY. ONE BLADE MADE IT INTO THE HEATER COILS AND WAS BEING MELTED. INSTALLED NEW FAN BLASDR 20000825SH004Hinge · crackedDURING INITIAL INSPECTION OF THE AILERON, A SLIGHT BUCKLING WAS OBSERVED IN THE UPPER HINGE AREA. UPON REMOVAL OF THE UPPER SKIN, A CRACK WAS DISCOVERED IN THE UPPER HINGE BRACKET AREA (P/N 5834120-6). THE CRACK EXTENDED FROM RIBS 5834110-90 TO 5834110-98, WSDR 2000ZZZX720Nut · splitDURING A PHASE INSPECTION, THE LEFT NUT THAT RETAINS THE HORIZONTAL STABILIZER WAS FOUND SPLIT FROM TOP TO BOTTOM. RECORDS SHOW THAT SB CQB 85-25 AND AD 85-25-11 WERE C/W IN 1986. THE SB AND AD ADDRESS THIS PROBLEM. THE NUT THAT SPLIT APPEARS TO HAVE BEEN TSDR 99ZZZX4236Hose · failedSIDE WALL OF RIGHT OIL COOLER HOSE, PN AE705976, FAILED WHERE HOSE MAKES A SHARP BEND WHEN INSTALLED. HOSE FAILED WITH NO SIGNS OF PREVIOUS LEAKAGE. CESSNA RECOMMENDED INSTALLATION OF LONGER OIL HOSE, PN AE7013002K0204. HOSE INSTALLATION REQUIRES FORM 337 FSDR AU990934Fitting · faulty(AUS) NOSE LANDING GEAR ACTUATOR SUPPORT CHANNEL FASTENERS FAILED.SDR 99ZZZX2101Wheel · crackedMAIN WHEEL CRACKED IN SPOKE AREA.SDR 99ZZZX809Encoder · malfunctionedERRORS AFTER 2 HOUR FLIGHT AT 13,000 FEET. REMOVED AND REPLACED WITH OVERHAULED UNIT.SDR 99ZZZX1005Aux Elec Heater · failedOPERATOR NOTED LOW HEAT OUTPUT. MAINTENANCE REMOVED AUXILIARY ELECTRIC HEATER AND FOUND TWO OUT OF THREE HEATER COILS BURNED THROUGH WHERE THEY ATTACH TO THE WIRE HARNESS POST. ALSO NOTED SOME CARBON BUILD-UP ON ATTACH POST SCREW THREADS. CAUSE OF FAILED COSDR 98ZZZX3621Windshield · crackedDURING REMOVAL OF COPILOT'S WINDSHIELD, NOTED 2 CRACKS EXTENDING FROM BOLT HOLES TO THE EDGE OF THE WINDSHIELD.SDR 98ZZZX3234Mount · crackedLEFT ENGINE OUTBOARD ENGINE MOUNT BRACKET HAS SMALL CRACK ON THE FORWARD LOWER SIDE OF MOUNT.SDR CA980707029Switch · out of rig(CAN) ON APPROACH, PILOT SELECTED GEAR DOWN AND HAD NO NOSE GEAR INDICATION. RECYCLED GEAR AND RECEIVED ALL GREEN LIGHTS, BUT ALSO HAD A GEAR INTRANSIT AND HYDRAULIC PRESSURE ON LIGHT. PULLED ALTERNATE GEAR EXTENSION WHICH PUTS 2,000 PSI ON DOWN SIDE AND LANSDR 98ZZZX2702Hose · meltedHOSE, P/N P610051, MELTED THROUGH AND BRITTLE. FACTORY SUGGESTED REPLACING HOSE WITH A HIGHER TEMPERATURE HOSE. LOUD AIR PRESSURE LEAK IN COCKPIT AREA. NO AIR PRESSURE INDICATION ON AIR PRESSURE GAUGE. HOSE RUNS FROM T-FITTING UNDER RIGHT AIR CONDITIONER ESDR CA980421002Fuel Nozzle · torching(CAN) DURING CLIMB AFTER TAKEOFF, NR 2 ENGINE POWER ROLLED BACK FROM 1244 POUNDS TORQUE TO 800 POUNDS, T5 TEMPERATURE WAS 670C AND NG WAS 81 PERCENT. PILOT RETURNED TO BASE. POWER SECTION REMOVED FOR HSI AND EXTENSIVE TORCHING DAMAGE WAS FOUND ON THE COMPRESSDR 97ZZZX4499Skin · crackedDURING REMOVAL OF WINDSHIELD RETAINER FOR REPLACMENT OF WINDSHIELD, FOUND APPROXIMATEY 2 INCH LONG CRACK UNDER LT LOWER CORNER OF WINDSHIELD RETAINER. CRACK APPARENTLY CAUSED BY IMPROPER REMOVAL PROCEDURES OF RETAINER DURING A PREVIOUS WINDSHIELD CHANGE. AN SDR 97ZZZX3803Actuator · intermittentRIGHT MLG SHOWED UNSAFE INDICATION WHEN EXTENDED. AFTER SEVERAL CYCLES, STILL NO DOWN AND LOCKED INDICATION. TROUBLESHOT SYSTEM AND FOUND DOWN AND LOCKED SWITCH WITHIN RT MLG ACTUATOR TO BE UNRELIABLE INTERMITTENTLY. REPLACED RT MLG ACTUATOR ASSY.SDR 97ZZZX2882Ground Wire · looseRIGHT GENERATOR CONTINUOUSLY DROPPED OFF-LINE, BUT WOULD RESET. FOUND GENERATOR GROUNDING ATTACHED TO SPAR WEB JUST AFT OF ENGINE. THE GROUND WIRE WAS LOOSE AND HAD BEEN ARCING TO SPAR WEB. ORIGINAL HOLE IS ORIGINALLY .375 INCH DIAMETER AND HAD BEEN ARCED OUSDR 97ZZZX1932Control Cable · failedPILOT REPORATED WHILE ON APPROACH, FULL FLAPS WERE SELECTED. AT THAT TIME, A LOUD NOISE WAS HEARD AND THE A/C VIOLENTLY ROLLED TO THE RIGHT. THE PILOT REGAINED CONTROL OF THE A/C BY RAISING THE FLAPS AND MADE A SAFE LANDING. UPON INSP FOUND RT FLAP HANGING SDR 97ZZZX1963Camloc · failedDURING REMOVAL OF ENGINE COWL, ONE CAMLOC DIFFICULT TO REMOVE. CAMLOC FINALLY CAME OUT WHEN CROSS PIN FELL OUT. THE CROSS PIN FELL INTO ENGINE INTAKE AIR PLENUM. THE PIN WAS RECOVERED. CAMLOC RECEPTACLE IS OF AN OPEN BACK TYPE AND LOCATED INSIDE INTAKE AISDR 96ZZZX5943Switch · malfunctionLEFT HAND GENERATOR APPEARED TO CARRY ONLY 60 AMP LOAD. TROUBLESHOT TO AN INDICATION ERROR. FOUND BAT/GEN SWITCH TO CAUSE LEFT GENERATOR AMMETER INDICATION ERROR. INSTALLED NEW SWITCH OPERATIONAL TEST GOOD. THIS IS THE SECOND TIME THIS FACILITY HAS FOUND TSDR 96ZZZX5411Piston · wornTHE PISTON, REF NR 20, IS WORN WHERE THE SEAL OR BEARING RIDES WHEN THE AIRCRAFT IS ON THE GROUND, ABOUT 6 INCHES UP FROM THE BOTTOM. THE WEAR AREA IS ABOUT 2.5 INCHES LONG AND ABOUT ONE-THIRD WAY AROUND THE PISTON ON THE FRONT OUTBOARD SIDE. TOTAL TIME ON ASDR 96ZZZX4150Elevator · mismanufacturedRECEIVED 'NEW' PART, DROP SHIPPED FROM CESSNA AIRCRAFT. PREPPED AND PAINTED TO MATCH AIRCRAFT. PLACED CONTROL SURFACE ON BALANCING JIG. PART REQUIRED 6 OUNCES OF ADDITIONAL COUNTERWEIGHT TO BRING WITHIN PRESCRIBED LIMITS. REMOVED EXISTING LT ELEVATOR DUE TSDR 96ZZZX4880Relay · failedRELAY CONTROLS THE APU CUT-OUT RELAY TO PREVENT USE OF WINDSHIELD HEAT WITHOUT THE GENERATOR OR APU ON-LINE. THIS RELAY SHORTED INTERNALLY WHICH POSSIBLY SENT A FALSE SIGNAL TO THE GCU WHICH CAUSED THE GENERATORS* TO GO OFF LINE IN-FLIGHT. AFTER EXTENSIVE TRSDR AU960586Microswitch · faulty(AUS) RH MAIN LANDING GEAR DOWNLOCK MICROSWITCH FAULTYSDR AU960189Solenoid · intermittent(AUS) LANDING GEAR EXTENSION SOLENOID INTERMITTENT IN OPERATIONSDR 96ZZZX2497Bracket · brokenFOUND THE RT WING NACELLE FUEL TANK PROBES MOUNTING BRACKETS BROKEN AND LEFT ONE BENT. THIS CONDITION CAUSES ERRONEOUS FUEL QUANTITY INDICATION. FOUND THE WEIGHT OF THE TOP OF THE FUEL TANK BLADDER TANK BEARS AGAINST THIS BRACKET WHEN THE TANK IS PARTIALLY OSDR EY2R9601412Actuati Pin · damagedACTUATING PIN DAMAGEDSDR 95ZZZX7024Arm · brokenPILOT SEAT BACK FELL BACK AFTER SUPPORT ARM BROKE, WHILE PILOT WAS DEPARTING AIRCRAFT. SUSPECT CAUSE IS METAL FATIGUE.SDR 95ZZZX2938Fuel Control · req lubeHOBBS 115.1. TT A/F 4861.2. ON DESCENT, LEFT ENGINE DID NOT RESPOND TO POWER REDUCTION. TROUBLESHOT, CLEANED, AND LUBRICATED F.C.U., ROD ENDS, AND LINKGAGE. OPS CHECK OKAY. FLIGHT CHECK OKAY. ENGINE T.S.O. 1369.7.SDR 95ZZZX2852Pump · failedFUEL PUMP ON LEFT ENGINE, SEAL LEAKED FUEL INTO FUEL CONTROL DRIVE, WASHING THE GREASE OUT OF THE DRIVE BEARING CAUSING BEARING FAILURE AND DRIVE COUPLING TO SHEAR.
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