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 = '152' 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 = '152' 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 EY2R9600015Fix Pitch · crackedNR 1 MOUNTING HOLESDR AU960115Hinge · cracked(AUS) TOP DOOR HINGE CRACKED IN AFT SECTION - DOOR HINGE PIN ALSO SHEAREDSDR 96ZZZX1255Floor Panel · corrodedDURING ROUTINE INSPECTION, CARPET WAS REMOVED. FOUND CORROSION ON FLOOR. FURTHER INSPECTION REVEALED CORROSION ON 5 OF 6 FUEL LINES UNDER FLOOR AND ALONG DOOR SILLS AND DOOR POST. SUBMITTER SUSPECTS IMPROPER FLAMEPROOFING ON CARPET CAUSED CORROSION.SDR AU960117Nut · loose(AUS) ENGINE THERMOSTATIC OIL COOLER BYPASS VALVE (VERNATHERM) NUT LOOSE - FOUND DURING INSPECTION IAW AD/LYC/78SDR 96ZZZX1099Carburetor · defectiveINSPECTION FOUND CARBURETOR COMPOSITE FLOATS BLACK AND CARBONED. IN ADDITION, THROTTLE ARM WORN. TWO PIECE VENTURI WAS INSTALLED.SDR 96ZZZX718Push Rod · defectiveON INSPECTION OF AD 95-03-10, PUSH ROD OF ACCEPTABLE PART NUMBER PER AD WAS FOUND TO HAVE A LOOSE BALL END AND TUBE WAS MUSHROOMED. THIS ENGINE WAS DUE FOR OVERHAUL IN 42 HOURS AT NEXT 100-HOUR INSPECTION, AND THE HIGH TIS WAS SUSPECT CAUSE OF DEFECT.SDR AU960088Terminal · broken(AUS) BATTERY CABLE POSITIVE TERMINAL BROKEN - FREE END OF CABLE SHORT CIRCUITED ALTERNATOR OUTPUT TO BATTERY BOXSDR 96ZZZX598Switch · defectiveDURING RUN-UP/MAG CHECK, THE IGNITION KEY COULD BE EASILY REMOVED (IN ANY POSITION). CESSNA SEB 92-29 AND TCM SB 636 CLEARLY CITES THIS AS A MANDATORY INSPECTION, AND A 'HOT MAG' IS NOT SAFE. YET, AD 93-05-06 'GERDES SWITCH INSPECTION', HAD BEEN SIGNED OFF.SDR CA960126038Valve · sticking(CAN)ENGINE HAD OIL LEAK #3 CYLINDER, AFTER REMOVING THE CYLINDER IT WAS FOUND THAT THE EXHAUST VALVE WAS STICKING AND THE PUSH ROD WAS BENT.SDR EY2R9600192Propeller · corrodedFIXED PITCH PROP ASSY IS CORRODEDSDR 96ZZZX781Bracket · crackedBRACKET FOUND CRACKED DURING REPAIRS TO HORIZONTAL STABILIZER FOLLOWING GROUND COLLISION. CRACKS IN WELDED AREA EXISTED BEFORE COLLISION. DISSIMILAR METAL CORROSION ALSO EXISTED BETWEEN STEEL BRACKET AND ALUMINUM SKINS.SDR 96ZZZX575Torque Tube · crackedFOUND AT 100-HOUR INSPECTION. CIRCUMFERENTIAL CRACK IN RIGHT ELEVATOR TORQUE TUBE. TSN - 6,851.8. CHECKED AIRCRAFT HISTORY, NO UNUSUAL OCCURRENCES DOCUMENTED. USED PRIMARILY IN FLIGHT TRAINING.SDR CA951221032Propeller · cracked(CAN)DURING INSPECTION 3 CRACKS WERE SUSPECTED IN THE PROPELLER. AT THE MOUNTING BOLTS, THIS COULD NOT BE CONFIRMED BY DYE PENETRANT INSPECTION. THE PROPELLER WAS SENT TO A PROPELLER OVERHAUL SHOP AND A ZY GLO INSPECTION CONFIRMED THE CRACKS.SDR CA951218017Wing Strut · loose rivet(CAN)DURING INSPECTION UPWARD PRESSURE WAS APPLIED TO THE WING AND A LOUD CRACKING NOISE WAS HEARD. THE SOURCE WAS TRACED TO THE UPPER WING STRUT ATTACH RIVETS WHICH HAD BECOME LOOSE. SUBMITTER REBUCKED TH E RIVETS AND RETURNED THE AIRCRAFT TO SERVICE.SDR 96ZZZX465Contactor · failedPILOT STARTED ENGINE FOR TAKEOFF. STARTER CONTACTOR WELDED IN THE 'ON' POSITION. WHEN PILOT RELEASED KEY, STARTER CONTINUED TO RUN UNTIL BURNED UP. PILOT WAS NOT AWARE OF CONDITION. SUBMITTER STATED THIS IS A FAIRLY COMMON OCCURRENCE WITH 24V STARTERS ON CSDR CA951215016Fork · cracked(CAN)NOSE GEAR FORK FOUND CRACKED DURING INSPECTION. NO CORROSION FOUND. CRACK MEASURED 1.25 INCHES IN LENGTH.SDR 96ZZZX687Safety Wire · errorPERTAINS TO AD 95-21-01 WHICH REFERS TO MCCAULEY SB 219 WHICH HAS A STEP-BY-STEP INSTRUCTION ON PERFORMING THIS AD TO THE PROPELLER. STEP 2F STATES THAT MOUNTING BOLTS ARE TO BE SAFETIED WITH .032 INCH SAFETY WIRE. AC 43:13 STATES THAT .041 INCH STAINLESS STSDR 96ZZZX349Tappet · defectiveENGINE EXPERIENCED INTERMITTENT MISS. WHILE TROUBLESHOOTING, DISCOVERED NR 4 CYLINDER ROCKER TO VALVE CLEARANCE COULD NOT BE SET PROPERLY. ENGINE TORN DOWN AND FOUND TWO TAPPETS DEFECTIVE. SOCKET END WAS LOOSE AND TURNED FREELY IN END OF BODY. CAUSED EXCESSDR 95ZZZX7008Push Rod · crackedFOUND BALL END IN PUSH ROD LOOSE AND PUSH ROD TUBE CRACKED ABOUT .75 INCH ON SAME END.SDR 95ZZZX7033Line · deterioratedWHILE REPAIRING FUEL LEAK ON RT FUEL TANK INTERCONNECT HOSE WHICH WAS INCORRECTLY INSTALLED AND LEAKING, IT WAS NOTICED THAT THE LT HOSE WAS ORIGINAL EQUIPMENT, SEVERELY AGED, AND READY TO FAIL. RECOMMENDATION: ALL FLEX FUEL LINES BE REPLACED AT MINIMUM OF 2SDR 96ZZZX170Control Cable · frayedDURING REPLACEMENT OF RUDDER PULLEYS IN EMPENNAGE, FOUND BOTH RUDDER CABLES FRAYED. THE RT CABLE WAS FRAYED AT STA 173 WHERE IT PASSES OVER A PULLEY. THE FRAYING WAS NOT EVIDENT UNTIL PULLEY WAS REMOVED. THE LT CABLE HAD THE SAME CONDITION AT STA 184. SUBMSDR 96ZZZX169Control Cable · frayedDURING REPLACEMENT OF RUDDER PULLEYS IN EMPENNAGE, FOUND BOTH RUDDER CABLES FRAYED. THE RT CABLE WAS FRAYED AT STA 173 WHERE IT PASSES OVER A PULLEY. THE FRAYING WAS NOT EVIDENT UNTIL PULLEY WAS REMOVED. THE LT CABLE HAD THE SAME CONDITION AT STA 184. SUBMSDR 95ZZZX6921Floor Pan · crackedCOPILOT INBOARD SEAT RAIL AFT END, STA 27.02 TO STA 56.69, FOUND FLOORBOARD CRACKED AT AFT END OF INBOARD SEAT RAIL (COPILOT SIDE). THE CRACK WAS 2 INCHES IN LENGTH AND CORRESPONDED DIRECTLY WITH THE AFT END OF THE SEAT RAIL. THE FLOOR BEGINS TO CONTOUR UPWASDR 95ZZZX6735Bracket · crackedCRACKS WERE FOUND AT THE LOWER, MOST FORWARD LOCATION OF BRACKET ASSEMBLY FOR THE ELEVATOR BELLCRANK.SDR 95ZZZX6572Pump · shaft shearedINSTALLED A RAPCO RE-BUILT VACUUM PUMP. CLEANED ALL LINES AND CHANGED BOTH FILTERS. PUMP FAILED AFTER 18 HOURS TIME IN SERVICE. FAILURE WAS DUE TO DRIVESHAFT SHEARING.SDR CA951030001Bearing Half · cracked(CAN)ROUTINE MAINTENANCE FOUND THE UPPER HALF OFTHE PLASTIC RUDDER BEARING FOR THE RUDDER PEDAL CROSS SHAFT CRACKED IN HALF.SDR 95ZZZX6757Floor Panel · crackedDURING 100-HOUR INSPECTION, COPILOT'S INBOARD SEAT TRACK AFT FLOOR AREA, FOUND 2 INCH CRACK. CRACK AT RADIUS COMES UP OVER MAIN LANDING GEAR ATTACH BOXES. SUSPECT CAUSE, SEAT TRACK TOO LONG ENDING IN THE START OF THE RADIUS. SUGGEST BEVEL SEAT TRACK TO PREVSDR 95ZZZX6537Pushrod · failedPUSHROD MARKED AS 73806# FAILED AT END OF PUSHROD. LYCOMING MANDATORY SB OA-522 IN CONJUNCTION WITH AD 95-03-10, WAS ACCOMPLISHED 2-16-95. NO DEFECTS IN ENGINE VALVE TRAIN OR VALVES STICKING WERE NOTED. PARTS WERE REPLACED AND ENGINE RAN OK AND RETURNED TO SDR 95ZZZX6570Cylinder · crackedLOSS OF POWER AND ENGINE ROUGHNESS WAS REPORTED. UPON INSPECTION, CYLINDER NR 2 WAS FOUND TO HAVE LOW COMPRESSION. FURTHER INSPECTION LED TO FINDING A CRACK APPROXIMATELY ONE-HALF WAY AROUND THE CIRCUMFERENCE OF THE CYLINDER BETWEEN THE FINS AT THE JUNCTION SDR 95ZZZX6185Spar · crackedDURING ANNUAL INSPECTION, A CRACK 3.25 INCHES LONG WAS FOUND IN LT WING REAR SPAR. THE CRACK STARTED AT FLAP PULLEY BRACKET, P/N 0460205-102, AND EXTENDED OUTBOARD, RUNNING HORIZONTALLY 3.25 INCHES. INBOARD HALF OF SPAR WAS REPLACED AND ACFT RETURNED TO SERVSDR 95ZZZX6073Rudder Bar · brokenRUDDER BAR BROKEN AT RIGHT PEDAL ATTACH ON PILOT'S SIDE. SUBMITTER SUGGESTS INSPECT MORE CLOSELY FOR CRACKS. THIS AREA IS NOT INSPECTED WELL ON MANY CESSNA AIRCRAFT BECAUSE IT IS UNDER A DIFFICULT TO REMOVE PANEL.SDR 95ZZZX6302Pushrod · looseDURING ROUTINE INSPECTION, A VALVE GUIDE CLEARANCE CHECK WAS DONE. THE NR 1 CYLINDER INTAKE PUSHROD WAS FOUND TO HAVE THE STEM LOOSE. IT COULD EASILY BE REMOVED BY HAND. THIS PART IS NORMALLY A PRESS-FIT AND IS NOT REMOVABLE. REPLACED WITH NEW.SDR 95ZZZX6616Cylinder · crackedINSTALLED CERMICHROME OHL CYLINDERS AT OVERHAUL. AT 350 SMOH, DETECTED AN OIL LEAK FROM THE HEAD-BARREL-JUNCTION. UPON REMOVAL, DETECTED A CIRCUMFERENTIAL CRACK 1.50 INCHES LONG, ONE INCH FROM THE TOP OF THE BARREL AT THE 12:00 POSITION.SDR 95ZZZX6752Bracket · crackedDURING C/W AD 80-11-04, IT WAS NOTICED THE WELD ON THE RIGHT FRONT OF THE V-FIN ATTACH FITTING WAS CRACKED. REMOVAL VERIFIED A 1 INCH CRACK.SDR 95ZZZX6540Hub · crackedWHILE PERFORMING AD 95-21-01 ON MCCAULEY PROPELLER, CRACK WAS FOUND TO BE UNACCEPTABLE AND BEYOND LIMITS. PROP SCRAPPED.SDR 95ZZZX6539Hub · crackedWHILE PERFORMING AD 95-21-01 ON MCCAULEY PROPELLER, CRACK WAS FOUND TO BE UNACCEPTABLE AND BEYOND LIMITS. PROP SCRAPPED.SDR 95ZZZX6538Hub · crackedWHILE PERFORMING AD 95-21-01 ON MCCAULEY PROPELLER, CRACK WAS FOUND TO BE UNACCEPTABLE AND BEYOND LIMITS. PROP SCRAPPED.SDR 95ZZZX6759Coil · openLEFT MAG INOP ON RUN-UP. REMOVED MAGNETO AND DISASSEMBLED. ELECTRICALLY CHECKED COIL AND FOUND OPEN CIRCUIT. REPLACED COIL WITH SERVICEABLE COIL AND OPS CHECK OK. DATE CODE ON FAILED COIL: 9/16/91.SDR 95ZZZX6009Push Rod · damagedDURING A 100-HOUR INSPECTION, A SMALL DENT IN NR 1 AND NR 4 EXHAUST PUSH ROD SHROUDS WAS DETECTED. THEY SEEMED TO BE LEAKING OIL. A FURTHER INSPECTION OF THE PUSH RODS REVEALED A VERY DEEP GROOVE OR CHANNEL WORN INTO THEM WHERE THE DENT IN THE SHROUD WAS LOCSDR 95ZZZX6444Control Cable · failedPILOT REPORTED POWER HAD BEEN REDUCED TO DESCEND, AND THAT IT WAS NOT POSSIBLE TO RESTORE ENGINE POWER; MOVEMENT OF THE THROTTLE YIELDED NO CHANGE IN ENGINE POWER. AN OFF-AIRPORT LANDING OCCURRED. THE AIRPLANE WAS NOT DAMAGED DURING THE LANDING ON A DRY DESERSDR 95ZZZX6410Pushrod · crackedANNUAL INSPECTION FOUND NR 4 INTAKE PUSHROD TO HAVE .75 INCH CRACK AT ROCKER ARM END. REFERENCE AD 80-25-02R2, AD 95-03-10, LYCOMING SB 453 AND LYCOMING SI 2388A. PART TOTAL TIME, 1,973.6 HOURS.SDR 95ZZZX5763Coil · openPILOT REPORTED RT MAG INOPERATIVE. INVESTIGATION FOUND MAGNETO COIL OPEN, COIL REPLACED AND MAGNETO FUNCTIONED NORMALLY. SUBMITTER STATED THIS IS 4TH SUCH PROBLEM WITH THIS COIL (ORANGE). NEW COIL IS BLACK, PN M3575.SDR 95ZZZX5973Floorboard · crackedDURING ROUTINE REPLACEMENT OF SEAT RAILS, THE FLOORBOARD WAS FOUND CRACKED AT THE AFT END OF THE RIGHT SEAT INBOARD SEAT RAIL. THE NEW AND OLD SEAT RAILS ARE NOT ROUNDED OFF AND HAVE SHARP EDGES WHICH MAY HAVE CONTRIBUTED TO THIS CRACKING PROBLEM. SUBMITTER SDR 95ZZZX5955Floorboard · crackedDURING REPLACEMENT OF SEAT RAILS, THE FLOORBOARD WAS FOUND CRACKED AT THE AFT END OF THE RT SEAT INBOARD SEAT RAIL. THE AREA AFT OF THE LT SEAT INBOARD SEAT RAIL SHOWS SIGNS OF CHAFING. THE NEW AND OLD RAILS ARE NOT ROUNDED OFF AND HAVE SHARP EDGES WHICH MAYSDR 95ZZZX5609Control Cable · frayedFLAP EXTENSION CABLE IN THE LEFT WING, THE CABLE HAS APPROXIMATELY 80 PERCENT OF THE STRANDS BROKEN. THE BROKEN WIRES WERE OVER THE HEADLINER AND WERE NOT VISIBLE UNTIL THE HEADLINER OPENED. DISCOVERED THE BROKEN CABLE WHILE REMOVING THE WINGS FROM THE AIRCRSDR 96ZZZX60Bracket · crackedWHILE PERFORMING 100-HOUR INSPECTION AND AD 80-11-04 (VERTICAL FIN ATTACH NUTPLATE), FOUND ATTACH BRACKET CRACKED IN 5 PLACES. NUTPLATES WERE IN GOOD CONDITION. BRACKET WAS REPLACED. SUBMITTER SUGGESTS THE AREA SHOULD BE CLEANED VERY WELL BEFORE INSPECTION SDR 95ZZZX5122Heat Flap · seal detachedAIRCRAFT LOST POWER DURING FLIGHT. PILOT MADE AN UNEVENTFUL EMERGENCY LANDING. UPON FURTHER INSPECTION, FOUND CARBURETOR HEAT FLAPPER SEAL HAD BROKEN OFF AND A PIECE LODGED IN CARBURETOR VENTURI. UPON REMOVAL OF PIECE OF SEAL, AIRCRAFT DEVELOPED FULL POWER.SDR 95ZZZX4522Hub · crackedAN OIL LEAK WAS REPORTED. INVESTIGATION DISCLOSED A CRACK IN THE (FIXED PITCH) PROPELLER HUB RUNNING FROM THE HUB INSIDE DIAMETER, THROUGH THE EDGE OF ONE LEADING EDGE BOLT HOLE TO THE OUTSIDE DIAMETER OF THE HUB. THE FORWARD SPINNER BULKHEAD ALSO HAD ONE 6 SDR 95ZZZX5617Gasket · faultyDURING COMPLIANCE WITH AD 95-03-02, IT WAS NOTED THAT FACTORY FURNISHED HOLES IN THE GASKET CAUSE MISALIGNMENT OF SEALING/GLUING SURFACE AND LACK OF CONTACT AREA WHICH COULD LEAD TO GASKET INGESTION. (TOPIC OF AD 95-0302).SDR 95ZZZX4343Hub · crackedFOLLOWING THE DISCOVERY OF A PROPELLER WITH A HUB CRACK AT THE LEADING EDGE BOLT HOLE OF NR 1 BLADE, INSPECTION OF SAME PROPELLER MODEL ON OTHER 'N' NUMBERED AIRCRAFT WAS MADE. THE OTHER PROPELLERS' TIMES RANGED FROM 3,950 HRS TO 6,171 HRS, TT. ALL OF THE OL
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