Continental TSIO-550-A

Service difficulty reports · 17

Newest first. General aviation reporting is voluntary.

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 engine_model_key = 'TSIO550A'
  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.

SDR 2016FA0000456Exhaust Header · crackedRIGHT TURBOCHARGER TRANSITION ASSEMBLY WAS FOUND CRACKED FRONT AND BACK DURING ANNUAL INSPECTION OF AIRCRAFT. PILOT REPORTED CO DETECTOR CHIRPING ON TRIP TO ANNUAL. THIS CRACKED PART IS ATTACHES THE TURBOCHARGER TO THE RIGHT EXHAUST, FORWARD AND BELOW THE CABSep 26, 2016 · N115RW · Columb LC41550FG400 · Reciprocating Engine Power SectionSDR 2016FA0000252Gps · failedFAILURE OF G1000 NAVIGATION & MAPPING SYS IN FLIGHT. FAILURE OF FMS TO ALLOW LOADING & CHANGE OF FLIGHT PLAN. FAILURE OF MFD TO ALLOW DISPLAY OF ASSOCIATED CHARTS ENROUTE, SID, STAR & APPROACH PLATES.May 19, 2016 · N780AF · Cirrus SR22T · Global Positioning SystemSDR ENEA20131112001Throttle Cable · brokenON THE LAST FLIGHT, AT APPROX 5:02 PM, THROTTLE CABLE BROKE DURING APPROACH TO LANDING. THREE MILES OUT AT 1000 FT, THE ACFT WAS CONFIG WITH 10 DEG FLAPS, L5OO RPM & AIRSPEED OF 80 KTS. WHILE ENTERING THE BASE LEG ATTEMPTED TO MAKE A PWR REDUCTION. WHEN THENov 12, 2013 · N9957M · Cessna 207A · Power LeverSDR 2012FA0000594Points · brokenIN FLIGHT, ENGINE BEGAN TO RUN POORLY. ON LANDING AND FURTHER INSPECTION, IT WAS DISCOVERED THAT THE LT MAGNETO WAS INOPERATIVE. THE MAGNETO WAS REMOVED, DISASSEMBLED AND INSPECTED. POINTS DISCOVERED BROKEN. FOLLOWER ARM FOR THE POINTS HAD SEPARATED AND WAAug 10, 2012 · N760SP · Magneto/DistributorSDR 2012FA0000355Check Valve · obstructedDURING SCHEDULED ANNUAL INSPECTION, OIL COOLER REMOVED TO PERFORM A WELD REPAIR TO A CRACKED MOUNTING FLANGE. AFTER REINSTALLATION AND COMPLETION OF THE ANNUAL, A POWER RUN UP WAS SCHEDULED. AFTER TAXI OUT AND UPON POWER APPLICATION FOR THE RUN UP, THE COCKPJun 2, 2012 · N244TA · Cirrus SR22 · Engine Oil Indicating SystemSDR 2011FA0000312Antenna · noisyDIGITAL DATA NOISE IN HEADSETS. ACFT MODE S TRANSPONDER SYS. CURRENT ANTENNA LOCATION IS TOO CLOSE TO CABIN ENVIRONMENT.Mar 24, 2011 · N289CM · Cirrus SR22 · Dependent Position Determining SystemSDR 2011FA0000184Torque Tube · corrodedELEVATOR TORQUE TUBE HAS INTERNAL CORROSION INSIDE TORQUE TUBE WITH RUST CONCENTRATION AROUND WELDED AREAS. AMM CHAP 27-30-00, PAGE 3 ITEM 2(C)(3) STATES TO INSPECT EVERY 200 HRS OR ANNUAL FOR INTEGRITY, EXCESSIVE WEAR, AND CRACKS. INSPECT WELD FOR CRACKS. TMar 18, 2011 · N2528D · Lancar LC41550FG · Elevator Control SystemSDR FCPR20110003Pressure Sensor · failedLOW OIL PRESSURE WARNING IN FLIGHT. READ ZERO. OIL PRESSURE SENSOR FOUND INOPERATIVE.Feb 3, 2011 · N271CP · Cirrus SR22 · Engine Oil Indicating SystemSDR 2010FA0001221Support · brokenWITH ENGINES RUNNING, PILOT NOTICED PIECES COMING OUT OF SPINNER. DURING INSP, DISCOVERED THAT THE LT SPINNER SUPPORT WAS COMING APART. AND SEVERAL PIECES FELL ON THE GROUND. THE SPINNER WAS NOT PROPERLY SHIMMED CAUSING THE SPINNER SUPPORT TO BE LOOSE AND VINov 4, 2010 · N414AV · Cessna 414A · Propeller Spinner SectionSDR T9ZR725YWO4459Starter · out of toleranceDURING REMOVAL OF THE STARTER AND THE O/H OF THE STARTER DRIVE ADAPTER IT WAS FOUND THAT THE NEWLY INSTALLED STARTER IS .015 SMALLER AT THE HOUSING FLANGE THAN THE FACTORY INSTALLED STARTER. THE STARTER DRIVE ADAPTER WAS OBSERVED TO BE LEAKING OIL WERE THE STAFeb 26, 2010 · N728SM · Lancar LC41550FG · Engine StarterSDR MDR40120009004Tube · chafedTHE OIL FILLER TUBES ARE BEING CHAFED BEYOND MFG LIMIT OF .010 DUE TO CONTACT WITH THE CYLINDER BAFFLING BETWEEN CYLINDERS NR 2 AND 4. SHOULD THE TUBE CHAFE COMPLETELY THROUGH, AN OIL LEAK WILL OCCUR AND DEPENDING HOW MUCH THE ENGINE CASE IS PRESSURIZING, ALLApr 1, 2009 · N2522F · Lancar LC41550FG · Reciprocating Engine Oil SystemSDR 2009FA0000016Pan · crackedOIL LEAK CAME FROM CRACK IN OIL PAN. CAUSE UNKNOWN. ENG TSMOH 95 HRS. CRACK/ FITTING WITH HOSE ATTACHED FOR REMOTE OIL DRAIN. (K)Dec 17, 2008 · N414PS · Cessna 414A · Reciprocating Engine Oil SystemSDR 2008FA0000211Duct · crackedRT TURBO TRANSITION DUCT CRACKED. (NOTE: THIS IS THE SECOND TIME WE HAVE SEEN THIS)Mar 12, 2008 · Lancar LC41550FG · Engine (Reciprocating)SDR 2007FA0000877Alternator · failedA FLIGHT TEST WAS BEING CONDUCTED ON 07/30/07 ON A REWORKED THERMAL SYSTEMS (KATS) EVADE SYSTEM, WHEN THE SYSTEM WENT UNSTABLE CAUSING THE ALTERNATOR TO GO OFF LINE. THE TECHNICIAN MONITORING THE SYSTEM ON A DIAGNOSTIC LAPTOP COMPUTER ANNOUNCED TO THE PILOT TAug 7, 2007 · N376PD · Columb LC41550FG400 · AC Generation SystemSDR 2005FA0000839Frame · crackedBULKHEAD FRAME ASSY AT STA 272. CRACKED AT TOP PORTION LT AND RT IN BEND RADIUS, APPROX CRACK TO BE ABOUT .5 INCH ON LT AND 1 INCH ON RT. (K)May 17, 2005 · N8131H · Beech A36 · Fuselage Main, FrameSDR 98ZZZX3683Line · crackedCRACKED COOLANT LINE CAUSED LOSS OF COOLANT AND ENGINE SHUT DOWN. LOG BOOKS NOT AVAILABLE AT TIME OF THIS REPORT.Aug 20, 1998 · N300SQ · Cessna 414A · Engine Cooling SystemSDR 99ZZZX595Piston · crackedDURING FLIGHT, THE RIGHT ENGINE BEGAN TO RUN ROUGH AND LOST OIL PRESSURE. THE PILOT SECURED THE ENGINE AND MADE A SAFE SINGLE-ENGINE LANDING. AN INVESTIGATION REVEALED A CRACK IN THE PISTON. THIS CRACK STARTED FROM THE OIL CONTROL RING LANDING THROUGH THE CJul 7, 1998 · N12455 · Cessna 414A · Reciprocating Engine Cylinder Section
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