Lycoming T5313B

Service difficulty reports · 147

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 = 'T5313B'
  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 CA980922009Blade · cracked(CAN) DURING A FUEL STOP, ENGINEER FOUND CRACK IN BLADE. NO ABNORMAL FLIGHT CHARACTERISTICS. CRACK RUNS FROM THE INBOARD CORNER OF THE TRIM TAB, FORWARD TO THE SPAR AND THEN INBOARD ALONG THE SPAR FOR 6 INCHES. BELL ASB 205-96-67 IS BEING DONE DAILY, BUT THISep 10, 1998 · Bell 205A1 · Main Rotor BladesSDR CA980915001Cap · debonded(CAN) CAPS COMING OFF ON BOTH LT AND RT SKID TUBES. ADHESIVE PEELING OFF FROM CAP AND ADHESIVE WAS APPLIED OVER THE PAINTED TUBE.Sep 3, 1998 · Bell 205A1 · Main Landing Gear Strut/Axle/TruckSDR CA980908010Governor · failed(CAN) ROTOR RPM DROPS AND OVERSPEEDS WITH COLLECTIVE LEVER MOVEMENT. ADJUSTMENT OF DROOP COMPENSATOR TO MAXIMUM DID NOT SOLVE THE PROBLEM. GOVERNOR WAS REPLACED AND PROBLEM SOLVED.Aug 24, 1998 · Bell 205A1 · Turbine GovernorSDR CA980908009Battery · thermal runaway(CAN) BATTERY 'HOT' INDICATOR CAME 'ON'. BATTERY THERMAL RUNAWAY.Aug 22, 1998 · Bell 204B · Battery/Charger SystemSDR CA980629002Cross Tube · broken(CAN) WHILE DISEMBARKING PASSENGER AFTER LANDING WITH THE ROTOR STILL TURNING, A LOUD SNAP WAS HEARD ACCOMPANIED WITH A SUDDEN ROLLING OF THE HELO TO THE RIGHT. PILOT PREVENTED ANY FURTHER ROLL BY APPLYING CYCLIC AND AC FLOWN BACK TO BASE WHERE IT WAS SAFELY Jun 14, 1998 · Bell 205A1 · Main Landing Gear Strut/Axle/TruckSDR CA980616003Rod · broken(CAN) ROD END OUTER RACE FRACTURED LOSING 1/3 OF CIRCUMFERENCE AND RELEASING THE BALL. LOSS OF CONTROL OF ONE BLADE AND TAIL ROTOR AUTHORITY.Jun 8, 1998 · Bell 205A1 · Tail Rotor HeadSDR CA980616002Crosstube · broken(CAN) ON LIFTING 6 FUEL DRUMS ON A SHORT LANYARD, PILOT SAW IN THE SLING MIRROR THAT THE LANYARD HAD CAUGHT ON THE RT SKID TUBE. ON ATTEMPT TO LAND, IT BECAME EVIDENT THAT THE REAR CROSSTUBE HAD BROKEN AND THE LANDING WAS ABORTED, THE LOAD RELEASED AND HELO RMay 30, 1998 · Bell 205A1 · Main Landing GearSDR CA980602030Bearing · broken(CAN) CHIP DETECTOR WARNING LIGHT ILLUMINATED IN FLIGHT. AFTER LANDING INSPECTION OF THE CHIP DETECTOR SHOWED EXCESSIVE METAL CONTAMINATION. A MORE DETAILED INSPECTION FOUND THE NR 21 BEARING HAD A BROKEN BEARING CAGE. NO OTHER DAMAGE WAS FOUND.May 29, 1998 · Bell 205A1 · Turbine Engine Reduction GearSDR CA980602031Bevel Gear · broken(CAN) ON FIRE FIGHTING MISSION, 90 DEGREE CHIP LIGHT ON. AFTER LANDING, CHIP PLUG WAS HEAVILY CONTAMINATED. INPUT GEAR 212-040-450-001 S/N A13-02363 HAD BROKEN TEETH, BEVEL GEAR 212-040-451-001 S/N A13-03609 HAD BROKEN TEETH, G/B HOUSING 212-040-468-001 S/N AMay 29, 1998 · Bell 205A1 · Tail Rotor GearboxSDR 99ZZZX2907Solenoid · leakingDURING A FLIGHT TEST BY THE ROYAL AUSTRALIAN AIR FORCE, LEAKAGE WAS NOTED ON THE ENGINE. THE PART AND ITS HOST REGULATOR WOULD BE THE SAME AS THAT USED BY COMMERCIAL AIRCRAFT. THE AUSTRALIAN DEPOT PERFORMING THE INVESTIGATION FOUND THE END CAP OF THE SOLENOIDMay 21, 1998 · Engine Fuel PumpSDR CA980521006Support · cracked(CAN) CRACK FOUND ON ONE OF THE EARS WHICH MOUNTS THE LIFT LINK ASSY. CRACKED FROM BOLT HOLE TO EDGE.May 9, 1998 · Bell 205A1 · Main Rotor GearboxSDR CA980513002Clamp · cracked(CAN) CLAMP CRACKED AT BASE OF T-BOLT HEAD BAND.May 5, 1998 · Bell 204B · Powerplant SystemSDR CA980513003Mount · cracked(CAN) DURING INSPECTION OF THE DIFFUSER, THERE WERE CRACKS FOUND IN THE STRUTS.May 5, 1998 · Bell 204B · Turbine Engine Combustion SectionSDR CA980512002Bearing · overheated(CAN) AFTER 1.2 HOURS TSN, BEARING HOTTER THAN NORMAL. BEARING ASSY REMOVED. TEARDOWN REVEALED THE SEAL FACE HAD STARTED TO TURN BLUE. BEARING ITSELF WAS SMOOTH AND HAD NO ROUGH SPOTS.May 4, 1998 · Bell 205A1 · Tail Rotor Drive ShaftSDR 98ZZZX2880Shroud · crackedIT WAS NOTED DURING OPERATION, ENGINE EGT WAS OBSERVED TO BE ABOVE NORMAL. UPON TEARDOWN OF HOT SECTION, THE FIRST STAGE TURBINE NOZZLE OUTER SHROUD WAS FOUND SEVERELY CRACKED. (X)May 3, 1998 · N58HJ · Bell 205A1 · Turbine SectionSDR CA980421004Bearing · rough(CAN) VIBRATION FROM OIL COOLER BLOWER. BOTH BEARINGS DRY AND ROUGH RUNNING. BEARING SEALS BROKEN.Apr 9, 1998 · Bell 205A1 · Rotorcraft Cooling Fan SystemSDR CA980504001Blade · cracked(CAN) BLADE CRACKED ON BOTH SKINS AT 77.25 INCHES FROM TIP T/E. CRACK IS 15 INCHES CHORDWISE FORWARD FROM TRAILING EDGE THEN INBOARD 9 INCHES TOP AND BOTTOM.Apr 5, 1998 · Bell 205A1 · Main Rotor BladesSDR CA980305002Nut · loose(CAN) DURING DISASSEMBLY OF THE ENGINE DUE TO ICE INGESTION, THE CARRIER ASSEMBLY WAS PULLED. CLOSER INSPECTION REVEALED THAT THE BEARING RETAINING NUT WAS SPINNING FREE (NO TORQUE) ON HE GEARSHAFT, HELD BY ONLY ONE TANG OF THE KEYWASHER. THE GEAR IN QUESTION Feb 25, 1998 · Bell 205A1 · Turbine Engine Accessory DriveSDR CA980403008Tube Assembly · broken(CAN) TUBE ASSEMBLY, PURGE SYSTEM, FOUND BROKEN AT THE BRAZING. THIS ASSEMBLY IS IN THE FUEL STARTING SYSTEM.Dec 28, 1997 · Bell 205A1 · Engine Fuel DistributionSDR CA971231024Fuel Cell · peeling(CAN) WHEN RIGHT HAND FUEL SUMP DRAINED, BLACK PARTICLES WERE FOUND. RUBBER COATING OF THE FUEL CELL HAD PEELED OFF.Nov 5, 1997 · Bell 205A1 · Fuel StorageSDR 97ZZZX4823Oil Pump · failedPILOT REPORTED LOSS OF OIL PRESSURE IN-FLIGHT. THE FLIGHT WAS TERMINATED IMMEDIATELY AND THE ENGINE WAS SHUT DOWN. UPON INVESTIGATION, THE ENGINE OIL PUMP DRIVESHAFT WAS FOUND BROKEN. WHEN PUMP WAS REMOVED, A PIECE OF GEAR TOOTH FELL FROM PUMP OIL PASSAGE. Oct 18, 1997 · N58HJ · Bell 205A1 · Turbine Engine Oil SystemSDR CA970916001Spar · cracked(CAN) FOUND CRACK ORIGINATING FROM A RIVET HOLE TO THE EDGE OF THE SPAR AND ANOTHER CRACK FROM RIVET HOLE INBOARD PER AD 97-18-01.Aug 25, 1997 · Bell 205A1 · Rotorcraft Tail BoomSDR CA970902013Beam · cracked(CAN) TAIL BOOM ATTACHMENT POINT T-CAP BEAM FOUND CRACKED. SOME RIVETS ALSO SHEARED. CRACK WAS ALONG TWO HI-SHEAR RIVET HOLES.Aug 21, 1997 · Bell 204B · Rotorcraft Tail BoomSDR CA970526001Actuator Lever · worn(CAN) DURING INSPECTION EXCESSIVE PLAY WAS FOUND ON THE INLET GUIDE VANES. FURTHER INSPECTION FOUND THE STRUT PIN HOLES WERE WORN.May 14, 1997 · Bell 205A1 · Turbine Engine Compressor SectionSDR CA970115002Blower · rough bearing(CAN) BEARINGS IN OIL COOLER BLOWER SOUND ROUGH AND DRY WHEN FAN IS TURNED BY HAND. BLOWER REMOVED AND BEARINGS REPLACED.Jan 7, 1997 · Bell 204B · Rotorcraft Cooling Fan SystemSDR CA970213010Elevator · cracked(CAN) 3 CRACKS WERE FOUND ON TOP SURFACE OF ELEVATOR. 2 CRACKS APPROXIMATELY 1" LONG AND 1 CRACK 6" LONG.Jan 5, 1997 · Bell 204B · Elevator, Plate/SkinSDR CA970114002Gp Section · damaged(CAN) AIRCRAFT LANDED AND ENGINE WAS SHUTDOWN. ON THE NEXT START THE ENGINE WAS GOING TO A HOT START, SO THE START WAS ABORTED. ON THE SECOND START ATTEMPT AN ENGINE VIBRATION WAS FELT AND THE EGT BEGAN TO RISE RAPIDLY AND COULD NOT BE CONTAINED BY CUTTING OFFDec 27, 1996 · Bell 205A1 · Turbine SectionSDR CA960916007Skin · debonded(CAN) MAIN ROTOR BLADE UPPER AND LOWER SKINS DEBONDED FROM TRAILING EDGE EXTRUSION FOR 66 INCHES FROM THE TIP INBOARDSep 9, 1996 · Bell 205A1 · Main Rotor BladesSDR CA960919006Engine · failed(CAN) THE HELICOPTER WAS ON THE INITIAL GROUND RUN AFTER A 1000 HOUR INSPECTION. THE AIRCRAFT WAS RUNNING IN FLIGHT IDLE FOR APPROXIMATELY 10 MINUTES AND ALL PARAMETERS WERE NORMAL. THE PILOT ACCELERATED THE ENGINE TO MAX POWER TURBINE (N2) SPEED TO ESTABLISH Sep 6, 1996 · Bell 205A1 · Engine (Turbine/Turboprop)SDR CA960909008Regulator · malfunction(CAN) ON STARTUP, LOADMETER SPIKES WHEN GENERATOR TURNED ON, THEN LOAD STAYS HIGHER THAN NORMAL FOR A LONG TIME. VOLTAGE REGULATOR REPLACED.Aug 24, 1996 · Bell 204B · DC RegulatorSDR CA960909023Fitting · cracked(CAN) LIFT BEAM ASSEMBLY FITTING CRACKED AT THE HOLE ON THE AFT EAR.Aug 24, 1996 · Bell 205A1 · Fuselage Miscellaneous StructureSDR CA960909002Blade · cracked(CAN) BLADE TOP SKIN CRACKED AT STATION 203 5 CRACKED APPROXIMATELY 6 INCHES FROM SPAR REARWARDAug 22, 1996 · Bell 205A1 · Main Rotor BladesSDR CA961112040Diffuser · cracked(CAN) EXHAUST DIFFUSER RECEIVED FOR INSPECTION, 4" X 1" METAL BREAK-OFF AND 2" CIRCUMFERENTIAL CRACK FOUND ON FORWARD FACE OF THE INNER CONE. CAUSE OF CRACK AND BREAK IS UNKNOWN.Jul 30, 1996 · Engine Collector/Tailpipe/NozzleSDR CA960802003Bearing · rough(CAN) HIGH TO MEDIUM FREQUENCY VIBRATION WAS BEING DETECTED BY THE PILOT THROUGH THE TAIL ROTOR PEDALS. EXAMINATION FOUND BLOWER ASSEMBLY MAKING VIBRATION. REPLACED ASSEMBLY AND RECTIFIED PROBLEM.Jul 27, 1996 · Bell 204B · Rotorcraft Cooling Fan SystemSDR CA960412003Fan · bearing failed(CAN) TURBINE AND FAN ASSEMBLY MAKING NOISE AND VIBRATION. BEARING P/N 9101 PP FOUND DRY.Apr 1, 1996 · Bell 204B · Rotorcraft Cooling Fan SystemSDR CA960412010Drag Brace · cracked(CAN) DURING A SCHEDULED 1200 HOUR INSPECTION OF THE DRAG BRACE ASSEMBLY, THE NUT 204-011-144-003 WAS FOUND TO HAVE A LONGTITUDINAL CRACK ACROSS THE OUTSIDE SURFACE.Apr 1, 1996 · Bell 205A1 · Main Rotor HeadSDR CA960329003Engine · failed(CAN)N2 FAILURE, N2 INDICATOR FLUCTUATED, NR ENGINE WARNING ON.Mar 22, 1996 · Bell 205A1 · Engine (Turbine/Turboprop)SDR CA960418002Retainer · broken(CAN)LOCKING TANG OF CUP WASHER RETAINER BROKEN. NUT LOST TORQUE AND FELL-OFF FROM GEARSHAFT CAUSING GEAR TO SHIFT AND DISENGAGE INTERMITTENTLY. NUT AND RETAINER FROUND IN NOSE HOUSING.Mar 22, 1996 · Bell 205A1 · Engine (Turbine/Turboprop)SDR CA960205010Engine · faulty(CAN)N2 FAILURE. #N2 INDICATION. CHIP DETECTOR LIGHT CAME ON. METAL FOUND IN AIRFRAME OIL FILTER. NO METAL IN ENGINE FILTER.Jan 29, 1996 · Bell 205A1 · Engine (Turbine/Turboprop)SDR CA960227011Spur Gear · broken(CAN) ENG ACCESSORY DRIVE FAILED. ENGINE REPAIRED.Jan 29, 1996 · Bell 205A1 · Turbine Engine Accessory DriveSDR CA960206101Bolt · sheared(CAN)THE DRIVE LINK WAS BEING REMOVED TO REPLACE THE TRUNNION BEARING IN THE SWASHPLATE OUTER RING ASSEMBLY. THE BOLT HEAD SHEARED OFF UPON DISASSEMBLY.Dec 29, 1995 · Bell 205A1 · Main Rotor HeadSDR CA960123101Drive · failed(CAN)ENGINE HAD CATASTROPHIC FAILURE, AIRCRAFT DESTROYED. ACCIDENT HAPPENED IN AUSTRALIA AND IS BEING INVESTIGATED BY BUREAU OF AIR SAFETY INVESTIGATION, FILE #9504205. PRELIMINARY OBSERVATIONS INDICATE FA ILURE OF N2 GEARBOX DRIVE.Dec 13, 1995 · Bell 205A1 · Turbine Engine Accessory DriveSDR CA951209103Diffuser Housing · cracked(CAN)ON DAILY INSPECTION IT WAS FOUND THAT THE PAN HAD CRACKED AROUND THE INSERT.Nov 20, 1995 · Bell 205A1 · Engine Mount SectionSDR CA951209104Diffuser Housing · cracked(CAN)ON DAILY INSPECTION IT WAS FOUND THAT THE PAN HAD CRACKED AROUND THE INSERT.Nov 20, 1995 · Bell 205A1 · Engine Mount SectionSDR 95ZZZX6242Impeller · failedDURING ENGINE OPERATION, CENTRIFUGAL COMPRESSOR IMPELLER FAILED CAUSING UNCONTAINED PARTS EXITING FROM ENGINE COMPRESSOR SPOOL CORE DURING FLIGHT. THIS UNCONTAINED FAILURE RESULTED IN POWERPLANT POWER SHUT DOWN WITH RESULTANT HARD LANDING OF AIRCRAFT. RECOMMSep 18, 1995 · N70410 · Bell UH1L · Turbine Engine Compressor SectionSDR CA960311003Gp Module · burned(CAN) ENGINE GP AND POWER TURBINE NOZZLE AND WHEEL BURNED. ALL ACCESSORIES SUCH AS NOZZLES. FCU, GOVERNOR, BLEED BAND, AIR VALVE WERE SENT FOR TEST AND HAVE TESTED SERVICEABLE. NO EROSION OR FOD FOUND ON COMPRESSOR ASSEMBLY. NO DAMAGE OR FAILURE FOUND ON ANY BAug 25, 1995 · Bell 204B · Turbine SectionSDR CA960122015Spur Gear · broken(CAN)SPUR GEAR BROKEN IN TWO PIECES.Jul 17, 1995 · Bell 205A1 · Turbine Engine Accessory Drive
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