U/A Canada PT6A-28

Service difficulty reports · 944

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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 = 'PT6A28'
  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 CA140918002Turbine · failed(CAN) REPORT EIR PT6A 2014-078, ENGINE WAS SENT FOR REPAIR AFTER THE OPERATOR REPORTED THAT THE ENGINE FAILED IN FLIGHT. THE OPERATOR REPORTED THAT THE PT BLADES WERE MISSING WHEN LOOKING IN THE EXHAUST PORTS AFTER THE FAILURE.Sep 17, 2014 · Beech A100 · Turbine SectionSDR CA140922012Torque Knee · broken(CAN) AFTER TOUCHDOWN THE PILOTS FELT A VIBRATION AND THE AIRCRAFT WANTING TO TURN TO THE RIGHT. AIRCRAFT STOPPED THEN TAXIED TO THE RAMP AND IT WAS FOUND THAT THE RIGHT HAND MAIN LANDING GEAR UPPER TORQUE LINK WAS FOUND BROKEN OFF (SEE PIC) THE TORQUE LINK WASep 16, 2014 · Beech A100 · Main Landing GearSDR CA140904001Torque Tube · cracked(CAN) DURING SCHEDULED VISUAL INSPECTION OF THE ELEVATOR TORQUE TUBE A CRACK WAS FOUND COMMING FROM UNDER THE BUSHING ON THE FLANGE THAT ATTACHES TO THE ELEVATOR. (SEE ATTACHED PICS) TUBE REPLACED AND CHECKED SERVICEABLE.Aug 25, 2014 · Beech A100 · Elevator Control SystemSDR CA140809001Blade · sheared(CAN) LEFT ENGINE FAILED IN FLIGHT. POWER TURBINE BLADES FOUND SHEARED, POWER TURBINE GUIDE VANES DAMAGED, ENGINE BEING REMOVED AND SENT TO OVERHAUL SHOP FOR INVESTIGATION.Aug 7, 2014 · Beech A100 · Turbine SectionSDR KCQA2014F00139Module · defectivePILOT PRIMARY FLIGHT DISPLAY (PFD), AVIONICS EFD1000C3 LOST ALL ATTITUDE AND DIRECTION DATA IN FLIGHT. AFTER LANDING ON SUBSEQUENT POWER ON CYCLES THE PFD POWER ON SELF TEST/INITIALIZATION PAGE DISPLAYED "RSM FAIL 4 CHECK LINK".Aug 4, 2014 · N899CZ · Beech 99A · Attitude and Direction Data SystemSDR CA140625003Governor · failed(CAN) DURING CRUISE THE RT PROPELLER RPM STARTED TO DROP AND TORQUE WENT UP. THIS STARTED TO FLUCTUATE UP AND DOWN. THE CREW FEATHERED THE PROPELLER AND SHUTDOWN THE ENGINE. THEY DIVERTED E THEY LANDED WITH NO ISSUES. AFTER INSPECTION THE PROP GOVERNOR WAS FOJun 24, 2014 · Piper PA31T · Propeller GovernorSDR CA140620012Torque Tube · corroded(CAN) TORQUE TUBE FOUND CORRODED AND PUNCTURED.Jun 19, 2014 · Beech A100 · Elevator StructureSDR CA140530002Exciter · failed(CAN) UNIT FAIL TO PRODUCE SHOWER SPARK TO IGNITER, NO ELECTRICAL POWER OUTPUT. UNIT WAS O/H AT NORMAL TBO 3500 HRS.May 28, 2014 · Beech A100 · ExciterSDR CA140530003Exciter · failed(CAN) UNIT FAIL, NO ELECTRICAL OUTPUT.May 27, 2014 · Beech A100 · ExciterSDR CA140527003Washer · damaged(CAN) DURING ROUTINE INSPECTION, THE KEY WASHER TO INSTALL THE NOSE WHEEL WAS FOUND ELONGATED AND SPUN, WITH COMPARISON TO NEW WASHER. WASHER WAS REPLACED THREADS ON NOSE GEAR INSPECTED AND RETURNED TO SERVICE.May 23, 2014 · Beech A100 · Nose/Tail Landing Gear Strut/AxleSDR CA140521002Connector · broken(CAN) INTERIOR NEON BALLAST, BURNED DUE TO CONNECTOR ALIGNMENT NOTCH MISSING/BROKEN INSIDE OF CONNECTOR. THIS ALLOW CONNECTOR TO MOVE AND CREATE A SHORT.May 20, 2014 · Beech A100 · Light System WiringSDR CA140505013Torque Tube · cracked(CAN) DURING SCHEDULED VISUAL INSPECTION OF THE ELEVATOR TORQUE TUBE A CRACK WAS FOUND. THIS MAY HAVE BEEN THE RESULT OF OVER-TORQUEING THE SCREW ATTACHING THE TUBE TO THE ELEVATOR. TUBE REPLACED AND CHECKED SERVICEABLE.Apr 25, 2014 · Beech A100 · Elevator StructureSDR CA140417010Hinge · loose(CAN) DURING A SCHEDULED PHASE INSPECTION THE LT AND RT OTBD ELEVATOR HINGES WERE FOUND TO BE LOOSE WHERE THEY ATTACH TO THE HORIZONTAL STABILIZER. THE ATTACHMENT BOLTS WERE REPLACED WITH NEW, 4 EACH LOCATION AND SECURED. THE OTHER HINGE LOCATIONS HAD NO DEFEApr 16, 2014 · Beech 100BEECH · Elevator StructureSDR CA140417012Duct · cracked(CAN) NOTED A SHIFT IN ENGINE TRENDS ITT AND FUEL FLOW INCREASE. VISUAL INSPECTION PERFORMED. VIEWED THROUGH EXHAUST STACKS. NOTED TURBINE EXHAUST DUCT IN THE SKI JUMP AREA WAS CRACKED AND SPLIT OPEN. NR 3 BEARING COVER LOOSE AND RUBBING ON POWER TURBINE DISApr 16, 2014 · Beech 100BEECH · Turbine SectionSDR CA140602022Cap · unsecure(CAN) THE PILOT REPORTS THAT AT THE SECOND TAKEOFF OF TRAINING JUST AFTER SETTING MAX TAKE-OFF POWER AT ABOUT 40-45 KTS, THEY HEARD A SOUND FROM THE ENGINE THAT IT HAD FALL IDLE. PILOT NOTES FEELING THE ACFT SHIFTING TO THE LT. THE CO-PILOT, PNF, NOTICED THEApr 5, 2014 · Beech A100 · Turbine Engine Oil SystemSDR CA140327006Downlock · broken(CAN) ON TAKEOFF THE LANDING GEAR FAILED TO FULLY RETACT, WHEN THE GEAR WAS EXTENDED THE RT GEAR FAILED TO LOCKDOWN, THE SOP`S WERE FOLLOWED, GEAR EMERGENCY BOTTLE WAS BLOWN BUT THE RT GEAR SLOWLY COLLAPSED ON LANDING. THE DOWN LOCK HOOK WAS FOUND TO BE BROKENMar 25, 2014 · Beech A100 · Landing Gear Retraction/Extension SystemSDR CA140305001Stator · cracked(CAN) THREE CRACKS FOUND ON OUTER RING WHEN INSPECTING BY BORESCOPE IN NOZZLE HOLES PARTS REMOVED FOR OVERHAUL AND REPLACED.Feb 10, 2014 · Beech A100 · Turbine SectionSDR CA140110010Boot · split(CAN) DURING INSPECTION, THE TAIL DE-ICE BOOTS DID NOT INFLATE DURING OPS TEST. INVESTIGATION NOTED THE TUBE SUPPLYING AIR PRESSURE TO THE RT HORIZONTAL STABILIZER DE-ICE BOOT HAD SPLIT APPROXIMATELY .8750" LONG. THE SPLIT OCCURED AT THE END OF THE HOSE THAT Jan 9, 2014 · Beech 100BEECH · Air Intake Anti/De-Ice SystemSDR CA131218006Panel · corroded(CAN) WHEN DOING AN INSPECTION, A TECH FOUND A FUEL LEAK UNDER THE RT NACELLE FUEL TANK. CLEAN THE PANEL UNDER THE TANK AND A STREAM OF FUEL START TO FLOW. EMPTIED THE TANK TO REMOVE THAT PANEL AND FOUND THAT THE PANEL WAS SO CORRODED THAT A HOLE PUNCTURED Dec 17, 2013 · Beech A100 · Fuel StorageSDR CA131129005Control Horn · cracked(CAN) WHILE DOING A PHASE INSPECTION ON THE TAIL SECTION, AN EMPLOYEE FOUND SOME LOOSENESS ON THE LT CONTROL HORN ASSY. THE LT ELEVATOR ASSY HAS BEEN REMOVED TO LOOK AT THE THE BEARING CONDITION. THE BEARING WAS IN GOOD CONDITION AND THE LOOSENESS WAS COMING FNov 28, 2013 · Beech A100 · Elevator Miscellaneous StructureSDR CA131115001Drive Assy · failed(CAN) WHILE BACK TRACKING ON THE RUNWAY, FLAPS WE RETRACTED BY FLIGHT CREW AND SHORTLY AFTER A BURNING ODOR WAS NOTICED IN THE CABIN. THE ACFT RETURNED TO THE APRON AND PASSENGERS WERE DEPLANED. THE FLIGHT CREW VISUALLY NOTED THAT THE RT INBD FLAP WAS IN THENov 12, 2013 · Beech A100 · Trailing Edge Flap Control SystemSDR CA130925001Wire · shorted(CAN) AFTER EXTENSION OF THE LANDING GEAR THERE WAS NO DOWN INDICATION, 3 GREEN. PILOTS COULD HEAR THE LANDING GEAR EXTEND AND COULD FEEL THE PARASITE DRAG BUT NO INDICATION. PILOTS CONTACTED EMERGENCY SERVICES AND LANDED THE ACFT WITHOUT INCIDENT. MAINTENANSep 21, 2013 · Beech A100 · Landing Gear System WiringSDR CA130920002Torque Knee · sheared(CAN) THE FLIGHT CREW FELT A VIBRATION FROM THE RT MLG UPON LANDING. POST FLIGHT WALK AROUND REVEALED THAT THE UPPER TORQUE KNEE ON THE RT MLG HAD SHEARED.Sep 17, 2013 · Beech A100 · Main Landing GearSDR CA131103007Indicator · failed(CAN) ON CLIMBOUT THE CREW NOTICED THE RT ATTITUDE GYRO HAD BECOME UNSERVICEABLE. THE FLIGHT CONTINUED WITH OUT INCIDENT TO DESTINATION. MAINTENANCE REPLACED THE GYRO AND THE SYS WAS GROUND FUNCTION CHECKED SERVICEABLE.Sep 14, 2013 · Beech A100 · Attitude and Direction Data SystemSDR CA130911005Skin · cracked(CAN) DURING A PHASE 3 INSPECTION, A CRACK WAS FOUND ON THE LT HORIZONTAL STABILIZER UPPER SURFACE. THERE WAS OIL CANNING ON THE UPPER SKIN, NEAR THE CRACK WHICH INDICATE PROBABLE DAMAGE AT THE RIB. DURING REPAIR, NO RIB WERE FOUND DAMAGED BUT ON SKIN STIFFESep 10, 2013 · Beech A100 · Horizontal Stabilizer, Plate/SkinSDR CA130906001Clevis · broken(CAN) UPON RETRACTION TEST, DURING PHASE 1 INSPECTION, MAINTENANCE PERSONNEL NOTICED THAT THE BOLT, PN AN24-23A, ATTACHING THE DRAG LEG TO THE RETRACTION ACTUATOR FORK WAS TOO LONG, NOT SEATING AGAINST THE YOKE. WHILE TRYING TO REMOVE THE BOLT, IT WAS FOUND BSep 3, 2013 · Beech A100 · Nose/Tail Landing Gear Strut/AxleSDR CA130808001Torque Shaft · corroded(CAN) ELEVATOR TORQUE SHAFT VISUAL INSPECTION INDICATED SOME CORROSION ON THE BOTTOM OF THE SHAFT AFTER REMOVAL IT WAS DISCOVERED THAT CORROSION HAD CREATED MULTIPLE HOLES IN THE SHAFT. NOTE THIS SHAFT GETS WET AFTER RAIN OR AIRCRAFT WASHING AND MAY STAY SUSPAug 7, 2013 · Beech A100 · Elevator StructureSDR CA131103006Radar · failed(CAN) THE CREW NOTED THAT THE RADAR DISPLAY WOULD POSSIBLY PAINT INACCURATE IMAGES OF THE WEATHER SYSTEMS. MAINTENANCE INVESTIGATED THE PROBLEM TO BE IN THE DISPLAY MONITOR. THE UNIT WAS REPLACED AND THE SYS GROUND FUNCTION CHECKED SERVICEABLE.Jul 4, 2013 · Beech A100 · Weather Radar SystemSDR CA130704003Diaphragm · torn(CAN) DURING APROACH, THE PILOT FOUND THAT THE LT ENGINE POWER WAS LOW. AFTER A GROUND RUN IT APPEAR THAT THIS ENGINE WAS UNDER POWER. BLEED VALVE HAS BEEN REMOVE AND THE DIAPHRAGM FOUND TEAR WERE IT NORMALLY BEND. PART HAS BEEN REPLACE AND ACFT RETURN IN SJun 20, 2013 · Beech A100 · Compressor Bleed ValveSDR CA130606007Exhaust Duct · cracked(CAN) EXHAUST DUCT INNER SECTION CRACKED, THREAD AT TURBINE EXIT, AT BEARING NR 3, THIS CAUSE THE TO DAMAGE THE T/E OF TURBINE BLADE.Jun 4, 2013 · Beech A100 · Engine Collector/Tailpipe/NozzleSDR CA130607002Gear · damaged(CAN) DURING A PHASE INSPECTION WHILE COMPLETING THE LANDING GEAR SWINGS THE RT GEAR ACTUATOR WAS MAKING AN UNUSUAL NOISE. THE ACTUATOR WAS REPLACED AND TESTED SERVICEABLE. UPON DISASSEMBLE OF THE ACTUATOR THE GEAR TEETH WERE FOUND TO BE CHIPPED AND BROKEN.Jun 4, 2013 · Beech A100 · Landing Gear ActuatorSDR CA130524003Gyro · failed(CAN) AFTER REPLACEMENT OF DISPLACEMENT GYRO, FLIGHT CREW NOTIFIED MAINTENANCE THAT THE ATTITUDE INDICATOR INFORMATION WAS BACKWARDS. MAINTENANCE FOUND THE FORWARD POINTING ARROW ON THE COVER OF THE UNIT WAS INSTALLED BACKWARDS. THIS ARROW IS TO GUIDE THE INMay 23, 2013 · Beech E90 · Attitude Gyro and Indicating SystemSDR CA130603005Oil System · low pressure(CAN) THE PILOT REPORTED A RT ENGINE OIL PRESSURE FLUCTUATION IN FLIGHT AND AN OIL PRESSURE DECREASE UP TO 40 PSI WHEN THE LOW OIL PRESSURE ALARM LIGHT ON. PILOT ELECTED TO SHUTDOWN THE RT ENGINE. THE ON GROUND INVESTIGATION EVEALED OIL STAINS ON THE ENGINE May 19, 2013 · Engine Oil PressureSDR CA130430021Torque Tube · cracked(CAN) OUTBOARD CASTING CRACKED FROM TAPER PIN HOLE TO EDGE VISUAL INSPECTION COMPLETE TORQUE TUBE ASSEMBLY.Apr 29, 2013 · Beech A100 · Elevator Control SystemSDR CA130422012Spar · damaged(CAN) ON A ROUTINE NDT WING FITTING INSPECTION (AS PER THE SIRM), IT WAS FOUND THAT THE FASTENERS THAT HOLD THE FITTING ON THE SPAR HAD WORKED LOOSE AND HAD BEEN "SMOKING". IN ORDER TOO INVESTIGATE FURTHER, THE WINGS HAD TO BE REMOVED AS WELL AS THE WING END RApr 10, 2013 · Beech A100 · Wing SparSDR CA130412005Shaft · worn(CAN) WHILE DOING PHASE INSPECTION MAINTENANCE CARRIED OUT INSPECTION OF THE STARTER/GENERATOR DRY SPLINE AND FOUND IT TO BE CLOSE TO LIMITS. ENGINE WAS REMOVED, ACCESSORY GEARBOX SPLIT, GEARSHAFT, PN 3021565. REMOVED AND O/H GEARSHAFT INSTALLED. ENGINE REIApr 9, 2013 · Beech A100 · Accessory GearboxesSDR CA130409010Door Frame · cracked(CAN) PILOTS REPORTED LOUD NOISE COMING FROM EMERGENCY EXIT. WHEN ENGINEER REMOVED EMERGENCY EXIT, FOUND CRACK ACROSS MIDDLE 2 LIGHTNING HOLES WHICH SPAN THE CENTER STOP. FRAME WAS REPLACED.Mar 30, 2013 · Beech 100BEECH · Fuselage Main, StructureSDR CA130328008Contact · corroded(CAN) AFTER TAKEOFF, PILOT SELECTED GEAR UP, GEAR DID NOT RETRACT, PILOT SELECTED GEAR HANDLE BACK TO DOWN POSITION AND CONTINUED TO DESTINATION. UPON INSPECTION BY MAINTENANCE FOUND LANDING GEAR REMOTE CIRCUIT BREAKER RELAY CONTACTS EXTREMELY PITTED. RELAY Mar 25, 2013 · Beech A100 · Landing Gear System WiringSDR CA130325018Arm · broken(CAN) PILOT REPORTED THAT THE ACFT WAS HARD TO STEER. MAINTENANCE FOUND THE PILOTS RT RUDDER PEDAL ARM HAD BROKEN OFF WHERE THE PEDAL IS ATTACHED TO THE ARM. THE ARM WAS REPLACED AND THE ACFT WAS RETURNED TO SERVICE. NOTE: THERE IS AN INSPECTION FOR THIS INMar 21, 2013 · Beech A100 · Rudder Control SystemSDR CA130322009Tube · cut(CAN) DURING LT HORIZONTAL STABILIZER DEICE BOOT REPLACEMENT, MAINTENANCE FOUND THE LT DEICE BOOT PLASTIC SUPPLY LINE CUT/WORN APPROXIMATELY 75 PERCENT OF WAY THROUGH WHERE THE TUBE PASSES FROM THE TAIL SECTION THROUGH THE HORIZONTAL STABILIZER STRUCTURE.Mar 20, 2013 · Beech 100BEECH · Airfoil Anti/De-ice SystemSDR CA130307005Wire Harness · damaged(CAN) AIRCRAFT TURNED BACK SHORTLY AFTER TAKEOFF BECAUSE OF ITT INDICATION DROP TO 220 DEGREES. ENGINE SPLIT AND T5 THERMOCOUPLE HARNESS BLOCK WIRING FOUND INTERMITTENT, WHERE PEN SHOWS ON PIC, WHEN MOVED BY HAND HARNESS BLOCK REPLACED BY O/H UNIT.Mar 5, 2013 · Beech A100 · Engine Indicating System WiringSDR CA130402009Light · malfunctioned(CAN) ON A ROUTINE FLIGHT FROM THE CREW WAS IN THE CLIMBOUT WHEN THE CO-PILOT ADJUSTED THE COCKPIT LIGHTING FROM DIM TO BRIGHT. ALMOST IMMEDIATELY THE CREW EXPERIENCED SMOKE AND FUMES IN THE COCKPIT, THE CREW ELECTED TO RETURN TO DEPARTURE AND LANDED WITHOUT Feb 11, 2013 · Beech A100 · Flight Compartment LightingSDR CA130211004Motor · failed(CAN) UPON LANDING, THE FLIGHT CREW NOTICED SMOKE BUILDING IN THE PASSENGER CABIN. THE ACFT WAS STOPPED ON THE RUNWAY, THE CIRCUIT BREAKER FOR THE FLAP MOTOR WAS PULLED AND ALL POWER AND ENGINES WERE SHUTDOWN. MAINTENANCE PERSONNEL FOUND THE FLAP MOTOR TO BE Feb 8, 2013 · Beech A100 · Trailing Edge Flap ActuatorSDR CA130129009Blower · smoke(CAN) VENT BLOWER WAS PRODUCING SMOKE, TURNED OFF VENT BLOWER AND SMOKE STOPPED.Jan 24, 2013 · Beech 100BEECH · Cabin Cooling SystemSDR CA130124002Motor · inoperative(CAN) ON FINAL, CREW ATTEMPTED TO LOWER LANDING GEAR WITHOUT SUCCES. OVERSHOOT WAS INITIATED, LANDING GEAR EXTENDED MANUALLY AND UNEVENTFULL LANDING FOLLOWED. MAINTENANCE DISCOVERED LDG MOTOR WORKING ONLY IN RETRACT MODE. UNABLE TO LOWER LDG ON JACKS. LDG MOJan 22, 2013 · Beech A100 · Landing Gear ActuatorSDR CA130402008Rmi · malfunctioned(CAN) ON A ROUTINE FLIGHT, ON APPROACH THE CREW NOTICED THE RMI NOT PROPERLY INDICTING IN THE CO-PILOT SIDE. THE CAPTAIN CARRIED OUT THE LANDING FROM THE LT SIDE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A DEFECTIVE RMI, THE UNIT WAS REPLACED WITH AN O/H UJan 22, 2013 · Beech A100 · Navigation SystemSDR CA130115004Computer · failed(CAN) PITCH TRIM COMPUTER HAS A 3 AMP FUSE INSTALLED. THE PITCH TRIM MOTOR IS RATED TO DRAW UP TO 6 AMPS UNDER HEAVY LOAD SITUATIONS. ANY TIME PITCH MOTOR DRAWS HEAVY LOAD, INTERNAL PITCH COMPUTER 3 AMP FUSE BLOWS, DISABLING AUTO PILOT SYSTEM. THE MFG IS AWAJan 15, 2013 · Beech A100 · Autopilot ComputerSDR CA130109007Limit Switch · failed(CAN) 50 AMP CIRCUIT BREAKER TRIPPED WHEN CYCLING LANDING GEAR. FOUND GEAR LIMIT SWITCH IN FLOOR HAD FAILED COMPLETELY, BOTH SWITCHES REPLACED AND ADJUSTED IAW SERVICE MANUAL, GEAR CYCLE CHECK OK , NO PROBLEMS FOUND.Jan 8, 2013 · Beech 65A901 · Landing Gear Retraction/Extension SystemSDR CA130107002Light · burned(CAN) SHORT CIRCUIT ON WHEAT LIGHT AT LT LOWER CORNER OF PITCH TRIM CIRCUIT BOARD ASSY. FOLLOWING THE SHORT CIRCUIT, SMOKE COMMING OUT FROM AREA OF ELEVATOR TRIM SWITCHES DUE TO MELTING OF PLASTIC OF EDGE LIGHTED PANEL, PN: 97-524047. CAUSING SUBPANEL LIGHT CDec 20, 2012 · Beech 100BEECH · Indicating/Recording SystemSDR CA121228006Engine · shutdown(CAN) THE ACFT SUFFERED AN IFSD OF 1 ENGINE UNDER UNKNOWN CIRCUMSTANCES. COMPRESSOR DAMAGE WAS REPORTED. MFG WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENT THE REPORT ONCE THE INFORMATION IS AVAILABLE.Dec 15, 2012 · Beech B99 · Engine (Turbine/Turboprop)
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