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 CA110802009Rib · crackedDURING INSP, FRETTING (SMOKING) WAS FOUND TO BE COMING FROM BETWEEN THE ELEVATOR TORQUE TUBE AND THE INBD RIB THAT THE TUBE ATTACHES TO. AFTER DISASSEMBLY, CRACKS WERE FOUND IN THE RIB AND DOUBLER. BOTH ELEVATORS HAVE SIMILAR DAMAGE.Aug 2, 2011 · Beech E90 · Elevator, Spar/RibSDR CA110623008Stringer · crackedDURING 3000 CYCLE INSPECTION ON ACFT, MX CREWS FOUND A CRACK ON THE NR 10 STRINGER ON RT SIDE AT ZEE CHANNEL ATTACH AFT OF REAR PRESSURE BULKHEAD. AN APPROVED REPAIR WAS CARRIED OUT.Jun 22, 2011 · Beech A100 · Fuselage Main, Longeron/StringerSDR CA110623009Door Frame · crackedDURING 3000 CYCLE AIRFRAME INSPECTION, MX CREWS FOUND CRACKS ON AFT PASSENGER DOOR FRAME, PN 50-430043-865 FROM LOWER AFT LOCKING PIN TO THE PIN MOUNTING SCREWS. DOOR WAS REMOVED AND DISASSEMBLED. CRACKS WERE ALSO FOUND AT THE LOWER HINGE ATTACH CHANNEL PN 50Jun 22, 2011 · Beech A100 · Fuselage Main, StructureSDR JIKA11062101Engine · malfunctionedAPPROXIMATELY 20 NM NORTH OF GORMAN AT 11,000 MSL, THE PILOT REPORTED A LOUD "BANG" FROM THE RIGHT ENGINE, FOLLOWED BY "AN INTENSE SHOWER OF SPARKS" COMING FROM THE FWD AREA OF THE ENGINE, APPARENTLY THE EXHAUST. THE PILOT PULLED THE FIREWALL SHUT-OFF, AND COJun 21, 2011 · N1924T · Beech B99 · Engine (Turbine/Turboprop)SDR CA110617009Bolt · crackedLOWER FOREWARD LT WING BOLT FOUND CRACKED DURING INSP SIRM 57-16-01, ITEM 10. THE AVIA DESIGN FRONT WING KIT IS INSTALLED ON THIS ACFT. TOTAL TIME ON THIS BOLT IS 12331.0 HOURS AND 12 YEARS, LIFE LIMIT ON THIS BOLT IS 15000 HOURS OR 15 YEARS.Jun 17, 2011 · Beech A100 · Wing StructureSDR CA110609001Blade · failedEIR PT6A 2011-051 CONFIRMED INTERNAL ENGINE FAILURE. THE INTERNAL ENGINE FAILURE WAS CAUSED BY A CT BLADE FAILURE. THE BLADE FAILED AT THE LAST FIRTREE SERRATION CAUSING HEAVY IMPACT DAMAGE OF THE SHROUD AND ITS HSG AND ALSO CAUSING HEAVY IMPACT DAMAGE OF THEJun 6, 2011 · Turbine SectionSDR CA110510003Bushing · wrong part(CAN) CABIN VENTILATION BLOWER FAILED IN FLIGHT. NO ACTION TAKEN. UNAPPROVED BRUSHES AND BEARING SHIMS FOUND IN MOTOR OF BLOWER ASSEMBLY. BLOWER ASSY CONSISTS OF A FAN AND HOUSING WITH A DE BRUSH TYPE ELECTRIC MOTOR. INSPECTION FOUND ONE BRUSH WORN BUT STILLApr 12, 2011 · Beech 100BEECH · Air Distribution FanSDR CA110412001Actuator · failed(CAN) DURING CLIMB AT APPROXIMATELY 13000 FT, CREW NOTICED SMOKE COMING UP FROM THE FLOOR IN THE CABIN. THE CAPTAIN REACHED FOR THE FLAP MOTOR CIRCUIT BREAKER BUT OBSERVED IT WAS ALREADY OUT. THE CREW RETURNED TO THE AIRPORT OF DEPARTURE. DURING THE DESCENT Mar 23, 2011 · Beech A100 · Trailing Edge Flap ActuatorSDR CA110105001Gear · wornMAINTENANCE COMPLETED A SCHEDULED STARTER GENERATOR SPLINE WEAR INSPECTION AND FOUND THE STARTER DRIVE GEAR ON THE ENGINE WORN TO LIMITS, GEAR REPLACE AND ENGINE RETURNED TO SERVICE.Dec 24, 2010 · Beech A100 · Engine StarterSDR CA101112005Torque Tube · cracked(CAN) ELEVATORS WERE REMOVED TO CARRY OUT MANDATORY SERVICE BULLETIN 2145 INSPECTION/REPLACEMENT OF ELEVATOR TORQUE TUBE. NDT COMPANY CARRIED OUT FLUORESCENT LIQUID PENETRANT INSPECTION ON LEFT AND RIGHT TORQUE TUBE ASSYS P/N 115-610010-325. THEY FOUNDED A CNov 10, 2010 · Beech A100 · Elevator Control SystemSDR CA101103006Door Frame · cracked(CAN) CABIN DOOR AFT FRAME CRACKED AT UPPER LOCK BAYONNET (WHEN DOOR CLOSED). CABIN DOOR FWD FRAME CRACKED AT LOWER LOCK BAYONNET (WHEN DOOR CLOSED).Nov 2, 2010 · Beech A100 · Fuselage Main, StructureSDR CA101108007Door · open(CAN) DURING CRUISE THE LT WING LOCKER DOOR CAME OPEN AND DEPARTED. COULD NOT DETERMINE WHY THE DOOR SEPARATED AS THE DOOR COULD NOT BE FOUND. THE WING LOCKER WERE REMOVED AND AIRCRAFT PUT INTO ORIGINAL CONFIGURATION. NACELLE WING LOCKER SYSTEM (BAGGAGE AREOct 21, 2010 · Beech A100 · DoorsSDR CA101001001Wire · looseAFTER T/O, THE CREW SMELLED SMOKE ODOR AND A FEW SECONDS LATER THEY SAW SMOKE COMING OUT FROM PEDESTAL FOR A FEW SECONDS SO THEY TURN OFF THE ENVIRONMENTAL SYS AND THEY DECIDE TO RETURN TO DEPARTURE. MX FLEW TO INVESTIGATE THE PROBLEM. FOUND OUT, A LOOSE WISep 29, 2010 · Beech 100BEECH · Electrical Power System WiringSDR CA101109008Skin · cracked(CAN) ON WING CENTER SECTION P/N 99-120000-603 SKINS 50-120068-96 LT AND 97 RT WERE CRACKED AT UPPER FEW WING ATTACH FITTINGS.Sep 23, 2010 · Beech A100 · Wing, Plate/SkinSDR CA100922002Control Cable · damagedELEVATOR TRIM CABLE WAS FOUND UNSPOOLED OFF BOTH FWD AND AFT TRIM DRUMS.Sep 17, 2010 · Beech E90 · Elevator Tab Control SystemSDR JDWA147F1Landing Gear · malfunctionedAFTER TAKEOFF, THE GEAR IN-TRANSIT LIGHT CAME ON. PILOT RETURNED WITHOUT FURTHER INCIDENT.Sep 7, 2010 · N147SF · Beech 99 · Landing Gear Retraction/Extension SystemSDR AXSA195WA08/31/10Switch · out of adjustACFT DEPARTED AT 1112Z, AFTER TAKEOFF, LANDING GEAR WAS RETRACTED AND THE RED GEAR UNSAFE LIGHT WOULD NOT GO OUT. PILOT CYCLED GEAR WITH NO CHANGE. PUT GEAR BACK DOWN AND LANDED WITHOUT INCIDENT. MX DETERMINED THAT THE CAUSE WAS THE UPLOCK INDICATION SWITCHAug 31, 2010 · N195WA · Beech 99 · Landing Gear Retraction/Extension SystemSDR CA100924007Coupling · blownDURING A ROUTINE FLIGHT, THE ACFT LOST PRESSURIZATION AFTER DESCENDING AND RETURNING BACK TO THE AIRPORT, THE ABOVE LISTED DUCT COUPLING WAS FOUND TO HAVE BLOWN OFF. THERE WAS NO DAMAGE TO EITHER DUCT COUPLING OR CLAMP AND THE PART WAS RE-INSTALLED TO THE COAug 30, 2010 · Piper PA31T · Air Distribution SystemSDR 2010FA0000894Warning Light · illuminatedAFTER TAKEOFF, THE HYD LIGHT CAME ON AND STAYED ON. PILOT RETURNED WITHOUT FURTHER INCIDENT.Aug 25, 2010 · N128SF · Beech 99A · Central WarningSDR CA100826002Torque Tube · crackedTHE ACFT WAS UNDER A PHASE 4 INSP, THE HORIZ ATTACHMEMT POINT SPECIAL WAS CARRIED OUT AT THIS TIME. THE ELEVATOR TORQUE TUBES WERE ALSO INSPECTED, A CRACK WAS FOUND ON THE INNER CASTING.Aug 25, 2010 · Beech A100 · Elevator StructureSDR CA100826004Support Bracket · crackedDURING PHASE/STAB ATTACH POINT INSP, TAIL CONE WAS REMOVED. LT ELEVATOR TORQUE TUBE SUPPORT BRACKET WAS FOUND CRACKED AT ONE OF THE TAPER PIN HOLES.Aug 23, 2010 · Beech A100 · Elevator StructureSDR CA100809015Motor · failed(CAN) ON TAXI IN FROM LANDING, IT WAS OBSERVED BY THE RAMP ATTENDANT THAT SMOKE WAS COMING FROM THE NOSE OF THE AIRCRAFT. THE AIRCRAFT WAS SHUTDOWN NORMALLY. THE CAPTAIN EXITED THE AIRCRAFT AND DISCONNECTED THE BATTERY. FURTHER INSPECTION INDICATED THAT THEAug 5, 2010 · Beech A100 · Cabin Cooling SystemSDR CA100817002Engine · failedDURING REVENUE FLIGHT, ENGINE WAS MAKING AN UNUSUAL NOISE ON APPROACH. THE NOISE FOLLOWED POWER LEVER MOVEMENTS AND PARAMETERS SHIFTED NOTICEABLY UPWARD. ENGINE WAS SHUTDOWN AND AN UNEVENTFUL SINGLE-ENGINE LANDING WAS ACCOMPLISHED. POST-FLIGHT INSP REVEALEDAug 2, 2010 · Mckinn G21G · Engine (Turbine/Turboprop)SDR CA100809012Carbon Seal · leaking(CAN) UPON A WALK AROUND INSPECTION IT WAS NOTICES THAT FUEL WAS DRIPPING FROM THE RT ENGINE FURTHER INSPECTION REVEALED THAT THE FUEL IN QUESTION WAS COMING FROM THE CASE DRAIN ON THE HP FUEL PUMP. THE FUEL PUMP AND FCU WERE REPLACED AND THE PROBLEM CORRECTEJul 27, 2010 · Beech A100 · Engine Fuel PumpSDR CA100728001Control Cable · wornDURING A SPECIAL INSP, THE ENGINE IDLE CABLE, BOTH THE LT AND RT CABLES WERE FOUND TO HAVE EXCESSIVE PLAY IN THE SWAGED END (THE ENGINE END). THE CABLES WERE REPLACED (LT PN 99-380005-21 AND RT PN 99-380005-3) AND ACFT RETURNED TO SERVICE. THIS SPECIAL INSP WJul 26, 2010 · Beech A100 · Power LeverSDR CA100806007Actuator · leakingDURING FLIGHT, THE CREW NOTICED THE HYD PUMP CYCLING. THE CREW PERFORMED AN EMERGENCY EXTENSION AND AN UNEVENTFUL LANDING WAS COMPLETED. MX FOUND THE RT MAIN GEAR ACTUATOR LEAKING FLUID OUT THE RAM. THE ACTUATOR WAS REPLACED.Jul 23, 2010 · Beech 99 · Landing Gear ActuatorSDR CA100809017Bellcrank · failed(CAN) DURING A PHASE INSPECTION THE DOOR LATCHES WERE OBSERVED NOT TO BE WORKING CORRECTLY. FURTHER INSPECTION REVEALED THE BELLCRANK HAD FAILED RESULTING IN IMPROPER TRAVEL OF THE UPPER DOOR HOOKS. THE BELLCRANK WAS REPLACED WITH NEW.Jul 22, 2010 · Beech A100 · Passenger/Crew DoorsSDR CA100809014Drive Gear · failed(CAN) ON ENGINE START CYCLE RT, NG CLIMBED NORMALLY TILL APPROX 14 PERCENT THEN DECLINED RAPIDLY. FURTHER INSPECTION REVEALED THE SPLINE DRIVE INSIDE THE DRIVE GEAR HAD STRIPPED OUT CAUSING THE STARTER/GENERATOR TO BECOME UNCOUPLED FROM THE GAS GENERATOR SECTJun 24, 2010 · Beech A100 · Starter-GeneratorSDR CA100622012Switch · unserviceable(CAN) WHEN LANDING IN CYSB THE CREW SELECTED GEAR DOWN AND THE RT GEAR INDICATION REMAINED RED (INTRANSIT). THE CREW ELECTED TO RETURN TO CYXU. DURING THE TRAVEL BACK TO CYXU I WAS IN CONTACT WITH THE CREW AND MULTIPLE ATTEMPTS WERE MADE TO EXTEND THE RT GEARJun 22, 2010 · Piper PA31T · Landing Gear Position and WarningSDR CA100624003Gauge · uncalibratedDURING TAKEOFF, THE PILOT NOTED THE RT OIL PRESSURE TO BE ABOVE RED LINE. ACFT LANDED WITHOUT INCIDENT AND INSPECTED. IT WAS DISCOVERED THE OIL PRESSURE GAUGE WAS READING 10 PSI HIGH. NEW GAUGE HAD BEEN INSTALLED 1 YEAR EARLIER FOR UNRELATED REASON.Jun 18, 2010 · Piper PA31T · Engine Oil PressureSDR UQMA913UActuator · brokenLEFT INNER GEAR DOOR ACTUATOR WOULD NOT OPEN DUE TO INTERNAL MALFUNCTION RESULTING IN NOT LETTING THE LEFT GEAR LEAVE THE GEAR WELL. THE AIRCRAFT MADE A GEAR UP LANDING. THE ACTUATOR IS AN OZONE P/N 2924-3, PIPER P/N 455-946. THE ACTUATOR WAS INSTALLED 12-9Jun 16, 2010 · N17TU · Piper PA31T · Landing Gear Door ActuatorSDR CA100528011Engine · failedACFT LANDED, UPON TAXI TO PICK-UP PASSENGERS, THE RT ENGINE QUIT. THE PILOT WAS UNSURE IF THE ENGINE QUIT ON ITS OWN OR IF THE CONDITION LEVER WAS INADVERTENTLY PUT TO CUTOFF. ENGINE STARTED UP NORMALLY ON THE NEXT START. MX INVESTIGATED ENGINE, FIREWALL FUEMay 26, 2010 · Beech 100BEECH · Engine (Turbine/Turboprop)SDR CA100531006Blower Motor · overheatedCABIN VENTILATION BLOWER MOTOR OVERHEATED AND CREATED SMOKE IN THE COCKPIT. PILOT WAS FORCED TO DO AN EMERGENCY LANDING. UPON INVESTIGATION THE BLOWER MOTOR CIRCUIT BREAKER WAS FOUND TRIPPED. THE BLOWER MOTOR WAS REPLACED WITH A O/H UNIT AND THE CIRCUIT BREMay 21, 2010 · Beech E90 · Air Distribution FanSDR CA100218014Yoke · damaged(CAN) DURING INSP, PLAY WAS FOUND WHERE THE NLG ACTUATOR ATTACHES TO THE YOKE IN THE DRAG BRACE ASSY. WHEN THE ACTUATOR WAS REMOVED FROM THE YOKE, IT WAS DISCOVERED THAT THE HOLE IN THE YOKE FOR THE ACTUATOR ATTACH BOLT (PN AN24-23A) WAS DRILLED TOO LARGE. THFeb 18, 2010 · Beech A100 · Landing Gear ActuatorSDR CA100212006Gyro · failed(CAN) ACFT STARTED UP AND TAXIED ACROSS THE FIELD TO PICK UP PASSENGERS. UPON THE NEXT START THE CO-PILOT ATTITUDE INDICATOR FAILED TO ERECT. THE ACFT RETURNED TO BASE FOR MX. THE ATTITUDE INDICATOR WAS REPLACED WITH A NEW UNIT, FUNCTION TESTED OK. (TC 2010Feb 10, 2010 · Beech 100BEECH · Attitude Gyro and Indicating SystemSDR CA100212007Gyro · failed(CAN) ACFT STARTED UP FOR AN INTENDED FLIGHT. THE CO-PILOT`S ATTITUDE INDICATOR FAILED TO ERECT. ACFT SHUTDOWN. THE ATTITUDE INDICATOR WAS REPLACED WITH NEW PN 23-500-06-16, FUNCTION CHECKED OK. (TC 20100212007)Feb 10, 2010 · Beech 100BEECH · Attitude Gyro and Indicating SystemSDR CA100218012Skin · cracked(CAN) FUSELAGE PRESSURE SKINS PN 50-120156-81 AND 82 CRACKED AT LOWER SPAR CAP PENETRATIONS. (TC 20100218012)Feb 10, 2010 · Beech E90 · Fuselage Main, Plate/SkinSDR CA100218013Skin · cracked(CAN) FUSELAGE PRESSURE SKINS P/N 50-420011-1051 AND 1052 CRACKED AND WORN BY CHAFING ACTION BETWEEN THEM AND FILLETS PN 50-420023-31 AND 32 DUE TO NORMAL WING MOVEMENT. (TC 20100218013)Feb 10, 2010 · Beech E90 · Fuselage Main, Plate/SkinSDR CA100224010Indicator · fluctuates(CAN) DURING THE RECTIFICATION OF THE RT FUEL GAUGE INTERMITTENT FLUCTUATING, 2 FUEL QTY INDICATOR (PN 100-380006-47) FAILED ON INSTALL. THE FIRST INDICATOR (SN 7127M) WAS INSTALLED, THE ACFT WAS POWERED AND THE GAUGE PEGGED FULL. UNABLE TO MAKE ANY ADJUSTMEFeb 4, 2010 · Beech A100 · Fuel Quantity IndicatorSDR CA100204009Starter Gen · failed(CAN) DURING A TRAINING FLIGHT, THE NR2 ENGINE WAS SHUTDOWN. FOLLOWING MOMENTS REVEALED THAT THE NR1 ENGINE GENERATOR WAS FAILED. 1 BATTERY START OF NR2 ENGINE WAS TRIED WITH NO SUCCESS. DUE TO COMPLETE ELECTRICAL POWER FAILURE, THE CREW SUCCEEDED TO CONTACT AFeb 1, 2010 · Beech A100 · Starter-GeneratorSDR CA100208002Frame · cracked(CAN) RT LOWER FUSELAGE FRAME AT STATION 207 FOUND CRACKED. FRAME REPLACED. (TC 20100208002)Jan 29, 2010 · Beech A100 · Fuselage Main, FrameSDR CA100208003Keelbeam · cracked(CAN) CRACKS FOUND IN THE LT & RT WHEEL WELL ON THE OTBD KEEL RIB. REPAIR ANGLES INSTALLED IAW MFG FIELD REPAIR NR FR-KA-03216. (TC 20100208003)Jan 29, 2010 · Beech A100 · Fuselage Main, KeelSDR CA100208004Stringer · cracked(CAN) 2 CRACKED STRINGERS ON REAR PRESSURE BULKHEAD FOUND CRACKED. STRINGERS REPLACED. (TC 20100208004)Jan 29, 2010 · Beech A100 · Fuselage Main, Longeron/StringerSDR CA100208005Fitting · worn(CAN) DURING REMOVAL OF THE ENGINE MOUNT FROM THE NACELLE THE LOWER MOUNT ATTACHMENT FITTINGS WERE FOUND LOOSE INSIDE THE NACELLE ON BOTH THE LT & RT SIDES. THE LT INBD AND OTBD LOWER FITTINGS WERE REPAIRED BY REMOVING THE FITTINGS NDT REINSTALLING THEN DRILLIJan 29, 2010 · Beech A100 · Nacelle/Pylon, Attach FittingsSDR TIMA201000009Blade · brokenLEFT ENGINE FAILED IN FLIGHT.Jan 28, 2010 · N99GH · Beech 99A · Turbine Engine Compressor SectionSDR CA100113001Altimeter · intermittent(CAN) AIRCRAFT DEPARTED CYXD. AFTER ROTATION THE CAPTAIN NOTED HIS ALTIMETER FLAGGED OFF. HE THEN RETURNED TO CYXD. UPON LANDING THE ALTIMETER BEGAN TO FUNCTION AGAIN. SHIPS WIRING CHECKED, NO FAULTS FOUND. ALTIMETER WAS REMOVED AND SENT TO A LOCAL AVIONIJan 12, 2010 · Beech 100BEECH · Altimeter, Barometric/EncoderSDR CA100111006Wheel · cracked(CAN) AFTER STRIPPING, A VISUAL INSPECTION OF BOTH HALF WHEELS WAS PERFORMED BEFORE SENDING TO NDT. BOTH HALF WHEELS TIE BOLTS HOLES FOUND CORRODED BEYOND LIMIT AND MANY SHOWED SIGNS OF CRACKS. (TC NR 20100111006)Jan 8, 2010 · Beech A100 · Wheel/Ski/FloatSDR CA100209010Spar · cracked(CAN) THE OTBD WING REAR SPAR WEB WAS FOUND CRACKED AT THE LAP JOIINT WS 110.11, THE LOCATION OF THE OTBD FLAP, INBD TRACK. THE RIVETS SECURING THE LOWER CLIPS TO THE FLAP TRACK FAILED. THE FORCES APPLIED TO THE FLAP TRACK WHEN THE FLAPS WERE LOWERED PULLED ONJan 1, 2010 · Beech A100 · Wing SparSDR 2010FA0000038Planetary Gear · mismanufactured2ND STAGE PLANET GEARS HAVE ON THE INTERNAL BORE A PRESS FIT BUSHING (PN E3035030). THIS BUSHING HAS ITS BORE COATED OR SPRAYED WITH BRONZE MATERIAL INTRODUCED BY SB 1404. DURING OUR INSP WE OBSERVED THAT THIS BRONZE COATING HAD ROTATED FROM ITS ORIGINAL POSIDec 22, 2009 · Engine (Turbine/Turboprop)SDR CA091223007Rod · binding(CAN) LEFT HAND ENGINE TORQUE DOES NOT DECREASE WHEN POWER LEVER IS RETARDED. LEFT EGINE INSPECTED FOUND AFT FUEL CONROL INTERCONNECT ROD END BIDING AND HOLDING PCU ARM AT A HICH POWER SETTING. AFT ROD END REALIGNED, CLEANED, AND LUBRICATED. AIRCRAFT GROUNDDec 8, 2009 · Beech A100 · Power Lever
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