U/A Canada PT6A-6

Service difficulty reports · 92

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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 = 'PT6A6'
  ORDER BY difficulty_date DESC"

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SDR G1IA20260810115Warning Message · multiple indHIGH ITT INDICATIONS WITH SUBSEQUENT EIS IND, INCLUDING CAUTION, WARNING & FLASHING ITT TEMP. ITT TEMP INDNS FLUCTUATE BTWN 920 & 960, REGARDLESS OF TORQUE SETTING. NO SECONDARY INDNS IN COCKPIT TO INCLUDE OIL TEMP NORMAL AS WELL AS ALL OTHER ENG INSTS. NO NOTAug 10, 2026 · N557PC · Pilats PC1245 · Engine (Turbine/Turboprop)SDR ENHA20240403001Engine · fodDURING FLIGHT, SMOKE AND BURNING SMELL NOTED IN CABIN. MX INSPECTED ENGINE AND FOUND A PIECE OF SPIRAL WRAP MELTED. REMOVED SPIRAL WRAP AND OPS CHECKED ENGINE. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N28AN · Cessna 208B · Engine (Turbine/Turboprop)SDR RU3A201910032048Clamp · leakingRIGHT BLEED AIR FAIL LIGHT ILLUMINATED. MAINTENANCE DISCOVERED SEVERAL HOLES RH INBD NAC EVA TUBING. R2 EVA TUBE, FOUND BAD CLAMPS AND SLEEVES (BLEED AIR LEAK) INSTALLED 3 NEW SLEEVES AND ALL NEW CLAMPSOct 1, 2019 · N69 · Beech 300BEECH · Engine Anti-Icing SystemSDR QMLA2016030616021Motor · failedAFTER TAKEOFF, WENT TO BRING THE GEAR UP & NOTICED THE INTRANSIT LIGHTS STAYED LIT. THE HYD CAWS LIGHT CAME ON INDICATING THERE WAS A FAILURE OF THE SYS. CLIMBED UP TO 6000 FT, BEGAN TROUBLESHOOTING. ATTEMPTED RECYCLING THE GEAR, BUT WAS ONLY ABLE TO GET 2 Mar 9, 2016 · N724HF · Pilats PC1245 · Landing Gear ActuatorSDR GLBA2013052800253Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 IN THE BEND RADIUS, 1" LENGTH. REPAIRED IAW EO 13-1900-53-043. MAJOR REPAIR.May 28, 2013 · N210GL · Beech 1900D · Fuselage Main, FrameSDR RL8R2014030700151Carriage · damagedINBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. THMar 13, 2013 · N702AV · Socata TBM700 · Trailing Edge FlapsSDR 2012FA0000837Support · damagedLEFT SUPPORT, AFT FLANGE RIVETS WERE MISSING. SUPPORT IS LOCATED BELOW THE CABIN FLOOR UNDER THE CENTER PEDESTAL.Dec 28, 2012 · N842E · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA2012080700028Spar Cap · crackedDURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN THE RT SIDE OF THE VERTICAL STAB, RT FWD SPAR CAP ANGLE AT APPROX AREA VSS 84.10, 20 PERCENT. REPAIRED AFFECTED AREA IAW EO 12-1900-55-022. MAJOR REPAIR.Aug 7, 2012 · N100UX · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR EHAA20120729005Brake Assy · failedRIGHT BRAKE FAILED ON LANDING. NO PEDAL PRESSURE ON EITHER PILOT'S OR CO-PILOT'S BRAKE PEDAL.Jul 29, 2012 · N171CJ · Beech 1900D · Landing Gear Brake SystemSDR 2011F00206Engine · malfunctionedRIGHT ENGINE SURGED AND OVER TORQUED, RT ENGINE SHUTDOWN IN THE AIR.Oct 2, 2011 · N136SL · Piagio P180 · Engine (Turbine/Turboprop)SDR GLBA20110801HActuator · inoperativePILOT REPORTED THAT THE LT MLG BOTH GREEN "L" AND "H" ANNUNCIATORS FLICKERED THEN EXTINGUISHED THEN REILLUMINATED, NO UNSAFE INDICATIONS ON APPROACH & LANDING. MX REPLACED THE LT MLG ACTUATOR, OPS AND RIG CKS IAW TC. 1900-3230.10.Jul 29, 2011 · N210GL · Beech 1900D · Landing Gear ActuatorSDR 5APR577Y73Motor · faultyHYD CAWS ILLUMINATED ON GEAR RETRACTION, LANDING GEAR DID NOT RETRACT. THE HYD POWER PACK MOTOR WAS FOUND TO BE FAULTY. THE MOTOR WAS R & R WITH A SERVICEABLE UNIT PN 960.30.02.104 IAW AMM 12-A-29-10-06-00A-920A-A. PERFORMED RETRACTIONS AND EXTENSIONS OF LANJul 5, 2011 · N558AF · Pilats PC1245 · Landing Gear Retraction/Extension SystemSDR DYV2011F00000Tach Generator · malfunctionedTHIS REPORT IS A SUPPLEMENT FROM 10 JUNE, 2011: THE PROP RPM INDICATION HAS FUNCTIONED NORMALLY SINCE THE INITIAL REPAIR OF THE ERRONIOUS INDICATION. THE PROP TACH GENERATOR WAS REPLACED WITH AN O/H PART. THE TIME SINCE NEW AND O/H ON THE FAILED PART IS UNKJun 22, 2011 · N1083S · Beech C90A · Engine RPM Indicating SystemSDR GUUA95553050311BAngle · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSP DISCOVERED RT CLOSING ANGLE CRACKED 2.1 INCHES AT FS 288.0. STOP DRILLED CRACK AND INSTALLED 13.5 INCH REPAIR ANGLE.May 3, 2011 · N87555 · Beech 1900D · Fuselage Miscellaneous StructureSDR 2011FA0000212Dipstick · brokenOIL DIPSTICK SEPARATED AT OIL CAP, STEM AND FELL INTO OIL TANK. THE STICK AND STEM WERE NOT ASSEMBLED CORRECTLY. THE STICK WAS NOT PUSHED FAR ENOUGH IN THE STEM SO THE RETENTION PIN DID NOT ENGAGE.Mar 30, 2011 · N980BC · Beech B300 · Turbine Engine Oil SystemSDR GLBA20110303HFrame · crackedDURING A SCHEDULED ROUNTINE INSP MX FOUND THE RT SIDE WALL HEAVY ANGLE AT FS 303, CRACKED IN THE BEND RADIUS, APPROX 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-010. MATERIALS UTILIZED ARE INCLUDED IN Mar 3, 2011 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20110214GStructure · damagedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX THE RT STABILON WAS DAMAGED. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 11-1900-55-003. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Feb 12, 2011 · N218YV · Beech 1900D · Vertical Stabilizer Miscellaneous StructureSDR GLBA20110202FStructure · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND 4 CRACKS AROUND THE VENT HOLE IN THE VERT STAB BEHIND THE BULLET CTR WEB, ALL 4 CRACKS ARE .5" IN LENGTH. SUPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPFeb 2, 2011 · N218YV · Beech 1900D · Horizontal Stabilizer StructureSDR GUUA52121310AHandle · stiffDURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE.Dec 13, 2010 · N87555 · Beech 1900D · Emergency ExitsSDR GUUA95552121310AHandle · stiffDURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE.Dec 13, 2010 · N87555 · Beech 1900D · Emergency ExitsSDR GLBA20101206ABleed Air Sys · inoperativeCLIMBING THROUGH 20,000 FT COULDN'T GET CABIN TO QUIT CLIMBING, HAD TO DEPLOY MASKS & RETURN TO DEPARTURE, DIR STUCK AT 3.4 PSI WOULD NOT GO HIGHER. STOWED & RELOCKED MASKS IAW MM 35-20-01. RAN ENG & PRESSURIZED - NO AIR FROM LT BLEED, REMOVED ORIFICE PLATE FDec 6, 2010 · N210GL · Beech 1900D · Engine Bleed Air SystemSDR E81RTT40346Bearing · disintegrated(E81RINVESTIGATED REPORTED IN-FLIGHT LOSS OF LT ENG DC GENERATOR FUNCTION. INITIAL VISUAL INSP OF LT ENGINE STARTER GENERATOR SHOWED INTERNAL FAILURE, METALLIC DEBRIS IN ADJACENT ENGINE COMPARTMENT AREA. UPON DISASSEMBLY, FOUND ANTI-DRIVE END BRG HAD FAILED, CNov 15, 2010 · N363CA · Raythn B300RAYTHEON · Starter-GeneratorSDR 2010FA0001127Light · false indicationBAGGAGE DOOR ANNUNCIATOR LIGHT ON IN FLIGHT.Oct 19, 2010 · N107SL · Piagio P180 · Door Warning SystemSDR GLBA201009061Autofeather Sys · malfunctionedCYCLED IN DURING APPROACH LT ENGINE ENTERED FEATHER & OUT OF FEATHER. MX TROUBLESHOT AUTOFEATHER SYS, SYS FOUND TO OPERATE NORMALLY IAW BMM 61-21-00.Sep 6, 2010 · N100UX · Beech 1900D · Propeller Feathering/ReversingSDR 2010F00204Fire Warning · false activationLT ENGINE FIRE WARNING LIGHT CAME ON IN FLIGHT, INDICATION ONLY, ENGINE WAS SHUTDOWN IN FLIGHT.Sep 4, 2010 · N131SL · Piagio P180 · Fire DetectionSDR 2010FA0000884Fitting · crackedRUDDER TRIM TAB ACTUATOR FITTING IS CRACKED ON LOWER LUG. CRACK EXTENDS FROM BEARING BORE THROUGH THE ENTIRE LUG THICKNESS. CRACK ORIGINATED AT SPOTS WHERE BEARING WAS STAKED INTO LUG.Aug 23, 2010 · N107SL · Piagio P180 · Horizontal Stabilizer, Attach FittingsSDR GUUA95532052710AMotor · inoperativeDURING DESCENT WHEN EXTENDING LANDING GEAR THE MOTOR STOPPED RUNNING, AND THE IN TRANSIT LIGHT REMAINED ILLUMINATED, THE LANDING GEAR HORN BEGAN TO SOUND WITH NO MOVEMENT OF POWER LEVERS, NO ILLUMINATION OF 3 GREEN LIGHTS AFTER A FEW SECONDS THE 3 GREEN LANDINMay 27, 2010 · N87555 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 19MA201002086413Drain · cloggedWHILE PERFORMING 36 MONTH FUEL COLLECTOR TANK INSP, INSPECTOR WAS UNABLE TO LOCATE THE COLLECTOR TANK AFT DRAIN OPENING IN LT COLLECTOR TANK. REMOVED DRAIL LINES FROM LOWER NACELLE AREA TO INSERT PIN UP THROUGH DRAIN FITTING TO TANK AREA TO LOCATE HOLES BUT FOFeb 8, 2010 · N886MA · Beech 1900D · Fuel StorageSDR CA090608001Turbine · stalled(CAN) EIR ENGINE STALLING.May 8, 2009 · Turbine SectionSDR DYV2009F00000Downlock Switch · intermittentBEFORE LANDING, WHEN GEAR WAS SELECTED DOWN, THE RT GREEN DOWN LIGHT FAILED TO ILLUMINATE. THE GEAR UNSAFE LIGHT AND HORN DID NOT INDICATE AN UNLOCKED GEAR. AFTER A FLYBY AND A VISUAL LOOK BY GROUND PERSONNEL, THE FAILED GEAR LIGHT CAME ON AND A LANDING WAS Jan 29, 2009 · N1083S · Beech C90A · Landing Gear Position and WarningSDR CA081125018Blades · failed(CAN) ACFT TYPE ID PC-9. WHILE APPLYING POWER DURING A TOUCH AND GO, THE ENGINE STARTED VIBRATING. THE PILOT REDUCED THE POWER TO IDLE AND ABORTED T/O. AS THE A/C SLOWED DOWN ON THE RUNWAY, OIL BEGAN TO SPRAY OVER THE CANOPY. ONCE CLEARED OF THE RUNWAY, THE Nov 16, 2008 · Turbine SectionSDR GLB2008F00003Skin · crackedPOPPED RIVET HEADS AND CRACK FOUND AT STATION 163.975 ABOVE AIRSTAIR DOOR. MAINTENANCE STOP DRILLED AROUND RIVETS AND REPAIRED THE AFFECTED AREA IAW B1900D SRM 53-90. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. (K)Jul 14, 2008 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLB2008F00004Skin · crackedBELLY SKIN CRACKED APPROXIMATELY 2 INCHES IN LENGTH AT FS 298.25 TO FS 300.25 APPROXIMATELY 5 INCHES OB OF STRINGER 12R AND APPROX 2 INCHES FROM OB EDGE OF BELLY SKIN. MAINTENANCE REMOVED DAMAGED SKIN AND PATCHED IAW SRM 53-90. PATCH 18 INCHES BY 4.5 INCHES.Jul 14, 2008 · N192GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GUU2008F00003Wire · brokenAFTER TAKEOFF LANDING GEAR DID NOT RETRACT, LANDING GEAR CIRCUIT BREAKER POPPED WHEN HANDLE PUT DOWN WITH ONLY (2) GREEN LIGHTS. CIRCUIT BREAKER PUSHED IN AND GEAR WENT DOWN BREAKER POPPED AGAIN. RETURNED TO PBI LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE SJul 1, 2008 · N87555 · Beech 1900D · Landing Gear System WiringSDR GUUA04210803Cap · missingFLIGHT 9197, AFTER TAKEOFF, NOSE LANDING GEAR TAKES EXCESS TIME TO RETRACT. INSTALLED AIR REGULATOR PORT CAP. OPERATIONAL CHECK NORMAL.Apr 21, 2008 · N87555 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA04050801Torque Tube · corrodedDURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LT ELEVATOR TORQUE TUBE EXFOLIATED. REPLACED LT ELEVATOR TORQUE TUBE.Apr 5, 2008 · N87555 · Beech 1900D · Elevator StructureSDR GUUA04040801Cable · brokenFLIGHT: 9205, PILOT REPORTED (4) REAR CAMS ON FWD CABIN DOOR WILL NOT ROTATE WHEN DOOR IS SECURED. REPLACED AIRSTAIR DOOR DOWN AFT CABLE.Apr 4, 2008 · N87555 · Beech 1900D · Entrance StairsSDR AMWA89766BCBattery · dischargedAFTER TAKEOFF, BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINT REPLACED BATTERY AND CLEARED DISCREPANCY.Jan 24, 2008 · N135YV · Beech 1900D · Battery/Charger SystemSDR AMWA89551BCGcu · malfunctionedDURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINT PARALLELED BOTH GCU'S AND CLEARED DISCREPANCY.Jan 10, 2008 · N135YV · Beech 1900D · DC Generating SystemSDR AMWA89557BCBattery · dischargedBATTERY CHARGE ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT. MAINT REPLACED BATTERY AND CLEARED DISCREPANCY.Jan 10, 2008 · N135YV · Beech 1900D · Battery/Charger SystemSDR GLBA20061041Bulb · burned outSMOKE/ODOR - PILOTS REPORTED THE GLARESHIELD INSTRUMENT EMERGENCY LIGHTS WERE SMOKING ON THE GROUND AFTER STARTING ENGINES. REMOVED EMERGENCY FUSE F127. MAINTENANCE REMOVED EMERGENCY FUSE F127 AND REMOVED AND REPLACED BULB IAW MM 33-10. OPERATIONAL CHECK GOJan 1, 2008 · N210GL · Beech 1900D · Emergency LightingSDR GUUA12040702Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET.Dec 4, 2007 · N218YV · Beech 1900D · Elevator Miscellaneous StructureSDR AMWA223904Skin · corrodedSURFACE TYPE CORROSION FOUND ON INTERIOR SURFACE OF FUSELAGE SKIN IN AIRCRAFT BELLY. FS213.25, 228.25, AND 243.25 ALONG STRINGER 16. INSPECTED, CLEANED AND REPAIRED IAW DER SUPPLIED REPAIR DATA.Oct 16, 2007 · N161YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20061004Angle · crackedLT HEAVY ANGLE CRACKED AT FS STA 288.0 FORWARD END IN BEND RADIUS. 09-26-07 CRACK APPROXIMATELY 1.75" IN LENGTH. MAINTENANCE INSTALLED REPAIR ANGLE I.A.W. BEECH SRM 53-90-23. REPAIR LENGTH 13.8 INCHES. .080 2024-0.Sep 21, 2007 · N210GL · Beech 1900D · Fuselage Main, StructureSDR GLBA20061005Frame · crackedFRAME CRACKED AT FS 164 AT STRINGER 9AL. CRACK LENGTH APPROXIMATELY 4 INCHES. 09-26-07 REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE FS 164 AT STRINGER 9AR IAW BEECH 1900D SRM 51-70. REAPIR APPROXIMATELY 2.5" BY 4.1" .080 2024 T-3.Sep 21, 2007 · N210GL · Beech 1900D · Fuselage Main, FrameSDR 2007FA0000735Ground Wire · brokenWIRE NR P73G16N AT RT ENGINE FIREWALL GROUND POINT GS15 SEPARATED FROM THE WIRE TERMINAL DURING CRUISE FLIGHT. THIS WIRE CONNECTS GROUND TO THE GCU PIN G. THE RT GENERATOR OUTPUT SPIKED AND OPENED THE 325 AMP RT BUSS CURRENT LIMITER, THE 50 AMP RT INVERTER CURAug 9, 2007 · N1925P · Beech B200 · Electrical Power System WiringSDR N843E12007Hed · faultedCREW LEFT STATION. TWENTY MINUTES IN FLIGHT "BATT TIE OPEN" ANNUNCIATOR ILLUMINATED. CREW RETURNED TO STATION WITHOUT ISSUE. REMOVED AND REPLACED BATTERY HED. OPS CHECK GOOD.Aug 1, 2007 · N843E · Beech 1900D · Battery/Charger SystemSDR 2007FA0000884Plate · crackedFOUND TORQUE PLATE CRACKED DURING ROUTINE INSPECTION. (K)Jul 17, 2007 · N9602F · Cessna 208 · Landing Gear Brake SystemSDR NSVA20070140Fitting · looseRT ENG OIL PRESS FLUCTUATED BETWEEN 65-70 THEN DROPPED BELOW 60 PSI WITH LOW OIL PRESS LIGHT ILLUMINATED. INFLIGHT SHUTDOWN. TIGHTENED OIL COOLER RETURN LINE FITTING IAW BE1900 MM 71-00-00, GROUND RAN AIRCRAFT 20 MIN IAW CRUISE CONFIGURATION, ALL ENGINE PARMay 27, 2007 · N136MJ · Beech 1900D · Turbine Engine Oil SystemSDR MDGA200700001Engine · unknownINFLIGHT SHUT DOWN OF RIGHT ENGINE. TIME SINCE OH WAS 1210.00 HOURS.May 5, 2007 · N977AA · Beech C90 · Engine (Turbine/Turboprop)
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