U/A Canada PT6A-112

Service difficulty reports · 110

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 = 'PT6A112'
  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 CA050419002Engine · inoperative(CAN) DURING TAKEOFF, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION. MFG WILL MONITOR THE INVESTIGATION OF THIS INCIDENT AND WILL ADVISE OF ROOT CAUSE, ONCEESTABLISHED.Nov 25, 2004 · Reims F406 · Engine (Turbine/Turboprop)SDR CA041026009Seal · leaking(CAN) PILOT DISCOVERED EXCESSIVE OIL LEAK AFTER FLIGHT. MAINTENANCE WAS DISPATCHED TO INVESTIGATE.FUEL PUMP OIL SEAL WAS FOUND TO BE DISLODGED FROM ITS CARRIER AND HAD MOVED DOWN THE SHAFT INTO THE ENGINE CASE.Oct 4, 2004 · Cessna 425 · Engine Fuel PumpSDR AUS20040496Truss · corroded(AUS) LT ENGINE LOWER LT ATTACHMENT TRUSS CORRODED.Jun 7, 2004 · Reims F406 · Engine Mount SectionSDR AUS20040374Wire · broken(AUS) FLAP CONTROL SYSTEM WIRE BROKEN. FAULT TRACE TO BROKEN WIRE A157B-A25799200 TO FLAP UP CONTROL SWITCH.May 7, 2004 · Reims F406 · Flight Control System WiringSDR AUS20040350Strip · separated(AUS) STALL STRIP MISSING.Apr 23, 2004 · Reims F406 · Stall Warning SystemSDR AUS20040385Computer · faulty(AUS) AUTOPILOT COMPUTER FAULTY.Apr 14, 2004 · Reims F406 · Autopilot ComputerSDR AUS20040214Clamp · failed(AUS) LT ENGINE PROPELLER REVERSING LEVER CABLE CLAMP BOLT FAILED ALLOWING PROPELLER REVERSING PY LEVER TO DISCONNECT FROM PUSH/PULL CABLE.Mar 20, 2004 · Reims F406 · Propeller Feathering/ReversingSDR EPUA070304AFire Loop · chafedAS FLIGHT ENTERED DOWNWIND, THE RT FIRE WARNING LIGHT ILLUMINATED. ENGINE WAS SHUTDOWN AND FLIGHT LANDED WITHOUT INCIDENT. MX FOUND THE AFT FIRE LOOP WAS CHAFFED UNDER CLAMP.Mar 7, 2004 · N406GV · Reims F406 · Fire DetectionSDR AUS20040137Servo · faulty(AUS) AUTOPILOT ROLL SERVO CAPSTAN FOUND IN PIECES ON AIRCRAFT FLOOR. SIX FASTENEING SCREWS FOUND IN CLOSE PROXIMITY TO THE SERVO MOUNT.Feb 29, 2004 · Reims F406 · Autopilot Main ServoSDR AUS20040059Altimeter · faulty(AUS) ALTIMETER FITTED TO AIRCRAFT WITH INCORRECT ALTITUDE RANGE. PERSONNEL/MAINTENANCE ERROR.Feb 3, 2004 · Reims F406 · Altimeter, Barometric/EncoderSDR AUS20040060Altimeter · faulty(AUS) ALTIMETER FITTED TO AIRCRAFT WITH INCORRECT ALTITUDE RANGE. PERSONNEL/MAINTENANCE ERROR.Feb 3, 2004 · Reims F406 · Altimeter, Barometric/EncoderSDR AUS20040071Controller · failed(AUS) COMMUNICATION SYSTEM CONTROL BOX FAILED.Jan 25, 2004 · Reims F406 · Communications SystemSDR CA040202013Engine · failed(CAN) ENGINE WAS INVOLVED IN A PROP STRIKE INCIDENT WHEN AIRPLANE PULLED OFF RUNWAY AND NLG STRUCK A STUMP, FORCE OF THIS IMPACT COLLAPSED THE LANDING GEAR AND BOTH PROPELLERS STRUCK THE GROUND. IT WAS CLEAR TO IDENTIFY THAT ENGINE HAD SUFFERED FROM A PROPELLJan 6, 2004 · Engine (Turbine/Turboprop)SDR CA040202014Engine · failed(CAN) ENG WAS INVOLVED IN A PROP STRIKE INCIDENT, AC PULLED OFF THE RUNWAY AND NLG STRUCK A STUMP, FORCE OF THIS IMPACT COLLAPSED LANDING GEAR, BOTH PROPS STRUCK THE GROUND. IT WAS CLEAR TO IDENTIFY THAT ENG SUFFERED FROM PROP STRIKE. EXHAUST DUCT WAS SEVEJan 6, 2004 · Turbine SectionSDR AUS20031121Tire · deflated(AUS) NOSE WHEEL TIRE DEFLATED. NO DAMAGE TO WHEEL RIM. NOSE WHEEL MUD GUARD MISSING. INVESTIGATION FOUND THE VALVE STEM SHEARED FROM THE TUBE. SUSPECT VALVE STEM FAILURE CAUSED BY FATIGUE AND AGING OF THE RUBBER AROUND THE VALVE BASE.Nov 6, 2003 · Reims F406 · TireSDR AUS20031067Spar Cap · corroded(AUS) RT WING MAIN SPAR LOWER SPAR CAP CORRODED. MICROBIOLOGICAL GROWTH FOUND ON INSIDE OF FUEL ACCESS PANELS 621BB AND 521BB AND 521CB.Oct 15, 2003 · Reims F406 · Wing SparSDR AUS20031013Switch · faulty(AUS) RT MAIN LANDING GEAR UPLOCK SWITCH FAILED.Oct 2, 2003 · Reims F406 · Landing Gear Position and WarningSDR AUS20031155Wire · broken(AUS) FLAP UP MICROSWITCH WIRE BROKEN. SWITCH IS LOCATED BEHINDFLAP SELECTOR.Aug 29, 2003 · Reims F406 · Flight Control System WiringSDR AUS20030775Motor · failed(AUS) FORWARD AIR CONDITIONER ELECTRIC MOTOR FAILED.Jul 31, 2003 · Reims F406 · Cabin Cooling SystemSDR AUS20030575Radome · bird strike(AUS) BIRDSTRIKE ON SURVEILLANCE RADOME.Jun 4, 2003 · Reims F406 · Aerodynamic FairingsSDR AUS20030457Switch · failed(AUS) NOSE LANDING GEAR ACTUATOR FAULTY. SWITCH OUT OF ADJUSTMENT.Apr 22, 2003 · Reims F406 · Landing Gear ActuatorSDR AUS20030403Clamp · corroded(AUS) NR 1 ENGINE SHUT DOWN FOLLOWING LT WING OVERHEAT WARNING.INVESTIGATION FOUND THE CLAMP ATTACHED TO THE PNEUMATIC FLOWCONTROL VALVE DOWNSTREAM FROM THE NO1 ENGINE BLEED PORT CORRODEDAND RUPTURED CAUSING EXCESSIVE AIR LEAKS.Apr 6, 2003 · Reims F406 · Pneumatic Distribution SystemSDR AUS20030378Actuator · faulty(AUS) NOSE LANDING GEAR ACTUATOR FAULTY.Mar 20, 2003 · Reims F406 · Landing Gear ActuatorSDR AUS20021189Lead · broken(AUS) STARTER-GENERATOR FAULTY. INSPECTION FOUND SEVERAL BRUSH LEADS BROKEN AND COMMUTATOR DAMAGED.Oct 16, 2002 · Reims F406 · Electrical Power System WiringSDR AUS20021058Rudder · fod(AUS) RUDDER DAMAGED BY ANOTHER AIRCRAFT TAXIING PAST. THE RUDDER SKINWAS DENTED AND BUCKLED AT THE MID POINT OF THE TRAILING EDGE. DURING DISASSEMBLY FOR REPAIR A PORTION OF THE RIB WAS ALSO DAMAGED.Sep 17, 2002 · Reims F406 · Rudder StructureSDR AUS20020918Link · cracked(AUS) COPILOTS OUTBOARD BRAKE PEDAL RH LINK ASSEMBLY CRACKED IN THE AREA OF THE WELD ATTACHING THE CLEVIS RODEND.Aug 12, 2002 · Reims F406 · Landing Gear Brake SystemSDR AUS20020678Motor · failed(AUS) REAR AIRCONDITIONING COMPRESSOR ELECTRIC MOTOR FAULTY. THECIRCUIT BREAKER WAS POPPED AND WHEN RESET, THE MOTOR WAS SPARKING EXCESSIVELY AND EMITTING SMOKE AT THE COMMUTATOR.Jun 29, 2002 · Reims F406 · Cabin Cooling SystemSDR AUS20020403Switch · faulty(AUS) DURING CRUISE THE LT WING OVERHEAT LIGHT ILLUMINATED. INVESTIGATION FOUND NO EVIDENCE OF BLEED AIR LEAK OR OVERHEAT CONDITION. SUSPECT FAULTY OVERHEAT SWITCH.Apr 27, 2002 · Reims F406 · Overheat DetectionSDR 2002FA0000503Hose · failedHOSE WAS INSTALLED ON 10-15-99 1869.1TT. CURRENT AIRCRAFT TIME 2234.8 HRS. THIS HOSE LASTED 365.7 HRS. THIS HAS BEEN AN ON GOING PROBLEM WITH THIS AIRCRAFT. CESSNA SUPERSEEDED THE ORIGNAL HOSE P/N AS705976-1 TO THE AE7013002K024 WHICH IS SLIGHTLY LONGER,IN HOPApr 18, 2002 · N50JN · Cessna 425 · Turbine Engine Oil SystemSDR AUS20011294Cooling Fan · failed(AUS) SURVEILLANCE RADAR COOLING FAN FAILED.Dec 9, 2001 · Reims F406 · Air Distribution SystemSDR AUS20011309Actuator · contaminated(AUS) ELEVATOR TRIM TAB ACTUATORS LUBRICATED WITH THE INCORRECT GREASE. ACTUATORS FREEZING IN FLIGHT. MAINTENANCE MANUAL SPECIFIES "TRIBOLUBE" ONLY. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.Dec 6, 2001 · Reims F406 · Elevator Tab Control SystemSDR AUS20011310Channel · cracked(AUS) NOSE LANDING GEAR ACTUATOR ATTACHMENT STRUCTURE CHANNEL CRACKED.FOUND DURING INSPECTION IAW AD/F406/7.Dec 6, 2001 · Reims F406 · Fuselage, Landing Gear Attach FittingsSDR AUS20011311Ignition Lead · chafed(AUS) RT IGNITER LEAD ON BOTH ENGINES CHAFING ON FUEL LINE TO FLOW DIVIDER.Dec 6, 2001 · Reims F406 · Ignition Harness (Distribution)SDR AUS20011004Pump · failed(AUS) HYDRAULIC PUMP FAULTY. INVESTIGATION FOUND THE PUMP CIRCLIP GROOVE WORN ALLOWING THE CIRCLIP TO SEPARATE AND THE SPLINE ADAPTER PNO 24100-646 TO DISENGAGE FROM THE ENGINE DRIVE.Sep 18, 2001 · Reims F406 · Hydraulic Pump (Electric/Engine), MainSDR AUS20010690Detector · faulty(AUS) LIFT DETECTOR FAULTY. INVESTIGATION FOUND THAT THE AIRCRAFT WIRING (WIRE NO A2K4S-20P3) HAD BEEN CUT APPROXIMATELY 76.2MM (3IN) UP FROM THE FORWARD SIDE CONSOLE CONNECTOR AND CONNECTED TO THE STALL WARNING HORN. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED MOJul 2, 2001 · Reims F406 · Stall Warning SystemSDR AUS20010655Detector · faulty(AUS) LIFT DETECTOR FAULTY. SWITCH OPERATES IN OPPOSITE SENSE.Jun 26, 2001 · Reims F406 · Stall Warning SystemSDR AUS20010734Control Cable · worn(AUS) LH AND RH AILERON CABLES (4OFF) LOCATED IN WING WORN.Jun 22, 2001 · Reims F406 · Aileron Control SystemSDR AUS20010656Detector · faulty(AUS) LIFT DETECTOR FAULTY. DETECTOR MICROSWITCH OPERATES IN OPPOSITE SENSE. SWITCH SPRING LOADED UP. PERSONNEL/MAINTENANCE ERROR.MANUFACTURING ERROR.Jun 20, 2001 · Reims F406 · Stall Warning SystemSDR 20010511CW009Hose · rupturedHOSE PN 156F001-12D0196 MANUFACTURED IQ99 INSTALLED 3, 00 RUPTURED IN FLIGHT DUMPING OIL ON LEFT ENGINE.Apr 26, 2001 · N5CE · Cessna 425 · Engine Oil Storage (Airframe Furnished)SDR AU010004Computer · faulty(AUS) AUTOPILOT COMPUTER SUSPECT FAULTY.Jan 4, 2001 · Reims F406 · Autopilot ComputerSDR CA001016009Door Frame · cracked(CAN) A CRACK WAS FOUND IN THE LOWER MAIN CABIN DOOR. THE CRACK WAS LOCATED ON THE FRAME ASSEMBLY IN THE RADIUS TO THE FLANGE WHERE THE SEAL RETAINER STRIP IS ATTACHED AROUND THE FRAME. (SEE ATTACHED PC REFERENCE). THE FRAME PART NUMBER IS 5711145-4. THE CRACKSep 20, 2000 · Cessna 425 · Passenger/Crew DoorsSDR AU000837Switch · faulty(AUS) LEFT AUTOFEATHER MICROSWITCH FAULTY. (X)Aug 28, 2000 · Reims F406 · Propeller Feathering/ReversingSDR AU000881Wire · misinstalled(AUS) NR 2 FIRE BOTTLE SQUIB WIRING INCORRECTLY WIRED TO THE BOTTLE ARM/FIRING SWITCH. SUBMITTER STATED THIS WOULD HAVE PREVENTED OPERATION OF THE FIRE BOTTLE. SUSPECT MANUFACTURING ERROR. (X)Aug 10, 2000 · Reims F406 · Extinguishing SystemSDR AU000912Strut · failed(AUS) NOSE LANDING GEAR OLEO OVER EXTENDED ALLOWING TORQUE LINKS TO INVERT. CAUSED BY OLEO UPPER BEARING LOOSENING FROM PISTON BARREL. (X)Jul 6, 2000 · Reims F406 · Nose/Tail Landing Gear Strut/AxleSDR AU000559Mount · cracked(AUS) LEFT ENGINE MOUNT CRACKED. FOUND DURING MAGNETIC PARTICLE INSPECTION.Jul 4, 2000 · Reims F406 · Engine Mount SectionSDR AU000203Retainer · damaged(AUS) LEFT PROPELLER FEEDBACK RING RETAINING CIRCLIP DEFORMED. PROPELLER WENT TO UNCOMMANDED FULL REVERSE ON LANDING.Apr 20, 2000 · Reims F406 · Propeller Blade SectionSDR AU990934Fitting · faulty(AUS) NOSE LANDING GEAR ACTUATOR SUPPORT CHANNEL FASTENERS FAILED.Aug 25, 1999 · Cessna 425 · Landing Gear ActuatorSDR AU990927Stall Warning · faulty(AUS) STALL WARNING VANE TIGHT TO MOVE IN BEARINGS CAUSING INTERMITTENT STALL WARNING INDICATIONS.Aug 6, 1999 · Reims F406 · Stall Warning SystemSDR AU990401Frame · mismanufactured(AUS) CANTED RIB UPPER CAP AT FS 177.45 CONTAINED MISDRILLED HOLES. FOUND DURING INSPECTION IAW RHEIMS SERVICE BULLETIN CAB 98-16.Jan 28, 1999 · Reims F406 · Fuselage Main, FrameSDR AU981565Rib · cracked(AUS) CANTED RIB CRACKED. FOUND DURING INSPECTION IAW SB CAB98-16.Nov 27, 1998 · Reims F406 · Fuselage Miscellaneous Structure
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