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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.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.SDR AUS20040496Truss · corroded(AUS) LT ENGINE LOWER LT ATTACHMENT TRUSS CORRODED.SDR AUS20040374Wire · broken(AUS) FLAP CONTROL SYSTEM WIRE BROKEN. FAULT TRACE TO BROKEN WIRE A157B-A25799200 TO FLAP UP CONTROL SWITCH.SDR AUS20040350Strip · separated(AUS) STALL STRIP MISSING.SDR AUS20040385Computer · faulty(AUS) AUTOPILOT COMPUTER FAULTY.SDR AUS20040214Clamp · failed(AUS) LT ENGINE PROPELLER REVERSING LEVER CABLE CLAMP BOLT FAILED ALLOWING PROPELLER REVERSING PY LEVER TO DISCONNECT FROM PUSH/PULL CABLE.SDR 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.SDR AUS20040137Servo · faulty(AUS) AUTOPILOT ROLL SERVO CAPSTAN FOUND IN PIECES ON AIRCRAFT FLOOR. SIX FASTENEING SCREWS FOUND IN CLOSE PROXIMITY TO THE SERVO MOUNT.SDR AUS20040059Altimeter · faulty(AUS) ALTIMETER FITTED TO AIRCRAFT WITH INCORRECT ALTITUDE RANGE. PERSONNEL/MAINTENANCE ERROR.SDR AUS20040060Altimeter · faulty(AUS) ALTIMETER FITTED TO AIRCRAFT WITH INCORRECT ALTITUDE RANGE. PERSONNEL/MAINTENANCE ERROR.SDR AUS20040071Controller · failed(AUS) COMMUNICATION SYSTEM CONTROL BOX FAILED.SDR 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 PROPELLSDR 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 SEVESDR 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.SDR 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.SDR AUS20031013Switch · faulty(AUS) RT MAIN LANDING GEAR UPLOCK SWITCH FAILED.SDR AUS20031155Wire · broken(AUS) FLAP UP MICROSWITCH WIRE BROKEN. SWITCH IS LOCATED BEHINDFLAP SELECTOR.SDR AUS20030775Motor · failed(AUS) FORWARD AIR CONDITIONER ELECTRIC MOTOR FAILED.SDR AUS20030575Radome · bird strike(AUS) BIRDSTRIKE ON SURVEILLANCE RADOME.SDR AUS20030457Switch · failed(AUS) NOSE LANDING GEAR ACTUATOR FAULTY. SWITCH OUT OF ADJUSTMENT.SDR 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.SDR AUS20030378Actuator · faulty(AUS) NOSE LANDING GEAR ACTUATOR FAULTY.SDR AUS20021189Lead · broken(AUS) STARTER-GENERATOR FAULTY. INSPECTION FOUND SEVERAL BRUSH LEADS BROKEN AND COMMUTATOR DAMAGED.SDR 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.SDR AUS20020918Link · cracked(AUS) COPILOTS OUTBOARD BRAKE PEDAL RH LINK ASSEMBLY CRACKED IN THE AREA OF THE WELD ATTACHING THE CLEVIS RODEND.SDR 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.SDR 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.SDR 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 HOPSDR AUS20011294Cooling Fan · failed(AUS) SURVEILLANCE RADAR COOLING FAN FAILED.SDR 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.SDR AUS20011310Channel · cracked(AUS) NOSE LANDING GEAR ACTUATOR ATTACHMENT STRUCTURE CHANNEL CRACKED.FOUND DURING INSPECTION IAW AD/F406/7.SDR AUS20011311Ignition Lead · chafed(AUS) RT IGNITER LEAD ON BOTH ENGINES CHAFING ON FUEL LINE TO FLOW DIVIDER.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.SDR 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 MOSDR AUS20010655Detector · faulty(AUS) LIFT DETECTOR FAULTY. SWITCH OPERATES IN OPPOSITE SENSE.SDR AUS20010734Control Cable · worn(AUS) LH AND RH AILERON CABLES (4OFF) LOCATED IN WING WORN.SDR AUS20010656Detector · faulty(AUS) LIFT DETECTOR FAULTY. DETECTOR MICROSWITCH OPERATES IN OPPOSITE SENSE. SWITCH SPRING LOADED UP. PERSONNEL/MAINTENANCE ERROR.MANUFACTURING ERROR.SDR 20010511CW009Hose · rupturedHOSE PN 156F001-12D0196 MANUFACTURED IQ99 INSTALLED 3, 00 RUPTURED IN FLIGHT DUMPING OIL ON LEFT ENGINE.SDR AU010004Computer · faulty(AUS) AUTOPILOT COMPUTER SUSPECT FAULTY.SDR 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 CRACKSDR AU000837Switch · faulty(AUS) LEFT AUTOFEATHER MICROSWITCH FAULTY. (X)SDR 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)SDR AU000912Strut · failed(AUS) NOSE LANDING GEAR OLEO OVER EXTENDED ALLOWING TORQUE LINKS TO INVERT. CAUSED BY OLEO UPPER BEARING LOOSENING FROM PISTON BARREL. (X)SDR AU000559Mount · cracked(AUS) LEFT ENGINE MOUNT CRACKED. FOUND DURING MAGNETIC PARTICLE INSPECTION.SDR AU000203Retainer · damaged(AUS) LEFT PROPELLER FEEDBACK RING RETAINING CIRCLIP DEFORMED. PROPELLER WENT TO UNCOMMANDED FULL REVERSE ON LANDING.SDR AU990934Fitting · faulty(AUS) NOSE LANDING GEAR ACTUATOR SUPPORT CHANNEL FASTENERS FAILED.SDR AU990927Stall Warning · faulty(AUS) STALL WARNING VANE TIGHT TO MOVE IN BEARINGS CAUSING INTERMITTENT STALL WARNING INDICATIONS.SDR AU990401Frame · mismanufactured(AUS) CANTED RIB UPPER CAP AT FS 177.45 CONTAINED MISDRILLED HOLES. FOUND DURING INSPECTION IAW RHEIMS SERVICE BULLETIN CAB 98-16.SDR AU981565Rib · cracked(AUS) CANTED RIB CRACKED. FOUND DURING INSPECTION IAW SB CAB98-16.
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