U/A Canada PT6A-11

Service difficulty reports · 75

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 = 'PT6A11'
  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 JOU2002F00002Wire · chafedPILOT REPORTED FLASHING BEACON TRIPPED CIRCUIT BREAKER INTERMITTENTLY. TROUBLESHOT BEACON CIRCUIT AND FOUND WIRE INSULATION CHAFING ON RIB LOCATED IN RUDDER FIN TIP ASSEMBLY. CONVELEX TUBING WAS FOUND INSTALLED ON WIRE HARNESS, IT WAS NOT SECURED TO PREVENTSep 26, 2002 · N125AR · Cessna 208B · Light System WiringSDR 2003FA0000179Latch · unsecureCARGO DOOR DEPARTED AIRCRAFT. AFTER INSPECTION OF THE REAR CARGO DOOR UPON ITS RECOVERY, IT WAS NOTED THAT AN ATTEMPT MAY HAVE BEEN TRIED TO OPEN THE DOOR ON THE AIRCRAFT AND THE DOOR WAS NOT FULLY SECURED WHEN THE AIRCRAFT DEPARTED. TESTING ON THE GROUND SHSep 26, 2002 · N204SA · Dhav DHC6300 · Cargo/Baggage DoorsSDR TIM2002F00016Attach Fitting · crackedCRACK FOUND IN RIGHT WING ATTACH FITTING. (BATH TUB FITTING) LOCATION CENTER SECTION UPPER FORWARD ATTACH FITTING. RECURRING INSPECTION INTERVAL (STANDARD SPAR WITH STAP) 500 HOURS OR 1 YEARS WHICHEVER OCCURS FIRST. (CONTROL NUMBER 005)Sep 24, 2002 · N950AA · Beech B99 · Wing, Attach FittingsSDR AMW2002F00003Pump · failedWHILE FLIGHT WAS ENROUTE, THE LT LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CREW THEREFORE RETURNED THE AIRCRAFT TO THE FIELD WITHOUT ANY FURTHER INCIDENT. THE CORRECTIVE ACTION WAS THAT REPLACED THE LT LOW PRESSURE ENGINE DRIVEN FUEL PUMP.Sep 16, 2002 · N244YV · Beech 1900D · Engine Fuel DistributionSDR AMW2002F00002Link · brokenAFTER DEPARTURE, THE FLAPS STILL INDICATED 17 DEGREES AFTER SELECTED UP. WHILE TRYING TO RECYCLE THE FLAPS, THE INDICATOR MOVED TO 35 DEGREES. THE FLAP INDICATOR HAD BECOME STUCK. THE CREW ASKED TO RETURN TO THE FIELD, BUT DID NOT DECLARE AN EMERGENCY. THESep 14, 2002 · N166YV · Beech 1900D · Trailing Flap Position Indicating SystemSDR AMW2002F00004Switch · dirtyDURING THE INITIAL CLIMB, THE CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CREW THEN RETURNED TO THE FIELD WITHOUT ANY FURTHER INCIDENT. NO TEARDOWN REPORT IS REQUIRED. THE CORRECTIVE ACTION WAS THAT THE DOOR SWITCH WAS CLEANED.Sep 11, 2002 · N231YV · Beech 1900D · Door Warning SystemSDR HSY2002F0000ABulkhead · crackedSTRUCTURAL DEFECT DISCOVERED DURING SCHEDULED INSPECTION (PHASE 5). METAL FATIGUE, CANTED BULKHEAD, STRUCTURAL REPAIR INITIATED, AND WORK IS IN PROCESS.Sep 10, 2002 · N924FE · Cessna 208B · Fuselage Main, BulkheadSDR ESM2002F00000Tire · splitPILOT NOTED AFTER LAST LANDING, SPLITS/TEARS APPROXIMATELY 1 INCH IN LENGTH, BETWEEN OUTBOARD TREAD IN GROOVE OF TIRE.Sep 5, 2002 · N112BC · Piper PA42 · TireSDR GUU2002F00001Bolt · looseAT SCHEDULED ROUTINE INSPECTION VERTICAL FIN LOWER ATTACH BOLTS REQUIRED RETORQUE. RETORQUED FOUR LOWER VERTICAL BOLTS IAW MM.Apr 12, 2002 · N49543 · Beech 1900D · FastenersSDR CGO2002F00000Tab · mismanufacturedTAB, LEFT ELEVATOR. RECEIVED TAB ASSEMBLY, LEFT ELEVATOR NEW FROM MANUFACTURER MISSING THE REQUIRED RIVETS. ASSEMBLY WAS BONDED AND PRIMERED BUT HAD NOT BEEN RIVETED.Apr 10, 2002 · N728AM · Beech B200 · Elevator StructureSDR 2002FA0000696Windshield · failedWAS AT FL 280 WHEN LOUD POP WAS HEARD AND SAW THE PILOT FRONT WINDSHIELD WAS SHATTERED. INITIATED AND EMERGENCY DESCENT AND LANDED AT AIRPORT FOR REPAIRS.Mar 22, 2002 · N350WH · Beech B300 · Flight Compartment WindowsSDR 2002FA0000387Windshield · brokenINNER PANE OF PILOT WINDSHIELD SHATTERED IN CRUISE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. WINDSHIELD HEAT CONTROLLER CHANGED IN CONJUNCTION WITH WINDSHIELD.Mar 19, 2002 · N969WB · Beech B200 · Flight Compartment WindowsSDR 2002FA0000395Windshield · brokenINNER PANE OF PILOT WINDSHIELD SHATTERED IN CRUISE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENCE. WINDSHIELD HEAT CONTROLLER CHANGED IN CONJUNCTION WITH WINDSHIELD. NO PROBABLE CAUSE FOR BREAKAGE.Mar 19, 2002 · N969WB · Beech B200 · Flight Compartment WindowsSDR 2002FA0000454Bolt · brokenUPON INSPECTION, FOUND RIGHT TOP ENGINE MOUNT BOLT BROKEN AT FIREWALL.Mar 1, 2002 · N75FL · Piper PA42720 · Engine Mount SectionSDR 2002FA0000198Washer · wrong partDURING A ROUTINE INSPECTION, FOUND THE ENGINE MOUNT BOLTS HAD AN960616L WASHERS INSTALLED UNDER BOLT HEADS (12 BOLTS ) TOTAL. THIS TYPE BOLT MUST HAVE MS20002C6 WASHERS.Jan 15, 2002 · N208LB · Cessna 208 · Engine Mount SectionSDR IJA2001F00000Bolt · damagedBOLT (PN NAS464P6-28M) RIDES INSIDE BUSHING (PN 105740X-YA1007) WHICH FITS INTO LOWER END OF DRAG BRACE AND ATTACHES TO A CASTING ON MAIN GEAR TRUNNION. AT 5338 AFTT, BOLT WAS FOUND TO HAVE STAGGERED SHANK DUE TO HIGH SHEAR LOAD. SHANK WAS STAGGERED APPROX .Dec 3, 2001 · N403EM · Beech C90 · Landing Gear Retraction/Extension SystemSDR COE2001F00001Servo · misalignedON CLIMB OUT FOR DEPARTURE, PILOT EXPERIENCED BINDING IN THE AILERON CONTROL SYSTEM. THE PILOT INITIATED AN AIR TURN BACK AND LANDED WITHOUT FURTHER INCIDENT. NO INFLIGHT EMERGENCY WAS DECLARED. TROUBLESHOOTING REVEALED THE COVER ON THE ROLL SERVO WAS MISALOct 5, 2001 · N775FE · Cessna 208B · Aileron Control SystemSDR 2001FA0000404Mount · crackedDURING NON ROUTINE INSPECTION OF ENGINE MOUNT, A CRACK WAS FOUND IN THE WELD OF THE LOWER RIGHT ATTACH POINT (RING TO AIRCRAFT SUPPORT) SHIMMY DAMPENER WAS IN GOOD CONDITION WITH NO LEAKS DETECTED. NOSE GEAR BUSHINGS WERE ALSO SATISFACTORY.Oct 1, 2001 · N9750B · Cessna 208B · Engine Mount SectionSDR WC72001F00000Link · corrodedTHE TRAILING LINK ASSEMBLY ON LEFT AND RIGHT MAIN LANDING GEAR HAD CORROSION AND PITTING PRESENT IN THE LIGHTENING BORE AT THE FORWARD OR UPPER END. PITTING IN AREAS WAS APPROXIMATELY .025. AFTER BLENDING AND REMAINING THICKNESS DETERMINED WITH UT THE PART WSep 19, 2001 · N425PL · Cessna 425 · Main Landing Gear Strut/Axle/TruckSDR TIMAP53Powerpack · inoperativeLANDING GEAR POWER PACK FAILED. INSPECTION OF THE POWER PACK REVELED MOTOR SHORTED, CAUSED BY INTERNAL LEAK IN THE POWER PACK. CREW LOWERED GEAR MANUALLY.Sep 6, 2001 · N216CS · Beech C99 · Landing Gear Retraction/Extension SystemSDR ER00101Control Cable · crossedDURING SCHEDULED INSPECTION, THE RIGHT HAND AILERON INTERCONNECT CABLE WAS FOUND TO BE CROSSED OVER THE PRIMARY RUDDER CONTROL CABLE (PT NO 46845-0)AT THE UNDERFLOOR SECTION AFT OF THE CABIN DOOR. THERE IS NO WEAR APPARENT AT THIS TIME, THE AIRCRAFT LOG BOOKSMay 2, 2001 · N2480X · Piper PA31T1 · Aileron Control SystemSDR 20010208CW010Fuel Cap · brokenUPON REMOVAL OF RT OUTBOARD FWD CAP, CAP FELL APART. PIN IN LOCKING TAP THAT SECURES CAP BODY TOGETHER IS LOOSE IN TAP AND FELL OUT, ALLOWING CAP TO FALL APART. REDESIGN OR MATERIAL CHANGE REQUIRED.Jan 9, 2001 · N845CA · Beech 1900D · Fuel StorageSDR CA000614063Bolt · sheared(CAN) UPON MAKING A QUICK/INSPECTION OF THE MAIN GEAR DRAG BRACES AND RODS, FOUND EXCESSIVE PLAY IN THE DOWNLOCK ROD AT THE CLEVIS BOLT. THE RT CLEVIS BOLT P/N 41789-000 WAS FOUND SHEARED; AND THE LT CLEVIS WORN ON ITS WAY TO SHEARING.Jun 7, 2000 · Piper PA31T1 · Landing Gear Retraction/Extension SystemSDR PNSA970101Oil Temp · highHIGH OIL TEMP INDICATION, PRECAUTIONARY SHUTDOWN PROBLEM NOT VERIFIED.Jan 2, 1997 · N700RD · Piper PA31T3 · Engine Oil TemperatureSDR 95ZZZX1664Bleed Valve · dirtyANC - DURING LANDING, RT ENGINE HAD AN INTERMITTENT COMPRESSOR STALL. THE LANDING WAS ABORTED DUE TO HIGH WINDS. THE PILOT SHUT DOWN RT ENGINE AND RETURNED TO ENA AND LANDED WITHOUT INCIDENT. ON INSPECTION OF THE RT ENGINE, THE BLEED VALVE WAS FOUND STUCK, Feb 15, 1995 · N314SC · Piper PA31T3 · Compressor Bleed Valve
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