# Service difficulty reports: U/A Canada PT6A-11

A list on [U/A Canada PT6A-11](https://openairdocs.org/engine/u-a-canada-pt6a-11.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 75 reports

- [SDR FXTA20250718001](https://openairdocs.org/sdr/FXTA20250718001.md): Pressure Switch · failed · Jul 15, 2025 · N753BA · Cessna 208B · Aircraft Fuel Distribution System
  > LOW FUEL PRESSURE ANNUNCIATOR WITH ENGINE RUNNING AND ELECTRIC BOOST PUMP ON.
- [SDR COEA2025012901897](https://openairdocs.org/sdr/COEA2025012901897.md): Engine · contaminated · Jan 28, 2025 · N897FE · Cessna 208B · Engine (Turbine/Turboprop)
  > FLIGHT NUMBER:4701 ROUTE: KGEG-KPSC DISCREPANCY: EXPERIENCED SMOKE IN THE COCKPIT, DECLARED AN EMERGENCY PERFORMED AIR TURN BACK TO KGEG CORRECTIVE ACTION: CLEANED DEICE FLUID FROM ENGINE COWLING, RAN ENGINE PER C208 CHECKLIST FOR 10 MINUTES WITH HEAT ON, NO A
- [SDR QMLA2024090620107](https://openairdocs.org/sdr/QMLA2024090620107.md): Warning Message · illuminated · Sep 4, 2024 · N316PM · Pilats PC1245 · Central Warning
  > DURING CLIMB FROM GJT, AT ABOUT 1000 AGL, I RECEIVED A MASTER WARNING ESSENTIAL BUS AND SEVERAL MASTER CAUTION LIGHTS GEN1, GEN2, AND BAT. THE QRH DOESN'T GIVE GUIDANCE ON THE SPECIFIC CONDITION I HAD (MULTIPLE BUS FAILURES SIMULTANEOUSLY). RETURNED TO BASE A
- [SDR 2023FA0000768](https://openairdocs.org/sdr/2023FA0000768.md): Lock Nut · missing · Jun 12, 2023 · Cessna 208B · Engine Air Intake System
  > WE WERE INFORMED THAT THE LAST COUPLE OF TREND NUMBERS WERE LOOKING A BIT HIGH FOR NG & ITT. BEFORE THE NEXT FLIGHT, WE LOOKED AT THE INERTIAL SEPARATOR AND FOUND THAT THE VANE HAD PLAY. A WASHER WAS ALSO FOUND IN THE BOTTOM OF THE ENGINE COWL. A PIVOT POINT O
- [SDR CGHR2021011401000](https://openairdocs.org/sdr/CGHR2021011401000.md): Mount · cracked · Jan 14, 2021 · N555FH · Beech 300BEECH · Engine Mount Section
  > CRACKS HAVE BEEN FOUND IN THE FIELD DURING ROUTINE VISUAL INSPECTIONS OF ENGINE MOUNT TRUSS/COWLING MOUNT ATTACH BRACKETS. THE CRACKS FOUND ARE ALMOST ALWAYS EXCLUSIVE TO THE UPPER RIGHT ENGINE MOUNT TRUSS (NR 1 ENGINE TRUSS UPPER INBOARD, NR 2 ENGINE TRUSS U
- [SDR AU3R2017041233286](https://openairdocs.org/sdr/AU3R2017041233286.md): Connector · burned · Apr 12, 2017 · N52PF · Piper PA31T · Ice/Rain Protection System Wiring
  > DURING CRUISE FLIGHT, ALL ANTI-ICE CIRCUIT BREAKERS TRIPPED. CREW SMELLED SMOKE. PROCEDED TO MAKE A NORMAL LANDING. OPENED THE FORWARD NOSE PANELS AND FOUND CONNECTOR E462, JUST FORWARD OF PRESSURE BULKHEAD, COMPLETELY BURNED AND MELTED ON BOTH HALVES AND
- [SDR 6CBA2016111816156](https://openairdocs.org/sdr/6CBA2016111816156.md): Pressure Switch · failed · Nov 18, 2016 · N531AF · Pilats PC1247E · Fuel Indicating System
  > AFTER DEPARTING,IN CRUISE FLIGHT THE FLIGHT CREW REPORTED BOTH FUEL PUMPS CYCLING ON & OFF 5 SEC. INTERVALS. COMPLETED QRH PROCEDURE, CYCLING PERSISTED. THE AIRCRAFT MADE AN UNSCHEDULED LANDING WHERE IT LANDED SAFELY. THE MAINTENANCE CREW ON SITE INSPECTED THE
- [SDR CA150604004](https://openairdocs.org/sdr/CA150604004.md): Engine · power loss · May 24, 2015 · Engine (Turbine/Turboprop)
  > (CAN) AFTER DEPARTURE, FIRST ENGINE LOST POWER FOLLOWED BY THE LOSS OF THE SECOND ENGINE WITHIN 20 MINUTES. THE PILOT PERFORMED A FORCED LANDING AROUND 20 NM OUT OF DESTINATION AIRPORT. ALL 7 PASSENGER AND 2 CREW ON BOARD SUFFERED MINOR INJURIES.
- [SDR RU3A20140204006](https://openairdocs.org/sdr/RU3A20140204006.md): Tube · ruptured · Feb 4, 2015 · N71 · Beech 300BEECH · Engine Bleed Air System
  > WITH RT BLEED AIR PNEUMATIC ENV OFF, RT BLEED FAIL LIGHT INTERMITTENT ON & OFF. FOUND & REPLACED RUPTURED EVA TUBE.
- [SDR CA141218007](https://openairdocs.org/sdr/CA141218007.md): Oil System · leaking · Dec 7, 2014 · Dhav DHC8102 · Engine (Turbine/Turboprop)
  > (CAN) DURING FLIGHT, ON APPROACH, THE STAND-BY GENERATOR WARNING ILLUMINATED. AN UNEVENTFUL LANDING WAS ACCOMPLISHED AT DESTINATION. POST-FLIGHT INSPECTION REVEALED OIL ON THE SIDE OF THE AIRCRAFT AND NO OIL SHOWING ON THE ENGINE DIPSTICK. 4 QUARTS OF OIL WERE
- [SDR RU3A20141112040](https://openairdocs.org/sdr/RU3A20141112040.md): Solenoid · dirty · Oct 30, 2014 · N75 · Beech 300BEECH · Propeller Controlling System
  > WITH FLAPS IN APPROACH MODE, ACFT EXPERIENCED SLIGHT YAW TO THE RT. AS POWER WAS FURTHER REDUCED FOR LANDING, THE YAW INCREASED. PILOT WAS UNABLE TO CORRECT WITH RUDDER & AILERON. AFTER GO AROUND AT SAFE ALTITUDE, FLIGHT CREW ATTEMPTED TO DUPLICATE THE PROB
- [SDR SBAA201400001](https://openairdocs.org/sdr/SBAA201400001.md): Panel · deformed · Apr 15, 2014 · N858FE · Cessna 208B · Airfoil Anti/De-ice System
  > DURING VISUAL INSPECTION NOTICED THAT LT & RT WING INBD TKS PANELS WERE SLIGHTLY DEFORMED ALONG LE FROM APPROX WS 37.00 TO WS 51.00. TKS PANELS DID NOT APPEAR LOOSE & SEEMED TO OPERATE NORMALLY.
- [SDR QMLA2013121913177](https://openairdocs.org/sdr/QMLA2013121913177.md): Control Valve · intermittent · Dec 19, 2013 · N613NA · Pilats PC1245 · Cabin Cooling System
  > FLIGHT NURSE NOTIFIED PILOT OF A BURNING SMELL IN BACK OF CABIN. NO FIRE WARNING INDICATIONS OR ENG INSTRUMENT IRREGULARITIES WERE SHOWING & NO SIGNS OF BURNING SMELL OR FIRE IN COCKPIT UNTIL SEVERAL MINUTES LATER. PILOT WAS BESIEGED WITH A NOXIOUS, CHEMICAL
- [SDR QMLA2013120413172](https://openairdocs.org/sdr/QMLA2013120413172.md): Flap · malfunctioned · Dec 4, 2013 · N129JW · Pilats PC1245 · Trailing Edge Flap Control System
  > ON APPROACH TO LANDING BELOW 163 KIAS SELECTED FLAP POSITION TO 15 DEGREES. FLAPS FAILED TO MOVE, MASTER CAUTION & AMBER FLAP CAWS LIGHT ILLUMINATED. COMPLETED NO FLAP LANDING WITHOUT FURTHER INCIDENT.
- [SDR 2013FA0000036](https://openairdocs.org/sdr/2013FA0000036.md): Tie Rod · loose · Dec 17, 2012 · N824VA · Piper PA31T1 · Turbine Engine Compressor Section
  > ENGINE WAS REMOVED FOR COMPRESSOR FOD. ON DISASSEMBLY AT AN APPROVED CRS, IT WAS DETERMINED THE COMPRESSOR TIE BOLTS HAD LOST THE TIE ROD STRETCH (TORQUE) ON 4 OF THE 6 TIE BOLTS. RESULTING IN COMPRESSOR BOWING (IMBALANCE) RESULTING IN COMPRESSOR RUB DOD. P
- [SDR 2013FA0000038](https://openairdocs.org/sdr/2013FA0000038.md): Tie Rod · loose · Oct 27, 2012 · N93SH · Piper PA31T1 · Turbine Engine Compressor Section
  > ENGINE WAS REMOVED FOR COMPRESSOR SEIZED AND COMPRESSOR FOD. UPON DISASSEMBLY AT CRS, IT WAS DETERMINED THE COMPRESSOR TIE BOLTS WERE FOUND TO HAVE NO STRETCH ON 4 OF 6. RESULTING IN COMPRESSOR IMBALANCE AND SEVERE RUB, SEIZING. POSSIBLE CAUSE: IMPROPER ASS
- [SDR 2010FA0001197](https://openairdocs.org/sdr/2010FA0001197.md): Warning Light · illuminated · Nov 22, 2010 · N105SL · Piagio P180 · Door Warning System
  > RED CABIN DOOR ANNUNCIATOR IN FLIGHT.
- [SDR E81RTT402984](https://openairdocs.org/sdr/E81RTT402984.md): Seal · leaking · Jun 5, 2010 · N155SL · Piagio P180 · Passenger/Crew Doors
  > (E81R) INVESTIGATED FLIGHT CREW REPORT OF CABIN DOOR SEAL ANNUNCIATOR LIGHT INDICATION ABOVE FL200. DRAINED SMALL AMOUNT OF WATER FROM DOOR SEAL DRAIN AND REPAIRED MINOR LEAK IN SEAL. HAVE HAD A SIMILAR DISCREPANCY IN OTHER ACFT. RECOMMEND MFG OR OPERATOR INVE
- [SDR CA090914010](https://openairdocs.org/sdr/CA090914010.md): Connector · misinstalled · Aug 3, 2009 · Bell 212 · Engine (Turbine/Turboprop)
  > (CAN) ACTUATOR CONNECTOR FOR SPHERICAL BEARING SCREW LOCK CUP INCORRECTLY LOCKED FROM MANUFACTURER. (TC# 20090914010)
- [SDR TT197941](https://openairdocs.org/sdr/TT197941.md): Motor · worn · Aug 11, 2006 · N5626Y · Beech B300 · Landing Gear Retraction/Extension System
  > ELECTRIC LANDING GEAR EXTENSION FAILED INFLIGHT. NORMAL LANDING ACCOMPLISHED USING MANUAL GEAR EXTENSION. LANDING GEAR MOTOR BRUSHES FOUND WORN EXCESSIVELY, COMMUTATOR PITTED. OVERHAULED MOTOR INSTALLED, NEW FILTER INSTALLED. GEAR RETRACTION CHECKS PERFORM
- [SDR 2006FA0000584](https://openairdocs.org/sdr/2006FA0000584.md): Trim Tab · mismanufactured · Jun 2, 2006 · N690GT · Beech C90 · Rudder, Tab Structure
  > WHEN INSPECTED IAW SB, THIS AC WAS IDENTIFIED AS MISSING THE DRAIN PROVISIONS. C/A WAS TAKEN IAW SB. DURING OUR RESEARCH INTO THIS MATTER IT WAS IDENTIFIED THAT THE CCORRELATING AD TO THIS ISSUE. THIS IS A NEARLY NEW AC. (K)
- [SDR GUU2006F00010](https://openairdocs.org/sdr/GUU2006F00010.md): Master Cylinder · inoperative · Jan 23, 2006 · N82539 · Beech 1900D · Master Cylinder/Brake Valve
  > DURING TAXI, LT PEDAL WENT FLAT. RETURNED TO GATE. REPLACED FO LT MASTER CYLINDER. (K)
- [SDR 2005FA0001589](https://openairdocs.org/sdr/2005FA0001589.md): Wire · chafed · Nov 29, 2005 · N5641X · Beech C90A · Landing Gear System Wiring
  > INVESTIGATED REPEATED INTERMITTENT LANDING GEAR RETRACT/ EXTENSION SYSTEM FAULTS. FOUND WIRES G45F22 AND G10L22 FOR NOSE LANDING GEAR DOWNLOCK SWITCH CHAFING ON ENVIRONMENTAL AIR CROSS-OVER DUCT IN LOWER RT NOSE KEEL AREA. REPAIRED DAMAGED WIRING AS REQUIRED
- [SDR CA051104005](https://openairdocs.org/sdr/CA051104005.md): Engine · making metal · Oct 7, 2005 · Piper PA31T · Engine (Turbine/Turboprop)
  > (CAN) IN FLIGHT, COMPRESSOR SPEED DECREASED UNCOMMANDED ACCOMPANIED BY AN INCREASE IN TURBINE TEMPERATURE. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED FOR AN UNSCHEDULED LANDING. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE ENGINE OIL A
- [SDR 2005FA0001227](https://openairdocs.org/sdr/2005FA0001227.md): Bearing · detached · Aug 26, 2005 · N195AA · Piper PA31T · Main Landing Gear Strut/Axle/Truck
  > FOUND UPPER BRGS SEPARATED FROM PISTON TUBES DUE TO PINS MIGRATING INTO PISTON TUBE, TURNING UPPER BRG LOOSE, PINS THEN BACKED OUT AND FELL OUTSIDE PISTON TUBE, LOCKED UP MAIN GEAR SHOCK STRUT TRAVEL. CAUSE OF PINS MIGRATING, TURNING UPPER BRGS LOOSE WAS THAT
- [SDR 2005FA0000181](https://openairdocs.org/sdr/2005FA0000181.md): Bearing · failed · Feb 6, 2005 · N893MC · Beech B300 · Starter-Generator
  > SHAFT BEARING AT THE COOLING FAN END OF THE S/G CAME APART. THIS CAUSE THIS END OF THE COMMUTATOR TO MOVE SIDE TO SIDE AND THE COOLING FUN RUBBED INTO THE HOUSING. (K)
- [SDR 341024](https://openairdocs.org/sdr/341024.md): Engine · failed · Dec 3, 2004 · N124CJ · Beech 1900D · Engine (Turbine/Turboprop)
  > RIGHT ENGINE FAILURE INFLIGHT.
- [SDR 197041](https://openairdocs.org/sdr/197041.md): Engine · shutdown · Jul 14, 2004 · N191CJ · Beech 1900D · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FAILED IN CLIMB, ENGINE SHUT DOWN EMERGENCY DECLARED AND RETURNED TO BLOCK (REASON FOR FAILURE STILL TO BE DETERMINED).
- [SDR HSY2004F00000](https://openairdocs.org/sdr/HSY2004F00000.md): Transmitter · malfunctioned · Apr 30, 2004 · N730FX · Cessna 208B · Fuel Quantity Indicator
  > UPON REMOVAL OF RT WING NR 3 OB FUEL TRANSMITTER, PART WAS FOUND MISSING THE ROLL PIN THAT SECURES THE FLOAT ARM TO THE TRANSMITTER ASSY. FUEL TRANSMITTER INSPECTION WAS PERFORMED ON 2/19/04. THE SERIAL NR OF THIS TRANSMITTER WAS NOT APPLICABLE TO THE SERIAL
- [SDR WIW2004F00000](https://openairdocs.org/sdr/WIW2004F00000.md): Pin · separated · Sep 12, 2003 · N208JW · Cessna 208 · Nose/Tail Landing Gear
  > NOSE LANDING GEAR STRUT WAS RESEALED 5/1/01 SO FAILURE OCCURED AFTER THAT TIME. AIRCRAFT WAS HAVING RECURING SHIMMY PROBLEMS WHICH LED TO THE STRUT DISASSEMBLY FOR INSPECTION. DURING INSPECTION THE LOWER PLUG WAS FOUND SEPARATED FROM METERING PIN ASSEMBLY CA
- [SDR FDJ2003F00000](https://openairdocs.org/sdr/FDJ2003F00000.md): Wheel · failed · May 15, 2003 · N126AR · Cessna 208B · Cabin Cooling System
  > PILOT REPORTED NO AIR MOVEMENT FROM EYE BALL VENTS WHEN AIR CONDITION WAS SELECTED. TROUBLESHOOTING REVEALED LEFT AND RIGHT WHEEL ASSEMBLIES HAD FAILED AT BLOWER ASSEMBLY SHAFT ATTACHMENTS. THE WHEEL IS MANUFACTURED FROM LIGHT/THIN ALUMINUM AND THE PLATE THA
- [SDR 2003FA0000506](https://openairdocs.org/sdr/2003FA0000506.md): Strut · defective · Apr 16, 2003 · N603TC · Cessna 182S · Main Landing Gear Strut/Axle/Truck
  > THE DIAMETER OF THE OLOE TUBE IS.0012 INCHES SMALLER THAN THE BORE OF THE FORK. THE FORK WAS HELD ON ONLY BY THE NR5 BOLT. THE OLEO TUBE HAS AN UNUSUAL WEAR PATTERN OF CIRCUMFERENTIAL WEAR AND RIDGES. IT IS BELIEVED THAT THIS OLEO WAS DEFECTIVE FROM THE MA
- [SDR CSA2003F00000](https://openairdocs.org/sdr/CSA2003F00000.md): Fire Detector · broken · Apr 15, 2003 · N217CS · Piper PA31T3 · Fire Detection
  > ON 11 APR 03, THE RIGHT ENGINE FIRE LIGHT CAME ON INTERMITTENTLY IN FLIGHT. THE AIRCRAFT WAS LANDED IN WBB WITHOUT INCIDENT, AND THE FIRE LIGHT CAME ON STEADY AT TOUCHDOWN. NO OTHER SIGN OF FIRE PRESENT, AND ENGINE WAS SHUT DOWN AT FIRST SAFE OPPORTUNITY. T
- [SDR BAQA085117](https://openairdocs.org/sdr/BAQA085117.md): Indicator · inoperative · Mar 10, 2003 · N90LF · Beech C90 · Attitude Gyro and Indicating System
  > ATTUTUDE INDICATOR LEANS TO ONE SIDE. STRAIGHT AND LEVEL. REPLACED WITH SERVICEABLE UNIT.
- [SDR TIM2003F00000](https://openairdocs.org/sdr/TIM2003F00000.md): Spar Cap · corroded · Mar 3, 2003 · N236AL · Beech C99 · Wing Spar
  > DURING AN ANNUAL WING OUTBOARD UPPER AND LOWER MAIN SPAR CAP INSPECTION SEVERAL SMALL SPOTS WERE NOTICED. FURTHER INVESTIGATING REVEALED CONSIDERABLE CORROSION.
- [SDR OEZ2003F00000](https://openairdocs.org/sdr/OEZ2003F00000.md): Hinge Bracket · broken · Feb 12, 2003 · N227SA · Dhav DHC6 · Horizontal Stabilizer Structure
  > DURING SCHEDULED INSPECTION MAINTENANCE PERSONNEL FOUND RIGHT ELEVATOR OUTBOARD HINGE PLATE LOOSE WITH RIVETS (WORKING) AT ATTACHMENT TO OUTBOARD STABILIZER RIB. UPON DISASSEMBLY FOR REPAIR. HINGE PLATE BRACKET WAS FOUND CRACKED AND BROKEN AWAY FROM FORWARD
- [SDR S2YA03006](https://openairdocs.org/sdr/S2YA03006.md): Squat Switch · dirty · Feb 9, 2003 · N831SK · Beech 1900D · Landing Gear Position and Warning
  > AFTER TAKEOFF OF FLIGHT 1007, THE GEAR INTRANSIT LIGHT ILLUMINATED WITH THE GEAR HANDLE UP AFTER, THE GEAR SHOULD HAVE RETRACTED. THE CREW MADE AN AIR TURNBACK. MECHANIC INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT UPLOCK SWITCH. MECHANIC OPS CHECK THE SYS
- [SDR LX52003F00000](https://openairdocs.org/sdr/LX52003F00000.md): Valve · sticking · Jan 24, 2003 · N981LL · Beech B300 · Ice Detection
  > THERE IS A PERSISTANT PROBLEM WITH THIS SERIES BRAKE DEICE VALVE STICKING IN THE OPEN POSITION. THIS PROBLEM SEEMS TO BE GREATER DURING THE WINTER (EXTREME COLD) BUT IT DOES OCCUR AT ALL TIMES OF THE YEAR.
- [SDR LX52003F00001](https://openairdocs.org/sdr/LX52003F00001.md): Valve · sticking · Jan 24, 2003 · N981LL · Beech B300 · Ice Detection
  > THERE IS A PERSISTANT PROBLEM WITH THIS SERIES BRAKE DEICE VALVE STICKING IN THE OPEN POSITION. THIS PROBLEM SEEMS TO BE GREATER DURING THE WINTER (EXTREME COLD) BUT IT DOES OCCUR AT ALL TIMES OF THE YEAR.
- [SDR S2YA03004](https://openairdocs.org/sdr/S2YA03004.md): Starter Gen · inoperative · Jan 23, 2003 · N118SK · Beech 1900D · Starter-Generator
  > AFTER STARTING THE NR 2 ENGINE, THE CREW HAD DIFFIUCULTY GETTING THE NR2 GENERATOR ON LINE. THEN THERE WAS A FIRE INDICATION ON THE RIGHT ENGINE, THE CREW PULLED THE FIRE HANDLE BUT DID NOT BLOW THE BOTTLE. MECHANIC INSPECTED THE SYSTEM AND FOUND THE RIGHT G
- [SDR AMW1](https://openairdocs.org/sdr/AMW1.md): Intercostal · failed · Nov 27, 2002 · N146ZV · Beech 1900D · Cargo/Baggage Doors
  > AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A VIBRATION PROBLEM. THE CARGO DOOR ANNUNCIATOR WAS EXTINGUISHED PRIOR TO NR 2 ENGINE START. TAKE OFF ROLL WAS NORMAL. JUST AFTER ROTATION, A VIBRATION BEGAN. THE LANDING GEAR RETRACTED AND THE ENGINE INSTRUMENTS WERE NO
- [SDR CGO2002F00005](https://openairdocs.org/sdr/CGO2002F00005.md): Pressure Switch · malfunctioned · Nov 15, 2002 · N8283S · Beech 2000 · Fuel Indicating System
  > REPLACED PRESSURE SWITCH ASSEMBLY. PILOT COMPLAINT OF LOW FUEL PRESSURE WARNING LIGHT COMING ON ALTITUDE. HAVE NOTED THIS TO BE A REOCCURRING PROBLEM WITH NEW -27 SWITCH ASSEMBLY. OLDER DASH NUMBER SWITCH ASSEMBLY USUALLY HAD A MUCH LONGER TBF RATE. PRESSU
- [SDR 2002FA0001335](https://openairdocs.org/sdr/2002FA0001335.md): Torque Tube · corroded · Nov 12, 2002 · N195AA · Piper PA31T · Rudder Control System
  > FLIGHT CONTROLS, RUDDER TORQUE TUBE/ RIBS CORROSION PRESENT, REPAIRABLE.
- [SDR 2002FA0001336](https://openairdocs.org/sdr/2002FA0001336.md): Torque Tube · corroded · Nov 12, 2002 · N855JL · Piper PA31T1 · Rudder Control System
  > DURING COMPLIANCE OF SB (RUDDER FLIGHT CONTROLS) TORQUE TUBE ASSEMBLY AND ASSOCIATED RIBS WERE NOTED TO BE NON-REPAIRABLE. CORROSION PRESENT.
- [SDR FFS2002F00008](https://openairdocs.org/sdr/FFS2002F00008.md): Latch · broken · Nov 2, 2002 · N575Q · Beech 1900C · Entrance Stairs
  > LOWER AFT AIRSTAIR DOOR LATCH CABLE BROKE, PREVENTING DOOR BEING OPENED. PASSENGERS HAD TO EXIT THRU CARGO DOOR. WHEN THE AIRSTAIR DOOR IS CLOSED, ANY DIRT OR MOISTURE ON THE TREADS IS FUNNELLED TOT HE LOWER PULLEY FOR THIS CABLE. THIS CABLE IS BLENDED AND
- [SDR QFY2002F00002](https://openairdocs.org/sdr/QFY2002F00002.md): Transorb · failed · Nov 1, 2002 · N875DM · Beech B200 · Landing Gear Retraction/Extension System
  > TRANSORB FAILED TO SHORTED CONDITION. RESULTED IN LANDING GEAR CIRCUIT BREAKER TO POP CAUSING NEED FOR MANUAL EXTENSION OF LANDING GEAR.
- [SDR PF212LW](https://openairdocs.org/sdr/PF212LW.md): Windshield · failed · Oct 29, 2002 · N212LW · Beech B200 · Flight Compartment Windows
  > INNER PANE OF PILOTS WINDSHIELD SHATTERED WHILE CLIMBING THROUGH 28000 FEET.
- [SDR 2002FA0001259](https://openairdocs.org/sdr/2002FA0001259.md): Fork · cracked · Oct 21, 2002 · N4PT · Beech B200 · Nose/Tail Landing Gear Strut/Axle
  > FOUND HOLE FORK CRACKED, INSTALLED KIT.
- [SDR 2002FA0001268](https://openairdocs.org/sdr/2002FA0001268.md): Bolt · corroded · Oct 4, 2002 · N5335R · Piper PA46500TP · Wheel/Ski/Float
  > DURING A TIRE REPLACEMENT ON THE RT MAIN WHEEL ASSEMBLY, ALL WHEEL THRU BOLTS FOUND WORN AND CORRODED. THERE WAS NO TYPE OF ANTI-SEIZE LUBRICANT ON THE BOLTS. PIPER MAINTENANCE MANUAL DOES NOT REQUIRE ANY ANTI-SEIZE LUBRICAN ON THE THRU BOLTS.
- [SDR PG22002F00000](https://openairdocs.org/sdr/PG22002F00000.md): Switch · shorted · Oct 1, 2002 · N200VC · Beech B300 · Attitude Gyro and Indicating System
  > PILOTS HEADING SYSTEM CONTINUOUSLY ROTATED COUNTER CLOCKWISE. TROUBLESHOT PROBLEM TO A2S2 IN THE CCU65 CONTROL UNIT. FOUND SPRING INTERNAL TO SWITCH SHORTED TO OPPOSITE TERMINAL. REPLACEMENT OF SWITCH CURED PROBLEM. A HEIGHT QUALITY SWITCH, OR INSULATION A

Next page: https://openairdocs.org/engine/u-a-canada-pt6a-11/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/u-a-canada-pt6a-11/reports

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