# Service difficulty reports: U/A Canada PT6A-28

A list on [U/A Canada PT6A-28](https://openairdocs.org/engine/u-a-canada-pt6a-28.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 19 · 944 reports

- [SDR 2024FA0000739](https://openairdocs.org/sdr/2024FA0000739.md): Gps · defective · Sep 26, 2024 · N98PM · Beech E90 · Global Positioning System
  > WHILE ENROUTE TO KLVS FROM KGUY, THE GARMIN GNS530W SCREEN SHUT OFF. WHILE TROUBLESHOOTING, A STRONG ELECTRICAL SMELL FILLED THE CABIN. THE AIRCRAFT DIVERTED TO KTDW FOR FURTHER EVALUATION BY THE MAINTENANCE TEAM. UPON FURTHER EVALUATION, IT HAS BEEN DETERMINE
- [SDR TIMA20220110010](https://openairdocs.org/sdr/TIMA20220110010.md): Door · unsecure · Aug 31, 2022 · N118MD · Beech 99A · Cargo/Baggage Doors
  > AFTER LOADING THE AIRCRAFT PILOT DID A FINAL WALK AROUND WHERE HE COMPLETED HIS CHECKLIST THAT ALL LATCHES WERE PUSHED IN AND LOCKED TO THE BEST OF MY KNOWLEDGE. AFTER A RUN UP THE TOOK OFF RUNWAY AND CLIMBING OUT OF 200 FEET PILOT FELT WHAT HE THOUGHT WAS TU
- [SDR T4OR2022071400002](https://openairdocs.org/sdr/T4OR2022071400002.md): Brake Assy · broken · Jul 14, 2022 · N29M · Beech E90 · Landing Gear Brake System
  > DURING LANDING ROLL-OUT BRAKING, THE LEFT BRAKE PEDAL WENT MOST OF ITS TRAVEL WITH LITTLE BRAKING EFFECT. IT WAS DISCOVERED THE LEFT BRAKE TORQUE PLATE WAS CRACKED AND OPENED UP SO CALIPER THE GUIDE PIN WAS NOT RETAINED IN THE TORQUE PLATE. TORQUE PLATE P/N
- [SDR KCQA20211130](https://openairdocs.org/sdr/KCQA20211130.md): Engine · failed · Nov 17, 2021 · N399CZ · Beech 99 · Engine (Turbine/Turboprop)
  > PILOT REPORTS "RH ENGINE SN PC-51404 FAILURE ON TAKEOFF ROLL. ALL ANNUNCIATORS WERE EXTINGUISHED AND ENGINE INSTRUMENTS IN THE GREEN. AS I BEGAN MY ROLLOUT AND BEFORE I COULD REACH THE DESIRED POWER SETTING, THERE WAS A POP FROM THE RH SIDE AND THE AIRPLANCE P
- [SDR KCQA202110412255](https://openairdocs.org/sdr/KCQA202110412255.md): Doubler · cracked · Oct 21, 2021 · N899CZ · Beech 99A · Fuselage Main, Bulkhead
  > REMOVED THE CRACKED BULKHEAD DOUBLER P/N 115-440026-3 S/N NSN AT FUSELAGE STATION TO 428.335 AT THE VERTICAL STABILIZER LOWER ATTACH BOLTS. INSTALLED A NEW BULKHEAD DOUBLER P/N 115-440026-3 S/N NSN IN ACCORDANCE WITH THE BEECHCRAFT MAINTENANCE MANUAL, CHAPTER
- [SDR 2021F00000](https://openairdocs.org/sdr/2021F00000.md): Drag Fitting · failed · Oct 14, 2020 · N499CZ · Beech 99A · Main Landing Gear Attach Section
  > DURING LANDING RT MAIN LANDING GEAR DRAG LEG FITTING FAILED.
- [SDR KCQA2020093000001](https://openairdocs.org/sdr/KCQA2020093000001.md): Fire Detector · false activation · Sep 30, 2020 · N199CZ · Beech 99 · Fire Detection
  > IN FLIGHT, PILOT RECEIVED FIRE INDICATION ON ENGINE NR 1 WHILE ON FINAL APPROACH. NO EVIDENCE OF FIRE WAS PRESENT AND WARNING EXTINGUISHED AFTER A FEW MINUTES. LEFT SIDE OF AIRCRAFT WAS FACING RISING SUN, IT IS BELIEVED THE FALSE WARNING MAY HAVE BEEN TRIGGE
- [SDR 2022FA0000771](https://openairdocs.org/sdr/2022FA0000771.md): Engine · malfunctioned · Jan 29, 2020 · N86NB · Beech A100 · Engine (Turbine/Turboprop)
  > ON 29TH JANUARY 2020, WHILE IN THE CRUISE AT 16000FT, THE PILOT REPORTED HEARING A INCREASING WHISTLING SOUND FROM THE PORT ENGINE WHICH STARTED STARTED TO LOSE POWER. HE LOOKED OUTSIDE AND NOTICE SPARKS COMING OUT THE EXHAUST AND IMMEDIATELY STARTED THE SHUTD
- [SDR CA190604005](https://openairdocs.org/sdr/CA190604005.md): Engine · shutdown · May 19, 2019 · Engine (Turbine/Turboprop)
  > (CAN) BEFORE TAKEOFF, THE PILOT REPORTED THAT THE ENGINE EXPERIENCED UN-COMMANDED ENGINE SHUTDOWN TOGETHER WITH A LOUD NOISE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED BACK TO BASE UNEVENTFULLY. THE ENGINE WILL BE SENT TO STANDARD AERO FOR INVESTIGATIO
- [SDR CA190108022](https://openairdocs.org/sdr/CA190108022.md): Line · leaking · Jan 3, 2019 · Engine Fuel Distribution
  > (CAN) CREW REPORTED A HIGHER FUEL CONSUMPTION ON LH ENGINE AS PER QUANTITY INDICATOR BUT FUEL FLOW WERE NORMAL ON BOTH ENGINES. DURING INVESTIGATION, MAINTENANCE FOUND A FUEL LEAK FROM THE LINE BETWEEN THE START CONTROL UNIT AND THE FUEL CONTROL UNIT OF THE #1
- [SDR KCQA20181206](https://openairdocs.org/sdr/KCQA20181206.md): Fire Warning · false indication · Dec 6, 2018 · N799CZ · Beech 99 · Fire Detection
  > PILOT RECEIVED A FIRE WARNING ON THE LT ENGINE. PERFORMED ENGINE FIRE PROCEDURE IAW COCKPIT CHECKLIST, VERIFIED FALSE WARNING. AFTER A SHORT PERIOD OF TIME WARNING CEASED. PART TOTAL TIME AND TOTAL CYCLES ARE UNKNOWN.
- [SDR TIMA2018102500001](https://openairdocs.org/sdr/TIMA2018102500001.md): Oil System · low pressure · Oct 22, 2018 · N99GH · Beech 99A · Turbine Engine Oil System
  > DURING CRUISE, PILOT NOTED LEFT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED, AND VERIFIED WITH LOW OIL PRESSURE ON THE GAUGE. PILOT SHUT DOWN THE ENGINE AND RETURNED SAFELY WITH NO FURTHER INCIDENT TO SLC, THE ORIGINAL DEPARTURE POINT. FURTHER INVESTIGATION TO
- [SDR KCQA2018090400001](https://openairdocs.org/sdr/KCQA2018090400001.md): Fire Detector · false activation · Sep 4, 2018 · N499CZ · Beech 99A · Fire Detection
  > IN FLIGHT PILOT RECEIVE FIRE INDICATION ON NR 1 ENGINE. ENGINE SHUTDOWN IAW EMERGENCY PROCEDURES. DURING EXAMINATION OF ENGINE AND NACELLE NO EVIDENCE OF FIRE WAS PRESENT.
- [SDR 2019F00061](https://openairdocs.org/sdr/2019F00061.md): Boot · detached · Aug 13, 2018 · N9029R · Beech E90 · Propeller Deice Boot Section
  > 08-11-2018 THE AIRCRAFT HAD A PROPELLER DE-ICE BOOT REPLACED THAT HAD FALLEN OFF. 08-12-2018 ON A FLIGHT, THE BOOT DETACHED FROM THE PROPELLER AND WAS REPAIRED. 08/15/2018 AT APPROXIMATELY 17:10, AT ABOUT 1000' AGL, THE PILOT HEARD A POP IN THE COCKPIT, C
- [SDR CA180117004](https://openairdocs.org/sdr/CA180117004.md): Bracket · cracked · Jan 16, 2018 · Beech E90 · Trailing Edge Flaps
  > (CAN) DURING ROUTINE MAINTENANCE DISCOVERED FLAP TRACK BRACKET CRACKED AT REAR OF SLOT. (TC NR 20180117004).
- [SDR CA160307007](https://openairdocs.org/sdr/CA160307007.md): Starter · malfunctioned · Mar 4, 2016 · Beech 100BEECH · Engine Starter
  > (CAN) RIGHT STARTER REMAINED ENERGIZED.
- [SDR CA160205009](https://openairdocs.org/sdr/CA160205009.md): Relay · failed · Feb 3, 2016 · Beech A100 · AC Inverter
  > (CAN) DURING TAKEOFF, THE NR 1 INVERTER FAILED. NR 2 INVERTER WAS SELECTED BY CREW BUT IT WAS ALSO FAILED. WITH THIS DOUBLE FAILURE CREW LOST MOST OF ENGINES INSTRUMENTS. ACFT LAND BACK IN YVP WITHOUT ANY ISSUES. MAINTENANCE FOUND ANNUNNCIATOR RELAY TO BE F
- [SDR CA160129007](https://openairdocs.org/sdr/CA160129007.md): Nut · loose · Jan 29, 2016 · Beech A100 · Starter-Generator
  > (CAN) DURING A SCHEDULED FUEL PUMP INSPECTION, THE STARTER GENERATOR AS BEEN REMOVED TO GIVE MORE ACCESS TO THE ENGINE FUEL PUMP. THE MECHANIC DISCOVER THAT SOME OF THE STARTER FRONT PLATE RETAINING SCREW WHERE LOOSE. THE STARTER SHAFT HOLDING NUT WAS FOUND
- [SDR CA160128002](https://openairdocs.org/sdr/CA160128002.md): Terminal · unsecure · Jan 26, 2016 · Beech A100 · Electrical Power System Wiring
  > (CAN) WHILE COMPLETING AD CF-1981-25R6, IT WAS WAS NOTED AFTER REMOVING WING PANEL INBOARD OF RT NACELLE, THAT 2 WIRES (P83D0 P83B0) WERE DISCONNECTED FROM THE EXTERNAL POWER TERMINAL STRIP AND BY ARCING, HAD BURNED A HOLE IN THE WING SPAR. A FLEET INSPECTION
- [SDR JIKA2016012201](https://openairdocs.org/sdr/JIKA2016012201.md): Flex Hose · leaking · Jan 18, 2016 · N199AF · Beech B99 · Turbine Engine Oil System
  > ON CLIMB OUT, THE PILOT REPORTED THAT AFTER THE CABIN BLEED HEAT WAS TURNED ON, THE COCKPIT RAPIDLY FILLED WITH SMOKE. THE PILOT TURNED THE BLEED HEAT OFF & COMPLETED THE SMOKE IN COCKPIT CHECKLIST, THE SMOKE DISSIPATED. THE PILOT NOTIFIED ATC OF THE ISSUE,
- [SDR CA160203013](https://openairdocs.org/sdr/CA160203013.md): Oil System · leaking · Jan 17, 2016 · Beech A100 · Turbine Engine Oil System
  > (CAN) THE AIRCRAFT WAS FORCED TO RETURN TO THE DEPARTURE AIRPORT FOLLOWING THE PRESENCE OF SMOKE IN THE COCKPIT. THE AIRCRAFT LANDED SAFELY. THE SMOKE IN COCKPIT WAS DUE TO OIL LEAK, FROM THE RT ENGINE, ON A PREVIOUS HSI RUN. THERE WAS A SMALL AMOUNT OF RES
- [SDR CA160115001](https://openairdocs.org/sdr/CA160115001.md): Control Panel · burned · Jan 11, 2016 · Beech A100 · Fuel Quantity Indicator
  > (CAN) AFTER HAVING COMPLETED HIS COCKPIT PRE-FLIGHT CHECKS AND WITH ALL ELECTRICAL POWER TURNED OFF, THE PILOT WENT OUTSIDE AND WAS PERFORMING HIS EXTERNAL ACFT PRE-FLIGHT CHECKS. THE PILOT THEN NOTICED FLAMES IN THE AREA OF THE LT SIDE COCKPIT WINDOW. HE T
- [SDR CA160106011](https://openairdocs.org/sdr/CA160106011.md): Channel · cracked · Jan 4, 2016 · Beech 100BEECH · Passenger/Crew Doors
  > (CAN) PRIOR TO DEPARTURE FROM BASE THE CREW WAS UNABLE TO CLOSE THE CABIN DOOR. MAINTENANCE INVESTIGATION REVEALED A 14" CRACK IN THE CABIN ENTRANCE DOOR CHANNEL PN 50-430043-619. THE CABIN DOOR HINGE, PN 50-430043-547 ATTACHES DIRECTLY TO THIS CHANNEL. THER
- [SDR CA160107006](https://openairdocs.org/sdr/CA160107006.md): Support · cracked · Dec 28, 2015 · Beech A100 · Wing, Attach Fittings
  > (CAN) DURING VISUAL INSPECTION IN THE ELEVATOR TORQUE TUBE AREA, THE RT ELEVATOR TORQUE TUBE SUPPORT WAS FOUND CRACKED. THE TORQUE TUBE AND SUPPORT ASSY WAS REPLACED AND ACFT RETURNED TO SERVICE.
- [SDR CA151126002](https://openairdocs.org/sdr/CA151126002.md): Skin · torn · Nov 24, 2015 · Beech 100BEECH · Ailerons
  > (CAN) ON PRE-FLIGHT INSPECTION, THE FLIGHT CREW NOTICED A LARGE TEAR ON THE OTBD SECTION OF THE RT AILERON. THE TEAR STEMMED FROM THE OVERLAP BETWEEN THE L/E AND T/E SKINS. MM 27-10-00, PG 202 HAS A SPECIAL NOTE TO INSPECT THIS AREA OF THE RT AILERON. UNFORTU
- [SDR CA151102003](https://openairdocs.org/sdr/CA151102003.md): Torque Tube · cracked · Oct 26, 2015 · Beech 100BEECH · Elevator Control System
  > (CAN) TORQUE TUBE FOUND CRACKED. THOSE BEEN REPLACED IN THE LAST 4 YEARS. ON ATTACHMENT YOU WILL FOUND PICTURE AND THE LIST OF ACFT AFFECTED WITH THE SAME REPLACEMENT IN THE LAST 6 YEARS. ACFT MFG SHOULD HAVE A EXPLANATION ABOUT THIS ISSUE SINCE THOSE ARE BUY
- [SDR CA151016003](https://openairdocs.org/sdr/CA151016003.md): Volt Regulator · failed · Oct 13, 2015 · Beech A100 · DC Regulator
  > (CAN) ON ACFT SHORT COMING IN TESTING PROCEDURES WAS DISCOVERED WHILE FOLLOWING THE MM FOR THE ADJUSTMENT OF THE VOLTAGE REGULATORS FOR THE GENERATORS. WHEN THE ACFT IS EQUIPPED WITH VR-1010-24-1A VOLTAGE REGULATORS AS ALLOWED BY MFG SERVICE INSTRUCTION NR 07
- [SDR CA151009007](https://openairdocs.org/sdr/CA151009007.md): Bolt · cracked · Oct 8, 2015 · Beech A100 · Wing, Attach Fittings
  > (CAN) DEFECT INDICATIONS WERE NOTED DURING LIQUID PENETRANT INSPECTION OF BOTH FORWARD UPPER AND LOWER WING ATTACHMENT BOLTS ON THE LT AND RT SIDES WHILE COMPLETING INSPECTION REQUIREMENT OF AD CF-81-25-R6. ALL 4 BOLTS, 2 OF PN 81784-14-32 LOWER FWD BOLTS AND
- [SDR CA151006005](https://openairdocs.org/sdr/CA151006005.md): Blade · failed · Oct 5, 2015 · Beech A100 · Turbine Section
  > (CAN) ENGINE WAS SENT FOR INVESTIGATION AND REPAIR AFTER AN IN-FLIGHT SHUTDOWN INCIDENT. THE INCIDENT STARTED WITH A LOUD NOISE FROM THE ENGINE WITH A SUBSEQUENT TORQUE DROP AND INCREASE OF THE ENGINE TEMPERATURE. THE ENGINE WAS SHUTDOWN AND THE FLIGHT WAS CON
- [SDR CA150903008](https://openairdocs.org/sdr/CA150903008.md): Control Cable · corroded · Sep 3, 2015 · Beech A100 · Aileron Tab Control System
  > (CAN) DURING AND INSPECTION IN THE LT WING ROOT AREA, IT WAS NOTED THAT THE AILERON TRIM AND AILERON PRIMARY CABLES WERE HEAVILY CORRODED. ONLY LITTLE HAND PRESSURE ON THE TRIM CABLE CAUSED THE CABLE TO BREAK DUE TO IT BEING EXTREMELY BRITTLE. FURTHER INVESTIG
- [SDR CA150731003](https://openairdocs.org/sdr/CA150731003.md): Engine · power loss · Jul 27, 2015 · Engine (Turbine/Turboprop)
  > (CAN) PILOTS REPORTED THE RT ENGINE LOST POWER WITH T5 INCREASE MORE THAN 730 DEGREES CELSIUS WHEN TAKE OF POWER WAS APPLIED. THE ACFT RETURNED TO ITS PARKING FOR INVESTIGATION.
- [SDR CA150930011](https://openairdocs.org/sdr/CA150930011.md): Limit Switch · faulty · Jul 6, 2015 · Beech 100BEECH · Landing Gear Position and Warning
  > (CAN) GEAR WOULD NOT RETRACT.
- [SDR CA150708004](https://openairdocs.org/sdr/CA150708004.md): Bonding Strap · crushed · Jul 4, 2015 · Beech A100 · Trailing Edge Flaps
  > (CAN) DURING A TRAINING FLIGHT SMOKE WAS OBSERVED IN THE CABIN. AIRCRAFT LANDED, MAINTENANCE FOUND THE FLAPS CIRCUIT BREAKER HAD POPPED AND THE FLAP MOTOR WAS UNSERVICEABLE AND THE CAUSE OF THE SMOKE. IT WAS DISCOVERED THAT THE RIGHT HAND INBOARD FLAP HAD A BO
- [SDR CA150618004](https://openairdocs.org/sdr/CA150618004.md): Socket · intermittent · Jun 15, 2015 · Beech A100A · Landing Gear Position and Warning
  > (CAN) AFTER GEAR DOWN SELECTION, FLIGHT CREW DID NOT GET A GREEN LIGHT INDICATION OF RIGHT MAIN GEAR BEING DOWN & LOCKED. NO GEAR IN TRANSIT LIGHT WERE ILLUMINATED. AFTER WIGGLING THE LIGHT SOCKET, RIGHT MAIN GEAR GREEN INDICATOR LIGHT ILLUMINATED, INDICATIN
- [SDR CA150618005](https://openairdocs.org/sdr/CA150618005.md): Torque Knee · broken · Jun 11, 2015 · Beech A100 · Main Landing Gear Strut/Axle/Truck
  > (CAN) AFTER TOUCHDOWN THE PILOTS FELT A VIBRATION, ACFT STOPPED THEN TAXIED TO THE RAMP & IT WAS FOUND THAT THE LT MLG, UPPER & LOWER TORQUE LINK WERE FOUND BROKEN OFF AT ATTACH POINT. THE TORQUE LINKS WERE REPLACED. ACFT INSPECTED & RETURNED TO SERVICE. W
- [SDR CA150511007](https://openairdocs.org/sdr/CA150511007.md): Torque Link · broken · May 10, 2015 · Beech A100 · Main Landing Gear Strut/Axle/Truck
  > (CAN) UPON LANDING, PILOT FELT LIKE HE HAD A FLAT. NO FLAT NOTED BUT UPON INSPECTION, IT WAS NOTED THAT THE RT MLG UPPER TORQUE LINK WAS FOUND TO BE BROKEN IN HALF ABOUT ONE INCH FROM THE ATTACH POINT TO THE LOWER TORQUE LINK. SPECIAL INSPECTION HAS BEEN INI
- [SDR CA150428006](https://openairdocs.org/sdr/CA150428006.md): Pressure Switch · intermittent · Apr 24, 2015 · Beech A100 · Hydraulic System, Main
  > (CAN) HYDRAULIC PRESSURE SWITCH INTERMITENT, FOUND DIRTY, LOCATED IN LT WHEEL WELL AREA, CLEANED AND TESTED, RE-INSTALLED AND PERFORMED 18 GEAR CYLCES THROUGHOUT THE DAY, RESPECTING MOTOR COOL DOWN TIMES, IAW SERVICE MANUAL, NO PROBLEMS FOUND.
- [SDR CA150417014](https://openairdocs.org/sdr/CA150417014.md): B-Nut · split · Apr 14, 2015 · Beech A100 · Turbine Engine Oil System
  > (CAN) DURING ROUTINE MAINTENANCE, SOME OIL LOSS, CLEANED AND TUBE B-NUT FOUND SPLIT.
- [SDR KCQA2015040901](https://openairdocs.org/sdr/KCQA2015040901.md): Display · malfunctioned · Apr 9, 2015 · N299CZ · Beech 99 · Cabin Temperature Control System
  > PILOT PRIMARY FLIGHT DISPLAY (PFD), DISPLAYED A TURN IN THE OPPOSITE DIRECTION PROVIDED MISLEADING AND INACCURATE DATA TO THE PILOT IN COMMAND DURING A TURN AFTER TAKEOFF. PILOT DIVERTED TO NEAREST SUITABLE AIRPORT. AFTER UNLOADING THE CARGO AND ON A SUBSEQUEN
- [SDR CA150407007](https://openairdocs.org/sdr/CA150407007.md): Radio · malfunctioned · Mar 31, 2015 · Beech A100 · Communications System
  > (CAN) CREW HAD A FAILURE OF RADIO`S AND WERE UNABLE TO CONTACT ATC CREW CYCLED AVIONICS MASTER SYS ALL TESTED SERVICEABLE. FLIGHT CONTINUED WITH NO FURTHER PROBLEMS.
- [SDR CA150324012](https://openairdocs.org/sdr/CA150324012.md): Tube · dislodged · Mar 24, 2015 · Beech A100 · Propeller Feathering/Reversing
  > (CAN) THE PILOT OF THE ACFT ABORTED TAKEOFF WHEN HE RECEIVED AN OVERTORQUE INDICATION FROM THE RT ENGINE. WHILE TAXIING BACK TO THE TERMINAL, THE PILOT TRIED TO UNFEATHER THE RT PROPELLER WITHOUT SUCCESS. THE PILOT REPORTED THE DEFECT IN THE ACFT JOURNEY LOG
- [SDR CA150224002](https://openairdocs.org/sdr/CA150224002.md): Engine · unresponsive · Feb 3, 2015 · Engine (Turbine/Turboprop)
  > (CAN) ENGINE WOULD NOT DECELERATE ON APPROACH. NO THROTTLE RESPONSE ON APPROACH AFTER 2HR FLIGHT. SUSPECT FROZEN P3 LINE.
- [SDR CA150119008](https://openairdocs.org/sdr/CA150119008.md): Housing · failed · Jan 16, 2015 · Piper PA31T · Hydraulic System, Main
  > (CAN) DURING APPROACH THE CREW SELECTED GEAR DOWN AND THE GEAR WOULD NOT EXTEND. THEY MANUALLY EXTENDED THE GEAR BUT THE NOSE WOULD NOT FULLY GO DOWN. AFTER ATTEMPTS TO EXTEND THE NOSE GEAR THEY LANDED WITH THE NOSE GEAR NOT EXTENDED. AFTER INSPECTION AND TALK
- [SDR CA150116003](https://openairdocs.org/sdr/CA150116003.md): Engine · malfunctioned · Jan 14, 2015 · Beech 100BEECH · Engine (Turbine/Turboprop)
  > (CAN) ENGINE WOULD NOT DECELERATE ON APPROACH, NO THROTTLE RESPONSE ON APPROACH AFTER 2HR FLIGHT, SUSPECT FROZEN P3 LINE (TC# 20150116003)
- [SDR CA141219003](https://openairdocs.org/sdr/CA141219003.md): Gearbox · making metal · Dec 17, 2014 · Beech A100 · Turbine Engine Reduction Gear
  > (CAN) SHORTLY AFTER TAKEOFF, THE LEFT PROPELLER AUTO FEATHERED. THE ENGINE WAS NOT SHUTDOWN AS THE PROP WAS ALREADY FEATHERED. THE CREW LANDED SAFELY. INVESTIGATION BY MAINTENANCE REVEALED SOME METAL CONTAMINATION IN THE RGB OIL STRAINER. THE ENGINE WILL BE
- [SDR CA141205008](https://openairdocs.org/sdr/CA141205008.md): Bearing · failed · Dec 4, 2014 · Beech 200BEECH · Air Distribution Fan
  > (CAN) AIRCRAFT TOOK OFF, DURING CLIMB APPROX. 7000` AGL CREW NOTED AN ODOR IN THE CABIN. THE CABIN THEN STARTED TO FILL WITH SMOKE. THE CREW REQUESTED A RETURN. MAINTENANCE FOUND THAT THE CABIN VENTILATION BLOWER DID NOT WORK. THE VENTILATION BLOWER WAS REM
- [SDR CA141208007](https://openairdocs.org/sdr/CA141208007.md): Shaft · cracked · Nov 20, 2014 · Beech A100 · Trailing Edge Flap Actuator
  > (CAN) DETAILED INSPECTION OF BOLTED CONNECTION AT RT INBOUND FLAP ACTUATOR - REVEALED A CRACK- RUNNING FROM THE RIVET HOVE DOWN THE LENGTH OF THE SHAFT APPROX. 1 INCH. AN ENTIRE NEW ACTUATOR WAS INSTALLED.
- [SDR CA141014010](https://openairdocs.org/sdr/CA141014010.md): Hinge Bracket · cracked · Oct 11, 2014 · Beech A100 · Horizontal Stabilizer Structure
  > (CAN) THE RIGHT HAND HORIZONTAL STABILIZER HINGE BRACKET WAS FOUND CRACKED DURING VISUAL INSPECTION. THE INSPECTION WAS BEING COMPLETED DUE TO OTHER COMPANY AIRCRAFT HINGE BRACKETS HAD BEEN RECENTLY FOUND CRACKED DURING SCHEDULED INSPECTION.
- [SDR CA141003005](https://openairdocs.org/sdr/CA141003005.md): Torque Knee · cracked · Oct 2, 2014 · Beech A100 · Main Landing Gear
  > (CAN) DURING REGULAR ACFT INSPECTION, A CRACK WAS FOUND ON THE LT MLG TORQUE KNEE UPPER LINK.
- [SDR CA140929006](https://openairdocs.org/sdr/CA140929006.md): Wire · misrouted · Sep 26, 2014 · Beech A100 · Landing Gear System Wiring
  > (CAN) ON GEAR DOWN SELECTION ON APPROACH, THE CREW EXPERIENCED A DOUBLE GENERATOR FAILURE WHICH LEFT THE GEAR ONLY PARTIALLY EXTENDED. THE GENERATORS WOULD NOT RESET AND THE EMERGENCY LANDING GEAR EXTENSION WOULD NOT EXTEND THE GEAR FURTHER. THE AIRCRAFT LAND

Next page: https://openairdocs.org/engine/u-a-canada-pt6a-28/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 = 'PT6A28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/u-a-canada-pt6a-28/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.