# Service difficulty reports: U/A Canada PT6A-42A

A list on [U/A Canada PT6A-42A](https://openairdocs.org/engine/u-a-canada-pt6a-42a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 69 reports

- [SDR 2026FA0000671](https://openairdocs.org/sdr/2026FA0000671.md): Eva Tube · blown · Aug 24, 2026 · N888ET · Beech 200BEECH · Pneumatic Indicating System
  > IN ROUTE OVER KCOU WHEN THE MASTER CAUTION CAME ON AND THE LT BLEED FAIL LIGHT ILLUMINATED. THE PILOTS FOLLOWED THE CHKLIST & CLOSED LT BLEED VALVE. THE CHKLIST INSTRUCTED THEM TO DESCEND BELOW 14K. ASKED ATC, CENTER WAS VERY BUSY & TO GIVE THEM PRIORITY HAND
- [SDR 2026FA0000188](https://openairdocs.org/sdr/2026FA0000188.md): Windshield · cracked · Mar 13, 2026 · N667CC · Beech B200 · Flight Compartment Windows
  > DURING TAKEOFF FROM KBIL TO KHLN, THE CREW OBSERVED THE LEFT WINDSHIELD CRACK. THE CREW RETURNED TO KBIL WITHOUT INCIDENT.
- [SDR JBZA20260223001](https://openairdocs.org/sdr/JBZA20260223001.md): Fire Detector · false indication · Feb 18, 2026 · N911RX · Beech 200BEECH · Fire Detection
  > DURING CRUISE FLIGHT LEFT ENGINE FIRE WARNING LIGHT ILLUMINATED, DETERMINED NO FIRE EXISTED, LANDED AIRCRAFT OAKLAND IAP. MAINTENANCE DETERMINED FIRE DETECTOR WAS MALFUNCTIONING REPLACED THE LOWER NR 1 ENGINE FIREWALL DETECTOR SYSTEM OPERATIONAL TESTS SATISFAC
- [SDR G1IA20250928098](https://openairdocs.org/sdr/G1IA20250928098.md): Check Valve · faulted · Sep 28, 2025 · N6728H · Beech B200 · Fuel Controlling System
  > DURING CRUISE LT FUEL PRESSURE LIGHT ILLUMINATED. LT FUEL FLOW GAUGE ERRATIC. TURNING ON LT STNDBY PUMP HAD NO EFFECT ON FUEL FLOW. LT ENG BEGAN SPOOLING DOWN ON IT'S OWN. SECURED ENG IAW CHKLST. NO EXTERNAL ABNORMALITIES, LEAKS, SMOKE, FUMES, OR FLAMES N
- [SDR 2025FA0000676](https://openairdocs.org/sdr/2025FA0000676.md): Steering Sys · broken · Sep 26, 2025 · N774LK · Beech 200CBEECH · Landing Gear Steering System
  > WHILE MAKING AN INITIAL LANDING AT KAUS, THE TOUCHDOWN OF NLG DIDN'T FEEL THE SAME AS OTHER IN THIS ACFT. ASKED AUSTIN TOWER TO ASK OPS CAR DRIVING BY, TO TAKE A LOOK WITH THEIR SPOTLIGHT AT THE GEAR), THEY DID AND DIDN'T SEE ANYTHING ON THE GEAR OR LEAKING
- [SDR JBZA20250930001](https://openairdocs.org/sdr/JBZA20250930001.md): Fire Detector · failed insp · Sep 26, 2025 · N314RX · Urocop EC135P2 · Fire Detection
  > RETURNING TO BASE FROM SCENE CALL FIRE WARNING AUDIO GONG SOUNDED INTERMITTENTLY. REMOVED AND REPLACED FIRE WARNING UNIT PN L315M5007051 RMVD PL650 INSTALLED PL107, SYSTEM FUNCTIONAL CHECK SATISFACTORY. APPROXIMATELY SEVEN MINUTES AFTER DEPARTURE FIRE WARNIN
- [SDR 2025FA0000630](https://openairdocs.org/sdr/2025FA0000630.md): Control Horn · broken · Sep 9, 2025 · N267JK · Dtafr EVOLUTION · Elevator Control System
  > DURING CONDITIONAL INSPECTION AND OPENING UP AIRCRAFT FOR INSPECTION I WAS CHECKING FREEDOM OF MOVEMENT OF FLIGHT CONTROLS AND NOTICED THE LEFT ELEVATOR FELT BOUNCY AND THAT THEIR WAS TO MUCH PLAY IN THE CONTROL COMPARED TO THE RIGHT ELEVATOR. I CONTINUED TO I
- [SDR 2025FA0000558](https://openairdocs.org/sdr/2025FA0000558.md): Engine · power loss · Aug 20, 2025 · N960JP · Beech 200CBEECH · Engine (Reciprocating)
  > PARTIAL POWER LOSS ON TAKEOFF. REJECTED TAKEOFF LEFT SIDE. PERFORMED A VISUAL INSPECTION OF BOTH ENGINES WITH NO DEFECTS NOTED. PERFORMED ENGINE PERFORMANCE GROUND RUNS WITH NO ISSUES FOUND DURING RUNS. ALL PARAMETERS WITHIN LIMITS. AIRCRAFT TEST FLIGHT GOOD N
- [SDR 2025FA0000506](https://openairdocs.org/sdr/2025FA0000506.md): Blades · separated · Jul 13, 2025 · N712RH · Beech 200BEECH · Turbine Section
  > ON DESCENT THROUGH FL 130 THE CREW REPORTED THE LEFT ENGINE POWER ROLLED BACK FOLLOWED BY A LOUD POP SOUND.ALL INDICATION ON THE MFD ENGINE PARAMETERS INDICATED NORMAL. THE ENGINE WAS SECURED AND THE FLIGHT DIVERTED TO NORTH TEXAS REGIONAL AIRPORT (KGYI). FU
- [SDR JBZA20250714001](https://openairdocs.org/sdr/JBZA20250714001.md): Elec Connector · loose · Jul 9, 2025 · N911RX · Beech B200 · Fire Protection System Wiring
  > DURING FLIGHT LEFT ENGINE FIRE WARNING LIGHT ERRATICALLY FLASHES. ELECTED TO PRECAUTIONARY LAND BACK TO BASE. MAINTENACE DISCOVERED LOOSE FIRE DETECTION AMPLIFIER CONNECTOR BACKSHELL
- [SDR 2025FA0000405](https://openairdocs.org/sdr/2025FA0000405.md): Starter Gen · malfunctioned · Jun 16, 2025 · N774LK · Beech 200CBEECH · Starter-Generator
  > DURING CLIMB OUT OF KELP AIRCRAFT EXPERIENCED DUAL GENERATOR FAILURE AND LOST COMMUNICATION WITH ATC. AFTER PILOT RESET GENERATORS, HE WAS ABLE TO REGAIN COMMUNICATION WITH ATC AND PROCEEDED TO LAND BACK AT KELP. PILOT DID NOT DECLARE AN EMERGENCY. ATC DECLARE
- [SDR 2025F00121](https://openairdocs.org/sdr/2025F00121.md): Windshield · cracked · May 8, 2025 · N774LK · Beech 200CBEECH · Flight Compartment Windows
  > WINDSHIELD OUTER PANE SHATTERED DURING DECENT FROM FLIGHT LEVEL 21000 WITH WINDSHIELD HEAT ON.
- [SDR 2025FA0000338](https://openairdocs.org/sdr/2025FA0000338.md): Connector · dirty · Apr 25, 2025 · N997LM · Beech 200BEECH · Engine Oil System Wiring
  > DURING TAXI: LH ENG OIL PRESSURE INTERMITENT INDICATION
- [SDR 1LXA20250103004](https://openairdocs.org/sdr/1LXA20250103004.md): Unknown · smoke · Jan 3, 2025 · N711BN · Beech 65B90 · Air Distribution System
  > SMOKE IN COCKPIT, PILOT CLOSED BLEED VALVES & OPEN DUMP VALVE, SMOKE DISSIPATED IMMEDIATELY, LAND AT THE NEAREST AIRPORT SAFELY.
- [SDR 1LXA2025012800062](https://openairdocs.org/sdr/1LXA2025012800062.md): Unknown · smoke · Dec 30, 2024 · N711BN · Beech C90 · Air Distribution System
  > SMOKE IN CABIN
- [SDR GSAA2024050101](https://openairdocs.org/sdr/GSAA2024050101.md): Skin · dented · May 1, 2024 · N4416P · Piper PA46500TP · Wing, Plate/Skin
  > AIRCRAFT SUFFERED A BIRDSTRIKE ON CLIMB OUT FROM KCXY. ACFT CLIMBING THRU 2000 FT MSL WITH AUTOPILOT ENGAGED. CLIMB SPEED 140 KTS INDICATED CLIMB RATE APPROX 1700 FPM. ACFT ON AN APPROX HEADING OF 260 WHEN ATC ASSIGNED A LT TURN TO 180 FOR OUR CLIMB TO 8000 F
- [SDR 2024F00100](https://openairdocs.org/sdr/2024F00100.md): Motor · failed · Mar 21, 2024 · N205EJ · Beech B200 · Trailing Edge Flap Actuator
  > DEPARTED KBIL ENROUTE KMSO. AFTER TAKEOFF THE CREW REPORTED THAT THE FLAPS WOULD NOT RETRACT BEYOND THE APPROACH POSITION. THEY THEN RETURNED TO KBIL WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP MOTOR AND THE FLAPS OPS CHECKED GOOD.
- [SDR 2024F00053](https://openairdocs.org/sdr/2024F00053.md): Hose · deteriorated · Mar 7, 2024 · N667CC · Beech B200 · Navigation System
  > WHILE TAXIING OUT AT 0630 IN KBIL ENROUTE KMLS, PILOT REPORTED THAT LEFT AIRSPEED INDICATOR NEVER ROSE ABOVE 0. AVIONICS TROUBLESHOT AND FOUND A ROTTED HOSE TO LEFT PITOT PROBE. REPLACED HOSE AND PRESSURE LEAK CHECK OK.
- [SDR 2024F00005](https://openairdocs.org/sdr/2024F00005.md): Pitot System · false indication · Jan 8, 2024 · N205EJ · Beech B200 · Pitot/Static System
  > AFTER DEPARTING KBIL FOR KGGW THE CREW OBSERVED LOSS OF PRIMARY AIRSPEED INDICATION SO THEY RETURNED TO KBIL WITHOUT INCIDENT.
- [SDR 2024FA0000054](https://openairdocs.org/sdr/2024FA0000054.md): Valve · unknown · Jan 8, 2024 · N911TC · Piper PA46500TP · Landing Gear System
  > MALIBU AEROSPACE IS A SHOP THAT WORKS EXCLUSIVELY ON THE PA46 AIRCRAFT. WE HAVE BEEN EXPERIENCING AN INCREASE IN THE FREQUENCY OF REPLACEMENT AND AND EXTREMELY SHORT LIFE OF THE LANDING GEAR EMERGENCY RELEASE VALVES (PN: 101758-802). THE FAILURE HAS BEEN WITH
- [SDR 2024FA0000897](https://openairdocs.org/sdr/2024FA0000897.md): Compressor Blade · fractured · Mar 25, 2023 · N80GE · Cessna 208B · Turbine Engine Compressor Section
  > CT BLADE SEPARATED FROM ENGINE WITH ENGINE ONLY 3049 HRS AND 3090 CYCLES SINCE OEM REPAIR ON COMPRESSOR. AIRCRAFT WAS ON A CROSS COUNTRY FLIGHT OVER MOUNTAINS WHEN CT BLADES SEPARATED.
- [SDR G1IA202012211005](https://openairdocs.org/sdr/G1IA202012211005.md): Bolt · bent · Dec 21, 2020 · N1074G · Beech B200 · Landing Gear Retraction/Extension System
  > FAR 135.415 REPORT. PILOT REPORTS "ON DECEMBER 21, 2020 WHILE ATTEMPTING TO LAND AT TED STEVENS AIRPORT. THE LEFT MAIN LANDING GEAR SHOWED AN UNSAFE RED GEAR HANDLE WITH HORN AND THE LEFT MAIN GREEN INDICATION LIGHT WASN'T ILLUMINATED. I INFORMED THE ANCHOR
- [SDR O9IA20201212530](https://openairdocs.org/sdr/O9IA20201212530.md): Engine · power loss · Dec 12, 2020 · N530LM · Beech B200 · Engine (Turbine/Turboprop)
  > ON TAKE OFF FROM PANC PILOT ROTATED AND AT AN ALTITUDE OF ABOUT 200-300FT, THE LT ENGINE ROLLED BACK ON POWER. ENGINE REMAINED RUNNING AND CREW PULLED POWER BACK AND FEATHERED THE ENGINE. ENGINE REMAINED RUNNING AND ONCE LEVELED OFF AFTER DECLARING A RETURN
- [SDR G1IA202011231004](https://openairdocs.org/sdr/G1IA202011231004.md): Warning Light · illuminated · Nov 23, 2020 · N1074G · Beech B200 · Landing Gear Selector
  > FAR 135.415 REPORT PILOT REPORTS "AFTER DEPARTURE TO ANCHORAGE, I HAD A GEAR UNSAFE LIGHT IN THE HANDLE. WHEN I LOWERED THE GEAR I COULD NOT GET THREE GREEN. THE GEAR MOTOR CIRCUIT BREAKER POPPED OUT. I WAS ABLE TO PUMP THE GEAR DOWN AND HAD THREE GREEN PRI
- [SDR 2020FA0000509](https://openairdocs.org/sdr/2020FA0000509.md): Timer · inoperative · Nov 18, 2020 · N2418W · Piper PA46500TP · Propeller/Rotor Anti-Ice/De-Ice System
  > OWNER REPORTED THE PROPELLER HEAT CONSTANTLY FAILS WITHIN 30 SECONDS OF SELECTING PROP HEAT TO ON. A PREVIOUS SHOP HAD CHECKED PROP HEAT BOOT RESISTANCE, SLIP RING CLEANING, RELAY OPERATION AND TIMER OPERATION. THE DE-ICE BRUSHES AND TIMER WERE REPLACED AND
- [SDR G1IA202010041003](https://openairdocs.org/sdr/G1IA202010041003.md): O-Ring · leaking · Oct 24, 2020 · N1074G · Beech B200 · Aircraft Fuel Distribution System
  > FAR 135.415 REPORT. PILOT REPORTS "NORMAL DEPARTURE. CLIMBING OUT OF 10000 RIGHT ENGINE TORQUE REDUCED TO 1400 ON IT'S OWN. FUEL FLOW INCREASED TO 450. RETURNED TO PAFA WITH NORMAL LANDING". DURING INSPECTION, MAINTENANCE FOUND EVIDENCE OF RT ENGINE FUEL
- [SDR 2020FA0000425](https://openairdocs.org/sdr/2020FA0000425.md): Gearbox · corroded · Sep 29, 2020 · N334ST · Piper PA46500TP · Turbine Engine Reduction Gear
  > WHILE PERFORMING POST MAINTENANCE ENGINE RUNS, THE CHIP LIGHT ILLUMINATED. INSPECTION OF OIL AND FOUND IT TO BE CLOUDY. REMOVED OIL FILTER AND FOUND EVIDENCE OF WATER AND VERY FINE GRIT MATERIAL. REMOVED REDUCTION GEARBOX CHIP DETECTOR, NO CHIPS NOTED. OIL
- [SDR 2020FA0000441](https://openairdocs.org/sdr/2020FA0000441.md): Horn · failed · Aug 13, 2020 · N115NX · Pitcan PA4 · Landing Gear Steering System
  > THE PILOT DELIVERING N115NX TO THE DEALER EXPERIENCED A LOSS OF NOSE WHEEL STEERING CONTROL UPON LANDING, RESULTING IN THE AIRCRAFT MAKING A SEVERE TURN TO THE RIGHT. THE PLANE EXITED THE RUNWAY RUNNING THROUGH AN INFIELD AREA AND COMING TO REST ON A TAXIWAY.
- [SDR QZJA20200728001](https://openairdocs.org/sdr/QZJA20200728001.md): Packing · leaking · Jul 25, 2020 · N800TP · Beech 200BEECH · Landing Gear Brake System
  > THIS WAS A PART 91 LEG WITH NO PASSENGERS ON BOARD. THE LOSS OF CONTROL INCIDENT OCCURRED ON 7/26/20 AT APPROXIMATELY 1740 LOCAL TIME WHILE TAXIING ONTO RUNWAY 20. THIS WAS ACTUALLY OUR SECOND TAKE OFF ATTEMPT - THE FIRST ATTEMPT WAS ABORTED DUE TO NO INDICAT
- [SDR 2020FA0000419](https://openairdocs.org/sdr/2020FA0000419.md): Landing Gear · broken · Jul 3, 2020 · N89MA · Nose/Tail Landing Gear
  > MECHANICAL FAILURE OF AN UNDETERMINED COMPONENT IN THE NOSE GEAR ASSEMBLY. THIS RESULTED IN THE AIRCRAFT NOT RESPONDING TO PILOT INPUTS UPON LANDING, CAUSING THE AIRCRAFT TO EXIT THE PAVED RUNWAY SURFACE & SKID 100 YARDS IN THE GRASS. IMPRESSIONS ON THE RUNW
- [SDR G1IA2020032061001](https://openairdocs.org/sdr/G1IA2020032061001.md): Unknown · malfunctioned · Mar 16, 2020 · N1074G · Beech B200 · Landing Gear Retraction/Extension System
  > FAR 135.415 REPORT. PILOT REPORTS "PLACED LANDING GEAR HANDLE DOWN. LANDING GEAR FAILED TO EXTEND AND LANDING GEAR RELAY CIRCUIT BREAKER POPPED AFTER A FEW SECONDS. EXTENDEDLANDING GEAR MANUALLY IN ACCORDANCE WITH HANDBOOK PROCEDURE". REPAIR NOT COMPLETE AT TH
- [SDR G1IA2020031300000](https://openairdocs.org/sdr/G1IA2020031300000.md): Gcu · contaminated · Mar 10, 2020 · N351SA · Beech B200 · AC Regulator
  > FAR 1135.415 REPORT. PILOT REPORTS "LH GENERATOR DROPPED OFFLINE CAUSING A MASTER CAUTION. TRIED ONE RESET, BOTH VOLTMETERS STARTED FLUCTUATING. TURNED LH GEN BACK OFF AS PER CHECKLIST". MAINTENANCE INSPECTED LH STARTER/GENERATOR AND CONTROL SYSTEM. WHEN CENTE
- [SDR G1IA2020030600000](https://openairdocs.org/sdr/G1IA2020030600000.md): Powerpack · defective · Mar 2, 2020 · N1074G · Beech B200 · Hydraulic Pump (Electric/Engine), Main
  > FAR 135.415 REPORT. PILOT REPORTS "THE LANDING GEAR DID NOT EXTEND WHEN THE GEAR HANDLE WAS LOWERED ON APPROACH INTO KALTAG. THE LANDING GEAR RELAY CB POPPED. WE TERMINATED THE APPROACH AND RETURNED TO FAIRBANKS. I RESET THE CB AND TRIED TO LOWER THE GEAR ON F
- [SDR V6HA201902080001](https://openairdocs.org/sdr/V6HA201902080001.md): Module · intermittent · Feb 5, 2019 · N332CA · Beech 200BEECH · Altitude Controller
  > ON RE-POSITIONING FLIGHT FOR MAINTENANCE OF OTHER SYSTEM, AIRCRAFT WAS ON AUTO-PILOT AND ALTITUDE HOLD WAS SELECTED AND WAS INDICATED AS ENGAGED. THE AIRCRAFT DRIFTED OFF OF ALTITUDE HOLD SETTING TO A HIGHER ALTITUDE WHICH OCCURRED VERY GRADUALLY. UPON ARRIV
- [SDR G1IA201803100001](https://openairdocs.org/sdr/G1IA201803100001.md): Downlock Switch · loose · Mar 7, 2018 · N68MN · Beech B200 · Landing Gear Position and Warning
  > PILOT REPORTED THAT WHILE ON FINAL APPROACH, PLACED THE GEAR HANDLE DOWN. IT FELT VERY MUCH LIKE A NORMAL EXTENSION. ON PERFORMING THE LANDING CHECKLIST, NOTICED THAT OF THE GREEN LIGHTS WERE ON. THE LNDG LIGHTS WERE REFLECTING OFF THE CLOUDS BACK INTO THE C
- [SDR 2017FA0000294](https://openairdocs.org/sdr/2017FA0000294.md): Transducer · shorted · Jun 8, 2017 · N911MN · Beech B200 · Engine Oil Indicating System
  > AFTER DEPARTURE, THE FLIGHT CREW RECOGNIZED A LOW OIL PRESSURE INDICATION ON THE LEFT ENGINE. WHILE ABORTING THE FLIGHT AND RETURNING TO DEPARTURE, THE CAPTAIN ASKED FOR THE ABNORMAL CHECKLIST AND COPILOT RETRIEVED THE APPROPRIATE CHECKLIST AND COMPLETED THE C
- [SDR 2017FA0000233](https://openairdocs.org/sdr/2017FA0000233.md): Combust Chamber · cracked · May 24, 2017 · N51265 · Beech A200C · Turbine Section
  > AFTER INITIAL POST PHASE ENGINE RUN, MAINTENANCE WAS INSTALLING THE LT ENGINE COWLING WHEN THEY DISCOVERED THAT THE COMBUSTION CHAMBER CASING WELD WAS CRACKED. CRACK WAS APPROXIMATELY 10 INCHES IN LENGTH.
- [SDR HDNA2017030515](https://openairdocs.org/sdr/HDNA2017030515.md): Line · melted · Mar 5, 2017 · N75LV · Beech B200 · Engine Bleed Air System
  > PLASTIC TUBING "SENSE" LINE FOR BLEED AIR INDICATING ANNUNCIATION MELTED DUE TO IMPROPER ROUTING CAUSING THE BLEED AIR FAIL CAUTION TO ILLUMINATE.
- [SDR 2017FA0000041](https://openairdocs.org/sdr/2017FA0000041.md): Elevator · frozen · Feb 3, 2017 · N917T · Piper PA46500TP · Control Column Section
  > AFTER BEING IN THE COLD, THE ELEVATOR CONTROL BECAME INCREASINGLY HARD TO CONTROL SUSPECTED GREASE IN THE COLD TEMPS.
- [SDR G1IA20161112983C1](https://openairdocs.org/sdr/G1IA20161112983C1.md): Downlock Switch · faulty · Nov 12, 2016 · N983C · Beech B200 · Landing Gear Position and Warning
  > PILOT REPORTS, THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS SELECTED TO THE DOWN POSITION. WE CYCLED THE GEAR THREE TIMES TO NO AVAIL. PROCEEDED TO EMERGENCY GEAR DOWN PROCEDURES VIA CHECKLIST AND GOT A GREEN NOSE GEAR LIGHT. LANDED UNEVENTFULLY.
- [SDR 2016FA0000564](https://openairdocs.org/sdr/2016FA0000564.md): Housing · leaking · Nov 10, 2016 · N950U · Piper PA46500TP · Turbine Engine Reduction Gear
  > AIRCRAFT LOST OIL PRESSURE DURING CRUISE FLIGHT, RESULTING IN AN ENGINE SHUTDOWN PRIOR TO LANDING AT CLOSEST AIRPORT. AIRCRAFT LANDED SAFELY WITH NO DAMAGE OR INJURIES. ENGINE WAS REMOVED FOR INSPECTION AND FOUND THE AFT REDUCTION GEARBOX HOUSING HAD SEVERE C
- [SDR 2016FA0000473](https://openairdocs.org/sdr/2016FA0000473.md): Tube · chafed · Oct 6, 2016 · N4489A · Beech B200C · Power Lever
  > DURING PHASE INSPECTION, FOUND THE NR 1 THROTTLE PUSH/PULL TUBE IN CENTER PEDESTAL RUBBING ON WIRE BUNDLE TRAY. NORMAL TUBE OD IS.497 AND OD FOR AREA BEING RUBBED.472. I
- [SDR 2016F00198](https://openairdocs.org/sdr/2016F00198.md): Motor · failed · Oct 2, 2016 · N42J · Beech 200BEECH · Trailing Edge Flap Actuator
  > APPROACHING THE FAF, FLAPS WERE LOWERED TO APPROACH SETTING. 1 MIN PRIOR TO CROSSING FAF, STRONG BURNING ODOR IN CABIN. NO SMOKE DETECTED. NOTICED FLAP MOTOR CIRCUIT BREAKER TRIPPED. TOWER WAS NOTIFIED OF SMELL, EMERGENCY VEHICLE WAS DISPATCHED FOR SAFETY RE
- [SDR 2016FA0000384](https://openairdocs.org/sdr/2016FA0000384.md): O-Ring · leaking · Aug 17, 2016 · N525S · Beech B200 · Turbine Engine Oil System
  > LEFT ENGINE OIL LEAK. FOUND INBOARD OIL PRESSURE SCAVENGE LINE LEAKING AT O-RINGS. REPLACED THE O-RINGS, RAN ENGINE FOUND OIL LEAKING AT COUPLING. INSTALLED NEW COUPLING. INSTALLED IAW MM 79-20-01. SERVICED ENGINE WITH 5 QTS OF OIL. RAN ENGINE AND LEAK CHECKED
- [SDR O9IA20160223001](https://openairdocs.org/sdr/O9IA20160223001.md): Fire Detector · failed · Feb 22, 2016 · N546LM · Beech B200 · Fire Detection
  > LOG PAGE WRITE UP IS AS FOLLOWS, RT ENG FIRE LIGHT ON APPROACH & LANDING, STAYED ON AFTER ENG SHUTDOWN. INSPECTED THE ENG FOR ANY SIGNS OF FIRE & FOUND NONE. THE FIRE WARNING LIGHT REMAINED LIT DURING INSPECTION. FOLLOWING THE TROUBLESHOOTING GUIDE IN THE A
- [SDR 2015FA0000472](https://openairdocs.org/sdr/2015FA0000472.md): Placard · inaccurate · Oct 1, 2015 · N716A · Beech B300C · Placards and Markings
  > AUXILIARY FUEL TANK PLACARDS FROM OEM REFLECT STANDARD CONFIGURATION WHEN ACFT ARE EQUIPPED WITH EXTENDED RANGE TANKS. ALSO, MLG PLACARDS FROM OEM REFLECT STANDARD LANDING GEAR HEIGHT RANGE WHEN HIGH FLOTATION GEAR ARE INSTALLED, 4.5"-5.0" STANDARD GEAR VS 5.
- [SDR VQMA201509041837](https://openairdocs.org/sdr/VQMA201509041837.md): Fire Detector · defective · Sep 4, 2015 · N918TC · Beech 200BEECH · Fire Detection
  > FLIGHT CREW EXPERIENCED A RT ENG FIRE LIGHT AT FLIGHT LEVEL 250. THE LIGHT INITIALLY ILLUMINATED FOR NO MORE THAN A FEW SECONDS THEN EXTINGUISHED. THE MASTER WARNING WAS CLEARED & THEN THE LIGHT RE-ILLUMINATED 10 TO 15 SECONDS LATER & REMAINED ILLUMINATED.
- [SDR 2015FA0000326](https://openairdocs.org/sdr/2015FA0000326.md): Blower · burned out · Jul 17, 2015 · N969MA · Beech B200 · Air Distribution Fan
  > AFTER TAKE OFF, PASSING THROUGH 16,000 FEET, OBSERVED AND SMELLED SMOKE IN THE AIRCRAFT. IT APPEARED TO ME TO BE VERY LIGHT GREY SMOKE, AND HAD AN ACRID SMELL AND WAS SLIGHTLY IRRITATING TO THE EYES AND THROAT. THE MED CREW IN THE REAR SAID THEY COULD ALSO SEE
- [SDR C41R201506190001](https://openairdocs.org/sdr/C41R201506190001.md): Rib · cracked · Jun 19, 2015 · N5355S · Piper PA46500TP · Wing, Rib/Bulkhead
  > AIRCRAFT WAS UNDERGOING AN ANNUAL INSPECTION AND A CRACK WAS DISCOVERED AT LT INBD BOTTOM AFT WING, WS 66.5. UPON FURTHER INVESTIGATION 2 PARTIAL RIBS, PN 83079-002, 83294-002 WERE FOUND CRACKED. INSTALLED NEW PARTIAL RIBS AND REPAIRED SKIN CRACK IAW DER DRA
- [SDR G9CR201506020001](https://openairdocs.org/sdr/G9CR201506020001.md): Encoder · binding · May 28, 2015 · N500XK · Piper PA46500TP · Elevator Tab Control System
  > THE ENCODER FOR CABIN PRESSURIZATION SYSTEM LOCATED FORWARD OF THE INSTRUMENT PANEL AND ABOVE THE PEDESTAL, SEPARATED FROM THE MOUNTING BRACKET AND LODGED IN THE ELEVATOR CONTROL QUADRANT, RESULTING IN LIMITED ELEVATOR CONTROL FOR THE PILOT ON APPROACH TO LAND

Next page: https://openairdocs.org/engine/u-a-canada-pt6a-42a/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 = 'PT6A42A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/u-a-canada-pt6a-42a/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.