# Service difficulty reports: Piper PA46-500TP

A list on [Piper PA46-500TP](https://openairdocs.org/model/piper-pa46-500tp.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 99 reports

- [SDR 2024FA0000373](https://openairdocs.org/sdr/2024FA0000373.md): Valve · faulted · May 20, 2024 · N51019 · Piper PA46500TP · Landing Gear Retraction/Extension System
  > WE RECENTLY HAVE EXPERIENCED AN INCREASE IN THE FREQUENCY OF REPLACEMENT AND SHORTER LIFE OF THE LANDING GEAR EMERGENCY RELEASE VALVES (PN: 101758-802 OR 101758-002). THE FAILURE HAS BEEN WITH THE REPLACEMENT VALVES. WE INSTALLED A NEW/OVERHAULED VALVE IN N510
- [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 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 2023FA0000737](https://openairdocs.org/sdr/2023FA0000737.md): Valve · faulted · Oct 17, 2023 · N51019 · Piper PA46500TP · Landing Gear System
  > MALIBU AEROSPACE IS A SHOP THAT WORKS EXCLUSIVELY ON THE PA46 AIRCRAFT. THE AIRCRAFT THAT IS BEING DISCUSSED IN THIS REPORT IS ONE OF OUR CUSTOMERS. THIS AIRCRAFT HAD THE EMERGENCY RELEASE VALVE (PN: 101758-802 / SN: 0402) REPLACED JUST AFTER THE ANNUAL INSPEC
- [SDR 2022FA0000680](https://openairdocs.org/sdr/2022FA0000680.md): Squat Switch · intermittent · Oct 6, 2022 · N248DA · Piper PA46500TP · Landing Gear Position and Warning
  > SQUAT SWITCH INTERNAL CONTACTS BTWN PIN 7 AND 9 DEVELOPED A HIGHER LEVEL OF RESISTANCE THAN THE OTHER INTERNAL PINS, CAUSING THE PRESSURIZATION SYSTEM TO SENSE A WEIGHT ON WHEELS SCENARIO, DEPRESSURIZING THE CABIN IN LEVEL FLIGHT. THE PILOT DROPPED FROM FLT LV
- [SDR 2022FA0000449](https://openairdocs.org/sdr/2022FA0000449.md): Lead · open · Aug 16, 2022 · N488WA · Piper PA46500TP · Propeller/Rotor Anti-Ice/De-Ice System
  > PILOT REPORTED THE PROPELLER DEICE OPERATION WAS INTERMITTENT. OPERATION WAS NOT CONSISTENT IN ANY PHASE OF FLIGHT OR GROUND MANEUVERING. PERFORMED A FUNCTIONAL CHECK OF PROP HEAT IN HANGAR AND CONFIRMED NOT ALL BLADES WERE HEATING. REMOVED SPINNER AND INSPEC
- [SDR LF1R202108200001](https://openairdocs.org/sdr/LF1R202108200001.md): Wire Harness · chafed · Aug 2, 2021 · N992ST · Piper PA46500TP · Ice/Rain Protection System Wiring
  > PILOT REPORTED THE PROPELLER HEAT CB OPENED AND A PROP HEAT FAIL MESSAGE ILLUMINATED ON THE MFD. ATTEMPTED ONE RESET OF CB WITHOUT SUCCESS. REMOVED SPINNER FOR VISUAL INSPECTION AND FOUND 4 OUT OF 5 PROPELLER HEAT HARNESSES HAD CHAFED THROUGH THE INSULATION CA
- [SDR VPEA202107300001](https://openairdocs.org/sdr/VPEA202107300001.md): Brake Sys · pressure loss · Jul 29, 2021 · N465TP · Piper PA46500TP · Landing Gear Brake System
  > LOSS OF PILOT SIDE BRAKES. PILOT NOTICED IN FLIGHT THAT BRAKES HAD LOSS PRESSURE. MAINTENANCE IN DURANGO CO, INSPECTED SYSTEM AND DETERMINED THERE HAD BEEN AN AIR BUBBLE IN THE SYTEM THAT WORKED ITS WAY TO THE PILOTS MASTER CYLINDERS CAUSING LOSS OF BRAKES. TH
- [SDR VPEA2021073000280](https://openairdocs.org/sdr/VPEA2021073000280.md): Brake Sys · failed · Jul 29, 2021 · N465TP · Piper PA46500TP · Landing Gear Brake System
  > TOTAL LOSS OF PILOT SIDE BRAKES. DISCOVERED DURING FLIGHT.
- [SDR LF1RN600PZ071621](https://openairdocs.org/sdr/LF1RN600PZ071621.md): Sensor · sheared · Jul 14, 2021 · N600PZ · Piper PA46500TP · Landing Gear Brake System
  > OWNER REPORTED AN EMERGENCY AUTOLAND WHEEL SPEED SENSOR DEGRADE MESSAGE ILLUMINATING ON LANDING. REMOVAL OF HUBCAPS FOR INSPECTION REVEALED THE RH WHEEL SPEED SENSOR HAD FAILED. THE SENSOR SHAFT HAD SHEARED BELOW THE ENGAGEMENT FITTING. NO CLEAR CAUSE NOTED FO
- [SDR LF1RN325ST060321](https://openairdocs.org/sdr/LF1RN325ST060321.md): Transducer · sheared · Jun 3, 2021 · N325ST · Piper PA46500TP · Landing Gear Position and Warning
  > OPERATOR HAD AN "EAL ( EMERGENCY AUTO LAND) DEGRADE " MESSAGE AND A "CHECK WHEEL SPEED SENOR" ILLUMINATE UPON LANDING. INSPECTED BOTH MAIN GEAR WHEEL AXLES AND FOUND THE RH MLG WHEEL SPEED SENSOR HAD FAILED MECHANICALLY. THE ACTUATOR SHAFT HAD SHEARED RESULTI
- [SDR LF1R20210215021](https://openairdocs.org/sdr/LF1R20210215021.md): Horn · excess play · Feb 12, 2021 · N282ST · Piper PA46500TP · Landing Gear Steering System
  > DURING COMPLIANCE WITH PIPER SB 1350A, FOUND ONE BOLT LOOSE ON THE NOSE GEAR STEERING HORN ASSEMBLY. THE ORIGINAL ISSUE OF PIPER SB 1350 HAD BEEN PREVIOUSLY COMPLIED WITH AT ANOTHER FACILITY. THE BOLT WAS FOUND TO BE SAFETIED, BUT THE SAFETY WIRE WAS ACTUALLY
- [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 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 2020FA0000409](https://openairdocs.org/sdr/2020FA0000409.md): Steering Unit · failed · Jun 10, 2020 · N115NX · Piper PA46500TP · Landing Gear Steering System
  > EXPERIENCED A LOSS OF NOSE WHEEL STEERING CONTROL ON LANDING.
- [SDR CA190207012](https://openairdocs.org/sdr/CA190207012.md): Guard · out of alignment · Feb 7, 2019 · Piper PA46500TP · Aileron Control System
  > (CAN) DURING SCHEDULED MAINTENANCE AND INSPECTION OF THE AILERON CABLE AND BELL CRANK IN ACCORDANCE WITH SL 1327 THE AILERON CABLE GUARD WAS OBSERVED TO BE BINDING ON THE AILERON CABLE AT THE BELL CRANK. THIS RESULTED IN DAMAGE TO THE CABLE AND BELL CRANK. PIC
- [SDR 2020FA0000075](https://openairdocs.org/sdr/2020FA0000075.md): Tube · broken · Nov 12, 2018 · N19CX · Piper PA46500TP · Trailing Edge Flap Control System
  > ON TAKEOFF FROM KEDC, SELECTED GEAR AND FLAPS UP. AIRCRAFT STARTED ROLLING TO THE LEFT HAVING TO USE FULL AILERON TO KEEP IT STRAIGHT, AT THIS POINT PILOT NOTICED RIGHT FLAP WAS DEPLOYED AND LEFT FLAP UP. SELECTED FLAPS DOWN AND WAS ABLE TO REGAIN CONTROL ON
- [SDR 2017FA0000531](https://openairdocs.org/sdr/2017FA0000531.md): Hinge · cracked · Sep 15, 2017 · N126ST · Piper PA46500TP · Ailerons
  > DURING ANNUAL INSPECTION, IT WAS DISCOVERED THAT THE CENTER AILERON HINGE HORN ATTACH BRACKETS, ON THE RIGHT WING, WERE CRACKED OUT TO THE POINT THAT IT HAD ALMOST SEPARATED FROM THE REAR WING SPAR. DURING REMOVAL OF THE RIGHT AILERON, IT WAS EVIDENT THAT THE
- [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 2016FA0000606](https://openairdocs.org/sdr/2016FA0000606.md): Radio · defective · Dec 8, 2016 · N25324 · Piper PA46500TP · Communications System
  > ABOUT EVERY 6TH OR 7TH START THE NR 1 RADIO GOES INOP I HAVE GONE THROUGH 3 RE-PROGRAMS. WITH 2 DIFFERENT FBO'S MANUFACTURER HAS NO FIX AND THE PROBLEM PERSIST. THE SYSTEM IS SUPPOSED TO BE THE FINEST AVIONICS SYSTEM AVAILABLE. THIS IS A 2013 MODEL AIRCRAFT WI
- [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 C41R2016051800246](https://openairdocs.org/sdr/C41R2016051800246.md): Control Module · burned · May 17, 2016 · N821J · Piper PA46500TP · Pitot/Static Anti-Ice System
  > FOUND 25 AMP PITOT HEAT REMOTE SWITCH MODULE SHORTING AND ARCHING BEHIND PILOT SIDEWALL. MODULE LOAD SIDE ATTACHMENT STUD FELL FROM UNIT AFTER WIRE REMOVAL. MODULE BUS SIDE ATTACHMENT WIRE WAS BURNED AND ARCHING CASE OF UNIT. REPAIRED WIRING AND INSTALLED NEW
- [SDR CA160216012](https://openairdocs.org/sdr/CA160216012.md): Engine · power loss · Feb 12, 2016 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) CUSTOMER REPORTS ON TAKE-OFF ENGINE ROLLED BACK ON POWER. CUSTOMER INSTANTLY REDUCED POWER AND ABORTED TAKEOFF AND DID NOT SEE WHAT INSTRUMENTATION WAS READING. NO DAMAGE, INJURIES OR INCIDENT REPORTED.
- [SDR CA160120004](https://openairdocs.org/sdr/CA160120004.md): Oil System · low pressure · Jan 6, 2016 · Piper PA46500TP · Turbine Engine Oil System
  > (CAN) WHILE IN CRUISE THE PILOT NOTED THE OIL PRESSURE WENT INTO THE YELLOW BAND (60 TO 99 PSI). FLIGHT WAS DIVERTED TO AN ALTERNATE AIRPORT AFTER LANDING WHILE TAXIING, THE OIL PRESSURE INDICATION STARTED TO FLICKER BETWEEN YELLOW AND RED AND THE PILOT SHUT T
- [SDR CA150728006](https://openairdocs.org/sdr/CA150728006.md): Horn · dented · Jul 8, 2015 · Piper PA46500TP · Landing Gear Steering System
  > (CAN) DURING A ROUTINE 100 HRS INSPECTION, WE FOUND THAT THE NOSE GEAR STEERING HORN WAS RUBBING WITH THE FRONT ENGINE MOUNT. HORN AND RUB BLOCK WERE REMOVED AND TRIMMED TO ENSURE CLEARANCE BETWEEN ENGINE MOUNT AND STEERING HORN. ENGINE MOUNT DAMAGE INSPECTE
- [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
- [SDR CA150518007](https://openairdocs.org/sdr/CA150518007.md): Engine · malfunctioned · Apr 23, 2015 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) THE PILOT REPORTED AN OIL CHIP DETECTOR LIGHT, LOW MOP & HIGH MOT. THE EVENT OCCURRED WHILE PERFORMING NEGATIVE ACCELERATION FLIGHT TESTING. THIS IS A PRODUCTION ENG OFF M600 PROTOTYPE ACFT. TROUBLESHOOTING REVEALED RBG METALLIC DEBRIS IN OIL, BRONZE.
- [SDR CA150224010](https://openairdocs.org/sdr/CA150224010.md): Engine · malfunctioned · Feb 13, 2015 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) THE PLANE CRASHED SHORTLY AFTER TAKEOFF AS A RESULT OF A REPORTED TECHNICAL ISSUE. PRELIMINARY INFORMATION IS STATING ENGINE TROUBLE OCCURRED JUST AFTER TAKEOFF AND THE CRASH IS DESCRIBED AS A FORCED LANDING.
- [SDR CA150120002](https://openairdocs.org/sdr/CA150120002.md): Engine · making metal · Jan 7, 2015 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) DURING TAKE OFF, THE AIRCRAFT HAD AN OIL PRESSURE DROP FROM 48 PSI TO 28 PSI. THE PILOT DECLARED AN IFSD AND LANDED WITHOUT INCIDENT. UPON LANDING, THE OIL PRESSURE RETURNED TO NORMAL. THE TROUBLESHOOTING REVEALED METALLIC DEBRIS IN THE OIL FILTER.
- [SDR YN8R11142014BH](https://openairdocs.org/sdr/YN8R11142014BH.md): Skin · cracked · Nov 14, 2014 · N3129X · Piper PA46500TP · Elevator, Plate/Skin
  > DURING START OF ANNUAL INSPECTION, VISUALLY SAW THE LOWER OUTER AFT SKIN OF THE ELEVATOR, PN 102051-803 WAS CRACKED ALONG THE FORWARD RIVET ROW AT THE SPAR FROM LT ELEVATOR STATION 58.5" TO 62.5". WE REMOVED THE ELEVATOR AND REMOVED AND REPLACED THE SKIN. IN
- [SDR CA140826017](https://openairdocs.org/sdr/CA140826017.md): Engine · power loss · Aug 25, 2014 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) DURING TAKE-OFF ROLL ENGINE SUFFERED A POWER ROLLBACK. AWAITING FURTHER DETAILS FROM FSR. SERVICE INVESTIGATION PROPOSED TO RETURN THE FCU TO THE MANUFACTURER FOR FURTHER INVESTIGATION.
- [SDR CA140721005](https://openairdocs.org/sdr/CA140721005.md): Engine · power loss · Jul 7, 2014 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) PRIOR TO TAKEOFF, THE PILOT OBSERVED A LOW PROPELLER SPEED FOLLOWED BY A LOSS OF POWER. FIRE IN THE ENGINE COMPARTMENT WAS REPORTED WHICH HAD EXTINGUISHED BEFORE THE FIRE DEPT ARRIVED.
- [SDR CA140619016](https://openairdocs.org/sdr/CA140619016.md): Engine · malfunctioned · Jun 4, 2014 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) PILOT STARTED THE ENGINE AND NOTICED THAT THE ENGINE DID NOT RESPOND TO POWER LEVER INPUT. PILOT ELECTED TO USE EMERGENCY MANUAL OVERRIDE LEVER TO TAXI FOR TAKE OFF. PILOT APPLIED EMERGENCY MANUAL OVERRIDE LEVER FOR TAKEOFF AND DURING TAKEOFF ROLL HE NOT
- [SDR 9PMA201304240001](https://openairdocs.org/sdr/9PMA201304240001.md): Resistor · burned · Apr 22, 2013 · N281SE · Piper PA46500TP · Electrical Power System Wiring
  > FOUND EMERGENCY LIGHTS ON BUT SWITCHES WERE OFF. PULLED CIRCUIT BREAKERS, LIGHT WENT OUT. SEVERAL HOURS LATER, ON PREFLIGHT, DISCOVERED BLACK SOOT COMING OUT OF ENGINE COWLING. DISCOVER WHAT APPEARS TO BE AN ELECTRICAL FIRE HAD OCCURRED. APPEARS THAT A
- [SDR CA130430012](https://openairdocs.org/sdr/CA130430012.md): Engine · power loss · Mar 13, 2013 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) DURING A SIMULATED FORCED LANDING, THE PILOT STATED THAT HE CLIMBED TO FL35 AND INITIATED SPIRAL TURNS FOR A LT TRAFFIC APPROACH TO THE RUNWAY. DURING FINAL APPROACH, THE ACFT STARTED DESCENDING AT A HIGHER RATE THAN EXPECTED. THE PILOT ATTEMPTED TO IN
- [SDR CA130118008](https://openairdocs.org/sdr/CA130118008.md): Check Valve · failed · Jan 17, 2013 · Piper PA46500TP · Fuel Controlling System
  > (CAN) FUEL PURGE TANK CHECK VALVE FOUND TO BE UNSERVICEABLE DURING ROUTINE INSPECTION/FUNCTION CHECK.
- [SDR CA120917003](https://openairdocs.org/sdr/CA120917003.md): Engine · malfunctioned · Sep 1, 2012 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) DURING DESCENT, AFTER THE PILOT RETARDED THE THROTTLE TO IDLE, REALIZED THAT THE TORQUE INDICATION WAS AT ZERO. THE PILOT CLOSED THE BLEED AIR AND THE AIR CONDITIONING SYSTEM AND PUSHED THE THROTTLE LEVER TO MAX. POSITION WITH NO RESPONSE FROM THE ENG
- [SDR 2012FA0000579](https://openairdocs.org/sdr/2012FA0000579.md): Scissor Link · detached · Aug 20, 2012 · N796JS · Piper PA46500TP · Nose/Tail Landing Gear
  > AFTER TAKEOFF, LANDING GEAR RETRACTED, PILOT NOTED THAT THE "HYD PUMP" ANNUNCIATOR STAYED ON. ON ARRIVAL AT DESTINATION, PILOT SELECTED GEAR DOWN AND ALL THREE GREEN LIGHTS ILLUMINATED. SOMETHING DIDN'T FEEL RIGHT WITH THE ACFT AND A FLY-BY OF THE CONTROL TO
- [SDR CA120717012](https://openairdocs.org/sdr/CA120717012.md): Display · malfunctioned · Jul 13, 2012 · Piper PA46500TP · Central Display
  > (CAN) ON A ROUTINE FLIGHT, THE PILOT IN COMMAND SELECTED A NEW SCREEN ON THE MULTIFUNCTION DISPLAY, THE KNOB TURNED AND THE MULTI FUNCTION DISPLAY LOST ALL INFORMATION. THE PILOT LANDED THE ACFT SAFELY USING BACK UP INSTRUMENTATION. MAINTENANCE DISCOVERED TH
- [SDR 2012FA0000140](https://openairdocs.org/sdr/2012FA0000140.md): Cotter Pin · backed out · Feb 27, 2012 · N2406P · Piper PA46500TP · Nose/Tail Landing Gear
  > OWNER NOTICED A VIBRATION SHORTLY AFTER LANDING. FOUND NLG CENTER TORQUE LINK HARDWARE MISSING AND NLG MISALIGNED. COMPLETED INSPECTION OF NLG ASSY AND FOUND BOLT, NUT, WASHER, AND COTTER KEY MISSING FROM CENTER TORQUE LINK AND NLG TIRE WAS LIGHTLY FLAT S
- [SDR 2012FA0000071](https://openairdocs.org/sdr/2012FA0000071.md): Connector · corroded · Jan 22, 2012 · N2424U · Piper PA46500TP · Emergency Locator Beacon
  > WATER IN ELT CONNECTOR CAUSING CORROSION BETWEEN PINS, CAUSING ELT TO TURN ON, COULD NOT RESET.
- [SDR CA111012008](https://openairdocs.org/sdr/CA111012008.md): Actuator · inoperative · Oct 6, 2011 · Piper PA46500TP · Landing Gear Actuator
  > (CAN) RT MAIN GEAR ACTUATOR UNLOCKED TWICE & GEAR STARTED RETRACTING WHEN ACFT WAS TOWED ON RAMP.
- [SDR CA110711007](https://openairdocs.org/sdr/CA110711007.md): Engine · power loss · Jun 27, 2011 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) NO RESPONSE FROM THROTTLE AFTER TAXIING AND PREPARING FOR TAKEOFF, THE ENGINE DID NOT RESPOND TO THROTTLE INCREASE. AFTER SEVERAL ATTEMPTS, THE ENGINE EVENTUALLY RESPONDED. THE FLIGHT WAS CANCELLED.
- [SDR CA110613003](https://openairdocs.org/sdr/CA110613003.md): Engine · power loss · Jun 2, 2011 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) POWER ROLLBACK THE TEST ACFT EXPERIENCED A POWER ROLL BACK DURING TAKEOFF. NO ADDITIONAL INFORMATION IS AVAILABLE AT THIS TIME. UPDATE NR 1: CONTRARY TO EARLIER INFO, THE POWER ROLL BACK OCCURRED AT IDLE, ON THE GROUND DURING TAXI PRIOR TO T/O.
- [SDR CA110516009](https://openairdocs.org/sdr/CA110516009.md): Engine · flamed out · May 6, 2011 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) FLAMEOUT, SINGLE ENGINE, DURING LANDING ROLL, THE ENGINE ROLLED BACK AND FLAMED OUT. THE PILOT WAS ABLE TO TAXI OFF THE RUNWAY AND THE ACFT WAS TOWED TO THE HANGER. ACCORDING TO THE OPERATOR, THIS IS THE 3RD SUCH EVENT ON THIS ENGINE AND HE ALSO HAD E
- [SDR CA110711006](https://openairdocs.org/sdr/CA110711006.md): Engine · unknown · Apr 14, 2011 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) NO RESPONSE FROM THROTTLE DURING A TRAINING FLIGHT, IN THE APPROACH PHASE AT 700` AGL AND AFTER RETRACTING THE FLAPS IN ORDER TO PRACTICE A FLAPLESS LANDING, THE ENGINE DID NOT RESPOND TO POWER LEVER ADVANCE. THE LEVER WAS RETARDED TO IDLE AND ADVANCED
- [SDR CA101115001](https://openairdocs.org/sdr/CA101115001.md): Engine · power loss · Oct 29, 2010 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > (CAN) ACCIDENT SHORTLY AFTER TAKEOFF, THE ENGINE LOST POWER. THE PILOT MADE A CRASH LANDING IN A FIELD AND HIT A POLE WITH THE RIGHT WING. ALL ON BOARD ESCAPED WITH MINOR INJURIES.
- [SDR CA101025003](https://openairdocs.org/sdr/CA101025003.md): Engine · power loss · Oct 21, 2010 · Piper PA46500TP · Engine (Turbine/Turboprop)
  > POWER LOSS (SINGLE ENG) AFTER T/O AT 300 FT ALTITUDE, THE ENGINE POWER ROLLED BACK. THE PILOT USED THE MANUAL OVERRIDE LEVER AND AFTER HEARING "BACK FIRES" HE WAS ABLE TO RE-GAIN ENGINE POWER. HE DECLARED EMERGENCY AND RETURNED TO THE AIRPORT FOR A SAFE LAND
- [SDR CA100720005](https://openairdocs.org/sdr/CA100720005.md): Timer · failed · Jul 15, 2010 · Piper PA46500TP · Propeller/Rotor Anti-Ice/De-Ice System
  > (CAN) PROPELLER DE-ICE TIMER HAD INTERNAL FAILURE AND BURNED OUT.

Next page: https://openairdocs.org/model/piper-pa46-500tp/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 aircraft_model_key = 'PA46500TP'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/piper-pa46-500tp/reports

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