# Service difficulty reports: Piaggio P180

A list on [Piaggio P180](https://openairdocs.org/model/piaggio-p180.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 269 reports

- [SDR 2025FA0000443](https://openairdocs.org/sdr/2025FA0000443.md): Brake · seized · Jul 1, 2025 · N481BR · Piagio P180 · Landing Gear Brake System
  > DURING AN AIRCRAFT JACKING PROCEDURE FOR UNRELATED MAINTENANCE, MAINTENANCE PERSONNEL NOTICED THAT THE RIGHT-HAND (RH) WHEEL WAS NOT ABLE TO SPIN NORMALLY DUE TO HIGH FRICTION. THE BRAKE WAS SENT OUT FOR EVALUATION AND WAS FOUND TO HAVE BEEN OVERHEATED, WHICH
- [SDR 2024FA0000068](https://openairdocs.org/sdr/2024FA0000068.md): Relay · overheated · Jan 19, 2024 · N481BR · Piagio P180 · Windshield/Door Rain/Ice Removal
  > DURING MAINTENANCE, IT WAS NOTED THAT RELAY K62 HAD BECOME EXCESSIVELY WARM AT SOME POINT AND THE HEAT SHIELDING ON WIRE H202A10 THAT IS CONNECTED TO THE RELAY TERMINAL A1 WAS ALSO MELTED. NO EVIDENCE OF FIRE AFFECTING SURROUNDING AREA. JUST THE OVERHEATING
- [SDR PAZR202305100001](https://openairdocs.org/sdr/PAZR202305100001.md): Adc · inoperative · Apr 28, 2023 · N105GP · Piagio P180 · Air Data Computer
  > APPLIED POWER TO AIRCRAFT AND VERIFIED THE #1 ADC SHOWS AS FAILED. PUSHED THE SELF TEST BUTTON ON FRONT OF UNIT, NO SIGN OF SELF TEST WAS SEEN. REMOVED #1 ADC UNIT AND VERIFIED POWER AND GROUNDS TO UNIT. ALL POWER AND GROUNDS CHECKED GOOD.
- [SDR 9JLA2023021034502](https://openairdocs.org/sdr/9JLA2023021034502.md): Unknown · unknown · Feb 10, 2023 · N989BJ · Piagio P180 · Engine Cowling System
  > DURING POST FLIGHT MAINTENANCE CHECKS THE TECHNICIAN NOTED A CRACK IN THE RIGHT ENGINE UPPER COWL MATERIAL THAT WAS APPROXIMATELY 3 INCHES LONG. THE CRACK IS POSITIONED 39 INCHES AFT OF THE LEADING EDGE OF THE RIGHT COWL INLET LIP ON THE INBOARD SIDE OF THE CO
- [SDR 2021F00214](https://openairdocs.org/sdr/2021F00214.md): Windshield · used · Sep 11, 2021 · N493JD · Piagio P180 · Flight Compartment Windows
  > THIS WAS IN A PIAGGIO AVANTI II AIRCRAFT. THE OUTER PANE OF THE CO-PILOT'S WINDSHIELD CRACKED IN FLIGHT.
- [SDR 9JLA2021080425175](https://openairdocs.org/sdr/9JLA2021080425175.md): Sensor · defective · Jul 16, 2021 · N989BJ · Piagio P180 · Propeller Controlling System
  > THE FLIGHT CREW REPORTED THAT PROPELLER SYNC FAULTED, THE CREW ADVISED, WHEN ENGAGED THE LEFT PROP WOULD SPEED-UP 25 TO 30 RPM. THE DISCREPANCY WAS DEFERRED FOR CONTINUED OPERATIONS. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE LEFT PROP SYNCHRO PHASER
- [SDR 3FPY20190711005](https://openairdocs.org/sdr/3FPY20190711005.md): Actuator · faulty · Jul 11, 2019 · N61WC · Piagio P180 · Stabilizer Actuator
  > AIRCREW REPORT: PITCH TRIM INDICATION INTERMITTENT. PITCH TRIM ACTUATOR OUTPUT SIGNAL FOR PITCH TRIM INDICATOR ERRATIC - INDICATION INACCURATE (FAILED COMPLETELY DURING FAULT FINDING). PITCH TRIM ACTUATOR REPLACED WITH OVERHAULED COMPONENT AND TESTED SERVICEAB
- [SDR 2019FA0000133](https://openairdocs.org/sdr/2019FA0000133.md): Brake Assy · locked · Apr 25, 2019 · N490JD · Piagio P180 · Landing Gear Brake System
  > UPON LANDING AT THE KRVS AIRPORT, THE RIGHT MAIN WHEEL/BRAKE WAS COMPLETELY LOCKED UP AND FAILED TO ROTATE WHATSOEVER. THIS WAS AFTER A SIMILAR EVENT AT KEDC. UPON LANDING AT KEDC, THE RIGHT MAIN WHEEL "APPEARED" TO LOCK UP MOMENTARILY CAUSE A FLAT SPOT ON T
- [SDR CA190428001](https://openairdocs.org/sdr/CA190428001.md): Seal · leaking · Apr 14, 2019 · Piagio P180 · Turbine Engine Compressor Section
  > (CAN) OIL ODOR NOTED IN CABIN DURING CLIMB, VISIBLE SMOKE/HAZE NOTED IN CABIN AT TOP OF CLIMB, ENGINE POWER REDUCED AND SMOKE/HAZE CLEARED AND OIL ODOR REDUCED. AIRCRAFT RETURNED TO BASE WITH NO FURTHER INCIDENT. POST FLIGHT INVESTIGATION REVEALED OIL CONTAMI
- [SDR 2019F00022](https://openairdocs.org/sdr/2019F00022.md): Pulley · failed · Feb 22, 2019 · N490JD · Piagio P180 · Rudder Control System
  > DURING A SCHEDULED 200FH INSPECTION AS REQUIRED BY CHAPTER 05-00-00, THE LEFT LOWER RUDDER PULLEY, IT WAS NOTICED THAT THE LOWER LEFT RUDDER PULLEY WAS APPROXIMATELY 1/4" HIGHER THEN THE RIGHT PULLEY. UPON REMOVAL OF THE PULLEY, THE BEARING AND RACE WAS FROZEN
- [SDR 2018FA0000108](https://openairdocs.org/sdr/2018FA0000108.md): Downlock Switch · malfunctioned · Mar 16, 2018 · N864HD · Piagio P180 · Landing Gear Position and Warning
  > ON DEPLOYMENT OF GEAR, NO GREEN LIGHT NOTED AT RIGHT MAIN GEAR ANNUNCIATOR, AND NO RED UNSAFE LIGHT NOTED AT RIGHT GEAR ANNUNCIATOR. HYDRAULIC POWER PACK WENT TO LOW MODE AFTER GEAR DEPLOYED BUT WARNING HORN COULD NOT BE SILENCED WITH GEAR SELECTED DOWN. WHEN
- [SDR 2017FA0000226](https://openairdocs.org/sdr/2017FA0000226.md): Brake Assy · binding · May 31, 2017 · N61WC · Piagio P180 · Brake
  > AIRCRAFT HAD THE LEFT WHEEL GO FLAT AFTER LANDING ROLLOUT. THIS IS THE SECOND TIME THAT IT HAS HAPPENED IN THE LAST TWO WEEKS. UPON INSPECTION OF THE WHEEL, IT WAS NOTICED THAT THE THERMAL FUESES WERE OPEN. AFTER CONSULTATION WITH THE AIRCRAFT MANUFACTURER,
- [SDR 2016F00231](https://openairdocs.org/sdr/2016F00231.md): Door · out of adjust · Nov 28, 2016 · N589H · Piagio P180 · Emergency Exits
  > DURING CLIMB OUT, THE AIRCRAFT FAILED TO PRESSURIZE. THE SOUND OF RUSHING AIR WAS HEARD. FOLLOWED THE CHECKLISTS AND COULD NOT GET THE PLANE TO PRESSURIZE. A DECISION WAS MADE TO RETURN FOR LANDING AND AN EMERGENCY DECLARED. DURING A POST FLIGHT INSPECTION,
- [SDR 2016FA0000551](https://openairdocs.org/sdr/2016FA0000551.md): Handle · failed · Nov 2, 2016 · N589H · Piagio P180 · Emergency Exits
  > ATTEMPTED OPENING THE EMERGENCY EXIT FROM THE EXTERIOR OF AIRCRAFT. EMERGENCY EXIT HANDLE FAILED.
- [SDR CA160301004](https://openairdocs.org/sdr/CA160301004.md): Heater · malfunctioned · Feb 17, 2016 · Piagio P180 · Fuel Heater
  > (CAN) AFTER LANDING, EXTERNAL FUEL LEAK WAS NOTICED. (THIS IS THE 3RD EVENT). THE FUEL WAS INSIDE THE RIGHT HAND ENGINE NACELLE, ON WING, FUSELAGE AND EVEN INSIDE THE LANDING GEAR VANE. PIAGGIO DID A GROUND RUN, AND REPORTED, ABOVE IDLE POWER, A FUEL SPRAY FRO
- [SDR CA160113002](https://openairdocs.org/sdr/CA160113002.md): Actuator · loose · Jan 11, 2016 · Piagio P180 · Rudder Tab Control System
  > (CAN) DURING INSPECTION, NOTICED ROD END JAM NUTS NOT SECURE ON RUDDER TRIM ACTUATOR.
- [SDR CA160119021](https://openairdocs.org/sdr/CA160119021.md): Engine · malfunctioned · Dec 30, 2015 · Piagio P180 · Engine (Turbine/Turboprop)
  > (CAN) THE OPERATOR REPORTED THAT 4 TIMES OUT OF 5, THE ENGINE WILL NOT GO IN REVERSE. CYCLING THE CONTROLS HAD NO EFFECT. TROUBLESHOOTING IS ON-GOING WITH RIGGING TESTING AND PROPELLER GOVERNOR SWAP.
- [SDR CA151125004](https://openairdocs.org/sdr/CA151125004.md): Hose · collapsed · Nov 23, 2015 · Piagio P180 · Engine Cooling System
  > (CAN) FOUND DURING A SCHEDULED INSPECTION RIGHT BLEED AIR PRE-COOLER OVERHEATED AND RT ENGINE BLEED AIR SUPPLY HOSE INTERIOR WALL COLLAPSED.
- [SDR CA151125005](https://openairdocs.org/sdr/CA151125005.md): Anti-Ice Valve · malfunctioned · Nov 20, 2015 · Piagio P180 · Airfoil Anti/De-ice System
  > (CAN) LEFT WING ANTI-ICE VALVE FAILED TO CLOSE WHEN SELECTED "OFF". INVESTIGATION FOUND "BUTTEFLY" TURNING ON SHAFT DUE TO STRIPPED SPLINES.
- [SDR CA150414004](https://openairdocs.org/sdr/CA150414004.md): Hinge Pin · sheared · Apr 13, 2015 · Piagio P180 · Air Intake Anti/De-Ice System
  > (CAN) ENGINE ANTI-ICE DIVERTER DOOR HINGE PINS SHEARED. DOOR WAS FOUND LOOSE IN COWL. TECH SUPPORT HAS SEEN THIS IN THE PAST. DAMAGE POSSIBLY CAUSED BY ICE BUILD-UP.
- [SDR J72A20150323001](https://openairdocs.org/sdr/J72A20150323001.md): Warning Light · illuminated · Mar 19, 2015 · N589H · Piagio P180 · Door Warning System
  > DURING CRUISE FLIGHT AT 37,000FT, DOOR SEAL ANNUNCIATOR LIGHT ILLUMINATED. CABIN WAS STARTING TO CLIMB. MADE AN UNSCHEDULED LANDING. COULD NOT DUPLICATE PROBLEM. REPLACED DOOR SEAL CHECK VLV & REGULATOR AS PRECAUTIONARY MEASURES.
- [SDR CA150325012](https://openairdocs.org/sdr/CA150325012.md): Engine · flamed out · Mar 11, 2015 · Piagio P180 · Engine (Turbine/Turboprop)
  > (CAN) FOLLOWING THROTTLE REDUCTION TO IDLE DURING DESCENT THE ENGINE FLAMED OUT. THE PILOT WAS ABLE TO RESTART THE ENGINE WHICH FLAMED OUT AGAIN TWICE WHILE BRINGING THROTTLE TO IDLE. ALL EVENTS OCCURRED IN EEC MODE.
- [SDR CA150313013](https://openairdocs.org/sdr/CA150313013.md): Blade · separated · Mar 10, 2015 · Piagio P180 · Turbine Engine Compressor Section
  > (CAN) IAW "AVIATION OCCURRENCE REPORT" DATED MARCH, 11, 2015: AFTER LANDING ON RUNWAY 23, WHILE ON TAXIWAY P, SMOKE ODOR WAS DETECTED BY CAPTAIN AND WAS VERIFIED TO BE PRESENT WITH THE FIRST OFFICER. THE SMOKE ODOR APPEARED TO INCREASE AS WAS ACCOMPANIED WITH
- [SDR J72A2015F00030](https://openairdocs.org/sdr/J72A2015F00030.md): Bulkhead · corroded · Feb 6, 2015 · N589H · Piagio P180 · Fuselage Main, Bulkhead
  > DURING "D" CHECK, VISUAL INSPECTION ON THE LOWER AFT FUSELAGE JOINT TO TAIL CONE AREA REVEALED CORROSION ON AFT FUSELAGE CANTED BULKHEAD AND LOWER SKIN AREA.
- [SDR J72A20150211](https://openairdocs.org/sdr/J72A20150211.md): Duct · cracked · Nov 30, 2014 · N589H · Piagio P180 · Airfoil Anti/De-ice System
  > LEFT WING ANTI-ICE DUCT ASSEMBLY HAS CRACKS WHICH EXCEED MM SRM LIMITS. REPAIRED DUCT ASSEMBLY.
- [SDR J72A20150211001](https://openairdocs.org/sdr/J72A20150211001.md): Duct · cracked · Nov 30, 2014 · N589H · Piagio P180 · Airfoil Anti/De-ice System
  > RIGHT WING ANTI-ICE DUCT ASSEMBLY HAS CRACKS WHICH EXCEED MM SRM LIMITS. REPAIRED DUCT ASSEMBLY IAW 337 DATED 11/30/2014.
- [SDR J72A2015021100001](https://openairdocs.org/sdr/J72A2015021100001.md): Bulkhead · corroded · Nov 30, 2014 · N589H · Piagio P180 · Fuselage Main, Bulkhead
  > DURING D CHECK INSPECTION, THE CANTED BULKHEAD LOCATED AT FS 8154 AT THE 6 O'CLOCK POSITION HAS CORROSION THAT EXCEEDS MM SRM LIMITS. THE CAUSE OF THE PROBLEM SEEMS TO BE THE BUILDUP OF WATER ENTRAPPED AFT OF THE BULKHEAD. THE DRAIN HOLE IS LOCATED TO FAR AF
- [SDR J72A2015F00032](https://openairdocs.org/sdr/J72A2015F00032.md): Bulkhead · corroded · Nov 30, 2014 · N589H · Piagio P180 · Fuselage Main, Bulkhead
  > DURING D-CHECK INSPECTION, THE CANTED BULKHEAD LOCATED AT FS 8154 6 O'CLOCK POSITION HAS CORROSION THE EXCEEDS MM SRM LIMITS. CAUSE OF PROBLEM SEEMS TO BE WATER ENTRAPMENT AFT OF THE BULKHEAD AND THE DRAIN HOLE LOCATED TO FAR AFT OF THE CANTED BULKHEAD TO DRAI
- [SDR CA141223007](https://openairdocs.org/sdr/CA141223007.md): Governor · failed · Nov 11, 2014 · Piagio P180 · Propeller Governor
  > (CAN) CREW DETERMINED PROPELLER CONTROLS NOT FUNCTIONING. IAW JLB ENTRY RT PROPELLER LOSS OF RPM. ENGINE SHUTDOWN PERFORMED IAW CHECKLIST. LANDED AIRCRAFT SAFELY. PROPELLER GOVERNOR REPLACED, AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT.
- [SDR 2014FA0000561](https://openairdocs.org/sdr/2014FA0000561.md): Bushing · worn · Sep 22, 2014 · N773RC · Piagio P180 · Elevator Structure
  > FOUND VERTICAL PLAY IN LT AND RT ELEVATOR HINGES. NOTED BOLTS WERE TIGHT BUT GRIPPED OUT. REMOVED HORIZONTAL COLLARS AND STINGER TO GAIN ACCESS TO ELEVATOR ATTACHMENTS. REPLACED BOLTS WITH SHORTER PN NAS6404A20 AND USED ORIGINAL WASHERS; LETTER DATED SEPTEMB
- [SDR CA140130008](https://openairdocs.org/sdr/CA140130008.md): Valve · frozen · Jan 29, 2014 · Piagio P180 · Passenger/Crew Doors
  > (CAN) AFTER LIFTOFF, CABIN DOOR LIGHT ILLUMINATED. CREW MAINTAINED FL 10 AND COMPLETED TRIP WITHOUT INCIDENT. 3 WAY VALVES FROZEN, AIC SAT ON RAMP APPROXIMATELY 6 HOURS -30C - TIS OF AIC C/O NFF SYSTEM DRAINED IAW AMM, AIC DEPARTED NEXT MORNING. NO ISSUES WI
- [SDR 2013FA0000763](https://openairdocs.org/sdr/2013FA0000763.md): Actuator · inoperative · Dec 10, 2013 · N871AT · Piagio P180 · Stabilizer Control System
  > AFTER ROTATION, THE PRIMARY PITCH TRIM WAS NOT WORKING. TRIM CLACKER WAS CLACKING BUT, THERE WAS NO MOVEMENT OF THE STABILIZER. SWITCHED TO SECONDARY HORIZONTAL PITCH TRIM WHICH WAS OPERATIONAL. MADE AN UNEVENTFUL LANDING. TROUBLESHOOTING REVEALED THE MOT
- [SDR V2JA2013F00133](https://openairdocs.org/sdr/V2JA2013F00133.md): Brake Disc · broken · Jun 11, 2013 · N131SL · Piagio P180 · Landing Gear Brake System
  > RIGHT WHEEL WAS REMOVED FOR SN VERIFICATION, AS WHEEL CAME OFF, BRAKE PAD PARTS AT KEY WAY FELL OUT.
- [SDR V2JA0602134154986](https://openairdocs.org/sdr/V2JA0602134154986.md): Display · failed · Jun 2, 2013 · N156SL · Piagio P180 · Flight Environment Data
  > IN FLIGHT, CAPTAINS PFD WENT BLANK, WITHIN A FEW SECONDS A STRONG BURNING ODOR FILLED THE COCKPIT.
- [SDR V2JA0523134153420](https://openairdocs.org/sdr/V2JA0523134153420.md): Fitting · leaking · May 23, 2013 · N143SL · Piagio P180 · Hydraulic Pump (Electric/Engine), Main
  > HYDRAULIC PUMP FAILED ON APPROACH. FOLLOWED CHECKLIST HAND-PUMPED GEAR DOWN. "HYD PRESS" CAUTION LIGHT ILLUMINATED, ASSOCIATED PRESSURE BETWEEN 0-200 PSI, DIVERTED.
- [SDR V2JA052313DEF130](https://openairdocs.org/sdr/V2JA052313DEF130.md): Seal · damaged · May 23, 2013 · N165SL · Piagio P180 · Passenger/Crew Doors
  > MASTER CAUTION (DOOR SEAL) AT 34,000. RAN CHECKLIST WITH F/O FOR DESCENT TO 30,000 FT. AT 30,000 FT AIRCRAFT WAS STABLE. AFTER ABOUT 5 TO 10 MINUTES A LOUD DOOR SEAL NOISE WAS NOTED AND CABIN BEGAN TO CLIMB RAPIDLY. AN EMERGENCY DESCENT WAS PERFORMED AS A
- [SDR CA130603006](https://openairdocs.org/sdr/CA130603006.md): Control System · malfunctioned · May 16, 2013 · Piagio P180 · Propeller Controlling System
  > (CAN) THE LEFT PROPELLER RPM DECAYED UNCOMMANDED TO FEATHER AT 1000` AGL. THE FAILURE OCCURRED AS THE POST TAKE OFF POWER REDUCTION WAS PERFORMED. THE CREW WAS UNABLE TO RECOVER THE PROPELLER TO NORMAL RPM AND, THEREFORE, THE PILOT SHUT DOWN AND SECURED THE LH
- [SDR CA130527011](https://openairdocs.org/sdr/CA130527011.md): Spring · weak · May 16, 2013 · Piagio P180 · Propeller Controlling System
  > (CAN) PROPELLER RPM DECAYED TO UNCOMMANDED FEATHER AT 1000` AGL AFTER TAKE OFF. PROPELLER FAILURE OCCURRED AFTER THE POST TAKE OFF POWER REDUCTION. UNABLE TO RECOVER PROPELLER TO NORMAL RPM. PRIOR TO THE FAILURE, THE PROPELLER GOVERNOR HAD BEEN REINSTALLED AF
- [SDR V2JA0504134142480](https://openairdocs.org/sdr/V2JA0504134142480.md): Adc · failed · May 4, 2013 · N165SL · Piagio P180 · Air Data Computer
  > BOTH ADC FAILED IN FLIGHT. ADC 1 FAILED FIRST, REVERTED TO ADC 2 WHICH FAILED 15 MINUTES LATER.
- [SDR V2JA0504134151771](https://openairdocs.org/sdr/V2JA0504134151771.md): Autofeather Sys · malfunctioned · May 4, 2013 · N132SL · Piagio P180 · Propeller Feathering/Reversing
  > CREW REPORTS UNCOMMANDED AUTOFEATHER ON LEFT ENGINE.
- [SDR V2JA2013043049004](https://openairdocs.org/sdr/V2JA2013043049004.md): Door · out of adjust · Apr 30, 2013 · N109SL · Piagio P180 · Cargo/Baggage Doors
  > CARGO DOOR LIGHT ON IN FLIGHT. ADJUSTED BAGGAGE DOOR IAW AMM 52-30-00. OPS CHECKED GOOD.
- [SDR 2013FA0000256](https://openairdocs.org/sdr/2013FA0000256.md): Wire Harness · misinstalled · Apr 26, 2013 · N79CN · Piagio P180 · Fuel System Wiring
  > RT FUEL QTY NOT DECREASING DURING RUN-UP. GROUND RUN-UP FINDING DATED 25-04, 2013. FOUND LT AND RT FUEL QUANTITY INDICATION SYSTEM CROSSED WITH EACH OTHER UNDERNEATH CENTER PEDESTAL FLOOR AT FS 500. WIRING BUNDLES REROUTED WITH THEIR RELATIVE INDICATORS TO T
- [SDR V2JA2013050447914](https://openairdocs.org/sdr/V2JA2013050447914.md): Landing Gear · failed · Apr 24, 2013 · N139SL · Piagio P180 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, WHEN GEAR SELECTED UP, HYD IN HIGH DUTY, 3 GREEN AND NO RED IN-TRANSIT. AFTER CYCLING THE LANDING GEAR HANDLE, LANDING GEAR RETRACTED NORMALLY. AFTER NOSE GEAR WAS LOWERED TO THE GROUND, FOLLOWING LANDING TOUCHDOWN, ACFT VEERED TO THE RT WITH
- [SDR V2JA2013033083417](https://openairdocs.org/sdr/V2JA2013033083417.md): Switch · out of adjust · Mar 30, 2013 · N132SL · Piagio P180 · Door Warning System
  > PILOT DISCREPANCY: BAG DOOR LIGHT IN FLIGHT. ADJUSTED AND OPS CHECKED BAGGAGE DOOR SWITCHES IAW P-180 LL MM 52-70-00, NO DEFECTS NOTED.
- [SDR V2JA20121218006](https://openairdocs.org/sdr/V2JA20121218006.md): Warning Light · illuminated · Mar 3, 2013 · N138SL · Piagio P180 · Door Warning System
  > CARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF, PERFORMED LT ENGINE SECURING CHECKLIST, LIGHT EXTINGUISHED AFTER THE ENGINE WAS SECURED, THEN ILLUMINATED AGAIN AND STAYED ON UNTILL SHORT FINAL, THEN EXTINGUISHED.
- [SDR V2JA201212180005](https://openairdocs.org/sdr/V2JA201212180005.md): Engine · failed · Feb 22, 2013 · N161SL · Piagio P180 · Engine (Turbine/Turboprop)
  > CLIMBING OUT OF FL260 TO FL310, RT TORQUE DROPPED 20 PERCENT AND IMMEDIATELY ROSE BACK TO 97 PERCENT. A SLIGHT HIGH FREQUENCY VIBRATION WAS THEN NOTICED BY CREW. CLIMB WAS CONTINUED TO FL310. AT FL310 OIL PRESSURE DROPPED BELOW 90PSI ON THE RT ENGINE WITH AU
- [SDR V2JA20121218004](https://openairdocs.org/sdr/V2JA20121218004.md): Autofeather Sys · activated · Feb 20, 2013 · N143SL · Piagio P180 · Propeller Feathering/Reversing
  > UNCOMMANDED AUTO FEATHER ON FINAL.
- [SDR V2JA0208134143337](https://openairdocs.org/sdr/V2JA0208134143337.md): Switch · dirty · Feb 8, 2013 · N143SL · Piagio P180 · Propeller Feathering/Reversing
  > UNCOMMANDED AUTOFEATHER IN FLIGHT ON LAST LEG. POWER LEVERS, AND ALL ENGINE PARAMETERS WERE EQUAL. FOUND SWITCH DIRTY.
- [SDR V2JA20121218003](https://openairdocs.org/sdr/V2JA20121218003.md): Propeller · faulty · Feb 7, 2013 · N143SL · Piagio P180 · Propeller Feathering/Reversing
  > UNCOMMANDED AUTO-FEATHER OF RT ENGINE ON FINAL.
- [SDR CA130212008](https://openairdocs.org/sdr/CA130212008.md): Oil System · low pressure · Jan 29, 2013 · Piagio P180 · Engine Oil Indicating System
  > (CAN) AFTER AN AIRCRAFT MAINTENANCE, DURING FLIGHT TESTING, 1 PROCEDURE CALLS FOR AN IN-FLIGHT SHUTDOWN AND RELIGHT. DURING THE RELIGHT ATTEMPT THE ENGINE NR 2 OIL PRESSURE WAS INDICATING 12 PSI. THE PILOT SHUTDOWN THE ENGINE AND LANDED SAFELY AT THE AIRPORT

Next page: https://openairdocs.org/model/piaggio-p180/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 = 'P180'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/piaggio-p180/reports

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