# N15PR: 1983 Piper PA-31-350, registration cancelled 2018-02-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 8, 2018 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Piper PA-31-350](https://openairdocs.org/model/piper-pa-31-350) (registry code 7103110) - Engine: [Lycoming TI0-540 series](https://openairdocs.org/engine/lycoming-ti0-540-series) (registry code 41533) - Data sheets: [TCDS A20SO](https://openairdocs.org/tcds/A20SO), [TCDS E14EA](https://openairdocs.org/tcds/E14EA) (OpenAirDocs) - Serial number: 31-8352011 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, normal - Airworthiness date: June 26, 1995 - Certificate issued: October 25, 2007 - Last registry action: July 18, 2012 - Mode S code: A0C92B - Owner when cancelled: [Limbo LLC](https://openairdocs.org/faa-owner/LIMBO%20LLC) - Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage) - Owner type: Corporation - Owner's area on the map: 61.1637° N, 149.9966° W: Placed by OpenAirDocs at the center of ZIP code 99502, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N15PR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=15PR - Page: https://openairdocs.org/deregistered/N15PR-2018-02-08 From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Piper PA-31-350: https://openairdocs.org/model/piper-pa-31-350.md ## Service difficulty reports (11) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR PNSA060403](https://openairdocs.org/sdr/PNSA060403), Apr 26, 2006: PROPELLER. DAMAGED. ON TAKEOFF THE NR 1 PROPELLER WAS DAMAGED BY ROCKS DUE TO SOFT SPOT IN GRAVEL RUNWAY. MX REPLACED PROPELLER, AND ENGINE WAS TO BE INSPECTED PER LYCOMING SB 475C - [SDR PNSA031103](https://openairdocs.org/sdr/PNSA031103), Nov 19, 2003: WIRE. BROKEN. WHILE IN IFR CRUISE EXPERIENCED TOTAL ELECTRICAL FAILURE. BY SHUTING OFF ANTI-ICE EQUIPMENT WAS ABLE TO RESTORE POWER. RECEIVED PRIOITY ATC HANDLING LANDED IN D - [SDR PNSA001202](https://openairdocs.org/sdr/PNSA001202), Dec 11, 2000: ALTIMETER. INTERMITTENT. PILOT NOTICED ALTIMETER APPEARED TO BE STUCK. THIS WAS CONFIRMED BY CROSS REFERENCEING THE CO-PILOT AND GPS ALTIMETERS. REPLACED FAULTY ALTIMETER. - [SDR PNSA000403](https://openairdocs.org/sdr/PNSA000403), Apr 20, 2000: FUEL LINE. LEAKING. DURING CRUISE, PILOT SMELLED FUEL. AFTER LOOKING AROUND THE COCKPIT, PILOT NOTICED A SMALL FUEL STAIN IN THE COPILOT''S CARPET. THE AIRCRAFT IMMEDIATELY RETURNE - [SDR PNSA990402](https://openairdocs.org/sdr/PNSA990402), Apr 6, 1999: SWITCH. LACK OF LUBE. UPON GEAR RETRACTION UNSAFE LIGHT WOULD NOT EXTINGUISH AND SELECTOR WOULD NOT GO TO NEUTRAL. RETURNED TO AIRPORT FOR UNEVENTFUL LANDING. CLEANED AND LUBED ALL G - [SDR PNSA990303](https://openairdocs.org/sdr/PNSA990303), Mar 19, 1999: INDICATOR. INOPERATIVE. ON APPROACH TO MYU, RT ENGINE RPM INDICATION WENT TO ZERO, ENGINE RUNNING OK. RETURNED TO BET FOR UNEVENTFUL LANDING. REPLACED RPM INDICATOR, OPS CHECKED OK. - [SDR PNSA980902](https://openairdocs.org/sdr/PNSA980902), Sep 19, 1998: PULLEY. WORN. RT ALTERNATOR LIGHT CAME ON WHILE CRUISING IN PRECIP. RETURNED TO BASE. REPLACED ALTERNATOR PULLEY DUE TO WEAR. - [SDR PNSA980501A](https://openairdocs.org/sdr/PNSA980501A), May 16, 1998: SENDING UNIT. FAILED. WHILE IN CRUISE, THE PILOT NOTED A RAPID DROP IN FUEL QTY INDICATION. SHORTLY THEREAFTER THE LT ENG LOST POWER. FOLLOWED BY A RT ENG POWER LOSS 2 MIN LATER. A S - [SDR PNSA980501](https://openairdocs.org/sdr/PNSA980501), May 16, 1998: ENGINE. POWER LOSS. WHILE IN CRUISE, THE PILOT NOTED A RAPID DROP IN FUEL QUANTITY INDICATION. SHORTLY THERE AFTER THE LEFT ENGINE LOST POWER. FOLLOWED BY A RT ENGINE POWER LOSS TW - [SDR PNSA980503](https://openairdocs.org/sdr/PNSA980503), May 5, 1998: TURBO CHARGER. MALFUNCTIONED. LT ENGINE WOULD NOT DEVELOPE FULL POWER, ABORTED TAKEOFF. REPLACED TURBO CHARGER, OPERATIONAL CHECK OK. - [SDR PNSA980210](https://openairdocs.org/sdr/PNSA980210), Feb 7, 1998: UPLOCK ROLLERS. LACK OF LUBE. NOSE GEAR WOULD NOT LOCK UP. CLEANED AND LUBED DIRTY NOSE GEAR UPLOCK ROLLER, OPS CHECK OK. ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB ANC13CA023](https://openairdocs.org/ntsb/ANC13CA023), Feb 16, 2013: Piper PA-31-350 (N15PR), Dutch Harbor, AK, substantial damage. Probable cause: The pilot's decision to land in wind conditions that exceeded the airplane's demonstrated crosswind capability, which resulted in a loss of airplane control during the landing roll. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20130216002649A](https://openairdocs.org/incident/20130216002649A), Feb 16, 2013: Piper PA-31-350 (N15PR), Dutch Harbor, AK, Substantial damage. When the pilot departed Dutch for akun the runway was wet and the weather was improving. When he returned 45 minutes later, the temperature had dropped below… --- 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.