# N315PD: 2003 Agusta A119, registration cancelled 2015-06-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 9, 2015
- Exported to: Canada
- Status when cancelled: Valid registration
- Airframe: [Agusta A119](https://openairdocs.org/model/agusta-a119) (registry code 0260102)
- Engine: [Pratt & Whitney PT6 series](https://openairdocs.org/engine/pratt-whitney-pt6-series) (registry code 52033)
- Data sheets: [TCDS H7EU](https://openairdocs.org/tcds/H7EU) (OpenAirDocs)
- Serial number: 14035
- Year built: 2003
- Type of aircraft: Rotorcraft
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: December 9, 2003
- Certificate issued: October 7, 2014
- Last registry action: October 7, 2014
- Mode S code: A35AAD
- Owner when cancelled: [Can See Aviation LLC](https://openairdocs.org/faa-owner/CAN%20SEE%20AVIATION%20LLC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.8187° N, 75.5062° W: Placed by OpenAirDocs at the center of ZIP code 19810, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N315PD
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=315PD
- Page: https://openairdocs.org/deregistered/N315PD-2015-06-09

From the FAA registry file of October 29, 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 Agusta A119: https://openairdocs.org/model/agusta-a119.md

## Service difficulty reports (2)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 2008FA0000774](https://openairdocs.org/sdr/2008FA0000774), Oct 31, 2008: TRIM TAB. DELAMINATED. UPON POST FLIGHT IT WAS NOTICED THE MAIN ROTOR BLADE TRIM TAB WAS SERIOUSLY DELAMINATED AND SEPARATED IN FLIGHT. THIS PROBLEM HAS OCCURRED NUMEROUS TIMES IN THE
- [SDR DT12006F00000](https://openairdocs.org/sdr/DT12006F00000), Jan 20, 2006: GRIP. DEBONDED. GRIP FOR MAIN ROTOR BLADE IS COMPOSITE LAMINATE. DEBONDED ON LEADING EDGE. 2ND GRIP ON AIRCRAFT. AIRCRAFT IS POLICE HELICOPTER. (K)

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