# N4513T: 1972 Piper PA-28R-200, registration cancelled 2025-06-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 23, 2025
- Status when cancelled: Sale reported, canceled
- Airframe: [Piper PA-28R-200](https://openairdocs.org/model/piper-pa-28r-200) (registry code 7102811)
- Engine: [Lycoming I0360 series](https://openairdocs.org/engine/lycoming-i0360-series) (registry code 41515)
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS 1E10](https://openairdocs.org/tcds/1E10) (OpenAirDocs)
- Serial number: 28R-7235073
- Year built: 1972
- Type of aircraft: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: February 21, 1972
- Last registry action: September 21, 2024
- Mode S code: A578A6
- Location: [Leesburg, VA](https://openairdocs.org/faa-place/VA/Leesburg)
- Owner type: Individual
- Owner's area on the map: 39.0644° N, 77.6038° W: Placed by OpenAirDocs at the center of ZIP code 20175, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N4513T
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=4513T
- Page: https://openairdocs.org/deregistered/N4513T-2025-06-23

From the FAA registry file of November 4, 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-28R-200: https://openairdocs.org/model/piper-pa-28r-200.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 H5GR2016060300273](https://openairdocs.org/sdr/H5GR2016060300273), May 13, 2016: RIB. CRACKED. SIDE LOAD STRESSES ON MLG ASSEMBLIES THAT ARE TRANSMITTED THROUGH THEIR RETRACT LINK ATTACH FORGING TO THE WIN SPAR AREA ARE CAUSING FATIGUE CRACKS TO FORM IN V
- [SDR H5GR2016060300272](https://openairdocs.org/sdr/H5GR2016060300272), May 13, 2016: RIB. CRACKED. SIDE LOAD STRESSES ON MLG ASSEMBLIES THAT ARE TRANSMITTED THROUGH THEIR RETRACT LINK ATTACH FORGING TO THE WING SPAR AREA ARE CAUSING FATIGUE CRACKS TO FORM IN 

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