# N505PJ: 2013 Embraer S A EMB-505, registration cancelled 2026-08-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 28, 2026
- Exported to: Pakistan
- Status when cancelled: Valid registration
- Airframe: [Embraer S A EMB-505](https://openairdocs.org/model/embraer-s-a-emb-505) (registry code 326040C)
- Engine: [Pratt & Whitney Canada PW535E](https://openairdocs.org/engine/pratt-whitney-canada-pw535e) (registry code 52297)
- Data sheets: [TCDS A60CE](https://openairdocs.org/tcds/A60CE), [TCDS E00053EN](https://openairdocs.org/tcds/E00053EN) (OpenAirDocs)
- Serial number: 50500165
- Year built: 2013
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 23, 2013
- Certificate issued: July 9, 2026
- Last registry action: July 9, 2026
- Mode S code: A64DD1
- Owner when cancelled: [Abb Aerospace LLC](https://openairdocs.org/faa-owner/ABB%20AEROSPACE%20LLC)
- Location: [Frisco, TX](https://openairdocs.org/faa-place/TX/Frisco)
- Owner type: LLC
- Owner's area on the map: 33.1334° N, 96.9147° W: Placed by OpenAirDocs at the center of ZIP code 75036, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N505PJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=505PJ
- Page: https://openairdocs.org/deregistered/N505PJ-2026-08-28

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 Embraer S A EMB-505: https://openairdocs.org/model/embraer-s-a-emb-505.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 9JLA2021060229008](https://openairdocs.org/sdr/9JLA2021060229008), May 27, 2021: MODULATING VALVE. BROKEN. THE FLIGHT CREW REPORTED THAT THE CABIN AND COCKPIT AIR FROM HEAT EXCHANGER / TEMPERATURE MODULATING VALVES WAS FAR TOO HOT. THE CREW STATED THEY WERE UNABLE TO
- [SDR 9JLA2021011129005](https://openairdocs.org/sdr/9JLA2021011129005), Jan 8, 2021: TRIM SYSTEM. FAILED. THE FLIGHT CREW REPORTED THAT THE PRIMARY PITCH TRIM FAILED IN FLIGHT LEVELING AT FLIGHT LEVEL 400. THEY INDICATED THAT THEY RECEIVED A PITCH TRIM FAIL CAS MESS

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