# N260AN: 1998 Learjet 60, registration cancelled 2009-12-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 2, 2009
- Exported to: Mexico
- Status when cancelled: Valid registration
- Airframe: [Learjet 60](https://openairdocs.org/model/learjet-60) (registry code 5170707)
- Engine: [Pratt & Whitney Canada 305 series](https://openairdocs.org/engine/pratt-whitney-canada-305-series) (registry code 52155)
- Data sheets: [TCDS A10CE](https://openairdocs.org/tcds/A10CE) (OpenAirDocs)
- Serial number: 124
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: October 16, 2004
- Certificate issued: October 22, 2009
- Last registry action: October 22, 2009
- Mode S code: A27F0A
- Owner when cancelled: [Four Star International Inc](https://openairdocs.org/faa-owner/FOUR%20STAR%20INTERNATIONAL%20INC)
- Location: [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas)
- Owner type: Corporation
- Owner's area on the map: 36.2051° N, 115.2237° W: Placed by OpenAirDocs at the center of ZIP code 89108, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N260AN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=260AN
- Page: https://openairdocs.org/deregistered/N260AN-2009-12-02

From the FAA registry file of November 7, 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 Learjet 60: https://openairdocs.org/model/learjet-60.md

## Service difficulty reports (1)

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

- [SDR JBG2008F00002](https://openairdocs.org/sdr/JBG2008F00002), Jun 30, 2008: HOSE. LEAKING. PILOT REPORTED A LOSS OF HYDRAULICS DURING FLIGHT AT CRUISE FL400. INSPECTION REVEALED THAT THE RT ENGINE DRIVEN HYD PUMP PRESSURE SIDE HYDRAULIC LINE WAS LEAKI

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