# N860TM: Raytheon HAWKER 800XP, registration cancelled 2017-02-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 16, 2017
- Exported to: India
- Status when cancelled: Valid registration
- Airframe: [Raytheon HAWKER 800XP](https://openairdocs.org/model/raytheon-hawker-800xp) (registry code 7150012)
- Data sheets: [TCDS A3EU](https://openairdocs.org/tcds/A3EU) (OpenAirDocs)
- Serial number: 258479
- Type of aircraft: Fixed wing multi engine
- Certificate issued: January 10, 2017
- Last registry action: January 10, 2017
- Mode S code: ABD08C
- Owner when cancelled: [Rangeflyers Inc](https://openairdocs.org/faa-owner/RANGEFLYERS%20INC)
- Location: [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- Owner type: Corporation
- Owner's area on the map: 37.6815° N, 97.1678° W: Placed by OpenAirDocs at the center of ZIP code 67230, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N860TM
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=860TM
- Page: https://openairdocs.org/deregistered/N860TM-2017-02-16

From the FAA registry file of November 5, 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 Raytheon HAWKER 800XP: https://openairdocs.org/model/raytheon-hawker-800xp.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 T17A201401078004](https://openairdocs.org/sdr/T17A201401078004), Jan 7, 2014: UNKNOWN. MALFUNCTIONED. DURING CLIMB, PILOT ATTEMPTED TO ENGAGE YAW DAMP & REPORTED THAT IT DID NOT ENGAGE. ABNORMAL FORCE WAS REQUIRED TO DEFLECT RUDDER PEDALS HOWEVER, AS IF YAW DAMP
- [SDR E81R2012032900001](https://openairdocs.org/sdr/E81R2012032900001), Mar 29, 2012: WEB. CRACKED. DURING SCHEDULED AIRFRAME "F" 24-MONTH AND "G" 48-MONTH INSPECTIONS, NOTED CRACK IN WEB OF FORWARD AND AFT RUNNING UNDER FLOORBEAM UNDER COPILOT'S SEAT AREA.

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