# N307RM: Raytheon HAWKER 800XP, registration cancelled 2025-03-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 27, 2025
- Status when cancelled: Valid registration
- Airframe: [Raytheon HAWKER 800XP](https://openairdocs.org/model/raytheon-hawker-800xp) (registry code 7150012)
- Engine: [Garrett TFE731 series](https://openairdocs.org/engine/garrett-tfe731-series) (registry code 29001)
- Data sheets: [TCDS A3EU](https://openairdocs.org/tcds/A3EU), [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (OpenAirDocs)
- Serial number: 258322
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 22, 1997
- Certificate issued: November 2, 2020
- Last registry action: April 1, 2023
- Mode S code: A33AD6
- Owner when cancelled: [Marklyn Jet Parts LLC](https://openairdocs.org/faa-owner/MARKLYN%20JET%20PARTS%20LLC)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: LLC
- Owner's area on the map: 32.8483° N, 96.8255° W: Placed by OpenAirDocs at the center of ZIP code 75209, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N307RM
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=307RM
- Page: https://openairdocs.org/deregistered/N307RM-2025-03-27

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 Raytheon HAWKER 800XP: https://openairdocs.org/model/raytheon-hawker-800xp.md

## Service difficulty reports (10)

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

- [SDR 9JLA2020120929950](https://openairdocs.org/sdr/9JLA2020120929950), Nov 24, 2020: ACTUATOR. LEAKING. THE FLIGHT CREW REPORTED THAT DURING POST FLIGHT CHECKS HYDRAULIC FLUID LEAKING FROM BOTH SIDES OF THE VERTICAL STAB AND UNDERNEATH THE HORIZONTAL STAB. THE MAI
- [SDR 9JLA2014122905110](https://openairdocs.org/sdr/9JLA2014122905110), Sep 27, 2014: INDICATOR. DEFECTIVE. THE STANDBY ATTITUDE INDICATOR FAILED IN FLIGHT. TROUBLESHOOTING FOUND THE STANDBY INDICATOR WAS DEFECTIVE. THE DEFECTIVE UNIT PN 501-1656-02 SN 1372 FAILED AFT
- [SDR 9JLA2014072104799](https://openairdocs.org/sdr/9JLA2014072104799), Jul 1, 2014: CIRCUIT BREAKER. DEFECTIVE. THE CREW REPORTED THAT THE MAIN RADIO MASTER FEEDER CB FOR THE PS2 POWER TRIPPED TAKING OUT ALL THE CO-PILOTS AVIONICS. TROUBLESHOOTING FOUND THE 35 AMP 3G MAIN
- [SDR 9JLA2014052904789](https://openairdocs.org/sdr/9JLA2014052904789), May 11, 2014: FILTER HOUSING. DEFECTIVE. THE HYD FILTER BYPASS PIN WAS FOUND TRIPPED DURING A POST FLIGHT CHECK. THE HYD FILTER WAS REMOVED & NO CONTAMINATION WAS FOUND. THE FILTER WAS REINSTALLED & TH
- [SDR 9JLA2013041704765](https://openairdocs.org/sdr/9JLA2013041704765), Apr 10, 2013: RMU. DEFECTIVE. IT WAS REPORTED THAT THE NR 2 RADIO MANAGEMENT UNIT SCREEN WAS SOLID RED, TROUBLESHOOTING FOUND THE NR 2 RMU DEFECTIVE. THE UNIT WAS REPLACED WITH A REPAIRED UN
- [SDR 9JLA2013031204755](https://openairdocs.org/sdr/9JLA2013031204755), Mar 8, 2013: GAUGE. LEAKING. MAINTENANCE DISCOVERED, DURING OXYGEN SERVICE THAT THE OXYGEN GAUGE LOCATED AT THE FILLER PORT HAD AN INTERNAL LEAK. REMOVED THE OXYGEN CONTENTS GAUGE AND INSTA
- [SDR 9JLA2012071904180](https://openairdocs.org/sdr/9JLA2012071904180), Jun 23, 2012: IGNITER BOX. FAILED. CREW REPORTED THAT THE APU WOULD NOT START, TROUBLESHOOTING IDENTIFED THE APU IGNITER BOX DEFECTIVE. A NEW UNIT WAS INSTALLED FUNCTIONAL CHECKED SATISFACTORY.
- [SDR 9JLA2012070704179](https://openairdocs.org/sdr/9JLA2012070704179), Jun 19, 2012: OVERHEAT SENSOR. DEFECTIVE. THE CREW REPORTED THAT THE DUCT OVERTEMP WARING ILLUMINATED DURING FLIGHT. TROUBLESHOT AND FOUND THAT THE LT HP AIR DUCT OVERHEAT DETECTOR WAS DEFECTIVE. REMOVE
- [SDR 9JLA2011122004169](https://openairdocs.org/sdr/9JLA2011122004169), Dec 11, 2011: WINDSHIELD. DEFECTIVE. PILOTS SIDE A PANEL HAD A 2 INCH VERTICAL SECTION THAT WAS NOT HEATING. REMOVED THE DEFECTIVE LEFT A PANEL. INSTALLED A REPAIRED WINDSHIELD IAW 56-10-11.
- [SDR 2011FA0000214](https://openairdocs.org/sdr/2011FA0000214), Mar 25, 2011: WINDSHIELD. DEFECTIVE. CREW REPORTED "THE CO-PILOTS A SCREEN IS NOT HEATING IN A SECTION ABOUT 1.5" WIDE AND RUNNING VERTICAL FROM TOP TO BOTTTOM". THE RT A WINDSHIELD WAS INSTALLED A

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