# N910CF: Raytheon Corporate Jets HAWKER 800

- Status: Valid registration
- Airframe: [Raytheon Corporate Jets HAWKER 800](https://openairdocs.org/model/raytheon-corporate-jets-hawker-800) (registry code 7450004, 17 seats)
- Engine: [Honeywell TFE731-5R](https://openairdocs.org/engine/honeywell-tfe731-5r) (registry code 33852)
- Data sheets: [TCDS A3EU](https://openairdocs.org/tcds/A3EU) (Textron Aviation Inc.), [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (Honeywell Aerospace US LLC) (OpenAirDocs)
- Serial number: 258267
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 10, 2014
- Certificate issued: January 2, 2023
- Expires: January 31, 2030
- Mode S code: AC96E3
- Registered owner: [Navi Aviation LLC](https://openairdocs.org/faa-owner/NAVI%20AVIATION%20LLC)
- Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover)
- Owner type: LLC
- Owner's area on the map: 39.1713° N, 75.5876° W: Placed by OpenAirDocs at the center of ZIP code 19904, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=910CF
- Page: https://openairdocs.org/aircraft/N910CF

From the FAA registry file of October 21, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 40 in force

### Matched by airframe (Raytheon Corporate Jets HAWKER 800)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2013-11-16](https://openairdocs.org/ad/2013-11-16): Flight Controls and Wings · Winglets (Aviation Partners STC ST01411SE). Effective Jul 2, 2013
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2006-12-20](https://openairdocs.org/ad/2006-12-20): Current limiters for the PE, PS1, and PS2 busses · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 9 more. Effective Jul 3, 2006
- [AD 2006-01-04](https://openairdocs.org/ad/2006-01-04): Fan venturi motor casing · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 42 more. Effective Feb 22, 2006
- [AD 2005-16-02](https://openairdocs.org/ad/2005-16-02): Cockpit ventilation and avionics cooling system blowers · Textron BAe.125 Series 800A, Hawker 800, Hawker 800XP and 1 more. Effective Sep 6, 2005
- [AD 2005-03-16](https://openairdocs.org/ad/2005-03-16): Engine compartment firewall · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125) and 40 more. Effective Mar 21, 2005
- [AD 2004-12-02](https://openairdocs.org/ad/2004-12-02): Wire bundles · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800B and 1 more. Effective Jul 14, 2004
- [AD 2004-11-01](https://openairdocs.org/ad/2004-11-01): Engine fire extinguishing wiring · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125) and 4 more. Effective Jul 7, 2004
- [AD 2003-07-07](https://openairdocs.org/ad/2003-07-07): Tie-bolt Nuts of Main Landing Gear (MLG) Wheels · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125) and 31 more. Effective May 8, 2003
- [AD 2003-06-06](https://openairdocs.org/ad/2003-06-06): Attachment bolts · Textron Hawker 800, Hawker 800 (U-125A) and Hawker 800XP. Effective Apr 30, 2003
- [AD 2003-04-20](https://openairdocs.org/ad/2003-04-20): Cylinder Head Lugs of Main Landing Gear (MLG) Actuator · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 43 more. Effective Apr 4, 2003
- [AD 2001-15-25](https://openairdocs.org/ad/2001-15-25): Attachment Bolt in the Main Landing Gear Door System · Textron Hawker 800 (U-125A) and Hawker 800XP. Effective Sep 10, 2001
- [AD 2001-13-05](https://openairdocs.org/ad/2001-13-05): Turbine Air Discharge Duct and Water Separator Outlet Duct · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 6 more. Effective Aug 1, 2001
- [AD 2000-24-25](https://openairdocs.org/ad/2000-24-25): Nose Landing Gear Drag Stay Roller Clearance Inspection · Textron Hawker 800 (U-125A) and Hawker 800XP. Effective Jan 16, 2001
- [AD 2000-22-22](https://openairdocs.org/ad/2000-22-22): Wire Bundle Exiting Panel · Textron Hawker 800 (U-125A) and Hawker 800XP. Effective Dec 19, 2000
- [AD 2000-22-03](https://openairdocs.org/ad/2000-22-03): Pitot/Static and Stall Vent Drain Valves · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 43 more. Effective Dec 4, 2000
- [AD 2000-08-07](https://openairdocs.org/ad/2000-08-07): Tooling Holes · Textron BAe.125 Series 800A, BAe.125 Series 800B, Hawker 800 and 1 more. Effective May 31, 2000
- [AD 2000-02-35](https://openairdocs.org/ad/2000-02-35): Oxygen System Plumbing · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 36 more. Effective Mar 13, 2000
- [AD 97-05-03 R1](https://openairdocs.org/ad/97-05-03-R1): Global Positioning Systems · BAE Systems Avro 146-RJ100A, BAe 146-200A, Jetstream Model 4101 and 27 more. Effective Apr 20, 1999
- [AD 98-11-13](https://openairdocs.org/ad/98-11-13): Fire Extinguisher Assemblies · Textron Hawker 800 (U-125A) and Hawker 800XP. Effective Jun 8, 1998
- [AD 97-21-05](https://openairdocs.org/ad/97-21-05): High Pressure Oxygen Hose Assemblies · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125) and 8 more. Effective Nov 24, 1997
- [AD 97-21-03](https://openairdocs.org/ad/97-21-03): Fuel Feed Hose Assemblies of Auxiliary Power Unit · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125) and 2 more. Effective Nov 19, 1997
- [AD 97-18-07](https://openairdocs.org/ad/97-18-07): Rudder · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125) and 3 more. Effective Oct 3, 1997
- [AD 97-03-07](https://openairdocs.org/ad/97-03-07): Main Landing Gear Sidestay Assemblies · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 42 more. Effective Mar 11, 1997
- [AD 96-18-09](https://openairdocs.org/ad/96-18-09): TKS Metering Pump · Textron BAe.125 Series 1000A, BAe.125 Series 800A, Hawker 1000 and 1 more. Effective Oct 9, 1996
- [AD 96-12-17](https://openairdocs.org/ad/96-12-17): Engine Starting Circuits Diode Soldered Connections · Textron BAe.125 Series 1000A, BAe.125 Series 800A, Hawker 1000 and 1 more. Effective Jul 15, 1996
- [AD 96-12-16](https://openairdocs.org/ad/96-12-16): Control Of Ailerons · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125) and 1 more. Effective Jul 15, 1996
- [AD 95-08-06](https://openairdocs.org/ad/95-08-06): Static Inverter · Textron BAe.125 Series 800A, BH.125 Series 400A, BH.125 Series 600A and 29 more. Effective May 18, 1995

### Matched by engine (Honeywell TFE731-5R)

- [AD 2016-07-02](https://openairdocs.org/ad/2016-07-02): Failure of the interstage turbine transition duct · Honeywell International TFE731-4, TFE731-4R, TFE731-5AR and 2 more. Effective May 5, 2016
- [AD 2014-12-52](https://openairdocs.org/ad/2014-12-52): Engines · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 11 more. Effective Jul 28, 2014
- [AD 2012-17-05](https://openairdocs.org/ad/2012-17-05): First stage low-pressure turbine (LPT1) rotor assembly · Honeywell International TFE731-4, TFE731-4R, TFE731-5 and 3 more. Effective Oct 2, 2012
- [AD 2010-06-11](https://openairdocs.org/ad/2010-06-11): Second stage low-pressure compressor rotor (LPCR) discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2C and 16 more. Effective Apr 21, 2010
- [AD 2008-19-12](https://openairdocs.org/ad/2008-19-12): ITT duct · Honeywell International TFE731-4, TFE731-4R, TFE731-5 and 3 more. Effective Oct 27, 2008
- [AD 2008-02-19](https://openairdocs.org/ad/2008-02-19): High pressure (HP) turbine rotor assemblies · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 15 more. Effective Mar 6, 2008
- [AD 2000-15-09](https://openairdocs.org/ad/2000-15-09): HPC Impeller · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 20 more. Effective Oct 10, 2000
- [AD 90-24-06](https://openairdocs.org/ad/90-24-06): Thermocouple Lead Assemblies · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 8 more. Effective Nov 13, 1990
- [AD 89-22-16](https://openairdocs.org/ad/89-22-16): Engine Acceleration or Deceleration · Honeywell International TFE731-2, TFE731-5, TFE731-5AR and 1 more

### Historical (superseded or no longer in force)

- [AD 2001-17-26 R1](https://openairdocs.org/ad/2001-17-26-R1) (historical): Actuator Cylinder Head Lugs · Raytheon BAe.125 Series (all), BH.125 Series (all), DH.125 Series (all) and 5 more. Effective Oct 3, 2001
- [AD 2001-17-26](https://openairdocs.org/ad/2001-17-26) (historical): Main Landing Gear Actuator · Raytheon BAe.125 Series (all), BH.125 Series (all), DH.125 Series (all) and 5 more. Effective Oct 3, 2001
- [AD 96-24-16](https://openairdocs.org/ad/96-24-16) (historical): Tooling Holes In Firewalls · Hawker Beechcraft BAe.125 Series 800A, Hawker 800, Hawker 800 (U-125A) and 1 more. Effective Jan 27, 1997
- [AD 94-11-03](https://openairdocs.org/ad/94-11-03) (historical): Fan Casing Clearance · Raytheon BAe.125 Series (all), BH.125 Series (all), DH.125 Series (all) and 5 more. Effective Jun 10, 1994

## Information bulletins (advisory) (5 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB CE-20-10](https://openairdocs.org/saib/CE-20-10): Air Distribution System: Loss of Cabin Pressure. Issued Apr 30, 2020
- [SAIB NM-15-24](https://openairdocs.org/saib/NM-15-24): Landing Gear. Issued Sep 29, 2015
- [SAIB NM-14-05](https://openairdocs.org/saib/NM-14-05): Wing: Ailerons. Issued Nov 27, 2013
- [SAIB NM-11-60](https://openairdocs.org/saib/NM-11-60): Landing Gear. Issued Sep 29, 2011
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N910CF.

## FAA accident and incident reports

None matched to N910CF.

## Service difficulty reports (1)

As reported by operators and repair stations.

- [SDR FVJA20181214001](https://openairdocs.org/sdr/FVJA20181214001), Dec 6, 2018: STARTER GEN. FAILED. DURING CRUISE FLIGHT AT AN ALTITUDE OF FL380 ENROUTE FROM TORONTO-PEARSON INTERNATIONAL AIRPORT (CYYZ) TO MCCARREN INTERNATIONAL AIRPORT (KLAS) THE CREW EXPERIE

## Related

- Other Raytheon Corporate Jets HAWKER 800 aircraft: https://openairdocs.org/model/raytheon-corporate-jets-hawker-800/aircraft.md
- STCs for the Raytheon Corporate Jets HAWKER 800: https://openairdocs.org/model/raytheon-corporate-jets-hawker-800/stcs.md
- The Honeywell TFE731-5R engine: https://openairdocs.org/engine/honeywell-tfe731-5r.md

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