# Hawker Beechcraft HAWKER 800XP

- Type: Aircraft model (FAA registry)
- Registry code: 4220000
- Manufacturer (registry): HAWKER BEECHCRAFT CORP
- Model: HAWKER 800XP
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 15
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A3EU](https://openairdocs.org/tcds/A3EU) (OpenAirDocs)
- Holder: Textron Aviation Inc.
- Registered aircraft: 1
- Page: https://openairdocs.org/model/hawker-beechcraft-hawker-800xp

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [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 2014-15-08](https://openairdocs.org/ad/2014-15-08): Fuel · Textron Hawker 800XP, Hawker 850XP and Hawker 900XP. Effective Sep 5, 2014
- [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 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2009-08-01](https://openairdocs.org/ad/2009-08-01): Honeywell FMSs · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R), CL-600-2B16 (CL-604) and 11 more. Effective May 14, 2009
- [AD 2008-21-01](https://openairdocs.org/ad/2008-21-01): Main landing gear (MLG) · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125) and 1 more. Effective Oct 22, 2008
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 2007-21-08](https://openairdocs.org/ad/2007-21-08): Inspection of panel DA wiring · Textron Hawker 800XP. Effective Nov 20, 2007
- [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 2006-11-07](https://openairdocs.org/ad/2006-11-07): Bus bars in the DA-A panel · Textron Hawker 800XP. Effective Jun 29, 2006
- [AD 2006-02-03](https://openairdocs.org/ad/2006-02-03): Hydraulic over-temperature switch · Textron Hawker 800XP. Effective Feb 24, 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 2005-09-03](https://openairdocs.org/ad/2005-09-03): Wiring in the flight compartment · Textron Hawker 800XP. Effective Jun 1, 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 2004-11-01](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 2004-09-26](https://openairdocs.org/ad/2004-09-26): Pitot probes · Textron Hawker 800XP. Effective Jun 15, 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 2002-26-22](https://openairdocs.org/ad/2002-26-22): Digital electronic engine · Textron Hawker 800XP. Effective Feb 18, 2003
- [AD 2002-20-09](https://openairdocs.org/ad/2002-20-09): Adaptive flight display units · Bombardier CL-600-2A12 (CL-601), 525, 525A and 5 more. Effective Nov 12, 2002
- [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 2001-12-17](https://openairdocs.org/ad/2001-12-17): Rivets at Fuselage Stations · Textron Hawker 800XP. Effective Jul 25, 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 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 98-23-15](https://openairdocs.org/ad/98-23-15): Fuel Feed Hose Assemblies · Textron Hawker 800XP. Effective Dec 18, 1998
- [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 97-18-07](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

Historical (superseded or no longer in force):

- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [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) (6)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 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

## Registered aircraft (1)

- [N847TX](https://openairdocs.org/aircraft/N847TX): [4 Ms Holding LLC](https://openairdocs.org/faa-owner/4%20MS%20HOLDING%20LLC), [Spring, TX](https://openairdocs.org/faa-place/TX/Spring), built 2007, S/N 258847

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (916, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR Y9PA2026031100169](https://openairdocs.org/sdr/Y9PA2026031100169), Mar 11, 2026: BRAKE ASSY. SEPARATED. NO. 4 BRAKE PAD SEPERATED WHEN AIRCRAFT WAS BEING TOWED OUT OF HANGAR CAUSING THE BRAKE TO LOCK UP.
- [SDR 2026F00024](https://openairdocs.org/sdr/2026F00024), Mar 9, 2026: WINDSHIELD. CRACKED. PILOT'S "A" SCREEN OUTER LAYER CRACKED AT FL370. EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED TO KRDU. LANDING WAS SUCCESSFUL WITH NO FURTHER ISSUE.
- [SDR MDGA202602100001](https://openairdocs.org/sdr/MDGA202602100001), Feb 8, 2026: HANGER ASSY. FRACTURED. AFTER DEPARTURE UPON SELECTION OF GEAR UP THE LEFT MAIN LANDING GEAR REMAINED EXTENDED. TOWER FLYBY CONFIRMED SINGLE LEG EXTENSION. THE DECISION WAS MADE TO DIV
- [SDR Y9PA20251111001](https://openairdocs.org/sdr/Y9PA20251111001), Nov 11, 2025: DISPLAY. INOPERATIVE. MFD DISPLAY INOPERATIVE. DOES NOT DISPLAY ANYTHING.
- [SDR EXFA2025FA0000730](https://openairdocs.org/sdr/EXFA2025FA0000730), Oct 20, 2025: WARNING MESSAGE. FALSE ACTIVATION. UPON REDUCING POWER FOR DESCENT FLIGHT CREW NOTICED HYDRAULIC LOW PRESSURE LIGHTS ON. COULD NOT DUPLICATE ON THE GROUND.
- [SDR 2025FA0000730](https://openairdocs.org/sdr/2025FA0000730), Oct 20, 2025: HYDRAULIC SYSTEM. LOW PRESSURE. #1 AND #2 HYDRAULIC LOW PRESSURE LIGHT ON. HYDRAULIC @ 2300PSI. PERFORMED GEAR FREE LANDING PROCEDURE.
- [SDR EXFA2025120800728](https://openairdocs.org/sdr/EXFA2025120800728), Oct 6, 2025: PIPE. CRACKED. WHILE IN CRUISE FLIGHT, CREW NOTED HYDRAULIC LOW PRESSURE LIGHTS ON, ENGINES 1 AND 2 WITH A HYDRAULIC PRESSURE OF 2300 PSI. CREW DIVERTED TO AN ALTERNATE AIRPOR
- [SDR 2025FA0000728](https://openairdocs.org/sdr/2025FA0000728), Oct 6, 2025: HYDRAULIC LINE. LEAKING. HYDRAULIC LOW PRESSURE LIGHTS #1 AND #2 FLIGHT LIGHTS IN HYDRAULIC PRESSURE INDICATOR READ 2300 PSI. CREW PERFORMED FREEFALLING LANDING GEAR PROCEDURE.
- [SDR 2025FA0000729](https://openairdocs.org/sdr/2025FA0000729), Sep 24, 2025: INSTRUMENT PANEL. FAULTED. STANDBY INSTRUMENT INOP
- [SDR 2RPA2025050100008](https://openairdocs.org/sdr/2RPA2025050100008), May 1, 2025: DUCT CLAMP. LOOSE. ON MAY 1, 2025, N80PK DEPARTED KBCT IN ROUTE TO KHPN WITH PAX. AT FL410 THE CREW NOTICED THE CABIN RATE BEGINNING TO CLIMB. SHORTLY AFTER, THE CABIN ALT LIGHT I
- [SDR 2025F00049](https://openairdocs.org/sdr/2025F00049), Feb 19, 2025: SQUAT SWITCH. INOPERATIVE. “ AT FLIGHT LEVEL 380 IN NORMAL CRUISE FLIGHT WE RECEIVED AUDIBLE AND MWS PANEL WARNINGS OF LOSS OF PRESSURIZATION. WE DONNED MASKS AND IMMEDIATELY BEGAN AN EME
- [SDR UVCA202502210016](https://openairdocs.org/sdr/UVCA202502210016), Feb 16, 2025: LANDING GEAR. ACTIVE. AIRCRAFT DEPARTED HVN IN LIGHT RAIN/ WINTRY MIX WEATHER TEMPERATURE 35 DEGREES HEADED OMA FOR A FUELING EVOLUTION, AIRCRAFT CLIMBED DIRECT TO THEIR ASSIGNED ALT
- [SDR G13A20250214001](https://openairdocs.org/sdr/G13A20250214001), Feb 14, 2025: WARNING MESSAGE. ILLUMINATED. AT FL380 ENROUTE AN IAS AND MACH TRIM FAIL MESSAGE CAME ON WHICH DISABLED THE AUTOPILOT AND YAW DAMPENER. AFTER ESTABLISHING CONTROL WE BEGAN RUNNING THE CHECKL
- [SDR UVCA202501270017](https://openairdocs.org/sdr/UVCA202501270017), Jan 17, 2025: OUTFLOW VALVE. WARNING MESSAGE. BETWEEN FLIGHT LEVEL'S 370 & 380 AT THE POINT OF LEVELING OFF AT 380 THE CABIN ALT RED ANNUNCIATOR ON THE MASTER WARNING PANEL ILLUMINATED AND THE AURAL HORN SO
- [SDR 2025F00016](https://openairdocs.org/sdr/2025F00016), Dec 24, 2024: APU. CONTAMINATED. SMOKE IN COCKPIT CAUSED BY DEICING FLUID IN APU INTAKE DURIMNG DEICING PROCEDURES ON GROUND PRIOR TO TAKEOFF
- [SDR 2RPA2024111800006](https://openairdocs.org/sdr/2RPA2024111800006), Nov 15, 2024: WIRE HARNESS. PINCHED. ON LANDING IN BUF, AFTER GEAR EXTENSION AND FLAPS 45 NOTICED NO GREEN LANDING GEAR LIGHTS. NOSE GEAR PIN WAS OUT INDICATING DOWN AND LOCKED NOSE GEAR. PERFORMED
- [SDR OZTA202407190170](https://openairdocs.org/sdr/OZTA202407190170), Jul 7, 2024: AIR DUCT. BUCKLED. DURING CRUISE PORTION OF FLIGHT AT ALTITUDE 39,000 FT. FLIGHT CREW EXPERIENCED CABIN DECOMPRESSION, DONNED THEIR OXYGEN MASKS, DECLARED EMERGENCY, AND DIVERTED 
- [SDR 2024FA0000004](https://openairdocs.org/sdr/2024FA0000004), Jan 1, 2024: PITOT SYSTEM. BLOCKED. LOST AIRSPEED INDICATOR DURING DESCENT IN EXCESSIVE/SEVERE ICING. ALSO RECEIVING A PITOT/VANE HEAT FAILURE ANNUNCIATOR LIGHT. PERFORMED VISUAL INSPECTION OF PIL
- [SDR 2024F00000](https://openairdocs.org/sdr/2024F00000), Dec 27, 2023: CONTROLLER. FAILED. ON CLIMB OUT FROM DENVER, CENTENNIAL, (KAPA), THE AIRPLANE WOULD NOT PRESSURIZE. THE CREW ELECTED TO RETURN TO THE POINT OF DEPARTURE. MAINTENANCE WAS SUMMONED.
- [SDR 2023FA0000835](https://openairdocs.org/sdr/2023FA0000835), Dec 15, 2023: MIXING VALVE. STUCK. AS FLIGHT CREW BEGAN DESCENT FROM FL380 TO THEIR DESTINATION AIRPORT KBOW CABIN ALTITUDE BEGAN TO CLIMB AND HIGH CABIN ALTITUDE WARNING HORN CAME ON . CABIN OXY
- [SDR 2023F00336](https://openairdocs.org/sdr/2023F00336), Nov 9, 2023: UNKNOWN. UNKNOWN. AFTER TAKEOFF FROM TETERBORO, NJ (KTEB), CLIMBING THROUGH FL 250, THE UPPER AND LOWER NAVIGATIONAL SCREENS ON THE CAPTAINS SIDE (LEFT), WENT BLANK. ON THE FIRST
- [SDR 2023F00330](https://openairdocs.org/sdr/2023F00330), Nov 5, 2023: UNKNOWN. UNKNOWN. ON CLIMB OUT LEFT ENGINE SHUT DOWN WITH OIL SMELL IN CABIN. AFTER LANDING NOTED NO OIL INDICTING IN SIGHT GAGE
- [SDR 1JAA20231011004](https://openairdocs.org/sdr/1JAA20231011004), Oct 11, 2023: UNKNOWN. UNKNOWN. AIRCRAFT DEPRESSURIZED DURING CLIMB FROM KBCT. CREW INITIATED DECENT TO 10000FT., PERFORMED THE DEPRESSURIZATION CHECKLIST, AND HELD TO BURN OFF FUEL AS REQUIRE
- [SDR 2023FA0000468](https://openairdocs.org/sdr/2023FA0000468), Aug 25, 2023: MOUNT. CRACKED. THE LOWER ENGINE MOUNT WAS FOUND TO BE CRACKED DURING MAJOR ENGINE INSPECTION NDT TASK 530017.
- [SDR 9JLA2023022140523](https://openairdocs.org/sdr/9JLA2023022140523), Feb 14, 2023: NONE. NONE. THE FLIGHT CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE IN AUTOMATIC MODE CONTROL. THE MAINTENANCE PROVIDER TROUBLESHOT THE SYSTEM TO A CLOGGED JET PIPE AND 
- [SDR 2023F00048](https://openairdocs.org/sdr/2023F00048), Jan 17, 2023: TIRE. DAMAGED. UPON LANDING AT BURLINGTON, WA (KBVS) THE #1 AND #2 TIRES SCUFFED BEYOND SERVICEABILITY., THE #1 AND #2 TIRES AND WHEELS WERE REPLACED AND THE AIRPLANE WAS RETU
- [SDR 2RPA2023011700002](https://openairdocs.org/sdr/2RPA2023011700002), Jan 15, 2023: ENGINE. STALLED. WHILE CLIMBING OUT A HIGH FREQUENCY SOUND OCCURRED AT ABOUT 10,000FT. AT ABOUT 25,000FT A STRONG VIBRATION DEVELOPED AND THE SOUND INTENSIFIED AND CABIN AND COC
- [SDR 9JLA2022122939632](https://openairdocs.org/sdr/9JLA2022122939632), Dec 7, 2022: RMU. DEFECTIVE. THE FLIGHT CREW REPORTED THAT THE CO-PILOTS INTERPHONE WAS INOP, CONTINUOUS STATIC WAS EMITTED FROM SPEAKERS AND CO-PILOTS OXYGEN MASK MICROPHONE WAS INOP DURIN
- [SDR YQKA202211290001](https://openairdocs.org/sdr/YQKA202211290001), Nov 29, 2022: SEAL. DAMAGED. REAR BAY OVERHEAT ILLUMINATED DURING DEPARTURE CLIMB TO CRUISE ALTITUDE.
- [SDR 9JLA2022092039607](https://openairdocs.org/sdr/9JLA2022092039607), Sep 3, 2022: COMPUTER. FAILED. THE FLIGHT CREW REPORTED THAT THE AOA INDEXER WAS STUCK AT 1.0 WHILE IN FLIGHT. THIS DISCREPANCY WAS DEFERRED UNDER MEL 34-20-5 AND OPERATIONS WERE ABLE TO CONT
- [SDR MDGA8733081722](https://openairdocs.org/sdr/MDGA8733081722), Aug 16, 2022: FUEL CONTROL. POWER LOSS. ENGINE POWER REDUCED FOR DESCENT AND UPON LEVEL OFF ENGINE WOULD NOT ACCELERATE ABOVE FLIGHT IDLE. ENGINE WOULD NOT RESPOND IN MANUAL MORE. ENGINE SECURED AND A
- [SDR 9JLA2022081233201](https://openairdocs.org/sdr/9JLA2022081233201), Aug 7, 2022: CONTROLLER. FAULTY. THE FLIGHT CREW REPORTED A PRESSURIZATION ISSUE ON TAKEOFF , THE CABIN CLIMBED TO 2000 FT AND THE DESCENDED TO 5000 FT. THEY INDICATED THE PRESSURIZATION FLUCTU
- [SDR 2022FA0000401](https://openairdocs.org/sdr/2022FA0000401), Jul 27, 2022: BRAKE. MISOVERHAULED. HAD THE #3 BRAKE ASSY FAIL DURING TOWING OPERATIONS CAUSING THE BRAKE TO LOCK UP AND SHED PARTS. UPON INSPECTION AFTER REMOVAL AND A SECOND FAILURE IN THE FLEET
- [SDR 2022F00300](https://openairdocs.org/sdr/2022F00300), Jul 27, 2022: BRAKE. BINDING. #2 BRAKE ASSEMBLY LOCKED UP WHEN TOWING AIRCRAFT INTO HANGAR. UPON REMOVAL AND INSPECTION OF BRAKE ASSEMBLY IT WAS FOUND THAT BRAKE PADS HAD SEPARATED FROM THE 
- [SDR 2022F00254](https://openairdocs.org/sdr/2022F00254), Jun 10, 2022: PUMP. FAILED. #2 (RIGHT) HYDRAULIC PUMP FAILURE.
- [SDR 6RNA2022F00135](https://openairdocs.org/sdr/6RNA2022F00135), Mar 8, 2022: FLAP SYSTEM. FAILED. UPON APPROACH TO LAND, FLAPS FAILED TO MOVE FROM ZERO. CREW PERFORMED ZERO FLAP LANDING PROCEDURE AND DECLARED EMERGENCY AS A PRECAUTION.
- [SDR CWQA20220119001](https://openairdocs.org/sdr/CWQA20220119001), Jan 16, 2022: ROD END. OUT OF LIMITS. DURING APPROACH FLAPS FAILED TO DEPLOY. CHECKLIST FOLLOWED, EMERGENCY DECLARED, AND UNEVENTFUL LANDING PERFORMED. MAINTENANCE EVALUATION FOUND CUT-OFF LEVER TO 
- [SDR OZCA25854509JUL21](https://openairdocs.org/sdr/OZCA25854509JUL21), Jul 9, 2021: WINDSHIELD. CRACKED. LEFT WINDSHIELD CRACKED
- [SDR 9JLA2021060230522](https://openairdocs.org/sdr/9JLA2021060230522), May 31, 2021: COMPUTER. FAULTED. THE FLIGHT CREW REPORTED THAT DURING FLIGHT THE ALTITUDE SELECT FAILED, COULD NOT SELECT ALTITUDE. RED ASEL INDICATION WAS ILLUMINATED. THE MAINTENANCE PROVIDER
- [SDR 2021F00053](https://openairdocs.org/sdr/2021F00053), Mar 9, 2021: SLEEVE. DETACHED. SYSTEM TROUBLE SHOT AND FOUND HOSE/SLEEVE UP STREAM OF WATER SEPARATOR DETACHED. ACCESS GAINED BY REMOVING DUCT INSTALLATION AIR CONDITION SYSTEM ASSY PN 25-8VF
- [SDR 9JLA2021020430507](https://openairdocs.org/sdr/9JLA2021020430507), Jan 29, 2021: RELAY. DEFECTIVE. DURING MAINTENANCE GROUND CHECKS THE MAINTENANCE TEAM DISCOVERED THAT THE ELECTRICAL EXTERNAL GROUND POWER WOULD NOT ENERGIZE AIRCRAFT SYSTEMS. TROUBLESHOOTING 
- [SDR 9JLA2021011830500](https://openairdocs.org/sdr/9JLA2021011830500), Jan 5, 2021: ADC. INTERMITTENT. THE FLIGHT CREW REPORTED THAT IN FLIGHT FL280 THE AUTOPILOT STARTED AN UNCOMMANDED CLIMB, 300' WHEN CREW CORRECTED. IN THE DESCENT IN VNAV AS IT WAS LEVELING IN
- [SDR 3WTR20210104](https://openairdocs.org/sdr/3WTR20210104), Jan 4, 2021: WIRE HARNESS. CHAFED. FOUND WIRE BUNDLE CHAFING INTO LOWER OUTBOARD WING SKIN LOCATED BETWEEN RIB 15 AND RIB 16 IN THE AFT BAY. THIS AREA IS DIFFICULT TO INSPECT AND THIS PROBLEM WAS
- [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 MDGA873311072020](https://openairdocs.org/sdr/MDGA873311072020), Nov 7, 2020: LAMP. INOPERATIVE. WHILE LANDING AT KPHL, THE NOSE LANDING LIGHT DID NOT ILLUMINATE AND A GO-AROUND WAS INITIATED. AFTER COMPLETION OF THE QRH, A LOW FLY-BY OVER THE RUNWAY WAS CO
- [SDR 9PMA2020121500538](https://openairdocs.org/sdr/9PMA2020121500538), Jun 8, 2020: LINK. LACK OF LUBE. PILOT REPORTS FUEL TRANSFER HANDLE HARD TO PULL INTO TRANSFER MODE. UPON FURTHER INSPECTION FOUND FUEL TRANSFER LINKAGES IN BELLY WERE HARD TO MOVE DUE TO LACK 
- [SDR MDGA2020030500000](https://openairdocs.org/sdr/MDGA2020030500000), Mar 3, 2020: CDU. MALFUNCTIONED. THE AIRCRAFT SMELLED SMOKE, THE CREW LANDED THE AIRCRAFT IN MCI WITHOUT INCIDENT. MAINTENANCE WAS SENT TO THE AIRCRAFT AND REPORTED THAT THE SMELL CAME FROM THE
- [SDR P6UR2020010298001](https://openairdocs.org/sdr/P6UR2020010298001), Jan 2, 2020: CIRCUIT BREAKER. BURNED. DURING ACCOMPLISHMENT SCREEN HEAT CIRCUIT BREAKERS INSPECTION (F6 INSPECTION) OVERHEATING/MELTING OF THE CIRCUIT BREAKER BODY WAS DETECTED.
- [SDR CDNA20191226002](https://openairdocs.org/sdr/CDNA20191226002), Dec 26, 2019: MIXING VALVE. BENT. PILOTS REPORT "REAR BAY OVERHEAT" ANNUNCIATOR ILLUMINATED DURING CRUISE FLIGHT. DESCENT WAS REQUESTED BUT NOT AUTHORIZED BY ATC, SO AN EMERGENCY WAS DECLARED IN
- [SDR MDGA202012045254](https://openairdocs.org/sdr/MDGA202012045254), Nov 21, 2019: WARNING MESSAGE. FALSE ACTIVATION. ON ROLL OUT THE AIRCRAFT SHOWED THAT THE OIL PRESSURE WAS LOW THE PILOT ABORTED AND RETURNED TO THE RAMP. UPON FURTHER INVESTIGATION THE CREW DETERMINED THAT AF

All 916: https://openairdocs.org/model/hawker-beechcraft-hawker-800xp/reports.md

## STCs that may be installed (OpenAirDocs) (283, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST12360WI](https://openairdocs.org/stc/ST12360WI): Installation of the Gogo Wi-Fi System, AVANCE L3 or AVANCE L5,. Yingling Aviation, Inc
- [STC ST12294SE](https://openairdocs.org/stc/ST12294SE): Installation of Starlink Aviation System. AeroMech Incorporated
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST04570CH](https://openairdocs.org/stc/ST04570CH): Installation of the following systems: Universal lnSight Electronic Flight Instrument System (EFIS), Dual Universal UNS 1FW WAAS FMS, Universal Datacom for CPDLC and FANS 1/A, Universal Kapture CVR with RIPS, Mid Continent Instruments MD 302 electronic standby instrument, Dual Garmin GTX 3000 ADS-B Transponders, Honeywell RDR-2100 weather radar, PS Engineering PAC 45 cockpit audio system. Southeast Aerospace, Incorporated
- [STC ST12344IB](https://openairdocs.org/stc/ST12344IB): Replacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST11216DS](https://openairdocs.org/stc/ST11216DS): Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft. BHE & Associates Ltd
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST02718LA](https://openairdocs.org/stc/ST02718LA): Modification to replace the existing standby instrument. Acron Aviation Inc
- [STC ST03292CH](https://openairdocs.org/stc/ST03292CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development, Inc
- [STC ST12091DE](https://openairdocs.org/stc/ST12091DE): Installation of Nine Passenger or Less Limitation. International Jet Aviation Service Inc
- [STC ST00749WI-D](https://openairdocs.org/stc/ST00749WI-D): Installation of AlliedSignal Digital Flight Data Recorder System. KGB Aviation Solutions LLC
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc
- [STC ST04654CH](https://openairdocs.org/stc/ST04654CH): Installation of Gogo Antennas. StandardAero Business Aviation Services LLC
- [STC ST11169SC](https://openairdocs.org/stc/ST11169SC): Installation of a Rockwell Collins Pro Line 21 update to include optional Terrain Awareness and Warning System (TAWS) mode 5 warning during Localizer Performance with Vertical Guidance (LPV) approaches, optional Automatic Dependent Surveillance Broadcast (ADS-B) Out, optional Synthetic Vision System (SVS), optional 3rd VHF datalink to support Controller Pilot Datalink Communication (CPDLC), optional SATCOM, optional handsets, optional FAA Privacy ICAO address (PIA) program. BHE & Associates LTD
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST01070DE](https://openairdocs.org/stc/ST01070DE): Installation of the Curtiss-Wright Fortress Flight Data Recorder (with Cockpit Voice Recorder). Peregrine
- [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine
- [STC ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine
- [STC ST11285DS](https://openairdocs.org/stc/ST11285DS): An update to the existing Collins Aerospace Integrated Flight Information System (IFIS) FSU-5010 and upgrade the existing XMWR-1000 to a XMWR-1000S (Sirius XM) in Part 25. BHE & Associates Ltd
- [STC ST04281AT](https://openairdocs.org/stc/ST04281AT): Installation for the Upgrade of the NZ-2000 FMS computer for software version NZ6. Chippewa Aerospace Inc
- [STC ST01086DE](https://openairdocs.org/stc/ST01086DE): Installation of the True Blue Power TS60 Lithium-ion Nanophosphate batteries as an alternate to existing Grimes Emergency Exit Lighting (EEL) Power Supply. Peregrine
- [STC ST04470CH](https://openairdocs.org/stc/ST04470CH): Installation of a Honeywell RDR-7000 Weather Radar System. Honeywell International Inc
- [STC ST04536CH](https://openairdocs.org/stc/ST04536CH): 1. Installation of Aviation Clean Air Ionizer System in accordance with Pentastar Aviation Master Data List, Document No. A-18028-210, Revision E, dated September 23, 2021 or later FAA approved revision. 2. The aircraft must be maintained in accordance with the Instructions for Continuted Airworthiness listed in Pentastar Aviation Master Data List, Document No. A-18028-210, Revision E, dated September 23, 2021 or later FAA approved revision is a required part of this modification. Pentastar Aviation LLC
- [STC ST04210NY](https://openairdocs.org/stc/ST04210NY): Installation of LAI Windshield Panel A. Lee Aerospace Inc
- [STC ST10001SC-D](https://openairdocs.org/stc/ST10001SC-D): Installation of the Honeywell Solid State Flight Data Recorder with interface to Collins Proline 21. Duncan Aviation Inc
- [STC ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST10137SC](https://openairdocs.org/stc/ST10137SC): Installation of leather handgrip covers on control yoke. Textron Aviation Inc
- [STC ST04202NY](https://openairdocs.org/stc/ST04202NY): Installation of Lee Aerospace Inc. Window Panel B. Lee Aerospace Inc
- [STC ST03595NY](https://openairdocs.org/stc/ST03595NY): Installation of Honeywell Laseref IV Upgrade. Dassault Aircraft Services (DAS)
- [STC ST01270WI-D](https://openairdocs.org/stc/ST01270WI-D): Installation of Honeywell MK V and MK VII EGPWS Runway Awareness and Advisory System (RAAS). This approval is limited to specifically idenitfied aircraft. Duncan Aviation Inc
- [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC ST00882DE](https://openairdocs.org/stc/ST00882DE): Installation of Becker Avionics BXT6553 transponder. Peregrine
- [STC ST00950DE](https://openairdocs.org/stc/ST00950DE): Installation of Refuel Valve Indicators. West Star Aviation
- [STC ST00934DE](https://openairdocs.org/stc/ST00934DE): Installation of Becker Avionics BXT6553 transponder. Peregrine
- [STC ST01130LA](https://openairdocs.org/stc/ST01130LA): Installation of Prime Mission Equipment Provisions. Approved for restricted category operation only. Lockheed Martin Corporation
- [STC ST01131LA](https://openairdocs.org/stc/ST01131LA): Installation of Prime Mission Equipment Operational Mission Equipment. Approved for serial number 25-8343 only. Approved for restricted category operation only. LOCKHEED MARTIN CORPORATION
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST00835DE](https://openairdocs.org/stc/ST00835DE): Installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and In functionality using the Garmin GTX 335R and GTX 345R Transponders plus qualified position sensor. Peregrine
- [STC ST02627SE](https://openairdocs.org/stc/ST02627SE): Group Reduced Vertical Separation Minimum (RVSM). AeroMech Incorporated
- [STC ST02068CH](https://openairdocs.org/stc/ST02068CH): Install air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC ST04308NY](https://openairdocs.org/stc/ST04308NY): Installation of Satcom with WiFi. 328 Support Services GmbH

All 283: https://openairdocs.org/model/hawker-beechcraft-hawker-800xp/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [NPMA-UN609-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161711503220261023152347.0001): Sleeve. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UN609 · Oct 7, 2026
- [S9413-008WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187096582920261009134009.0001): Packing, Preform - Fluorocarbon. Wencor, LLC · PMA PQ1370NM · Replaces S9413-008 · Oct 1, 2026
- [06655200-510](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194002194720260910160117.0001): STARLINK AVIATION BLOCK 4 ANTENNA DATA LIST, PN 06655200-510. Space Exploration Technologies · PMA PQ00001WB · Modification part · Jul 22, 2026
- [06652310-531](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188307572820260910160119.0001): COVER PLATE ASSEMBLY, STARLINK AVIATION. Space Exploration Technologies · PMA PQ00001WB · Modification part · Jul 22, 2026
- [06652360-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172071713320260910160119.0001): SPRAY SHIELD ASSEMBLY, XS, STARLINK AVIATION. Space Exploration Technologies · PMA PQ00001WB · Modification part · Jul 22, 2026
- [06655300-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171218446820260910160118.0001): STARLINK AVIATION BLOCK 5 ANTENNA DATA LIST, PN 06655300-501. Space Exploration Technologies · PMA PQ00001WB · Modification part · Jul 22, 2026
- [06652350-556](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160866118420260910160118.0001): AVIATION TRAY ASSEMBLY, XXL LUGS, WIDE STANCE. Space Exploration Technologies · PMA PQ00001WB · Modification part · Jul 22, 2026
- [06658430-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151175068420260910160118.0001): MASTER DATA LIST – 06658430-501 – BLOCK 4 ROUTER – STARLINK AVIATION. Space Exploration Technologies · PMA PQ00001WB · Modification part · Jul 22, 2026
- [06652147-511](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149188950320260910160117.0001): STARLINK AVIATION HEAVY TRAY ASSEMBLY – DRAWING LIST, PN 06652147-511. Space Exploration Technologies · PMA PQ00001WB · Modification part · Jul 22, 2026
- [06651101-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144438279620260910160117.0001): STARLINK AVIATION AEROSHELL ASSEMBLY– DRAWING LIST, PN 06651101-501. Space Exploration Technologies · PMA PQ00001WB · Modification part · Jul 22, 2026
- [06652360-571](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125727911920260910160119.0001): PAGODA ASSEMBLY, STARLINK AVIATION. Space Exploration Technologies · PMA PQ00001WB · Modification part · Jul 22, 2026
- [06658400-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108374520920260910160118.0001): MASTER DATA LIST–06658400-501 – BLOCK 4 PSU – STARLINK AVIATION. Space Exploration Technologies · PMA PQ00001WB · Modification part · Jul 22, 2026
- [NP-UM1213-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123748027320260826222138.0001): Seal Housing. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-UM1213 · Jun 23, 2026
- [NPMA-8UM101-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110447470620260522104204.0001): Plug. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-8UM101-1 · May 21, 2026
- [NPMA-8UM93-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173912587120260522104239.0001): Swivel Plate. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UM1151 · Apr 23, 2026
- [NPMA-8UM93-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155157410320260522104239.0001): Swivel Plate. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-8UM93-1 · Apr 23, 2026
- [NPMA-8UN257-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163208700820260522104258.0001): Barrel Assembly. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-UN-385A/B · Apr 20, 2026
- [NPMA-8UN257-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161302303420260522104258.0001): Barrel Assembly. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-8UN257-27A · Apr 20, 2026
- [NPMA-8UN257-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109826392820260522104259.0001): Barrel Assembly. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-8UN257-1A · Apr 20, 2026
- [NP-UN213-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193128948820260522104312.0001): Pivot Pin Assembly. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-UN213A · Apr 16, 2026
- [NP-UN213-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128422954820260522104312.0001): Pin. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UN213-1 · Apr 16, 2026
- [NP-UN211-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107246616020260522104312.0001): Plug. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UN211 · Apr 16, 2026
- [NPMA-UM183-7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144276443320260522104327.0001): Adaptor. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UM183/3 · Apr 7, 2026
- [NPMA-UM183-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130339736020260522104326.0001): Adaptor. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UM183/1 · Apr 7, 2026
- [NPMA-UM1333-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193772478020260324201130.0001): Jack Pivot. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UM1231 · Dec 2, 2025
- [NP-UN561-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171393766620260324203934.0001): Axle. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UN561 · Dec 2, 2025
- [NP-UN561-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165575874820260324203934.0001): Axle. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UN561-9 · Dec 2, 2025
- [NPMA-UM1333-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164299893020260324201130.0001): Jack Pivot. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-UM1333-1 · Dec 2, 2025
- [NPMA-UM1333-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118866791120260324201130.0001): Jack Pivot. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-8UM89-1 · Dec 2, 2025
- [NP-UN561-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111192153120260324203935.0001): Axle. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UN561-11 · Dec 2, 2025
- [NPMA-UM1333-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106328163720260324201131.0001): Jack Pivot. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-UM1333-3 · Dec 2, 2025
- [858885-3WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159160685320260107202053.0001): Diaphragm-Air. Wencor, LLC · PMA PQ1370NM · Replaces 858885-3 · Oct 30, 2025
- [NPMA-UN653-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158577569820260324203947.0001): Pin (Jack to Bridge). AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-UN653 · Oct 20, 2025
- [RFS90011727](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181148137320250807134526.0001): Spring. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 90011727 · Aug 5, 2025
- [207218HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166816467420250807185055.0001): Thrust Washer. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 207218 · Aug 4, 2025
- [207460HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145152614120250805133123.0001): Bearing, Ball Annular. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 207460 · Aug 4, 2025
- [NPMA-UM123-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124564489620260324201029.0001): Bolt. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UM123 · Jun 24, 2025
- [NP-UN649-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136553741320250610210940.0001): Plunger Tube. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UN-649 · May 28, 2025
- [P-1119](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194612143820250602133045.0001): Seal Assy. Donaldson Company Inc · PMA PQ2432CE · Replaces 3830159-1 · May 23, 2025
- [PM-380](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195920097420251118174940.0001): Dorsal Fin Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025
- [PM-381](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195829944420251118174940.0001): Elevator Tip Mask Set. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025
- [PM-86](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193650109720251118174939.0001): Generator Inlet Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025
- [PM-88](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187052129220251118174939.0001): Vertical Stabilizer Tip Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025
- [PM-382](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183127931920251118174940.0001): Wing Root Fairing Mask Set. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025
- [PM-8104](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161635627820251118174941.0001): Outboard Flaptrack Fairing Forward Mask Set. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025
- [PM-82](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161043720620251118174938.0001): Navigation Light Lens Mask Set. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025
- [PM-8102](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155172920720251118174941.0001): Inboard Flaptrack Fairing Forward Mask Set. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025
- [PM-89](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154959062420251118174939.0001): Keel Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025
- [PM-84](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149726125020251118174939.0001): Air Intake Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025
- [PM-8106](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143198762020251118174942.0001): Inboard Wing Blister Panel Mask Set. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025

All of them: https://openairdocs.org/model/hawker-beechcraft-hawker-800xp/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Raytheon HAWKER 800XP](https://openairdocs.org/model/raytheon-hawker-800xp): 251 registered aircraft, registry code 7150012
- [Raytheon Corporate Jets HAWKER 800XP](https://openairdocs.org/model/raytheon-corporate-jets-hawker-800xp): 23 registered aircraft, registry code 7450006

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