# Raytheon HAWKER 800 - Type: Aircraft model (FAA registry) - Registry code: 7150011 - Manufacturer (registry): RAYTHEON AIRCRAFT COMPANY - Model: HAWKER 800 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 17 - Weight class: 12,500 to 19,999 lb - Certification: Type certificated - Data sheet: [TCDS A3EU](https://openairdocs.org/tcds/A3EU) (OpenAirDocs) - Holder: Textron Aviation Inc. - Registered aircraft: 0 - Page: https://openairdocs.org/model/raytheon-hawker-800 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 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 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) (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 None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (83, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR Y9PA2025060900392](https://openairdocs.org/sdr/Y9PA2025060900392), Jun 9, 2025: BRAKE ASSY. SEIZED. RIGHT MAIN TIRE LOST PRESSURE AFTER TAXI IN AT HOBBY. NOTICED THAT DURING TAXI IN AFTER LANDING ON LEG 1 OF 4 THAT BRAKES SEEMED TO ENGAGE WITHOUT PEDDLES BEING - [SDR 2023FA0000594](https://openairdocs.org/sdr/2023FA0000594), Oct 11, 2023: CONTROLLER. FAILED. CABIN TEMPERATURE CONTROL SYSTEM FAILED IN FULL HOT CAUSING CABIN TEMP TO CLIMB AND EVENTUALLY CAUSED SMOKE IN THE CABIN. - [SDR MY5A202308030729](https://openairdocs.org/sdr/MY5A202308030729), Jul 29, 2023: SWITCH. FAILED. ENGINE #2 FUEL LIGHT ILLUMINATED AFTER 25 MINUTES OF FLIGHT AT FL320. FOLLOWED CHECKIST PROCEDURE. REDUCED POWER TO IDLE AND LIGHT WENT OUT. DIVERTED TO DEPARTU - [SDR 2022F00273](https://openairdocs.org/sdr/2022F00273), Jun 23, 2022: NONE. NONE. #1 (LEFT) MAIN BOOST PUMP FAILED - [SDR 2021F00032](https://openairdocs.org/sdr/2021F00032), Feb 13, 2021: OIL SYSTEM. FLUCTUATES. AFTER DEPARTURE FROM KJVL DURING CLIMB OUT THE CREW NOTICED THE RH ENGINE OIL PRESSURE FLUCTUATING. THE CREW FOLLOWED CHECKLIST PROCEDURES AND SHUT THE ENGINE D - [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 - [SDR G73R201808225587](https://openairdocs.org/sdr/G73R201808225587), Aug 19, 2018: CABIN PRESSURE. MALFUNCTIONED. DURING CRUISE AT FL360, WITH CABIN CONTROLLER SET TO FL380 AND NORMAL PRESSURIZATION. AT TOP OF DESCENT REDUCED POWER SLIGHTLY AND AT THE SAME TIME THE CABIN RA - [SDR G73R20180515445](https://openairdocs.org/sdr/G73R20180515445), May 3, 2018: BUSHING. WORN. DURING ARRIVAL, AFTER LEVELLING OFF AT 10,000 FT AN ABNORMAL VIBRATION WAS NOTICED. MOVING EACH THRUST LEVER INDEPENDENTLY INDICATED THAT THE VIBRATION WAS ASSO - [SDR C40A201803050001](https://openairdocs.org/sdr/C40A201803050001), Mar 2, 2018: HINGE BRACKET. CRACKED. DURING CLIMB, THE LEFT GEAR UNSAFE, IN TRANSIT INDICATION ILLUMINATED WITH NOTICEABLE DECREASE IN PERFORMANCE. DIVERTED WITH UNEVENTFUL FULL STOP LANDING. VISUA - [SDR 2018F00097](https://openairdocs.org/sdr/2018F00097), Feb 8, 2018: STARTER GEN. FAILED. ENROUTE, ABOUT 3 HOURS INTO FLIGHT, HAD A SMALL VIBRATION THAT LASTED TWO SECONDS AND WENT AWAY. AT FL360 M.72 KEPT GETTING SMALL VIBRATIONS, ENGINE INDICATIONS - [SDR C40A20171206001](https://openairdocs.org/sdr/C40A20171206001), Nov 22, 2017: SWITCH. FALSE ACTIVATION. TAKEOFF ROLL AT 50-60KTS, AIRBRAKES OPEN WARNING ILLUMINATED WITH ASSOCIATED WARNING HORN. PILOTS EXECUTED TAKEOFF ABORT AND SAFELY RETURNED TO RAMP AT ATLANTIC - [SDR ZP7A2017080200001](https://openairdocs.org/sdr/ZP7A2017080200001), Aug 1, 2017: CABIN PRESSURE. MALFUNCTIONED. CLIMBING THROUGH APPROXIMATELY 17,500 MSL A POPPING SOUND WAS HEARD, THEN THE CABIN ALTITUDE BEGAN TO CLIMB APPROXIMATELY 2000FT PER MINUTE. PROCEDURES IN THE Q - [SDR G73R2016080400001](https://openairdocs.org/sdr/G73R2016080400001), Jul 22, 2016: CONTROLLER. INOPERATIVE. RIGHT WINDSCREEN GOES INTO OVERHEAT. - [SDR G73R2016060300001](https://openairdocs.org/sdr/G73R2016060300001), May 26, 2016: THERMAL SWITCH. DEFECTIVE. APU FIRE BELL AND LIGHT SOUNDED AND ILLUMINATED DURING AIRCRAFT ROLL OUT ON LANDING WITH APU OFF. - [SDR C40A20150924001](https://openairdocs.org/sdr/C40A20150924001), Sep 18, 2015: PLUNGER. OBSTRUCTED. CRUISE AT FL360, ACFT EXPERIENCED A REAR BAY DOOR MWS INDICATION IMMEDIATELY FOLLOWED BY CABIN ALTITUDE. CREW & PAXS DONNED 02 MASKS. CREW DESCENDED TO SAFE ALT - [SDR 9JLA201506247566](https://openairdocs.org/sdr/9JLA201506247566), May 12, 2015: CONTROLLER. DEFECTIVE. CREW REPORTED THAT DURING FLIGHT THE RT ENG DEEC LIGHT CAME ON AT 86% N1. THE CREW INDICATED THAT THE ENG DIVERTED TO MANUAL MODE. TROUBLE SHOT THE DISCREPANCY - [SDR 9JLA201504227550](https://openairdocs.org/sdr/9JLA201504227550), Apr 8, 2015: JACK. CONTAMINATED. DURING FLIGHT, FL 330 & 300, THE LT & RT AUTO PILOT SYS DISENGAGED. ABLE TO REENGAGE THE SYS FOR ONLY 2 MIN BEFORE THE SYS DISENGAGED AGAIN. THE SYS WAS TROUBLE - [SDR 9JLA201504227561](https://openairdocs.org/sdr/9JLA201504227561), Mar 28, 2015: POSITION SWITCH. SHORTED. DURING FLIGHT THE AIRBRAKE, OPEN, INDICATION ANNUNCIATION REMAINED ILLUMINATED WITH AIRBRAKES IN THE SHUT POSITION. THE POSITION INDICATOR CB WAS TRIPPED. TROUB - [SDR 9JLA201504227560](https://openairdocs.org/sdr/9JLA201504227560), Mar 23, 2015: SKIN PANEL. CRACKED. DURING THE POST-FLIGHT INSPECTION THAT THE RT UPPER AIRBRAKE HAD A 4 INCH CRACK ON THE TOP SKIN ALONG THE TE. NO CAUSE FOR THE CRACK WAS FOUND. REMOVED THE DAMA - [SDR BWVR201503200002](https://openairdocs.org/sdr/BWVR201503200002), Mar 19, 2015: CLAMP. DISENGAGED. DURING ROUTINE MX, ONE OF OUR TECHNICIANS WAS TASKED TO TAKE A SOAP SAMPLE FROM THE ACFT APU. WHILE TAKING THE SAMPLE HE NOTICED THE APU STARTER GEN WAS LOOSE. - [SDR 9JLA2014101307187](https://openairdocs.org/sdr/9JLA2014101307187), Sep 18, 2014: DIODE. DEFECTIVE. THE MULTIFUNCTION DISPLAY WENT BLANK. TROUBLESHOOTING FOUND THAT THE SG WAS INOPERATIVE. FURTHER TROUBLESHOOTING FOUND DIODES CR79 & CR80 DEFECTIVE. IT’S UNCLEA - [SDR 9JLA2014040907167](https://openairdocs.org/sdr/9JLA2014040907167), Apr 2, 2014: INVERTER. FAILED. CREW REPORTED THAT THE NR 1 INVERTER FAILED IN FLIGHT. THE FAILED INVERTER WAS REMOVED PN 140-380010-7, SN SG1347 & A REPAIRED INVERTER WAS INSTALLED. - [SDR 9JLA2014042107165](https://openairdocs.org/sdr/9JLA2014042107165), Mar 30, 2014: WINDSHIELD. DEFECTIVE. THE FLIGHT CREW REPORTED THAT THE RIGHT B SCREEN WOULD NOT HEAT IN FLIGHT. TROUBLESHOOTING DISCOVERED THE RT B PANEL WINDSCREEN DEFECTIVE. THE DEFECTIVE WINDSCR - [SDR 9JLA2014030406397](https://openairdocs.org/sdr/9JLA2014030406397), Feb 27, 2014: WINDOW. FAILED. THE PILOT, SIC, REPORTED THAT WHILE CLIMBING OUT OF FL320 TO FL360, HE HEARD A LOUD BANG. THE SIC STATED THAT HE LOOKED OVER HIS SHOULDER TO THE CABIN & THE PAX - [SDR VPQA2014FA0000083](https://openairdocs.org/sdr/VPQA2014FA0000083), Feb 13, 2014: THROTTLE SWITCH. WEAK. NR 2 T/R FAILED TO DEPLOY UPON LANDING. FOUND NR 2 T/R PIGGY BACK POSITION SWITCH, PN 25-8CX213-1A, HARNESS WIRES BROKEN AT ADEL SECURING POINT DEEP WITHIN THE - [SDR 9JLA2014011507160](https://openairdocs.org/sdr/9JLA2014011507160), Dec 26, 2013: ADC. DEFECTIVE. THE FLIGHT CREW REPORTED THAT THE NR 2 ADC INDICATED AN INTERMITTENT OVER SPEED WARNING INFLIGHT & ON THE GND. TROUBLESHOOTING OF THE NR 2 FOUND IT TO BE DEFECT - [SDR 9JLA2013110406378](https://openairdocs.org/sdr/9JLA2013110406378), Oct 12, 2013: PUMP. FAILED. FLIGHT CREW REPORTED THAT THE RT ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON IN FLIGHT. TROUBLESHOT AND IDENTIFIED THE RT ENGINE DRIVEN HYDRAULIC PU - [SDR 9JLA2013110406377](https://openairdocs.org/sdr/9JLA2013110406377), Oct 7, 2013: GCU. DEFECTIVE. DURING THE TAKEOFF ROLL, CREW REPORTED THAT THE NR 1 DC GENERATION SYS FAILED PRIOR 80 KNOTS AND THE TAKEOFF WAS ABORTED. TROUBLESHOOTING IDENTIFIED THE NR 1 GE - [SDR 9JLA2013072206365](https://openairdocs.org/sdr/9JLA2013072206365), Jul 9, 2013: FIRE LOOP. DEFECTIVE. THE FLIGHT CREW REPORTED THAT DURING THE PREFLIGHT INSPECTION THE NR 2 ENGINE FIRE DETECTION SYSTEM FAILED TO TEST. TROUBLESHOOTING DETERMINED THAT THE ZONE 2 F - [SDR 2013FA0000371](https://openairdocs.org/sdr/2013FA0000371), May 11, 2013: TIRE. DAMAGED. INSTALLED REPAIRED WHEEL ASSY WITH NEW TIRE, AFTER ONE LANDING, ACFT PULLED TO RT DURING TAXI. NOSE WHEEL STEERING OPS CHECKED GOOD, SWAPPED NOSE WHEELS ACFT PU - [SDR 9JLA2013042405688](https://openairdocs.org/sdr/9JLA2013042405688), Apr 8, 2013: FAN. DEFECTIVE. CREW REPORTS THE CABIN RECIRCULATING FAN WAS DEFECTIVE. REMOVED THE DEFECTIVE CABIN FAN PN 0901-2, SN 0696. INSTALLED AN O/H UNIT. THIS IS THE THIRD FAN ASSY RE - [SDR 9JLA2013011803545](https://openairdocs.org/sdr/9JLA2013011803545), Dec 13, 2012: INDICATOR. DEFECTIVE. DURING THE POST FLIGHT INSPECTION, THE NR 1 ENGINE OIL FILTER BYPASS INDICATOR WAS NOTED IN THE BYPASS POSITION. A SOAP WAS TAKEN AND RESULTS WERE NORMAL. THE B - [SDR 9JLA2012110706339](https://openairdocs.org/sdr/9JLA2012110706339), Oct 31, 2012: CONTROLLER. DEFECTIVE. THE CREW REPORTED THAT THE RT WINDSCREEN WOULD OVERHEAT WITH THE LT AND RT WINDSHIELD HEATS ON. TROUBLESHOOTING IDENTIFIED THE RT TEMP CONTROL UNIT AS DEFECTIVE - [SDR UVVR2012101700025](https://openairdocs.org/sdr/UVVR2012101700025), Oct 17, 2012: SCISSOR LINK. BENT. THE RT MLG UPPER SCISSOR LINK WAS FOUND BENT CLOSE TO THE CENTER PIVOT AREA DURING A PHASE INSPECTION. NO COMPLAINTS FROM THE PILOTS OR OPERATOR THAT THE ACFT H - [SDR 9JLA2012040905660](https://openairdocs.org/sdr/9JLA2012040905660), Apr 3, 2012: INVERTER. FAILED. CREW REPORT THE NR 2 INVERTER FAILED. FOUND INVERTER TO BE DEFECTIVE. - [SDR 9JLA2012032806316](https://openairdocs.org/sdr/9JLA2012032806316), Mar 28, 2012: PUMP. FAILED. THE CREW REPORTED THAT THE RT WING FUEL BOOST PUMP FAILED. THE FAILED FUEL BOOST PUMP WAS INSTALLED 8 MONTHS PRIOR AND LASTED ONLY 283.5 HRS AND WAS O/H. - [SDR 9JLA2012032324205](https://openairdocs.org/sdr/9JLA2012032324205), Mar 23, 2012: INVERTER. FAILED. CREW REPORTED THAT THE NR 1 MAIN INVERTER FAILED. FOUND UNIT TO BE DEFECTIVE. PN 501-1235-01, SN 1170 - [SDR 9JLA2011122806314](https://openairdocs.org/sdr/9JLA2011122806314), Dec 26, 2011: PUMP. DEFECTIVE. THE CREW REPORTED THAT THE "HYD 2 LO PRESS" ANNUNCIATOR ILLUMINATED DURING LANDING. TROUBLESHOOTING IDENTIFIED THE NR 2 ENGINE HYD PUMP AS DEFECTIVE. THE PUMP W - [SDR 9JLA2011120706313](https://openairdocs.org/sdr/9JLA2011120706313), Dec 4, 2011: PRESSURE SWITCH. DEFECTIVE. THE CREW REPORTED THE HYDRAULIC PRESSURE NR 2 LOW PRESSURE ANNUNCIATOR ILLUMINATED. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE HYDRAULIC LOW PRESSURE SWITCH D - [SDR 9JLA20110829001](https://openairdocs.org/sdr/9JLA20110829001), Aug 29, 2011: PUMP. LOW PRESSURE. THE CREW HAS BEEN REPORTING DURING APU START THAT IT WOULD HANG AT ABOUT 45% FOR ABOUT 5-6 SECONDS AND THEN LET OUT A LOUD "POP" AND THEN CONTINUE ONTO START AN - [SDR 9JLA20110801001](https://openairdocs.org/sdr/9JLA20110801001), Aug 1, 2011: PUMP. DEFECTIVE. THE CREW REPORTED DURING CLIMBOUT THAT THE ENG 2 FUEL ANNUNCIATOR ILLUMINATED. THE FUEL FILTER HAD BEEN REPLACED 2 DAYS PRIOR WITH SATISFACTORY OPERATIONAL CHEC - [SDR CA110614011](https://openairdocs.org/sdr/CA110614011), Jun 13, 2011: TURBINE BLADES. DAMAGED. (CAN) ON CLIMB-OUT THROUGH 25,000 FT A LARGE BANG WAS HEARD AND MODERATE VIBRATION FELT THROUGH THE REAR OF THE ACFT FOLLOWED BY AN EXHAUST ODOR. AIRCRAFT LEVEL - [SDR 9JLA2650](https://openairdocs.org/sdr/9JLA2650), May 1, 2011: SWITCH. INTERMITTENT. CREW REPORTED THAT THE AIRBRAKE INDICATOR WAS INOP. REQUIRED SYSTEM TO BE DEFERRED. TROUBLESHOT SYSTEM AND FOUND THE LT AIRBRAKE SWITCH TO BE INTERMITTENT. REMO - [SDR 9JLA03503](https://openairdocs.org/sdr/9JLA03503), Apr 25, 2011: PRESSURE SWITCH. DEFECTIVE. THE FLIGHT CREW REPORTED THE "HYD 1 LO PRESS" ILLUMINATED AFTER THE FINAL FLAP SETTING AND REMAINED ON. TROUBLESHOOTING FOUND THE NR 1 HYD PRESSURE SWITCH P/N 1 - [SDR V0JA041176H](https://openairdocs.org/sdr/V0JA041176H), Apr 19, 2011: OIL SYSTEM. LOW PRESSURE. DURING TAXI TO RUNWAY THE CREW WAS ALERTED TO LOW OIL PRESSURE IN THE NR 1 ENGINE BY THE MWS ANNUNCIATORS. THE LOW OIL PRESSURE WAS VERIFIED BY THE NR 1 ENGINE - [SDR 2011F00036](https://openairdocs.org/sdr/2011F00036), Mar 23, 2011: STARTER GEN. FAILED. ACFT EXPERIENCED MODERATE VIBRATION IN CRUISE, FLIGHT CREW FELT VIBRATION WAS FROM NR 2 ENGINE, FOLLOWED SHORTLY AFTER WITH GEN 2 FAIL INDICATION, CREW SHUTDOWN - [SDR 2011F00040](https://openairdocs.org/sdr/2011F00040), Jan 28, 2011: COOLING TURBINE. DEFECTIVE. CREW REPORTED NOISE IN THE AIR CONDITIONING SYS, TROUBLESHOOTING FOUND THE COOLING TURBINE ASSY TO HAVE A BAD VIBRATION WHILE OPERATING. REMOVED THE DEFECTIVE C - [SDR 9JLA20110107001](https://openairdocs.org/sdr/9JLA20110107001), Jan 7, 2011: POSITION SWITCH. SHORTED. THE FLIGHT CREW DISCOVERED DURING THE PREFLIGHT CHECKS A SSU/FLAP FAULT INDICATION. MX TROUBLESHOT THE FAULT AND FOUND BOTH THE RT INBD/OTBD FLAP POSITION FLAP - [SDR 2010F00226](https://openairdocs.org/sdr/2010F00226), Aug 7, 2010: ANNUNCIATOR. ACTIVATED. CREW REPORTED THE "ENG 2 FUEL" ANNUNCIATOR ILLUMINATED DURING FLIGHT. - [SDR BKEA201008011](https://openairdocs.org/sdr/BKEA201008011), Aug 1, 2010: VALVE. OPEN. DURING REPOSITION FLIGHT WITH NO PASSENGERS ON ACFT, AFTER TAKEOFF. DURING CLIMB OUT, ACFT EXPERIENCED IN FLIGHT SMOKE IN CABIN. ACFT RETUREND TO DEPARTURE, HAV All 83: https://openairdocs.org/model/raytheon-hawker-800/reports.md ## STCs that may be installed (OpenAirDocs) (179, 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 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 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 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 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 ST04654CH](https://openairdocs.org/stc/ST04654CH): Installation of Gogo Antennas. StandardAero Business Aviation Services LLC - [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 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 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 ST04210NY](https://openairdocs.org/stc/ST04210NY): Installation of LAI Windshield Panel A. Lee Aerospace Inc - [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 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 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 SA3656SW](https://openairdocs.org/stc/SA3656SW): Installation of TR5000BA Thrust Reverser. The NORDAM Group LLC - [STC ST02068CH](https://openairdocs.org/stc/ST02068CH): Install air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed - [STC ST00790DE](https://openairdocs.org/stc/ST00790DE): Installation of BendixKing CAS 67B Traffic Alert and Collision Avoidance System (TCAS) II Version 7.1. Peregrine - [STC ST00813DE](https://openairdocs.org/stc/ST00813DE): Replacement of Honeywell (formerly Sperry) ED-800 cathode ray tube (CRT) display, part number 7003110-90 I or 7003110-902, with Esterline CMC Electronics CMA-6800 multi-purpose liquid crystal display (LCD),. Peregrine - [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC - [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC - [STC ST02499AK](https://openairdocs.org/stc/ST02499AK): Approval of the Thomas Global Systems TFD8601Active Matrix Liquid Crystal Display installed. ADS-B Technologies, LLC - [STC ST03139CH](https://openairdocs.org/stc/ST03139CH): Installation of Aircell Axxess II Iridium Satcom and High Speed Internet with Wireless Local Area Network (WLAN (IEEE 802.11 b, g, and n only)). Nextant Aerospace - [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc - [STC ST00304WI](https://openairdocs.org/stc/ST00304WI): Installation of Keddeg Company 21BC113 coaleser assembly. Purolator Facet, Inc - [STC ST01228WI](https://openairdocs.org/stc/ST01228WI): Replacement of OEM window pane assemblies with Lee Aerospace laminated window assembly and termination of OEM dry air system. Lee Aerospace, Inc - [STC SA4710SW](https://openairdocs.org/stc/SA4710SW): Installation of solar auxiliary power unit (APU) Model T62T-40C or T62T-40C8D1. Textron Aviation Inc - [STC SA5921SW](https://openairdocs.org/stc/SA5921SW): Installation of Dual Refuel/Defuel Panel. Textron Aviation Inc - [STC ST09041SC](https://openairdocs.org/stc/ST09041SC): Installation of Sundstrand Mark VII ground proximity warning system. Textron Aviation Inc - [STC ST09119SC](https://openairdocs.org/stc/ST09119SC): Installation of Honeywell FMZ-2000 Flight Management System with optional dual Honeywell OZ-800 Omega/VLF Sensors or optional Single Canadian Marconi CMA-764 Omega Navigation Sensor. Textron Aviation Inc - [STC ST09412SC](https://openairdocs.org/stc/ST09412SC): Installation of nose taxi light switching modification. Textron Aviation Inc - [STC ST09480SC](https://openairdocs.org/stc/ST09480SC): Installation of Universal CVR-30B cockpit voice recorder. Textron Aviation Inc - [STC ST02632LA](https://openairdocs.org/stc/ST02632LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out and optionally install ACSS NXG-900 GPS as a position source for ADS-B Out. Aviation Communications and Surveillance Systems All 179: https://openairdocs.org/model/raytheon-hawker-800/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 - [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 - [MK25700-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190042954320260325180456.0001): O-Ring. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces K25700-5 · Dec 9, 2025 - [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 - [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 - [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 - [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 - [400-21149G-3-305, 400-21149G-3-315, 400-21149G-3-405, 400-21149G-3-415, 400-21149G-3-505, 400-21149G-3-515, 400-21149G-3-605, 400-21149G-3-615, 400-21149G-3-915](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195387574620250603134043.0001): Assy, LRU Adapter (avRDC or MAX). Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025 - [804-1250-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192207126420250612143631.0001): avRDC QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025 - [804-1250-32](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168158510420250612143635.0001): avRDC MAX QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025 - [650-0100-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163107069620250603134032.0001): Cellular Module, avCM LTE. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025 - [802-0100-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159877857720250603134035.0001): Kit, avCM 4G Adapter. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025 - [400-21149G-3-101, 400-21149G-3-103, 400-21149G-3-105, 400-21149G-3-111, 400-21149G-3-113, 400-21149G-3-115, 400-21149G-3-205, 400-21149G-3-215, 400-21149G-3-715, 400-21149G-3-815](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148779431820250603134039.0001): Assy, LRU Adapter (miniQAR MKIII). Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025 - [21149GK-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145331540120250612143627.0001): Installation Kit, miniQAR / avRDC QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025 - [804-1201, 804-1205, 804-1205-03, 804-1212, 804-1216](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138145552920250612143623.0001): miniQAR MKIII. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025 - [650-0100-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132354161620250603134028.0001): Cellular Module (avCM 4G), GSM / GRPS 4G, Quad Band, SMA. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025 - [NPMA-6UM43-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170806127120250604135630.0001): Flanged Distance Piece. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-6UM43 · Apr 14, 2025 - [NPMA-UM391-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133599450020250604135629.0001): Roller. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UM391 · Apr 14, 2025 - [NPMA-6UM47-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109677854020250604135630.0001): Distance Piece. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25-6UM47 · Apr 14, 2025 - [NPMA-810396-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125209806120250604135619.0001): Bolt - Axle Barrel. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 140-810396-0001 · Mar 20, 2025 - [NPMA-FC6933-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174964364720250604173228.0001): L.A. Tube. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25FC6933-1 · Mar 13, 2025 All of them: https://openairdocs.org/model/raytheon-hawker-800/pma.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Raytheon Corporate Jets HAWKER 800](https://openairdocs.org/model/raytheon-corporate-jets-hawker-800): 9 registered aircraft, registry code 7450004 - [Hawker Beechcraft HAWKER 800](https://openairdocs.org/model/hawker-beechcraft-hawker-800): 0 registered aircraft, registry code 422000A --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.