# Raytheon HAWKER 1000 - Type: Aircraft model (FAA registry) - Registry code: 1500290 - Manufacturer (registry): RAYTHEON AIRCRAFT COMPANY - Model: HAWKER 1000 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-jet - Seats: 13 - 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: 1 - Page: https://openairdocs.org/model/raytheon-hawker-1000 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 2016-13-13](https://openairdocs.org/ad/2016-13-13): Engine Exhaust · Textron BAe.125 Series 1000A, BAe.125 Series 1000B and Hawker 1000. Effective Aug 12, 2016 - [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 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 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 94-09-11 R1](https://openairdocs.org/ad/94-09-11-R1): Thrust Reverser System · BAe.125 Series 1000A and Hawker 1000. Effective Sep 3, 2002 - [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 2000-22-03](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 2000-02-35](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 2000-01-02](https://openairdocs.org/ad/2000-01-02): Turbine Air Discharge Duct in the Air Conditioning System · Textron BAe.125 Series 1000A, BAe.125 Series 1000B and Hawker 1000. Effective Feb 15, 2000 - [AD 99-25-01](https://openairdocs.org/ad/99-25-01): P1 Pitot Pipes · Textron BAe.125 Series 1000A, BAe.125 Series 1000B and Hawker 1000. Effective Jan 4, 2000 - [AD 99-23-10](https://openairdocs.org/ad/99-23-10): PS Wire Bundle · Textron Hawker 1000. Effective Dec 17, 1999 - [AD 97-26-10](https://openairdocs.org/ad/97-26-10): Aft Core Cowl Nozzles Of Engine Nacelles · Textron Hawker 1000. Effective Jan 23, 1998 - [AD 97-09-05](https://openairdocs.org/ad/97-09-05): Venting Of Cabin Pressure · Textron BAe.125 Series 1000A and Hawker 1000. Effective May 30, 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 96-22-03](https://openairdocs.org/ad/96-22-03): Thrust Reverser · Textron BAe.125 Series 1000A and Hawker 1000. Effective Dec 11, 1996 - [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 96-17-13](https://openairdocs.org/ad/96-17-13): Elevator Pulley Assembly · Textron BAe.125 Series 1000A and Hawker 1000. Effective Sep 30, 1996 - [AD 96-17-09](https://openairdocs.org/ad/96-17-09): Fuel Hose Assembly on Auxiliary Power Unit (APU) · Textron BAe.125 Series 1000A and Hawker 1000. Effective Sep 24, 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 96-11-17](https://openairdocs.org/ad/96-11-17): Flap, Turnbuckle, Airbrakes, And Flight Control Cables · Textron BAe.125 Series 1000A and Hawker 1000. Effective Jul 9, 1996 - [AD 96-07-11](https://openairdocs.org/ad/96-07-11): Hydraulic Pipes Inspection · Textron BAe.125 Series 1000A and Hawker 1000. Effective May 6, 1996 - [AD 95-21-17](https://openairdocs.org/ad/95-21-17): Electrical Cable Loom · Textron BAe.125 Series 1000A and Hawker 1000. Effective Nov 17, 1995 - [AD 94-24-08](https://openairdocs.org/ad/94-24-08): Install Modification 253627A & 253661B · Textron BAe.125 Series 1000A and Hawker 1000. Effective Jan 4, 1995 - [AD 94-15-15](https://openairdocs.org/ad/94-15-15): Electrical And Hydraulic Cables, Pipes, And Looms · Textron BAe.125 Series 1000A and Hawker 1000. Effective Aug 15, 1994 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 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 - [AD 94-09-11](https://openairdocs.org/ad/94-09-11) (historical): Thrust Reverser System · Hawker Beechcraft BAe.125 Series 1000A and Hawker 1000. Effective May 16, 1994 ## Information bulletins (advisory) (5) - [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 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) - [N261PA](https://openairdocs.org/aircraft/N261PA): [Calla Airways LLC](https://openairdocs.org/faa-owner/CALLA%20AIRWAYS%20LLC), [Cohasset, MA](https://openairdocs.org/faa-place/MA/Cohasset), built 1998, S/N 259003 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20220805014149I](https://openairdocs.org/incident/20220805014149I), Aug 5, 2022: Raytheon HAWKER 1000 (N261PA), Plymouth, MA, Minor damage. After landing and decelerating to less than 80 knots a deer suddenly appeared in the pilots field of view from the left. The deer crossed left to right in… ## Service difficulty reports (63, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR ZKFA20240701058](https://openairdocs.org/sdr/ZKFA20240701058), Jul 2, 2024: FILTER HOUSING. PULLED. DURING A MAINTENANCE GROUND RUN, THE RT ENGINE DEVELOPED A MAJOR OIL LEAK AND WAS IMMEDIATELY SHUT DOWN. TECHNICIANS DISCOVERED THE OIL FILTER BOWL HAD BLOWN OF - [SDR ZKFA2024030600201](https://openairdocs.org/sdr/ZKFA2024030600201), Mar 5, 2024: ELECTRONIC UNIT. OVERHEATED. PILOTS NOTICED SMOKE SMELL IN COCKPIT DURING CRUISE FLIGHT, ON TRIP KHYA-KAPF, FOLLOWED BY OBSERVING SMOKE. CONDUCTED EMERGENCY DESCENT AND LANDING AT KSAV. MAI - [SDR 2022F00364](https://openairdocs.org/sdr/2022F00364), Aug 5, 2022: NONE. NONE. AIRCRAFT IMPACTED A DEER ON LANDING AT KPYM. RIGHT TRAILING EDGE FLAP WAS DAMAGED BEYOND REPAIR AND WAS REPLACED. - [SDR FUKA202201020001](https://openairdocs.org/sdr/FUKA202201020001), Jan 2, 2022: O-RING. FAILED. WHILE CRUISING AT 36,000 FT, CREW NOTED AN E1 LOW OIL PRESSURE INDICATION. ON CONFIRMING LOSS OF OIL PRESSURE ON THE ANALOG INDICATOR. THE CREW COMPLIED WITH QR - [SDR 2021FA0000311](https://openairdocs.org/sdr/2021FA0000311), Nov 4, 2021: HINGE. CORRODED. RH AILERON SIGNIFICANT CORROSION FOUND AT CENTER TRIM TAB HINGE, AROUND BONDING STRAP ATTACHMENT HOLE, IN AFT SPAR STRUCTURE. TEXTRON ENGINEERING NOTIFIED AND N - [SDR CA160216010](https://openairdocs.org/sdr/CA160216010), Feb 10, 2016: ENGINE. SURGES. (CAN) DURING TAXIING, IN PREPARATION OF A REPOSITIONING FLIGHT, THE PILOT HEARD A LOUD NOISE REPORTED AS A COMPRESSOR SURGE. ENGINE POWER WAS PULLED BACK TO IDL - [SDR CA150602011](https://openairdocs.org/sdr/CA150602011), May 17, 2015: ENGINE. FAILED. (CAN) CUSTOMER REPORTED THAT DURING TAKEOFF ROLL THE ACFT WAS SHAKING & ALL NR 2 ENG PARAMETERS WERE FLUCTUATING, ERRATIC. THE PILOT ELECTED TO PERFORM IFSD OF - [SDR 2CJA20150528001](https://openairdocs.org/sdr/2CJA20150528001), May 17, 2015: SOLENOID. INTERMITTENT. AT 0915 LOCAL TIME THEY WERE POSITIONED ON AIRPORT HOLDING, SHORT OF RUNWAY 19. NOTICED AIR CONDITIONING WAS NOT MAINTAINING & CABIN WAS GETTING WARM. AFTER CLE - [SDR CA140312001](https://openairdocs.org/sdr/CA140312001), Feb 22, 2014: BLEED VALVE. MALFUNCTIONED. DURING LANDING, THE ENGINE POWER REDUCED UNCOMMANDED TO BELOW IDLE POWER. THE ENGINE WAS SECURED AND THE TRIP COMPLETED WITHOUT FURTHER ISSUE. REPEATED ATTEMPTS - [SDR ZKFR20130724001](https://openairdocs.org/sdr/ZKFR20130724001), Jul 24, 2013: ATTACH FITTING. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON LT SIDE OF VERTICAL TO HORIZONTAL STABILIZER ATTACH FITTING. CORROSION IS INTERGRANULAR, AND IS LOCATED AROUND 1 - [SDR 2CJA2013F00139](https://openairdocs.org/sdr/2CJA2013F00139), Jul 1, 2013: FIRE WARNING. ILLUMINATED. AFTER TAKEOFF AND MAKING TURN NORTH. AT ROUGHLY 3500 FT, NR 2 ENGINE FIRE ALARM VERY BRIEFLY SOUNDED AND THE RESPECTIVE ENGINE FIRE LIGHTS CAME ON VERY BRIEFLY. - [SDR CA130401012](https://openairdocs.org/sdr/CA130401012), Mar 23, 2013: OIL SYSTEM. LOW PRESSURE. (CAN) AFTER LANDING, WHILE ON TAXI, THE OIL PRESSURE WENT DOWN, THE ENGINE ROLLED BACK AND SHUTDOWN BY ITSELF. THE PILOT CONTINUED TAXIING AND THE FIRE WARNING - [SDR ZKFR20130117002](https://openairdocs.org/sdr/ZKFR20130117002), Jan 10, 2013: O-RING. LEAKING. DURING PREFLIGHT, FLIGHT CREW NOTICED LT OTBD TIRE LOOKED LOW. MX DISCOVERED TIRE ALMOST COMPLETELY DEFLATED BUT NOT BLOWN. WHEEL ASSYS ONLY HAD 9 CYCLES SINCE - [SDR ZKFR20130117001](https://openairdocs.org/sdr/ZKFR20130117001), Jan 10, 2013: O-RING. LEAKING. DURING PREFLIGHT, FLIGHT CREW NOTICED LT INBD TIRE LOOKED LOW. MX DISCOVERED TIRE ALMOST COMPLETELY DEFLATED BUT NOT BLOWN. WHEEL ASSYS ONLY HAD 9 CYCLES SINCE - [SDR ZKFR20120605001](https://openairdocs.org/sdr/ZKFR20120605001), Jun 5, 2012: CHECK VALVE. LEAKING. OXYGEN SYS NON-RETURN VALVE LEAKING ALLOWING OXYGEN TO FLOW BACKWARDS AND LEAK OUT OF FILLER PORT. THIS WAS A BRAND NEW CHECK VALVE FROM MFG. REMOVED AND REPLAC - [SDR ZKFR20120530001](https://openairdocs.org/sdr/ZKFR20120530001), May 30, 2012: CHECK VALVE. LEAKING. OXYGEN SYSTEM LEAKING: FOUND OXYGEN SYSTEM NON-RETURN VALVE INOP AND ALLOWING OXYGEN TO FLOW BACKWARDS AND LEAKING OUT OF FILLER PORT. REMOVED AND REPLACED NON- - [SDR ZKFR2012040900001](https://openairdocs.org/sdr/ZKFR2012040900001), Apr 9, 2012: SKIN. DELAMINATED. DURING ENGINE CHANGE, CORE COWL SEGMENT FOUND DELAMINATED. MFG HAS A REPAIR FOR THIS PROBLEM BUT UNFORTUNATELY THE EXTENT OF DAMAGE TO THIS CORE COWL IS BEYOND - [SDR ZKFR201112163233](https://openairdocs.org/sdr/ZKFR201112163233), Dec 16, 2011: CONTROLLER. FAULTY. CABIN TEMPERTURE UNCONTROLLABLE IN AUTO MODE. FOUND CABIN TEMPERTURE CONTROLLER NOT PROVIDING ANY OUTPUT VOLTAGE. CONTROLLLER GIVES MOMENTARY PULSES ONLY VISIBL - [SDR CA110228001](https://openairdocs.org/sdr/CA110228001), Feb 13, 2011: ENGINE. SHUTDOWN. (CAN) IFSD DURING TAXI AFTER LANDING, THE PILOT NOTICED AN UNCOMMANDED ENGINE SHUTDOWN. THE ACFT CONTINUED TO THE HANGAR AND ATTEMPTED ENGINE RE-START WAS UNSUC - [SDR S8A2009F00004](https://openairdocs.org/sdr/S8A2009F00004), Jul 12, 2009: FIRE LOOP. FALSE ACTIVATION. ACFT DEPARTED ENROUTE WITH (4) PASSENGERS AND (2) CREW. AT CLIMB OUT AT APPROX 2000 FT AGL NR 1 ENG HAD FIRE INDICATION. CREW DECLARED AN EMERGENCY WITH ATC AND - [SDR S8A2009F00001](https://openairdocs.org/sdr/S8A2009F00001), Apr 15, 2009: O-RING. FAILED. ACFT DEPARTED ON REPO LEG WITH ONLY CREW ON BOARD. ON CLIMBOUT NOTICED NR 2 SYS LOW PRESSURE LIGHT CAME ON FOLLOWED BY MAIN HYD LOW LEVEL LIGHT AND NR. 1 SYS LO - [SDR CA090311007](https://openairdocs.org/sdr/CA090311007), Mar 4, 2009: ENGINE. FLAMED OUT. (CAN) DURING DESCENT, THE STARTER GENERATOR (OUT) WARNING CAME ON FOLLOWED BY ENGINE FLAMEOUT. THE CREW LANDED THE ACFT SINGLE ENGINE AT DESTINATION. TROUBLESHO - [SDR S8A2008F00000](https://openairdocs.org/sdr/S8A2008F00000), Apr 16, 2008: BYPASS VALVE. STUCK. ENROUTE, AIRCRAFT N547LR AT 22,000 FT EXPERIENCED A UNCOMMANDED LOSS OF PRESSURIZATION FROM 16,000 TO 6,000 FT. THE AIRCRAFT MADE A DIVERSION, WITH AN UNEVENTFU - [SDR EOX2008F00000](https://openairdocs.org/sdr/EOX2008F00000), Jan 5, 2008: STARTER GEN. VIBRATION. AIRCRAFT WAS FL360 ENROUTE, FLIGHT CREW NOTED A VIBRATION IN THE RT ENGINE AND DID A PRECAUTIONARY SHUTDOWN OF THE RT ENGINE. THE AIRCRAFT DIVERTED AND MADE AN - [SDR DXTA200601612](https://openairdocs.org/sdr/DXTA200601612), Sep 23, 2006: UNKNOWN. FUMES. FUMES IN CABIN WHEN AIRCRAFT ON THE GROUND AND APU RUNNING WITH APU AIR VALVE OPENED. RAN LT AND RT ENG, APU IAW H/S M/M 49-20 + HS1000 M/M CHAP 80-10-00. OPS C - [SDR DXTA200601543](https://openairdocs.org/sdr/DXTA200601543), Aug 7, 2006: BRAKE ASSY. MALFUNCTIONED. BRAKES ARE MUSHY, ALMOST 3/4 TRAVEL ON PILOTS SIDE BEFORE BRAKES BEGIN TO TAKE EFFECT. ABOUT 1/2 TRAVEL ON CO-PILOTS SIDE. PERFORMED BRAKE BLEED PROCEDURE TO AL - [SDR DXTA200601452](https://openairdocs.org/sdr/DXTA200601452), Jun 23, 2006: TIRE. FAILED. BLOWN RT MAIN OUTBOARD TIRE INBOARD RT MAIN + OUTBOARD LT MAIN HAVE FLAT SPOT WITH 6 CORDS SHOWING. FOUND RT MAIN OUTBOARD TIRE BLOWN, RT MAIN INBOARD TIRE FLAT - [SDR DXTA200601414](https://openairdocs.org/sdr/DXTA200601414), May 31, 2006: FLUID. DETECTED. LT IB TIRE VERY HOT AFTER LANDING. STREAM OF SMOKE FROM THE 12 O'CLOCK IB POSITION. PLANE PULLS TO LT WHEN BRAKES ARE APPLIED GENTLY. SUSPECT DRAGGING IB PORT B - [SDR DXTA200601369](https://openairdocs.org/sdr/DXTA200601369), Apr 30, 2006: WARNING LIGHT. UNKNOWN. AUX TRANSFER LIGHT ILLUMINATED, TAKE OFF ABORTED. ITEM IS UNDER INVESTIGATION. - [SDR DXTA200601229](https://openairdocs.org/sdr/DXTA200601229), Feb 2, 2006: UNKNOWN. UNKNOWN. REPEAT WRITEUP, DURING NORMAL TAXI SPEED, WHEN BRAKES APPLIED AIRCRAFT VEERED LEFT. - [SDR DXTA200601216](https://openairdocs.org/sdr/DXTA200601216), Jan 26, 2006: BRAKE ASSY. HOT. REPEAT WRITE-UP. AFTER LOW SPEED 60KT ABORTED TAKEOFF, LEFT BRAKE ASSEMBLY WAS VERY HOT AND SMOKING. LARGE TEMP DIFFERENCE BETWEEN LEFT (HOT) AND RIGHT (COOLER) - [SDR DXTA200601201](https://openairdocs.org/sdr/DXTA200601201), Jan 17, 2006: INDICATOR. ACTIVATED. T/O ROLL ABORTED FOR ENG/FUEL LOOK UP LIGHT. ITEM IS UNDER INVESTIGATION. - [SDR DXTA200601180](https://openairdocs.org/sdr/DXTA200601180), Jan 3, 2006: FIRE WARNING. ILLUMINATED. DURING ROTATION NR 2 ENG FIRE LIGHT ILLUMINATED WITH MASTER WARNING LIGHT & FIRE BELL. DURING EMERGENCY PROCEDURE FIRE LIGHT WENT OUT WHEN HANDLE WAS PULLED. FI - [SDR DXTA200501129](https://openairdocs.org/sdr/DXTA200501129), Dec 5, 2005: MASTER CYLINDER. MALFUNCTIONED. UPON LANDING, CAPTAINS BRAKE PEDALS ARE SPONGY & PEDALS TEND TO GO TO THE FLOOR IN ORDER TO STOP THE AIRCRAFT. BRAKES CHECKED NORMAL ON TAXI OUT PRIOR TO DEPART - [SDR 2005FA0001528](https://openairdocs.org/sdr/2005FA0001528), Nov 8, 2005: EXTINGUISHER. INCORRECT. REMOVING HAND HELD FIRE EXTINGUISHER FROM THE COCKPIT FOR ROUTINE INSPECTION IT WAS NOTED THAT THE HANDLE DID NOT APPEAR TO BE CORRECT. FURTHER INSPECTION SHOWE - [SDR DXTA200500898](https://openairdocs.org/sdr/DXTA200500898), Aug 14, 2005: LANDING GEAR. INOPERATIVE. RED LANDING GEAR LIGHT ON THE RIGHT SIDE (RIGHT MAIN) STAYED ON AFTER GEAR RETRACTION, WITNESS ON THE GROUND REPORTED THAT THE RIGHT MAIN GEAR NEVER RETRACTED. - [SDR DXTA200500893](https://openairdocs.org/sdr/DXTA200500893), Aug 10, 2005: WARNING LIGHT. MALFUNCTIONED. RED LANDING GEAR UNSAFE LIGHT ON THE RIGHT SIDE STAYED LIT AFTER GEAR RETRACTION. EXCESS WIND NOISE AND SLIGHT VIBRATION WAS NOTICED WHILE AIRBORNE. VISUALLY IN - [SDR DXTA200500788](https://openairdocs.org/sdr/DXTA200500788), Jun 19, 2005: POSITION SWITCH. MALFUNCTIONED. DEPARTING LIT GEAR SELECTED UP L MAIN GEAR UNSAFE LIGHT ILLUMINATED. 400FT AGL SELECTED FLAPS UP AND GEAR LIGHT EXTINGUISHED. CYCLED LANDING GEAR OPS GOOD. AT 1 - [SDR DXTA200500734](https://openairdocs.org/sdr/DXTA200500734), May 21, 2005: WIRE. BROKEN. AFTER TAKEOFF, THE MACH TRIM YAW DAMPER AND AUTO-PILOT WOULD NOT ENGAGE ON THE FGC PANEL. REPAIRED BROKEN WIRES AT LAFGS ANNUNCIATOR TRANSFER BUTTON. CLEANED BU - [SDR DXTA200500699](https://openairdocs.org/sdr/DXTA200500699), Apr 26, 2005: STRUT. DAMAGED. THRU V1, RUDDER BECAME EXTREMELY STIFF AND REMAINED STIFF UNTIL AFTER AIRCRAFT CAME TO A TAXI. YAW DAMPER WAS CYCLED ON THEN OFF TWICE AND APPEARED TO FUNCTION - [SDR DXTA200500660](https://openairdocs.org/sdr/DXTA200500660), Apr 3, 2005: WARNING LIGHT. ILLUMINATED. ON CLIMBOUT, AFTER GEAR SELECTED UP, THREE RED UNSAFE LIGHTS SHOWED (LM, NOSE, RM) AS WELL AS THE GREEN RIGHT MAIN LIGHT. RETURNED FOR LANDING GEAR SELECTED DOW - [SDR DXTA200500594](https://openairdocs.org/sdr/DXTA200500594), Feb 15, 2005: LINE. LEAKING. ON LANDING BRAKES WERE VERY SOFT AND MADE STOPPING THE AIRPLANE DIFFICULT. ALSO CO-PILOTS BRAKES CONFIRMED THE BRAKE ISSUE. LEFT PEDAL ON CO-PILOTS SIDE WENT TO - [SDR DXTA200500587](https://openairdocs.org/sdr/DXTA200500587), Feb 11, 2005: QUICK DISCONNECT. CONTAMINATED. ON A ROLLING TAKEOFF NR 1 ENGINE DID NOT SPOOL UP TO FULL POWER I FIRST NOTICED A SPLIT IN N2 RPM THEN SAW N1 RPM ON NR 1 ENGINE WAS ABOUT 5 PERCENT BELOW TAKEO - [SDR DXTA200500576](https://openairdocs.org/sdr/DXTA200500576), Feb 3, 2005: CONTROL CABLE. OUT OF ADJUST. CONTROLS ARE BINDING. WHILE MOVING THE CONTROLS LT & RT THERE IS A NOISE AND FEELING OF BINDING IN PILOT CONTROL COLUMN. AT HIGHER SPEED MORE PRONOUNCED, AT SLO - [SDR DXTA200400503](https://openairdocs.org/sdr/DXTA200400503), Dec 30, 2004: OIL SYSTEM. OVERSERVICED. IMMEDIATELY AFTER AIRBORNE & SELECTING MAIN AIR VALVE TO ON, SMOKE BEGAN TO BELLOW THROUGHOUT THE COCKPIT AND CABIN AREAS. MAIN AIR VALVES WERE IMMEDIATELY SELE - [SDR DXTA200400468](https://openairdocs.org/sdr/DXTA200400468), Dec 7, 2004: WARNING SYSTEM. ACTIVATED. ON TAKEOFF ROLL AT APPROX 65-70 KTS FUEL/ENG LOOK UP LIGHT WITH ASSOCIATED AUX TRANSFER FAULT ILLUMINATED. ITEM IS UNDER INVESTIGATION. - [SDR DXTA200400457](https://openairdocs.org/sdr/DXTA200400457), Nov 22, 2004: ODOR. DETECTED. AFTER TWO HOURS OF FLIGHT BOTH PILOTS SMELLED STRONG ELECTRICAL / BURNED OIL FUMES WHICH IRRITATED EYES. NO VISIBLE FUMES MAIN AIR VALVES SELECTED TO LOW PRESSU - [SDR DXTA200400428](https://openairdocs.org/sdr/DXTA200400428), Oct 17, 2004: BRAKE ASSY. MALFUNCTIONED. WHEN APPLYING THE BRAKES FROM THE LT SEAT, THE FIRST APPLICATION RESULTS IN ALMOST NO BRAKING ACTION. THE PEDALS GO TO THE STOPS WITH VERY LITTLE RESULTS. BREAK - [SDR DXTA200400352](https://openairdocs.org/sdr/DXTA200400352), Aug 2, 2004: ODOR. DETECTED. WHILE CLIMBING THROUGH FL250 SELECTED ENGINE ANTI ICE ON, SHORTLY THEREAFTER NOTICED A STRONG BURNING SMELL IN THE COCKPIT. DE-SELECTING ANTI ICE, SMELL WENT AW - [SDR DXTA200400271](https://openairdocs.org/sdr/DXTA200400271), Mar 19, 2004: TAPE. LOOSE. CLIMBING THROUGH APPROXIMATELY FL280, EXPERIENCED A SEVERE LONGITUDINAL OSCILLATION. THE YOKE OSCILLATED LEFT AND RIGHT RAPIDLY AND WINGS WERE FLEXING 4 TO 6 IN All 63: https://openairdocs.org/model/raytheon-hawker-1000/reports.md ## STCs that may be installed (OpenAirDocs) (60, 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 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 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 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 ST02346AT-D](https://openairdocs.org/stc/ST02346AT-D): Installation of Composite Stang Fairings. Summit Aviation 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 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 ST04265AT](https://openairdocs.org/stc/ST04265AT): Replacement of the inner aluminum barrel of the engine inlet cowl, with an inlet barrel of carbon graphite sandwich construction. Quiet Technology Aerospace - [STC ST00934DE](https://openairdocs.org/stc/ST00934DE): Installation of Becker Avionics BXT6553 transponder. Peregrine - [STC SA00096LA](https://openairdocs.org/stc/SA00096LA): Installation of a Patient Loading and Utility System (PLUS). LifePort LLC - [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 ST01248CH](https://openairdocs.org/stc/ST01248CH): Installation of an air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed - [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 ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC - [STC ST00135BO](https://openairdocs.org/stc/ST00135BO): Modification of Honeywell TCAS II system installation with R/T 910 and software Version 6.4a to R/T 910 with Change 7.0 software; or TCAS 2000 system with R/T 950, 951 and software Version 6.4a to R/T 950, 951 with Change 7.0 software. Pro Star Aviation, 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 ST09069SC](https://openairdocs.org/stc/ST09069SC): Installation of King KHF-950 HF Communication Systems. Textron Aviation Inc - [STC ST09158SC](https://openairdocs.org/stc/ST09158SC): Installation of a Honeywell TCZ-910 TCAS system. Textron Aviation Inc - [STC ST04367AT](https://openairdocs.org/stc/ST04367AT): Removal of the Existing Honeywell DL-900 or DL-950 Data Loader and Installation of the Honeywell DL-1000 Data Loader. Chippewa Aerospace Inc - [STC ST04154CH](https://openairdocs.org/stc/ST04154CH): Installation of acoustic insulation kit for Fuselage and Aft Pressure Bulkhead. Damping Technologies Inc - [STC ST04155CH](https://openairdocs.org/stc/ST04155CH): Installation of acoustic insulation kit for Forward Wing-to-Body Fairing. Damping Technologies Inc - [STC ST04156CH](https://openairdocs.org/stc/ST04156CH): Installation of acoustic insulation kit for Interior Panels. Damping Technologies Inc - [STC ST09250AC](https://openairdocs.org/stc/ST09250AC): Logo light installation on lower surface of the horizontal stabilizer. Textron Aviation Inc - [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS - [STC ST01560CH](https://openairdocs.org/stc/ST01560CH): Install Aero Medical Products Mfg., Inc. Air Ambulance Stretcher P/N 125 using Installation Kit P/N 805. Paul/ Lanna Egan LLC - [STC ST02542LA](https://openairdocs.org/stc/ST02542LA): Installation of PPG Aerospace cockpit windshields P/Ns 196600-1 and 196600-2. PPG Aerospace - [STC ST03185CH-D](https://openairdocs.org/stc/ST03185CH-D): Activation of a TrueNorth Avionics, Inc. Simphone WiFi System. Standard Aero - [STC ST546CH-D](https://openairdocs.org/stc/ST546CH-D): Installation of an AlliedSignal Avionics, Dual GNS-XLS, Flight Management System with GPS as a primary means of navigation. Standard Aero - [STC ST01933CH-D](https://openairdocs.org/stc/ST01933CH-D): Installation of Honeywell Runway Awareness and Advisory System (RAAS). Standard Aero - [STC ST01406WI-D](https://openairdocs.org/stc/ST01406WI-D): Installation of the Honeywell Primus EPIC Control Display System/Retrofit (CDS/R). Duncan Aviation Inc - [STC ST02146NY](https://openairdocs.org/stc/ST02146NY): Installation of EMS Technologies Ltd. Cabin Network Xcelerator (CNX). EMS Technologies Canada Ltd - [STC ST01512LA-D](https://openairdocs.org/stc/ST01512LA-D): Installation of -218-218 software with Runway Awareness Advisory System (RAAS) activation option on Honeywell MK V Enhanced Ground Proximity Warning System (EGPWS). Gulfstream Aerospace Corporation All 60: https://openairdocs.org/model/raytheon-hawker-1000/stcs.md ## PMA parts (OpenAirDocs) (857, 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 - [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/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-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 - [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 - [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 - [PM-8112](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133503698020251118174943.0001): Outboard Speed Brake Hing Mask Set. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025 - [PM-8111](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118962975220251118174942.0001): Inboard Speed Brake Hing Mask Set. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025 - [PM-8105](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117980667320251118174941.0001): Outboard Flaptrack Fairing AFT Mask Set. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025 - [PM-8109](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108106833220251118174942.0001): Horizontal Stabilizer Tip Mask Set. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 2025 - [PM-8103](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107937688020251118174941.0001): Inboard Flaptrack Fairing AFT Mask Set. PM Research, Inc. · PMA PQ10049NE · Modification part · May 5, 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-FC6933-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174964364720250604173228.0001): L.A. Tube. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25FC6933-1 · Mar 13, 2025 - [NPMA-UN381-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149282509320250604173224.0001): Bolt. AV8 PMA, LLC. · PMA PQ03885SW · Replaces 25UN381 · Mar 13, 2025 - [NP-DC630C-72](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171216714520250604173221.0001): Poppet Assy. AV8 PMA, LLC. · PMA PQ03885SW · Replaces DC630C-72 · Mar 4, 2025 - [NP-DC630C-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165311568720250604173220.0001): Valve Body. AV8 PMA, LLC. · PMA PQ03885SW · Replaces DC630-10 · Mar 4, 2025 - [NP-DC630C-67](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164174407220250604173221.0001): Poppet Base. AV8 PMA, LLC. · PMA PQ03885SW · Replaces DC630C-67 · Mar 4, 2025 - [NP-DC630C-71](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131872507120250604173221.0001): Poppet Stem. AV8 PMA, LLC. · PMA PQ03885SW · Replaces DC630C-71 · Mar 4, 2025 - [NP-DC630C](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114368465520250604173220.0001): Charging Valve. AV8 PMA, LLC. · PMA PQ03885SW · Replaces DC630C · Mar 4, 2025 - [NP-DC630C-51](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106100036020250604173221.0001): Plug. AV8 PMA, LLC. · PMA PQ03885SW · Replaces DC630C-51 · Mar 4, 2025 All of them: https://openairdocs.org/model/raytheon-hawker-1000/pma.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Raytheon Corporate Jets HAWKER 1000](https://openairdocs.org/model/raytheon-corporate-jets-hawker-1000): 8 registered aircraft, registry code 7450005 --- 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.