# Raytheon HAWKER 900XP

- Type: Aircraft model (FAA registry)
- Registry code: 7150017
- Manufacturer (registry): RAYTHEON AIRCRAFT COMPANY
- Model: HAWKER 900XP
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 17
- Weight class: 20,000 lb and over
- 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-900xp

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 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

## Information bulletins (advisory) (3)

- [SAIB CE-20-10](https://openairdocs.org/saib/CE-20-10): Air Distribution System: Loss of Cabin Pressure. Issued Apr 30, 2020
- [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 (141, newest 50)

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

- [SDR 2026FA0000839](https://openairdocs.org/sdr/2026FA0000839), Sep 11, 2026: BRACKET. OUT OF POSITION. RIGHT ENGINE (#2) REAR COWLING BRACE PIN CABLE CAUGHT AROUND THROTTLE LEVER AND WOULD NOT ALLOW THROTTLE MOVEMENT. CABLE AND BRACKET WERE ADJUSTED TO PREVENT FU
- [SDR E0YA2025FA0000081](https://openairdocs.org/sdr/E0YA2025FA0000081), Oct 19, 2025: ENGINE. FAILED. NUMBER 1 ENGINE FAILURE AT FL150. CREW HEARD A BANG, AIRCRAFT YAWED, ENGINE ROLLBACK, NO THRUST AVAILABLE, ITT STARTED TO RISE AND CREW SHUTDOWN. DIVERTED AND L
- [SDR 3SRA20240425001](https://openairdocs.org/sdr/3SRA20240425001), Apr 16, 2024: BEARING. DESTROYED. CREW INDICATED ON TAXI AFTER LANDING A VIBRATION/NOISE FROM L/H SIDE OF AIRCRAFT. AIRCRAFT WAS JACKED AND THE #1 MAIN WHEEL HAD SIDE TO SIDE PLAY IN THE WHEEL. 
- [SDR 2023FA0000753](https://openairdocs.org/sdr/2023FA0000753), Nov 10, 2023: NONE. NONE. ANY HAWKER AIRCRAFT THAT HAS WINGLETS WILL RUN OUT OF NOSE DOWN TRIM IF IT IS NOT SET TO FULL AVAILABLE TRAVEL WITH THE TOLERANCE. TRAVELS AS STATED IN THE AMM 
- [SDR 2023F00179](https://openairdocs.org/sdr/2023F00179), May 19, 2023: FITTING. CRACKED. CREW REPORTS AGGRESSIVE VIBRATION THROUGH THE MAIN LANDING GEAR UPON TOUCHDOWN. UPON PERFORMING VISUAL INSPECTION OF THE MAIN LANDING GEAR, DISCOVERED THE LEFT 
- [SDR Y9PA4202303210001](https://openairdocs.org/sdr/Y9PA4202303210001), Mar 16, 2023: CIRCUIT BREAKER. BURNED. DURING A CREW TRAINING SESSION THE DIRECTOR OF OPS FOUND 3 CIRCUT BREAKERS ON WINDOW HEAT TEST PANEL BEHIND THE CO-PILOT (SUB PANEL B)POPPED AND UPON FURTHER IN
- [SDR DBCA202212200010](https://openairdocs.org/sdr/DBCA202212200010), Dec 20, 2022: FUEL NOZZLE. FAILED. PRIOR TO POWER APPLICATION ON TAKEOFF THE NR 2 ENGINE ROLLED BACK. CREW EXITED THE RUNWAY AND RETURNED TO RAMP. MTN REMOVED AND INSPECTED ENGINE. FOUND FUEL NOZ
- [SDR DBCA202212070009](https://openairdocs.org/sdr/DBCA202212070009), Dec 7, 2022: DISPLAY. FAILED. DURING TAKE-OFF ROLL PILOT'S PFD WENT BLANK. CREW EXECUTED A LOW SPEED ABORT AND RETURNED TO BED.MTN REMOVED AND REPLACED PILOT'S PFD WITH OVH UNIT. OPS CHECKED
- [SDR 9JLA2022080333655](https://openairdocs.org/sdr/9JLA2022080333655), Aug 3, 2022: PRESSURE SYSTEM. INOPERATIVE. THE FLIGHT CREW DESCRIBED HAVING A PRESSURIZATION ISSUE DURING THE CLIMB AFTER TAKEOFF. THE FLIGHT CREW ELECTED TO RETURN BACK TO THE AIRPORT AND LAND FOR MAINT
- [SDR 2022FA0000521](https://openairdocs.org/sdr/2022FA0000521), Jul 31, 2022: COMPRESSOR BLADE. FAILED. AIRCRAFT DEPARTED KHLN JULY 31 2022 AROUND 9:55 AM MDT CLIMBING THROUGH 25,000FT PILOT REPORTED LOUD BANG FROM #2 ENGINE AND THEN THE ENGINE ROLLED BACK AND SHU
- [SDR 3SRA20220110001](https://openairdocs.org/sdr/3SRA20220110001), Jan 10, 2022: FUEL CONTROL. INOPERATIVE. PHYSICAL ROLLBACK OF #1 ENGINE FOLLOWED BY THE AMBER #1 ENGINE COMPUTER LIGHT ILLUMINATING. ENGINE CONTINUED TO OPERATE IN MANUAL MODE. AIRCRAFT RETURNED TO KSU
- [SDR 9JLA2021120812616](https://openairdocs.org/sdr/9JLA2021120812616), Dec 1, 2021: TCAS SYSTEM. INTERMITTENT. THE FLIGHT CREW REPORTED OF A INTERMITTENT TCAS FAIL ON THE PDF. THE MAINTENANCE TEAM DETERMINED THE TCAS PROCESSOR WAS DEFECTIVE AND WAS REMOVED AND REPLACED W
- [SDR 9JLA2021120612616](https://openairdocs.org/sdr/9JLA2021120612616), Dec 1, 2021: TCAS SYSTEM. DEFECTIVE. THE FLIGHT CREW REPORTED ON FLIGHT LEG #2 THE TCAS FAIL INTERMITTENT ON PRIMARY FLIGHT DISPLAY. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE TCAS RECEIVE
- [SDR 9JLA2021120634618](https://openairdocs.org/sdr/9JLA2021120634618), Nov 22, 2021: NONE. NONE. THE FLIGHT CREW NOTED FUEL LEAKING FROM THE VENTRAL FUEL TANK AFTER LANDING. OPERATIONS WERE CONTINUED PER MEL 28-22-1-2. THE MAINTENANCE TEAM DISCOVERED THE RE
- [SDR 2021FA0000261](https://openairdocs.org/sdr/2021FA0000261), Sep 20, 2021: BUSHING. MIGRATED. THE HAWKER 900XP MAINTENANCE MANUAL "POWER PLANT (ENGINE CHANGE) - REMOVAL/INSTALLATION" CHAPTER XP-71-00-01-401 PARAGRAPH 4. B. (3) (A) (B), (5) (A) (B) READS 
- [SDR 3SRA20210922001](https://openairdocs.org/sdr/3SRA20210922001), Sep 2, 2021: PRESSURE SYSTEM. INOPERATIVE. AFTER TAKEOFF CREW REPORTED THAT THE AIRCRAFT WAS NOT PRESSURIZING. PIC RETURNED TO AIRPORT AND LANDED WITH NO PROBLEMS.
- [SDR 9JLA2021081025962](https://openairdocs.org/sdr/9JLA2021081025962), Jul 29, 2021: SWITCH. DEFECTIVE. THE FLIGHT CREW REPORTED THAT DURING LANDING THE RIGHT THRUST REVERSER GREEN REVRS LIGHT FLASHES INTERMITTENTLY AND EXTINGUISHES WITH TR ACTIVATION. THEREFORE N
- [SDR 9JLA2021080227994](https://openairdocs.org/sdr/9JLA2021080227994), Jul 29, 2021: TERMINAL. DIRTY. THE FLIGHT CREW REPORTED THAT AFTER STARTING THE NO1 ENGINE THE NO2 ENGINE WOULD NOT START. NO1 ENGINE START SELECT DID NOT ILLUMINATE AND THERE WAS NO ENGINE R
- [SDR 9JLA2021072825960](https://openairdocs.org/sdr/9JLA2021072825960), Jul 9, 2021: WARNING MESSAGE. FALSE ACTIVATION. THE FLIGHT CREW REPORTED A "TCAS FAIL" ANNUNCIATION ON THE PDF AND TCAS TEST FAIL AURAL ANNOUNCEMENT DURING PREFLIGHT TESTING. OPERATIONS WERE CONTINUED PER MEL
- [SDR UG8A21P04261349JF](https://openairdocs.org/sdr/UG8A21P04261349JF), Apr 26, 2021: I/O MODULE. MALFUNCTIONED. RED TRIM ANNUNCIATOR ILLUMINATED CONTINUOUSLY DURING ALL MODES OF FLIGHT, CLIMB, CRUISE AND DESCENT. THE LIGHT WOULD ILLUMINATE SHORTLY AFTER AP WAS ENGAGED. WE
- [SDR 9JLA2021041627971](https://openairdocs.org/sdr/9JLA2021041627971), Apr 12, 2021: CONTROLLER. DEFECTIVE. THE FLIGHT CREW REPORTED THAT DURING FLIGHT THE COPILOTS A WINDSCREEN DID NOT HEAT. THE MAINTENANCE TEAM DETERMINED THAT THE THERMAL CONTROLLER WAS DEFECTIVE. T
- [SDR 9JLA2020110929419](https://openairdocs.org/sdr/9JLA2020110929419), Nov 4, 2020: WIRE HARNESS. DEFECTIVE. THE FLIGHT CREW REPORTED THAT THE NR 1 ENGINE N2 INDICATIONS WERE ERRATIC IN FLIGHT. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE NR 1 ENGINE HARN
- [SDR 9JLA2020110929404](https://openairdocs.org/sdr/9JLA2020110929404), Jul 23, 2020: WIRE HARNESS. DEFECTIVE. THE FLIGHT CREW REPORTED THAT THE NO 1 ENGINE N1 FLUCTUATED AT CRUISE AND ALSO RECEIVED AN AMBER COMPUTER NO 1 ANNUNCIATOR. THE MAINTENANCE VENDOR TROUBLESHOT, 
- [SDR 2020F00325](https://openairdocs.org/sdr/2020F00325), Jun 26, 2020: WINDOW. DAMAGED. RIGHT DV WINDOW OUTER PANE SEPARATED AFTER TAKE-OFF NO INDICATION BEFORE SEPARATION P/N 25-8FN353-44A. AIRCRAFT HAD JUST TAKEN OFF AT 2,000 FEET WINDOW DELAMINA
- [SDR 9JLA2020110921237](https://openairdocs.org/sdr/9JLA2020110921237), Mar 31, 2020: WIRE HARNESS. DEFECTIVE. THE FLIGHT CREW REPORTED THAT THE NUMBER 1 ENGINE N2 INDICATIONS WERE ERRATIC CAUSING A FLIGHT DIVERSION. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT
- [SDR 2GYR201912190007](https://openairdocs.org/sdr/2GYR201912190007), Dec 2, 2019: TRUNNION. DAMAGED. WHILE INSTALLING THE RIGHT MLG LEG WE NOTICED THAT THE FWD UPPER AND LOWER TRUNNION ATTACH POINTS, WHERE THE BARREL NUTS SLIDE INTO, BOTH HAD GROOVES WORN INTO 
- [SDR 2GYR201910240001](https://openairdocs.org/sdr/2GYR201910240001), Oct 21, 2019: BOLT. FAILED. WHEN THE AIRCRAFT TOUCHED DOWN ON LANDING, THE CREW NOTED A LARGE VIBRATION THROUGHOUT THE AIRFRAME. THE VIBRATION LESSENED IN INTENSITY AS THE AIRCRAFT SLOWED 
- [SDR 2GYR20191023004](https://openairdocs.org/sdr/2GYR20191023004), Oct 21, 2019: BOLT. BROKEN. UPON LANDING AT KGYY AT APPROX. 8:00 P.M. ON THE NIGHT OF OCTOBER 21, 2019 AIRCRAFT N163DK FELT A ABNORMAL VIBRATION FORM THE LEFT MLG. THE AIRCRAFT TAXIED TO T
- [SDR ZESA201942301](https://openairdocs.org/sdr/ZESA201942301), Apr 22, 2019: DUCT. LOOSE. DURING CRUISE AT 40,000FT A LOUD BANG WAS HEARD AND THE CABIN STARTED TO DEPRESSURIZE, PILOTS FOLLOWED THEIR CHECKLIST AND DESCENDED AND LANDED ASAP. THE PROBLE
- [SDR 3FPY201810078004](https://openairdocs.org/sdr/3FPY201810078004), Oct 4, 2018: SEAT TRACK. CORRODED. LT INBOARD SEAT RAIL CORRODED - FOUND DURING C1-C12 INSPECTION. ASSESSED BY STRUCTURES AND SUPPORTS CONTINUED AIRCRAFT OPERATION FOR ANOTHER 100 FLIGHT HOURS WI
- [SDR 3FPY201810078003](https://openairdocs.org/sdr/3FPY201810078003), Oct 4, 2018: STATOR VANE. DAMAGED. DURING ROUTINE ENGINE INSPECTIONS, THE LT ENGINE FAN STATOR VANES - LEADING EDGE SCREENS WERE FOUND DAMAGED - QTY 13 NEW VANE FAN STATORS INSTALLED.
- [SDR 3FPY201810078002](https://openairdocs.org/sdr/3FPY201810078002), Oct 4, 2018: CONTROL CABLE. CORRODED. ELEVATOR CONTROL CABLE CORRODED AT REAR FUSELAGE - FOUND DURING C1-C12 INSPECTION.
- [SDR 3FPY201810078001](https://openairdocs.org/sdr/3FPY201810078001), Oct 4, 2018: LEVER. CORRODED. FUEL SYSTEM LOW PRESSURE VALVE LEVER FOUND CORRODED DURING C1-C12 INSPECTION.
- [SDR ZESA10280724001](https://openairdocs.org/sdr/ZESA10280724001), Jul 23, 2018: SENSOR. FAULTY. AIRCRAFT LEFT KLBE WITH NORMAL TAKE OFF AND CLIMB, AT CRUISE THE ENGINE WENT INTO MANUAL MODE, CHECK LIST WERE FOLLOWED AND PILOTS RETURNED TO BLOCK AT KLBE AND
- [SDR XCGA201804160001](https://openairdocs.org/sdr/XCGA201804160001), Apr 10, 2018: FUEL CONTROL. FAILED. PILOT REPORTED THAT WHILE DESCENDING THROUGH 24,000 FEET ON APPROACH, THE LEFT ENGINE ROLLED BACK AND FAILED. NO RESTART WAS ATTEMPTED, THE AIRPLANE MADE AN UNE
- [SDR 2018F00099](https://openairdocs.org/sdr/2018F00099), Feb 14, 2018: RIB. CORRODED. LIGHT CORROSION FROM LT WING OTBD RIB 16. REPAIRED IAW FR-HA-0019-3819, REV 1.
- [SDR DXTA2018012100499](https://openairdocs.org/sdr/DXTA2018012100499), Jan 21, 2018: TRANSDUCER. INOPERATIVE. DURING CRUISE, THE RIGHT ENGINE N1 ROLLED BACK APPROX 5 TO 7 PERCENT. SIGNIFICANT YAWING WAS NOTICED AS THE ENGINE ROLLED BACK AND THEN RESUMED NORMAL POWER. FE
- [SDR 9JLA2018012612392](https://openairdocs.org/sdr/9JLA2018012612392), Nov 27, 2017: STARTER GEN. DEFECTIVE. THE FLIGHT CREW REPORTED THAT DURING FLIGHT THAT THEY WERE SHOWING A AMP SPLIT BETWEEN GENERATORS AND THE RH SIDE WAS LOWER THAN NORMAL. MAINTENANCE TROUBLESHOT
- [SDR 9JLA2018012612584](https://openairdocs.org/sdr/9JLA2018012612584), Nov 21, 2017: SPIGOT. BROKEN. DURING THE PRE-FLIGHT INSPECTION CHECKS, THE TOP AFT MAIN CABIN DOOR SPIGOT PIN ASSEMBLY WAS FOUND TO BE BROKEN. THE PIN WAS REPLACED AND THE DOOR SYSTEM RIG CH
- [SDR 9JLA2018012612583](https://openairdocs.org/sdr/9JLA2018012612583), Oct 24, 2017: GCU. FAILED. DURING FLIGHT, THE FLIGHT CREW REPORTED THAT THEY LOST THE NR 2 AC ALTERNATOR. THE SYSTEM WAS SECURED AND THE FLIGHT CONTINUED. TROUBLESHOT AND DETERMINED THAT 
- [SDR 2017FA0000299](https://openairdocs.org/sdr/2017FA0000299), Jul 20, 2017: WINDSHIELD. CRACKED. PILOTS WINDSHIELD CRACKED DURING FLIGHT FROM KIAH TO KCAK. THE AIRCRAFT DEPARTED KIAH AT 0707 CDST AND LANDED AT KCAK AT 1046 CDST. THE CREW DECLARED AN EMERGEN
- [SDR DXTA2017070406420](https://openairdocs.org/sdr/DXTA2017070406420), Jul 4, 2017: CONNECTOR. DIRTY. LEFT ENGINE ROLLED BACK. AT 38,000 APX 5 MIN INTO CRUISE PHASE. LEFT ENGINE ROLLED BACK 10% PLUS. OBSERVED LEFT ENGINE GAUGE AND CONFIRMED WITH AIRCRAFT YAWNING
- [SDR UVVR2017052300045](https://openairdocs.org/sdr/UVVR2017052300045), May 19, 2017: STUD. SHEARED. LEFT MLG FAILED TO RETRACT AFTER TAKEOFF. RT MLG AND NLG RETRACTED NORMALLY. LG EXTENDED NORMALLY. JACKED AIRCRAFT & PERFORMED FUNCTIONAL TEST OF MLG SYSTEM WIT
- [SDR ZESA20170131001](https://openairdocs.org/sdr/ZESA20170131001), Jan 31, 2017: LAMP. BURNED OUT. DURING A FLIGHT, THE PILOTS DIVERTED DUE TO THE LANDING GEAR DOWN AND LOCK INDICATION DID NOT ILLUMINATE. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE
- [SDR DXTA2017012606363](https://openairdocs.org/sdr/DXTA2017012606363), Jan 26, 2017: LINE. LEAKING. STRONG ODOR OF HYDRAULIC FLUID COMING FROM VENTS WITH MAIN AIR VALVES SELECTED ON IN FLIGHT. CLEANED RESIDUAL HYDRAULIC FLUID FROM HYDRAULIC RESEVOIR AIR CHARGE
- [SDR P6UR201701173249](https://openairdocs.org/sdr/P6UR201701173249), Jan 16, 2017: CABLE. BROKEN. DEFECTIVE AIRBRAKE CONTROL CABLE FOUND BROKEN AT PULLEY JUST AFT OF COCKPIT CENTER PEDESTAL.
- [SDR 2016FA0000569](https://openairdocs.org/sdr/2016FA0000569), Nov 16, 2016: CONTROL PANEL. MALFUNCTIONED. PILOT COULD NOT SELECT AN ALTITUDE ON THE AUTO-PILOT ALTITUDE PRESELECT FUNCTION. THE CONTROLLER KEPT CHANGING ALTITUDES INSTEAD OF THOSE SELECTED. TWO MORE FLI
- [SDR BKEA20161031](https://openairdocs.org/sdr/BKEA20161031), Oct 28, 2016: WARNING MESSAGE. FALSE ACTIVATION. DURING CLIMB, PASSING THRU APPROXIMATELY FL 280, RECEIVED A YELLOW CAUTION MESSAGE HYD 2 LOW PRESSURE WARNING. AFTER RUNNING APPROPRIATE CHECK LISTS, DETERMINED
- [SDR DXTA2016092406310](https://openairdocs.org/sdr/DXTA2016092406310), Sep 24, 2016: SENSOR. FAILED. DURING CRUISE AT FL 400, THE RIGHT ENGINE ROLLED BACK THEN WENT BACK TO NORMAL. ROLL BACK WAS ENOUGH TO MAKE THE PLANE YAW. RETURNED TO DEPARTURE. REPLACED INLE
- [SDR DXTA2016092106304](https://openairdocs.org/sdr/DXTA2016092106304), Sep 21, 2016: CONNECTOR. DIRTY. AT 40,000 FT APPROXIMATELY 200 MILES FROM DESTINATION, -48C IS A+8. RIGHT ENGINE ROLLED BACK 2 TIMES IN APPROXIMATELY 30 SECONDS. FIRST ROLL BACK UNABLE TO RECO

All 141: https://openairdocs.org/model/raytheon-hawker-900xp/reports.md

## STCs that may be installed (OpenAirDocs) (92, 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 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 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 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 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 ST04773NY](https://openairdocs.org/stc/ST04773NY): Interior Refurbishment. Exacaire Inc A Division of IMP Group Ltd
- [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 ST04704NY](https://openairdocs.org/stc/ST04704NY): Cabin Reconfiguration. Exacaire IMP Group Ltd
- [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 ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04202NY](https://openairdocs.org/stc/ST04202NY): Installation of Lee Aerospace Inc. Window Panel B. Lee Aerospace Inc
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC ST00950DE](https://openairdocs.org/stc/ST00950DE): Installation of Refuel Valve Indicators. West Star Aviation
- [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 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
- [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 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 SA7972SW-D](https://openairdocs.org/stc/SA7972SW-D): Installation of Global AFIS System. Textron Aviation Inc
- [STC ST10597SC-D](https://openairdocs.org/stc/ST10597SC-D): Installation of Conversion of Aft LH Interior Seating. Textron Aviation Inc
- [STC ST09262SC-D](https://openairdocs.org/stc/ST09262SC-D): Installation of a third and fourth, 750 liter, oxygen bottle in aft equipment bay. Textron Aviation Inc
- [STC ST09651SC](https://openairdocs.org/stc/ST09651SC): Installation of a Cabin Interior and Avionics Systems. Textron Aviation Inc
- [STC ST09873SC-D](https://openairdocs.org/stc/ST09873SC-D): Installation of Protective Breathing Equipment (PBE). Textron Aviation Inc
- [STC ST09955SC-D](https://openairdocs.org/stc/ST09955SC-D): Installation of a Divan Cargo Net Assembly. Textron Aviation Inc
- [STC ST10596SC-D](https://openairdocs.org/stc/ST10596SC-D): Installation of an Aircell Voice/Data Communication System. Textron Aviation Inc
- [STC ST10599SC-D](https://openairdocs.org/stc/ST10599SC-D): Installation of an Espresso Maker in accordance with STC Required Documents List (RDL) No. 230-2003 Revision 5 dated January 14, 2010, or later FAA approved revision. Textron Aviation Inc
- [STC ST10961SC](https://openairdocs.org/stc/ST10961SC): Installation of a galley shell. Textron Aviation Inc
- [STC SA7944SW](https://openairdocs.org/stc/SA7944SW): Installation of a cabin oxygen system. Textron Aviation Inc
- [STC SA8062SW](https://openairdocs.org/stc/SA8062SW): Installation of a therapeutic oxygen system. Textron Aviation Inc

All 92: https://openairdocs.org/model/raytheon-hawker-900xp/stcs.md

## PMA parts (OpenAirDocs) (746, 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
- [L610510-20629](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142852436520260705233750.0001): Cup. Timken Corporation · PMA PQ4105CE · Replaces L610510-20629 · Jun 4, 2026
- [L610549-20629](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101297111220260705233750.0001): Cone. Timken Corporation · PMA PQ4105CE · Replaces L610549-20629 · Jun 4, 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
- [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
- [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
- [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

All of them: https://openairdocs.org/model/raytheon-hawker-900xp/pma.md

## The same model under other registry codes

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

- [Hawker Beechcraft HAWKER 900XP](https://openairdocs.org/model/hawker-beechcraft-hawker-900xp): 129 registered aircraft, registry code 4220011

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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.