# Raytheon BAE 125-800A

- Type: Aircraft model (FAA registry)
- Registry code: 7150040
- Manufacturer (registry): RAYTHEON AIRCRAFT COMPANY
- Model: BAE 125-800A
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-jet
- 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: 2
- Page: https://openairdocs.org/model/raytheon-bae-125-800a

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 2009-08-01](https://openairdocs.org/ad/2009-08-01): Honeywell FMSs · Bombardier CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R), CL-600-2B16 (CL-604) and 11 more. Effective May 14, 2009
- [AD 2008-21-01](https://openairdocs.org/ad/2008-21-01): Main landing gear (MLG) · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125) and 1 more. Effective Oct 22, 2008
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 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 2003-04-20](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 2001-13-05](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 2000-08-07](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 89-18-07 R1](https://openairdocs.org/ad/89-18-07-R1): Elevator Balance Spigot · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 34 more. Effective Dec 18, 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 96-25-12](https://openairdocs.org/ad/96-25-12): Auxiliary Power Units · BAE Systems HS 748 Series 2A, HS 748 Series 2B, 707-100 Long Body and 74 more. Effective Jan 13, 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 95-15-04](https://openairdocs.org/ad/95-15-04): Wing Leading Edge Skins · Textron BAe.125 Series 1000A and BAe.125 Series 800A. Effective Aug 23, 1995
- [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
- [AD 94-01-06](https://openairdocs.org/ad/94-01-06): Traffic Alert and Collision Avoidance System II Processors · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 176 more. Effective Feb 4, 1994
- [AD 94-01-04](https://openairdocs.org/ad/94-01-04): Traffic Alert and Collision Avoidance System · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 136 more. Effective Feb 4, 1994
- [AD 93-24-08](https://openairdocs.org/ad/93-24-08): Engine Fire Extinguisher Systems · Textron BAe.125 Series 1000B, BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and 38 more. Effective Jan 18, 1994
- [AD 93-23-08](https://openairdocs.org/ad/93-23-08): Battery and Emergency Contactors · Textron BAe.125 Series 1000B, BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and 38 more. Effective Dec 29, 1993
- [AD 93-24-07](https://openairdocs.org/ad/93-24-07): Auxiliary Power Unit (APU) Fuel Control Enclosure Box · Solar T62T-39 turbine auxiliary power unit (Textron STC SA1923SW). Effective Dec 23, 1993
- [AD 93-22-07](https://openairdocs.org/ad/93-22-07): Forward Cabin Door · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and BAe.125 Series 800A (U-125). Effective Dec 20, 1993
- [AD 93-02-10](https://openairdocs.org/ad/93-02-10): Battery Cables · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 39 more. Effective Mar 26, 1993
- [AD 93-01-10](https://openairdocs.org/ad/93-01-10): Battery Overheating · Textron BAe.125 Series 1000A, BAe.125 Series 1000B, BAe.125 Series 800A and 37 more. Effective Mar 2, 1993
- [AD 92-26-06](https://openairdocs.org/ad/92-26-06): Disable Circuit Breakers · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and BAe.125 Series 800A (U-125). Effective Feb 1, 1993
- [AD 92-27-09](https://openairdocs.org/ad/92-27-09): Mail Landing Gear Sidestay Upper Arm Assembly · Textron BAe.125 Series 1000B, BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and 38 more. Effective Jan 27, 1993
- [AD 92-25-11](https://openairdocs.org/ad/92-25-11): Hydraulic Accumulator · Textron BAe.125 Series 1000B, BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and 38 more. Effective Jan 12, 1993
- [AD 92-18-09](https://openairdocs.org/ad/92-18-09): Auxiliary Power Unit Wiring · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and BAe.125 Series 800A (U-125). Effective Nov 17, 1992
- [AD 92-17-12](https://openairdocs.org/ad/92-17-12): Fluorescent Lighting Systems · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125) and 3 more. Effective Sep 28, 1992
- [AD 92-17-09](https://openairdocs.org/ad/92-17-09): Thrust Reversers · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and BAe.125 Series 800A (U-125). Effective Sep 28, 1992
- [AD 92-16-12 R1](https://openairdocs.org/ad/92-16-12-R1): Tail Cone Vents · Textron BAe.125 Series 1000B, BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and 38 more. Effective Sep 28, 1992
- [AD 92-15-04](https://openairdocs.org/ad/92-15-04): Main Landing Gear · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and BAe.125 Series 800A (U-125). Effective Aug 20, 1992
- [AD 92-10-09](https://openairdocs.org/ad/92-10-09): Rudder Pedal Torque Tubes · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and BAe.125 Series 800A (U-125). Effective Jun 29, 1992
- [AD 92-07-03](https://openairdocs.org/ad/92-07-03): Wash Basin Water Tank · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and BAe.125 Series 800A (U-125). Effective May 4, 1992
- [AD 92-06-05 R1](https://openairdocs.org/ad/92-06-05-R1): Nose Landing Gear · Textron BAe.125 Series 1000B, BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and 38 more. Effective Apr 21, 1992
- [AD 92-06-04](https://openairdocs.org/ad/92-06-04): Dimmer System · Textron BAe.125 Series 800A, BAe.125 Series 800A (C-29A) and BAe.125 Series 800A (U-125). Effective Apr 21, 1992

Historical (superseded or no longer in force):

- [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

All 84: https://openairdocs.org/model/raytheon-bae-125-800a/ads.md

## Information bulletins (advisory) (3)

- [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 (2)

- [N884AB](https://openairdocs.org/aircraft/N884AB): [Jetsteam Aviation Inc](https://openairdocs.org/faa-owner/JETSTEAM%20AVIATION%20INC), [Cheyenne, WY](https://openairdocs.org/faa-place/WY/Cheyenne), S/N 258097
- [N8881J](https://openairdocs.org/aircraft/N8881J): [Gdc Aviation LLC](https://openairdocs.org/faa-owner/GDC%20AVIATION%20LLC), [Jacksonville, FL](https://openairdocs.org/faa-place/FL/Jacksonville), built 1992, S/N 258219

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (2)

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 20130316010729I](https://openairdocs.org/incident/20130316010729I), Mar 16, 2013: Raytheon Aircraft Company BAE 125-800A (N801SA), Pontiac, MI, No damage. On March 16, 2013 N38CZ (registered as N801SA), a bae 125-800A, departed Pontiac Michigan IFR for aspen, CO. The aircraft climbed and leveled at FL270. The…
- [Incident 20110203002419I](https://openairdocs.org/incident/20110203002419I), Feb 3, 2011: Raytheon Ai BAE 125-800 (N705BB), Chesterfield, MO, No damage. PILOT HEARD A LOUD BANG FROM THE LEFT ENGINE AND NOTICED ITT DECREASING. ENGINE WAS SHUT DOWN AND PILOT RETURNED TO KSUS, APPROXIMATELY 24 MILES WITHOUT…

## Service difficulty reports (282, newest 50)

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

- [SDR 2023FA0000353](https://openairdocs.org/sdr/2023FA0000353), Apr 27, 2023: OUTFLOW VALVE. JAMMED. AIRCRAFT LOST PRESSURIZATION AT FL039, PERFORMED AN EMERGENCY DECENT AND LANDED BACK TO PBI WITHOUT INCIDENT.
- [SDR 2023FA0000352](https://openairdocs.org/sdr/2023FA0000352), Apr 24, 2023: AIR DUCT. DETACHED. AIRCRAFT LOST PRESSURIZATION AT FL015 AND RETURNED TO PBI. AFTER LANDING IT WAS DISCOVERED THAT AN AIR-CONDITIONING DUCT HAD SEPARATED FROM THE REAR PRESSURE BU
- [SDR 2022FA0000279](https://openairdocs.org/sdr/2022FA0000279), Jun 2, 2022: NONE. NONE. DURING CLIMB PASSING FL 355 THE "CABIN ALTITUDE" LIGHT CAME ON WITH DIFFERENTIAL PRESSURE INDICATOR SHOWING ZERO. CABIN DID NOT LOSE PRESSURIZATION; HOWEVER THE
- [SDR A8JA202103120035](https://openairdocs.org/sdr/A8JA202103120035), Mar 12, 2021: CIRCUIT BREAKER. FAULTED. DURING APPROACH FROM KFXE TO KHOU AT APPROXIMATELY 1930 HRS LOCAL, FLIGHT CREW OBSERVED NO LANDING GEAR DOWN AND LOCKED INDICATION. CREW ELECTED TO ABORT LANDIN
- [SDR JGVR20181102001](https://openairdocs.org/sdr/JGVR20181102001), Nov 2, 2018: TERMINAL. BURNED. INVESTIGATED SMOKE IN THE COCKPIT BEHIND THE CO-PILOT INSTRUMENT PANEL. FOUND THE -A- SCREEN ELECTROSTATIC FILTER WIRE TERMINALS BURNED ON SUPPLY SIDE. REMOVED 
- [SDR 4TDA2018091300001](https://openairdocs.org/sdr/4TDA2018091300001), Sep 12, 2018: ACCUMULATOR. LOW PRESSURE. AS AIRCRAFT WAS RELEASED FOR FLIGHT, THE PILOT RELEASED THE PARKING BRAKE, ACTIVATED THE REGULAR BRAKE SYSTEM AND NOTICED THE PRESSURES ROSE TO 1,000 PSI AND FE
- [SDR E0YA2018062900087](https://openairdocs.org/sdr/E0YA2018062900087), Jun 28, 2018: STARTER GEN. FAILED. DURING CRUISE THE NR 2 ENGINE STARTER/GENERATOR FAILED AND CAUSED VIBRATION.
- [SDR 4TDA201805293805](https://openairdocs.org/sdr/4TDA201805293805), May 23, 2018: CONTROLLER. MALFUNCTIONED. AT FL 400, THE CAPTAIN NOTICED AN INCREASE IN CABIN CLIMB RATE AND DECREASE IN CABIN PRESSURE. CREW DONNED OXYGEN MASKS AND MADE A DESCENT TO FL100. FLIGHT CONT
- [SDR 2018FA0000149](https://openairdocs.org/sdr/2018FA0000149), Apr 22, 2018: WIRE. PINCHED. WANDER LIGHT BEHIND CAPTAIN`S CHAIR, WIRING FOUND PINCHED AND ARCED. CREW REPORTED A SMALL FLAME FOR A MOMENT UNTIL THE CIRCUIT BREAKER. NOTHING FURTHER WAS REP
- [SDR 6EMY20171105856](https://openairdocs.org/sdr/6EMY20171105856), Nov 2, 2017: NOT REPORTED. FIRE. AN EMPLOYEE OBSERVED BLACK SMOKE EMERGING FROM THE UPPER FUSELAGE REAR EQUIPMENT BAY ACCESS PANELS OF THE SUBJECT AIRCRAFT. POWER WAS IMMEDIATELY TURNED OFF AND
- [SDR PAIR20160916S3570](https://openairdocs.org/sdr/PAIR20160916S3570), Sep 14, 2016: AIR DUCT. BROKEN. CLIMBING THROUGH 23,000 FT, AIRCRAFT EXPERIENCED REAR BAY OVERHEAT WARNING FOLLOWED BY CABIN ALTITUDE STARTING TO CLIMB. ACFT RETURNED TO POINT OF DEPARTURE. MA
- [SDR ZP7A2016F00039](https://openairdocs.org/sdr/ZP7A2016F00039), Dec 1, 2015: FUEL CONTROL. DEFECTIVE. AT FL400, ENGINE NR 2 BEGAN LOOSING POWER, N1 REDUCED TO BELOW 60 PERCENT, DESCENDED TO 14,000 FT N1 REDUCED TO BELOW 40 PERCENT. AT BELOW 8000 FT MSL ENGINE PO
- [SDR 9PVA2015F00111](https://openairdocs.org/sdr/9PVA2015F00111), Sep 9, 2015: SEAL. SHIFTED. CABIN ALTITUDE TOD CABIN ALTITUDE INCREASED VIELENTY AT 200 FT + IAE MINUTE ALL THE WAY TO 20,000 FT. PAX O2 MASK PARTIALLY DEPLOYED. DOOR SEAL SHIFTED.
- [SDR 2015F00105](https://openairdocs.org/sdr/2015F00105), Sep 2, 2015: BOLT. CORRODED. REMOVED AND INSPECTED MASS BALANCE WEIGHTS, AND SPIGOTS. THE BOLT HAD EXCESSIVE CORROSION AND HAD TO BE REPLACED. WEIGHTS WERE CLEANED AND REUSED. BROKEN BOLT C
- [SDR 9PVA2015F00110](https://openairdocs.org/sdr/9PVA2015F00110), Aug 28, 2015: IRS. MISALIGNED. HAD TO RETURN TO THE AIRPORT BECAUSE THERE WAS 30 TO 90 DEGREES HEADING DIFFERENCE DUE TO A MISS ALIGNMENT OF THE IRS SYSTEM.
- [SDR JLTA20150824001](https://openairdocs.org/sdr/JLTA20150824001), Aug 21, 2015: ENGINE. MALFUNCTIONED. ON FRIDAY, AUGUST 21ST AT APPROX 1900Z, ACFT DEPARTED EMPTY & ENTERED CRUISE, EVERYTHING WAS NORMAL. ON THE INITIAL DESCENT CREW HEARD A STRANGE NOISE & OBSERVE
- [SDR DIXA2015F00097](https://openairdocs.org/sdr/DIXA2015F00097), Aug 19, 2015: OVERHEAT SENSOR. INTERMITTENT. CREW REPORTED CLIMBING THROUGH FL 150, RED REAR BAY OVERHEAT LIGHT ILLUMINATED, CREW FOLLOWED CHECKLIST PROCEDURES. LIGHT EXTINGUISHED WHILE STILL CLIMBING THRO
- [SDR T6FA2015072903](https://openairdocs.org/sdr/T6FA2015072903), Jul 29, 2015: INTERCOSTAL. CRACKED. FOUND CRACKED DENT IN FUSELAGE RT SIDE INTERCOSTAL UNDER LAVATORY FLOOR BETWEEN FRAME 16 TO FRAME 17. REPAIRED IAW FIELD REPAIR.
- [SDR T6FA2015072902](https://openairdocs.org/sdr/T6FA2015072902), Jul 29, 2015: SKIN. CORRODED. CORROSION FOUND ON FUSELAGE KEEL SKIN & DOUBLER BETWEEN FRAMES 12 & 12A. REPAIRED IAW FIELD REPAIR INSTRUCTIONS.
- [SDR T6FA2015072901](https://openairdocs.org/sdr/T6FA2015072901), Jul 29, 2015: SKIN. CORRODED. CORROSION FOUND ON LT SIDE MLG LEG FAIRING OUTER SKIN. REPAIRED IAW FIELD REPAIR.
- [SDR CA150525014](https://openairdocs.org/sdr/CA150525014), May 24, 2015: B-NUT. CRACKED. (CAN) DURING THE REPLACEMENT OF THE OXYGEN SYS CHARGING VLV WHICH WAS SUSPECTED OF A LEAK, IT WAS NOTICED THAT THE B NUT WHICH CONNECTS TO THE FILTER & IS PART 
- [SDR CA150113022](https://openairdocs.org/sdr/CA150113022), Jan 2, 2015: TUBE. LEAKING. (CAN) POST ARRIVAL, FLIGHT CREW CONDUCTED POST FLIGHT INSPECTION OF ACFT AND NOTED SIGNIFICANT OIL LEAKAGE ON LT ENGINE COWLINGS, NO INFLIGHT INDICATIONS WERE E
- [SDR 9JLA2014122607198](https://openairdocs.org/sdr/9JLA2014122607198), Dec 12, 2014: POSITION SWITCH. SHORTED. DURING TAXI THE SSU STALL IDENT LIGHT ILLUMINATED & THE NR 1 STALL CHANNEL DOES NOT TEST. EXTENSIVE TROUBLESHOOTING FOUND THE LT INBD FLAP POSITION MICRO SWITCH
- [SDR 9JLA2014122607197](https://openairdocs.org/sdr/9JLA2014122607197), Dec 10, 2014: AHRS. INTERMITTENT. NUMBER 2 AHRS UNIT INTERMITTENTLY ROLLS COPILOTS ATTITUDE INDICATOR CREATING A COMPARATOR MONITOR DISAGREE. THE DEFECTIVE UNIT WAS REMOVED PN7003360-943 SN 9508
- [SDR 2014FA0000506](https://openairdocs.org/sdr/2014FA0000506), Aug 26, 2014: INDICATION SYS. FAILED. FAILURE OF RT MLG INDICATION WHEN GEAR SELECTED DOWN FOR LANDING.
- [SDR FVJA2014082600148](https://openairdocs.org/sdr/FVJA2014082600148), Aug 22, 2014: COOLING TURBINE. FAILED. DURING THE CLIMB, CREW REPORTED LOUD SQUEAL FOLLOWED BY ODOR OF BURNED OIL AND REPORT OF SMOKE COMING FROM AIR VENTS. THE ACM, COOLING TURBINE FOUND TO HAVE FER
- [SDR 9JLA201405217509](https://openairdocs.org/sdr/9JLA201405217509), May 9, 2014: SWITCH. STUCK. THE CREW REPORTED THAT AFTER TAKEOFF & GEAR RETRACTION AN UNSAFE GEAR INDICATION, 3 RED LIGHTS & 1 MAIN GEAR GREEN LIGHT. THE CREW CYCLED THE GEAR BACK DOWN & R
- [SDR CA140407014](https://openairdocs.org/sdr/CA140407014), Apr 2, 2014: WIRE HARNESS. CHAFED. (CAN) FLIGHT CREW REPORTED LANDING GEAR SELECTOR WOULD NOT MOVE AFTER TAKEOFF. CHECKLIST CARRIED OUT AND FLIGHT CREW DECIDED TO RETURN TO AIRPORT AFTER CIRCLING
- [SDR CA140303002](https://openairdocs.org/sdr/CA140303002), Feb 27, 2014: SWITCH. FAILED. (CAN) FLIGHT CREW REPORTED AIRBRAKE SPOILER CIRCUIT BREAKER WAS FOUND TRIPPED AFTER SHUTDOWN. THE CIRCUIT BREAKER WAS RESET AND DID NOT OPEN AGAIN. DURING MAINT
- [SDR BN5A20142190001](https://openairdocs.org/sdr/BN5A20142190001), Feb 17, 2014: SEAL. WEAK. CREW REPORTED REAR BAY OVERHEAT AT FL 250. TROUBLESHOOTING FOUND BLEED AIR LEAK AT LT BLEED AIR VLV & LT NON-RETURN VLV. REMOVED LT BLEED AIR SOV & LT NON-RETUR
- [SDR BJYA 20130717001](https://openairdocs.org/sdr/BJYA%2020130717001), Jul 15, 2013: WARNING LIGHT. ILLUMINATED. CABIN HIGH ALTITUDE LIGHT ILLUMINATE AFTER REACHING FL 370. ON LEVEL OFF DURING ACCELERATION, CABIN HIGH ALTITUDE LIGHT ILLUMINATED. DONNED OXYGEN MASKS, DEPLOY
- [SDR 2013FA0000351](https://openairdocs.org/sdr/2013FA0000351), Jun 13, 2013: RELAY. BLOWN. RIGHT WINDSHIELD HEAT WAS FOUND INOPERATIVE ALONG WITH TAXI LIGHTS. INVESTIGATION FOUND THAT RELAY FOR RT WINDHSHIELD DEICE HAD BLOWN THE GUTS OUT OF THE RELAY 
- [SDR WTXR2013060329204](https://openairdocs.org/sdr/WTXR2013060329204), Jun 3, 2013: LINE. CHAFED. THE VENTURI VACUUM LINE, FROM THE PRESSURIZATION CONTROLLER TO THE CABIN AIR OPERATED VENTURI IS BEING RUBBED THROUGH BY THE AILERON CONTROL CABLE THAT SITS DIR
- [SDR VIBR20131202001](https://openairdocs.org/sdr/VIBR20131202001), May 25, 2013: STUD. UNSECURE. ENGINE STARTER GENERATOR "B" STUD NOT SECURE IN STARTER GENERATOR TERMINAL BLOCK.
- [SDR JLTA20130520001](https://openairdocs.org/sdr/JLTA20130520001), May 15, 2013: BOLT. CORRODED. DURING A POSTFLIGHT INSPECTION, DISCOVERED THE RT AIRBRAKE OTBD COVERS WERE NOT ALIGNED. FOUND BOLTS IN BRACKET WERE LOOSE. SAFETY WIRE WAS STILL INTACT. SAFETY
- [SDR V0JA20130506001](https://openairdocs.org/sdr/V0JA20130506001), Apr 30, 2013: FILTER. MALFUNCTIONED. PILOTS SIDE WINDSHIELD HEAT ELECTROSTATIC FILTER PRODUCED SMOKE DURING OPERATION AND OPENED CIRCUIT BREAKER.
- [SDR KKYA20121031001](https://openairdocs.org/sdr/KKYA20121031001), Oct 21, 2012: FILTER. UNKNOWN. AFTER DEPARTURE NR 1 ENGINE FUEL LIGHT CAME ON. REDUCED NR 1 THROTTLE TO IDLE - LIGHT REMAINED ON. REPLACED THE ENGINE FUEL FILTER WITH NEW PER HONEYWELL TFE731
- [SDR KKYA20120924001](https://openairdocs.org/sdr/KKYA20120924001), Sep 21, 2012: PITOT SYSTEM. OBSTRUCTED. COMPUTER MONITOR NR 1 AND NR 2 AIRSPEEDS PLUS ALTITUDE DISCREPANCIES. FOUND DEBRIS IN BOTH PITOT SYSTEMS AND ADC NR 1 SYSTEM WAS PLUGGED.
- [SDR 9JLA2012073106330](https://openairdocs.org/sdr/9JLA2012073106330), Jul 25, 2012: COMPUTER. DEFECTIVE. CREW REPORTED THE LT ENGINE DEEC LIGHT COMES ON STEADY IN FLIGHT. THE ENGINE COMPUTER WAS REMOVED. A NEW COMPUTER WAS INSTALLED. FUNCTIONAL CHECKS WERE SATISFAC
- [SDR 2012FA0000490](https://openairdocs.org/sdr/2012FA0000490), Jul 18, 2012: AUTOPILOT SYS. MALFUNCTIONED. AT 24000 FT, INBOUND TO DESTINATION, AUTOPILOT WARNING HORN SOUNDED CONTINUOUSLY AND ALL AUTOPILOT WARNING LIGHTS WERE ON AND AUTOPILOT ENGAGE LIGHTS WERE ON WI
- [SDR 2012F00067](https://openairdocs.org/sdr/2012F00067), Mar 29, 2012: TRANSDUCER. INOPERATIVE. ON THE LAST LEG OF THE TRIP, ON START UP, THE RT ENGINE COMPUTER INOPERATIVE LIGHT ILLUMINATED. FOUND BAD N2 TRANSDUCER. REPLACED THE TRANSDUCER, OPS CHECKED GO
- [SDR L7OA201203270127](https://openairdocs.org/sdr/L7OA201203270127), Mar 21, 2012: VALVE. MALFUNCTIONED. ON CLIMBOUT FROM SJU, IT WAS NOTICED THAT FUEL WAS COMING FROM THE LEFT WING VENT AREA. THE AIRCRAFT RETURNED TO SJU WITHOUT INCIDENT.
- [SDR L7OA2012F00066](https://openairdocs.org/sdr/L7OA2012F00066), Mar 21, 2012: FUEL SYS. LEAKING. ON CLIMB OUT, NOTICED FUEL COMING FROM THE LT WING VENT AREA. ACFT RETURNED TO DEPARTURE WITHOUT INCIDENT.
- [SDR E81R2011122632222](https://openairdocs.org/sdr/E81R2011122632222), Dec 26, 2011: PUMP. LOW PRESSURE. INVESTIGATED REPORTED "HYD 2 LO PRESS" ANNUNCIATOR LIGHT INDICATION. REPLACED FAILED NR 2 ENGINE HYD PUMP WITH AN O/H PUMP AND DRAINED HYD SYS RESERVOIR, REPLAC
- [SDR BLUA2012F00025](https://openairdocs.org/sdr/BLUA2012F00025), May 16, 2011: MONOPOLE. FAILED. NR 2 ENGINE COMPUTER LIGHT ILLUMINATED IN FLIGHT. FOUND MONOPOLE FAILED.
- [SDR UVCA20110418001](https://openairdocs.org/sdr/UVCA20110418001), Apr 18, 2011: STARTER GEN. MALFUNCTIONED. RT STARTER GENEREATOR WOULD NOT START.
- [SDR CA110209027](https://openairdocs.org/sdr/CA110209027), Feb 9, 2011: B-NUT. CRACKED. (CAN) DURING INSPECTION A CRACK IN THE B-NUT ATTACHED TO THE SEQUENCE VALVE IN THE LT LANDING GEAR WELL AS NOTED. THE CRACK WAS RUNNING PERPENDICULAR TO THE THR
- [SDR CA110209031](https://openairdocs.org/sdr/CA110209031), Feb 9, 2011: FRAME. CRACKED. (CAN) DURING 24 YEAR INSP, A CRACK IN THE TOP CTR MEMBER OF THE LOWER PRESSING WAS FOUND.
- [SDR CA110209028](https://openairdocs.org/sdr/CA110209028), Feb 9, 2011: NUT. CRACKED. DURING REMOVAL OF THE VENTRAL FUEL TANK, THE ABOVE MENTIONED NUT WAS FOUND TO BE SEIZED IN PLACE. 2 CRACKS WERE NOTED ON THE OUTER SURFACE OF THE NUT: 1 PERPEND
- [SDR CA110209026](https://openairdocs.org/sdr/CA110209026), Feb 9, 2011: B-NUT. CRACKED. DURING INSP, A CRACK IN THE B-NUT ATTACHED TO THE SEQUENCE VALVE IN THE LT LANDING GEAR WELL AS NOTED. THE CRACK WAS RUNNINQ PERPENDICULAR TO THE THREADS OF THE

All 282: https://openairdocs.org/model/raytheon-bae-125-800a/reports.md

## STCs that may be installed (OpenAirDocs) (409, 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 ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [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 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 ST03292CH](https://openairdocs.org/stc/ST03292CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development, Inc
- [STC ST02410CH-D](https://openairdocs.org/stc/ST02410CH-D): Installation of Rockwell Collins Pro Line 21 IDS (Integrated Display System) with IFIS-5000 (Integrated Flight Information System) and Engine Instrument Display. BHE & Associates LTD
- [STC ST11145SC](https://openairdocs.org/stc/ST11145SC): Installation of Rockwell Collins dual AHC-3000 Attitude Heading Reference System (AHRS). BHE & Associates Ltd
- [STC ST00029LB](https://openairdocs.org/stc/ST00029LB): Installation of BFGoodrich traffic alert and collision avoidance system(TCAS I). Acron Aviation 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 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 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 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 SA7634SW](https://openairdocs.org/stc/SA7634SW): Installation of Mark V ground proximity warning system. Honeywell International Inc
- [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 ST01270WI-D](https://openairdocs.org/stc/ST01270WI-D): Installation of Honeywell MK V and MK VII EGPWS Runway Awareness and Advisory System (RAAS). This approval is limited to specifically idenitfied aircraft. Duncan Aviation Inc
- [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC ST00882DE](https://openairdocs.org/stc/ST00882DE): Installation of Becker Avionics BXT6553 transponder. Peregrine
- [STC ST00950DE](https://openairdocs.org/stc/ST00950DE): Installation of Refuel Valve Indicators. West Star Aviation
- [STC ST00934DE](https://openairdocs.org/stc/ST00934DE): Installation of Becker Avionics BXT6553 transponder. Peregrine
- [STC 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 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 ST00373BO](https://openairdocs.org/stc/ST00373BO): Installation of Rockwell Collins TDR-94D Transponders with ADS-B Out. Pro Star Aviation, LLC
- [STC ST00100BO](https://openairdocs.org/stc/ST00100BO): Installation of an AlliedSignal Corp. EGPWS MK VII Terrain Awareness and Warning 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 ST02499AK](https://openairdocs.org/stc/ST02499AK): Approval of the Thomas Global Systems TFD8601Active Matrix Liquid Crystal Display installed. ADS-B Technologies, LLC

All 409: https://openairdocs.org/model/raytheon-bae-125-800a/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
- [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
- [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
- [WF326058](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193418029220250624152912.0001): Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 169009-1, Alternate: 179411 · Jun 2, 2025
- [WF328893](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164487868320250624152913.0001): Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 49131-2 · Jun 2, 2025
- [WF331667](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130843592120250624152914.0001): Filter Assembly. Donaldson Company Inc · PMA PQ2432CE · Replaces Sundstrand Turbomach 179411 · Jun 2, 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
- [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

All of them: https://openairdocs.org/model/raytheon-bae-125-800a/pma.md

## The same model under other registry codes

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

- [British Aerospace BAE 125 SERIES 800A](https://openairdocs.org/model/british-aerospace-bae-125-series-800a): 59 registered aircraft, registry code 1500285
- [Corporate Jets BAE 125-800A](https://openairdocs.org/model/corporate-jets-bae-125-800a): 8 registered aircraft, registry code 1500103
- [Raytheon Corporate Jets BAE 125-800A](https://openairdocs.org/model/raytheon-corporate-jets-bae-125-800a): 8 registered aircraft, registry code 7450002
- [British Aerospace BAE 125-800A](https://openairdocs.org/model/british-aerospace-bae-125-800a): 5 registered aircraft, registry code 1500119
- [British Aerospace BAE 125 SERIES 800A](https://openairdocs.org/model/british-aerospace-bae-125-series-800a): 2 registered aircraft, registry code 1500286

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