# N909VJ: 1981 Dassault-Breguet FALCON 50

- Status: Valid registration
- Airframe: [Dassault-Breguet FALCON 50](https://openairdocs.org/model/dassault-breguet-falcon-50) (registry code 2730106, 10 seats)
- Engine: [Garrett TFE731 series](https://openairdocs.org/engine/garrett-tfe731-series) (registry code 29001)
- Data sheets: [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (Honeywell Aerospace US LLC) (OpenAirDocs)
- Serial number: 69
- Year built: 1981
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 5, 1981
- Certificate issued: November 26, 2012
- Expires: November 30, 2028
- Mode S code: AC927F
- Registered owner: [Wc Aviation LLC](https://openairdocs.org/faa-owner/WC%20AVIATION%20LLC)
- Location: [Gypsum, CO](https://openairdocs.org/faa-place/CO/Gypsum)
- Owner type: LLC
- Owner's area on the map: 39.7795° N, 107.1057° W: Placed by OpenAirDocs at the center of ZIP code 81637, within about 16 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=909VJ
- Page: https://openairdocs.org/aircraft/N909VJ

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Garrett TFE731 model are included.

## ADs that may apply (OpenAirDocs): 34 in force

### Matched by airframe (Dassault-Breguet FALCON 50)

None in force.

### Matched by engine (Garrett TFE731 series)

- [AD 2016-07-02](https://openairdocs.org/ad/2016-07-02): Failure of the interstage turbine transition duct · Honeywell International TFE731-4, TFE731-4R, TFE731-5AR and 2 more. Effective May 5, 2016
- [AD 2014-12-52](https://openairdocs.org/ad/2014-12-52): Engines · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 11 more. Effective Jul 28, 2014
- [AD 2012-17-05](https://openairdocs.org/ad/2012-17-05): First stage low-pressure turbine (LPT1) rotor assembly · Honeywell International TFE731-4, TFE731-4R, TFE731-5 and 3 more. Effective Oct 2, 2012
- [AD 2010-06-11](https://openairdocs.org/ad/2010-06-11): Second stage low-pressure compressor rotor (LPCR) discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2C and 16 more. Effective Apr 21, 2010
- [AD 2008-19-12](https://openairdocs.org/ad/2008-19-12): ITT duct · Honeywell International TFE731-4, TFE731-4R, TFE731-5 and 3 more. Effective Oct 27, 2008
- [AD 2008-02-19](https://openairdocs.org/ad/2008-02-19): High pressure (HP) turbine rotor assemblies · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 15 more. Effective Mar 6, 2008
- [AD 2005-13-07](https://openairdocs.org/ad/2005-13-07): Turbine rotor discs. · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Jul 27, 2005
- [AD 2005-05-15](https://openairdocs.org/ad/2005-05-15): (LPT) stage 1 disks · Honeywell International TFE731-2, TFE731-2C, TFE731-3 and 5 more. Effective Apr 18, 2005
- [AD 2001-23-09](https://openairdocs.org/ad/2001-23-09): Fan Rotor Discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Dec 21, 2001
- [AD 2000-15-09](https://openairdocs.org/ad/2000-15-09): HPC Impeller · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 20 more. Effective Oct 10, 2000
- [AD 98-17-01 R1](https://openairdocs.org/ad/98-17-01-R1): Flex Fuel Tube · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Nov 29, 1999
- [AD 97-04-03](https://openairdocs.org/ad/97-04-03): First stage low pressure turbine (LPT) seal plates · Honeywell International TFE731-2A, TFE731-3C and TFE731-3CR. Effective May 5, 1997
- [AD 96-05-03](https://openairdocs.org/ad/96-05-03): Fan rotor disks · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 13 more. Effective Apr 2, 1996
- [AD 96-04-01](https://openairdocs.org/ad/96-04-01): Fan Rotor Assembly · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Mar 15, 1996
- [AD 95-07-02](https://openairdocs.org/ad/95-07-02): Low Pressure Turbine Disks · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 3 more. Effective Jun 19, 1995
- [AD 94-23-05](https://openairdocs.org/ad/94-23-05): Honeywell International TFE731-3A and TFE731-3AR. Effective Dec 1, 1994
- [AD 94-07-03](https://openairdocs.org/ad/94-07-03): Turbine Nozzles · Honeywell International TFE731-2A, TFE731-3, TFE731-3A and 4 more. Effective Jun 6, 1994
- [AD 92-02-18](https://openairdocs.org/ad/92-02-18): Inflight Operation · Honeywell International TFE731-5BR. Effective Feb 10, 1993
- [AD 92-21-06](https://openairdocs.org/ad/92-21-06): Low Pressure Turbine (LPT) Rotor Disks · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 2 more. Effective Nov 27, 1992
- [AD 90-24-06](https://openairdocs.org/ad/90-24-06): Thermocouple Lead Assemblies · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 8 more. Effective Nov 13, 1990
- [AD 90-03-04](https://openairdocs.org/ad/90-03-04): High Pressure Turbine Rotor Discs · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 1 more. Effective Feb 22, 1990
- [AD 88-18-03](https://openairdocs.org/ad/88-18-03): High Pressure Turbine Rotor Disc · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 1 more. Effective Jul 21, 1989
- [AD 86-03-01](https://openairdocs.org/ad/86-03-01): Turbine Interstage Transition Ducts · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 4 more. Effective Feb 24, 1986
- [AD 82-23-03 R1](https://openairdocs.org/ad/82-23-03-R1): High Pressure Compressor Impellers · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Dec 9, 1983
- [AD 81-24-08](https://openairdocs.org/ad/81-24-08): Turbine Interstage Transition Ducts · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 2 more. Effective Jan 6, 1982
- [AD 80-16-04](https://openairdocs.org/ad/80-16-04): Tie Rod · Honeywell International TFE731-2, TFE731-3 and TFE731-3R. Effective Aug 7, 1980
- [AD 78-22-10](https://openairdocs.org/ad/78-22-10): Low Pressure Rotor Thrust Ball Bearings · Honeywell International TFE731-2, TFE731-3 and TFE731-3R. Effective Nov 13, 1978
- [AD 75-07-10](https://openairdocs.org/ad/75-07-10): Transfer Gearbox Vertical Bevel Gear Bearing · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective May 1, 1975
- [AD 74-23-05](https://openairdocs.org/ad/74-23-05): Fuel Pumps · Honeywell International TFE731-2. Effective Nov 14, 1974
- [AD 74-11-06](https://openairdocs.org/ad/74-11-06): Fuel Control Computer · Honeywell International TFE731-2. Effective Sep 23, 1974
- [AD 74-18-16](https://openairdocs.org/ad/74-18-16): Fuel Control Computer · Honeywell International TFE731-2. Effective Sep 6, 1974
- [AD 74-18-12](https://openairdocs.org/ad/74-18-12): Fuel Control Orifice Assembly · Honeywell International TFE731-2. Effective Sep 3, 1974
- [AD 74-13-09](https://openairdocs.org/ad/74-13-09): Fuel Pump Assemblies · Honeywell International TFE731-2. Effective Jul 31, 1974
- [AD 89-22-16](https://openairdocs.org/ad/89-22-16): Engine Acceleration or Deceleration · Honeywell International TFE731-2, TFE731-5, TFE731-5AR and 1 more

### Historical (superseded or no longer in force)

- [AD 98-17-01](https://openairdocs.org/ad/98-17-01) (historical): Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Oct 13, 1998
- [AD 96-18-13](https://openairdocs.org/ad/96-18-13) (historical): Fan rotor disk · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 10 more. Effective Nov 12, 1996
- [AD 86-11-05](https://openairdocs.org/ad/86-11-05) (historical): Fan Rotor Discs · Honeywell International TFE731-2, TFE731-3 and TFE731-3R

## Information bulletins (advisory) (1 in force)

- [SAIB NE-06-70](https://openairdocs.org/saib/NE-06-70): . Issued Sep 25, 2006

## NTSB investigations

None matched to N909VJ.

## FAA accident and incident reports

None matched to N909VJ.

## Reports on N909VJ not matched to an aircraft (1)

They name N909VJ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19940624026549I](https://openairdocs.org/incident/19940624026549I), Jun 24, 1994: Doug DC932 (N909VJ), Atlanta, GA, Minor damage. On gear retraction gear door light on. Gear stayed down. Landed.doors damaged still open. Prior same other DC9S.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N909VJ not matched to an aircraft (37)

They name N909VJ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR VJ9800434](https://openairdocs.org/sdr/VJ9800434), Sep 28, 1998: POWER SUPPLY. INOPERATIVE. IN EMERGENCY POSITION, LH NACELLE LIGHT WON'T WORK. REPLACED BATTERY POWER SUPPLY IAW MM 33-50.
- [SDR VJ9800220](https://openairdocs.org/sdr/VJ9800220), Jul 8, 1998: COVER. DISLODGED. ON ARRIVAL AT GATE, EMERGENCY SLIDE PACK COVER DISLODGED. REINSTALLED IAW MM 25-60. PERFORMED REQUIRED INSPECTIONS.
- [SDR VJ9800177](https://openairdocs.org/sdr/VJ9800177), May 10, 1998: BATTERY PACK. DISCHARGED. EPL TRACK LIGHTING FROM ROW 24 TO AFT CABIN DOOR INOP. RECONNECTED CANNON PLUG TO BATTERY PACK, OPS CHECKS GOOD IAW MM 33-50.
- [SDR VJ9800045](https://openairdocs.org/sdr/VJ9800045), Mar 12, 1998: SPAR CHORD. CORRODED. VISUAL INSPECTION OF BLEND AREA AT XRS80 PER AIRTRAN WO 30343, CORROSION WAS NOTED IN THE BLEND AREA AND AROUND 1 FASTENER NEXT TO TO THE BLENDED AREA ON THE RI
- [SDR VJ9800044](https://openairdocs.org/sdr/VJ9800044), Mar 6, 1998: BULKHEAD. CORRODED. TWO FASTENER HEADS POPPED AND BULGING UNDER PRESSURE DOME AT STA 597, RBL 18. DRILLED NEW PANEL, FABRICATED FINGER DOUBLERS PLUS 2 ADDITIONAL DOUBLERS IAW DC9 S
- [SDR VJ9800039](https://openairdocs.org/sdr/VJ9800039), Mar 6, 1998: WEB. CORRODED. TWO FASTENER HEADS POPPED OFF AND BULGING UNDER PRESSURE DOME AT FS STA 597, RBL 18. REMOVED BULKHEAD PRESSURE PANEL AT FS STA 597, DRILLED NEW PANEL, FABRICATE
- [SDR VJ9800043](https://openairdocs.org/sdr/VJ9800043), Mar 5, 1998: STRUCTURE. CORRODED. LOWER END CAP CORRODED AND 6 RIVET POPPED IN CARGO COMAPARTMENT BELOW CENTER FUEL TANK PRESSURE BULKHEAD. REMOVED DUCT SEAL CONTAINER, DOUBLER AROUND DUCT CUT O
- [SDR VJ9800057](https://openairdocs.org/sdr/VJ9800057), Feb 28, 1998: SKIN. CORRODED. AFT CARGO FUSELAGE SKIN AND FRAME CORRODED AT FRAME STATION 980 BETWEEN L27R AND L28R ON AFT SIDE. CUT OUT PLATING BETWEEN L27R AND L28R, FABRICATED FILLER USIN
- [SDR VJ9800050](https://openairdocs.org/sdr/VJ9800050), Feb 28, 1998: SKIN. CORRODED. AFT CARGO FUSELAGE SKIN AND FRAME ARE CORRODED HEAVILY ON AFT SIDE AT FRAME STA 980 BETWEEN LONG 28 R AND 27R. CUT OUT AREA OF PLATING BETWEEN L27R AND 28R. FAB
- [SDR 98ZZZM438](https://openairdocs.org/sdr/98ZZZM438), Feb 28, 1998: SKIN. CORRODED. AFT CARGO FUSELAGE SKIN AND FRAME CORRODED AT FRAME STATION 980 BETWEEN L27R AND L28R ON AFT SIDE. CUT OUT PLATING BETWEEN L27R AND L28R, FABRICATED FILLER USIN
- [SDR VJ970348](https://openairdocs.org/sdr/VJ970348), Nov 24, 1997: LIGHT. INOPERATIVE. EMERGENCY PATH LIGHTS IN AFT TAIL COMPARTMENT INOPERATIVE. REPAIRED SHORT AT TAIL CONE LIGHT AND REPLACED BLOWN FUSE IN EPL BATTERY PACK MODULE.
- [SDR VJ970339](https://openairdocs.org/sdr/VJ970339), Nov 5, 1997: SMOKE DETECTOR. MALFUNCTIONED. SMOKE DETECTOR CHIRPING IN RT AFT LAVATORY. REPLACED SMOKE DETECTOR, OPS CHECKS NORMAL IAW MM 26-00.
- [SDR VJ970338](https://openairdocs.org/sdr/VJ970338), Nov 5, 1997: COVER. LOOSE. MAIN PASSENGER DOOR EMERGENCY SLIDE COVER CAME LOOSE. REINSTALLED IAW MM 25-60 AND PERFORMED REQUIRED INSPECTION.
- [SDR VJ970185](https://openairdocs.org/sdr/VJ970185), Mar 24, 1997: BATTERY. DISCHARGED. EMERGENCY OVERHEAD LIGHTS AT SEAT ROWS 12, 14, 16 AND 18 ARE OUT. PERFORMED VISUAL AND CONTINUITY CHECK OF WIRING, CLEANED CORROSION FROM TERMINAL STRIP AND REP
- [SDR VJ970052](https://openairdocs.org/sdr/VJ970052), Feb 11, 1997: BATTERY. DISCHARGED. CEILING EMERGENCY LIGHTS FROM ROW 11 TO ROW 18 INOPERATIVE. REPLACED BATTERIES. OPS CHECKED NORMAL PER MM 33-50-0. (X)
- [SDR VJ970042](https://openairdocs.org/sdr/VJ970042), Jan 31, 1997: LIGHT. INOPERATIVE. SUBMITTER STATES, SUSPECT REMOVABLE HAND-HELD EMERGENCY LIGHT ASSEMBLY HAS AN INTERNAL SHORT. REPLACED EMERGENCY LIGHT ASSEMBLY PER MM 33-50. OPS CHECKED NORMAL
- [SDR VJ970009](https://openairdocs.org/sdr/VJ970009), Jan 23, 1997: LIGHT. BROKEN. EMERGENCY FLASHLIGHT AT FORWARD PASSENGER DOOR BROKEN. REPLACED EMERGENCY FLASHLIGHT PER MM 25-66-0. (M)
- [SDR VJ970008](https://openairdocs.org/sdr/VJ970008), Jan 19, 1997: BATTERY PACK. DISCHARGED. VENTRAL STAIR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS CHECKED GOOD PER MM 33-50-0. (M)
- [SDR VJ970003](https://openairdocs.org/sdr/VJ970003), Jan 17, 1997: POWER SUPPLY. INOPERATIVE. EMERGENCY PATH LIGHTS FROM AFT OVERWING EXITS INOPERATIVE. REPLACED POWER SUPPLY PER MM 33-51-01 AND REPAIRED BROKEN WIRES. OPERATIONALLY CHECKED GOOD. (M)
- [SDR VJ970018](https://openairdocs.org/sdr/VJ970018), Jan 2, 1997: ANGLE. CRACKED. DURING AN UNSCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE CENTER WING UPPER SURFACE FLOOR BEAM LONGITUDINAL SUPPORT AT RBL 44 AND FS 650-663 WAS FOUND 
- [SDR VJ970017](https://openairdocs.org/sdr/VJ970017), Jan 2, 1997: ANGLE. CRACKED. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE CENTER WING UPPER SURFACE FLOOR BEAM LONGITUDINAL SUPPORT AT LBL 44 IS CRACKED FROM FS 650 TO 66
- [SDR VJ970016](https://openairdocs.org/sdr/VJ970016), Jan 2, 1997: ANGLE. CRACKED. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE LEFT OUTBOARD FLOOR BEAM LOWER ATTACH ANGLE ON THE LOWER FLANGE AT FS 658 WAS FOUND WITH A .5 CR
- [SDR VJ970015](https://openairdocs.org/sdr/VJ970015), Jan 2, 1997: SPAR. BLEND OUT. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE RIGHT WING LOWER REAR SPAR XRS 80 HAS DEEP BLEND OUT. REWORKED BLEND OUT (ROTO PEENED). ALODINED
- [SDR VJ970014](https://openairdocs.org/sdr/VJ970014), Jan 2, 1997: SKIN. CORRODED. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE FUSELAGE CROWN SKIN AT THE FORWARD AND AFT ADF ANTENNA AT FS 256 TO FS 275 AND FS 294 TO FS 313 
- [SDR VJ970013](https://openairdocs.org/sdr/VJ970013), Jan 2, 1997: ANGLE. NON CONFORMING. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE DORSAL FIN AT THE LT OUTBOARD ATTACH WAS FOUND WITH A EXISTING REPAIR THAT WAS NOT IAW THE SRM. 
- [SDR VJ970012](https://openairdocs.org/sdr/VJ970012), Jan 2, 1997: ANGLE. CRACKED. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA THE DORSAL FIN ATTACH ANGLE ON THE LT SIDE INBOARD JUST AFT OF FS 1076 WAS FOUND CRACKED. REMOV
- [SDR 97ZZZM113](https://openairdocs.org/sdr/97ZZZM113), Jan 2, 1997: SKIN. CORRODED. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE FUSELAGE CROWN SKIN AT THE FORWARD AND AFT ADF ANTENNA AT FS 256 TO FS 275 AND FS 294 TO FS 313 
- [SDR 97ZZZM112](https://openairdocs.org/sdr/97ZZZM112), Jan 2, 1997: ANGLE. MIS MFG. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE DORSAL FIN AT THE LT OUTBOARD ATTACH WAS FOUND WITH A EXISTING REPAIR THAT WAS NOT IAW THE SRM. 
- [SDR 97ZZZM111](https://openairdocs.org/sdr/97ZZZM111), Jan 2, 1997: ANGLE. CRACKED. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE LEFT OUTBOARD FLOOR BEAM LOWER ATTACH ANGLE ON THE LOWER FLANGE AT FS 658 WAS FOUND WITH A .5 IN
- [SDR 97ZZZM110](https://openairdocs.org/sdr/97ZZZM110), Jan 2, 1997: ANGLE. CRACKED. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE DORSAL FIN ATTACH ANGLE ON THE LEFT SIDE INBOARD JUST AFT OF FS 1076 WAS FOUND CRACKED. REMOVED 
- [SDR 97ZZZM109](https://openairdocs.org/sdr/97ZZZM109), Jan 2, 1997: SPAR. BLEND OUT. DURING A SCHEDULED INSPECTINO AT AERO CORP IN LAKE CITY, FL THE RT WING LOWER REAR SPAR XRS 80 HAS DEEP BLEND OUT. REWORKED BLEND OUT (ROTO PEENED). ALODINED AN
- [SDR 97ZZZM108](https://openairdocs.org/sdr/97ZZZM108), Jan 2, 1997: ANGLE. CRACKED. DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE CENTER WING UPPER SURFACE FLOOR BEAM LONGITUDINAL SUPPORT AT LBL 44 IS CRACKED FROM FS 650 TO 66
- [SDR 97ZZZM107](https://openairdocs.org/sdr/97ZZZM107), Jan 2, 1997: ANGLE. CRACKED. DURING A SCHEDULED INSPECTION AT AERO CORP IS LAKE CITY, FL THE CENTER WING UPPER SURFACE FLOOR BEAM LONGITUDINAL SUPPORT AT RBL 44 AND FS 650-663 WAS FOUND WIT
- [SDR 96ZZZM70](https://openairdocs.org/sdr/96ZZZM70), Dec 18, 1995: DOOR SWITCH. FAILED. FLT NR 231 - ATL - AIRCRAFT RETURNED AFTER TAKEOFF AND GEAR RETRACTION LEFT GEAR DOOR OPEN LIGHT CAME ON IN FLIGHT. REMOVED AND REPLACED LEFT LANDING GEAR DOOR 
- [SDR 95ZZZM552](https://openairdocs.org/sdr/95ZZZM552), Jul 28, 1995: CONNECTOR. DIRTY. FLT NR 572 - ATL-MCI - RECEIVED AN UNSAFE NOSE GEAR INDICATION AFTER HANDLE WAS LOWERED FOR LANDING. WHEN AIRSPEED REDUCED BELOW 160 KTS FOR APPROACH, NOSE GEAR
- [SDR 95ZZZM253](https://openairdocs.org/sdr/95ZZZM253), Jul 26, 1995: CONNECTOR. LOOSE. FLT 120 - TPA-ATL - ON APPROACH TO ATL DID NOT HAVE GEAR WARNING HORN. FOUND CANNON PLUG LOOSE ON NOSE GEAR UPLOCK SWITCH. CLEANED CANNON PLUG AND SECURED. ALL 
- [SDR 95ZZZX1946](https://openairdocs.org/sdr/95ZZZX1946), Apr 10, 1995: STRUT. FLAT. RDU/ATL - FLT 299 - AIR RETURNED TO RDU DUE TO LANDING GEAR HANDLE WOULD NOT RETRACT, CABIN WOULD NOT PRESSURIZE AND NOSE WHEEL STEERING STILL WORKED. CYCLED GR

## STCs that may be installed (OpenAirDocs) (2)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Garrett TFE731 series)

- [STC SE00648CH](https://openairdocs.org/stc/SE00648CH): Convert AlliedSignal TFE731-3-1E/F/K engines to TFE731-3-2AP engines. International turbine Industries. Lists TFE731-3
- [STC SE1040EA](https://openairdocs.org/stc/SE1040EA): Installation of hydraulically actuated target type thrust reverser system. Northrop Grumman Comm Aircraft Div. Lists TFE731-2

## Related

- Other Dassault-Breguet FALCON 50 aircraft: https://openairdocs.org/model/dassault-breguet-falcon-50/aircraft.md
- The Garrett TFE731 series engine: https://openairdocs.org/engine/garrett-tfe731-series.md

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