# Dassault FALCON 10

- Type: Aircraft model (FAA registry)
- Registry code: 2730166
- Manufacturer (registry): DASSAULT AVIATION
- Model: FALCON 10
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 11
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS A33EU](https://openairdocs.org/tcds/A33EU) (OpenAirDocs)
- Holder: Dassault Aviation
- Registered aircraft: 0
- Page: https://openairdocs.org/model/dassault-falcon-10

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 2010-26-05 R1](https://openairdocs.org/ad/2010-26-05-R1): Air conditioning · Dassault Falcon 10, Fan Jet Falcon, Fan Jet Falcon Series C and 14 more. Effective Dec 6, 2023
- [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 2021-04-20](https://openairdocs.org/ad/2021-04-20): Time Limits/Maintenance Checks · Dassault Falcon 10. Effective Apr 9, 2021
- [AD 2021-03-12](https://openairdocs.org/ad/2021-03-12): Ice and rain protection · Dassault Falcon 10. Effective Mar 31, 2021
- [AD 2020-17-14](https://openairdocs.org/ad/2020-17-14): Flight Controls · Dassault Falcon 10. Effective Oct 8, 2020
- [AD 2016-19-07](https://openairdocs.org/ad/2016-19-07): Ice and Rain Protection · Dassault Falcon 10. Effective Oct 21, 2016
- [AD 2013-25-01](https://openairdocs.org/ad/2013-25-01): Flight controls · Dassault Falcon 10. Effective Dec 24, 2013
- [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 2008-04-14](https://openairdocs.org/ad/2008-04-14): Overwing emergency exit · Dassault Falcon 10, Falcon 900EX, Fan Jet Falcon and 14 more. Effective Apr 1, 2008
- [AD 2005-04-02](https://openairdocs.org/ad/2005-04-02): Airplane flight manual (AFM) · Dassault Falcon 10. Effective Mar 25, 2005
- [AD 2002-13-07](https://openairdocs.org/ad/2002-13-07): Inertial Reference Units (IRU) · Dassault Falcon 10, Falcon 900EX, Fan Jet Falcon and 8 more. Effective Aug 9, 2002
- [AD 2001-13-11](https://openairdocs.org/ad/2001-13-11): Dual Non-return Valves of the Fire Extinguishing System · Dassault Falcon 10. Effective Jul 12, 2001
- [AD 2001-01-05](https://openairdocs.org/ad/2001-01-05): Parking Brake · Dassault Falcon 10, Mystere-Falcon 50, Falcon 10 and 1 more. Effective Feb 22, 2001
- [AD 2000-05-20](https://openairdocs.org/ad/2000-05-20): Passenger Oxygen Masks · Dassault Falcon 10, Falcon 900EX, Fan Jet Falcon and 13 more. Effective Apr 18, 2000
- [AD 97-05-03 R1](https://openairdocs.org/ad/97-05-03-R1): Global Positioning Systems · BAE Systems Avro 146-RJ100A, BAe 146-200A, Jetstream Model 4101 and 27 more. Effective Apr 20, 1999
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 95-22-01](https://openairdocs.org/ad/95-22-01): Fluorescent Lighting System · Aerospace Lighting Fluorescent lighting systems, A310-203, A310-204 and 74 more. Effective Dec 4, 1995
- [AD 90-07-08 R1](https://openairdocs.org/ad/90-07-08-R1): Fluorescent Lighting and Remote Power Units · British Aerospace Regional Jetstream 3201, Jetstream Series 3101, Falcon 10 and 10 more. Effective Jul 2, 1990
- [AD 87-24-10](https://openairdocs.org/ad/87-24-10): Air Conditioning Freon Compressor Motor · Dassault Falcon 10. Effective Dec 29, 1987
- [AD 86-15-06](https://openairdocs.org/ad/86-15-06): Rudder Servo Actuator System · Dassault Falcon 10. Effective Aug 25, 1986
- [AD 86-13-03](https://openairdocs.org/ad/86-13-03): Automatic Leading Edge Slat Extension System · Dassault Falcon 10. Effective Jul 24, 1986
- [AD 84-02-02](https://openairdocs.org/ad/84-02-02): Wing Leading Edge Slat Anti-Icing System · Dassault Falcon 10. Effective Jan 31, 1984
- [AD 83-24-02](https://openairdocs.org/ad/83-24-02): Eexterior Emergency Lighting · Dassault Falcon 10. Effective Dec 23, 1983
- [AD 83-15-02](https://openairdocs.org/ad/83-15-02): Passenger Door Latches · Dassault Falcon 10. Effective Aug 1, 1983
- [AD 82-25-02](https://openairdocs.org/ad/82-25-02): Landing Gear Retraction System · Dassault Falcon 10. Effective Dec 6, 1982
- [AD 81-19-06](https://openairdocs.org/ad/81-19-06): Seat Belt Attachments · Dassault Falcon 10. Effective Oct 14, 1981
- [AD 81-05-02](https://openairdocs.org/ad/81-05-02): Compressor Starting Circuit · Dassault Falcon 10. Effective Mar 2, 1981
- [AD 80-15-04](https://openairdocs.org/ad/80-15-04): Passenger Door Microswitch · Dassault Falcon 10. Effective Aug 11, 1980
- [AD 78-14-02](https://openairdocs.org/ad/78-14-02): Oxygen Pressure · Dassault Falcon 10. Effective Jul 11, 1978
- [AD 78-01-10](https://openairdocs.org/ad/78-01-10): Fire Extinguishing System · Dassault Falcon 10. Effective Jan 19, 1978
- [AD 77-23-04](https://openairdocs.org/ad/77-23-04): Total-Pressure Probes · Dassault Falcon 10. Effective Dec 10, 1977
- [AD 77-15-08](https://openairdocs.org/ad/77-15-08): Pilot or Copilot Seats · Dassault Falcon 10. Effective Aug 22, 1977
- [AD 77-07-09](https://openairdocs.org/ad/77-07-09): Tailpipes · Dassault Falcon 10. Effective Apr 18, 1977
- [AD 76-11-08](https://openairdocs.org/ad/76-11-08): Electrical Power · Dassault Falcon 10. Effective Jun 15, 1976

Historical (superseded or no longer in force):

- [AD 2019-03-27](https://openairdocs.org/ad/2019-03-27) (historical): Ice and rain protection · Dassault Falcon 10. Effective Mar 8, 2019
- [AD 2018-24-03](https://openairdocs.org/ad/2018-24-03) (historical): Time Limits/Maintenance Checks · Dassault Falcon 10. Effective Jan 4, 2019
- [AD 2010-26-05](https://openairdocs.org/ad/2010-26-05) (historical): Air Conditioning · Dassault Falcon 10, Falcon 900EX, Fan Jet Falcon and 14 more. Effective Jan 25, 2011
- [AD 2008-19-08](https://openairdocs.org/ad/2008-19-08) (historical): Airplane flight manual · Dassault Falcon 10. Effective Oct 27, 2008
- [AD 2007-18-08](https://openairdocs.org/ad/2007-18-08) (historical): Airplane flight manual (AFM) · Dassault Falcon 10. Effective Oct 11, 2007
- [AD 2005-18-14](https://openairdocs.org/ad/2005-18-14) (historical): Airplane flight manual (AFM) · Dassault-Aviation Falcon 10. Effective Sep 26, 2005
- [AD 2005-07-23](https://openairdocs.org/ad/2005-07-23) (historical): Airplane flight manual (AFM) · Dassault-Aviation Falcon 10. Effective Apr 26, 2005
- [AD 2000-12-15](https://openairdocs.org/ad/2000-12-15) (historical): Overwing Emergency Exit · Dassault-Aviation Falcon 10, FALCON 2000, Falcon 900EX and 12 more. Effective Jul 20, 2000

## 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 (134, newest 50)

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

- [SDR 2022FA0000087](https://openairdocs.org/sdr/2022FA0000087), Feb 10, 2022: UPLOCK. MALFUNCTIONED. LEFT MAIN LANDING GEAR UNLOCKED IN FLIGHT. PILOT FOLLOWED ABNORMAL PROCEDURES IN AFM AND SLOWED AIRCRAFT TO GEAR DOWN SPEED. EXTENDED GEAR AND LANDED AT SCHEDUL
- [SDR YBBA201910100001](https://openairdocs.org/sdr/YBBA201910100001), Oct 10, 2019: PRESSURE SYSTEM. MALFUNCTIONED. WHILE OPERATING A CFAR 135 REGULATED FLIGHT LEG WITH A DEPARTURE FROM KMSY WITH INTENTIONS TO FLY TO KPHX, THE AIRCRAFT INCURRED A MECHANICAL ISSUE. DURING THE 
- [SDR CA190913004](https://openairdocs.org/sdr/CA190913004), Aug 9, 2019: ANTI-SKID VALVE. CRACKED. (CAN) TROUBLESHOOTING A LEAKING LH MLG ANTI-SKID VALVE THE BODY WAS FOUND CRACKED.. UNIT WAS REPLACED WITH A SERVICEABLE UNIT. (TC# 20190913004)
- [SDR YBBA2019070800001](https://openairdocs.org/sdr/YBBA2019070800001), Jul 7, 2019: TIRE. SEPARATED. PIC REPORTED NOISE ON TAKE OFF, LANDED @ KAPA UPON VISUAL INSPECTION FOUND LT OUTBOARD TIRE, THREAD RUBBER SEPARATED FROM CASING, THREAD SEPARATION. MX NOTIFIED
- [SDR YBBA20181203001](https://openairdocs.org/sdr/YBBA20181203001), Nov 30, 2018: GLIDE SLOPE. FALSE INDICATION. PIC REPORTED #1 GLIDE SCOPE INTERMITTENT DURING DESCENT TO KAPA, DOM NOTIFIED. MX CALLED OUT TO LOCATION. UNIT MEL CAT "C" IAW FACILITY APPROVED MEL DATED 01/15
- [SDR YBBA2018082702](https://openairdocs.org/sdr/YBBA2018082702), Aug 13, 2018: PUMP. NO TEST. PILOT REPORTED THE NR 1 HYD PUMP HAD FAILED AN OPS TEST. REMOVED AND REPLACED THE NR 1 HYDRAULIC PUMP, REPLACED THE RESERVOIR FILTERS, DRAINED SYSTEM FLUID, CLE
- [SDR YBB2018F00002](https://openairdocs.org/sdr/YBB2018F00002), Jul 28, 2018: FIRE LOOP. FAILED. DURING POST FLIGHT OF AIRCRAFT AT FACILITY LOCATED IN KHUM ENG NR 2 FIRE LOOP FAILED OPS TEST. NOTIFIED DOM, DOM GROUNDED AIRCRAFT. REMOVED NR 2 ENGINE FIRE DET
- [SDR YBBA2018082701](https://openairdocs.org/sdr/YBBA2018082701), Jul 28, 2018: FIRE LOOP. NO TEST. DURING A POST FLIGHT OF AIRCRAFT, THE NR 2 ENG FIRE LOOP FAILED AN OPS TEST. GROUNDED THE AIRCRAFT. REMOVED AND REPLACED THE FIRE DETECTION LOOP. OPS CHECKED WI
- [SDR YBB2018F00003](https://openairdocs.org/sdr/YBB2018F00003), Jul 27, 2018: FIRE LOOP. FAILED. DURING POST FLIGHT OF ACFT AT FACILITY LOCATED IN KHUM, ENG NR 2 FIRE LOOP FAILED OPS TEST. NOTIFIED DOM, DOM GROUNDED ACFT. REMOVED NR 2 ENG FIRE DETECTION LOO
- [SDR 2CJA2018020700003](https://openairdocs.org/sdr/2CJA2018020700003), Feb 7, 2018: DISPLAY. MALFUNCTIONED. FLIGHT CREW REPORTED ONE HOUR FROM DESTINATION, DURING CRUISE, PILOT SIDE AIR SPEED DECREASING AND EVENTUALLY WENT TO ZERO. THE AUTO PILOT ALTITUDE HOLD STARTED
- [SDR 2CJA102023917](https://openairdocs.org/sdr/2CJA102023917), Mar 29, 2017: ENGINE. POWER LOSS. AFTER START UP AND TAXI OUT, RUNNING ALL CHECK LISTS, CLEARED FOR TAKE OFF. MONITORED THE ENGINES ON TAKEOFF. HAD NO WARNING LIGHTS AND TAKE OFF POWER WAS SET .
- [SDR 4DUA2017031500001](https://openairdocs.org/sdr/4DUA2017031500001), Mar 12, 2017: LANDING GEAR. MALFUNCTIONED. LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. NO MOVEMENT, THREE GREEN INDICATED, RETURNED TO FIELD.
- [SDR XVOR2017080900399](https://openairdocs.org/sdr/XVOR2017080900399), Feb 28, 2017: HOSE. DETERIORATED. THIS HOSE IS A LIFE LIMITED PART AND THE PART IS BREAKING DOWN IN THE INTERIOR OF THE HOSE WHICH COULD POTENTIALLY ALLOW DETERIORATED SECTIONS TO SEPARATE AND B
- [SDR CA151022002](https://openairdocs.org/sdr/CA151022002), Aug 11, 2015: FAN. FAILED. (CAN) DURING CRUISE, THE CREW NOTICED AND SMELLED SMOKE FROM THE GASPERS. SHUTOFF THE FANS AND THE SMOKE DISAPPEARED. THE ACFT LANDED WITH NO ISSUES. AFTER INSP
- [SDR T6FA2014FA0000502](https://openairdocs.org/sdr/T6FA2014FA0000502), Aug 6, 2014: FMS. SMOKE. ELECTRICAL SMOKE COMING FROM FMS, DIVERTED. REPLACED FMS AND RTS.
- [SDR CA140122008](https://openairdocs.org/sdr/CA140122008), Jan 17, 2014: HOSE. COLLAPSED. (CAN) DURING DESCENT, THE CREW NOTICED THAT THE LT INBD SLAT WAS NOT SHEDDING ICE. THE ANTI-ICE FLEX HOSE FOR THE LT INBD SLAT WAS REMOVED AND THE INNER LINING 
- [SDR CA130109009](https://openairdocs.org/sdr/CA130109009), Jan 4, 2013: HOSE. COLLAPSED. (CAN) DURING CRUISE FLIGHT, THE CREW NOTICED THAT THE LT INBD SLAT WAS NOT SHEDDING ICE. THE ANTI-ICE FLEX HOSE FOR THE LT INBD SLAT WAS REMOVED AND FOUND TO BE
- [SDR 2012FA0000041](https://openairdocs.org/sdr/2012FA0000041), Jan 19, 2012: HOSE. OBSTRUCTED. POST FLIGHT INSP REVELED ICE BUILD UP ON LT OTBD WING SLAT. PERFORMED ACFT RUN-UP TO TEST THE SLAT ANTI-ICE SYS AND USING A TEMPERATURE GUN FOUND THE SLAT TEMPE
- [SDR 2012FA0000116](https://openairdocs.org/sdr/2012FA0000116), Jan 9, 2012: CONTROL UNIT. FAILED. ON LANDING, ANTI-SKID CONTROL RELEASED LEFT BRAKES CAUSING ACFT TO PULL TO THE RIGHT ON THE RUNWAY. FAILURE OF THE ANTI-SKID CONTROL UNIT. REPLACE ANTI-SKID CON
- [SDR SFOA20111201001](https://openairdocs.org/sdr/SFOA20111201001), Dec 1, 2011: INDICATOR. DEFECTIVE. DURING CRUISE FLIGHT THE NR 1 ITT INDICATOR WENT TO ZERO. THE AIRCRAFT RETURNED TO HOME BASE WHERE AN UNEVENTFUL LANDING WAS MADE, DURING RETURN FLIGHT THE INDI
- [SDR SFOA20110804001](https://openairdocs.org/sdr/SFOA20110804001), Aug 4, 2011: WINDSHIELD. CRACKED. AFTER REACHING THIS ALTITUDE THE PILOT’S WINDOW CRACKED IN NUMEROUS PLACES. FOLLOWING FLIGHT MANUAL PROCEDURES, THE CREW SLOWED THE AIRCRAFT TO 230K AND DESCEND
- [SDR CA110607012](https://openairdocs.org/sdr/CA110607012), Jun 2, 2011: FCU. UNSERVICEABLE. ACT WAS AT 35,000 FT WHEN THE CREW NOTICED THE NR 2 ENGINE WAS SHUTTING DOWN. THE WAS NO ANNUNCIATORS TO GIVE THE CREW NOTICE OF POSSIBLE FUEL LOSS. THE CREW DE
- [SDR SFOA20110317001](https://openairdocs.org/sdr/SFOA20110317001), Mar 17, 2011: FUEL CONTROL. MALFUNCTIONED. JUST PRIOR TO DESCENT TO SCHEDULED AIRPORT, THE LT ENGINE COMPUTER ANNUNCIATOR ILLUMINATED. FOLLOWING AFM PROCEDURES THE COMPUTER WAS RESET AND THE LIGHT WOULD 
- [SDR SFOA77N2MONO](https://openairdocs.org/sdr/SFOA77N2MONO), Mar 7, 2011: MONOPOLE. FAULTY. AFTER DEPARTURE FROM AIRPORT THE RT ENGINE COMPUTER ANNUNCIATOR ILLUMINATED. FOLLOWING AFM PROCEDURES THE COMPUTER WAS RESET AND THE LIGHT EXTINGUISHED. A SHORT
- [SDR 2010FA0000824](https://openairdocs.org/sdr/2010FA0000824), Aug 3, 2010: ELEMENT. DEFECTIVE. INSTALLED A NEW LAMP PN Q4581 ON ACFT. ACFT MADE (1) LANDING AFTER THE INSTALLATION AND THE ELEMENT FELL OUT OF ITS SOLDERED LOCATION INSIDE THE GLOBE. PROBABLE
- [SDR 2010FA0000710](https://openairdocs.org/sdr/2010FA0000710), Jul 8, 2010: WHEEL. BENT. NOSE WHEEL AND TIRE SEPARATED FROM ACFT AFTER ROTATION AT APPROX 20 FEET IN AIR. PILOT HEARD A "THUD" AT ROTATION AND SUSPECT ENCOUNTER WITH FOD. WHEEL BENT ON 
- [SDR CA100701006](https://openairdocs.org/sdr/CA100701006), Jul 1, 2010: CONTROL ROD. CHAFED. (CAN) DURING A SCHEDULED INSP, THE RUDDER NON ADJUSTABLE ROD WAS FOUND CHAFING AGAINST A STAINLESS STEEL BRAIDED HYDR LINE AT ZONE 324. ROD REPLACED WITH SERVIC
- [SDR CA081222007](https://openairdocs.org/sdr/CA081222007), Dec 19, 2008: AUDIO PANEL. MALFUNCTIONED. (CAN) DURING THE BASIC INSPECTION WITH AIRCRAFT POWER ON, FUMES AND LIGHT SMOKE WHERE NOTICED IN THE COCKPIT. AFTER INSPECTION THE AUDIO WARNING PANEL BOX WAS F
- [SDR MJN1](https://openairdocs.org/sdr/MJN1), Feb 4, 2008: SEAL. WORN. CREW REPORTED SMOKE IN CABIN, FOLLOWED PROCEDURES TO CLEAR SMOKE AND ISOLATED POWER TO MEDICAL EUIPMENT BELIEVING THAT WAS THE SOURCE. NO ADDITIONAL SMOKE OR SM
- [SDR UVV2007F00000](https://openairdocs.org/sdr/UVV2007F00000), Dec 10, 2007: HOSE. DELAMINATED. THE LT OB SLAT ANTIICING HOSE (PN FAL 1007) WAS INSTALLED ON 9/8/2005 WHILE COMPLYING WITH AD 2005-07-23 AND SB F10-313. AD 2007-18-08 HAS SUPERSEDED AD 2005-07
- [SDR CA071122001](https://openairdocs.org/sdr/CA071122001), Nov 16, 2007: CONTROL HANDLE. INOPERATIVE. (CAN) DURING THE CLIMB, THE LT MAIN LANDING GEAR INTRANSIT STAYED ON DURING GEAR RETRACTION. THE CREW FLEW BACK TO DEPARTURE WITH THE GEAR DOWN. AFTER THEY LAND
- [SDR EBVR200700000](https://openairdocs.org/sdr/EBVR200700000), Jun 9, 2007: MOTOR. FAILED. FAILED NORMAL MOTOR TRAVEL TIME CHECKS. SUSPECT NORMAL MOTOR BRAKE WAS PREVIOUSLY ASSEMBLED INCORRECTLY CAUSING DAMAGE TO MOTOR.
- [SDR 2007FA0000465](https://openairdocs.org/sdr/2007FA0000465), May 9, 2007: PITOT LINE. LOOSE. WHILE TROUBLESHOOTING A LEAK IN NR 2 STATIC SYSTEM, THE RT SIDE STATIC PLATE HAD TO BE TAKEN LOOSE. UPON REMOVAL OF THE PLATE, SILICONE RTV WAS FOUND ON THE FIT
- [SDR CA070509003](https://openairdocs.org/sdr/CA070509003), May 4, 2007: SIGNAL COND UNIT. MALFUNCTIONED. (CAN) IN FLIGHT, ON THE WAY BACK TO BASE THE CREW NOTICED THE RT FUEL GAUGE WAS INTERMITTENT AND NOT WORKING MOST OF THE TIME. THE DEFECTIVE PART WAS JUST REPLA
- [SDR THMN4346179](https://openairdocs.org/sdr/THMN4346179), Apr 10, 2007: SPLICE PLATE. CRACKED. SPLICE PLATE ON RT SIDE OF CABIN AT FRAME 13 JUST BELOW WINDOW LINE CRACKED. MADE AIRWORTHY REPAIR IAW SRM 51-00-01 FIG. 201 AND 51-40-11.
- [SDR THMN4346177](https://openairdocs.org/sdr/THMN4346177), Apr 10, 2007: ATTACH BRACKET. CRACKED. LT NOSE LANDING GEAR DOOR ATTACH POINT IN THE LT NOSE COMPARTMENT HAS 2 EA CRACKS AT FRAME C. MADE AIRWORTHY REPAIR IAW SRM 51-20-02-0, 51-40-11, AND 51-40-13.
- [SDR THMN4346176](https://openairdocs.org/sdr/THMN4346176), Apr 10, 2007: ATTACH BRACKET. CRACKED. RT NOSE LANDING GEAR DOOR ATTACH POINT IN THE RT NOSE COMPARTMENT HAS 2 EA CRACKS AT FRAME C. MADE AIRWORTHY REPAIR IAW SRM 51-20-02-0, 51-40-11, AND 51-40-13.
- [SDR 2007FA0000187](https://openairdocs.org/sdr/2007FA0000187), Feb 22, 2007: COUPLING. DEFECTIVE. THIS COUPLING IS A QUICK-DISCONNECT TYPE FITTING THAT IS IN LINE OF THE ENGINE DRIVEN HYDRAULIC PUMP AND LOCATED IN THE ENGINE PYLON. THERE IS ONLY ONE ON EACH 
- [SDR CA070314005](https://openairdocs.org/sdr/CA070314005), Feb 17, 2007: ENGINE. VIBRATION. (CAN) NR1 ENGINE FAILED, TEMPERATURE SPIKE ABOVE 1000 DEGREES C. AS VIBRATION INCREASED, THEN INDICATIONS (ITT, FIFY N2) DECREASED. N1 TURNED, SECURITY, PULLED 
- [SDR CA061207002](https://openairdocs.org/sdr/CA061207002), Dec 7, 2006: WINDOW FRAME. CORRODED. (CAN) REMOVED FRONT WINDSHIELDS TO COMPLY WITH COCKPIT WINDOW FRAME INSPECTION REQUIREMENT OF THE C2 INSPECTION. FOLLOWING REMOVAL OF PILOT’S WINDSHIELD, SEVERE
- [SDR CA061106011](https://openairdocs.org/sdr/CA061106011), Nov 2, 2006: HOSE. COLLAPSED. (CAN) AFTER LANDING THE PILOTS NOTICED THAT THE LT IB SLAT HAD A SMALL TRACE OF ICE FORMED. AFTER INSPECTION IT WAS FOUND THAT THE LT IB SLAT ANTI-ICE HOSE INNE
- [SDR CA060515006](https://openairdocs.org/sdr/CA060515006), May 14, 2006: FCU. INOPERATIVE. (CAN) UPON RIGGING OF FCU, LOW IDLE STOPS ON THE THROTTLE QUADRANT WERE ADJUSTED TO ACHIEVE DESIRED 20 DEGREES ON THE FCU. THIS ADJUSTMENT WOULD NOT PHYSICALLY 
- [SDR 2006FA0000436](https://openairdocs.org/sdr/2006FA0000436), Apr 5, 2006: PUMP. FAILED. NR 1 HYDRAULIC PUMP FAILED ON TAKEOFF ROLL. REMOVED PUMP AND INSPECTED BUT FOUND NO OBVIOUS PHYSICAL DEFECTS. REMOVED HYDRAULIC SYSTEM FILTER AND INSPECTED FOR 
- [SDR SWIA200616239](https://openairdocs.org/sdr/SWIA200616239), Feb 2, 2006: BATTERY PACK. DISCHARGED. ALL 3 FWD BULKHEAD EMERG EXIT LIGHTS. FAIL TO ILLUMINATE. REPLACED FWD BATTERY PACK. OPERATIONAL CHECK GOOD.
- [SDR CA060210003](https://openairdocs.org/sdr/CA060210003), Jan 31, 2006: HOSE. COLLAPSED. (CAN) DURING APPROACH THE FLIGHT CREW NOTICED THAT THE RT OB SLAT WAS NOT SHEDDING ICE WITH THE WING ANTI-ICE ACTIVATED. UPON INSPECTION THE RT OB SLAT FLEX HOS
- [SDR CA051209004](https://openairdocs.org/sdr/CA051209004), Nov 30, 2005: PUMP. MALFUNCTIONED. HYD NR 1 ANNUNCIATOR ILLUMINATED AFTER TAKEOFF. HYDRAULIC PRESSURE WAS LOST ON SYSTEM 1. QUANTITY WAS SUFFICIENT AND STANDBY SYSTEM WORKED NORMALLY. HYD NR 1 SY
- [SDR SFO2005F00001](https://openairdocs.org/sdr/SFO2005F00001), Jul 27, 2005: PUMP. FAILED. AFTER LANDING, THE NR 2 HYDRAULIC LIGHT CAME ON AND THE NR 2 HYDRAULIC PRESSURE WENT TO -0- PSI. INVESTIGATION REVEALED THE NR 2 HYDRAULIC PUMP HAD FAILED. THE 
- [SDR 2005FA0001255](https://openairdocs.org/sdr/2005FA0001255), Jul 14, 2005: SHAFT. SHEARED. WHILE PERFORMING AN ENGINE GROUND OPERATION THE HYDRAULIC PUMP OUTPUT CEASED. A SHEARED PUMP EXTERNAL DRIVE SHAFT WAS DISCOVERED. SYSTEM REGULATION AND RETURN F
- [SDR CA050603004](https://openairdocs.org/sdr/CA050603004), May 29, 2005: SERVO VALVE. LEAKING. (CAN) HYDRAULIC LEAK AT NOSE GEAR. HYDRAULIC SERVO VALVE FOUND LEAKING. VALVE REPLACED.
- [SDR CA050603005](https://openairdocs.org/sdr/CA050603005), May 25, 2005: VALVE. UNSERVICEABLE. (CAN) ON INSPECTION, LT ANTI-SKID VALVE FOUND UNSERVICEABLE. LT ANTI-SKID VALVE REPLACED.

All 134: https://openairdocs.org/model/dassault-falcon-10/reports.md

## STCs that may be installed (OpenAirDocs) (230, 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 SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [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 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 ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings 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 ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine
- [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC SA1223CE](https://openairdocs.org/stc/SA1223CE): Install King KFC-300 dual flight director flight control system(Category I configuration). Honeywell International Inc
- [STC SA1224CE](https://openairdocs.org/stc/SA1224CE): Installation of King KFC-300 dual flight director flight control system (Category II configuration). Honeywell International 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 ST00652SE](https://openairdocs.org/stc/ST00652SE): Installation of emergency medical stretcher and base, oxygen and electrical systems. 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 ST02395CH](https://openairdocs.org/stc/ST02395CH): Install air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed
- [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 ST00373BO](https://openairdocs.org/stc/ST00373BO): Installation of Rockwell Collins TDR-94D Transponders with ADS-B Out. Pro Star Aviation, LLC
- [STC SA2217SW](https://openairdocs.org/stc/SA2217SW): Installation of Collins Dual FD-109 Y and Z Flight Directors and associated sensors for Category II operation. Textron Aviation Inc
- [STC SA2218SW](https://openairdocs.org/stc/SA2218SW): Installation of single Collins NCS-31 Area Navigation System with mechanical back-up controls. Textron Aviation Inc
- [STC SA2219SW](https://openairdocs.org/stc/SA2219SW): Installation of Intercontinental Dynamics Corporation Servo/Pneumatic, Pneumatic, Flight Instruments. Textron Aviation Inc
- [STC SA2221SW](https://openairdocs.org/stc/SA2221SW): Revision of existing Inverter Control System. Textron Aviation Inc
- [STC SA2222SW](https://openairdocs.org/stc/SA2222SW): Installation of additional nose cone mounted landing lights. Textron Aviation Inc
- [STC SA2223SW](https://openairdocs.org/stc/SA2223SW): Installation of wing inspection lights. Textron Aviation Inc
- [STC SA2224SW](https://openairdocs.org/stc/SA2224SW): Installation of Long Range/RNAV System. Textron Aviation Inc
- [STC SA2227SW](https://openairdocs.org/stc/SA2227SW): Installation of Canadian Marconi CMA-730 Engine and Fuel Quantity Instrumentation. Textron Aviation Inc
- [STC SA2228SW](https://openairdocs.org/stc/SA2228SW): Installation of Fairchild Flight Data Recorder and Collins Cockpit Voice Recorder. Textron Aviation Inc
- [STC SA2301SW](https://openairdocs.org/stc/SA2301SW): Modification of Dassault installed main cabin door counterbalance system. Textron Aviation Inc
- [STC ST02632LA](https://openairdocs.org/stc/ST02632LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out and optionally install ACSS NXG-900 GPS as a position source for ADS-B Out. Aviation Communications and Surveillance Systems
- [STC ST02609LA](https://openairdocs.org/stc/ST02609LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA2225SW](https://openairdocs.org/stc/SA2225SW): Passenger compartment interior. Textron Aviation Inc
- [STC SA2226SW](https://openairdocs.org/stc/SA2226SW): Pressurization of nose cone to improve avionics reliability. Textron Aviation Inc
- [STC SA3650SW](https://openairdocs.org/stc/SA3650SW): Installation of No. 2 Global GNS-500A, Series 4, VLF/Omega Navigation System. Textron Aviation Inc
- [STC SA3651SW](https://openairdocs.org/stc/SA3651SW): Installation of Lockheed flight data recorder, Model 650/1/14040/001. Textron Aviation Inc
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST04273AT](https://openairdocs.org/stc/ST04273AT): Replace Original Main Battery Connector with Concorde Connector, Part Number 4000. Concorde Battery Corporation
- [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc
- [STC ST00800DE](https://openairdocs.org/stc/ST00800DE): Modification of a TCAS II system installation to Change 7.1. West Star Aviation Inc
- [STC ST00774LA](https://openairdocs.org/stc/ST00774LA): Installation of Two Concorde Battery Model No. RG-390E Batteries. Concorde Battery Corporation
- [STC ST01474WI-D](https://openairdocs.org/stc/ST01474WI-D): Modication of a Rockwell Collins Weather Radar System installation. Rockwell Collins Inc
- [STC SA2846WE](https://openairdocs.org/stc/SA2846WE): Installation of Hoskins Pulstar Twilight Supplemental Lighting System in accordance with FAA sealed Hoskins Top Drawing No. 10-202864. BF Goodrich Aerospace
- [STC ST01202WI-D](https://openairdocs.org/stc/ST01202WI-D): Modification of an existing FAA approved Collins TPR-720, TPR-900 or TPR-901 Mode S transponder installation in Part 25 Aircraft using Collins Drawing Index as listed on AML No. ST01202WI-D, latest FAA approved revision. Rockwell Collins Inc
- [STC ST00673WI-D](https://openairdocs.org/stc/ST00673WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation. Rockwell Collins Inc
- [STC ST00682WI-D](https://openairdocs.org/stc/ST00682WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation in accordance with Collins Installation Instructions as listed on AML No. ST00682WI-D, Revision -, or later FAA approved revisions. Rockwell Collins Inc
- [STC ST00632WI-D](https://openairdocs.org/stc/ST00632WI-D): Installation of an Allied Signal MK VI GPWS System. Duncan Aviation Inc
- [STC ST01131WI-D](https://openairdocs.org/stc/ST01131WI-D): Installation of Honeywell MK-VIII Enhanced Ground Proximity Warning System (EGPWS). Duncan Aviation Inc
- [STC ST02760CH](https://openairdocs.org/stc/ST02760CH): Installation of a single Universal Avionics Systems Corporation UNS-1Lw Flight Management System and an LP/LPV Monitor. Elliott Aviation Technical Products

All 230: https://openairdocs.org/model/dassault-falcon-10/stcs.md

## The same model under other registry codes

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

- [Dassault-Breguet FALCON 10](https://openairdocs.org/model/dassault-breguet-falcon-10): 56 registered aircraft, registry code 2730101
- [Avion Marcel Dassault Breguet FALCON 10](https://openairdocs.org/model/avion-marcel-dassault-breguet-falcon-10): 2 registered aircraft, registry code 2730122
- [Avions Marcel Dassault Breguet FALCON 10](https://openairdocs.org/model/avions-marcel-dassault-breguet-falcon-10): 1 registered aircraft, registry code 2730114

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