# Dassault FALCON 900B - Type: Aircraft model (FAA registry) - Registry code: 2730171 - Manufacturer (registry): DASSAULT AVIATION - Model: FALCON 900B - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 3 ยท Turbo-fan - Seats: 12 - Weight class: Up to 12,499 lb - Certification: Not type certificated - Registered aircraft: 10 - Page: https://openairdocs.org/model/dassault-falcon-900b 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. None matched. ## Registered aircraft (10) - [N10AZ](https://openairdocs.org/aircraft/N10AZ): [Anschutz Corp](https://openairdocs.org/faa-owner/ANSCHUTZ%20CORP), [Englewood, CO](https://openairdocs.org/faa-place/CO/Englewood), built 1999, S/N 178 - [N167BD](https://openairdocs.org/aircraft/N167BD): [Jrb Aviation LLC](https://openairdocs.org/faa-owner/JRB%20AVIATION%20LLC), [Nashville, TN](https://openairdocs.org/faa-place/TN/Nashville), built 1998, S/N 174 - [N260RF](https://openairdocs.org/aircraft/N260RF): [Hampton Holdings LLC](https://openairdocs.org/faa-owner/HAMPTON%20HOLDINGS%20LLC), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta), built 1996, S/N 160 - [N595PL](https://openairdocs.org/aircraft/N595PL): [Fly High Inc](https://openairdocs.org/faa-owner/FLY%20HIGH%20INC), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita), built 1994, S/N 97 - [N876MR](https://openairdocs.org/aircraft/N876MR): [Budget Jet LLC](https://openairdocs.org/faa-owner/BUDGET%20JET%20LLC), [Greenville, DE](https://openairdocs.org/faa-place/DE/Greenville), built 1994, S/N 125 - [N886DC](https://openairdocs.org/aircraft/N886DC): [Lcjna Management LLC](https://openairdocs.org/faa-owner/LCJNA%20MANAGEMENT%20LLC), [Leesburg, VA](https://openairdocs.org/faa-place/VA/Leesburg), built 1998, S/N 177 - [N900LJ](https://openairdocs.org/aircraft/N900LJ): [Savage Leasing LLC](https://openairdocs.org/faa-owner/SAVAGE%20LEASING%20LLC), [Lebanon, TN](https://openairdocs.org/faa-place/TN/Lebanon), built 1989, S/N 049 - [N900R](https://openairdocs.org/aircraft/N900R): [Falcons R LLC](https://openairdocs.org/faa-owner/FALCONS%20R%20LLC), [Addison, TX](https://openairdocs.org/faa-place/TX/Addison), built 1998, S/N 171 - [N900UJ](https://openairdocs.org/aircraft/N900UJ): [N900uj LLC](https://openairdocs.org/faa-owner/N900UJ%20LLC), [Miami Beach, FL](https://openairdocs.org/faa-place/FL/Miami%20Beach), built 1999, S/N 173 - [N909PM](https://openairdocs.org/aircraft/N909PM): [Mason Aviation LLC](https://openairdocs.org/faa-owner/MASON%20AVIATION%20LLC), [Aberdeen, WA](https://openairdocs.org/faa-place/WA/Aberdeen), built 1998, S/N 176 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (33) As reported by operators and repair stations, by the model named in the report. - [SDR FSEA202601260005](https://openairdocs.org/sdr/FSEA202601260005), Jan 26, 2026: PCB. BURNED. CLIMBING THROUGH 17K THE CREW NOTICES A BURNING SMELL IN THE COCKPIT, THEY GOT A PITCH FEEL ANNUNCIATOR AND THE SLATS DEPLOYED. THEY DECLARED AN EMERGENCY AND R - [SDR 5DLA2024122700323](https://openairdocs.org/sdr/5DLA2024122700323), Dec 19, 2024: WINGLET. DISTORTED. I NEED TO REPORT ON AN INCIDENT THAT HAPPENED ON DECEMBER 19, 2024 AT APPROXIMATELY 13:30 LOCAL TIME. AIRCRAFT DASSAULT FALCON 900B N24FJ WAS TAXING UP TO THE V - [SDR X42A202501141224](https://openairdocs.org/sdr/X42A202501141224), Dec 1, 2024: FLEX HOSE. LEAKING. DURING CLIMB OUT AFTER TAKEOFF THE SLATS AND FLAPS REMAINED EXTENDED AND FAILED TO RETRACT WHEN SELECTED TO 'CLEAN'. DISCOVERED THE LOSS OF HYDRAULIC SYSTEM 2 P - [SDR 6RNA202408120001](https://openairdocs.org/sdr/6RNA202408120001), Jun 20, 2024: SKIN. CORRODED. LEVEL 3 CORROSION FOUND BEHIND RIGHT PYLON LOWER DRAG ANGLE. - [SDR 9JLA2022100739009](https://openairdocs.org/sdr/9JLA2022100739009), Oct 5, 2022: SEAL. LEAKING. DURING POST-FLIGHT CHECKS THE MAINTENANCE TECH DISCOVERED AN OIL LEAK FROM THE NO3 ENGINE. THE MAINTENANCE PROVIDER FOUND A LIP SEAL ON THE ACCESSORY GEARBOX FO - [SDR 2022F00333](https://openairdocs.org/sdr/2022F00333), Sep 7, 2022: NONE. NONE. UPON LANDING INTO KVNY CREW EXPERIENCED AN INTERMITTENT LOSS OF LEFT SIDE BRAKING FORCE CONSISTENT WITH ANTISKID ACTIVATION. RUNWAY WAS DRY AND CREW WAS APPLYIN - [SDR 9JLA2022080339000](https://openairdocs.org/sdr/9JLA2022080339000), Jul 17, 2022: ANTI-ICE VALVE. FAILED. THE FLIGHT CREW REPORTED THAT THE WING ANTI-ICE VALVE WOULD NOT CLOSE IN FLIGHT. THE BASE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE WING ANTI-ICE VALVE HA - [SDR 2022F00172](https://openairdocs.org/sdr/2022F00172), Mar 30, 2022: LIFE RAFT. LEAKING. AFTER OVERHAUL BY FLIGHTPATH CRS #5FSR433B IT WAS FOUND BY MAINTENANCE THAT THE RAFT WOULDN'T FIT IN IT'S ORIGINAL POSITION. IT HAS BEEN SENT BACK 3 TIMES TO TH - [SDR 9JLA2021100726186](https://openairdocs.org/sdr/9JLA2021100726186), Oct 5, 2021: RELAY. DEFECTIVE. THE MAINTENANCE TEAM REPORTED THE CO-PILOT AVIONICS NOT TURNING OFF WITH MASTER SWITCH. THE MAINTENANCE TEAM TROUBLESHOT AND VERIFIED THAT THE COPILOTS EFIS REL - [SDR 9JLA2021091426172](https://openairdocs.org/sdr/9JLA2021091426172), Sep 9, 2021: ACCUMULATOR. LEAKING. THE FLIGHT CREW REPORTED THAT DURING POST FLIGHT CHECKS HYDRAULIC FLUID WAS FOUND LEAKING FROM GANG DRAIN. THE MAINTENANCE VENDOR DETERMINED THE NO1 HYDRAULIC A - [SDR 9JLA2021090826169](https://openairdocs.org/sdr/9JLA2021090826169), Aug 26, 2021: PRESSURE SWITCH. FAILED. THE FLIGHT CREW REPORTED THAT THE NO3 ENGINE FUEL LIGHT ILLUMINATED IN FLIGHT. NO FUEL LEAKS WERE NOTED ON POST FLIGHT CHECKS. THE MAINTENANCE VENDOR TROUBLESHO - [SDR CJPA2021072600021](https://openairdocs.org/sdr/CJPA2021072600021), Jul 14, 2021: LINE. FAILED. ABOUT 20 MILES FROM LANDING, ATC ISSUED INSTRUCTIONS TO SLOW TO 190 KTS. I USED THE AIRBRAKES TO SLOW, AND WHEN RETRACTING THE AIRBRAKES, THE PM NOTICED THE #2 - [SDR 2021FA0000178](https://openairdocs.org/sdr/2021FA0000178), Jun 15, 2021: POSITION SWITCH. OUT OF ADJUST. AIRCRAFT WAS CLEARED FOR TAKE OFF. TOOK THE RUNWAY, LINED UP, CAME TO A STOP & ADVANCED POWER LEVERS TO TAKE OFF. AS NR 2 ENGINE SPOOLED UP, THERE WAS AN INDICA - [SDR 2019FA0000333](https://openairdocs.org/sdr/2019FA0000333), Oct 8, 2019: BOLT. LOOSE. N404BC, SN 128, LINE CASUALTY AIRCRAFT RETURNED AFTER BECOMING AIRBORNE. THE CREW REPORTED UNABLE TO RETRACT SLATS. INVESTIGATION REVEALED, THE L/H OUT BOARD SL - [SDR PRIA20170725001](https://openairdocs.org/sdr/PRIA20170725001), Jul 24, 2017: WIRE HARNESS. SHORTED. CRUISE ALTITUDE FL410 ENG NR 1 COMPUTER LIGHT ILLUMINATED WITH SLIGHT RPM ROLLBACK. FOLLOWED CHECKLIST, RESETTING COMPUTER. 30 SECONDS LATER REPEAT OCCURRENCE. - [SDR YRJR201707180001](https://openairdocs.org/sdr/YRJR201707180001), Jul 17, 2017: CLAMP. BROKEN. AFTER TAKE OFF, A FIRE WARNING ON THE NR 1 ENGINE ILLUMINATED. AIRCRAFT RETURNED TO AIRPORT. EXAMINATION REVEALED TWO HIGH PRESSURE BLEED AIR CLAMPS HAD FAILED. - [SDR 4DUA201703300001](https://openairdocs.org/sdr/4DUA201703300001), Mar 30, 2017: WARNING LIGHT. ACTIVATED. WHILE DESCENDING FROM FL450, CABIN WARNING LIGHT AND TONE ACTIVATED DUE TO PARTIAL LOSS OF CABIN PRESSURE. CREW DONE MASKS, DECLARED EMERGENCY AND LANDED UNEVEN - [SDR CJPA20170104001](https://openairdocs.org/sdr/CJPA20170104001), Jan 4, 2017: FAN. FAILED. AT FL30, THE PILOT REPORTED SMOKE IN THE COCKPIT. DECLARED AN EMERGENCY AND DIVERTED. NOTICED THE SMOKE WENT AWAY AND AFTER DESCENDING TO FL15, CANCELED THE EME - [SDR 7SSA2015102802](https://openairdocs.org/sdr/7SSA2015102802), Jun 14, 2015: ACCESS DOOR. MISSING. AIRCRAFT DEPARTED AFTER SCHEDULED MX & FLEW TO HOME BASE. WHILE PERFORMING THE POST FLIGHT WALK AROUND THE TECHNICIAN NOTICED THE CTR BELLY FUEL BAY DOOR WAS MI - [SDR YYMA2014F00105](https://openairdocs.org/sdr/YYMA2014F00105), Jun 5, 2014: PROXIMITY SWITCH. FAILED. DURING APPROACH, CREW SELECTED GEAR DOWN AND RECEIVED BOTH MAIN DOOR RED INDICATIONS AND NO GREEN DOWN AND LOCK INDICATIONS. RETURNED TO DEPARTURE AND SELECTED - [SDR EV7A201408220001](https://openairdocs.org/sdr/EV7A201408220001), Nov 1, 2013: DOOR FRAME. CORRODED. CORROSION WAS FOUND AROUND MAIN ENTRY DOOR UPPER OPENING AT FRAME 5 DURING A SCHEDULED 3C, 18 YEAR, AIRFRAME INSPECTION. CORROSION WAS REMOVED AND A FABRICATED - [SDR EV7A2014082200001](https://openairdocs.org/sdr/EV7A2014082200001), Nov 1, 2013: SKIN. CORRODED. CORROSION WAS FOUND ON ALUMINUM SKIN AT FRAME 10 DURING A SCHEDULED 3C, 18 YEAR, AIRFRAME INSPECTION. CORROSION WAS REMOVED, SKIN WAS REPAIRED AND A FABRICATED - [SDR 2011FA0000375](https://openairdocs.org/sdr/2011FA0000375), Jun 10, 2011: FAN. FAILED. WHILE TAXING LIGHT SMOKE ENTERED THE CABIN VIA AIR CONDITIONING DUCTS. - [SDR 2011FA0000357](https://openairdocs.org/sdr/2011FA0000357), Jun 3, 2011: SCREW. WRONG PART. SCREW LISTED IN SEC 5, WHEN INSTALLED, (DEPENDING ON THE LOCATION ON THE PROTECTOR) DO NOT FULLY ENGAGE THE LOCKING DEVICE ON THE NUTPLATE BECAUSE THE LENGTH OF - [SDR 2007FA0000458](https://openairdocs.org/sdr/2007FA0000458), May 2, 2007: FUEL CONTROL. FAULTY. PILOTS REPORTED THAT ENGINE THAT THIS FUEL CONTROL UNIT WAS INSTALLED ON COULD NOT BE CONTROLLED BY NORMAL COMPUTER MODE, AND THAT WHEN THEY WENT TO MANUAL MODE - [SDR CA060116005](https://openairdocs.org/sdr/CA060116005), Jan 3, 2006: COOLING FAN. SEIZED. WHILE ON THE GROUND WITH THE APU RUNNING, SMOKE WAS OBSERVED IN THE CABIN. THE CREW IMMEDIATELY SHUT DOWN THE APU. THE TURBO COOLING FAN WAS FOUND SEIZED. - [SDR 2005FA0001225](https://openairdocs.org/sdr/2005FA0001225), Mar 29, 2005: DUCT. CRACKED. DURING INVESTIGATION OF OIL PRESSURE TRANSMITTER ENGINE NR 1 FOUND HOT AIR LEAK FROM PYLON. AFTER REMOVAL OF PYLON DOOR FOUND BLEED AIR DUCT PROBE TEMPERATURE S - [SDR 2005FA0000210](https://openairdocs.org/sdr/2005FA0000210), Dec 29, 2004: ANTI-ICE VALVE. FAILED. DURING TROUBLESHOOTING FOR (HIGHER THAN NORMAL) GASPER AIR TEMPERATURE, FOUND THE TURBOFAN TURBINE ANIT-ICE VALVE DISASSEMBLED BETWEEN THE VALVE AND THE MOTOR. - [SDR CA050324005](https://openairdocs.org/sdr/CA050324005), Sep 29, 2004: INVERTER. FAILED. (CAN) THE GPWS FAILED IN FLIGHT. THE CONNECTOR PLUG ON THE GPWS INVERTER WAS CLEANED OF MOISTURE AND THE SYSTEM WAS TESTED SERVICEABLE. - [SDR CA050324007](https://openairdocs.org/sdr/CA050324007), Sep 29, 2004: ANTI-ICE VALVE. FAILED. (CAN) DURING DESCENT, THE FLIGHT CREW NOTICED THAT THE NR 1 ENGINE ANTI-ICE VALVE WOULD NOT CLOSE UNLESS POWER WAS REDUCED TO IDLE. THE VALVE WAS REPLACED AND A - [SDR AMCR200400004](https://openairdocs.org/sdr/AMCR200400004), Sep 9, 2004: FUSIBLE PLUG. LEAKING. DURING A PREFLIGHT, FOUND TIRE PRESSURE TO BE DOWN SIGNIFICANTLY. INVESTIGATION FOUND ONE WHEEL FUSE PLUG TO BE LEAKING. WHEN FUSE WAS REMOVED, THERE APPEARED T - [SDR 2004FA0000757](https://openairdocs.org/sdr/2004FA0000757), Aug 18, 2004: PRESSURE SWITCH. LEAKING. APPROX 5-10 MINUTES AFTER TAKEOFF, PILOTS NOTED NR 2 HYDRAULIC SYSTEM LOSING FLUID. SYSTEM CONTINUED TO LOSE FLUID SO NR 2 ENGINE WAS SHUT DOWN AND AIRCRAFT LAN - [SDR AMCR200300007](https://openairdocs.org/sdr/AMCR200300007), Oct 30, 2003: EXTINGUISHER. LEAKING. DURING BASIC INSPECTION, TECHNICIAN FOUND THE COCKPIT FIRE EXTINGUISHER PRESSURE GAUGE TO BE READING AT VERY BOTTOM OF GREEN RANGE. FURTHER INSPECTION REVEALED --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.