# Service difficulty reports: Dassault FALCON 10

A list on [Dassault FALCON 10](https://openairdocs.org/model/dassault-falcon-10.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 134 reports

- [SDR 2022FA0000087](https://openairdocs.org/sdr/2022FA0000087.md): Uplock · malfunctioned · Feb 10, 2022 · N485A · Amd FALCON10 · Landing Gear Retraction/Extension System
  > 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 SCHEDULED DESTINATION WITH NO OTHER ANOMALIES.
- [SDR YBBA201910100001](https://openairdocs.org/sdr/YBBA201910100001.md): Pressure System · malfunctioned · Oct 10, 2019 · N111WH · Amd FALCON10 · Cabin Pressure Control System
  > 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 CLIMB ABOVE APPROXIMATELY 10,000’ THE CABIN RATE BEGAN TO DESCEND AT A RATE OF 1,500 FT/MIN WHEN TH
- [SDR CA190913004](https://openairdocs.org/sdr/CA190913004.md): Anti-Skid Valve · cracked · Aug 9, 2019 · Amd FALCON10 · Brake Anti-Skid Section
  > (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.md): Tire · separated · Jul 7, 2019 · N6FJ · Amd FALCON10 · Tire
  > PIC REPORTED NOISE ON TAKE OFF, LANDED @ KAPA UPON VISUAL INSPECTION FOUND LT OUTBOARD TIRE, THREAD RUBBER SEPARATED FROM CASING, THREAD SEPARATION. MX NOTIFIED FACILITY MX ROUTED TO AIRCRAFT@ KAPA, R&R BOTH LT INBOARD AND OUTBOARD TIRE ASSY, INSPECTED & FUNCT
- [SDR YBBA20181203001](https://openairdocs.org/sdr/YBBA20181203001.md): Glide Slope · false indication · Nov 30, 2018 · N111WH · Amd FALCON10 · Glide Slope System
  > 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 01/15/2018.
- [SDR YBBA2018082702](https://openairdocs.org/sdr/YBBA2018082702.md): Pump · no test · Aug 13, 2018 · N6FJ · Amd FALCON10 · Hydraulic Pump (Electric/Engine), Main
  > 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, CLEANED THREE FILTERS. SERVICED THE SYSTEM AND OPS TESTED, NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO
- [SDR YBB2018F00002](https://openairdocs.org/sdr/YBB2018F00002.md): Fire Loop · failed · Jul 28, 2018 · N6FJ · Amd FALCON10 · Fire Detection
  > 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 DETECTION LOOP PN 30011690040012 SN 71292. INSTALLED SERVICEABLE FIRE LOOP PN 30011690040012 AN 8528
- [SDR YBBA2018082701](https://openairdocs.org/sdr/YBBA2018082701.md): Fire Loop · no test · Jul 28, 2018 · N6FJ · Amd FALCON10 · Fire Detection
  > 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 WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE, IAW AMM 26-10-00.
- [SDR YBB2018F00003](https://openairdocs.org/sdr/YBB2018F00003.md): Fire Loop · failed · Jul 27, 2018 · N6FJ · Amd FALCON10 · Fire Detection
  > 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 LOOP PN 3001-16-900/400-12 SN 71292. INSTALLED SERVICEABLE FIRE LOOP PN 3001-16-900/400-12 SN 85258.
- [SDR 2CJA2018020700003](https://openairdocs.org/sdr/2CJA2018020700003.md): Display · malfunctioned · Feb 7, 2018 · N244A · Amd FALCON10 · Indicating/Recording System
  > 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 TO HUNT UP AND DOWN AND OR - 200 FEET AND THE YOKE STARTED SHAKING RIGHT TO LEFT. CREW SHUT OFF T
- [SDR 2CJA102023917](https://openairdocs.org/sdr/2CJA102023917.md): Engine · power loss · Mar 29, 2017 · N908TF · Amd FALCON10 · Engine (Turbine/Turboprop)
  > 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. DEPARTED. ABOUT 1000 FT OFF THE GROUND THE NR 1 ENGINE STARTED TO SPOOL BACK. IT TOOK MAYBE
- [SDR 4DUA2017031500001](https://openairdocs.org/sdr/4DUA2017031500001.md): Landing Gear · malfunctioned · Mar 12, 2017 · N220C · Amd FALCON10 · Landing Gear Retraction/Extension System
  > LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. NO MOVEMENT, THREE GREEN INDICATED, RETURNED TO FIELD.
- [SDR XVOR2017080900399](https://openairdocs.org/sdr/XVOR2017080900399.md): Hose · deteriorated · Feb 28, 2017 · N528JL · Amd FALCON10 · Airfoil Anti/De-ice System
  > 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 BE PUSHED DOWN STREAM WHICH COULD CAUSE INSUFFICIENT DEICING OF THE WINGS. AD20161907 REQUIRES REPLA
- [SDR CA151022002](https://openairdocs.org/sdr/CA151022002.md): Fan · failed · Aug 11, 2015 · Amd FALCON10 · Air Distribution Fan
  > (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 INSPECTION THE RT EVAPORATOR FAN WAS FOUND SEIZED AND SMELT BURNED. THE FAN WAS REPLACED WITH ANOTHER
- [SDR T6FA2014FA0000502](https://openairdocs.org/sdr/T6FA2014FA0000502.md): Fms · smoke · Aug 6, 2014 · N349JC · Amd FALCON10 · Landing and Taxi Aids
  > ELECTRICAL SMOKE COMING FROM FMS, DIVERTED. REPLACED FMS AND RTS.
- [SDR CA140122008](https://openairdocs.org/sdr/CA140122008.md): Hose · collapsed · Jan 17, 2014 · Amd FALCON10 · Air Intake Anti/De-Ice System
  > (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 WAS FOUND TO BE DE-LAMINATED, RESTRICTING FLOW TO THE SLAT. UPON FURTHER INSPECTION, THE LEFT OTBD S
- [SDR CA130109009](https://openairdocs.org/sdr/CA130109009.md): Hose · collapsed · Jan 4, 2013 · Amd FALCON10 · Airfoil Anti/De-ice System
  > (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 DELAMINATED IN SEVERAL AREAS OF THE INNER LINING.
- [SDR 2012FA0000041](https://openairdocs.org/sdr/2012FA0000041.md): Hose · obstructed · Jan 19, 2012 · N349JC · Amd FALCON10 · Airfoil Anti/De-ice System
  > 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 TEMPERATURE ON THE OTBD SECTION TO BE HALF OF THE OTHER 3 SECTIONS. INSPECTION FOUND THAT THE HOT AIR S
- [SDR 2012FA0000116](https://openairdocs.org/sdr/2012FA0000116.md): Control Unit · failed · Jan 9, 2012 · N106TW · Amd FALCON10 · Brake Anti-Skid Section
  > 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 CONTROL.
- [SDR SFOA20111201001](https://openairdocs.org/sdr/SFOA20111201001.md): Indicator · defective · Dec 1, 2011 · N77SF · Amd FALCON10 · Engine EGT/TIT Indicating System
  > 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 INDICATOR BEGAN TO WORK BUT WAS LOWER THAN NORMAL AND ERRATIC. THE GAUGE WAS PARTIALLY REMOVED FROM TH
- [SDR SFOA20110804001](https://openairdocs.org/sdr/SFOA20110804001.md): Windshield · cracked · Aug 4, 2011 · N77SF · Amd FALCON10 · Flight Compartment Windows
  > AFTER REACHING THIS ALTITUDE THE PILOT’S WINDOW CRACKED IN NUMEROUS PLACES. FOLLOWING FLIGHT MANUAL PROCEDURES, THE CREW SLOWED THE AIRCRAFT TO 230K AND DESCENDED TO AN ALTITUDE WHERE A CABIN DIFFERENTIAL PRESSURE OF 7.5 COULD BE MAINTAINED. THE CREW THEN DE
- [SDR CA110607012](https://openairdocs.org/sdr/CA110607012.md): Fcu · unserviceable · Jun 2, 2011 · Amd FALCON10 · Fuel Control/Turbine Engines
  > 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 DESCENDED TO 30,000 TO RE-LIGHT THE ENGINE. THEY STARTED THE ENGINE WITH NO ISSUES. AFTER INSP, NO FAU
- [SDR SFOA20110317001](https://openairdocs.org/sdr/SFOA20110317001.md): Fuel Control · malfunctioned · Mar 17, 2011 · N77SF · Amd FALCON10 · Fuel Control/Turbine Engines
  > JUST PRIOR TO DESCENT TO SCHEDULED AIRPORT, THE LT ENGINE COMPUTER ANNUNCIATOR ILLUMINATED. FOLLOWING AFM PROCEDURES THE COMPUTER WAS RESET AND THE LIGHT WOULD NOT REMAIN EXTINGUISHED. ALL OTHER ENGINE INDICATIONS WERE NORMAL. A SAFE LANDING WAS MADE. THE
- [SDR SFOA77N2MONO](https://openairdocs.org/sdr/SFOA77N2MONO.md): Monopole · faulty · Mar 7, 2011 · N77SF · Amd FALCON10 · Engine RPM Indicating System
  > AFTER DEPARTURE FROM AIRPORT THE RT ENGINE COMPUTER ANNUNCIATOR ILLUMINATED. FOLLOWING AFM PROCEDURES THE COMPUTER WAS RESET AND THE LIGHT EXTINGUISHED. A SHORT TIME LATER THE ANNUNCIATOR ILLUMINATED AGAIN AND WAS AGAIN RESET. ALL OTHER ENGINE INDICATIONS W
- [SDR 2010FA0000824](https://openairdocs.org/sdr/2010FA0000824.md): Element · defective · Aug 3, 2010 · N700AL · Amd FALCON10 · Lighting System
  > 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 CAUSE: SOLDERED JOINT DEFECTIVE.
- [SDR 2010FA0000710](https://openairdocs.org/sdr/2010FA0000710.md): Wheel · bent · Jul 8, 2010 · N169LS · Amd FALCON10 · Wheel/Ski/Float
  > 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 ONE SIDE AND TIRE SIDEWALL HAD CORD SEPARATION DUE TO TIRE COMPRESSION.
- [SDR CA100701006](https://openairdocs.org/sdr/CA100701006.md): Control Rod · chafed · Jul 1, 2010 · Amd FALCON10 · Rudder Control System
  > (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 SERVICEABLE UNIT AND LINES REPOSITIONED.
- [SDR CA081222007](https://openairdocs.org/sdr/CA081222007.md): Audio Panel · malfunctioned · Dec 19, 2008 · Amd FALCON10 · Audio Integrating System
  > (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 FOUND TO BE THE CAUSE. THE AUDIO WARNING PANEL BOX WAS REPLACED WITH A REPAIRED SERVICEABLE UNIT FR
- [SDR MJN1](https://openairdocs.org/sdr/MJN1.md): Seal · worn · Feb 4, 2008 · N769B · Amd FALCON10 · Pneumatic Distribution System
  > 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 SMELL WAS OBSERVED. WHILE EN ROUTE TO MAINTENANCE FACILITY THE CREW REPORTED HEARING AND FEELING A L
- [SDR UVV2007F00000](https://openairdocs.org/sdr/UVV2007F00000.md): Hose · delaminated · Dec 10, 2007 · N222MU · Amd FALCON10 · Airfoil Anti/De-ice System
  > 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 2005-07-23. IAW REQURIEMENTS OF THE MOST RECENT AD 2007-18-08, THE SLAT ANTI-ICE HOSES BEARING PN FAL 100
- [SDR CA071122001](https://openairdocs.org/sdr/CA071122001.md): Control Handle · inoperative · Nov 16, 2007 · Amd FALCON10 · Landing Gear Selector
  > (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 LANDED AT DEPARTURE AIRPORT. WE INSPECTED THE GEAR IAW THE MM AND CAR 605.88. IT WAS FOUND THAT THE MANU
- [SDR EBVR200700000](https://openairdocs.org/sdr/EBVR200700000.md): Motor · failed · Jun 9, 2007 · N55DG · Amd FALCON10 · Stabilizer Actuator
  > 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.md): Pitot Line · loose · May 9, 2007 · N160FJ · Amd FALCON10 · Pitot/Static System
  > 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 FITTING FOR THE NR 1 STATIC SYSTE. WHEN THE FITTING WAS LOOSENED, FOUND A LAGRE AOUNT OF TEFLON PIPE
- [SDR CA070509003](https://openairdocs.org/sdr/CA070509003.md): Signal Cond Unit · malfunctioned · May 4, 2007 · Amd FALCON10 · Fuel Quantity Indicator
  > (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 REPLACED 7 HOURS PRIOR WITH THE SAME ISSUE. ANOTHER SIGNAL CONDITIONER HAS BEEN INSTALLED AND CALIBRATE
- [SDR THMN4346179](https://openairdocs.org/sdr/THMN4346179.md): Splice Plate · cracked · Apr 10, 2007 · N101HS · Amd FALCON10 · Fuselage Miscellaneous Structure
  > 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.md): Attach Bracket · cracked · Apr 10, 2007 · N101HS · Amd FALCON10 · Fuselage Main, Attach Fittings
  > 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.md): Attach Bracket · cracked · Apr 10, 2007 · N101HS · Amd FALCON10 · Fuselage Main, Attach Fittings
  > 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.md): Coupling · defective · Feb 22, 2007 · N43EC · Amd FALCON10 · Hydraulic System, Main
  > 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 ENGINE AND ONLY ON THE SUCTION LINE. THESE FITTINGS HAVE NO TIME CHANGE REQUIREMENT. WHEN THIS PA
- [SDR CA070314005](https://openairdocs.org/sdr/CA070314005.md): Engine · vibration · Feb 17, 2007 · Amd FALCON10 · Engine (Turbine/Turboprop)
  > (CAN) NR1 ENGINE FAILED, TEMPERATURE SPIKE ABOVE 1000 DEGREES C. AS VIBRATION INCREASED, THEN INDICATIONS (ITT, FIFY N2) DECREASED. N1 TURNED, SECURITY, PULLED FIRE HANDLE. ON ARRIVAL, COULD NOT TURN N1, FOUND OIL AND METAL PIECES IN EXHAUST, ENGINE REMOVED
- [SDR CA061207002](https://openairdocs.org/sdr/CA061207002.md): Window Frame · corroded · Dec 7, 2006 · Amd FALCON10 · Fuselage Main, Structure
  > (CAN) REMOVED FRONT WINDSHIELDS TO COMPLY WITH COCKPIT WINDOW FRAME INSPECTION REQUIREMENT OF THE C2 INSPECTION. FOLLOWING REMOVAL OF PILOT’S WINDSHIELD, SEVERE EXFOLIATION CORROSION WAS FOUND ON LOWER FRAME APPROX. 16 INCHES FROM OUTER RAIL OVER AN 8 INCH WI
- [SDR CA061106011](https://openairdocs.org/sdr/CA061106011.md): Hose · collapsed · Nov 2, 2006 · Amd FALCON10 · Airfoil Anti/De-ice System
  > (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 INNER WALL HAD COLLAPSED. THE HOSE WAS REPLACED AND ALL OTHER SLAT ANTI-ICE HOSES WERE INSPECTED AND F
- [SDR CA060515006](https://openairdocs.org/sdr/CA060515006.md): Fcu · inoperative · May 14, 2006 · Amd FALCON10 · Fuel Control/Turbine Engines
  > (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 ALLOW THE QUADRANT TO DEPLOY THE THRUST REVERSERS. ENGINES WERE GROUND RUN AND FOUND TO BE SERVICE
- [SDR 2006FA0000436](https://openairdocs.org/sdr/2006FA0000436.md): Pump · failed · Apr 5, 2006 · N700FH · Amd FALCON10 · Hydraulic Pump (Electric/Engine), Main
  > 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 DEBRIS, NONE NOTED. INSTALLED SERVICEABLE HYDRAULIC PUMP IN NR 1 POSITION, ALL SYSTEMS FUNCTION N
- [SDR SWIA200616239](https://openairdocs.org/sdr/SWIA200616239.md): Battery Pack · discharged · Feb 2, 2006 · N296SW · Amd FALCON10 · Emergency Lighting
  > ALL 3 FWD BULKHEAD EMERG EXIT LIGHTS. FAIL TO ILLUMINATE. REPLACED FWD BATTERY PACK. OPERATIONAL CHECK GOOD.
- [SDR CA060210003](https://openairdocs.org/sdr/CA060210003.md): Hose · collapsed · Jan 31, 2006 · Amd FALCON10 · Airfoil Anti/De-ice System
  > (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 HOSE WAS FOUND TO BE SLIGHTLY COLAPSED INTERNALLY. ANTI-ICE SYSTEM WAS ACTIVATED 44 TIMES. (TC NR 200
- [SDR CA051209004](https://openairdocs.org/sdr/CA051209004.md): Pump · malfunctioned · Nov 30, 2005 · Amd FALCON10 · Hydraulic Pump (Electric/Engine), Main
  > 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 SYSTEM PRESSURE PUMP HAS BEEN REPLACED, P/N 40053-03, S/NOFF AH-16041A, S/NON AH-16086A. FILTER IN
- [SDR SFO2005F00001](https://openairdocs.org/sdr/SFO2005F00001.md): Pump · failed · Jul 27, 2005 · N77SF · Amd FALCON10 · Hydraulic Pump (Electric/Engine), Main
  > 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 PUMP AND REQUIRED FILTERS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THIS FAILED, OV
- [SDR 2005FA0001255](https://openairdocs.org/sdr/2005FA0001255.md): Shaft · sheared · Jul 14, 2005 · N401JW · Amd FALCON10 · Hydraulic Pump (Electric/Engine), Main
  > WHILE PERFORMING AN ENGINE GROUND OPERATION THE HYDRAULIC PUMP OUTPUT CEASED. A SHEARED PUMP EXTERNAL DRIVE SHAFT WAS DISCOVERED. SYSTEM REGULATION AND RETURN FILTERS AND PUMP HOSES SHOW NO INDICATIONS OF METAL CONTAMINATES. THE PUP STUB SHAFT STILL TURNS B
- [SDR CA050603004](https://openairdocs.org/sdr/CA050603004.md): Servo Valve · leaking · May 29, 2005 · Amd FALCON10 · Steering Unit
  > (CAN) HYDRAULIC LEAK AT NOSE GEAR. HYDRAULIC SERVO VALVE FOUND LEAKING. VALVE REPLACED.
- [SDR CA050603005](https://openairdocs.org/sdr/CA050603005.md): Valve · unserviceable · May 25, 2005 · Amd FALCON10 · Brake Anti-Skid Section
  > (CAN) ON INSPECTION, LT ANTI-SKID VALVE FOUND UNSERVICEABLE. LT ANTI-SKID VALVE REPLACED.

Next page: https://openairdocs.org/model/dassault-falcon-10/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = 'FALCON10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/dassault-falcon-10/reports

---
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.