Dassault FALCON 10

Service difficulty reports · 134

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duckdb -csv -c "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"

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SDR 2022FA0000087Uplock · malfunctionedLEFT 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.Feb 10, 2022 · N485A · Amd FALCON10 · Landing Gear Retraction/Extension SystemSDR YBBA201910100001Pressure System · malfunctionedWHILE 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 THOct 10, 2019 · N111WH · Amd FALCON10 · Cabin Pressure Control SystemSDR CA190913004Anti-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)Aug 9, 2019 · Amd FALCON10 · Brake Anti-Skid SectionSDR YBBA2019070800001Tire · separatedPIC 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 & FUNCTJul 7, 2019 · N6FJ · Amd FALCON10 · TireSDR YBBA20181203001Glide Slope · false indicationPIC 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.Nov 30, 2018 · N111WH · Amd FALCON10 · Glide Slope SystemSDR YBBA2018082702Pump · no testPILOT 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 TOAug 13, 2018 · N6FJ · Amd FALCON10 · Hydraulic Pump (Electric/Engine), MainSDR YBB2018F00002Fire Loop · failedDURING 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 8528Jul 28, 2018 · N6FJ · Amd FALCON10 · Fire DetectionSDR YBBA2018082701Fire Loop · no testDURING 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.Jul 28, 2018 · N6FJ · Amd FALCON10 · Fire DetectionSDR YBB2018F00003Fire Loop · failedDURING 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.Jul 27, 2018 · N6FJ · Amd FALCON10 · Fire DetectionSDR 2CJA2018020700003Display · malfunctionedFLIGHT 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 TFeb 7, 2018 · N244A · Amd FALCON10 · Indicating/Recording SystemSDR 2CJA102023917Engine · power lossAFTER 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 Mar 29, 2017 · N908TF · Amd FALCON10 · Engine (Turbine/Turboprop)SDR 4DUA2017031500001Landing Gear · malfunctionedLANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. NO MOVEMENT, THREE GREEN INDICATED, RETURNED TO FIELD.Mar 12, 2017 · N220C · Amd FALCON10 · Landing Gear Retraction/Extension SystemSDR XVOR2017080900399Hose · deterioratedTHIS 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 REPLAFeb 28, 2017 · N528JL · Amd FALCON10 · Airfoil Anti/De-ice SystemSDR CA151022002Fan · 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 INSPECTION THE RT EVAPORATOR FAN WAS FOUND SEIZED AND SMELT BURNED. THE FAN WAS REPLACED WITH ANOTHER Aug 11, 2015 · Amd FALCON10 · Air Distribution FanSDR T6FA2014FA0000502Fms · smokeELECTRICAL SMOKE COMING FROM FMS, DIVERTED. REPLACED FMS AND RTS.Aug 6, 2014 · N349JC · Amd FALCON10 · Landing and Taxi AidsSDR CA140122008Hose · 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 WAS FOUND TO BE DE-LAMINATED, RESTRICTING FLOW TO THE SLAT. UPON FURTHER INSPECTION, THE LEFT OTBD SJan 17, 2014 · Amd FALCON10 · Air Intake Anti/De-Ice SystemSDR CA130109009Hose · 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 DELAMINATED IN SEVERAL AREAS OF THE INNER LINING.Jan 4, 2013 · Amd FALCON10 · Airfoil Anti/De-ice SystemSDR 2012FA0000041Hose · obstructedPOST 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 SJan 19, 2012 · N349JC · Amd FALCON10 · Airfoil Anti/De-ice SystemSDR 2012FA0000116Control Unit · failedON 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.Jan 9, 2012 · N106TW · Amd FALCON10 · Brake Anti-Skid SectionSDR SFOA20111201001Indicator · defectiveDURING 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 THDec 1, 2011 · N77SF · Amd FALCON10 · Engine EGT/TIT Indicating SystemSDR SFOA20110804001Windshield · crackedAFTER 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 DEAug 4, 2011 · N77SF · Amd FALCON10 · Flight Compartment WindowsSDR CA110607012Fcu · unserviceableACT 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 FAUJun 2, 2011 · Amd FALCON10 · Fuel Control/Turbine EnginesSDR SFOA20110317001Fuel Control · malfunctionedJUST 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 Mar 17, 2011 · N77SF · Amd FALCON10 · Fuel Control/Turbine EnginesSDR SFOA77N2MONOMonopole · faultyAFTER 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 WMar 7, 2011 · N77SF · Amd FALCON10 · Engine RPM Indicating SystemSDR 2010FA0000824Element · defectiveINSTALLED 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.Aug 3, 2010 · N700AL · Amd FALCON10 · Lighting SystemSDR 2010FA0000710Wheel · bentNOSE 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.Jul 8, 2010 · N169LS · Amd FALCON10 · Wheel/Ski/FloatSDR CA100701006Control 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 SERVICEABLE UNIT AND LINES REPOSITIONED.Jul 1, 2010 · Amd FALCON10 · Rudder Control SystemSDR CA081222007Audio 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 FOUND TO BE THE CAUSE. THE AUDIO WARNING PANEL BOX WAS REPLACED WITH A REPAIRED SERVICEABLE UNIT FRDec 19, 2008 · Amd FALCON10 · Audio Integrating SystemSDR MJN1Seal · wornCREW 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 LFeb 4, 2008 · N769B · Amd FALCON10 · Pneumatic Distribution SystemSDR UVV2007F00000Hose · delaminatedTHE 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 100Dec 10, 2007 · N222MU · Amd FALCON10 · Airfoil Anti/De-ice SystemSDR CA071122001Control 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 LANDED AT DEPARTURE AIRPORT. WE INSPECTED THE GEAR IAW THE MM AND CAR 605.88. IT WAS FOUND THAT THE MANUNov 16, 2007 · Amd FALCON10 · Landing Gear SelectorSDR EBVR200700000Motor · failedFAILED NORMAL MOTOR TRAVEL TIME CHECKS. SUSPECT NORMAL MOTOR BRAKE WAS PREVIOUSLY ASSEMBLED INCORRECTLY CAUSING DAMAGE TO MOTOR.Jun 9, 2007 · N55DG · Amd FALCON10 · Stabilizer ActuatorSDR 2007FA0000465Pitot Line · looseWHILE 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 May 9, 2007 · N160FJ · Amd FALCON10 · Pitot/Static SystemSDR CA070509003Signal 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 REPLACED 7 HOURS PRIOR WITH THE SAME ISSUE. ANOTHER SIGNAL CONDITIONER HAS BEEN INSTALLED AND CALIBRATEMay 4, 2007 · Amd FALCON10 · Fuel Quantity IndicatorSDR THMN4346179Splice Plate · crackedSPLICE 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.Apr 10, 2007 · N101HS · Amd FALCON10 · Fuselage Miscellaneous StructureSDR THMN4346177Attach Bracket · crackedLT 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.Apr 10, 2007 · N101HS · Amd FALCON10 · Fuselage Main, Attach FittingsSDR THMN4346176Attach Bracket · crackedRT 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.Apr 10, 2007 · N101HS · Amd FALCON10 · Fuselage Main, Attach FittingsSDR 2007FA0000187Coupling · defectiveTHIS 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 PAFeb 22, 2007 · N43EC · Amd FALCON10 · Hydraulic System, MainSDR CA070314005Engine · vibration(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 Feb 17, 2007 · Amd FALCON10 · Engine (Turbine/Turboprop)SDR CA061207002Window 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 EXFOLIATION CORROSION WAS FOUND ON LOWER FRAME APPROX. 16 INCHES FROM OUTER RAIL OVER AN 8 INCH WIDec 7, 2006 · Amd FALCON10 · Fuselage Main, StructureSDR CA061106011Hose · 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 INNER WALL HAD COLLAPSED. THE HOSE WAS REPLACED AND ALL OTHER SLAT ANTI-ICE HOSES WERE INSPECTED AND FNov 2, 2006 · Amd FALCON10 · Airfoil Anti/De-ice SystemSDR CA060515006Fcu · 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 ALLOW THE QUADRANT TO DEPLOY THE THRUST REVERSERS. ENGINES WERE GROUND RUN AND FOUND TO BE SERVICEMay 14, 2006 · Amd FALCON10 · Fuel Control/Turbine EnginesSDR 2006FA0000436Pump · failedNR 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 NApr 5, 2006 · N700FH · Amd FALCON10 · Hydraulic Pump (Electric/Engine), MainSDR SWIA200616239Battery Pack · dischargedALL 3 FWD BULKHEAD EMERG EXIT LIGHTS. FAIL TO ILLUMINATE. REPLACED FWD BATTERY PACK. OPERATIONAL CHECK GOOD.Feb 2, 2006 · N296SW · Amd FALCON10 · Emergency LightingSDR CA060210003Hose · 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 HOSE WAS FOUND TO BE SLIGHTLY COLAPSED INTERNALLY. ANTI-ICE SYSTEM WAS ACTIVATED 44 TIMES. (TC NR 200Jan 31, 2006 · Amd FALCON10 · Airfoil Anti/De-ice SystemSDR CA051209004Pump · malfunctionedHYD 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 INNov 30, 2005 · Amd FALCON10 · Hydraulic Pump (Electric/Engine), MainSDR SFO2005F00001Pump · failedAFTER 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, OVJul 27, 2005 · N77SF · Amd FALCON10 · Hydraulic Pump (Electric/Engine), MainSDR 2005FA0001255Shaft · shearedWHILE 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 BJul 14, 2005 · N401JW · Amd FALCON10 · Hydraulic Pump (Electric/Engine), MainSDR CA050603004Servo Valve · leaking(CAN) HYDRAULIC LEAK AT NOSE GEAR. HYDRAULIC SERVO VALVE FOUND LEAKING. VALVE REPLACED.May 29, 2005 · Amd FALCON10 · Steering UnitSDR CA050603005Valve · unserviceable(CAN) ON INSPECTION, LT ANTI-SKID VALVE FOUND UNSERVICEABLE. LT ANTI-SKID VALVE REPLACED.May 25, 2005 · Amd FALCON10 · Brake Anti-Skid Section
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