Israel Aircraft Industries 1124

Service difficulty reports · 131

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '1124'
  ORDER BY difficulty_date DESC"

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SDR FJTA201601104811Unknown · smokeTWENTY MINUTES AFTER TAKEOFF AT 39,000 FEET, FLIGHT CREW REPORTED SMOKE IN CABIN & COCKPIT. CREW LANDED WITHOUT FURTHER INCIDENT. INSPECTED THE ACFT & PERFORMED GND OPERATIONAL CHECKS. COULD NOT DUPLICATE PROBLEM. FLIGHT CREW TOOK THE ACFT ON A FUNCTIONAL Jan 9, 2016 · N481NS · Israel 1124 · Air Distribution SystemSDR CA100227006Trunnion · damaged(CAN) AIRCRAFT RETURNED TO BASE REPORTING THAT NO GEAR UP INDICATION AND THAT THE LH MAIN GEAR APPEARED TO HANG DOWN FROM WHEEL WELL. UPON JACKING THE AIRCRAFT TO DO A FUNCTIONAL GEAR SWING WITH EXTERNAL HYDRAULIC POWER IT WAS NOTED THAT THE LH MAIN WAS CONTACMar 12, 2015 · Israel 1124 · Fuselage, Landing Gear Attach FittingsSDR BN5A201521800001Relief Valve · faultyAFTER TAKEOFF CREW REPORTED THE ACFT WOULD NOT PRESSURIZE. CREW SWITCHED AIR SOURCE TO EMER AIR AT WHICH TIME THEY NOTICED A HAZE WITH AN EXHAUST ODOR. RETURNED & UPON TAXI TURN OFF THE PILOT THOUGHT A LITTLE SMOKE MIGHT HAVE COME FROM THE OUTSIDE NOSE LT AFeb 8, 2015 · N349MC · Israel 1124 · Cabin Pressure Control SystemSDR BN5A2014092400001Amplifier · faultyEXPERIENCED AN UN-COMMANDED 400 DECENT BY THE AUTOPILOT. PILOTS ADI TUMBLED 15 DEGREES WITH HEADING & NAV MODE UNRESPONSIVE. CREW DESCENDED ACFT TO FL020. CONTINUED FLIGHT WITHOUT AUTOPILOT TO HOME BASE. R & R THE AUTOPILOT AMPLIFIER PN 522-2900-028 SN 2617Sep 21, 2014 · N300X · Israel 1124 · Autopilot SystemSDR FJTA14064811Unknown · unknownDURING CRUISE AT FL360, THE CABIN LOST PRESSURIZATION. THE CABIN STOPPED CLIMB AT APPROX 10,500 FT & WOULD NOT RESPOND UP OR DOWN FOR THE DURATION OF THE DESCENT TO 10,000 FT AT WHICH POINT THE CABIN DESCENDED WITH THE AIRPLANE UNTIL LANDING. THE CREW DECIDEJun 3, 2014 · N481NS · Israel 1124 · Cabin Pressure Control SystemSDR BN5A2013042300001Pin · bentDURING TAKEOFF MAIN LANDING GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION. DURING TROUBLESHOOTING FOUND BENT AND DAMAGED PINS ON LEFT LANDING GEAR CONNECTOR P217. REMOVED LEFT MLG CONNECTORS P 217 AND INSTALLED NEW PLUG P/N MS3126F20-39S AND MS3126F20-3Apr 12, 2013 · N349MC · Israel 1124 · Landing Gear System WiringSDR BN5A2013031100001Hinge Fitting · crackedC/W AD 89-12-08 STABILIZER AFT SPAR INSPECTION IAW SB 1124-55-020 R2. FOUND CRACK ON LEFT OUTER HINGE LUG UPPER FLANGE ONE INCH FROM TRAILING EDGE TRAVEL THRU TRAILING EDGE.Mar 1, 2013 · N349MC · Israel 1124 · Horizontal Stabilizer StructureSDR 2013F00056Actuator · defectiveON APPROACH TO LANDING FOR RWY 19 THE LANDING GEAR WAS SELECTED DOWN. UPON EXTENSION THE LT MAIN GEAR LIGHT DID NOT ILLUMINATE. SWAPPED LAMPS WITH NO RESOLUTION AND PROCEEDED TO CYCLE THE GEAR SEVERAL TIMES WITH THE SAME RESULTS, STILL NO LT MAIN GEAR LIGHT.Feb 15, 2013 · N335VB · Israel 1124 · Landing Gear ActuatorSDR 2013FA0000089Control Switch · misalignedBLEED AIR CONTROL WAS DIMINISHED DUE TO THE BLEED AIR SELECTOR SWITCH BEING CLOCKED IN THE WRONG POSITION. THE SWITCH POSITION INDICATED "BOTH" WHEN THE SWITCH WAS ACTUALLY IN THE "RIGHT" POSITION.Feb 13, 2013 · N57PT · Israel 1124 · Pneumatic Distribution SystemSDR T8VA20120605001Engine · leakingON DESCENT FLIGHT CREW NOTICED THAT THE LEFT OIL PRESSURE GAUGE WAS GETTING INTO THE YELLOW ARCH AND A FEW MINUTES LATER THE OIL PRESSURE ANNUNCIATOR BEGAN TO FLICKER. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN CHECKLIST TO AVOID DAMAGING THE ENGINE AND LANDED Jun 5, 2012 · N36SF · Israel 1124 · Engine (Turbine/Turboprop)SDR 2012FA0000258Hydraulic Line · corrodedLINE CONNECTED TO NR 2 THRUST REVERSER CONTROL VALVE STOW PORT RUPTURED IN FLIGHT AT A 90 DEGREE BEND, SPRAYING 1.5 PINTS IN THE AFT SECTION OF THE ACFT. INSPECTION OF THE LINE REVEALED A PIN HOLE SIZE FAILURE ON THE OUTER BEND RADIUS OF THE TUBE. FURTHER INMar 21, 2012 · N942WC · Israel 1124 · Hydraulic System, MainSDR T8VA2011F00211Switch · defectiveON APPROACH, LANDING GEAR WAS SELECTED DOWN AND THERE WAS NO INDICATION OF GEAR BEING DOWN AND LOCKED (GREEN LIGHTS). THE GEAR HAD APPEARED TO TO ACT AND SOUND NORMAL DURING EXTENSION. CIRCUIT BREAKERS WERE CHECKED AND THE GEAR WAS CYCLED UP AND INDICATED BOTHOct 13, 2011 · N36SF · Israel 1124 · Landing Gear Position and WarningSDR SSWR2011032900001Frame · crackedTHE FS 174.000 FRAME HAS A 2 INCH CRACK THRU THE INBD FLANGE AND INTO THE WEB LOCATED AT THE FLOOR LINE.Mar 29, 2011 · N50M · Israel 1124 · Fuselage Main, FrameSDR CA110321019Elt · malfunctioned(CAN) DURING PERFORMANCE TESTING THE THE 15 BIT BEACON, ID SHOWED 2DC6000000FFBFF AND COUNTRY CODE SHOWED 366 USA. THE ELT HAD ORIGINALLY BEEN PROGRAMMED FOR A BEACON ID 27878 03274 FFBFF AND COUNTRY CODE OF 316 CANADA. THE UNIT WAS SENT TO A LOCAL AVIONICS SMar 15, 2011 · Israel 1124 · Emergency Locator BeaconSDR T8VA36SF101609O-Ring · leakingLT HYD PRESSURE LOW LIGHT ILLUMINATED, INDICATING HYD PRESSURE BELOW 1400 PSI AT LT ENG DRIVEN HYD PUMP, SYS PRESSURE REMAINED NORMAL AT 2000 PSI, AS CREW MONITORED SYS PRESSURE THE RT HYDR PRESSURE LOW LIGHT ILLUMINATED, CREW AT THIS POINT DIVERTED TO MSP FOROct 16, 2009 · N36SF · Israel 1124 · Hydraulic System, MainSDR CA090810001Hydraulic System · leakingACFT LOST HYD FLUID IN FLIGHT.Aug 8, 2009 · Israel 1124 · Hydraulic System, MainSDR CA081210012Bracket · cracked(CAN) FOUND CRACK IN BRACKET LOCATED ON THE FORWARD SIDE OF THE VERTICAL STAB ATTACH FITTING AT FS 521.75. THREE CRACKS EXTEND FROM THE RIGHT OUTBOARD ATTACHMENT BOLT HOLE. THE ATTACHING BOLTS RUNS HORIZONTALLY FWD AND AFT THROUGH THE RUDDER STOP BRACKET, VDec 8, 2008 · Israel 1124 · Vertical StabilizerSDR WAI2008F00001Planetary Gear · brokenDURING A PREFLIGHT INSPECTION, DISCOVERED NR 2 ENGINE FAN WOULD NOT ROTATE. DISCOVERED PLANETARY GEARSHAFT HAD A MISSINGTOOTH. PERFORMED A 4200 HR. FAN SUPPORT INSPECTION; REPLACED PLANETARY GEARSHAFT; BALANCED FAN ASSY; DRAINED OIL SYSTEM AND REPLACE OIL FILJun 17, 2008 · N211ST · Israel 1124 · Accessory GearboxesSDR 2008FA0000306Oxygen Mask · collapsedDURING AN OPS INSPECTION OF THE PASSENGER OXYGEN DROP DOWN MASKS, THERE WAS ONE THAT WOULD NOT LET OXYGEN FLOW THRU THE CONNECTION BETWEEN THE LARGER LINE ATTACHED TO THE BARBED FITTING ON THE OXYGEN DROP DOWN BOX AND THE SMALLER LINE THAT GOES TO THE MASK. INMay 1, 2008 · Israel 1124 · Passenger Oxygen SystemSDR 2008FA0000308Oxygen Mask · collapsedDURING AN OPS INSPECTION OF THE PASSENGER OXYGEN DROP DOWN MASKS, THERE WAS ONE THAT WOULD NOT LET OXYGEN FLOW THRU THE CONNECTION BETWEEN THE LARGER LINE ATTACHED TO THE BARBED FITTING ON THE OXYGEN DROP DOWN BOX AND THE SMALLER LINE THAT GOES TO THE MASK. INMay 1, 2008 · Israel 1124 · Passenger Oxygen SystemSDR 2008FA0000333Indicator · inoperativePASSENGER OXYGEN MASK FLOW INDICATOR INOPERATIVE. THIS UNIT CAME FROM LOT LC 0521 K OR LOT LC 0526KApr 25, 2008 · N500KE · Israel 1124 · Passenger Oxygen SystemSDR CA071026007Brake Assy · failed(CAN) A-CHECK INSPECTION COMPLETED AT AIRCRAFT. FOLLOWING INSPECTION A TEST FLIGHT WAS COMPLETED, ON RETURN TO BASE, IT WAS NOTED THAT THE RT BRAKE WAS DRAGGING. MAINTENANCE FOUND TOP AFT GRIP AND TUBE OUT OF ADJUSTMENT. REMOVED AND RESET ASSEMBLY TO NEUTRAL POct 18, 2007 · Israel 1124 · Landing Gear Brake SystemSDR CA071026005Actuator · failed(CAN) WHILE PERFORMING AN A-CHECK, THE RUDDER TRIM ACTUATOR (PN: 793500-501) FAILED THE FREE PLAY CHECK IAW MM 5-20-06 PARA: 1.F.(4) AND MM 27-20-00 PAGE 503 PARA: 4.A. A NEW RUDDER TRIM LOWER ACTUATOR (PN: 793500-501) (ALTERNATE PN:1092AS100-3) WAS ORDERED. WOct 16, 2007 · Israel 1124 · Rudder ActuatorSDR 2007FA0000701Rod · cracked(REF CNTRL NR WW1045) RECOVERED AIRCRAFT FROM TAXI WAY AFTER A LANDING WITH NO MLG GREEN LIGHTS. LT GEAR STARTED RETRACTING DURING TAXI. FOUND LT AFT GEAR RETRACT ACTUATOR PISTON ROD BROKEN INSIDE PISTON WHICH HAD CAUSED A MIS-DIRECT OF GEAR DOWN FLOW TO ROJul 9, 2007 · N40TA · Israel 1124 · Landing Gear ActuatorSDR 2007FA0000539Actuator · misalignedINSTALLED REBUILT FLAP ACTUATOR IN RT OB POSITION; PN 1391T1008, SN 387AB. FLAP OPERATION WAS NORMAL. WHILE CHECKING AILERON TRAVELS IT WAS DISCOVERED THAT AILERON TRAVELS WERE LIMITED BY THE REBUILT FLAP ACTUATOR. A COVER PLATE ON THE FLAP ACTUATOR HAD BEEMay 30, 2007 · N27TZ · Israel 1124 · Trailing Edge Flap ActuatorSDR 2007FA0000487Actuator · misalignedINSTALLED REBUILT FLAP ACTUATOR IN RT OB POSITION; PN 1391T100-8, SN 387AB. FLAP OPERATION WAS NORMAL. WHILE CHECKING AILERON TRAVELS IT WAS DISCOVERED THAT AILERON TRAVELS WERE LIMITED BY THE REBUILT FLAP ACTUATOR. A COVER PLATE ON THE FLAP ACTUATOR HAD BEMay 30, 2007 · N27TZ · Israel 1124 · Trailing Edge Flap ActuatorSDR 2007FA0000486Actuator · misalignedINSTALLED REBUILT FLAP ACTUATOR IN RT OB POSITION; PN 1391T100-8, SN 387AB. FLAP OPERATION WAS NORMAL. WHILE CHECKING AILERON TRAVELS IT WAS DISCOVERED THAT AILERON TRAVELS WERE LIMITED BY THE REBUILT FLAP ACTUATOR. A COVER PLATE ON THE FLAP ACTUATOR HAD BEMay 30, 2007 · N27TZ · Israel 1124 · Trailing Edge Flap ActuatorSDR 2007FA0000405Skin · corrodedFOUND SEVERE (PITTING CORROSION) ON BOTH THE LT AND RT SIDES BETWEEN FRAME, STATIONS 184 AND 194 BELOW EMERGENCY ESCAPE DOORS. THIS IS DUE TO WATER LEAKING AROUND THE EMERGENCY ESCAPE DOORS AND SOAKING THE SOUND DAMPENING INSULATION. THE PITTING WAS SO BAD IMay 22, 2007 · N600NY · Israel 1124 · Fuselage Main, Plate/SkinSDR 2007FA0000437Skin · corrodedFOUND SEVERE PITTING CORROSION ON BOTH THE LT AND RT SIDES BETWEEN FRAME STATIONS 184 AND 194 BELOW EMERGENCY ESCAPE DOORS. THIS IS DUE TO WATER LEAKING AROUND THE EMERGENCY ESCAPE DOORS AND SOAKING THE SOUND DAMPENING INSULATION. THE PITTING WAS SO BAD IT CMay 22, 2007 · N600NY · Israel 1124 · Fuselage Main, Plate/SkinSDR 2007FA0000404Skin · corrodedFOUND SEVERE PITTING CORROSION ON BOTH THE LT AND RT SIDES BETWEEN FRAME, STATIONS 184 AND 194 BELOW EMERGENCY ESCAPE DOORS. BELIEVE THIS IS DUE TO WATER LEAKING AROUND THE EMERGENCY ESCAPE DOORS AND SOAKING THE SOUND DAMPENING INSULATION. THE PITTING WAS SOMay 22, 2007 · N600NY · Israel 1124 · Fuselage Main, Plate/SkinSDR 2007F00033Bracket · brokenNOSE DOWNLOCK SWITCH MOUNTING BRACKET BROKEN: REPLACED BRACKET ASSEMBLY, INSTALLED A NEW UNIT PN: 823012-17. SECURITY, LEAK AND FUNCTION CHECKS PERFORMED WITH NO FAULTS FOUND. MAINTENANCE DONE IAW MM CHAPTERS: 29 AND 32. REF: 8130-3 (1/22/98) W.O. 4105-080112Apr 18, 2007 · N890BA · Israel 1124 · Landing Gear Position and WarningSDR 2007F00032Bracket · brokenNOSE DOWNLOCK SWITCH MOUNTING BRACKET BROKEN: REPLACED BRACKET ASSEMBLY, INSTALLED A NEW UNIT PN: 823012-17. SECURITY, LEAK AND FUNCTION CHECKS PERFORMED WITH NO FAULTS FOUND. MAINTENANCE DONE IAW MM CHAPTERS: 29 AND 32. REF: 8130-3 (1/22/98) WO 4105-08011270Apr 18, 2007 · N890BA · Israel 1124 · Landing Gear Position and WarningSDR 2007FA0000107Seal · leakingTHE AIRCRAFT DEPARTED, CLIMBING THROUGH 30000. THE CABIN ALT BEGAN TO CLIMB WITH THE AIRCRAFT. THE PILOTS REQUESTED TO DESCEND. CENTER DECLARED EMERGENCY AND GAVE CREW 12000 FT. AIRCRAFT PRESSURIZED PROPERLY AT THAT ALT. PILOT REQUESTED DEVIATION AND TO HJan 25, 2007 · N300XL · Israel 1124 · Passenger/Crew DoorsSDR GNL2006F00000Hydraulic Line · crackedIN FLIGHT, AC EXPERIENCED A HYD PRESSURE WARNING LIGHT ON THE RT ENGINE HYD PUMP, THEN THE LT ENGINE DRIVEN HYD PUMP. THE LANDING GEAR WAS EXTENDED WITH THE EMERGENCY BLOW DOWN SYSTEM. THE AC LANDED WITH NO OTHER ISSUES. THE AC WAS TOWED FROM THE RUNWAY TO Aug 29, 2006 · N730CA · Israel 1124 · Hydraulic System, MainSDR 2006FA0000266Flex Duct · deterioratedDURING C-CHECK, BY ACCESS OF FUSELAGE REPAIR, IT WAS FOUND THAT FLEXIBLE AIR CONDITIONING DUCTS WERE BADLY DETERIORATED. FOAM ON INSIDE OF DUCTS WERE COMING LOOSE AND SOME OF DUCTS WERE COLLAPSED. THESE DUCTS ARE JUST PLAIN OLD. MFG TIME LIMITS DO NOT COVERFeb 17, 2006 · N290CA · Israel 1124 · Air Distribution SystemSDR CA051110001Cable · frayed(CAN) DURING ROUTINE NLG SERVICING THE FRAYED CABLE WAS NOTICED BETWEEN 2 PULLEYS. ONLY A FEW STRANDS REMAINED INTACT AND THE PROBLEM HAS BEEN THERE FOR QUITE SOMETIME IAW THE PART CONDITION. THE CREW HAD REPORTED THAT THE PLANE HAD A SLIGHT TENDANCY TO GO TNov 8, 2005 · Israel 1124 · Landing Gear Steering SystemSDR CA051101001Tube · ruptured(CAN) ENGINE NACELLE HEAT WOULD NOT TEST PROPERLY ON GROUND. FURTHER TROUBLESHOOTING REVEALED THAT THE BLEED SUPPLY PIPE WAS RUPTERED IN THE BYPASS DUCT AREA. PIPE WAS REPLACED AND SYSTEM WAS GROUND CHECK WITH NO FURTHER FAULTS FOUND.Oct 30, 2005 · Israel 1124 · Air Intake Anti/De-Ice SystemSDR 2005FA0000668O-Ring · defectiveFOLLOWING MAINT TROUBLESHOOTING OF HYD SYS. IT WAS FOUND TO HAVE DEFECTIVE O-RING JUST AFT OF THE HYD RESERVOIR AT A T-FITTING LOCATION. DEFECTIVE O-RING DEPLEATED HYDRAULIC RESERVOIR RUNNING HYDRAULIC SYS OUT OF FLUID. THIS CAUSED THE RT ENGINE DRIVEN HYD Apr 18, 2005 · N711KE · Israel 1124 · Hydraulic System, MainSDR ZN3R425038Bearing · fracturedENGINE RETURNED TO SERVICE CENTER FOLLOWING COMMANDED SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE. DURING INSPECTION A FRACTURED CAGE AND OUTER RACE WAS FOUND ON A FORWARD PLANETARY ROLLER BEARING.Apr 1, 2005 · Israel 1124 · Engine (Turbine/Turboprop)SDR 2005FA0000599Bearing Race · fracturedENGINE RETURNED TO SERVICE CENTER FOLLOWING COMMANDED SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE. DURING INSPECTION A FRACTURED CAGE AND OUTER RACE WAS FOUND ON A FORWARD PLANETARY ROLLER BEARING.Apr 1, 2005 · Israel 1124 · Engine (Turbine/Turboprop)SDR 2005FA0000372Housing · crackedAFTER LANDING, TAXIIED TO REPAIR SERVICE, THE NOSE STRUT BOTTOMS OUT, STOPPED AT RAMP. EXITED AC, NOTED A LARGE PUDDLE OF HYDRAULIC FLUID AROUND NLG. JACKED AC UP, NOTICED THE LARGE CRACK IN THE LOWER STRUT HOUSING, STARTING FROM BACK SIDE OF TORQUE KNEE ATTNov 21, 2004 · N730CA · Israel 1124 · Main Landing Gear Strut/Axle/TruckSDR IXXA0400105OStriker · out of adjustAFTER TAKEOFF FROM PDX, DOOR LIGHT CAME ON DURING GEAR UPLATCH CHECK, GEAR AND DOOR LIGHT REMAINS ON WITH GEAR UP AND LOCKED. CREW RECYCLE GEAR AND NO CHANGE, AND RETURNED BACK TO PDX. MX INSPECTED MAIN GEAR AND FOUND RT GEAR DOOR STRIKER MISSING DOOR SWITCHAug 28, 2004 · N830 · Israel 1124 · Door Warning SystemSDR I262004F00000Switch · stuckFLAPS STUCK IN 12 DEGREE POSITION. FOUND THE NR 2 SWITCH STUCK IN CLOSED POSITION. REPLACED SLIDER ASSY. OPS CHECK GOOD.Jul 9, 2004 · N140VJ · Israel 1124 · Trailing Edge Flap Control SystemSDR 2004FA0000570Shutoff Valve · leakingTHIS VALVE INSTALLED PREVIOUSLY TO COMPLY WITH REQURIEMENTS OF AD 2003-11-07. FOUND DURING INSPECTION THAT VALVE WILL NOT SHUT OFF OXYGEN FLOW WHEN TURNED TO CLOSED. REPLACED VALVE WITH NEW PN 27550-3, THIS CORRECTED PROBLEM.Jun 15, 2004 · N79KP · Israel 1124 · Pneumatic Distribution SystemSDR 2005FA0000460Wire Harness · arcedFOUND WIRE HARNESS CHAFFING AND ARCING IN THE AREA OF THE COCKPIT ENTRANCE OVERHEAD. THIS PROBLEM HAS BEEN ADDRESSED BY SB 1124-24A-154. CONSIDERATION SHOULD BE GIVEN TO MAKE THIS AD. DUE TO POTENTIAL OF IN-FLIGHT SMOKE AND FIRE HAZZARD. (K)May 17, 2004 · N900VP · Israel 1124 · Electrical Power System WiringSDR 705050704Indicator · erraticAIRCRAFT ABORTED TAKEOFF DUE TO A AIRSPEED INDICATION ANOMALY. BRAKES EXPERIENCED AN OVERHEAT.May 4, 2004 · N705AC · Israel 1124 · Airspeed/Mach IndicatorSDR X6U2003F00000Actuator · failedDURING ROUTINE 200 HOUR AIRFRAME INSPECTION, FOUND APPROX 0.125 INCH VERTICAL MOVEMENT OF THE LT AND RT ROD END ADAPTERS. TIE BOLT IS LOOSE AND BENT WHERE IT PASSES THROUGH EACH ADAPTER. ALSO FOUND VERTICAL MOVEMENT OF THE JACKSHAFT THREADS. BOTH ROD ENDS JOct 8, 2003 · N274HM · Israel 1124 · Stabilizer Control SystemSDR N382003F00011Support Bracket · brokenWHILE ON VECTORS FOR A VISUAL RIGHT DOWNWIND TO RUNWAY 01 AT KMKC WE SELECTED GEAR DOWN. NO NOSE GEAR DOWN LIGHT AND GEAR IN TRANS LIGHT STAYED ON. THE GEAR WAS CYCLED ABOUT FOUR TIMES WITH NO CHANGE. WE FOLLOWED THE PROCEDURES OF THE 1124 CHECKLIST AND COUSep 28, 2003 · N163WC · Israel 1124 · Fuselage Miscellaneous StructureSDR 2003FA0000912Line · corrodedBRAKE LINE IS MADE FROM -4 ALUMINUM LINE. CRACK STARTS .2500 INCH FROM FLARED END, AND RUNS APPROX. .3750 INCH LONG LENGTH OF LINE. PROBABLE CAUSE IS FATIGUE OR LINE STRESSED, OR CORROSION.Aug 14, 2003 · N809JC · Israel 1124 · Hydraulic System, MainSDR ZES2003F00002Brake Assy · failedDURING TAKE OFF ROLL FROM DLHA, VIBRATION WAS FELT FROM THE RT MLG. PILOT ABORTED TAKE OFF AND BROUGHT THE AIRCRAFT TO A STOP AT THE END OF THE RUNWAY. SUBSEQUENT INVESTIGATION REVEALED THAT THE RT BRAKE HAD FAILED. REPLACED BRAKE ASSEMBLY WITH AN OVERHAULEAug 8, 2003 · N351C · Israel 1124 · Landing Gear Brake System
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