Israel Aircraft Industries 1124A

Service difficulty reports · 39

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

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SDR 9LVA202412180001Pump · leakingLH AND RH HYDRAULIC LOW PRESSURE INDICATORS ILLUMINATED IN CRUISE FLIGHT, MAIN PRESSURE INDICATED ZERO PSI. MAINTENANCE OBSERVED LOW HYDRAULIC FLUID LEVEL CAUSED BY LEAK ON RH MAIN HYDRAULIC PUMP. REPLACED RH MAIN HYDRAULIC PUMP, SERVICED RESERVOIR AND CW OPERDec 18, 2024 · N22AV · Israel 1124A · Hydraulic Pump (Electric/Engine), MainSDR 9LVA202211190001Flap System · faultedON APPROACH INTO KJAC, SELECTED FLAPS 12, FLAPS OPERATED NORMALLY TO 12 DEGREE POSITION. UPON REACHING 12 DEGREES, FLAPS UNBALANCE INDICATOR ILLUMINATED AND FLAPS WOULD NOT MOVE FROM 12 DEGREE POSITION. DISCONTINUED APPROACH AND RAN CHECKLIST. UNABLE TO RESET Nov 19, 2022 · N241CT · Israel 1124A · Trailing Edge Flap Control SystemSDR 9LVA2021072100100Acm · seizedON APPROACH TO KFTW, CREW NOTED A PRESSURIZATION BUMP AND THEN AN ODOR OF SMOKE THROUGH THE COCKPIT VENTS. CREW SELECTED BLEED TO 'RAM' AND SMELL SUBSIDED. MAINTENANCE TECHNICIANS GAINED ACCESS TO ACM COOLING TURBINE AND FOUND TURBINE SEIZED. ACM REPLACED IAW Jul 21, 2021 · N22AV · Israel 1124A · Cabin Cooling SystemSDR 2017F00137Not Reported · malfunctionedTHE FLIGHT OF THE MORNING OF THE 26TH OF AUGUST, AFTER DEPARTURE THE CREW NOTICED THE IN TRANSIT WARNING LIGHT ON THE GEAR WAS STILL ILLUMINATED. AFTER A LOW PASS INFRONT OF THE CONTROL TOWER IT WAS CONFIRMED THE NOSE GEAR WAS IN THE DOWN POSITION STILL. CREW Aug 26, 2017 · N911GU · Israel 1124A · Landing Gear Retraction/Extension SystemSDR 2017F00131Engine · failedENGINE FAILURE DURING CLIMB OUT. ALL INDICATIONS NORMAL CLIMB, HEARD A LOUD NOISE AND SEVERE VIBRATION FROM THE NR 1 ENGINE, FUEL CONTROLLER WENT TO MANUAL, REDUCED ENGINE SETTINGS TO HALF OF NORMAL IN VIEW OF CONTINUED VIBRATION. ENGINE SECURED USING CHECK LJun 15, 2017 · N57BE · Israel 1124A · Engine (Turbine/Turboprop)SDR T4BA20120301440Actuator · leakingAFTER LANDING; DURING TAXI THE PILOT NOTICED THE BRAKES AND STEERING ERRATIC. FOR SAFETY, HE SHUT DOWN THE ENGINES ON THE TAXI WAY AND INVESTIGATED. PILOT FOUND A LARGE HYDRAULIC SPILL BY THE RT GEAR. THE AIRCRAFT WAS TOWED BACK TO THE HANGAR. MAINTENANCE DFeb 25, 2012 · N30GF · Israel 1124A · Drag Control ActuatorSDR 2010FA0000007Vane · brokenRT NR 3 FLAP VANE DEPARTED ACFT IN OR AROUND 12/6/2009. ACFT LANDED AND CREW DISCOVERED THAT THE FLAP VANE BROKE OFF OF THE FLAP AT THE BOLT HEAD OF THE ATTACHING BRACKET.Dec 10, 2009 · N788FS · Israel 1124A · Trailing Edge FlapsSDR 2010FA0000026Vane · brokenACFT WAS ARRIVING OR DEPARTING WHEN RT FLAP VANE BROKE OFF. THE AREA SUSPECTED WAS THE RT HINGE OF THE FLAP VANE THAT ATTACHES TO L/E OF THE FLAP AT THE ATTACHING HARDWARE.Dec 9, 2009 · N788FS · Israel 1124A · Trailing Edge FlapsSDR 2008FA0000502Amplifier · inoperativeAFTER (1) HOUR DISENGAGES AUTOPILOT. PRELIMINARY INSPECTION RESULTS, NO DEFECTS NOTED AFTER BENCH CHECK. (K)Jul 18, 2008 · N818JH · Israel 1124A · Auto Flight SystemSDR JM02007F00000Tube · leakingAPPROX 2 MINUTES AFTER THE LANDING GEAR WAS DEPLOYED AND A FEW SECONDS BEFORE LANDING, FLIGHT CREW REPORTED AN (UNUSUAL SMELL) ON THE FLIGHT DECK. NO OTHER WARNING OR INDICATOR WAS NOTED. LANDING PROCEEDED AS USUAL. ON POST FLIGHT INSPECTION, HYDRAULIC RESENov 29, 2007 · N407W · Israel 1124A · Hydraulic System, MainSDR 2007FA0000229Valve · crackedCRACK IN INTERCONNECT VALVE MOTOR HOUSING. FOUND DURING BAG REMOVAL AND REINSTALLATION. CAUSE OF CRACK, UNKNOWN. (K)Mar 8, 2007 · N328PC · Israel 1124A · Aircraft Fuel Distribution SystemSDR WAI2007F00000Outflow Valve · leakingAIRCRAFT PRESSURIZATION INTERMITTENT. PRESSURIZATION WILL WORK WITH NO DEFECTS ON ONE FLIGHT; THE VERY NEXT FLIGHT, SYSTEM WOULD NOT WORK AT ALL. CLEANED OUTFLOW AND SAFETY VALVES; STILL INTERMITTENT. INSTALLED NEW SAFETY AND OUTFLOW SOLENOID VALVES (A AND Mar 5, 2007 · N325LW · Israel 1124A · Pressure Regulator/Outflow ValveSDR 2007F00022Safety Valve · leakingAIRCRAFT PRESSURIZATION INTERMITTENT. PRESSURIZATION WILL WORK WITH NO DEFECTS ON ONE FLIGHT; THE VERY NEXT FLIGHT, SYSTEM WOULD NOT WORK AT ALL. CLEANED OUTFLOW AND SAFETY VALVES; STILL INTERMITTENT. INSTALLED NEW SAFETY AND OUTFLOW SOLENOID VALVES (A AND B),Mar 5, 2007 · N325LW · Israel 1124A · Cabin Pressure Control SystemSDR 2006FA0001139Wire · chafedAIRCRAFT ARRIVED WITH INOPERATIVE STRATER-GENERATOR. TROUBLESHOOTING REVEALED INOPERATIVE GENERATOR, FAILED GENERATOR CONTROL UNIT, AND FAILED CONTROL RELAY. FURTHER TROUBLESHOOTING FOUND (A) AND (D) LEADS TO STARTER-GENERATOR AT ENGINE WIRING WAS BRITTLE ANNov 1, 2006 · N794TK · Israel 1124A · Electrical Power System WiringSDR 2006F00048Probe · malfunctionedPRIOR TO REFUELING AIRCRAFT, CREW NOTICED LEFT FUEL QUANTITY GAUGE WAS 1400 LBS HEAVIER THAN RIGHT. SUBMITTED SPECIAL FLIGHT PERMIT AND RETURNED TO BASE. FOUND LEFT MAIN FUEL PROBE BAD. REMOVED AND REPLACED FUEL PROBE, CALIBRATED FUEL QUANTITY SYSTEM. PERFSep 25, 2006 · N211ST · Israel 1124A · Fuel Quantity IndicatorSDR 2006F00047Probe · malfunctionedPRIOR TO REFUELING AIRCRAFT, CREW NOTICED LEFT FUEL QUANITY GAGE WAS 1400 LBS HEAVIER THAN RIGHT. SUBMITTED SPECIAL FLIGHT PERMIT AND RETURNED TO BASE. FOUND LEFT MAIN FUEL PROBE BAD. REMOVED AND REPLACED FUEL PROBE, CALIBRATED FUEL QUANITY SYSTEM. PERFORMSep 25, 2006 · N211ST · Israel 1124A · Fuel Quantity IndicatorSDR 2006FA0000187Cover · missingWHILE PERFORMING A 200 HOUR INSPECTION ON THIS AIRCRAFT, THE TAIL SECTION FAIRINGS AND PANELS WERE REMOVED. THE PITCH TRIM ACTUATOR WAS FOUND WITH THE DUST SHIELD DOWN AGAINS THE MOTOR HOUSING. IT WAS OBVIOUS THAT THE TIE BOLT HAD BEEN REMOVED, DUST SHIELD LFeb 21, 2006 · N411HB · Israel 1124A · Stabilizer Position IndicatingSDR 2004FA0000892Trunnion · crackedDURING A 1200 HOUR SCHEDULED INSPECTION, THE OUTER STRUT BODY OF THE NOSE LANDING GEAR UPPER TRUNNION WAS FOUND TO HAVE A CRACK IN THE OUTER BARREL STARTING FROM THE UPPER THREAD LOCK BORE EXTENDING DOWN 5.75 INCHES.Aug 20, 2004 · N788FS · Israel 1124A · Nose/Tail Landing GearSDR 2005FA0000229Tube · leakingTUBE LEAKING THRU SEVERAL PIN HOLES, SUSPECT INTERNAL CORROSION. SLOW EVACUATION OF HYDRAULIC FLUID PREVENTED ACTUATION OF HYDRAULIC FUSE. TAKEOFF WITH GEAR (UP) SELECTION REVEALED SLOW ACTUATION AND A RETURN TO BASE. GEAR (DOWN) SLOW BUT CAME DOWN AND LOCKJun 24, 2004 · N437SJ · Israel 1124A · Hydraulic System, MainSDR 070201Trim Switch · malfunctionedPILOT REPORTED UNCOMMAND VIOLENT ROLL TO LEFT. CREW LOST 15000 FT OF ALTITUDE BEFORE GAINING CONTROL. CONTINUED TO VAN NUYS & LANDED WITHOUT INCIDENT. GULFSTREAM TECHNICAL OPERATIONS CAME TO OBSERVE TEST IAW IAI REF LETTER DATED 6-26-2002. PERFORMED A OPS CJun 28, 2002 · N118MP · Israel 1124A · Autopilot SystemSDR 2002F00764Dampener · faultyAT CRUISE ALTITUDE THE AIRCRAFT EXPERIENCED FULL LEFT RUDDER DEFLECTION. EMERGENCY PROCEDURES WHERE INITIATED. DURING RECOVERY PROCEDURES ALTITUDE LOSS OF 15,000 FEET. YAW DAMPENER WAS DISABLED AND AIRCRAFT CONTROLS RETURNED TO NORMAL. AIRCRAFT RETURNED TOJun 19, 2002 · N118MP · Israel 1124A · Autopilot SystemSDR 2002F00623Brake Assy · lockedUPON LANDING THE NR 1 BRAKE LOCKED OVERHEATING THE BRAKE. THE HEAT DAMAGED THE BRAKE, WHEEL AND AXLE. THE WHOLE ASSEMBLY WAS REPLACED AND FUNCTION CHECK SATISFACTORY.Jun 9, 2002 · N118MP · Israel 1124A · BrakeSDR Z972002F00000Transducer · failedANTI-SKID TRANSDUCER FAILED (LOCK UP) CAUSING THE MAIN WHEEL BEARING TO HEAT-UP INTURN CAUSED LEFT MAIN WHEEL BEARING FAILURE CAUSING SEVERE DAMAGE TO AXLE, LOWER FORK, WHEEL HALVES. ALL NEW PARTS INSTALLED.May 20, 2002 · N118MP · Israel 1124A · Brake Anti-Skid SectionSDR N9W2002F00001Light · meltedAIRCRAFT DEPARTED, CREW NOTICED SMOKE AND FUMES IN THE CABIN AND COCKPIT. CREW ACCOMPLISHED EMERGENCY ACTION CHECKLIST, MANUALLY DEPLOYED OXYGEN MASKS AND PERFORMED AN EMERGENCY DECENT. THE PILOT IN COMMAND ELECTED TO DIVERT FLIGHT TO THE NEAREST AIRPORT FOMay 5, 2002 · N407W · Israel 1124A · Passenger Compartment LightingSDR LS32002F00000Line · crackedHYD FLUID LEAKING FROM FORWARD CABIN BELLY ANTENNA. FOUND GEAR UPLOCK LINE TO BE CRACKED IN BEND RADIUS UNDER CABIN FLOOR AT APPROX STA 66.45. AIRCRAFT TT: 5055.6 CYCLES 3384Feb 8, 2002 · N73CL · Israel 1124A · Hydraulic System, MainSDR T1I2002F00000Adapter · looseHYDRAULIC SYSTEM FAILURE IN FLIGHT. ADAPTER WAS NOT TIGHTENED DURING MAINTENANCE PREVIOUS DAY. SAFETY WIRE LOOSE. PILOT STATED SWITCH WAS CHANGED BY ANOTHER SHOP.Jan 30, 2002 · N439WW · Israel 1124A · Hydraulic System, MainSDR N9W2002F00000Ring Gear · failedENGINE SHUT DOWN DUE TO FAN SHAFT RING GEAR PN 30770774-1 CAME APART. THE CAUSE OF FAILURE IS NOT KNOWN. PARTS SENT TO MFG FOR ANALYSIS.Aug 13, 2001 · N407W · Israel 1124A · Fuel Controlling SystemSDR 20010419CW004Battery Pack · misinstalledBATTERY PACK ASSEMBLY HAS OTHER THAN ORIGINAL DATA PLATE INSTALLED, OTHER THAN ORIGINAL TOP AND BOTTOM COVERS INSTALLED APPEAR TO BE MAIN NICA CELL SHIMS; ROUND HEAD SCREWS IN CUNTER SUNK HOLES. OTHER THAN ORIGINAL TERMINAL POST, INSTALLED COUNTER SUNK SDec 28, 2000 · N365CX · Israel 1124A · Emergency LightingSDR 99ZZZX4108Window · crackedPER IAI MM, CHAPTER 5-20-02, PAGE 202, PARA D(4), THIS PART NUMBERED SIDE WINDOW IS NO LONGER INSPECTED AT 800-HOUR INTERVALS. THIS WINDOW CRACKED AT A MOUNT BOLT HOLE AT THE PILOT'S DV WINDOW. CRACK WAS DETECTED WITH A PRISM. SUBMITTER RECOMMENDED ALL COCKOct 11, 1999 · N50HS · Israel 1124A · Flight Compartment WindowsSDR 99ZZZX1470Window · crackedIAW IAI MM CHAP 5-20-02 PG 202 PARA D(4), THIS COCKPIT SIDE WINDOW IS NO LONGER INSPECTED AT THE 800-HOUR INTERNAL. THIS NEW STYLE WINDOW, PN 343017-183, CRACKED AT A MOUNT BOLT HOLE ALONG THE UPPER EDGE OF THE D.V. WINDOW. THIS CRACK WAS DETECTED WITH THE USEMar 9, 1999 · N494BP · Israel 1124A · Flight Compartment WindowsSDR 99ZZZX59Door Jamb · crackedDURING INSPECTION, FOUND CABIN DOOR LOWER DOOR JAMB CRACKED AT LOCATION WHERE DOOR STEP ASSY FORWARD STOP CONTACTS DOOR JAMB ANGLE, P/N 333046-03. DOOR JAMB ANGLE SHOULD BE REINFORCED WHERE STEP ASSY STOP CONTACTS AREA.May 15, 1998 · N365CX · Israel 1124A · Passenger/Crew DoorsSDR 98ZZZX1071Engine · failedDURING A TOUCH AND GO LANDING, CONDUCTED FOR CREW PROFICIENCY TRAINING, THE RIGHT ENGINE FAILED SHORTLY AFTER TAKEOFF POWER WAS SET ON BOTH ENGINES.Sep 12, 1997 · N849HS · Israel 1124A · Engine (Turbine/Turboprop)SDR 97ZZZX616Torque Tube · wornUPON PERFORMING SB 1124-27-129 AND AD 96-24-11, FOUND WEAR INDICATED PER AD AND SB. FURTHER INSPECTION INDICATED GROOVES ON THE BOTTOM OF THE TUBE CAUSED BY THE EDGES OF THE ROLLERS. PILOT STATED THAT THE OTHER TUBE PREVIOUSLY REPLACED HAD THE SAME GROOVES IJan 22, 1997 · N2BG · Israel 1124A · Aileron Control SystemSDR 96ZZZX3630Aileron Skin · crackedFOUND RIGHT AILERON TOP SKIN CRACKED AT OUTBOARD END. CRACK EXTENDED OUT FROM TWO SIDES OF A RIVET HEAD, APPROXIMATELY .1875 INCH IN BOTH DIRECTIONS. AILERON WAS REPAIRED AND WILL BE MONITORED FOR FURTHER CRACKING.Mar 13, 1996 · N551TP · Israel 1124A · AileronsSDR 96ZZZX806Control Rod · brokeLEFT NOSE GEAR DOOR VERTICAL CONTROL ROD - ROD END BROKE OFF WHEN GEAR LOWERED. ROD END CRACKED IN THREAD LINE WHERE SCREWED INTO ACTUAL ROD END. DARK LINE ON CROSS SECTION INDICATED CRACK NOT NEW. SUBMITTER STATED STRESS POSSIBLE FROM DOORS BEING ADJUSTED Jan 13, 1996 · N730CA · Israel 1124A · Landing Gear Door Retract SectionSDR 95ZZZX6834Blade · failedFL 24,000 FEET CRUISE - LOUD BOOM NOISE OCCURRED WITH VIBRATION FOLLOWING. RIGHT ENGINE WAS PULLED BACK TO IDLE BY CREW WHICH CUT DOWN ON VIBRATION LEVEL. ENGINE WAS SHUT DOWN AS PRECAUTIONARY MEASURE.Nov 13, 1995 · N1904G · Israel 1124A · Turbine SectionSDR 95ZZZX2831Filter Assy · o-ring crimpedABOUT 30 MINUTES BEFORE LANDING IN GRI, RT HYDRAULIC ANNUNCIATOR STARTED FLICKERING, ALL OTHER INDICATIONS NORMAL. AFTER PARKING AND WHEN SETTING THE PARKING BRAKES, BOTH HYDRAULIC ANNUNCIATORS CAME ON AND HYDRAULIC PRESSURE WAS LOST. A CRIMPED TEFLON O-RINGMay 17, 1995 · N76ER · Israel 1124A · Hydraulic Filter, MainSDR 95ZZZW791O-Ring · crimpedABOUT 30 MINUTES BEFORE LANDING IN GRI THE RIGHT HYDRAULIC ANNUNCIATOR STARTED FLICKERING, ALL OTHER INDICATIONS NORMAL. AFTER PARKING AND WHEN SETTING THE PARKING BRAKES BOTH HYDRAULIC ANNUNCIATORS CAME ON AND HYDRAULIC PRESSURE WAS LOST. A CRIMPED TEFLON OMay 11, 1995 · N76ER · Israel 1124A · Hydraulic System, MainSDR 95ZZZX2076Control Cable · frayedDURING COMPLIANCE OF SB 1124-32-116, A SHINY AREA WAS NOTED ON THE CABLE AT THE POINT WHERE THE CABLE WAS SECURED BY THE LOCK TAB. THE CABLE WAS REMOVED FOR INSPECTION. SUBSEQUENT INSPECTION REVEALED NUMEROUS BROKEN STRANDS. APPROXIMATELY 2 INCHES FORWARD OFApr 7, 1995 · N50XX · Israel 1124A · Landing Gear Steering System
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