# Service difficulty reports: Israel Aircraft Industries 1124

A list on [Israel Aircraft Industries 1124](https://openairdocs.org/model/israel-aircraft-industries-1124.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 131 reports

- [SDR FJTA201601104811](https://openairdocs.org/sdr/FJTA201601104811.md): Unknown · smoke · Jan 9, 2016 · N481NS · Israel 1124 · Air Distribution System
  > TWENTY 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
- [SDR CA100227006](https://openairdocs.org/sdr/CA100227006.md): Trunnion · damaged · Mar 12, 2015 · Israel 1124 · Fuselage, Landing Gear Attach Fittings
  > (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 CONTAC
- [SDR BN5A201521800001](https://openairdocs.org/sdr/BN5A201521800001.md): Relief Valve · faulty · Feb 8, 2015 · N349MC · Israel 1124 · Cabin Pressure Control System
  > AFTER 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 A
- [SDR BN5A2014092400001](https://openairdocs.org/sdr/BN5A2014092400001.md): Amplifier · faulty · Sep 21, 2014 · N300X · Israel 1124 · Autopilot System
  > EXPERIENCED 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 2617
- [SDR FJTA14064811](https://openairdocs.org/sdr/FJTA14064811.md): Unknown · unknown · Jun 3, 2014 · N481NS · Israel 1124 · Cabin Pressure Control System
  > DURING 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 DECIDE
- [SDR BN5A2013042300001](https://openairdocs.org/sdr/BN5A2013042300001.md): Pin · bent · Apr 12, 2013 · N349MC · Israel 1124 · Landing Gear System Wiring
  > DURING 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 MS3126F20-3
- [SDR BN5A2013031100001](https://openairdocs.org/sdr/BN5A2013031100001.md): Hinge Fitting · cracked · Mar 1, 2013 · N349MC · Israel 1124 · Horizontal Stabilizer Structure
  > C/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.
- [SDR 2013F00056](https://openairdocs.org/sdr/2013F00056.md): Actuator · defective · Feb 15, 2013 · N335VB · Israel 1124 · Landing Gear Actuator
  > ON 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.
- [SDR 2013FA0000089](https://openairdocs.org/sdr/2013FA0000089.md): Control Switch · misaligned · Feb 13, 2013 · N57PT · Israel 1124 · Pneumatic Distribution System
  > BLEED 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.
- [SDR T8VA20120605001](https://openairdocs.org/sdr/T8VA20120605001.md): Engine · leaking · Jun 5, 2012 · N36SF · Israel 1124 · Engine (Turbine/Turboprop)
  > ON 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
- [SDR 2012FA0000258](https://openairdocs.org/sdr/2012FA0000258.md): Hydraulic Line · corroded · Mar 21, 2012 · N942WC · Israel 1124 · Hydraulic System, Main
  > LINE 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 IN
- [SDR T8VA2011F00211](https://openairdocs.org/sdr/T8VA2011F00211.md): Switch · defective · Oct 13, 2011 · N36SF · Israel 1124 · Landing Gear Position and Warning
  > ON 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 BOTH
- [SDR SSWR2011032900001](https://openairdocs.org/sdr/SSWR2011032900001.md): Frame · cracked · Mar 29, 2011 · N50M · Israel 1124 · Fuselage Main, Frame
  > THE FS 174.000 FRAME HAS A 2 INCH CRACK THRU THE INBD FLANGE AND INTO THE WEB LOCATED AT THE FLOOR LINE.
- [SDR CA110321019](https://openairdocs.org/sdr/CA110321019.md): Elt · malfunctioned · Mar 15, 2011 · Israel 1124 · Emergency Locator Beacon
  > (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 S
- [SDR T8VA36SF101609](https://openairdocs.org/sdr/T8VA36SF101609.md): O-Ring · leaking · Oct 16, 2009 · N36SF · Israel 1124 · Hydraulic System, Main
  > LT 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 FOR
- [SDR CA090810001](https://openairdocs.org/sdr/CA090810001.md): Hydraulic System · leaking · Aug 8, 2009 · Israel 1124 · Hydraulic System, Main
  > ACFT LOST HYD FLUID IN FLIGHT.
- [SDR CA081210012](https://openairdocs.org/sdr/CA081210012.md): Bracket · cracked · Dec 8, 2008 · Israel 1124 · Vertical Stabilizer
  > (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, V
- [SDR WAI2008F00001](https://openairdocs.org/sdr/WAI2008F00001.md): Planetary Gear · broken · Jun 17, 2008 · N211ST · Israel 1124 · Accessory Gearboxes
  > DURING 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 FIL
- [SDR 2008FA0000306](https://openairdocs.org/sdr/2008FA0000306.md): Oxygen Mask · collapsed · May 1, 2008 · Israel 1124 · Passenger Oxygen System
  > DURING 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. IN
- [SDR 2008FA0000308](https://openairdocs.org/sdr/2008FA0000308.md): Oxygen Mask · collapsed · May 1, 2008 · Israel 1124 · Passenger Oxygen System
  > DURING 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. IN
- [SDR 2008FA0000333](https://openairdocs.org/sdr/2008FA0000333.md): Indicator · inoperative · Apr 25, 2008 · N500KE · Israel 1124 · Passenger Oxygen System
  > PASSENGER OXYGEN MASK FLOW INDICATOR INOPERATIVE. THIS UNIT CAME FROM LOT LC 0521 K OR LOT LC 0526K
- [SDR CA071026007](https://openairdocs.org/sdr/CA071026007.md): Brake Assy · failed · Oct 18, 2007 · Israel 1124 · Landing Gear Brake System
  > (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 P
- [SDR CA071026005](https://openairdocs.org/sdr/CA071026005.md): Actuator · failed · Oct 16, 2007 · Israel 1124 · Rudder Actuator
  > (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. W
- [SDR 2007FA0000701](https://openairdocs.org/sdr/2007FA0000701.md): Rod · cracked · Jul 9, 2007 · N40TA · Israel 1124 · Landing Gear Actuator
  > (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 RO
- [SDR 2007FA0000539](https://openairdocs.org/sdr/2007FA0000539.md): Actuator · misaligned · May 30, 2007 · N27TZ · Israel 1124 · Trailing Edge Flap Actuator
  > INSTALLED 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 BEE
- [SDR 2007FA0000487](https://openairdocs.org/sdr/2007FA0000487.md): Actuator · misaligned · May 30, 2007 · N27TZ · Israel 1124 · Trailing Edge Flap Actuator
  > INSTALLED 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 BE
- [SDR 2007FA0000486](https://openairdocs.org/sdr/2007FA0000486.md): Actuator · misaligned · May 30, 2007 · N27TZ · Israel 1124 · Trailing Edge Flap Actuator
  > INSTALLED 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 BE
- [SDR 2007FA0000405](https://openairdocs.org/sdr/2007FA0000405.md): Skin · corroded · May 22, 2007 · N600NY · Israel 1124 · Fuselage Main, Plate/Skin
  > FOUND 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 I
- [SDR 2007FA0000437](https://openairdocs.org/sdr/2007FA0000437.md): Skin · corroded · May 22, 2007 · N600NY · Israel 1124 · Fuselage Main, Plate/Skin
  > FOUND 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 C
- [SDR 2007FA0000404](https://openairdocs.org/sdr/2007FA0000404.md): Skin · corroded · May 22, 2007 · N600NY · Israel 1124 · Fuselage Main, Plate/Skin
  > FOUND 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 SO
- [SDR 2007F00033](https://openairdocs.org/sdr/2007F00033.md): Bracket · broken · Apr 18, 2007 · N890BA · Israel 1124 · Landing Gear Position and Warning
  > NOSE 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. 4105-080112
- [SDR 2007F00032](https://openairdocs.org/sdr/2007F00032.md): Bracket · broken · Apr 18, 2007 · N890BA · Israel 1124 · Landing Gear Position and Warning
  > NOSE 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 4105-08011270
- [SDR 2007FA0000107](https://openairdocs.org/sdr/2007FA0000107.md): Seal · leaking · Jan 25, 2007 · N300XL · Israel 1124 · Passenger/Crew Doors
  > THE 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 H
- [SDR GNL2006F00000](https://openairdocs.org/sdr/GNL2006F00000.md): Hydraulic Line · cracked · Aug 29, 2006 · N730CA · Israel 1124 · Hydraulic System, Main
  > IN 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
- [SDR 2006FA0000266](https://openairdocs.org/sdr/2006FA0000266.md): Flex Duct · deteriorated · Feb 17, 2006 · N290CA · Israel 1124 · Air Distribution System
  > DURING 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 COVER
- [SDR CA051110001](https://openairdocs.org/sdr/CA051110001.md): Cable · frayed · Nov 8, 2005 · Israel 1124 · Landing Gear Steering System
  > (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 T
- [SDR CA051101001](https://openairdocs.org/sdr/CA051101001.md): Tube · ruptured · Oct 30, 2005 · Israel 1124 · Air Intake Anti/De-Ice System
  > (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.
- [SDR 2005FA0000668](https://openairdocs.org/sdr/2005FA0000668.md): O-Ring · defective · Apr 18, 2005 · N711KE · Israel 1124 · Hydraulic System, Main
  > FOLLOWING 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
- [SDR ZN3R425038](https://openairdocs.org/sdr/ZN3R425038.md): Bearing · fractured · Apr 1, 2005 · Israel 1124 · Engine (Turbine/Turboprop)
  > ENGINE 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.
- [SDR 2005FA0000599](https://openairdocs.org/sdr/2005FA0000599.md): Bearing Race · fractured · Apr 1, 2005 · Israel 1124 · Engine (Turbine/Turboprop)
  > ENGINE 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.
- [SDR 2005FA0000372](https://openairdocs.org/sdr/2005FA0000372.md): Housing · cracked · Nov 21, 2004 · N730CA · Israel 1124 · Main Landing Gear Strut/Axle/Truck
  > AFTER 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 ATT
- [SDR IXXA0400105O](https://openairdocs.org/sdr/IXXA0400105O.md): Striker · out of adjust · Aug 28, 2004 · N830 · Israel 1124 · Door Warning System
  > AFTER 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 SWITCH
- [SDR I262004F00000](https://openairdocs.org/sdr/I262004F00000.md): Switch · stuck · Jul 9, 2004 · N140VJ · Israel 1124 · Trailing Edge Flap Control System
  > FLAPS STUCK IN 12 DEGREE POSITION. FOUND THE NR 2 SWITCH STUCK IN CLOSED POSITION. REPLACED SLIDER ASSY. OPS CHECK GOOD.
- [SDR 2004FA0000570](https://openairdocs.org/sdr/2004FA0000570.md): Shutoff Valve · leaking · Jun 15, 2004 · N79KP · Israel 1124 · Pneumatic Distribution System
  > THIS 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.
- [SDR 2005FA0000460](https://openairdocs.org/sdr/2005FA0000460.md): Wire Harness · arced · May 17, 2004 · N900VP · Israel 1124 · Electrical Power System Wiring
  > FOUND 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)
- [SDR 705050704](https://openairdocs.org/sdr/705050704.md): Indicator · erratic · May 4, 2004 · N705AC · Israel 1124 · Airspeed/Mach Indicator
  > AIRCRAFT ABORTED TAKEOFF DUE TO A AIRSPEED INDICATION ANOMALY. BRAKES EXPERIENCED AN OVERHEAT.
- [SDR X6U2003F00000](https://openairdocs.org/sdr/X6U2003F00000.md): Actuator · failed · Oct 8, 2003 · N274HM · Israel 1124 · Stabilizer Control System
  > DURING 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 J
- [SDR N382003F00011](https://openairdocs.org/sdr/N382003F00011.md): Support Bracket · broken · Sep 28, 2003 · N163WC · Israel 1124 · Fuselage Miscellaneous Structure
  > WHILE 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 COU
- [SDR 2003FA0000912](https://openairdocs.org/sdr/2003FA0000912.md): Line · corroded · Aug 14, 2003 · N809JC · Israel 1124 · Hydraulic System, Main
  > BRAKE 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.
- [SDR ZES2003F00002](https://openairdocs.org/sdr/ZES2003F00002.md): Brake Assy · failed · Aug 8, 2003 · N351C · Israel 1124 · Landing Gear Brake System
  > DURING 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 OVERHAULE

Next page: https://openairdocs.org/model/israel-aircraft-industries-1124/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 = '1124'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/israel-aircraft-industries-1124/reports

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