# Israel Aircraft Industries 1124A

- Type: Aircraft model (FAA registry)
- Registry code: 4500103
- Manufacturer (registry): ISRAEL AIRCRAFT INDUSTRIES
- Model: 1124A
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 12
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS A2SW](https://openairdocs.org/tcds/A2SW) (OpenAirDocs)
- Holder: Israel Aircraft Industries Ltd.
- Registered aircraft: 28
- Page: https://openairdocs.org/model/israel-aircraft-industries-1124a

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2025-11-04](https://openairdocs.org/ad/2025-11-04): Engine Exhaust · Israel Aircraft Industries 1124 and 1124A. Effective Jun 23, 2025
- [AD 2005-18-13](https://openairdocs.org/ad/2005-18-13): Overhead circuit breaker panel · Israel Aircraft Industries 1124 and 1124A. Effective Sep 22, 2005
- [AD 2004-14-14](https://openairdocs.org/ad/2004-14-14): Rudder skins and ribs · Israel Aircraft Industries 1121, 1121A, 1121B and 3 more. Effective Aug 13, 2004
- [AD 2003-12-03](https://openairdocs.org/ad/2003-12-03): Airplane flight manual (oxygen masks) · Israel Aircraft Industries 1124 and 1124A. Effective Jul 17, 2003
- [AD 2003-11-07](https://openairdocs.org/ad/2003-11-07): Oxygen Shutoff Valve · Israel Aircraft Industries 1121, 1121A, 1121B and 3 more. Effective Jul 3, 2003
- [AD 2002-01-26](https://openairdocs.org/ad/2002-01-26): Bolts on Engine Inlet Cowl and Aft Nacelle Attachment Flanges · Israel Aircraft Industries 1124, 1124A and 1125 Westwind Astra. Effective Mar 7, 2002
- [AD 2000-23-13](https://openairdocs.org/ad/2000-23-13): Horizontal Stabilizer Trim Actuator · Israel Aircraft Industries 1121, 1121A, 1121B and 3 more. Effective Dec 4, 2000
- [AD 2000-10-04](https://openairdocs.org/ad/2000-10-04): Aileron Ribs · Israel Aircraft Industries 1124 and 1124A. Effective Jun 6, 2000
- [AD 99-18-08](https://openairdocs.org/ad/99-18-08): Hydraulic Low Pressure Warning Lights · Israel Aircraft Industries 1124 and 1124A. Effective Oct 5, 1999
- [AD 97-05-03 R1](https://openairdocs.org/ad/97-05-03-R1): Global Positioning Systems · BAE Systems Avro 146-RJ100A, BAe 146-200A, Jetstream Model 4101 and 27 more. Effective Apr 20, 1999
- [AD 98-20-35](https://openairdocs.org/ad/98-20-35): Trim Actuator of Horizontal Stabilizer · Israel Aircraft Industries 1121, 1121A, 1121B and 3 more. Effective Nov 3, 1998
- [AD 98-06-10](https://openairdocs.org/ad/98-06-10): Hydraulic Fuses In Brake System And Emergency Hydraulic Indicating System · Gulfstream Aerospace LP 1125 Westwind Astra, Astra SPX, 1121 and 5 more. Effective Apr 17, 1998
- [AD 96-24-11](https://openairdocs.org/ad/96-24-11): Inspect Aileron Push-Pull Tube · Israel Aircraft Industries 1123, 1124 and 1124A. Effective Jan 6, 1997
- [AD 95-22-01](https://openairdocs.org/ad/95-22-01): Fluorescent Lighting System · Aerospace Lighting Fluorescent lighting systems, A310-203, A310-204 and 74 more. Effective Dec 4, 1995
- [AD 92-12-02](https://openairdocs.org/ad/92-12-02): Aileron Control Rod Assemblies · Israel Aircraft Industries 1123, 1124 and 1124A. Effective Jul 31, 1992
- [AD 91-13-08](https://openairdocs.org/ad/91-13-08): Nose Landing Gear · Israel Aircraft Industries 1121, 1121A, 1121B and 3 more. Effective Jul 22, 1991
- [AD 89-12-08](https://openairdocs.org/ad/89-12-08): Horizontal Stabilizer · Israel Aircraft Industries 1121, 1121A, 1121B and 3 more. Effective Jul 10, 1989
- [AD 81-07-07](https://openairdocs.org/ad/81-07-07): Intercom System Overheating · Israel Aircraft Industries 1123, 1124 and 1124A. Effective Aug 5, 1985
- [AD 80-19-15](https://openairdocs.org/ad/80-19-15): Electrical Wiring Fuselage Station 112 · Israel Aircraft Industries 1124 and 1124A. Effective Aug 10, 1981

Historical (superseded or no longer in force):

- [AD 98-05-09](https://openairdocs.org/ad/98-05-09) (historical): Trim Actuator Of Horizontal Stabilizer Inspection · Israel Aircraft Industries 1121, 1121A, 1121B and 3 more. Effective Apr 10, 1998

## Registered aircraft (28)

- [N110JD](https://openairdocs.org/aircraft/N110JD): [Chandler Air LLC](https://openairdocs.org/faa-owner/CHANDLER%20AIR%20LLC), [Bossier City, LA](https://openairdocs.org/faa-place/LA/Bossier%20City), built 1984, S/N 414, First renewal notice
- [N123EG](https://openairdocs.org/aircraft/N123EG): [Butler Brian S](https://openairdocs.org/faa-owner/BUTLER%20BRIAN%20S), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), S/N 306
- [N123RC](https://openairdocs.org/aircraft/N123RC): [Bwa Westwind 2 LLC](https://openairdocs.org/faa-owner/BWA%20WESTWIND%202%20LLC), [Orlando, FL](https://openairdocs.org/faa-place/FL/Orlando), S/N 349
- [N127PT](https://openairdocs.org/aircraft/N127PT): [N325nw LLC](https://openairdocs.org/faa-owner/N325NW%20LLC), [Lodi, OH](https://openairdocs.org/faa-place/OH/Lodi), built 1981, S/N 337
- [N21HR](https://openairdocs.org/aircraft/N21HR): [Jetsteam Aviation Inc](https://openairdocs.org/faa-owner/JETSTEAM%20AVIATION%20INC), [Cheyenne, WY](https://openairdocs.org/faa-place/WY/Cheyenne), built 1981, S/N 335, Registration ineffective or invalid
- [N224GF](https://openairdocs.org/aircraft/N224GF): [Shamrock Kelly Energy Inc](https://openairdocs.org/faa-owner/SHAMROCK%20KELLY%20ENERGY%20INC), [Blanco, TX](https://openairdocs.org/faa-place/TX/Blanco), S/N 402
- [N229D](https://openairdocs.org/aircraft/N229D): [N229d LLC](https://openairdocs.org/faa-owner/N229D%20LLC), [Stuart, FL](https://openairdocs.org/faa-place/FL/Stuart), built 1985, S/N 427
- [N241CT](https://openairdocs.org/aircraft/N241CT): [Avalair Aircraft Management LLC](https://openairdocs.org/faa-owner/AVALAIR%20AIRCRAFT%20MANAGEMENT%20LLC), [Brookshire, TX](https://openairdocs.org/faa-place/TX/Brookshire), built 1981, S/N 355
- [N29CL](https://openairdocs.org/aircraft/N29CL): [Jordan Air LLC](https://openairdocs.org/faa-owner/JORDAN%20AIR%20LLC), [Fort Smith, AR](https://openairdocs.org/faa-place/AR/Fort%20Smith), built 1984, S/N 404
- [N29LN](https://openairdocs.org/aircraft/N29LN): [Lucky29 Liquors LLC](https://openairdocs.org/faa-owner/LUCKY29%20LIQUORS%20LLC), [Loveland, CO](https://openairdocs.org/faa-place/CO/Loveland), S/N 389
- [N30TK](https://openairdocs.org/aircraft/N30TK): [Gravitas Aero LLC](https://openairdocs.org/faa-owner/GRAVITAS%20AERO%20LLC), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas), built 1982, S/N 374
- [N317JS](https://openairdocs.org/aircraft/N317JS): [West Air LLC](https://openairdocs.org/faa-owner/WEST%20AIR%20LLC), [Little Rock, AR](https://openairdocs.org/faa-place/AR/Little%20Rock), S/N 385
- [N328PC](https://openairdocs.org/aircraft/N328PC): [Sn 328 Corp](https://openairdocs.org/faa-owner/SN%20328%20CORP), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), S/N 328
- [N345TR](https://openairdocs.org/aircraft/N345TR): [Jog068 Inc](https://openairdocs.org/faa-owner/JOG068%20INC), [Lewes, DE](https://openairdocs.org/faa-place/DE/Lewes), built 1981, S/N 345
- [N406HR](https://openairdocs.org/aircraft/N406HR): [Dodson International Parts Inc](https://openairdocs.org/faa-owner/DODSON%20INTERNATIONAL%20PARTS%20INC), [Rantoul, KS](https://openairdocs.org/faa-place/KS/Rantoul), S/N 324
- [N424JR](https://openairdocs.org/aircraft/N424JR): [Gravitas Aviation LLC](https://openairdocs.org/faa-owner/GRAVITAS%20AVIATION%20LLC), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas), built 1984, S/N 405
- [N437SJ](https://openairdocs.org/aircraft/N437SJ): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1986, S/N 437
- [N64FS](https://openairdocs.org/aircraft/N64FS): [Jetvue Texas LLC](https://openairdocs.org/faa-owner/JETVUE%20TEXAS%20LLC), [Richardson, TX](https://openairdocs.org/faa-place/TX/Richardson), built 1984, S/N 417
- [N70DT](https://openairdocs.org/aircraft/N70DT): [Jet Set Aviation LLC](https://openairdocs.org/faa-owner/JET%20SET%20AVIATION%20LLC), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), S/N 334
- [N728TG](https://openairdocs.org/aircraft/N728TG): [Digital Interstate Management Inc](https://openairdocs.org/faa-owner/DIGITAL%20INTERSTATE%20MANAGEMENT%20INC), [Keller, TX](https://openairdocs.org/faa-place/TX/Keller), built 1984, S/N 420
- [N772DC](https://openairdocs.org/aircraft/N772DC): [Best Aircraft Deals LLC](https://openairdocs.org/faa-owner/BEST%20AIRCRAFT%20DEALS%20LLC), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), S/N 410
- [N777HD](https://openairdocs.org/aircraft/N777HD): [Butler Brian S](https://openairdocs.org/faa-owner/BUTLER%20BRIAN%20S), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), built 1983, S/N 397
- [N790JR](https://openairdocs.org/aircraft/N790JR): [Transenergie Inc](https://openairdocs.org/faa-owner/TRANSENERGIE%20INC), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston), built 1984, S/N 424
- [N900DM](https://openairdocs.org/aircraft/N900DM): [Mwm Air LLC](https://openairdocs.org/faa-owner/MWM%20AIR%20LLC), [Adrian, MI](https://openairdocs.org/faa-place/MI/Adrian), built 1981, S/N 358
- [N911GU](https://openairdocs.org/aircraft/N911GU): [Team Aero LLC](https://openairdocs.org/faa-owner/TEAM%20AERO%20LLC), [Olathe, KS](https://openairdocs.org/faa-place/KS/Olathe), built 1981, S/N 343
- [N928HR](https://openairdocs.org/aircraft/N928HR): [Howard Aviation LLC](https://openairdocs.org/faa-owner/HOWARD%20AVIATION%20LLC), [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio), built 1984, S/N 415
- [N959JJ](https://openairdocs.org/aircraft/N959JJ): [Jesus Saves LLC](https://openairdocs.org/faa-owner/JESUS%20SAVES%20LLC), [Conroe, TX](https://openairdocs.org/faa-place/TX/Conroe), built 1981, S/N 319
- [N98HG](https://openairdocs.org/aircraft/N98HG): [N98hg LLC](https://openairdocs.org/faa-owner/N98HG%20LLC), [Sheridan, WY](https://openairdocs.org/faa-place/WY/Sheridan), built 1983, S/N 394

## NTSB investigations (7)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB GAA21WA165](https://openairdocs.org/ntsb/GAA21WA165), Jul 5, 2021: Iai 1124 (N790JR), Treasure Cay, Bahamas, destroyed, 2 fatal
- [NTSB ERA14FA300](https://openairdocs.org/ntsb/ERA14FA300), Jun 18, 2014: Israel Aircraft Industries 1124A (N793BG), Huntsville, AL, destroyed, 3 fatal. Probable cause: The flight crew's inability to maintain airplane control during initial climb following deployment of the right thrust reverser for reasons that could not be determined because postaccident…
- [NTSB NYC05WA114](https://openairdocs.org/ntsb/NYC05WA114), Jun 8, 2005: Israel Aircraft Industries 1124A (N639AT), Shannon, Ireland, incident, minor damage
- [NTSB FTW03FA036](https://openairdocs.org/ntsb/FTW03FA036), Nov 8, 2002: Israel Aircraft Industries 1124A (N61RS), Taos, NM, destroyed, 2 fatal. Probable cause: The pilot's inadvertent flight into mountain wave weather conditions while IMC, resulting in a loss of aircraft control.
- [NTSB NYC00MA048](https://openairdocs.org/ntsb/NYC00MA048), Dec 12, 1999: Israel Aircraft Industries 1124A (N50PL), Gouldsboro, PA, destroyed, 3 fatal. Probable cause: The improper assembly of the horizontal stabilizer trim actuator unit by maintenance personnel.
- [NTSB LAX94FA073](https://openairdocs.org/ntsb/LAX94FA073), Dec 16, 1993: Israel Aircraft Industries 1124A (N309CK), Santa Ana, CA, destroyed, 5 fatal. Probable cause: THE PILOT-IN-COMMAND'S FAILURE TO MAINTAIN ADEQUATE SEPARATION BEHIND THE BOEING 757 AND/OR REMAIN ABOVE ITS FLIGHT PATH DURING THE APPROACH, WHICH RESULTED IN AN ENCOUNTER WITH WAKE VORTICES FROM…
- [NTSB NYC91LA124](https://openairdocs.org/ntsb/NYC91LA124), May 1, 1991: Israel Aircraft Industries 1124A (N445BL), Oxford, CT, substantial damage. Probable cause: THE FAILURE OF THE PILOT TO MAINTAIN THE PROPER LANDING DESCENT RATE AND THE RESULTANT RIGHT MAIN LANDING GEAR ASSEMBLY COLLAPSE.

## FAA accident and incident reports (13)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20140618011029A](https://openairdocs.org/incident/20140618011029A), Jun 18, 2014: Israel Aircraft Industries 1124A (N793BG), Huntsville, AL, Destroyed, 3 fatal. During a crew training exercise, aircraft N793BG initated take-off roll and after rotation, raised gear and continued down the runway at approximately 50 to…
- [Incident 20131127022999I](https://openairdocs.org/incident/20131127022999I), Nov 27, 2013: Israel Aircraft Industries 1124A (N123RC), Minor damage. The crew of N123RC noticed a laud noise from the nose gear after departure from svpr. They decided to cancel the flight plan to skcl to make a precacionary…
- [Incident 20080424840159I](https://openairdocs.org/incident/20080424840159I), Apr 24, 2008: Israel 1124A (N818JH), FL, No damage. (-23) Aircraft departed fort lauderdale international (kfll) at 9:21 local on 4/28/2008. Proceeded to flight level 330 out of climb under control of miami…
- [Incident 20041105027499I](https://openairdocs.org/incident/20041105027499I), Nov 5, 2004: Israel 1124A (N83SG), Houston, TX, Minor damage. (-23) On 11/05/2004 @ approximately 18:32 local time, aircraft N83SG was landing on runway 04 at Houston William p. Hobby airport. At approximately 80 knts…
- [Accident 20021108031189A](https://openairdocs.org/incident/20021108031189A), Nov 8, 2002: Israel 1124A (N61RS), Taos, NM, Destroyed, 2 fatal. (.19) On November 8, 2002, approximately 1457 mountain standard time, an Israel aircraft industries 1124A (westwind 24) business jet, N61RS, was destroyed when…
- [Incident 20010201002029I](https://openairdocs.org/incident/20010201002029I), Feb 1, 2001: Israel 1124A (N437SJ), San Luis Obispo, CA, Minor damage. (-23) The a/c was departing San Luis Obispo, CA (sbp) airport for long beach, CA on runway 29 which is 4,799 feet in length. The distant required for takeoff…
- [Accident 19991212036899A](https://openairdocs.org/incident/19991212036899A), Dec 12, 1999: Israel 1124A (N50PL), Teterboro, NJ, Destroyed, 3 fatal. (.19) On December 12, 1999, about 1635 eastern standard time, an Israel aircraft industries 1124A, N50PL, was destroyed after impacting terrain near…
- [Incident 19990110012869I](https://openairdocs.org/incident/19990110012869I), Jan 10, 1999: Israel 1124A (N407W), Cedar City, UT. Left main wheel brake overheated during aborted takeoff at the Cedar City, Utah airport. Pilot returned to ramp where l/h wheel thermal releif valve blew. Tire…
- [Incident 19971028034789I](https://openairdocs.org/incident/19971028034789I), Oct 28, 1997: Israel 1124A (N793BG), Clarksburg, WV, Minor damage. Narrative: a/c struck deer on rollout on runway 21 at ckb. Radome damaged and nose gear door bent. No assistance needed and a/c taxied to ramp. Only minor…
- [Incident 19940224010179I](https://openairdocs.org/incident/19940224010179I), Feb 24, 1994: Israel 1124A (N76ER), Teterboro, NJ, Minor damage. Lost control while landing on snow and slush runway. Pilot not advised of runway conditions.
- [Accident 19931215046879A](https://openairdocs.org/incident/19931215046879A), Dec 15, 1993: Israel 1124A (N309CK), Santa Ana, CA, Destroyed, 5 fatal. Too close on approach behind a 757. Caught his wake turbulence. Lost control pitched down rolled and crashed.
- [Accident 19910501013879A](https://openairdocs.org/incident/19910501013879A), May 1, 1991: Israel 1124A (N445BL), Oxford, CT, Substantial damage. Made hard landing. Impact drove struts upward through wings. Collapsed right main gear. Flaps were up at zero degrees.
- [Incident 19900823045349I](https://openairdocs.org/incident/19900823045349I), Aug 23, 1990: Israel 1124A (N445BL), Santa Monica, CA. Pilot stated he could not transmit due to electrical problems. Climbed above assigned altitude.

## Service difficulty reports (39)

As reported by operators and repair stations, by the model named in the report.

- [SDR 9LVA202412180001](https://openairdocs.org/sdr/9LVA202412180001), Dec 18, 2024: PUMP. LEAKING. LH AND RH HYDRAULIC LOW PRESSURE INDICATORS ILLUMINATED IN CRUISE FLIGHT, MAIN PRESSURE INDICATED ZERO PSI. MAINTENANCE OBSERVED LOW HYDRAULIC FLUID LEVEL CAUSE
- [SDR 9LVA202211190001](https://openairdocs.org/sdr/9LVA202211190001), Nov 19, 2022: FLAP SYSTEM. FAULTED. ON APPROACH INTO KJAC, SELECTED FLAPS 12, FLAPS OPERATED NORMALLY TO 12 DEGREE POSITION. UPON REACHING 12 DEGREES, FLAPS UNBALANCE INDICATOR ILLUMINATED AND FLA
- [SDR 9LVA2021072100100](https://openairdocs.org/sdr/9LVA2021072100100), Jul 21, 2021: ACM. SEIZED. ON 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. MAIN
- [SDR 2017F00137](https://openairdocs.org/sdr/2017F00137), Aug 26, 2017: NOT REPORTED. MALFUNCTIONED. THE 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 PA
- [SDR 2017F00131](https://openairdocs.org/sdr/2017F00131), Jun 15, 2017: ENGINE. FAILED. ENGINE 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, RED
- [SDR T4BA20120301440](https://openairdocs.org/sdr/T4BA20120301440), Feb 25, 2012: ACTUATOR. LEAKING. AFTER 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
- [SDR 2010FA0000007](https://openairdocs.org/sdr/2010FA0000007), Dec 10, 2009: VANE. BROKEN. RT 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 ATTACHI
- [SDR 2010FA0000026](https://openairdocs.org/sdr/2010FA0000026), Dec 9, 2009: VANE. BROKEN. ACFT 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 ATTACHI
- [SDR 2008FA0000502](https://openairdocs.org/sdr/2008FA0000502), Jul 18, 2008: AMPLIFIER. INOPERATIVE. AFTER (1) HOUR DISENGAGES AUTOPILOT. PRELIMINARY INSPECTION RESULTS, NO DEFECTS NOTED AFTER BENCH CHECK. (K)
- [SDR JM02007F00000](https://openairdocs.org/sdr/JM02007F00000), Nov 29, 2007: TUBE. LEAKING. APPROX 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 WARN
- [SDR 2007FA0000229](https://openairdocs.org/sdr/2007FA0000229), Mar 8, 2007: VALVE. CRACKED. CRACK IN INTERCONNECT VALVE MOTOR HOUSING. FOUND DURING BAG REMOVAL AND REINSTALLATION. CAUSE OF CRACK, UNKNOWN. (K)
- [SDR WAI2007F00000](https://openairdocs.org/sdr/WAI2007F00000), Mar 5, 2007: OUTFLOW VALVE. LEAKING. AIRCRAFT PRESSURIZATION INTERMITTENT. PRESSURIZATION WILL WORK WITH NO DEFECTS ON ONE FLIGHT; THE VERY NEXT FLIGHT, SYSTEM WOULD NOT WORK AT ALL. CLEANED OUTFLO
- [SDR 2007F00022](https://openairdocs.org/sdr/2007F00022), Mar 5, 2007: SAFETY VALVE. LEAKING. AIRCRAFT PRESSURIZATION INTERMITTENT. PRESSURIZATION WILL WORK WITH NO DEFECTS ON ONE FLIGHT; THE VERY NEXT FLIGHT, SYSTEM WOULD NOT WORK AT ALL. CLEANED OUTFLO
- [SDR 2006FA0001139](https://openairdocs.org/sdr/2006FA0001139), Nov 1, 2006: WIRE. CHAFED. AIRCRAFT ARRIVED WITH INOPERATIVE STRATER-GENERATOR. TROUBLESHOOTING REVEALED INOPERATIVE GENERATOR, FAILED GENERATOR CONTROL UNIT, AND FAILED CONTROL RELAY. FU
- [SDR 2006F00048](https://openairdocs.org/sdr/2006F00048), Sep 25, 2006: PROBE. MALFUNCTIONED. PRIOR TO REFUELING AIRCRAFT, CREW NOTICED LEFT FUEL QUANTITY GAUGE WAS 1400 LBS HEAVIER THAN RIGHT. SUBMITTED SPECIAL FLIGHT PERMIT AND RETURNED TO BASE. FOUND 
- [SDR 2006F00047](https://openairdocs.org/sdr/2006F00047), Sep 25, 2006: PROBE. MALFUNCTIONED. PRIOR TO REFUELING AIRCRAFT, CREW NOTICED LEFT FUEL QUANITY GAGE WAS 1400 LBS HEAVIER THAN RIGHT. SUBMITTED SPECIAL FLIGHT PERMIT AND RETURNED TO BASE. FOUND LE
- [SDR 2006FA0000187](https://openairdocs.org/sdr/2006FA0000187), Feb 21, 2006: COVER. MISSING. WHILE 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 SHIE
- [SDR 2004FA0000892](https://openairdocs.org/sdr/2004FA0000892), Aug 20, 2004: TRUNNION. CRACKED. DURING 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 FRO
- [SDR 2005FA0000229](https://openairdocs.org/sdr/2005FA0000229), Jun 24, 2004: TUBE. LEAKING. TUBE LEAKING THRU SEVERAL PIN HOLES, SUSPECT INTERNAL CORROSION. SLOW EVACUATION OF HYDRAULIC FLUID PREVENTED ACTUATION OF HYDRAULIC FUSE. TAKEOFF WITH GEAR (UP
- [SDR 070201](https://openairdocs.org/sdr/070201), Jun 28, 2002: TRIM SWITCH. MALFUNCTIONED. PILOT REPORTED UNCOMMAND VIOLENT ROLL TO LEFT. CREW LOST 15000 FT OF ALTITUDE BEFORE GAINING CONTROL. CONTINUED TO VAN NUYS & LANDED WITHOUT INCIDENT. GULFSTREA
- [SDR 2002F00764](https://openairdocs.org/sdr/2002F00764), Jun 19, 2002: DAMPENER. FAULTY. AT CRUISE ALTITUDE THE AIRCRAFT EXPERIENCED FULL LEFT RUDDER DEFLECTION. EMERGENCY PROCEDURES WHERE INITIATED. DURING RECOVERY PROCEDURES ALTITUDE LOSS OF 15,00
- [SDR 2002F00623](https://openairdocs.org/sdr/2002F00623), Jun 9, 2002: BRAKE ASSY. LOCKED. UPON 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 SATISFA
- [SDR Z972002F00000](https://openairdocs.org/sdr/Z972002F00000), May 20, 2002: TRANSDUCER. FAILED. ANTI-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, LOW
- [SDR N9W2002F00001](https://openairdocs.org/sdr/N9W2002F00001), May 5, 2002: LIGHT. MELTED. AIRCRAFT DEPARTED, CREW NOTICED SMOKE AND FUMES IN THE CABIN AND COCKPIT. CREW ACCOMPLISHED EMERGENCY ACTION CHECKLIST, MANUALLY DEPLOYED OXYGEN MASKS AND PERFO
- [SDR LS32002F00000](https://openairdocs.org/sdr/LS32002F00000), Feb 8, 2002: LINE. CRACKED. HYD 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
- [SDR T1I2002F00000](https://openairdocs.org/sdr/T1I2002F00000), Jan 30, 2002: ADAPTER. LOOSE. HYDRAULIC SYSTEM FAILURE IN FLIGHT. ADAPTER WAS NOT TIGHTENED DURING MAINTENANCE PREVIOUS DAY. SAFETY WIRE LOOSE. PILOT STATED SWITCH WAS CHANGED BY ANOTHER SHO
- [SDR N9W2002F00000](https://openairdocs.org/sdr/N9W2002F00000), Aug 13, 2001: RING GEAR. FAILED. ENGINE 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.
- [SDR 20010419CW004](https://openairdocs.org/sdr/20010419CW004), Dec 28, 2000: BATTERY PACK. MISINSTALLED. BATTERY 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
- [SDR 99ZZZX4108](https://openairdocs.org/sdr/99ZZZX4108), Oct 11, 1999: WINDOW. CRACKED. PER 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 BO
- [SDR 99ZZZX1470](https://openairdocs.org/sdr/99ZZZX1470), Mar 9, 1999: WINDOW. CRACKED. IAW 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, CRACKE
- [SDR 99ZZZX59](https://openairdocs.org/sdr/99ZZZX59), May 15, 1998: DOOR JAMB. CRACKED. DURING 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 ANG
- [SDR 98ZZZX1071](https://openairdocs.org/sdr/98ZZZX1071), Sep 12, 1997: ENGINE. FAILED. DURING A TOUCH AND GO LANDING, CONDUCTED FOR CREW PROFICIENCY TRAINING, THE RIGHT ENGINE FAILED SHORTLY AFTER TAKEOFF POWER WAS SET ON BOTH ENGINES.
- [SDR 97ZZZX616](https://openairdocs.org/sdr/97ZZZX616), Jan 22, 1997: TORQUE TUBE. WORN. UPON 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
- [SDR 96ZZZX3630](https://openairdocs.org/sdr/96ZZZX3630), Mar 13, 1996: AILERON SKIN. CRACKED. FOUND 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 WA
- [SDR 96ZZZX806](https://openairdocs.org/sdr/96ZZZX806), Jan 13, 1996: CONTROL ROD. BROKE. LEFT 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 C
- [SDR 95ZZZX6834](https://openairdocs.org/sdr/95ZZZX6834), Nov 13, 1995: BLADE. FAILED. FL 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. ENGIN
- [SDR 95ZZZX2831](https://openairdocs.org/sdr/95ZZZX2831), May 17, 1995: FILTER ASSY. O-RING CRIMPED. ABOUT 30 MINUTES BEFORE LANDING IN GRI, RT HYDRAULIC ANNUNCIATOR STARTED FLICKERING, ALL OTHER INDICATIONS NORMAL. AFTER PARKING AND WHEN SETTING THE PARKING BR
- [SDR 95ZZZW791](https://openairdocs.org/sdr/95ZZZW791), May 11, 1995: O-RING. CRIMPED. ABOUT 30 MINUTES BEFORE LANDING IN GRI THE RIGHT HYDRAULIC ANNUNCIATOR STARTED FLICKERING, ALL OTHER INDICATIONS NORMAL. AFTER PARKING AND WHEN SETTING THE PARK
- [SDR 95ZZZX2076](https://openairdocs.org/sdr/95ZZZX2076), Apr 7, 1995: CONTROL CABLE. FRAYED. DURING 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 INS

## STCs that may be installed (OpenAirDocs) (108, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST08995AC](https://openairdocs.org/stc/ST08995AC): Replacement of original O rings and backup rings from landing gear lower bearing and floating piston with Green Tweed, Inc. AGT seals. Metrea Special Aerospace ISR Inc
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine
- [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC
- [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC SA5556SW](https://openairdocs.org/stc/SA5556SW): Installation of an electric driven vapor cycle air conditioning system. Air Comm Corporation
- [STC ST00835DE](https://openairdocs.org/stc/ST00835DE): Installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and In functionality using the Garmin GTX 335R and GTX 345R Transponders plus qualified position sensor. Peregrine
- [STC ST09772AC](https://openairdocs.org/stc/ST09772AC): Replacement of certain pneumatic deicer boots. SMR Technologies Inc
- [STC ST02429CH](https://openairdocs.org/stc/ST02429CH): Install air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC ST00790DE](https://openairdocs.org/stc/ST00790DE): Installation of BendixKing CAS 67B Traffic Alert and Collision Avoidance System (TCAS) II Version 7.1. Peregrine
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC
- [STC ST00373BO](https://openairdocs.org/stc/ST00373BO): Installation of Rockwell Collins TDR-94D Transponders with ADS-B Out. Pro Star Aviation, LLC
- [STC ST00193BO](https://openairdocs.org/stc/ST00193BO): Installation of Honeywell MK-VIII Enhanced Ground Proximity Warning System. Pro Star Aviation, LLC
- [STC ST00318NY-D](https://openairdocs.org/stc/ST00318NY-D): Installation of a Single Loral F-800 digital flight data recorder (DFDR). Delta Engineering Corporation
- [STC ST00304WI](https://openairdocs.org/stc/ST00304WI): Installation of Keddeg Company 21BC113 coaleser assembly. Purolator Facet, Inc
- [STC ST02632LA](https://openairdocs.org/stc/ST02632LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out and optionally install ACSS NXG-900 GPS as a position source for ADS-B Out. Aviation Communications and Surveillance Systems
- [STC ST02609LA](https://openairdocs.org/stc/ST02609LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA1178GL](https://openairdocs.org/stc/SA1178GL): Install Egan Aviation air ambulance stretcher P/N 125, using Installation Kit P/N 805. Paul/ Lanna Egan LLC
- [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc
- [STC ST04238AT](https://openairdocs.org/stc/ST04238AT): Upgrade of Honeywell Traffic Collision Avoidance Systems II (TCAS II) Processor Software from TCAS II Version 7.0 to TCAS II Version 7.1. Aviation Partners Group Inc
- [STC ST01855CH-D](https://openairdocs.org/stc/ST01855CH-D): Installation of Honeywell N1 Digital Electronic Engine Controls (DEEC). Honeywell International Inc
- [STC ST01202WI-D](https://openairdocs.org/stc/ST01202WI-D): Modification of an existing FAA approved Collins TPR-720, TPR-900 or TPR-901 Mode S transponder installation in Part 25 Aircraft using Collins Drawing Index as listed on AML No. ST01202WI-D, latest FAA approved revision. Rockwell Collins Inc
- [STC ST00673WI-D](https://openairdocs.org/stc/ST00673WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation. Rockwell Collins Inc
- [STC ST00682WI-D](https://openairdocs.org/stc/ST00682WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation in accordance with Collins Installation Instructions as listed on AML No. ST00682WI-D, Revision -, or later FAA approved revisions. Rockwell Collins Inc
- [STC ST00558WI-D](https://openairdocs.org/stc/ST00558WI-D): Installation of a Universal Avionics Corporation dual UNS-1B Flight Management System. Duncan Aviation Inc
- [STC ST01098WI-D](https://openairdocs.org/stc/ST01098WI-D): Installation of Universal Avionics Corporation Terrain Awareness System (TAWS). Duncan Aviation Inc
- [STC ST00514WI-D](https://openairdocs.org/stc/ST00514WI-D): Installation of an AlliedSignal Avionics, Inc., GNS-XIs Flight Management System (Dual). Duncan Aviation Inc
- [STC ST00697WI-D](https://openairdocs.org/stc/ST00697WI-D): Installation of AlliedSignal EGPWS System in the Israel Aircraft Industries Ltd. Models 1124 and 1124A Airplanes. Duncan Aviation Inc
- [STC ST01650CH-D](https://openairdocs.org/stc/ST01650CH-D): Installation of Innovative Solutions & Support (IS&S) Air Data Display Unit (ADDU) and Rockwell Collins ADC-87A Air Data Computer. Duncan Aviation Inc
- [STC ST737CH-D](https://openairdocs.org/stc/ST737CH-D): Installation of Universal Navigation Corporation UNS-1K flight management system, using software (SCN) 602.x. Duncan Aviation Inc
- [STC ST599CH-D](https://openairdocs.org/stc/ST599CH-D): Installation of a Universal Navigation Corp UNS-1M flight management system with software level (SCN) 23.x for enroute and terminal operations, GPS non-precision approaches and GPS Primary use oceanic/remote operation. Duncan Aviation Inc
- [STC ST458CH-D](https://openairdocs.org/stc/ST458CH-D): Installation of an AlliedSignal Aeropsace TFE731-3D-1G Turbofan Engine(s). Honeywell International Inc
- [STC ST01142WI-D](https://openairdocs.org/stc/ST01142WI-D): Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92E control head. Rockwell Collins Inc
- [STC ST00844WI-D](https://openairdocs.org/stc/ST00844WI-D): Modification of Collins TCAS II or TCAS-94 (TCAS II) system installation with Collins TTR-920 Change 7.0 Receiver Transmitter to a Collins TCAS II or TCAS-94 OTCAS II) system installation with Collins TTR-921 or Collins TTR-4000 Change 7.0 TCAS Receiver Transmitter. Rockwell Collins Inc
- [STC ST01221SE](https://openairdocs.org/stc/ST01221SE): Group aircraft approval for Reduced Vertical Separation Minimum (RVSM). AeroMech Incorporated
- [STC ST01307WI-D](https://openairdocs.org/stc/ST01307WI-D): Modification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation. Rockwell Collins Inc
- [STC ST02150CH-D](https://openairdocs.org/stc/ST02150CH-D): Installation of a Honeywell CAS-67A Traffic and Collision Avoidance System (TCAS II), in accordance with ElectroSonics Drawing ES1124-200352-01, Rev. A., dated April 07, 2005 or later FAA approved revision. Garrett Aviation Services
- [STC ST01772NY-D](https://openairdocs.org/stc/ST01772NY-D): Installation of a Honeywell Mark VIII Enhanced Ground Proximity Warning System. Limited to installation on 1124A, serial number 337 ONLY. Dassault Falcon Jet - Wilmington Corp
- [STC ST01773NY-D](https://openairdocs.org/stc/ST01773NY-D): Installation of an L3 Communications F1000 Digital Flight Data Recorder. Limited to installation on 1124A, serial number 337 ONLY. Dassault Falcon Jet - Wilmington Corp
- [STC ST01238WI](https://openairdocs.org/stc/ST01238WI): Reduced Vertical Separation Minimum (RVSM) group airworthiness approval. Kohlman Systems Research Inc
- [STC SA4431NM](https://openairdocs.org/stc/SA4431NM): Installation of an Asinc Entertainment System Model No. 985100 in accordance with FAA sealed Asinc Top Drawing No. 985510, Rev. "B", dated May 21, 1982, or later FAA approved revision. Rockwell Collins Inc
- [STC ST01116SE](https://openairdocs.org/stc/ST01116SE): Group aircraft approval for Reduced Vertical Separation Minimum (RVSM) in accordance with AeroMech Document No. AMI-QD-WW-0115, Revision A, dated March 28, 2003, or later FAA-approved revisions. AeroMech Incorporated
- [STC SA1192SO](https://openairdocs.org/stc/SA1192SO): Install Utah Research & Development Co. Model 126BC-101 battery charger system. Aviall Services, Inc
- [STC ST01098WI](https://openairdocs.org/stc/ST01098WI): Installation of Universal Avionics Terrain Awareness System (TAWS). Duncan Aviation Inc
- [STC ST02536AT](https://openairdocs.org/stc/ST02536AT): Installation of Dual Universal Flight Management Systems (SCN 604.(x)software), certified as GPS Primary Means of Navigation for Oceanic/Remote Operations. Garrett Aviation Services

All 108: https://openairdocs.org/model/israel-aircraft-industries-1124a/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [207218HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141434704920250807185055.0001): Thrust Washer. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 207218 · Aug 4, 2025
- [207460HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129226125820250805133124.0001): Bearing, Ball Annular. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 207460 · Aug 4, 2025
- [RFS5002857](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193306717920250106202733.0001): Wear Pad. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 5002857 · Dec 19, 2024
- [RFS18B8](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188901433720250106202731.0001): Rivet, Pressure Plate. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces GY18B-8 · Dec 19, 2024
- [RFS5004020](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144706067120250106202733.0001): Wear Pad. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 5004020 · Dec 19, 2024
- [447883LA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177539331520241107175410.0001): Valve, Safety Assy. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 447883 · Nov 5, 2024
- [M06-201100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185138376620241022163144.0001): Label. Miraj Corporation · PMA PQ0870NE · Replaces Safran 06-201100 · Oct 10, 2024
- [LA01000X200A20B6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152605473220241016174903.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R01000X200A20B6 · Aug 28, 2024
- [LA449039](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134941423920241016174955.0001): Mask Lock. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 449039 · Aug 28, 2024
- [N1235XXXX](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143295344420240819142524.0001): Fluorescent Lamp. Aircraft Lighting International · PMA PQ2043NE · Replaces AL1235XXXX · Aug 6, 2024
- [PM-210](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156758408120260625165244.0001): Radome Mask. PM Research, Inc. · PMA PQ10049NE · Replaces NA · May 13, 2024
- [M06-200001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134897851220240223153731.0001): Label. Miraj Corporation · PMA PQ0870NE · Replaces Safran 06-200001 · Feb 15, 2024
- [398042-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169695078120230914150616.0001): Valve, Butterfly Shutoff. Honeywell International Inc. · PMA PQ1222NM · Replaces 398042-1-1 · Apr 5, 2023
- [2100428-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167370199620230914150617.0001): Engine Synchronizer. Honeywell International Inc. · PMA PQ1222NM · Replaces 2100428-1 · Apr 5, 2023
- [130374-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128940048120230914150615.0001): Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 130374-6 · Apr 5, 2023
- [PA-210816-321](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173311211720230406142600.0001): Mounting Plate Assembly,GI-275 IVSI. Southeast Aerospace, Inc. · PMA PQ4019CE · Replaces PA-210816-321 · Jan 11, 2023
- [PA-210816-551](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117173126920230406142610.0001): Adapter Harness, Garmin GI 275. Southeast Aerospace, Inc. · PMA PQ4019CE · Replaces PA-210816-551 · Jan 11, 2023
- [AD-38451-004](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103472290020230216160001.0001): Battery Assy. Aero Design Inc/A HEICO Aerospace Company · PMA PQ1465CE · Replaces 38451-004 · Oct 27, 2022
- [135157-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196386602120230731171158.0001): Filter. Honeywell International Inc. · PMA PQ1222NM · Replaces 135157-4 · Jul 14, 2022
- [102464-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165901193920230731171139.0001): Control. Honeywell International Inc. · PMA PQ1222NM · Replaces 102464-1 · Jul 14, 2022
- [102464-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162117369020230731171140.0001): Control. Honeywell International Inc. · PMA PQ1222NM · Replaces 102464-15 · Jul 14, 2022
- [103278-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111995151620230731171141.0001): Outflow/Safety Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 103278-1 · Jul 14, 2022
- [L387X](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167425063020220615130146.0001): 28VDC  LED Bulb. Aircraft Lighting International · PMA PQ2043NE · Replaces 387, MS18209-387, MS25237-387, GE387… · Jun 6, 2022
- [1302-006](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181345855320220617133344.0001): Incubator Transport. Spectrum Aeromed LLC · PMA PQ2435CE · Modification part · Mar 17, 2022
- [400226](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117699733520220617133345.0001): Shortbox Stretcher Adapter. Spectrum Aeromed LLC · PMA PQ2435CE · Modification part · Mar 17, 2022
- [1430-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108359332220220617133346.0001): Cabinet. Spectrum Aeromed LLC · PMA PQ2435CE · Modification part · Mar 17, 2022
- [6341-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106265521420220617133346.0001): Adapter Pin. Spectrum Aeromed LLC · PMA PQ2435CE · Modification part · Mar 17, 2022
- [2101144-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199361827320230724174001.0001): Engine Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2101144-1 · Mar 1, 2022
- [179510-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186366669420230724173959.0001): Water Separator. Honeywell International Inc. · PMA PQ1222NM · Replaces 179510-1 · Mar 1, 2022
- [103278-8](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177658496320230724173955.0001): Outflow Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 103278-8 · Mar 1, 2022
- [130398-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168797965720230724173954.0001): Outflow Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 130398-3 · Mar 1, 2022
- [107312-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162956288720230724173956.0001): Pneumatic Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 107312-2 · Mar 1, 2022
- [131078-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147297858120230724173953.0001): Manual Dump Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 131078-1 · Mar 1, 2022
- [102466-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138102845120230724173957.0001): Air Pressure Regulator. Honeywell International Inc. · PMA PQ1222NM · Replaces 102466-1 · Mar 1, 2022
- [2200165-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129760701720230724173958.0001): Refrigeration Unit. Honeywell International Inc. · PMA PQ1222NM · Replaces 2200165-2 · Mar 1, 2022
- [131052-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116149896020230724174000.0001): Venturi. Honeywell International Inc. · PMA PQ1222NM · Replaces 131052-1 · Mar 1, 2022
- [131358-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111167723220230724173952.0001): AUX. Vol Tank, Pressure Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 131358-1 · Mar 1, 2022
- [RFS5002894-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID981758224320210723162949.0001): Piston Insulator. Rapco Fleet Support Inc · PMA PQ2386CE · Replaces 5002894-1 · Jun 22, 2021
- [R1235XXXX](https://drs.faa.gov/browse/excelExternalWindow/D509AE89EEB5DFE086258618004BDA08.0001): LED Lamp. Aircraft Lighting International · PMA PQ2043NE · Replaces AL1235XXXX · Oct 29, 2020
- [N1235XXXX](https://drs.faa.gov/browse/excelExternalWindow/C18A1D02C7887EAF86258618004BDA8B.0001): Fluorescent Lamp. Aircraft Lighting International · PMA PQ2043NE · Replaces AL1235XXXX · Oct 29, 2020
- [NOHIPOT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100009293520240320173405.0001): Decal. Augusta Aero Innovations LLC · PMA PQ04441CE · Replaces 06-201020 · Oct 6, 2020
- [L1235XXXX KIT](https://drs.faa.gov/browse/excelExternalWindow/BA375A52AAD1423F862585D80046E4EB.0001): LED Lamp and Adapter Kit. Aircraft Lighting International · PMA PQ2043NE · Replaces AL1235XXXX and AL2000 · Aug 22, 2020
- [443613-00](https://drs.faa.gov/browse/excelExternalWindow/FE732206F3742AAA86258560003BDD25.0001): Harness, 833613-00. Shadin Avionics · PMA PQ2088CE · Replaces 443613-00 · Jun 6, 2019
- [613603-00](https://drs.faa.gov/browse/excelExternalWindow/F474BD51883E678086258560003BDD89.0001): Bracket, AFID RA Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613603-00 · Jun 6, 2019
- [833613-00](https://drs.faa.gov/browse/excelExternalWindow/E9293882A965D1D286258560003BDC47.0001): ADS-B Flight ID Adapter. Shadin Avionics · PMA PQ2088CE · Replaces 833613-00 · Jun 6, 2019
- [613604-00](https://drs.faa.gov/browse/excelExternalWindow/C99B32ED23A9740F86258560003BDDC9.0001): Bracket, AFID Side Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613604-00 · Jun 6, 2019
- [833613-10](https://drs.faa.gov/browse/excelExternalWindow/99326314CB6EBE8F86258560003BDCEA.0001): Digital Discrete Adapter (DDA). Shadin Avionics · PMA PQ2088CE · Replaces 833613-10 · Jun 6, 2019
- [613606-00](https://drs.faa.gov/browse/excelExternalWindow/501E105EA0BF714E86258560003BDE36.0001): Bracket, AFID Under Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613606-00 · Jun 6, 2019
- [443613-10](https://drs.faa.gov/browse/excelExternalWindow/313ABE429C4C505186258560003BDD5A.0001): Harness, DDA. Shadin Avionics · PMA PQ2088CE · Replaces 443613-10 · Jun 6, 2019
- [613605-00](https://drs.faa.gov/browse/excelExternalWindow/078709A82EB7C91386258560003BDDF9.0001): Bracket, AFID Top Mount. Shadin Avionics · PMA PQ2088CE · Replaces 613605-00 · Jun 6, 2019

All of them: https://openairdocs.org/model/israel-aircraft-industries-1124a/pma.md

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