# N900DM: 1981 Israel Aircraft Industries 1124A

- Status: Valid registration
- Airframe: [Israel Aircraft Industries 1124A](https://openairdocs.org/model/israel-aircraft-industries-1124a) (registry code 4500103, 12 seats)
- Engine: [Garrett TFE731 series](https://openairdocs.org/engine/garrett-tfe731-series) (registry code 29001)
- Data sheets: [TCDS A2SW](https://openairdocs.org/tcds/A2SW) (Israel Aircraft Industries Ltd.), [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (Honeywell Aerospace US LLC) (OpenAirDocs)
- Serial number: 358
- Year built: 1981
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 30, 1981
- Certificate issued: October 31, 2012
- Expires: October 31, 2028
- Mode S code: AC6F83
- Registered owner: [Glenbrook Aviation LLC](https://openairdocs.org/faa-owner/GLENBROOK%20AVIATION%20LLC)
- Location: [Fort Wayne, IN](https://openairdocs.org/faa-place/IN/Fort%20Wayne)
- Owner type: LLC
- Owner's area on the map: 41.1001° N, 85.1177° W: Placed by OpenAirDocs at the center of ZIP code 46805, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=900DM
- Page: https://openairdocs.org/aircraft/N900DM

From the FAA registry file of October 22, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Garrett TFE731 model are included.

## ADs that may apply (OpenAirDocs): 53 in force

### Matched by airframe (Israel Aircraft Industries 1124A)

- [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

### Matched by engine (Garrett TFE731 series)

- [AD 2016-07-02](https://openairdocs.org/ad/2016-07-02): Failure of the interstage turbine transition duct · Honeywell International TFE731-4, TFE731-4R, TFE731-5AR and 2 more. Effective May 5, 2016
- [AD 2014-12-52](https://openairdocs.org/ad/2014-12-52): Engines · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 11 more. Effective Jul 28, 2014
- [AD 2012-17-05](https://openairdocs.org/ad/2012-17-05): First stage low-pressure turbine (LPT1) rotor assembly · Honeywell International TFE731-4, TFE731-4R, TFE731-5 and 3 more. Effective Oct 2, 2012
- [AD 2010-06-11](https://openairdocs.org/ad/2010-06-11): Second stage low-pressure compressor rotor (LPCR) discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2C and 16 more. Effective Apr 21, 2010
- [AD 2008-19-12](https://openairdocs.org/ad/2008-19-12): ITT duct · Honeywell International TFE731-4, TFE731-4R, TFE731-5 and 3 more. Effective Oct 27, 2008
- [AD 2008-02-19](https://openairdocs.org/ad/2008-02-19): High pressure (HP) turbine rotor assemblies · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 15 more. Effective Mar 6, 2008
- [AD 2005-13-07](https://openairdocs.org/ad/2005-13-07): Turbine rotor discs. · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Jul 27, 2005
- [AD 2005-05-15](https://openairdocs.org/ad/2005-05-15): (LPT) stage 1 disks · Honeywell International TFE731-2, TFE731-2C, TFE731-3 and 5 more. Effective Apr 18, 2005
- [AD 2001-23-09](https://openairdocs.org/ad/2001-23-09): Fan Rotor Discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Dec 21, 2001
- [AD 2000-15-09](https://openairdocs.org/ad/2000-15-09): HPC Impeller · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 20 more. Effective Oct 10, 2000
- [AD 98-17-01 R1](https://openairdocs.org/ad/98-17-01-R1): Flex Fuel Tube · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Nov 29, 1999
- [AD 97-04-03](https://openairdocs.org/ad/97-04-03): First stage low pressure turbine (LPT) seal plates · Honeywell International TFE731-2A, TFE731-3C and TFE731-3CR. Effective May 5, 1997
- [AD 96-05-03](https://openairdocs.org/ad/96-05-03): Fan rotor disks · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 13 more. Effective Apr 2, 1996
- [AD 96-04-01](https://openairdocs.org/ad/96-04-01): Fan Rotor Assembly · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Mar 15, 1996
- [AD 95-07-02](https://openairdocs.org/ad/95-07-02): Low Pressure Turbine Disks · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 3 more. Effective Jun 19, 1995
- [AD 94-23-05](https://openairdocs.org/ad/94-23-05): Honeywell International TFE731-3A and TFE731-3AR. Effective Dec 1, 1994
- [AD 94-07-03](https://openairdocs.org/ad/94-07-03): Turbine Nozzles · Honeywell International TFE731-2A, TFE731-3, TFE731-3A and 4 more. Effective Jun 6, 1994
- [AD 92-02-18](https://openairdocs.org/ad/92-02-18): Inflight Operation · Honeywell International TFE731-5BR. Effective Feb 10, 1993
- [AD 92-21-06](https://openairdocs.org/ad/92-21-06): Low Pressure Turbine (LPT) Rotor Disks · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 2 more. Effective Nov 27, 1992
- [AD 90-24-06](https://openairdocs.org/ad/90-24-06): Thermocouple Lead Assemblies · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 8 more. Effective Nov 13, 1990
- [AD 90-03-04](https://openairdocs.org/ad/90-03-04): High Pressure Turbine Rotor Discs · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 1 more. Effective Feb 22, 1990
- [AD 88-18-03](https://openairdocs.org/ad/88-18-03): High Pressure Turbine Rotor Disc · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 1 more. Effective Jul 21, 1989
- [AD 86-03-01](https://openairdocs.org/ad/86-03-01): Turbine Interstage Transition Ducts · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 4 more. Effective Feb 24, 1986
- [AD 82-23-03 R1](https://openairdocs.org/ad/82-23-03-R1): High Pressure Compressor Impellers · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Dec 9, 1983
- [AD 81-24-08](https://openairdocs.org/ad/81-24-08): Turbine Interstage Transition Ducts · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 2 more. Effective Jan 6, 1982
- [AD 80-16-04](https://openairdocs.org/ad/80-16-04): Tie Rod · Honeywell International TFE731-2, TFE731-3 and TFE731-3R. Effective Aug 7, 1980
- [AD 78-22-10](https://openairdocs.org/ad/78-22-10): Low Pressure Rotor Thrust Ball Bearings · Honeywell International TFE731-2, TFE731-3 and TFE731-3R. Effective Nov 13, 1978
- [AD 75-07-10](https://openairdocs.org/ad/75-07-10): Transfer Gearbox Vertical Bevel Gear Bearing · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective May 1, 1975
- [AD 74-23-05](https://openairdocs.org/ad/74-23-05): Fuel Pumps · Honeywell International TFE731-2. Effective Nov 14, 1974
- [AD 74-11-06](https://openairdocs.org/ad/74-11-06): Fuel Control Computer · Honeywell International TFE731-2. Effective Sep 23, 1974
- [AD 74-18-16](https://openairdocs.org/ad/74-18-16): Fuel Control Computer · Honeywell International TFE731-2. Effective Sep 6, 1974
- [AD 74-18-12](https://openairdocs.org/ad/74-18-12): Fuel Control Orifice Assembly · Honeywell International TFE731-2. Effective Sep 3, 1974
- [AD 74-13-09](https://openairdocs.org/ad/74-13-09): Fuel Pump Assemblies · Honeywell International TFE731-2. Effective Jul 31, 1974
- [AD 89-22-16](https://openairdocs.org/ad/89-22-16): Engine Acceleration or Deceleration · Honeywell International TFE731-2, TFE731-5, TFE731-5AR and 1 more

### 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
- [AD 98-17-01](https://openairdocs.org/ad/98-17-01) (historical): Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Oct 13, 1998
- [AD 96-18-13](https://openairdocs.org/ad/96-18-13) (historical): Fan rotor disk · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 10 more. Effective Nov 12, 1996
- [AD 86-11-05](https://openairdocs.org/ad/86-11-05) (historical): Fan Rotor Discs · Honeywell International TFE731-2, TFE731-3 and TFE731-3R

## Information bulletins (advisory) (1 in force)

- [SAIB NE-06-70](https://openairdocs.org/saib/NE-06-70): . Issued Sep 25, 2006

## NTSB investigations

None matched to N900DM.

## FAA accident and incident reports

None matched to N900DM.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## STCs that may be installed (OpenAirDocs) (110, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Israel Aircraft Industries 1124A)

- [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 110: https://openairdocs.org/aircraft/N900DM/stcs.md

## Earlier aircraft with N900DM

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N900DM before.

- [Cancelled 2011-05-14](https://openairdocs.org/deregistered/N900DM-2011-05-14): Mueller Doug RX6, S/N 01. Assigned (non-type certificated), pending cancellation

## Related

- Other Israel Aircraft Industries 1124A aircraft: https://openairdocs.org/model/israel-aircraft-industries-1124a/aircraft.md
- The Garrett TFE731 series engine: https://openairdocs.org/engine/garrett-tfe731-series.md

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