# N234G: 1965 Aero Commander 1121 - Status: Valid registration - Airframe: [Aero Commander 1121](https://openairdocs.org/model/aero-commander-1121) (registry code 0142002, 10 seats) - Engine: [GE CJ610-SER series](https://openairdocs.org/engine/ge-cj610-ser-series) (registry code 30006) - Data sheets: [TCDS A2SW](https://openairdocs.org/tcds/A2SW) (Israel Aircraft Industries Ltd.), [TCDS 1E16](https://openairdocs.org/tcds/1E16) (General Electric Company) (OpenAirDocs) - Serial number: 28 - Year built: 1965 - Type: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: November 1, 1965 - Certificate issued: December 11, 2013 - Expires: December 31, 2029 - Mode S code: A217F2 - Registered owner: [Aviation Buisness Corp](https://openairdocs.org/faa-owner/AVIATION%20BUISNESS%20CORP) - Location: [Saint Louis, MO](https://openairdocs.org/faa-place/MO/Saint%20Louis) - Owner type: Corporation - Owner's area on the map: 38.5194° N, 90.2927° W: Placed by OpenAirDocs at the center of ZIP code 63125, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=234G - Page: https://openairdocs.org/aircraft/N234G From the FAA registry file of October 24, 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 GE CJ610-SER model are included. ## ADs that may apply (OpenAirDocs): 26 in force ### Matched by airframe (Aero Commander 1121) - [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 2003-11-07](https://openairdocs.org/ad/2003-11-07): Oxygen Shutoff Valve · Israel Aircraft Industries 1121, 1121A, 1121B and 3 more. Effective Jul 3, 2003 - [AD 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 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 93-25-03](https://openairdocs.org/ad/93-25-03): Structural Integrity Of Wings · Israel Aircraft Industries 1121, 1121A, 1121B and 1 more. Effective Jan 19, 1994 - [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 87-16-01](https://openairdocs.org/ad/87-16-01): Fuel Line Shrouds and Drains · GTCP30-92 or GTCP30-92C auxiliary power unit (UNC/CFC Acquisition STC SA1043WE or 2 others). Effective Aug 26, 1987 - [AD 81-01-08](https://openairdocs.org/ad/81-01-08): Placard-Operating Speeds · Israel Aircraft Industries 1121, 1121A, 1121B and 2 more. Effective Jan 16, 1981 - [AD 78-24-04](https://openairdocs.org/ad/78-24-04): Flexible Fuel Line Installation · Israel Aircraft Industries 1121, 1121A and 1121B. Effective Dec 20, 1978 - [AD 74-03-03](https://openairdocs.org/ad/74-03-03): Main Landing Gears · Israel Aircraft Industries 1121 and 1123. Effective Mar 17, 1977 - [AD 74-24-09](https://openairdocs.org/ad/74-24-09): Auxiliary Power Units · Airbus BAC 1-11 200 Series, BAC 1-11 400 Series, Auxiliary Power Units and 63 more. Effective Nov 19, 1975 - [AD 75-16-16](https://openairdocs.org/ad/75-16-16): Autopilot · Israel Aircraft Industries 1121, 1121A, 1121B and 1 more. Effective Aug 12, 1975 - [AD 69-12-08](https://openairdocs.org/ad/69-12-08): Fuel Supply System · Israel Aircraft Industries 1121, 1121A and 1121B. Effective Jun 21, 1969 - [AD 69-08-10](https://openairdocs.org/ad/69-08-10): Horizontal Stabilizer Trim System · Israel Aircraft Industries 1121, 1121A and 1121B. Effective May 24, 1969 - [AD 73-11-05](https://openairdocs.org/ad/73-11-05): Main Landing Gear · Israel Aircraft Industries 1121, 1121A and 1121B ### Matched by engine (GE CJ610-SER series) - [AD 2010-09-08](https://openairdocs.org/ad/2010-09-08): AFT Technologies combustion liners · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective May 28, 2010 - [AD 2001-10-12](https://openairdocs.org/ad/2001-10-12): Unapproved Parts · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Jun 7, 2001 - [AD 98-23-06](https://openairdocs.org/ad/98-23-06): Combustion Liner Assemblies · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Nov 20, 1998 - [AD 97-25-08](https://openairdocs.org/ad/97-25-08): General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Jan 2, 1998 - [AD 85-18-03](https://openairdocs.org/ad/85-18-03): Stage 1 Turbine Disk · General Electric CF700-2D, CF700-2D-2, CJ610-8A and 1 more. Effective Nov 15, 1985 - [AD 80-08-06 R1](https://openairdocs.org/ad/80-08-06-R1): Turbine Disks · General Electric CF700-2D, CF700-2D-2, CJ610-8A and 1 more. Effective Feb 2, 1981 - [AD 75-19-05](https://openairdocs.org/ad/75-19-05): Horizontal Drive Shaft · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 1 more. Effective Sep 26, 1975 - [AD 78-07-06](https://openairdocs.org/ad/78-07-06): Compressor Disks · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 2 more - [AD 73-23-05](https://openairdocs.org/ad/73-23-05): First Stage Turbine Discs · General Electric CF700-2C, CJ610-1, CJ610-4 and 2 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 ## Information bulletins (advisory) (2 in force) - [SAIB NE-08-49R1](https://openairdocs.org/saib/NE-08-49R1): Turbine Engine Combustion Section. Issued Sep 17, 2008 - [SAIB NE-00-31](https://openairdocs.org/saib/NE-00-31): . Issued Aug 29, 2000 - [SAIB NE-08-49](https://openairdocs.org/saib/NE-08-49) (historical): Turbine Engine Combustion Section. Issued Sep 9, 2008 ## NTSB investigations None matched to N234G. ## FAA accident and incident reports None matched to N234G. ## 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) (79, 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 (Aero Commander 1121) - [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 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 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 SA1879SW](https://openairdocs.org/stc/SA1879SW): Installation of Engine thrust reversers. The NORDAM Group LLC - [STC ST00304WI](https://openairdocs.org/stc/ST00304WI): Installation of Keddeg Company 21BC113 coaleser assembly. Purolator Facet, Inc - [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 SA416CE](https://openairdocs.org/stc/SA416CE): Installation of Hoskins Supplementary Twilighter Mark III High Lighting System encompassing Model A Single Wing Tip Lights and Model D (Dual) Tail Light or Tail Light Assembly per Hoskins Drawings 30-0208-3. BF Goodrich Aerospace - [STC SA1315WE](https://openairdocs.org/stc/SA1315WE): Installation of Mixture Monitor (exhaust gas temperature probe, gage and selector) in accordance with Delta Products Part Lists A-192 and A-193, or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9, 1981, or later FAA approved revision and/or Drawing List MM-127 dated November 15, 1981, or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29, 1968, copy attached, or later FAA approved revision. Universal Corporation - [STC SA922SW](https://openairdocs.org/stc/SA922SW): Drag chute as safety item. JSF Aviation Services Inc - [STC SA1298SW](https://openairdocs.org/stc/SA1298SW): Installation of Teledyne Avionics normalized angle of attack system model 112B400 w/input to slow/fast indicators of Collins FD108 or FD109 flight director w/indicator model 329B-8( ), Sperry HZ6F, HZ6B flight director,or Bendix FD60 flight director. Aerosonic Corporation - [STC SA927EA](https://openairdocs.org/stc/SA927EA): Installation of Grimes three light strobe kit P/N 34-0305-1 as supplemental lighting. Honeywell International Inc - [STC SA791CE](https://openairdocs.org/stc/SA791CE): Installation of either of the following electronic synchronizer kits P/N 213521 or P/N 213517. Ontic Engineering and Manufacturing Inc - [STC SA1192SO](https://openairdocs.org/stc/SA1192SO): Install Utah Research & Development Co. Model 126BC-101 battery charger system. Aviall Services, Inc - [STC SA2894SW](https://openairdocs.org/stc/SA2894SW): Installation of hydraulic accumulator pressure gages. AAR Airframe and Accessories Group - [STC SA3000WE](https://openairdocs.org/stc/SA3000WE): Installation of logo light assembly. DeVore Aviation Corporation of America, a New Mexico Corporation - [STC SA1943SW](https://openairdocs.org/stc/SA1943SW): Installation of DHC 26-1071-058 seats. Sierra Industries, Inc - [STC SA1274SW](https://openairdocs.org/stc/SA1274SW): Installation of CA5 batteries. AAR Aircraft Services Inc - [STC SA1513SW](https://openairdocs.org/stc/SA1513SW): Installation of ground air conditioner. AAR Aircraft Services Inc - [STC SA1947SW](https://openairdocs.org/stc/SA1947SW): Installation of a fuel drain collector. AAR Aircraft Services Inc - [STC SA2389SW](https://openairdocs.org/stc/SA2389SW): Installation of identification and recognition lights in wings. AAR Aircraft Services Inc - [STC SA2396SW](https://openairdocs.org/stc/SA2396SW): Fabrication and installation of aircraft positive door latch. AAR Airframe and Accessories Group - [STC SA2471SW](https://openairdocs.org/stc/SA2471SW): Fabrication and installation of aircraft cabin door retainer. AAR Airframe and Accessories Group - [STC SA2695SW](https://openairdocs.org/stc/SA2695SW): Installation of aircraft taxi lights on main landing gears. AAR Aircraft Services Inc - [STC SA2712SW](https://openairdocs.org/stc/SA2712SW): Modify existing TSO three-place forward facing couch with adjustable back. AAR Aircraft Services Inc - [STC SA2713SW](https://openairdocs.org/stc/SA2713SW): Installation of two and three-place couches (TSO 39a) side facing at right side of cabin. AAR Aircraft Services Inc - [STC SA2716SW](https://openairdocs.org/stc/SA2716SW): Relocation of thrust reverser hydraulic accumulator pressure gauge. AAR Aircraft Services Inc - [STC SA2745SW](https://openairdocs.org/stc/SA2745SW): Installation of aft baggage compartment. AAR Aircraft Services Inc - [STC SA2847SW](https://openairdocs.org/stc/SA2847SW): Installation of forward cabin window, left and right side at fus. sta. 115.78 to 134.78 and right side window at fus. sta. 150.15. AAR Aircraft Services Inc - [STC SA4045SW](https://openairdocs.org/stc/SA4045SW): Installation of manually activated ignitor switches with G.E. ignition exciter unit P/N 4026T0301. AAR Airframe and Accessories Group - [STC SA4256SW](https://openairdocs.org/stc/SA4256SW): Fabrication and installation of combination seat and toilet. AAR Aircraft Services Inc - [STC SA4329SW](https://openairdocs.org/stc/SA4329SW): Installation of pitot heat monitor system. AAR Aircraft Services Inc - [STC SA4125SW](https://openairdocs.org/stc/SA4125SW): Two-place side facing seat, frame only and side facing only. Aviation Fabricators Inc - [STC SA1213SO](https://openairdocs.org/stc/SA1213SO): Replace existing nickel-cadmium batteries with Gill BB638/T series lead-acid batteries. Teledyne Battery Products - [STC SA1165SW](https://openairdocs.org/stc/SA1165SW): Installation of bleed air heated engine inlet ducts. Astra Jet Corporation - [STC SA1246SW](https://openairdocs.org/stc/SA1246SW): Install equipment necessary to certify aircraft to 45,000 feet(crew only) and 41,000 feet(passenger). Astra Jet Corporation - [STC SA1311SW](https://openairdocs.org/stc/SA1311SW): Redesigned nose wheel corotating drive shaft. Astra Jet Corporation - [STC SA1345SW](https://openairdocs.org/stc/SA1345SW): Gross weight increase to 18,500 lbs. takeoff with B.F. Goodrich wheels, brakes and anti-skid system. Astra Jet Corporation - [STC SA1434SW](https://openairdocs.org/stc/SA1434SW): Increase maximum zero fuel weight from 12,000 lbs. to 12,340 lbs. Astra Jet Corporation - [STC SA1487SW](https://openairdocs.org/stc/SA1487SW): Replacement of existing cockpit light dimmers. Astra Jet Corporation - [STC SA2203SW](https://openairdocs.org/stc/SA2203SW): Install capacitance type fuel gaging system. Astra Jet Corporation - [STC SA4008SW](https://openairdocs.org/stc/SA4008SW): Installation of GE CJ610-9 engines. Astra Jet Corporation - [STC SA1356WE](https://openairdocs.org/stc/SA1356WE): Installation of AiResearch gas turbine GTCP30-92 auxiliary power unit. AlliedSignal Aviation Services - [STC SA7894SW](https://openairdocs.org/stc/SA7894SW): Installation of provisions for a patient litter with electrical power connectors. AVIEX Jet, Inc - [STC SA964CE](https://openairdocs.org/stc/SA964CE): Installation of Aircraft Instrument and Development, Inc. (AID) battery temperature indicating and over temperature warning system. R C Allen Instruments Inc - [STC SA383NE](https://openairdocs.org/stc/SA383NE): Overhaul and rework of nose- steering actuator assemblies P/N 713096-501 and -505. Atlantic Aviation Corporation - [STC SA398EA](https://openairdocs.org/stc/SA398EA): Installation of radome kit No. 3065. Norton Company, Performance Plactics - [STC SA630SW](https://openairdocs.org/stc/SA630SW): Installation of antenna for electronics system, and electronicequipment shelves. Tiger Air Svc Center, Inc All 79: https://openairdocs.org/aircraft/N234G/stcs.md ## Earlier aircraft with N234G The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N234G before. - [Cancelled 1974-07-18](https://openairdocs.org/deregistered/N234G-1974-07-18): Beech C18S, S/N 44-47606. Owner: [Atlanta Area Technical School](https://openairdocs.org/faa-owner/ATLANTA%20AREA%20TECHNICAL%20SCHOOL), [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta) ## Related - Other Aero Commander 1121 aircraft: https://openairdocs.org/model/aero-commander-1121/aircraft.md - The GE CJ610-SER series engine: https://openairdocs.org/engine/ge-cj610-ser-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.