# Beech RC-45J

- Type: Aircraft model (FAA registry)
- Registry code: 1151021
- Manufacturer (registry): BEECH
- Model: RC-45J
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 10
- Weight class: Up to 12,499 lb
- Cruise speed: 153 mph
- Certification: Type certificated
- Data sheet: [TCDS A-765](https://openairdocs.org/tcds/A-765) (OpenAirDocs)
- Holder: Textron Aviation Inc.
- Registered aircraft: 4
- Page: https://openairdocs.org/model/beech-rc-45j

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 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 81-18-07](https://openairdocs.org/ad/81-18-07): Tricycle Landing Gear · Textron 3N, 3NM, 3TM and 13 more. Effective Sep 10, 1981
- [AD 72-16-02 R3](https://openairdocs.org/ad/72-16-02-R3): Volpar Nose Landing Gear Fork · Volpar Mark IV tricycle landing gear (Southwestern Aero Exchange STC SA111WE or 2 others). Effective Apr 16, 1981
- [AD 75-27-09 R2](https://openairdocs.org/ad/75-27-09-R2): Wing Structure · Textron 18A, 18D, 18S (Army C-45C) and 27 more. Effective Aug 21, 1980
- [AD 77-19-07](https://openairdocs.org/ad/77-19-07): Control Column Assembly · Textron 18A, 18D, 18S (Army C-45C) and 27 more. Effective Sep 29, 1977
- [AD 72-25-06](https://openairdocs.org/ad/72-25-06): Nose Gear Extension · Volpar Mark IV tricycle landing gear (Southwestern Aero Exchange STC SA111WE or 2 others). Effective Dec 9, 1972

## Registered aircraft (4)

- [N145J](https://openairdocs.org/aircraft/N145J): [Melton Ricky N](https://openairdocs.org/faa-owner/MELTON%20RICKY%20N), [Luttrell, TN](https://openairdocs.org/faa-place/TN/Luttrell), built 1943, S/N 51233
- [N40189](https://openairdocs.org/aircraft/N40189): [Jacob Mark K](https://openairdocs.org/faa-owner/JACOB%20MARK%20K), [East Lansing, MI](https://openairdocs.org/faa-place/MI/East%20Lansing), built 1943, S/N 51218
- [N4207](https://openairdocs.org/aircraft/N4207): [American Airpower Hrtg Flg Museum](https://openairdocs.org/faa-owner/AMERICAN%20AIRPOWER%20HRTG%20FLG%20MUSEUM), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas), built 1943, S/N 67124
- [N7032](https://openairdocs.org/aircraft/N7032): [Gohman Charles S](https://openairdocs.org/faa-owner/GOHMAN%20CHARLES%20S), [Salinas, CA](https://openairdocs.org/faa-place/CA/Salinas), built 1943, S/N 67232

## NTSB investigations (3)

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 GAA15CA120](https://openairdocs.org/ntsb/GAA15CA120), Jun 11, 2015: Beech RC 45J (N585PB), Everett, WA, substantial damage. Probable cause: The pilot's failure to maintain directional control, which resulted in a runway excursion, and a collision with a sign.
- [NTSB MIA96LA136](https://openairdocs.org/ntsb/MIA96LA136), May 2, 1996: Beech UC45J (N64819), Opa Locka, FL, substantial damage. Probable cause: inadequate inspection of the fuel line connector by company maintenance personnel, and failure of a connector resulting in a fuel leak and fire.
- [NTSB FTW87LA205](https://openairdocs.org/ntsb/FTW87LA205), Aug 20, 1987: Beech RC-45J (N11249), Houston, TX, substantial damage

## FAA accident and incident reports (4)

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 19960502009199A](https://openairdocs.org/incident/19960502009199A), May 2, 1996: Beech RC45J (N64819), Miami, FL, Substantial damage. Lost right engine fuel pump on climbout. Landing fire in same engine. Smoke blinded ran into canal. Fuel line leak.
- [Incident 19950509014219I](https://openairdocs.org/incident/19950509014219I), May 9, 1995: Beech RC45J (N64819), Miami, FL, Minor damage. During taxi to runway collided with a parked tug.
- [Incident 19920409019729I](https://openairdocs.org/incident/19920409019729I), Apr 9, 1992: Beech RC45J (N64819), Ft Lauderdale, FL, Minor damage. Engine sputtered on takeoff roll. Aircraft veered off runway. Carburetor linkage loose causing power loss.
- [Accident 19870819075729A](https://openairdocs.org/incident/19870819075729A), Aug 19, 1987: Beech RC45J (N11249), Houston, TX, Substantial damage. Veered off runway on rollout. Struck a ditch. Tail wheel in locked position. Tail wheel swiveled almost 90 degrees.

## Service difficulty reports (2)

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

- [SDR 2007FA0000663](https://openairdocs.org/sdr/2007FA0000663), Nov 21, 2006: CONTROL ARM. CRACKED. DURING COMPLIANCE WITH AD 77-19-07 PARA B, DYE PENETRANT INSPECTION REVEALED 2 POSSIBLE DEFECTS, 0.75 INCH AND 0.5 INCH LONG. BOTH INDICATIONS RADIATING FROM TH
- [SDR 96ZZZX2657](https://openairdocs.org/sdr/96ZZZX2657), May 2, 1996: ENGINE. FIRE. FIRE IN RIGHT WHEELWELL DURING LANDING. WHILE LANDING, TOWER INFORMED THE PILOT THERE WAS FIRE COMING OUT OF WHAT APPEARED TO BE THE RIGHT ENGINE. AT THIS POINT

## STCs that may be installed (OpenAirDocs) (78, 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 SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA01240SE](https://openairdocs.org/stc/SA01240SE): Installation of secondary voltage indication system. Visual Instruments LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc
- [STC SA1222GL](https://openairdocs.org/stc/SA1222GL): Replace existing main wheels and brakes with Cleveland 40-211/30-170. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA788GL](https://openairdocs.org/stc/SA788GL): Installation of Cleveland wheels and brakes conversion kit #199-127. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA829GL](https://openairdocs.org/stc/SA829GL): Installation of Cleveland wheels and brakes conversion kit No. 199-129. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". Genesys Aerosystems Inc
- [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc
- [STC SA01828SE](https://openairdocs.org/stc/SA01828SE): Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System. J. P. Instruments
- [STC SA6070NM](https://openairdocs.org/stc/SA6070NM): Installation of a 'quick-disconnect drain plug' on the engine rocker sump for the oil drain retrieval system after engine shutdown. West Coast Air Creations
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC
- [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA01229SE PAGE 2](https://openairdocs.org/stc/SA01229SE%20PAGE%202): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC
- [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02930NY](https://openairdocs.org/stc/SA02930NY): Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments. Insight Instrument Corporation
- [STC SA02717NY PAGE 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC
- [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument. J P Instruments
- [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments
- [STC SA02825NY PAGE 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc
- [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc
- [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation
- [STC SA02016SE-D](https://openairdocs.org/stc/SA02016SE-D): Installation of Garmin GTS 800, GTS 820 or GTS 850 Traffic System. Garmin International Inc
- [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc
- [STC SA00243BO](https://openairdocs.org/stc/SA00243BO): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200). Icarus Avionics, LLC
- [STC SA01473SE](https://openairdocs.org/stc/SA01473SE): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc

All 78: https://openairdocs.org/model/beech-rc-45j/stcs.md

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