# TCDS A19WE: Bushmaster Aircraft Corporation - Type: Type certificate data sheet - Status: Current - Holder: Bushmaster Aircraft Corporation - Revision: 1 - Revised: July 15, 1971 - Product: Aircraft, Small Airplane - Certification basis: Part 3, Part 21, CAR 3 - Data sheet PDF: https://openairdocs.org/files/sha256/59/05/5905f83dfd67cef201d74541295fdb6e1308054024ea3227cbbbd3cdb9298dd4 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2CC8B98C36FC1F7085256730004DC415.0001 - Page: https://openairdocs.org/tcds/A19WE ## Models (1) As the data sheet lists them. - Bushmaster 2000 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 Rev No. 1 1 Reformatted 1/94. FEDERAL AVIATION AGENCY A19WE Revision 1 Bushmaster Acft. Corp. Bushmaster 2000 July 15, 1971 TYPE CERTIFICATE DATA SHEET NO. A19WE This data sheet which is a part of Type Certificate No. A19WE prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder Bushmaster Aircraft Corporation 2701 Wardlow Road Long Beach, California I - Model Bushmaster 2000 (Normal Category) Approved October 8, 1968. Engines 3 Pratt & Whitney R-985-AN-14B or AN1 Fuel 80/87 Octane (Min. Grade Aviation Gasoline) Engine limits Press HP RPM In.Hg. Alt. Takeoff (2 minutes) 450 2300 36.5 SL Max Continuous 400 2200 33.5 5000' Propeller and 3 Hartzell HC-B3R30 hubs with 10152-5 1/2 blades propeller limits Pitch settings at 30 inch station High Pitch (Feather) 88° + 1/2° Low Pitch Stop 17° + 1/2° Diameter 95 1/2 inches No further reduction permitted Airspeed limits Vne - Never exceed 145 MPH (126 knots) (CAS) Vno - Normal operating 129 MPH (112 knots) (CAS) Vp - Maneuvering 112 MPH ( 97 knots) (CAS) Vmc - Minimum control 63 MPH ( 55 knots) (CAS) C.G. range (+212.47) to +224.09) Empty weight C.G. range None Datum 100" Fwd. of center firewall MAC 133.55" Leveling means Lower sill of sidewindows A19WE 2 Maximum weight 12,500 lb. Minimum crew One (+131) Passengers One (+131) Maximum baggage 3,380 lbs. Fuel capacity 366 gallons 360 gallons usable, 120 gal. in each of three tanks Oil capacity 8 gal. (center engine) 9 gal. ea. (outboard engines) Control surface movements (Tolerance = + 1°) Elevator 17° Up 17° Down Horiz. Stab. 4° Up 4° Down Ailerons 15° Up 15° Down Aileron Trim Tab 9° Up 9° Down Rudder 18° Right 18° Left Rudder Trim Tab 13° Right 13° Left Serial Nos. eligible No. 1 and subsequent Certification basis CAR 3 dated May 15, 1956 plus Amendments 3-1 through 3-8 with exemptions No's 710 and 710A granting relief from the requirements of FAR 21.17(b)(2) Application for Type Certificate dated 6-16-64 Production basis None. Prior to original certification of each aircraft, an FAA representative must perform a detailed inspection for workmanship, materials, and conformity with the approved technical data, and a check of the flight characteristics. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight, and loading instructions when necessary must be provided for each aircraft at the time of original certification. NOTE 2. A placard shall be provided in clear view of the pilot stating: "This airplane must be operated as a Normal Category Airplane in compliance with the operating limitations stated in the form of placards, markings and manuals." ---END--- ``` ## ADs None name its models. ## STCs approved under this data sheet (27) - [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 SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [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 SA01282NY](https://openairdocs.org/stc/SA01282NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K015 on aircraft powered by Pratt & Whitney radial reciprocating engine Series R-985, R-1340 and R-1830.. Airwolf Filter Corporation - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation - [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 SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [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 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 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 SA01695SE](https://openairdocs.org/stc/SA01695SE): Installation of an antenna. Garmin AT Inc. - [STC SA01487SE](https://openairdocs.org/stc/SA01487SE): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.. Garmin AT Inc. - [STC SA2546NM](https://openairdocs.org/stc/SA2546NM): Install Lockheed airplane Model 18 tailgear on BMR2000.. Bushmaster Aircraft Corporation - [STC SA2545NM](https://openairdocs.org/stc/SA2545NM): Installation of 1/2" Marine Plywood floort, Seat Rails, TSO Seats and Interior Arrangement for 13 passenger configuration.. Bushmaster Aircraft Corporation - [STC SA01933LA](https://openairdocs.org/stc/SA01933LA) (historical): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin AT Inc. --- 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.