TCDS A19WE

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---