TCDS AR-31

Page No. 1 2 Rev. No. 2 2 FEDERAL AVIATION ADMINISTRATION AR-31 Revision 2 RAWDON T-1 May 1, 1978 TYPE CERTIFICATE DATA SHEET NO. AR-31 This data sheet which is a part of type certificate No. AR-31 prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder M. H. Spinks, Sr. Spinks Industries Oak Grove Airport Fort Worth, Texas I - Model T-1, 1 PCLM (Restricted Category Only), Approved April 24, 1959 Engine Lycoming O-320-A2A, O-360-A1A, or O-360-A1D Fuel 80/87 min. grade aviation gasoline for O-320-A2A 91/96 min. grade aviation gasoline for O-360-A1A and O-360-A1D Engine limits O-320-A2A: for all operations, 2700 r.p.m. (150 hp.) O-360-A1A and O-360-A1D:for all operations, 2700 r.p.m. (180 hp.) Propeller and A. With O-320-A2A engine propeller limits 1. Fixed pitch metal, Sensenich M74DM-0 Static r.p.m. at maximum permissible throttle setting: Not over 2350, not under 2250. No additional tolerance permitted. Diameter: Not over 74 in., not under 72.5 in. B. With O-360-A1A or O-360-A1D engine 1. Fixed pitch metal, McCauley 1A200-FA Static r.p.m. at maximum permissible throttle setting: Not over 2400, not under 2300. No additional tolerance permitted. Diameter: Not over 82 in., not under 80 in. 2. McCauley constant speed installation a. McCauley hub 2D36C14 with 78KM blades. Diameter: not over 74 in., not under 72.5 in. b. Woodward hydraulic governor 210235-C. Airspeed limits Level flight or climb 110 m.p.h. ( 96 knots) True Ind. Glide or dive 154 m.p.h. (134 knots) True Ind. C.G. range (+89.7) to (+90.5) at 2110 lb. (+83.5) to (+90.5) at 1519 lb. or less. Straight line variation between points given. Empty weight C.G. range None Datum 73.3 in. forward of wing leading edge. Leveling means Upper right longeron in front cockpit. 2 AR-31 Maximum weight 2110 lb. Any increase in maximum weight to be determined in accordance with CAM 8.10-3(e)(3). No. seats 1 (+79) Maximum baggage None Hopper weight Maximum structural compliance with CAM 8 is 800 lb. The following placard must be displayed on the hopper in plain view of the ground crew filling the hopper: "Maximum weight of contents lb." The actual weight to be determined in accordance with CAM 8.10 -3(e)(3). Fuel capacity 50 gal. (45 gal. usable) (Two 25 gal. wing tanks) (+100). Oil capacity 8 qt. (6 qt. usable) (+28). Control surface movements Elevator Up 26° Down 28° Elevator tab Up 11° Down 19° Rudder Right 21° Left 21° Aileron Up 23° Down 17° Flaps Down 30° Serial Nos. eligible T1-29SD and up Certification basis CAR 8.10(b) effective October 11, 1950, and CAM 8. Type Certificate No. AR-31 issued April 24, 1959. Application for Type Certificate dated October 3, 1957. Production basis None. Prior to original certification of each aircraft manufactured, an FAA representative must perform a detailed inspection for workmanship, materials, and conformity with the approved technical data. Equipment: The basic required equipment as prescribed in the applicable airworthiness regulations must be installed in the aircraft for certification. NOTE 1. Current weight and balance report together with 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. The following placard must be displayed in cockpit in full view of pilot: "Maneuvering Speed, Vp - 110 m.p.h. Server Pull-Ups should be confined to speeds below 110 m.p.h. No acrobatic maneuvers including spins approved." .....END.....