TCDS ATC 384

MODEIS: Iockheed Vega 5-C (Army UC-101), 7 PCL-SM I-C. NUMBER: ATC 384 Engine P&W Wasp C1 402 hp, SC-1 450 hp or S3D1 450 hp Fuel 96 gallons cil 10 gallons No. passengers Baggage Landplane 180 lts. Seaplane 84 1bs. Maximum weight Landplane 4500 1bs. (See NOTE 1) Seaplane 4880 1bs. C.G. limits 22.2 in. and 36.5 in. aft of wing leading edge at fuselage Serial Nos. Serials below 138 eligible upon manufacturer's affidavit of conformity. Class I equipment: flectric starter; battery; heater; propeller - adj. metal; Fdo k floats and auxiliary tail fin surface (Seaplane). Class III equipment: Engine ring cowl 50 1bs.; wheel streamlines 50 lbs.; landing lights 30 lbs.; - in baggage compartment 45 lbs.; extra 48 gallon center radiator 15 1rs.; tires 25 1bs.; 15 gallon oil tank replacing 10 gallon tank, no change weight; 300 lb. baggage compartment in center section substituted for center controllable metal propeller (Hamilton Standard hub S84601, Flades 6101A-12, low pitch setting 16 degrees) . NOTE 1. Landplane standard weight may ke increased to 4750 1bs. provided the following changes are made: (These changes are also required on all All plywood covering is removed from the top surface of the wings between spars. Additional stringers of same size as old stringers are installed between the present stringers extending between the ribs and parallel to the present stringers. The total number of stringers between each rib will be seven when completed. The top surface is recovered using 1/8 inch plywood between the spars and between the No. 10 ribs at elsewhere should be the same thickness as the present installation.