TCDS TC 705

MODELS: American S1-B, 2 PCLM T-C. NJMBER: 705 Engine American S-5-125 Placard limits For all operations, 1950 rpm (125 hp) Placard speeds Level flight or climb - 111 mph True Ind. Glide or dive - 135 mph True Ind. Propeller Maximum permissible diameter 09 Fuel capacity 23-1/2 gallons (in fuselage) (-1) Oil capacity 3 gallons (-16) No. passengers Baggage (one 25 1bs. compartment in Standard weight C. G. limits (+20.1) and (+23.9) Spec. basis Serial Nos. papa certificate per y and up eligible per NOTE A Equipment: (Datum is leading edge center section wing) (* Means net increase) 101. Propeller - adj. metal (Hamilton Standard, hub 7061-C, blades 19B-1/2) (-44) 102. Collector (-25) 12 volt generator (Bosch) (-20) Battery (Willard) (-11) 6.50-10 wheels (Hayes 651M) with brakes and tires (+3) 106. Tail wheel (Goodrich Model 61) and 6x2-1/2 solid tire (Goodrich) 3 1bs. (+208) 107. Two landing gear shock struts (American S-100, Dwg. 8-107) 17 1bs. (+8) 108. Carburetor air heater Class III: 301. Propeller - wood (fixed or adj. pitch) (including hub) (See NOTF 27 1bs. (-44) Each aircraft manufactured after 11-10-41 must, prior to original certification, satisfactorily pass: An inspection for workmanship, materials and conformity before any covering, metal priming or finish is applied. A final inspection of the completed aircraft. A check of flight characteristics. NOTE Eligible for export as follows, subject of provisions of MOP-2-4: Canada - Landplane - eligible - Skiplane - not eligible All other countries except Great Britain, Australia, and New Zealand. NOTE 2. fuel valves must be placarded as follows: "Use reserve for take-off and landing." When wood propeller, item 301, is installed - Iwo 18-1/2 1bs. ballast weights must be installed in accordance wit! American Aircraft Dug. No. 7-100-1. The following limitations static rpn at maximun permissible throttle setting - not over 1930, Diameter - not over 99 in. not under 87 in.