TCDS TC 733

AETNA AEROCRAFT CORPORATION MODELS: Aerocraft 2SA, 2POLM I.C. NUMBER: 733 Engine Kinner R-5 Series 2 (See Item 201) Fuel 73 minimum octane aviation gasoline Engine limits For all operations, 1850 rpm (160 hp) Airspeed limits Level flight or climb - 132 mph True Ind. Glide or dive - 170 mph True Ind. Propeller limits Static rpm at maximum permissible throttle setting (+50 rpm) - not more than 1800, permissible.) Diameter - not more than 89 in. Diameter - not less than 86 in. C.G. range (+1862) to (+2206) Datum Wing leading edge Leveling means Inclinometer on left side (Serials 4 and up) lugs on left side of front Maximum weight (Serial 2) 2036 1bs. (Serials 3 and 4) 2180 1bs. (Serials 5 and up) 2120 1bs. No. seats 2 (one at +23 and one at +52) (See NOTE 2) Maximum baggage (Serial 2) 16 1bs. (wing compartments) (+23) (Serials 3 and up) None Fuel capacity 3-1/2 gallons (-22) gallons (tank in fuselage) (-7) Oil capacity Control surface movements Elevators - up 18 degrees, down 28 degrees; Elevator tabs - up 17; down 28 degrees Ailerons - up 25; down 25 degrees; Rudder - right 35 degrees; left 25.5 degrees (except serials 3 and 4 - 24.5 degrees right and lett Serial Nos. 2 and up eligible (See NOTE A Required equipment Item 101, 102, and 103 SPECIFICATIONS PERTINENT TO ALL MODELS: Certification basis Type Certificate No. 733 (CAR 4a) Production basis None (See NOTE A) Export eligibility Eligible for export as follows, subject to provisions of MOP 2-4: Canada - Landplane - eligible seaplane - not eligible (b) All other countries except Australia, Great Britain and New Zealand Equipment: (A plus (+) sign preceding the weight of an optional item indicates the new weight between the item and the equivalent Propeller and Propeller Accessories 101- Propeller - wood (fixed pitch) and hub (-51) Engines and Engine Accessories - Fuel and Oil System Kinner R-55 engine (same engine limits as R-5 Series 2) 21 1bs. (-38) Landing Gear and Floats 102- 7.00-8 wheels with brakes (Shinn 8C1FB) 55 lbs. (+2) 103- 8x3 steerable tail wheel and tire 3 lbs. (+207) NOTE A. Prior to original certification, each aircraft must satisfactorily pass: An inspection for workmanship, materials and conformity before any covering, metal priming or final finish is applied. All woodwork may be varnished. A final inspection of the completed aircraft. Check of flight characteristics including spin and stability test at rear C.G. and trim at forward C.G. Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions when necessary, must be in each aircraft at the time of original certificati and at all times thereafter. NOTE 2. Placard front cockpit, "Solo flying from rear seat only."