TCDS ATC 556

MODELS: Stinson A, 10 PCIM I.C. NUMBER: ATC 556 Ergines 3 Lycomir.gs R-680-B6 (See NOTE 5) Placard limits махі, except take-off 2100 rpm (225 hp) (one minute) 2300 rpm (245 hp) Placard speeds Level flight or climb - 202 mph True Ind. Glide or dive - 220 mph True Ind. Flaps extended - 112 mph True Placard ceiling 7650 ft. (density altitude) - Any engine inoperative (See NOTE 5) Fuel 220 gallons (four tanks: two 80 gallon wing tanks with let tank divided 20 and 60, and two 30 gallon tanks in outboard nacelles) Oil 15 gallons (three 5 gallon tanks) or 12 gallons (three 4 gallon tanks) No. passengers Baggage 500 1bs. aft in fuselage (Nacelle compartments may may be installed instead of fuel tanks, capacity of each 150 1bs. Maximum total 800 1bs.) Standard weight 10200 1bs. (See NOTE 5) C.G. limits (+4.6) and (+22.4) Specification basis Approved Type Certificate No. Serial numbers 9102 and up manufactured prior to 9/30/39 eligible. Approval expired as of that date. (See NOTES 2 and 3.) EQUIPMENT: (Datum is fuselage station 1 - first station aft of pilot's window and is in line with center line of wing front spar at fuselage) (* Means net Class I: Three engine ring cowls 78 1bs. wheel mud guards 10 1bs. Two landing lights 18 Ibs. 60 1bs. 20 lbs. Toilet compartment 40 ibs. Water container and water 14 1bs. Hot air heating system 9 ibs. (includes bonding and shielding) 174 1ks. 110. Battery (under pilot's compartment) 63 Its. Flares (one 3-minute and three 37 1bs. 36x15-6 wheels (Goodyear with Bendix power crakes) and 35x16-6 Heavy Duty (wheels must be placarded for these tires) 113. 12x5-3 tail wheel (Goodyear) with extra heavy duty tire (Wheel must be placarded for extra heavy duty tire.) 194. Delco-Remy retracting motor unit (including transmission) for landing gear and wing flaps with emergency hand crank for both flaps and gear 115. Propellers - controllable metal (Lycoming Smith P-220 hub and Pitts- Durgh B300SO blades) (See NOTFS 4 Class II: 200. Miscellaneous items as noted in approved Weight and Balance Report Class III: 301. Heavier gage fuel tanks 74 gallon capacity (replacing 80 gallon tanks) weight and Balance Report including list of equipment included ir certificated weight empty, and loading instructions when necessary, be submitted for each aircraft with original inspector's report and each subsequent report covering changes in such equipment. NOTE 2. Serial No. 9100 eligible as 9 PCIM with the following: Fuel 160 gallons (two at 80 gallons) oil 12 gallons No. passengers Baggage 800 1bs. (aft in fuselage 500 lbs. and nacelle compartments 150 1bs. each) EQUIPMENT: class I except - radio (two-way bs.. replaces co-pilot) 157 1bs., landing Lights 26 1bs., 3 starters 78 25 amp. generator 30 1bs. NOTE 3. Serial number 9101 designated as EXECUTIVE MODEL A eligible as PCIM with the following: Fuel 220 gallons oil 15 gallons No. passengers Baggage 400 1ks. (aft in fuselage) (Compartment must te placarded for reduction to 230 lts. when berth is occupied.) EQUIPMENT: class I except - radio (W.E. 208A two-way and motorola receiver) 205 lbs., berth, 4 swivel chairs, one fixed chair, card table and desk, cabin air- speed and altimeter, rug 46 1bs., entrance ladder 8 1bs., baggage compart- ment under berth. Propellers (Item 115) must have the following settings (include both 11.4 degrees and 15.4 degrees Outboard - 11.7 degrees and 15.7 degrees. Blades of serial numbers 3271 and up ONLY are eligible on this model. Also eligible with the following engine-propeller combinations: 3 Lycomings R-680-P2 Placard limits For all operations, 2000 rpm (240 hp) Adjustable metal, Hamilton Standard with 5B1-9 or 531-10 blades 79 1bs. each. Diameter 8'3" maximum, 8'1" minimum (low pitch settings - center 14.8 degrees, outboard 15.2 Placard ceiling Not determined Standard weight 3 Lycomings R-650-B5 Placard limits Maximum, except take-off 2000 pm (240 hp) Take-off (one minute) 2300 rpm (260 hp) Standard hubs 2B20, klades 6109A-9 or 6109A-10 105 1bs. each plus 10 1bs. each for Diametex 8'3-1/8" maximum, 817/8" controls (low pitch setting 14 degrees). Placard ceiling 5000 ft. density altitude - any engine inoperative NOTE 6. Eligible for export as follows subject to inspection for equipment specified in Chapter XII of Inspection Handbook (2/13/36) : - Landplane - Skiplane - not eligible. All other countries except Australia. NOTE 7. Also eligible with deflector tab installed on the outhoard flaps (two per airplane). No change in weights.