TCDS TC 2-566

FLEET AIRCRAFT, LTD. MODELS: Fleet 16E (?CAF Finch II), 2 PO-CLB I.C. NUMBER: 2-566 Engine Kinner E-5 Fuel 73 mininum octane (CF9) ariation gasoline Engine limits For all operations, 1925 rpm (125 hp) Airspeed limits Level flight or clinb - 105 nph True Ind. Glide or dive - 135 nph True Ind. Propeller limits (See NOTE 3) C.G. range (-1.93) (25.0 percent MAC) to (+2.89) (35.9 percent MAC) Datum MAC 44 in. L.1. MAC (-12.93) at 2o00 MAC (-12.93) Leveling means Bottom of top longeron in front cockpit Maximum weight 1878 1bs. No. seats 2 (+9.5) and (+39.5) Baggage 104 lbs. maximum (See NOTE 1) Fuel capacity 32 gallons (-9.5) Oil capacity 3 gallons (-19) Control surface Ailerons movements 23 degrees up 1 2 degrees 15 degrees down + 2 degrees Elevator • 36 degrees up + 3 degrees 24 degrees down 1 3 degrees Rudder 41 degrees right + 3 degrees 43 degrees left t 3 degrees 4 degrees up + 1 degree 4 degrees down ‡ 1 degree Certification basis Canadian Certificate of Airvorthiness for Export Serial Nos. All eligible in accordance with the provisions of Required equipment Items 1, 101, 102, 201, 202, 401, 402 EQUIPMENT: (Items included under "Required equipment" may not be removed unless replaced by approved equivalent items. The effect upon balance of all equipment changes must be computed and the aircraft operation record revised accordingly.) Propellers and Propeller Accessories: Propeller fixed pitch wood (See NOTE 3) (-62) Engine and Engine Accessories (Fuel and Oil System 101. cooler (integral with oil tank) (-19) 102- Carburetor air heater 103. Carburetor air filter - Air Maze 106. Staket heater se haust type electric Landing Gear 201. 7.50-10 wheels and brakes (Kelsey Wheel Co. Model 750A) 202. 10x3 tail wheel Electrical and Radio Equipment None Interior Equipment 401. First air kit 402. Safety belt Model L-RCAF Miscellaneous (not listed above) Miscellaneous items as noted in approve! weight and balance report NOTE A. The Canadian Certificate of Airworthiness for Export nust be subnitted for each individual aircraft for which application for certification is made and each aircraft shall be inspected by a C.A.A. inspector. NOTE 1. The following placards must be appropriately displayed: "Intentional Spinning Prohibited. "Solo From Front Seat Only." 'Mininun of Ibs. necessary in baggage compartment for solo flight.i "Maximum of Ibs. permitted in baggage compartment when passenger is carried. With regard to Items (3) and (4) the C.A.A. inspector shall determine for each aircraft the amount of ballast, if any, which is necessary in the baggage compartment when the airplane is flown solo and also the maxinun baggage permissible when a passenger is carried. NOTE 2. Aircraft should be checked for contormity with the following: (1) Rigging specifications: Dinedral o degrees upper, 4 degrees lower Stagger 23 inches Gap 54 inches at center Sweepback 0 Fuel and oil placards: "fuel 32 gals." and "73 octane" should be marked adjacent to the fuel tank filler opening. The words "oil 3 gals." should be marked adjacent to the oil filler All openings in and around firewall should be sealed. Placard the fuse ratings on the fuse panel and provide a master switch or remove the battery and battery box, if any, fron the Cockpit instruments should be marked to indicate the proper airspeed and engine limitations. The tollowing Canadian-approved propellers are eliqible. rpm limits need be specified if one of these propellers is used. Canadian Vickers wood propeller (Drawing No. 3435 Diameter - 87 in. to 90 in. (2) S. and S. Wood propeller (Drawing No. 1242) Diameter - 89 in. to 92 in. (3) Hartzell wood propeller models 409, 6713 or 671C with hub for 7/15 inch diameter bolts. If any other fixed pitch wood propeller is used, the following limits shall iameter - not more than 92 in.; not less than 89 in. static rpm - not more than 1650: not less than 1650