TCDS TC 2-574

CANADIAN VICKERS, LTD. MODELS: Canadian Vickers Stranraer, 3 PCPOB I.C. NUMBER: 2-574 (Approved 10/15/45) (Manufacturer: Canadian Vickers Itd., Montreal, Canada) Engines Fuel 91 minimum octane (CFR) aviation gasoline Engine limits except take-off 35 in. Hg., 2250 rpm (790 hp) (4000 ft.) 35 in. Hg.. 2250 Ipm (825 h. Airspeed limits rever fiight of climb'- 2600 Ipm (1010 hp) Glide or dive - 141 knots True Ind. C.G. range Datum Leveling means 16 ft. 6 in. aft of hull nose Leveling lugs on outside port side of hub (0" Maximum weight No. of seats Paggage Fuel capacity 590 gallons (2 tanks 295 gallons each (+50.6), left and right upper center wing) oil capacity 57.6 gallons (2 tanks 28.8 gallons each (+20.2), leading edge of left and right upper center Control surface movements Elevator - Up 24 degrees, Down 20.5 degrees Elevator trim tab - 14 degrees up and dowr Aileron - 19 degrees up and down Rudder * 28 degrees left and right Rudder trim tab - 11 degrees left and right Rudder balance tab - 13.5 degrees left Serial Nos. eligible All in accordance with the provisions of NOTE A. Required equipment Certification basis Canadian Certificate of Airvorthiness for Export (Items included in required lists under specifications pertinent to individual models may not be removed unless replaced by approved equiralent items. The effect upon balance of all equipment changes must be computed and the aircraft operation record revised accordingly. Values in inches shown in parenthesis after each item represent horizontal arms to the C.G. of the item measured minus (-) ahead and plus (+) or minus (-) sign preceding the weight of an optional item indicates the net weight change between that item and the equivalent required item. Propellers and Propeller Accessories Propellers DeHavilland 5/37A hubs, P55253/3 blades Low pitch 24.5 dogrees at 42 station High pitch 31 degrees at 42 station Engine and Engine Accessories - Puel and Oil System Two starters (Eclipse E-160) (+2) Two fuel pumps (Bristol Dual Vane PB66233/2) Two oil coolers (U.A.P. 0-316Q-DS) Cylinder head temperature gauges 105. Carburetor air heat control valve Landing Gear None Electrical and Radio Equipment 301. Generator (G.E. Type A) (+50) 302. Battery (Exide, Canadian 5J/1391) 50 1bs. (+60) 303- Radio transmitter (Northern elective AT-1) (-120) 304- Radio receiver (Canadian Marconi AR-2) (-120) Interior Equipment 401. Approved operating manual (See NOTE 1) Dual controls 14 Ibs. (-94-5) Miscellaneous (not listed above) 600- Miscellaneous items as noted under this item in approved weight and balance report NOTE A. The Canadian Certificate of Airworthiness for Export must be submitted for each individual aircraft for which application for certifi- cation is made and each aircraft shall be inspected by a C.A.A. inspector. The following placard must be installed on the instrument panel in full view of the pilot: "This Airplane Shall be Operated in Accordance with Part I of the C.A.A. Approved Operating Manual for Canadian Vickers Stranraer Flying Boat. certification the following must be accomplished: The elevator trim tab control must be marked to indicate direction of rotation. The instruments must be marked for approved limits. Fuel and oil filler caps must be marked as to contents and capacity Firewalls of one of the following types must be provided: A single sheet of terne-plate not less than 0.028 in. single sheet of stainless steel not less than 0.015 in. Two sheets of aluminum or aluminum alloy not less than 0.02 in. thick fastened together and having between them an asbestos paper or asbestos fabric sheet at least 1/8 in. thick. identification plate must be permanently affixed in a visible location in the pilot's compartment. This plate must contain the manufacturer's name, the date of manufacture, the manufacturer's serial number and the model designation. A suitable identification plate should be permanently attached to the engine in a locaticn which will be readily accessible when the This plate should contain the manufacturer's name, engine name and model, serial number, crankshaft speed (METO and take-off) and power. Propellers should be identified with permanent data containing the following: propeller name and model, These data may be printed or painted in a prominent location of a non-critical surface of the hub and blade. All cargo and baggage compartments must be placarded for the maximum permissible floor Floor beams and flooring provided for such compartments should be capable of withstanding a limit load factor of 4.33 without undue permanent deformation and must have sufficient strength to withstand an ultimate load factor of Adequate cargo tie-downs must be provided. dump valves should be made inoperative. Individual landing light switches must be provided if certificated for night operation.