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Aviation History
1934
1934 - 0534.PDF
FLIGHT, MAY 31, 1934 THE BUSINESS END : The Siddeley " Lynx " is enclosed in a N.A.C.A. cowling. An electric starter is fitted. THE AVRO "COMMODORE" 215 h.p. Siddeley "Lynx" Engine Dimensions Length o.a. Height o.a. Wing span (both) Wing chord (both) Gap Dihedral angle Angle of incidence ft. 27 10 37 4 5 2 • 5 deg. 3-25 deg. in. 3 0 4 9 3 Areas Wings (incl. ailerons) Ailerons (total) . . Tail plane and elevator Rudder Fin sq. ft. 307-0 31 -5 39-6 120 3-3 m 8,33) (3,05) UJO) (1,45) (1,60) (28,5) (2,92) (3,67) (1.11)(0,31) Weights Tare weight, incl. cabin furnishing Pilot 3 Passengers at 160 lb. Baggage Fuel (49 gals. = 2231)Oil (5 gals. = 23 I) Total disposable loadGross weight Wing loading Power loading 1b. 2,225 160 480 209 377 49 1,275 3,500 10-82 lb/sq. ft15-45 lb/h.p. Performance "g-(1 009) (72,5)(217,7) (94,8)(170,9) (22,2)(578) (1 587) (5,28 kgltn7,02 kgjCV) 130m.p.h. 209km\h.Max. speed at sea level . .„ 5,000 ft. (1 524 m.) „ 10,000 ft. (3 048 m.Cruising speed at 1,000 ft. (305 m. Landing speed Initial rate of climb . . 700 ft Time to 1,000 ft. (305 m.) 1 -60 min. „ 5,000 ft. (1524 m.) 9-50 min. „ 10,000 ft. (3 048 m.) 28-00 min. ...:: Service ceiling .. . . 11,500 ft. (3 505 m. 124 115 110 50 (200 (185 (177 (80 /min. (3,57 mjsec.) The larger sketch shows the arrangement of the main fuselage and wing structure members, while the smaller sketches illustrate some of the details. 534
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