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Aviation History
1936
1936 - 0620.PDF
MARCH 12, 1936. ADVERTISEMENTS. FLIGHT. 3 (jg(n gjlj3©EJ®@EB®i^®®EI0iHH®^l C~ 7> 3D 0 0 0 0 HD 0 0 0 03 CD 0 QD 03 0 0 0 03 0 0 AERO ENGINES The 80/90 h.p. CIRRUS a AA 1 u *\ w% ff INOR The photograph alongside shows clearly the extreme simplicity of the Cirrus "MINOR" design and the clean lines of the engine. It should offer no difficulty to the Private Owner who prefers to carry out his own maintenance, as it is one of the simplest engines yet produced. The compact arrangement of the accessories can be seen from the rear view * of the engine. Its compactness results n a low frontal area which permits good aerodynamic lines being obtained and also renders installation easy. All accessories are carefully placed so as to be readily accessible and the interior of the engine is easily exposed by removing the crankcase cover and timing cover which is split on the centre line to allow same to be lifted with the crankcase cover BRIEF SPECIFICATION Normal B.H.P. @ 2300 r.p.m. ... 82 Maximum B.H.PM 2600 r.p.m. ... 90 Petrol Cons. @ 2300 r.p.m. 31'4 Gals, per hour „ ,, @ 2600 r.p.m. 6'6l , Oil Consumption 1'H Pints „ „ Cruising Speed 2200-2300 r.p.m. Weight with Induction and Ignition system 195 lbs. ± 5 lbs. Cowling 4J lbs. Airscrew Hub 7\ lbs. Bearerfeetcpte 51 lbs. Fue! Pumps and Pipes41 lbs. Telephone : Brough 121. CIRRUS HERMES ENGINEERING CO. LTD. BROUGH, EAST YORKS. tniED IID 0300 003 QD0G311300 Cables : " Ocirruso, Broughyorks." Kindly mention "Flight" when corresponding with advertisers.
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