Wright aircraft engines; complete instructions for their installation, operation and maintenance; (1921)
Wright Aeronautical Corporation, Cautley, John R., ed · Paterson, N.J., Wright aeronautical corporation · leaf 80
Oil Moles in /leading side of cam Tapping Fit.001 desired Loose002Loose Max. .000 .0015Tight desired 003 Tight Max. .000 to .001 clearance.000to .004Clearance … cross section of camshaftbrg. 58 WRIGHT AERONAUTICAL ENGINES should be tight in the shaft, and the hub should be a goodsliding fit. Hubs which are not perfectly bedded downto the taper end of the shaft will always work in ser-vice and this causes roughness to develop which mayeasily lock the two…
Airplanes
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