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
Min. end clearance .010- Flange must registerin cylinder jacket. ^Oil tight joint Clearances, fits and tolerances for all models Camshaft bearings shouldbe line reamed 002 Min. 003 Loose desired 004 Max. /////i/iii/iil
Airplanes
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