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
he key. Lapthe hub, using fine grinding compound, and continue lap-ping till the very best possible contact is obtained. Greatcare must be taken that the hub does not ride on the topof the key. The key should be replaced if damaged, .002 TightTapping fit desired.004 Loose■f////// ZZZZ Z TZZi.00 2… … 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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