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 85
ches and forwear. Slight damage may be removed with a very finefile. In fitting new vanes the greatest care must be takento insure that they work through the slot in the shaftquite smoothly without shake. The two springs which Tola I side clearance.001 Min..004 desired007 Max Shaft with side ofbody… … End ClearanceVanes in b.001 Min..002 desired.003 Max. End Clearance in Shaft .OOlMm. .004 Loose desired .007Max. Oil pump and release valve fits for Models E and I .0005Loose desired.001 Max. End clearance Total f~\of assembly.004 Min..008 desired Key Top Clearance 002 C/earonce O08 Clearance…
Airplanes
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