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 58
bolting down. 2. The holes in the bed timbers for the bolts should bea tight fit, so that the bolts require to be driven in. Thespacing of the holes should be sufficiently accurate toallow the engine to set readily over the bolts. 3. Cut two fiber strips about ^\-inch thick. Mark offand drill… … Showing proper method of attaching rope for lifting engine 6. Apply second washer and nut to all bolts. 7. Tighten down nuts gradually and in rotation. Neverdraw up any one nut much tighter than the next. 8. Apply cotter pins of correct size and make sure theyare well spread. Attaching Controls…
Airplanes
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