Specification sheet for Kestrel FS 6 cylinder Unit No. 2.
| Identifier | ExFiles\Box 54\4\ Scan146 | |
| Date | 30th May 1933 | |
| 84659. To Hs. {Lord Ernest Hives - Chair} from RHC {R. H. Coverley - Production Engineer} /WSC. {W. S. Cassel} c. Hs {Lord Ernest Hives - Chair} /Ryc. RHC {R. H. Coverley - Production Engineer} /WSC. {W. S. Cassel} 9/AP.30.5.33. Kestrel(Aero Engine) FS. {F. Steele} 6 cylinder Unit No.2. We give herewith complete specification of the above Unit:- Passed to Test. 24.5.33. Crankcase & Bearings LOP.E.36040. New, complete to the above LOP. E.36596/2 Crankcase (T.H.) E.33041/1 " (L.H.) E.40163/4/5/6/7/8 Lead Bronze Main bearings incorporating Oil grooves to Ex.10410 except No.7. The following parts fitted to "A" side only:- 4-E.40337 Studs. 10-E.38707 Clamps. 10-E.38708 Nuts-BZ/A. 10-E.38709 Studs. The following new parts fitted to suit increased capacity Oil Pumps. 2-E.28190 Stud. 1-E.28194 Stud. 1-E.28191 " 1-E.41154 " 1-E.28192 " 1-E.41159 " Crankshaft LOP.E.35857-DES.1447. New, Complete to the above LOP. & Scheme. 1-E.32052/1 Crankshaft. The following parts fitted to suit Direct Drive. 1-E.29509 Bush. 1-E.29511 Flange. continued. | ||
From the Rolls-Royce experimental archive: a quarter of a million communications from Rolls-Royce, 1906 to 1960's. Documents from the Sir Henry Royce Memorial Foundation (SHRMF).