Design modifications for the 'Goshawk II' rear springs and fittings.
| Identifier | WestWitteringFiles\F\April1921\ Scan42 | |
| Date | 25th April 1921 | |
| To BY. {R.W. Bailey - Chief Engineer} from E. {Mr Elliott - Chief Engineer} copy to CG. " " HB. {C. E. Harcombe} ORIGINAL EL/G25/4/21. 2 XHR 62 RE "GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) II" REAR SPRINGS AND FITTINGS: In reply to your memo BY {R.W. Bailey - Chief Engineer} /P22/4/21, kindly note Mr. Royce would like to adopt the suggestion to use finishing dies, and merely grind up the faces of the bosses on the spring pin bracket, and he wishes the bracket to be reduced in width to, say, .875" throughout. The brake cables should remain at their present centres. E. {Mr Elliott - Chief Engineer} | ||
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).