Instruction regarding the 'N' Scheme 852 for the Goshawk II piston and connecting rod, putting a previous memo on hold.
| Identifier | ExFiles\Box 77\3\ scan0254 | |
| Date | 2nd May 1921 | |
| X4224 To BY from DA {Bernard Day - Chassis Design} /JHC. c. to HS. {Lord Ernest Hives - Chair} c. to TB (1 print). c. to RHC {R. H. Coverley - Production Engineer} (1 print). DA {Bernard Day - Chassis Design} /JHC1/FE2-5-21. X422-4 X 4223 PISTON AND CONNECTING ROD - GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) II. In accordance with Mr Day's instructions, please, proceed with "N" Scheme 852, with the exception of the oil pipe particulars of a revised wavy pipe will be supplied shortly. Memo E6/G31-3-21 instructing "that the connecting rods be made in M.S. and tapering in section" is in abeyance for the present. [Stamp: RECEIVED] [Handwritten initials: KVW, GH] DA {Bernard Day - Chassis Design} /JHC. | ||
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).