Mr. Royce's suggestion for an adjustment to the Goshawk 11 battery ignition HT moulding.
| Identifier | WestWitteringFiles\I\May1922\ Scan87 | |
| Date | 23th May 1922 | |
| To Hy. {Tom Haldenby - Plant Engineer} from E. {Mr Elliott - Chief Engineer} c. to GDT. c. to Dor. {Mr Dorey} c. to HS. {Lord Ernest Hives - Chair} ✓ c. to RWH. c. to PF- ORIGINAL Hs {Lord Ernest Hives - Chair} MAY 24 1922 REC'VED Seen HS {Lord Ernest Hives - Chair} E4/M23.5.22. X 43 57. GOSHAWK(Aero Engine)(Codename for 20HP Car / Aero Engine after Kestrel(Aero Engine)) 11. BATTERY IGNITION. With reference to the trouble due to the HT. moulding on the above being tight on the spigot, Mr.Royce suggests that we should definitely make these 5/1000 slack as he does not think the moulding being 2 1/2/1000 out of centre would give rise to any appreciable disadvantage as regards the HT. points. 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).
