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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).
Four tests conducted on a Rear Shock Damper for Chassis 18-G-IV.

Identifier  ExFiles\Box 5a\2\  02-page359
Date  24th December 1930
  
x5840.

To Hs{Lord Ernest Hives - Chair}/Rm.{William Robotham - Chief Engineer}
From G.W.H.

Hotel de France,
Chateauroux,
France.

24/12/30.

Re Chassis 18-G-IV.

We yesterday carried out tests on the Rear Shock Damper to verify the results taken at Cricklewood. The results were very similiar to those tests taken.

1.st Test
With valve drilled .055", valve ball left .010". Result O.K.

2.nd Test
Air vent enlarged to .156" diameter, ball valve restricted to .004", standard valve .031" hole. Result, free from knocks but movement can be felt at end of lever.

3.rd Test
Air vent enlarged to .156" diameter, ball valve restricted to .004", with undrilled valve. Result O.K.

4.th Test
Ball taken out of valve, standard valve fitted .031" hole. Shock damper filled with oil. Result O.K.

G.W.H.
[Signature]
  
  


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