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The wear measurements for engine bores and pistons for chassis B 60 FB.


Identifier  ExFiles\Box 144\3\  scan0046
Date  13th March 1936
  
REPORT RE WEAR IN BORES & PISTONS.

Fitter: Trotts
Chassis No: B 60 FB
Date: 13. 3. 36
Job No.: 3182
Mileage: 3120

BORES TABLE
NOMINAL. | TAPER. | OVAL.
1: 3.250" S | + .0035" | .0005"
2: S | + .003" | NIL"
3: S | + .0035" | NIL
4: S | + .003" | NIL
5: S | + .003" | .001"
6: S | + .0025" | .0005"

S/sc Satisfactory.

PISTONS TABLE (Aerolite F.B. 2441)
TOP. thrust | BOTTOM. thrust
1: - .004" | - .004"
2: - .004" | - .003"
3: - .004" | - .004"
4: - .004" | - .004"
5: - .004" | - .003"
6: - .004" | - .004"

Signature: JOD
  
  
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).


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