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Condition and bore dimensions of six engine cylinders after a first grind out.


Identifier  ExFiles\Box 146\3\  scan0091
Date  22th September 1936
  
B
REPORT UPON CONDITION OF CYLINDERS
CHASSIS N° B-38-EF.
JOB N° 35620.
DATE 22/9/36.
MILEAGE 37,114 HMS.
1ST GRIND OUT
ORIGINAL BORES YES.
Please refer to sheet 'A' attached
CYLINDER BORE DIMENSIONS
NOTE {
DIM'S "AA {D. Abbot Anderson} " TAKEN AT RT ANGLES TO C' SHAFT.
DIM'S "BB" TAKEN PARALLEL TO C' SHAFT.
Note the "AA {D. Abbot Anderson} " & BB measurements taken at the crown were taken .500" below the face of the Cylinder Block. Please refer to sheet A attached
TABLE DATA:
CYLINDER | MOUTH | CENTRE | CROWN
CYLINDER | AA {D. Abbot Anderson} | BB | OVALITY | WEAR | AA {D. Abbot Anderson} | BB | OVALITY | WEAR | AA {D. Abbot Anderson} | BB | OVALITY | WEAR
1 | NEW | | | | | | | | 3.253 | 3.255 | |
2 | NEW | | | | | | | | 3.253 | 3.255 | |
3 | NEW | | | | | | | | 3.2535 | 3.255 | |
4 | NEW | | | | | | | | 3.2535 | 3.256 | |
5 | NEW | | | | | | | | 3.253 | 3.254 | |
6 | NEW | | | | | | | | 3.253 | 3.2545 | |
  
  
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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