Now that the unexpected engine change on the T-6G is done that is up and running and I have moved onto the Spitfire to prepare it for Reading.
The Griffon ate up a Cam Lobe on the A bank. It was discovered in the fall by inspection and has been parked in one of the multiple corners in the hangar since.
(I think Jim's next hangar will be a circular structure so there are no corners. No corners, no broke airplanes sitting in a corner. It's logical at least.)
The Finger that the cam lobe displaces has a contact pad coated in a layer of hard chrome. If that chrome breaks down and flakes off it becomes a cutting tool and erodes the cam lobe.
Finger showing that damage-


The damage to the cam lobe-


We have some NOS cam racks but they are for the B side. We had Roush NDT and polish a set of cams. Both A and B cams are the same P/N in a Griffon. They are the same part number.
The puzzle begins with fitting the cam racks to an engine. I had hoped it would just pop in but clearances have to be set up for each set of fingers. There are 12 sets of fingers on each cam rack.
New clearances are .005" - .010". Book says max is .020. The bigger the clearance the more oil you lose so this is an important step.
Measuring clearance on a set of fingers in place on the engine-
The shims come in different thicknesses varying by a little as a .001".
Box of spacers and shims-

Hopefully we can run this afternoon.
Rich