 | Prototype block #1 pictured. First step was to fit crank, check all tapped holes, deburr, dry fit etc. I smoothed out and enlarged all oil returns. When spraying wd40, certain areas of the block will retain oil, and of course getting the oil back to the sump is important. |
 | All work is prior to machine shop. Decks were not cut yet.
Pictured here is dip stick hole I tapped with 1/4 npt to plug. Using Canton pan with external dip stick provision. |
 | Pictured next is the large bore head gasket in place. This particular block had the coolant holes repaired, not an issue with the production run. Block was sonic tested and bores have plenty of meat with 4.350 bore. There was core shift, though and Allpontiac is addressing that issue as well. Keep in mind this block is a prototype and all minor issues are being addressed. Of the 3 blocks being tested, all info is being compaired and addressed - pretty impressive - gotta love what these guys are doing to get a quality product out there. |
 | Great news! The IA2 block is machined and ready for assembly. Everything checked out. Pressure test was good. No porosity. The arrow points to the clutch ball threads I tapped to plug. It's a reminder to reinstall plug. The machining went through to the coolant. Not a problem for the production run. The oil pan rail has the torque specs for use with moly. A nice time saver on freshen-ups. |
 | Next is a photo of the hone of the bore with proper cross hatch for moly rings (being used). As I recall, like just about every new aftermarket block out there, (for the brand X's) you will need to deck, bore, hone (with plate- I hope everyone does), and the saddles may need to be line honed depending on builders choice/clearance desired. To make sure this block checked out ok, many operations were done. Sonic checked, pressure tested, cleaned, preassembled, clearancing, etc. Everything checked out good (some improvements are being implemented) so the machining cost was higher than what a production block would run. |
 | Eagle crank 3" journal 4.250 stroke. Weight added during balance, checked for cracks and straightness, polished journals to achieve clearance (was too tight from Eagle), semi-polished thrust area, polished seal area. |