Thanks guys,
I did a little more research I found the following:
O-360-
A1A180 hp (134 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL
avgas, compression ratio 8.50:1. The base model. A four cylinder, horizontally opposed, air cooled, direct drive engine which includes provisions for supplying oil through the propeller shaft for installation of a single-acting controllable pitch propeller. First certified 20 July 1955.
O-360-
A1AD180 hp (134 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.50:1. Same as the A1A except it is equipped with a Bendix D4LN-2021 dual magneto instead of two single magnetos.
O-360-
A1C180 hp (134 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.50:1. Same as the A1A except with a rear mounted Bendix carburetor and 200 series magnetos.
O-360-
A1D180 hp (134 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.50:1.
Same as the A1A except with Bendix 200 series magnetos.
Maybe this will be of some help to someone else besides me.