Here are some differences from Lycoming document SSP-289, dated July, 1989.
The HIO-360B1A has a compression ratio of 8.50:1 and is rated at 180 HP at 2900 rpm. It has a Bendix injection system with a dual diapham fuel pump. The engine must have been used in a helicopter and probably ran at 2900 rpm most of its life.
The base 0-360-B1A was 168 HP that ran on 80 octane fuel.
The IO-360-B1A was 180 HP with a Simmons FI system.
Can't tell you anything about exhaust system or how it fits, but for sure you will not have 180 HP at 2700 rpm.
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