Is there an increased concern for stall safety in a 1G steep turn? Most people know the standard, "At a 60 degree bank, an aircraft experiences 2G's" checkpoint for load-factor on an airplane.

I assume that this statement has an underlying, unspoken assumption that the aircraft is maintaining a constant altitude in the bank.

This leads on to matters of increased stall speed during turns.

My question is, if no pitch adjustment is made while in a coordinated turn, which I think means that no additional load-factor is acting on the aircraft, is the stall speed still affected?
To fly a 60-degree bank coordinated turn with 1 G on the aircraft, you'll be dropping like a rock.

But your stall speed with 1 G on the aircraft is what it is, regardless of how you obtain that 1 G -- straight &amp; level, or coordinated turn with deceleration down to reduce the G loading, or inverted &amp; pulling 1 G... the angle of attack that stalls your wing will be reached at the same speed in all of those cases.