If it is pitching hard be careful not to pull to hard or the flight controls may stall. They are designed to stall outside of coffin corner ,to protect the airplane from self destruction from excessive g loading.
My gosh, ah no...
Some basic facts:
A stabilator flight control may stall - at very slow airspeed. Otherwise stalling flight controls won't be a factor in dive recoveries, because before a flight control could stall in a dive, the plane would have disintegrated from being overstressed.
I'll defer to a jet pilot, which I am not, but I believe that "coffin corner" is a term associated with high altitude cruise flight, not dive recovery. "Coffin corner" is a 1.0 G flight condition.
An airfoil/aerodynamic surface stalls at high AoA's, which are generally associated with slower speeds. As airspeed increases, the amount of flight control displacement needed to affect an attitude change reduces.
Excessive G loading can only occur at fast speeds. Flight controls become much more effective at fast speeds - which is why at speed, overstressing the plane is a risk, stalling the elevator is not.
Let's review some aircraft design fundamentals:
Va maneuvering speed is established for pitch attitude change (not yaw or roll). Slower than Va, gentle application of full nose up pitch control will result in the wing stalling before the G structural limit is reached. This protects the aircraft from overstressing, if the pilot flies with this speed as a self imposed limit. This speed has less to do with the effectiveness of the tail/flight controls, than it does with the ability of the wing to develop lift with speed. None the less, stalling a GA plane at Va is scary stuff!
So,
be careful not to pull to hard
, if you can determine what "too hard" would be without a G meter. Va is a reference, but that's still a risky approach. On the other hand, while referring to an appropriate means of determining G, if you're diving, pull hard enough! If you don't, you're not coming out of the dive, and speed will build up to a very unsafe condition. Once you've allowed the plane to exceed Va in a dive, you're only going to slow by pulling pitch - a lot!
Therefore, the best thing to do, is to assure that you do not allow a plane to be in a dive, in which Va is exceeded early in the dive. If you re in a dive, and accelerating, pull enough G within limits to prevent accelerating above Va if you can. If you have ended up up side down from anything like cruise flight speeds, and you are maintaining any positive G, you're building up speed fast, you have nanoseconds to make it better before it gets worst because the plane sped up too quickly to prevent.
This is why I like the roll out approach, as entering a roll from inverted does not put the plane in an attitude which will promote acceleration as fast as a dive does, and, you have a better chance of safely rolling out above Va. Erring with application of aileron and rudder in GA aircraft above Va is not as dangerous as getting the pitch control application wrong.
But all of this is on the edge of dangerous in any certified aircraft, do not take this casually, and don't experiment 'cause you read about it here - get competent instruction!