The key has been touched upon a couple times here. When a rotary wing aircraft's attitude exceed 90 degrees from horizonal it must maintain positive G's, allowing only momentary successful flight beyond that 90 degree point. Helicopters such as the UH-1, OH-58, AH-1, etc., with their two bladed, semi-rigid, underslung rotor head (my old friend Rex Reinl used to call it the semi-ridiculous rotor system) will encounter a condition called mast bumping when the rotor disc is unloaded (approaching zero G's). At normal RPM (approx. 320) the hub of the two blades contact the mast approximately 11 times per second, which is about how long it takes the rotor to become a free flying frisbee and the fuselage to achieve the aerodynamic properties of a brick.
A maneuver called return to target will be familiar to gun ship pilots. That maneuver pushes the limits of the above named aircraft when it comes to unloading the rotor system. There are other things that can induce mast bumping, and in fact, I lost a friend in 1980 who lost his rotor right in front of me while he was doing emergency maneuver training in a UH-1H. All four in the aircraft died.
The fully articulated rotor system, as used in the UH-60, AH-64, etc., etc. are not subject to mast bumping and therefore can unload the system without catastrophic results. However, rolling a UH-60 in CONTROLLED flight does require maintaining positive G forces throughout the maneuver, which, of course, requires quite a lot of spare altitude, because some power must be applied throughout.
I never rolled a Blackhawk because that was against regulation AR-95-1.

Lift counters gravity/ thrust counters drag, until you are inverted,
A maneuver called return to target will be familiar to gun ship pilots. That maneuver pushes the limits of the above named aircraft when it comes to unloading the rotor system. There are other things that can induce mast bumping, and in fact, I lost a friend in 1980 who lost his rotor right in front of me while he was doing emergency maneuver training in a UH-1H. All four in the aircraft died.
The fully articulated rotor system, as used in the UH-60, AH-64, etc., etc. are not subject to mast bumping and therefore can unload the system without catastrophic results. However, rolling a UH-60 in CONTROLLED flight does require maintaining positive G forces throughout the maneuver, which, of course, requires quite a lot of spare altitude, because some power must be applied throughout.
I never rolled a Blackhawk because that was against regulation AR-95-1.


Lift counters gravity/ thrust counters drag, until you are inverted,
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