gdan454 wrote:
Good grief! Nothing could be further from the truth. Of the three surfaces on the empennage, left horizontal stab/elevator, right horizontal stab/elevator and vertical stab/rudder, the one you may definitely not live without is the vertical fin. The R-2800's torque coupled with the gyroscopic force of the 13.5 foot diameter prop makes it impossible to survive without the directional control provided by the rudder/fin. You will certainly find that F4U's along with other piston engine aircraft have made successful returns with almost the entire left or right horizontal stab/elevator missing. This condition can be controlled with judicious use of aileron and rudder along with the help of the trims. Had the vertical stab been reduced much further than what is pictured, the aircraft would have been uncontrollable under high power settings due to the engine/prop physics. The aircraft would have begun snap-rolls probably followed by the pilot exiting the aircraft after reducing power, which would have most likely resulted in a flat spin. In my time, I have never found that an aircraft, piston or jet, minus the vertical stab has ever survived.
The one correct statement here is that a wave-off or bolter in my time, would have been most likely unsuccessful due to the reduced rudder/stab surface area.
If the aircraft landed this way, I'd say the photo refutes your statement. If so, without a doubt, great airmanship on the part of the pilot. The vertical stab appears completely intact although probably 50-60% of the rudder is missing. What remains appears operable as the rudder is displaced to the left slightly.
The fuselage provides some longitudinal stability/weathervaning. The seas appear relatively calm. Low power setting and presuming a return to the ship at altitude. Looks like he did a great job.
I would agree that a bolter would not be an option. Did carriers of this era have the barricades yet?
Caveat: this presumes the aircraft landed like this and was not chomped-on by the prop of the aircraft behind it.