Noticed something in the photos...Might be caused by poor photo quality, but they don't all look bad enough not to show this.
First, look at photo 22. The pilot is clearly visible in the cockpit and is fairly well forward of the rear cockpit bulkhead.
Next note photo 3. You can see the union of the front and rear canopy sections, but no pilot is visible. Several photos do not show the pilot, but this is the best one and the others maybe distorted.
I'm not saying he isn't in there, but where he able, he would be visible at the controls trying to fly out of the stall.
I guess the high G's of the initial pitch up may have knocked him out and he is slumped out of sight. Or he could be cringing, knowing the end is coming.....these guys aren't cringes by nature, though
http://news.yahoo.com/photos/air-race-crash-in-reno-1316226189-slideshow/friday-sept-16-2011-photo-p-51-mustang-photo-231406637.html#crsl=%252Fphotos%252Fair-race-crash-in-reno-1316226189-slideshow%252Ffriday-sept-16-2011-photo-p-51-mustang-photo-231406637.htmlI agree. In photo #9 with the aircraft inverted moments before the crash, his head is clearly visible right up against the instrument panel. (Not a natural flying position in the least.) In photo #10 he is not visible at all. Cockpit canopies in these aircraft are very small. He could very well have been incapacitated at this point. Also notice the tail wheel is retracted fully down, but the main gear is fully retracted in the up position?
On a P-51 The main gear doors are hanging open when the plane is parked at the ramp. As soon as the engine starts, and the hydraulic pump starts to build hydraulic pressure, the main gear doors immediately retract up. When the gear is retracted after takeoff the main gear folds in after the wheel well doors reopen, and then retract last to cover the wheel well completely after the main gear folds in. The tail wheel retracts with the main gear while all of this is going on. There is no reason for the tail wheel to deploy with the main gear up.
In photo #11 taken just a moment before impact you get a clear view of the canopy, yet again without the pilots head visible at all. The same appears in a larger photo #12. In photo #27 showing the plane taxing on the ramp, his head takes up almost 2/3rds of the canopy in a normal upright seated position as the pilot would be during the entire course of the flight. As was mentioned their helmets are constantly banging into the canopy during flight because of the limited visibility of these small, teardrop designed canopies. If you look at any of these airplanes parked at the ramp, the inside of the canopies around the pilots head are heavily scratched from this constant contact with the pilots helmet.
Again, if you look at photos # 10, 11, and 12, they show zero up elevator input while the plane was in a full power on dive. The plane descended in a straight down fashion right up until impact. He proved he had elevator control just before because he pulled up into a near vertical climb after announcing a "Mayday" call on the radio. So there was no doubt he had full elevator control then. As the plane went inverted you can see his head up against the panel, then moments later after the plane went into near vertical decent, you cannot see him at all. During all of this he had full power on with zero up elevator input.
It appears at this point he became incapacitated during the high G-load pull up. There was also no reason for him to allow the plane to go inverted over the top in an emergency situation like it did. You can also see in photo #9 in addition to his head being right up against the panel, there is clearly right stick input being applied by looking at the position of the ailerons. These aircraft under normal race conditions pull 3.5+ G's around the pylons. In a high speed pull up with full power they can easily exceed 6 G's. I'm guessing at some point in this crash investigation, they'll find he became incapacitated. Another thing is the trim tab fell off long before he executed the high G pull up because it was found on the course, a long distance away from the crash site, so based on his ability to perform that maneuver, it didn't appear to cause any loss of elevator control in the moments leading up to the crash due to the trim tab separating from the aircraft. Bill T.