One thing that had me puzzled for a while is that while the firewall of the P-51H is clearly ahead of the wing, the firewalls of all other Mustangs intercept the wing.
This is true even on the LW Mustangs, which didn't have the leading edge kink, so their leading edges were further back. So why weren't their firewalls now ahead of the wing?
The reason is because of that change in firewall angle between the P-51D and XP-51F. This made the firewall more vertical and therefore it still intercepted the wing even though the kink was no longer there.
I'm in the middle of my Lightweight Mustangs book so not quite at liberty to share everything.
I can however answer some questions for you.
1. NAA changed the FS reference 'FS=0' several times then quit with the XP-51F/G/J & H. The change in FS=0 reference was first caused by the addition of Packard Merlin inst'l. The P-51B FS = 0 at 7.69" aft of Cowl/Spinner. NA-73 thru NA-99 F= 0 at 8"aft
2. With the right combination of drawings you can see that everything aft of the firewall, including location of the 25% chord line remains at FS=99. The Main Spar attach is at FS=104, IIRC the aft spar attach is FS= 143. The tip of the Spinner relative to the 25% chord line remained the same for all allison models, and the same for all Packard models - but very slightly different from each other.
So many parts were same or dimensionally the same from NA-73 through NA-122, with first major changes from upper longeron relationship with aft deck for P-51D.
3. Beginning with the XP-51F, the reference FS=0 was at tip of spinner.
4. The P-51H firewall did not move forward, the wing 25% chord line (and associated spar attach locations) moved aft. The aft fuselage frame assy was lengthened ~ 13", moving the empennage further away from the 25% chrd line, changing some stability derivatives - but necssary to accomodate the 50gal fuselage tank - with no aft cg issues.
5. From Spinner tip to 25% chord line
XP-51 = 133in
P-51B/D = 132.69in
XP-51F = 130.25in
XP-51G/NA-117 = 128.25 This was going into production but lack of fuselage tank forced change to the longer NA-126
XP-51J = 135.25
P-51H - 139.25
From these you can see that the first real 25% chord line changes (visually perceptible on a model) occurred with NA-105B and NA-126. The primary reason was inst'l of 50-gal fuse tank - which is why NA-117 died when AAF reguired the 85gal fuse tank for all post Jan 1 1944 deliveries. The H was accepted because it increased wing fuel to 205gal from 180 in the other LW Mustangs.
You have to be careful on XP-51F drawings. The first NA-105 dated Jan 1943 differed from final April 1943 as the wing changed from 45-100 to the final NACA 66. Interesting (to some) was the change from birdcage to bubble canopy occurred for both NA-106 and NA-105 in the same month.
You brought up a subject, namely mold techniques for canopy. I have only found obscure and unhelpful references to the summer 1943 two piece bubble canopy forned by 'draping' over mold, then moving to molded single piece - do you have a source I could go look at?
Regards,
Bill