drgondog
Major
So, I pulled the IARCs for 41-37352 and 421 ---------> XP-51B #1 and #1 respectively.
#41-37353 (next prod # after XP-51B#1) was accepted 7 days earlier than 352 - on 8-18
The AAF selected factory deliveries of P-51-NA were interspersed with the ones produced for RAF but the last P-51-NA (41-37469 FD567 for RAF) were delivered 10-4-42. NOTE that ALL NA-91 were completed and delivered to AAF and RAF before the first Packard 1650-3 was sent from Wright Field bench tests. The span of actual staging and work on 352 (XP-51B) began earliest on or around 8-25-1942 and completed on October 1, ready for Merlin engine delivered on 10-18.
That said, both airframes were complete with contract cost of $41, 088 unit cost for each, same as the RAF destined Mustang IA.
I do not have a source for the disposition/trade to release the two Allison V-1710-39s Insalled in the completed airframes.
The acquisition costs for the agreed Packard V-1650s which were delivered to NAA October 8th (then failed in run up after installed on 352). The second delivered in November for 352, in which all early testing identifying the cooling issues experienced with the new design were achieved.
The third 1650-3 was delivered in February 1943 for 421 and first flight made by Chilton 3-9-43. 421 is the ship in which all the cooling systems and design changes to plenum, intake scoop geometry and lowered placement relative to frestream induced boundary layer - were made in April 1943. All the wind tunnel tests were at Ames on 421 which returned in late April to NAA.
Changes made during wind tunnel testing and real time modifications on 421, were quickly made to P-51B-1-NA 43-12093 in time for its first test flight on May 5th.
Following return both ships were flown to Eglin (5-12 for 421) and Wright Field (5-12 for 352).
BOTH were accepted on 8-25-1942. Same day. Design work (funded under NA-101 while AC-32073 was being finalized) began in late May 1942 and AAF committed V-1650-3s for the two ship product in June. Both airframes were identified at nearly the same time all committed Mustang IA had been completed and accepted. The first P-51-NA 41-37320 was accepted on 5-30 and Chilton flew first functional the next day.So is the idea 2 airframes were accepted as P-51 then modified and accepted a second time, but as XP-51B? Even though most references talk about 2 engineless airframes set aside?
#41-37353 (next prod # after XP-51B#1) was accepted 7 days earlier than 352 - on 8-18
The AAF selected factory deliveries of P-51-NA were interspersed with the ones produced for RAF but the last P-51-NA (41-37469 FD567 for RAF) were delivered 10-4-42. NOTE that ALL NA-91 were completed and delivered to AAF and RAF before the first Packard 1650-3 was sent from Wright Field bench tests. The span of actual staging and work on 352 (XP-51B) began earliest on or around 8-25-1942 and completed on October 1, ready for Merlin engine delivered on 10-18.
That said, both airframes were complete with contract cost of $41, 088 unit cost for each, same as the RAF destined Mustang IA.
I do not have a source for the disposition/trade to release the two Allison V-1710-39s Insalled in the completed airframes.
The acquisition costs for the agreed Packard V-1650s which were delivered to NAA October 8th (then failed in run up after installed on 352). The second delivered in November for 352, in which all early testing identifying the cooling issues experienced with the new design were achieved.
The third 1650-3 was delivered in February 1943 for 421 and first flight made by Chilton 3-9-43. 421 is the ship in which all the cooling systems and design changes to plenum, intake scoop geometry and lowered placement relative to frestream induced boundary layer - were made in April 1943. All the wind tunnel tests were at Ames on 421 which returned in late April to NAA.
Changes made during wind tunnel testing and real time modifications on 421, were quickly made to P-51B-1-NA 43-12093 in time for its first test flight on May 5th.
Following return both ships were flown to Eglin (5-12 for 421) and Wright Field (5-12 for 352).
Acceptance preceded physical Modification. Mods in Experimental Production hanger to accept 1650-3/Merlin 61 (Firewall forward and Doghouse and lower cowl, primarily) began immediately to be ready for the actual engine installation by October 1st,. See aboveSo you have not looked up whether the modifications were done before acceptance? Which is what the production reports indicate.
Yes, in the case of P-51D-NA and P-51D-1-NT as I have explained earlier. They were crafted from NA-102 Fuselage Spares and NA-106 production six gun wing. I also suspect P-51M was assembled from Fuselage and Wing spare from P-51D-20-NT pre-assembly invetory, then modified to install the 1650-9A.It is known a number of earlier P-51 were modified, and the August 1944 report for Inglewood states "84 accepted as P-51 but delivered as F-6" while F-6K acceptances started in November 1944, switching to D in March 1945. So advanced production could be before acceptance?
The designation 'XP-82 - quantity two' survived the cancellation of the 'P-82A-quantity two'. The original contract and charge number was for four P-82. The P-82A was designed for a Packard Merlin 1650-11/21, Ditto P-82B, ditto P-82C and D. P-82E was first to be forced to install the doggy Allisons with aux second stage supercharger. On this last point I emailed Bob Gurenhagen to se if the C and D, in addition to the new radar mods - may have also installed Allisons to replace Merlins.Meantime the RC-301 reports have FP AC-2029 for 2 XP-82 and 2 XP-82A from Inglewood, with the 2 XP-82 accepted by end September 1945 and the XP-82 moved to unsheduled and as is known ultimately not built. Various references talk about the A being Allison powered prototypes. What is the explanation for the lack of a P-82A?
Oh yes, you must be very good.One of the things I note is the way go look up X is never accompanied with details of where X is and how it can be accessed. And apparently I am so good I can look at all that documentation in a few days.
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