The first testbed, as Jon pointed out, was a civil airframe. It was assigned a DOD serial number and was pulled off the Bell production line. The nose FM posts generally were not part of the civil package to my knowledge, I'll have to do some research. Maybe they were or maybe they were retrofitted. It's quite possible that is in fact the civil airframe because Hughes retained the airframe and the installed package XM-26 into 1972. According to some documents Jon shared with me on TOW history the package was yanked in the spring of 1972 and sent with 553 and 554 to Vietnam. Both of those aircraft came from Ft Lewis and had T53-11 engines in them, the same as UH-1Ds. The uprated engines were commonly retrofitted to UH-1Bs and in many cases the tailbooms were replaced with the C model type with larger chord fin. The lift capacity beyond normal base weight for the UH-1D was 2,000 lbs. In my view, they were probably close to max ability with the hardware they had and the exhaust suppressor does affect (degrade) the overall performance envelope to a small degree. The turret fitting sure looks like the AH-56 turret with the 40mm in it, it was swapped because the feed system for the minigun was proving to be difficult to maintain. Since 5 total XM-26 packages were built and at minimum 2 were in Vietnam, 3 were still in the US in 1972. The Cheyenne project funding was yanked in 1972. SO the photo may predate the TOW deployment during AH-56 system testing and may well be the civil airframe and have the latest and most up to date equipment installed on it. But, in my view, they would be really walking the safety line by adding weight to an already stretched airframe unless power upgrades were made. Even then the limitations of the -11 engine in a B type rotor system lift envelope is being challenged. Since only one NUH-1M is documented it would make sense that it's increased ability would be preferred in the testing enviroment. The TOW development continued for the AH-1 series and of course was eventually adopted and installed. The TOW history papers do not specifically address the total number of airframes used in testing but do allude to the single initial test airframe and the two deployed airframes. At this point I'd say it's very hard to determine exactly which one that is based on a single photo. There are alot of anomolies in the picture, the partial M-5 system supports and the nose modified access door. And that may not be the Cheyenne turret at all, but a test package with sensor probes sticking out of. And since the TOW history states the package was yanked off the test bird, only part of the system is installed on this one. If the site has been relocated to the roof, since being able to sight the weapons is required, the implication is that an additional airframe is in use. Given the text mentioning the AH-56 there is no question it's a test use airframe, which one is still at question.
Chief Snake
An additional thought- given the experience that Hughes would have in dealing with the airframe and associated systems in a hot weather enviroment it makes perfect sense that they would use a better airframe than the initial B provided. The XM-26 package had been validated and sidelined in 1968 and "stored" according to the TOW history documents. IF it was stored in 1968 and that picture is 1971, and the the package was yanked from the "stored" airframe, that sure implies that a different airframe would exist (NUH-1M?) and be in use. AND the time requirement for deployment was critical. The best available close airframes were 553 and 554 with uprated -11 engines in them. It certainly stands to reason that the best available UH-1C and M airframes were most likely still in combat use in Vietnam and in DEMAND given the uptempo of NVA activity. The whole package was assembled and airlifted from Ft Lewis in 7 DAYS! Since 5 total packages were assembled, it wouldn't be neccessary to have the weapons pods pulled off an aircraft but it WOULD be neccessary to pull off the sighting systems if only TWO existed. That airframe clearly does not have the sighting system that 553 and 554 used. Is the documentation wrong in that the system was pulled off the stored aircraft? Maybe, like all records they could contain errors but I don't think this is in error. I'm leaning to a totally different airframe, the NUH-1M. The need (common sense) had to be recognized, and it's known for sure that such an airframe was in existence.