Gents, Garry gave a good back ground on the three helos that were removed from service and portions of their separate capabilities were provided by the Griffon. Garry and I were quite involved in the implementation of the Griffon (its entry into service) in the mid-to-later 90's, then he went on to fly them while I kept flying my desk. There were a number of challenges including determining how the Griffon really was going to be operated by the Tactical Aviation community once it was fully entered into operational service. There was much discussion of how much of the Kiowa's and Twin Huey's roles would the Griffon be used to provide. In the end, the direction was principally to provide roles that the Twin Huey had provided earlier and to save until later the employment of the Griffon in the kind of recce and surveillance missions that Garry noted earlier for the Kiowa.
I'll start off by saying that the Griffon is what it is...a single main-rotor, utility helicopter that can perform a variety of tasks, either as a basic aircraft or with the addition of several mission kits (FLIR, Nitesun searchlight, C6 MG, cabin armour, skis, hoist, etc....) Folks love to make comparisons, but a direct comparison is not always a fair thing to do. The closest comparision to the Griffon is obviously the Twin Huey, but there are noticable iddferences between the two helicopters...both in their characteristics and in the way that they were/are employed. Some folks (myself included) like to compare the Griffon and Twin as a Ford F-150 Lariat-trim, Super Cab with a/c, cruise, p/w, p/s, p/b and a short-bed (Griffon) with an older regular cab, long-bed, vinyl seating, no a/c, no cruise, base-model F-100 (Twin Huey). You could put a bit more in the F-100 but the F-150 was much nicer to drive for extended periods.
As noted earlier in the thread, the Griffon is a little heavier than the Twin and even with the four-bladed rotor (vs. the Twin's two blades), leads to a noticably heavier rotor loading. Guys may tell you that the Griffon is not quite as solid hovering on its column of air as the Twin was, until you get down into "ground effect" (by definition 1/2 the distance of the main rotor, in practive around 4-5' above the ground). The Griffon's avionics are far more integrated than the other previous helicopters in the CF...the first of the "electric aircraft" if you will. The Avionics Management System (AMS) uses a dual digital databus (MIL-STD-1553-B) and has Cockpit Display Units (CDUs) that the pilots uses to program the avionics, communications and some of other mission systems. Ironically, though, it was a hybrid system that took much of the digital information running through the data-buses and reconverted it back to analog signals and (aside from the two CDUs) presented the information in a traditional "steam-driven" instrument panel. We are missing a few flat-screen MFD (multi-function displays) that would have kept the modernization theme throughout the aircraft.
Operationally, the Griffon is not without its challenges...mind you, nor is any other helicopter. Depending on the mission kits installed, the Griffon is limited to how much paylod it can carry. The Griffon also has some performance limitations based on how it manages torque...which tends to oscillate more than the Twin. This means guys will usually add a bit of a "buffer" to how much power they pull, so that they don't overtorque the aircraft inadvertantly. Interestingly, many of the missions, like those that Spike referred to in Haiti, don't use the aircraft at its AUW (all up weight) and the capability the Griffon then provides (surveillance, overwatch, illumination, small reation team insertion, etc... vs. large fore mobility) it quite useful to the Task Force commander. I think it's more an issue of finding what and where the Griffon can be best leveraged...moving large numbers of troops in an airmobile is perhaps not the best employment of the asset.
Where it's future leads (as with just about everybody else in the CF, right about now, eh?) remains to be seen. Time will tell how the Griffon can be developed in the future to contribute to the CF.
p.s. Just to caveat my words, I only have two hours in the Griffon...my op time was all on the CH147 and CH135 (including the infamous trip of 29 April 1992 to transport Marcel Masse to Bell in Mirabel to anounce the 100 Griffons to be purchased
). Much of my words above were based on dealing with supporting the Griffon from a number of different positions (EW, systems, life support, engineering, employment, ops management, torque-sensitivity solutions, etc...) now for almost a decade. I feel I know the beastie pretty well and have worked with others to make it as much as it is today (which to be honest, could have been a lot worse were it not for the contributions of lots of motivated folks). That said, I'm still holding out for a little "something else" before I get back in the cockpit... *nudge, nudge, wink, wink* ;D
Cheers,
Duey
*edit* - Got my Garry/Gary's mixed up...I worked for Gary, not Garry although both flew on Kiowas...mea culpa....P.S. Garry's summary of the helos was still very good, though!