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Steve said:Thanks for the info bigD. Do you know anything about the airframe? Ive readt that it is bonded (glued) together and has almost no rivets, is this correct. I though I read something about an AD on the glue a few years back.
FutureTEDpilot said:My dad had a Grumman Cougar in 1979. Flew it from our farm in South Dakota to MSP for his trips (NWA Pilot)
Always loved that plane, may buy one in the future, heck maybe I will buy it from you when you are done? I had a BE-55 last year, little nicer but $$$$ to operate!
Good luck
bigD said:Yes - it is bonded, and the airframe is smooth. I think this is how Grumman managed to get Seminole/Duchess like performance on less horsepower and a wider airframe. Unfortunately I can't say about an AD on the glue, although I have been told that there are no recurring AD's for the airframe. Don't know if that's true or not - I didn't verify for myself.
Another interesting tidbit about the Cougar is that it doesn't have a Janitrol heater in the nose - it uses the same exhaust shroud method that most singles use. I was told way back when learning to fly twins that the Janitrol was necessary because by the time you piped the heat from the nacelles and into the cabin, the air has already cooled off. Wrongo - you'll cook inside that cabin with the heat on. It's pretty impressive, and one less MX item to deal with as well (although of course beware of CO).
pilotmiketx makes an interesting point - if you're just buying this airplane for time building (meaning you won't be holding on to it for a long period of time), you may want to consider the fact that a GA-7 might be harder to sell down the line.
Steve said:I am looking to hold onto it for at least a few years and use to travel for business. I also read that the inner spar is life limited to around 5,000 hours? Is that a life ending part like it is in the Seminole?
pilotmiketx said:If you want to keep $50K in the bank, you could always spring for a nice Apache. You won't have any choice, but to build time.![]()
Steve said:Thanks for the info bigD. Do you know anything about the airframe? Ive read that it is bonded (glued) together and has almost no rivets, is this correct. I though I read something about an AD on the glue a few years back.
siucavflight said:The engines are counter rotating
You are right, I was thinking about the Duchess, the Cougar is not counter rotating, damn it is too early in the morning, nice catch.bigD said:You sure about this? The one I flew had two O320-D1D's on it. I don't think Grumman built other GA-7's any differently.
bigD said:I know parts are a lot harder to find, making them more expensive. But it didn't seem to be a very troublesome airplane.
Steve said:I am looking to hold onto it for at least a few years and use to travel for business. I also read that the inner spar is life limited to around 5,000 hours? Is that a life ending part like it is in the Seminole?
ms6073 said:Parts may be a problem for the Cougar as to my knowledge, Fletcher Aviation in Houston (http://www.fletchair.com/) is one of only a few companies left with PMA for parts (like engine and flight control linkages) for the Gruman aircraft like the Cougar.
siucavflight said:The engines are counter rotating.
TIS said:Uhh, no they're not - not on a GA-7.
TIS said:Oops. Missed that one. Sorry.
TIS
erj-145mech said:According to the Type Certificate Data Sheet for the GA-7, the inboard spar assy 1W10201-1 has a service life of 47,674 hours. Shouldn't be too much of a factor unless you put 40,000 hours on it.
erj-145mech said:I've repaired several airplanes that have bellied in. The one that I hated was on a brand new Piper Seneca, 15 hours on the clock. New owner was getting checked out, and pulled the gear control breaker to silence the horn while doing single engine maneuvers. They had the nav lights on so the gear indicator lights were dim, threw the handle down on downwind, and made such a pretty landing, real short though.
The problem with repairing a Cougar is that its an orphan, the mechanic will most likely have to fabricate formers and skins from sheet stock. Check the motor mount tubular structure for cracks and buckling also. That energy from the prop strikes has to be transferred somewhere. There's a new Lycoming AD Note out to replace the crank gear bolt on prop strikes too. You might get away with leaving the pistons in the cylinders on the engine teardown and just tackle the bottom end of the engine, depending on the time on the engine.