Roger Roger
I am le tired
I love flying the 'jo but there's a lot of truth in this.Yet they'll have the dispatch reliability of a 1980's built piston twin.
I love flying the 'jo but there's a lot of truth in this.Yet they'll have the dispatch reliability of a 1980's built piston twin.
They're not targeting the US/Canada. Africa, Australia, Indonesia, etc are a much bigger market and expanding than US/Canada combined. Plus the Canucks are going to keep flying Beavers until they hit a century, and Cessna has the Alaska market locked with the Van.What market is this though? The 207 market? The market for aircraft between 6 and 9 seats? The 206 (well an old 206) can carry around 1000 to 1200lbs legally, a Caravan carries about 2200 to 2600lbs legally? So this airplane is looking to carry 1600 to 1900lbs of stuff? Honestly, I really don't see a market for this in the US or Canada.
I love flying the 'jo but there's a lot of truth in this.
They're not targeting the US/Canada. Africa, Australia, Indonesia, etc are a much bigger market and expanding than US/Canada combined. Plus the Canucks are going to keep flying Beavers until they hit a century, and Cessna has the Alaska market locked with the Van.
I'm having a lot of trouble seeing past the Airvans power to weight ratio though. Even the GA8 normally aspirated is 300 HP for a 4000 lb airplane, that same engine was used in the PA32 at 3400 or 3600 lbs depending on the year and it doesn't seem like it would be enough. This turbine one the numbers seem similar.Likewise. When I flew them at AMF, we had as many as 6 airplanes based in PHX, for as few as 3 runs, and it wasn't uncommon for MX to have to scramble to find 3 to send out flying.
Exactly. Somebody might make it work in the US, but I was really just thinking outloud in terms of where it could be used. Even the Kodiak has barely made a dent into 208 sales, and it's more comparable than the GA10
Shorts Skyvan?Hmmmmm. If I only had sheets of plywood, what would my airplane look like?....
I'm having a lot of trouble seeing past the Airvans power to weight ratio though. Even the GA8 normally aspirated is 300 HP for a 4000 lb airplane, that same engine was used in the PA32 at 3400 or 3600 lbs depending on the year and it doesn't seem like it would be enough. This turbine one the numbers seem similar.
Well, they're flying out of the YK delta right? Little different story than say central Africa on a 37° C day at a couple thousand feet elevation. Or even launching out of HNH runway 6 with a full boat.I know quite a few people flying the GA8 these days - the chief complaint isn't the power to weight ratio, the big problems I hear about are all realted to the fact that the airplane was designed to operate in hot places and now operates in a cold place.
I know quite a few people flying the GA8 these days - the chief complaint isn't the power to weight ratio, the big problems I hear about are all realted to the fact that the airplane was designed to operate in hot places and now operates in a cold place.