Dav8or
Final Approach
I get the Cessna and I too love the Aerostar, but why not a Twin Commander, don't some of those have a lav too?
What scares me is the "G" in GTSIO.....
421 v Aerostar; No comparison. If you need a potty for a 3.5 hour flight, meh - other issues. I'd be all over a P version of the Aerostar.
I was terrified of the "G" for years, I heard all the horror/hangar stories from all the guys that never flew then. I even bought a 414A because of the engine nightmares of the 421's! Well, after a buddy of mine flew his 421C's engines 100 and 200 hours past TBO with very little unscheduled engine maintenance, I changed my mind. I owned Charlene (421B) for 3 years and I don't think we even changed a spark plug. My mechanic tells me the key to "G" engines is who overhauls them and how they are operated.
Will a Comanche 400 do 200 knots? It's certainly got the range and the load carrying ability. The 400 would sure be a fun way to tackle this mission.
The PA-24-400 Comanche 400,[7] while identical in platform to other single-engined Comanches, is structurally strengthened, primarily in the tail. The aircraft has an extra nose rib in the stabilator and in the vertical fin. The stabilator, vertical fin, and rudder of the 400 share virtually no common parts with the 180, 250, or 260 hp (190 kW) Comanches. In addition, the 400's rudder is aerodynamically balanced in a manner similar to that of the Piper PA-30 Twin Comanche and does not have the lead external balance weights of the lower-powered single-engined Comanches.[citation needed]
The Comanche 400 is powered by the 400-horsepower 8-cylinder Lycoming IO-720 engine, an engine developed specifically for the Comanche.[8]
The aircraft was produced from 1964 to 1966,[1] with only 148 PA-24-400s having been built. The aircraft's high fuel burn means that it is expensive to operate. There have been cooling problems with the rear cylinders of the horizontally opposed eight-cylinder engine. Even with the huge engine, the PA-24-400 manages a top speed of only 194 knots (360 km/h) and cruising speed of 185 knots (343 km/h), considerably slower than more modern light aircraft, such as the Cessna 400, operating with much less horsepower.[9]
The Comanche 400 has a three-bladed propeller and carries 100 US gallons (380 L) of fuel, or 130 US gallons (490 L) with optional extended tanks. Fuel burn was advertised as 16 to 23 US gallons (61 to 87 L) per hour, at 55%-75% power. The 400 had a typical empty weight of 2,110 pounds and a max gross weight of 3,600 pounds. New base price for 1964 was $28,750.[citation needed]
Kevin - Could the Mirage do 800 lbs of pax and luggage and get to key west in 3.5 hours (700 NM) with 20 gals ish remaining?
Also..what exactly is the glide ratio?
Isn't that the one with the GTSIO-520-Ks in it at 425hp and hydraulic pressurization?
It's got the GTSIO's, but bleed air pressurisation. The GTSIO's are highly strung, but if flown correctly should be reasonably reliable.
It's the 680FLP and the FP that has the hydraulic pressurisation. Best to stay away from that.
Why not go with one of the Flying Magazines picks?
Rising Stars: 5 Planes That Will Change Aviation
http://www.flyingmag.com/aircraft/rising-stars-5-planes-will-change-aviation#milKVJQUe45lzT6T.99
Can you actually buy any of them?