The plane is a tank - 1500 lbs heavier empty weight than a 425, 700 lbs heavier empty weight than a Cheyenne II. The 414 A (basically a 421C with direct drive 310 HP engines) has less performance and a poor usefull load but cost more year for year. The 421A type was approved 19 November 1968, powered by two Continental GTSIO-520-Ds of 375 hp (280 kW) each, maximum takeoff weight 6,840 lb (3,103 kg) This is mainly due to the IMO undeserved poor reputation of the 421's geared GTSIO 520 engines. gear difficulties), but aside from the service history of the engines has no unique problems. In 1976, Cessna redesigned the 400 series, beginning with its best seller, the 421. Re: KingAir 90 vs Cessna 414-421 Post by Hedley » Mon Feb 02, 2009 2:04 am The geared engines on the C421 and P Navaho are very low TBO and cost a lot to overhaul 2) Vs. the 414 and even factoring in the cost of the hot section we had to do first thing, the MU-2's operating costs are much cheaper. Cessna wanted a more cost competitive cabin class aircraft and it was able to achieve this by utilizing parts from the existing 400 series models. Overall I think the 421 is the best value going. All that weight is in the structure. Compared to its biggest competitors-the 421 and Duke-a 414 provides a more room than the Duke, as much as the 421, travels a little slower, but does so more economically. The following information is meant to provide customers interested in a Cessna 414A Chancellor or a 421C Golden Eagle with information to aid in making a selection. A 414 appears to be a good choice for anyone who wants a pressurized airplane with a big cabin and lots of baggage space. The six- to seven-seat pressurized light transport is a step up for owners of the pressurized 340 and is fitted with the same 310-hp turbocharged engines. It was a derivative of the 421. [3] Some 421s have been modified to accept turboprop engines, [4] making them very similar to the Cessna 425 , which itself is a turboprop development of the 421. A new bonded wet wing replaced the riveted tip-tanked wing. The Cessna 421 Golden Eagle is an American six or seven seat twin-engined light transport aircraft, developed in the 1960s by Cessna as a pressurized version of the earlier Cessna 411. The 421 shares the same problems as other 400-series Cessna twins (e.g. When the changes trickled to the 414 … Cessna 414A Chancellor versus 421C Golden Eagle Discussion Jerry Temple Aviation (JTA) typically represents several Cessna 414/414A’s and 421B/C’s. MAINTENANCE The model 414, a 411 derivative introduced in 1970, utilized the 421’s fuselage and tail unit with the 401’s wings. The 414 first flew in 1968 and was certified in 1969. The Cessna 414 Chancellor was regarded by many as a better airplane in most respects. Much of the debate stemmed from the 421’s temperamental geared Continental engines. The 421 was first certified on 1 May 1967 and shares a common type certificate with models 401, 402, 411, 414 and 425.
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