Beechcraft Duchess

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Model 76 Duchess
N60244 1978 Beech 76 Duchess.jpg
A Beech 76 Duchess on final approach
RoleFour-seat cabin monoplane
Manufacturer Beechcraft
First flightSeptember 1974 [1]
Introduction1978 [1]
Primary userFlight schools [1]
Produced1978-1983
Number built437
Developed from Beechcraft Sierra
US registered 1979 model Duchess Beech 76 N6697D Timm, Milw, WI 07.06.06R edited-2.jpg
US registered 1979 model Duchess
1979 model Duchess Beechcraft76DuchessC-GJFE02.jpg
1979 model Duchess

The Beechcraft Model 76 Duchess is an American twin-engined monoplane built by Beechcraft intended partly as a low cost introduction to twin-engine aircraft. [1] [2]

Contents

Development

Developed as Model PD289 (Preliminary Design 289), the prototype was unveiled on November 4, 1974, although it had first flown in September 1974. [1] [3] :409–410 The Model 76 was designed as an economical twin-engine trainer for the Beech Aero Centers and to compete with the similar Gulfstream Cougar as well as the Cessna 310. [1] [4]

The first production version flew on 24 May 1977, and the name "Duchess" was chosen through a company competition. [1] [3] Construction of the Duchess was set for a new factory built at the Liberal Division, [5] with deliveries beginning early in 1978. [3] :473

Production of the Duchess continued until 1983, with no significant changes. [6] A single example was tested with turbocharged engines in 1979, but did not proceed to production. [7] :56

Design

The Duchess is an all-metal low-wing monoplane with retractable tricycle landing gear and a T-tail. It seats four. [8] The design used components and the bonded wing construction from Beechcraft's single-engined Musketeer line. [7] :55 The basic fuselage and wing structure was adapted from the Model 24 Sierra, a Musketeer variant with retractable landing gear, but the Sierra wing spar was redesigned to support the added weight of the engines. [9] Nose landing gear from the A36 Bonanza was used. [9]

The Model 76 incorporates right and left "handed" Lycoming O-360 engines that rotate in opposing directions to eliminate the critical engine during single engine operation. [10]

In 1979, a single example was converted to test the turbocharged versions of the engine. The cowlings were reshaped and the exhaust moved to accommodate the aft-mounted turbochargers. [7] :56

The Duchess wing is of aluminum honeycomb construction fastened by bonding, rather than rivets, to reduce cost and produce a smoother aerodynamic surface. [10]

T-tail

The use of a T-tail on the Model 76 met with mixed critical reception when the aircraft was introduced. Plane & Pilot pronounced: "Outstanding design characteristics of the new Duchess include an aerodynamically advantageous T-tail, which places the horizontal surfaces above the propeller slipstream for better stability and handling.", [10] while Gerald Foster said: "[Beechcraft's] interest in T-tails was perhaps an affectation triggered by their wide use on jet airliners". [11] AVweb wrote that Beechcraft adopted the T-tail after flight tests revealed that the initially used conventional horizontal stabilizer was too small and suffered from buffeting problems, increasing noise and vibration during flight; moving the horizontal stabilizer out of the propeller slipstream eliminated the buffeting and the need for enlargement while adding only 15 pounds (6.8 kg) of weight. [9] Additionally, the T-tail design moved the stabilizer rearward, increasing its effectiveness and giving the aircraft a broader center of gravity range. [9] The later Piper Seminole also adopted a T-tail. [9]

Variants

Model 76 Duchess
Four-seat, twin-engine (Lycoming O-360), low-winged trainer with bonded aluminum construction.
Model 76TC Duchess
Unofficial designation for single test aircraft using turbocharged Lycoming O-360.

Operators

The aircraft remains popular with flight training schools.

Specifications

1976 model Duchess instrument panel Beechcraft 76 Duchess C-FDMO instrument panel 01.JPG
1976 model Duchess instrument panel

Data fromJane's All The World's Aircraft 1980–81. [17]

General characteristics

Performance

See also

Related development

Aircraft of comparable role, configuration, and era

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References

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