Aeronca Chief

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Aeronca Chief

Type	Light utility aircraft
Manufacturer	Aeronca
Designed by	Raymond F. Hermes at Aeronca
Maiden flight	1945
Introduced	1946
Produced	1946-1950
Number built	over 2,300
Variants	Hindustan Aeronautics Pushpak

Aeronca also used the name Chief for a series of designs produced prior to World War II; for these aircraft, see Aeronca Chief (pre-war).

The Aeronca Chief is a two-seat fixed conventional gear general aviation airplane which entered production in the United States in 1945. Designed for flight training and personal use, the Chief was produced in the United States between 1946 and 1950.

1 Production history
2 Design
3 Variants
4 Specifications (1946 11AC Chief)
5 References
6 External link
7 Related content

[edit] Production history

The model 11 Chief was designed and built by Aeronca Aircraft Corporation. While it shared the name "Chief" with the pre-war models, the design was not a derivative. Rather, the post-war 11AC Chief was designed in tandem with the 7AC Champion ("Champ")—the Chief with side-by-side seating and yoke controls, and the Champ with tandem seating and joystick controls. The intention was to simplify production and control costs by building a pair of aircraft with a significant number of parts in common; in fact, the two designs share between 70% and 80% of their parts. The tail surfaces, wings, landing gear, and firewall forward—engine, most accessories, and cowling—are common to both airplanes.

The 11AC Chief entered production at Aeronca in 1946, with upgraded versions introduced as the 11BC (also called the "Chief") and 11CC "Super Chief," in 1947 and 1948, respectively. Aeronca was at the time headquartered at Middletown, Ohio, but production facilities there were occupied with the Champ; because of this, the model 11 aircraft were assembled at the Dayton Municipal Airport in Vandalia, Ohio. While the Vandalia location was first used only for the assembly of parts fabricated at Middletown, activities there later expanded to include some fabrication work.

Aeronca ceased all production of light aircraft in 1951. Production of the Chief, which had been outsold by its sibling the Champ by a margin of nearly 4 to 1, had already ended in 1950. This marked the last time the Chief design was built in the United States.

The design was sold in the mid-1950s to E. J. Trytek, who held the design until the late 1960s or early 1970s. The HUL-26 Pushpak, built by Hindustan Aeronautics between 1958 and 1968, was very similar to the Super Chief. Some sources say that the Pushpak was produced under license from Trytek, while others suggest that the Pushpak design resulted from reverse engineering.

Ownership of the Chief design passed to Bellanca Aircraft Corporation in the early 1970s, around the same time they acquired the Champ and its derivative designs. In 1973 Bellanca considered producing an updated version of the Chief for flight training, but the aircraft never entered production. The model 11 designs are currently owned by American Champion Aircraft Corporation, which acquired them sometime before 1991. Ownership of the design in the period between Bellanca's liquidation in 1982 and the American Champion acquisition is unclear.

[edit] Design

Like the Taylorcraft B, Piper Vagabond, Cessna 120/140, and Luscombe 8 with which it competed, the Chief features side-by-side seating. As with many light aircraft of the time, including the Taylorcraft B and Piper Vagabond, the Chief's fuselage and tail surfaces are constructed of welded metal tubing. The outer shape of the fuselage is created by a combination of wooden formers and longerons, covered with fabric. The cross-section of the metal fuselage truss is triangular, a design feature which can be traced all the way back to the earliest Aeronca C-2 design of the late 1920s.

The strut-braced wings of the Chief are, like the fuselage and tail surfaces, fabric covered, utilizing aluminum ribs and wood spars. The landing gear of the Chief is in a conventional arrangement, with steel tube main gear which use an oleo strut for shock absorption, and a steerable tailwheel.

All of the models—11AC, 11BC, and 11CC—were approved as seaplanes, with the addition of floats and vertical stabilizer fins; the seaplane versions were designated the S11AC, S11BC, and S11CC, respectively.

[edit] Variants

Introduced in 1946, the 11AC was the first version of the design and utilized the Continental A-65-8 engine of 65 horsepower, featuring also a McDowell mechanical starter; a handful of 11AC's were built in a basic version designated the 11ACS "Scout." The 11BC model, introduced in 1947, upgraded the engine to a Continental C-85-8F of 85 horsepower; the design was otherwise substantially similar to the 11AC save for the addition of an extended dorsal fin in front of the vertical stabilizer for the purpose of increasing directional stability. The 11CC "Super Chief" of 1948 brought an upgraded interior, toe brakes on the pilot’s side, and balanced elevators.

In 1973 Bellanca built and flew a prototype trainer based on the model 11. The trainer featured a tricycle landing gear arrangement and appeared to share many parts with the 7ECA Citabria (a derivative of the Champ design). The Bellanca trainer's cowling, wings and struts, main gear, and horizontal tail surfaces all appeared to have come from the Citabria. The vertical stabilizer and rudder appeared similar, though shorter vertically. The fuselage of the trainer featured a rear window. The cabin had a modernized instrument panel and other furnishings. The design was never put into production.

[edit] Specifications (1946 11AC Chief)

General characteristics

Crew: one pilot
Capacity: one passenger
Length: 20 ft 10 in (6.4 m)
Wingspan: 36 ft 0 in (11 m)
Height: 6 ft 10 in (2.1 m)
Wing area: 175.5 ft² (16.3 m²)
Airfoil: NACA 4412
Empty weight: 725 lb (328.9 kg)
Loaded weight: 1,250 lb (567 kg)
Useful load: 525 lb (238.1 kg)
Max takeoff weight: 1,250 lb (567 kg)
Powerplant: 1× Continental A-65-8 , 65 hp (48.5 kW)

Performance

Maximum speed: 105 mph (169 km/h)
Cruise speed: 95 mph (152.9 km/h)
Stall speed: 40 mph (64.4 km/h)
Range: 330 mi (531.1 km)
Service ceiling: 10,800 ft (3291.9 m)
Rate of climb: 500 ft/min (2.54 m/s)
Wing loading: 7.1 lb/ft² (34.8 kg/m²)
Power/mass: 19.2 lb/hp (11.7 kg/kW)

[edit] References

Abel, Alan (Ed.) (1988). The best of Paul Matt: A collection from the historical aviation albums. Terra Haute, IN: SunShine House.
Aircraft specification no. A-796. Revision 14. (Aug. 1, 1991.) Department of Transportation. Federal Aviation Administration.
American airplanes: Aeronca. Aerofiles: A Century of American Aviation. Retrieved on 2006-08-12.
Bellanca. Aerofiles: A Century of American Aviation. Retrieved on 2006-08-12.
Bhargava, Kapil. The IAF as an aircraft manufacturer. Indian Air Force – History. Retrieved on 2006-09-05.
HAL Pushpak. Warbirds of India. Retrieved on 2006-09-05.
Hollenbaugh, Bob, John Houser (1993). Aeronca: A photo history. Destin, FL: Aviation Heritage Books. ISBN 0-943691-10-9.
Juptner, Joseph P. (1994). "ATC #761 (9-28-45): Aeronca 'Chief,' 11AC (11BC)". U. S. Civil Aircraft Series 8 (ATC 701-800): 211-213. Blue Ridge Summit, PA: Tab Aero—McGraw-Hill.
Juptner, Joseph P. (1994). "ATC #796 (9-28-45): Aeronca 'Super Chief,' 11CC". U. S. Civil Aircraft Series 8 (ATC 701-800): 332-334. Blue Ridge Summit, PA: Tab Aero—McGraw-Hill.
Type certificate data sheet no. A-761. Revision 17. (Aug. 1, 1991.) Department of Transportation. Federal Aviation Administration.