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American Champion Citabria

The Citabria is a light single-engine, two-seat, fixed conventional gear airplane which entered production in the United States in 1964.

Designed for flight training, utility and personal use, it is capable of sustaining aerobatic stresses from +5g to -2g. 

Champion introduced the 7GCBC in 1965.

It was substantially similar to the 7GCAA of the same year, with a Lycoming O-320-A2B engine of 150 horsepower (110 kW), wood-spar wings, and spring steel main gear legs.

The major differences between these two models are that the 7GCBC has a wingspan of 34.5 feet (10.5 m), 1-foot (0.30 m) longer than the 7ECA and 7GCAA and carries wing flaps.

Bellanca continued production of the 7GCBC, calling it the Citabria “C” Package (a designation apparently begun by Champion).

American Champion’s 7GCBC, reintroduced in 1994 as the Citabria “Explorer,” is similar to earlier versions, with the exception of the metal-spar wings and the use of the Lycoming O-320-B2B of 160 horsepower (120 kW); the most recent significant design change has been the switch to aluminium main gear legs in 2004.

A “High Country Explorer” version, with a Superior Vantage O-360-A3A2 engine of 180 horsepower (130 kW) and larger wheels, is also produced by American Champion.

The 7GCBC Citabria was used as an observation aircraft by the Turkish Army and the Tongan Maritime Force Air Force.

Variants

7ECA

Citabria Standard, Citabria Aurora

7GCAA

Citabria 150, Citabria “A” Package, Citabria Adventure

7GCBC

Citabria 150s, Citabria “C” Package, Citabria Explorer

7KCAB

Citabria “B” Package

Citabria Pro

Specifications

Crew

One

Capacity

One passenger

Length

22 ft 8 in (6.91 m)

Wingspan

33 ft 5 in (10.19 m)

Height

6 ft 7+34 in (2.03 m)

Wing area

165 sq ft (15.3 m2)

Aspect ratio

6.72:1

Airfoil

NACA 4412

Empty weight

1,037 lb (470 kg)

Gross weight

1,650 lb (748 kg)

Fuel capacity

39 US gal (32 imp gal; 150 L)

Powerplant

1 × Lycoming O-320-A2B four cylinders, 

Horizontally opposed aircraft engine,

150 hp (110 kW)

Propellers

2-bladed McCauley 1C172AGM fixed-pitch metal propeller

Performance

Maximum speed

130 mph (210 km/h, 110 kn) at sea level

Cruise speed

125 mph (201 km/h, 109 kn) at 8,000 ft (2,400 m)

Stall speed

50 mph (80 km/h, 43 kn)

(Without flaps)

Never exceed speed

162 mph (261 km/h, 141 kn)

Range

537 mi (864 km, 467 nmi)

(At max cruise speed)

Service ceiling

17,000 ft (5,200 m)

Rate of climb

1,120 ft/min (5.7 m/s)

Take-off run to 50 ft (15 m)

630 ft (192 m)

Landing run from 50 ft (15 m)

755 ft (230 m)

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