Aerotécnica AC-12
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The Aerotécnica AC-12 Pepo was a Spanish two-seat light helicopter of the 1950s.
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[edit] Design and development
Aerotécnica AC-12 was designed by Jean Cantinieau and like other Cantinieau designs featured a distinctive "spine" above the fuselage pod that carried the engine ahead of the rotor assembly. Development costs were borne by the Spanish government, and the first of two prototypes took to the air on 20 July 1954.
[edit] Operational history
Twelve (two prototypes and ten production) were ordered for the Spanish Air Force where they served for three years under the designation EC-XZ-2.
[edit] Operators
[edit] Specifications
[edit] General characteristics
- Crew: one, pilot
- Capacity: 1 passenger
- Length: 8.30 m (27 ft 2 in)
- Main rotor diameter: 8.50 m (27 ft 10 in)
- Height: 2.75 m (9 ft 0 in)
- Main rotor area: 56.7 m² (610 ft²)
- Empty weight: 490 kg (1,080 lb)
- Maximum weight: 770 kg (1,700 lb)
- Powerplant: 1 × Lycoming O-360-B2A, 125 kW (168 hp)
[edit] Performance
- Maximum speed: 140 km/h (87 mph)
- Range: 170 km (100 miles)
- Service ceiling: 3,100 m (10,000 ft)
- Rate of climb: 258 m/min (846 ft/min)
[edit] Related content
Related development:
Comparable aircraft:
Designation sequence: AC-11 - AC-12 - AC-13 - AC-14 - AC-21
[edit] References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
- Simpson, R. W. (1998). Airlife's Helicopters and Rotorcraft. Ramsbury: Airlife Publishing.
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