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Agusta AZ.8L

Airliners and Commercial Jet Aircraft

The Agusta AZ.8L, also called the Agusta-Zappata AZ.8L, was an Italian airliner prototype that first flew on 9 June 1958. It was designed by Filippo Zappata and grew out of an earlier twin-engined transport project, the AZ.1, which was never built. The aircraft was a conventional low-wing monoplane of all-metal construction with a tricycle undercarriage, powered by four Alvis Leonides 503/2 nine-cylinder air-cooled radial piston engines driving three-bladed constant-speed propellers. It had a crew of two and was laid out to carry 22 first-class or 26 economy-class passengers over a range of about 2,500 km at a maximum speed of 427 km/h. The AZ.8L failed to attract customers, and Agusta abandoned the project to concentrate on its helicopter manufacturing business, in particular another Zappata design, the A.101. Its only listed operator is the Italian Air Force, and it was never developed beyond the prototype stage.

Facts
Year
1958 1
Engine Class
Piston 1
Status
Abandoned 1
Top Speed (km/h)
427 1
Mass (kg)
7620 1
Maximum Mass (kg)
11,300 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Agusta AZ.8L (Wikipedia)

Of Make

Source Agusta AZ.8L (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Agusta AZ.8L (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
The Agusta AZ.8L, or Agusta-Zappata AZ.8L

Also in Business Atlas: the manufacturer of this subject.

Source Agusta AZ.8L (Wikipedia)Lead, maker
Quote, Lead, maker
Agusta abandoned the project to focus on its helicopter manufacturing operations

Originated In

Also in Geography Atlas: where this subject originated.

Source Agusta AZ.8L (Wikipedia)Lead, origin
Quote, Lead, origin
was an Italian airliner prototype
Sources
1. Agusta AZ.8L (Wikipedia)
  • Lead
    The Agusta AZ.8L, or Agusta-Zappata AZ.8L, was an Italian airliner prototype first flown on 9 June 1958.
  • Lead, body style
    was an Italian airliner prototype
  • Specifications, powerplant
    9 cyl. air-cooled radial piston engines
  • Lead, fate
    Agusta abandoned the project to focus on its helicopter manufacturing operations
  • Specifications, empty weight
    Empty weight: 7,620 kg (16,799 lb) equipped
  • Specifications, take-off weight
    Max takeoff weight: 11,300 kg (24,912 lb)
  • Specifications, performance
    Maximum speed: 427 km/h (265 mph, 231 kn)
  • Lead, manufacturer
    The Agusta AZ.8L, or Agusta-Zappata AZ.8L
  • Lead, origin
    was an Italian airliner prototype
  • In Group: Piston and Turboprop Airliners, Lead and specifications
    was an Italian airliner prototype first flown on 9 June 1958
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