Boeing 80

Boeing 80

infobox Aircraft
name = Model 80
type = Airliner
manufacturer = Boeing



caption =
designer =
first flight = 27 July 1928
introduced =
retired =
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The Boeing 80 was an early United States airliner. It was the first purpose-built airliner for the Washington aircraft company Boeing. A biplane like its predecessor, the Model 40A, it was significantly larger, with three radial engines, an enclosed flight deck for 2 pilots, and a cabin for 12 passengers. A larger model, the 80A, increased passenger capacity to 18, making its first flight on September 12, 1929. Ten Model 80A aircraft flew for the Boeing airlines.

Despite complaints by pilots accustomed to flying in an open cockpit, the size of the Model 80 required a separate, enclosed flight deck. The Model 80 carried passengers in a spacious cabin appointed with leather upholstery, reading lamps, forced-air ventilation, and hot and cold running water.

The 80A also introduced aviation's first female flight attendants, when registered nurse Ellen Church convinced managers at Boeing women registered as nurses would be a useful part of an aircraft's crew.

Variants

* Model 80 - original production version with Pratt & Whitney Wasp engines (4 built)
* Model 80A - improved aerodynamics and Pratt & Whitney Hornet engines (10 built)
** Model 80A-1 - version with revised empennage; all 10 Model 80As converted to this standard
* Model 80B-1 - single Model 80A built with open flight deck. Later modified to Model 80A-1 standard
* Model 226 - one-off Model 80A converted to executive transport for Standard Oil. Modified tail surfaces later adopted on all Model 80As (see Model 80A-1)

pecifications (Model 80A)

aircraft specification
plane or copter?=plane
jet or prop?=prop
crew=Three
capacity=18 passengers
length main=56.5 ft (17.2 m)
length alt=
span main=80 ft (24.4 m)
span alt=
height main=
height alt=
area main=
area alt=
airfoil=
empty weight main=
empty weight alt=
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main= 17,500 lb (7,937.9 kg)
max takeoff weight alt=
more general=

engine (jet)=
type of jet=
number of jets=
thrust main=
thrust alt=
thrust original=
afterburning thrust main=
afterburning thrust alt=
engine (prop)=Pratt & Whitney Hornet
type of prop= air-cooled radials
number of props=3
power main= 525hp
power alt=
power original=

max speed main= 138mph (222.1 km/h)
max speed alt=
cruise speed main= 125mph (201.2 km/h)
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main= 460mi (740.3 km)
range alt=
ceiling main= 14,000ft (4,267.2 m)
ceiling alt=
climb rate main=
climb rate alt=
loading main=
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=

References

* [http://www.boeing.com/history/boeing/m80.html Boeing History - Boeing Model 80 Commercial Transport] Retrieved June 17, 2006.

ee also

aircontent

related=
similar aircraft=
*Fokker F.VIII
*Ford Trimotor
*Junkers Ju 52/3m
lists=
* List of airliners

see also=


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