- Boeing 80
infobox Aircraft
name = Model 80
type =Airliner
manufacturer =Boeing
caption =
designer =
first flight =27 July 1928
introduced =
retired =
status =
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variants with their own articles = The Boeing 80 was an earlyUnited States airliner . It was the first purpose-builtairliner for theWashington aircraft companyBoeing . Abiplane like its predecessor, the Model 40A, it was significantly larger, with threeradial engine s, 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 onSeptember 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 nurseEllen 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 andPratt & Whitney Hornet engines (10 built)
** Model 80A-1 - version with revisedempennage ; 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 forStandard 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=
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thrust/weight=
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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 airlinerssee also=
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