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1938
Lockheed Electra 12A
|
<<Back
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Specifications
|
|
Wingspan
|
49.5
ft.
|
Wing
area
|
352
sq. ft.
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Overall
Length
|
36.3
ft.
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Overall
Height
|
9.9
ft.
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Landing
Gear Type
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Conventional,
retractable
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Seats
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8
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Engine
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|
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Two
Pratt & Whitney Wasp Juniors R-985-SB
single-row radial engines, 450 hp at 2300
rpm for takeoff.
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Propeller
|
|
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Hamilton
Standard two-blade, controllable-pitch,
diameter 9 feet, or fully feathering
hydromatic, diameter 9 feet.
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Manufacturer
|
|
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Lockheed
Aircraft Corporation
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Weights
& Loadings
|
|
Gross
weight
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9200
lb.
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Empty
Weight
|
6380
lb
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Useful
load
|
2820
lb.
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Wing
loading
|
26.14
lb./sq. ft.
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Power
Loading
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20.44
lb./hp
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Fuel
capacity
|
250
gal.
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Performance
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|
Maximum
speed, sea level
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214
mph
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Cruise
speed, 5,000 ft.
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202
mph
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Range,
75% power
|
850
s.m. plus reserve
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Rate
of Climb, sea level
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1360
fpm
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Service
Ceiling
|
24,000
ft.
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Stall
speed, clean
|
78
mph
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Stall
speed, flaps and gear
|
65
mph
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Approach
speed (1.3 x stall)
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84
mph
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Takeoff
ground roll
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770
ft.
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Takeoff
over 50-ft. obstacle
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1600
ft.
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Landing
over 50 ft. obstacle
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1200
ft.
|
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