Consolidated P-30

Length
9.14 m
Flat Wing Span
13.38 m
Height
2.51 m
Flat Wing Area
27.6 m²
Cruise Speed
346 km/h
Max Speed
443 km/h
Max Ceiling
8530 m
Number of Engines
1
First Flight
1934-01-01
Number Built
60
Maximum Range
818 km

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Aircraft Weight Variants

Aircraft Maximum Range (km)
Consolidated P-30 818

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All data (21 fields)
Name
Consolidated P-30
Manufacturer
Bell Aircraft Corporation
Description
The Consolidated P-30 (PB-2) was a 1930s United States two-seat fighter aircraft.
First Flight
1934-01-01
Designer
Bell Aircraft Corporation
Type
Fighter aircraft
Length (m)
9.14
Height (m)
2.51
Max Speed (km/h)
443
Cruise Speed (km/h)
346
Max Ceiling (m)
8530
Armament
; 2 × 0.30 in machine guns firing through the propeller; 1 × 0.30 in machine gun in the rear cockpit; 170 lb bombs
National Origin
United States of America
Number Built
60
Powerplant Description
1 × Curtiss V-1570-61 Conqueror liquid-cooled V12 engine, 520 kW (697 hp) each
Primary Users
United States Army Air Corps
Status
Retired
Wikipedia Article (URL)
en.wikipedia.org/wiki/Consolidated_P-30
Flat Wing Span (m)
13.38
Flat Wing Area (m²)
27.6
Number of Engines
1