PZL P.23 Kara light bombers
Specification
MODEL P-23B "Karas B"
CREW 3
ENGINE 1 x Bristol Pegasus VIII, 507kW
WEIGHTS
Take-off weight 3525 kg 7771 lb
Empty weight 1928 kg 4251 lb
DIMENSIONS
Wingspan 13.95 m 45 ft 9 in
Length 9.7 m 31 ft 10 in
Height 3.3 m 10 ft 10 in
Wing area 26.8 m2 288.47 sq ft
PERFORMANCE
Max. speed 320 km/h 199 mph
Ceiling 7300 m 23950 ft
Range 1260 km 783 miles
ARMAMENT 3 x 7.7mm machine-guns, 700kg of bombs
PZL P80 Fighter
Specifications
Engine K14-1000a 14 cylinder air-cooled double-row radial, rated at 1000 hp.
Powerplant similar in design to Gnome-Rhone.
Construction Cantilever low-winged monoplane with semi-monocoque rear fuselage and welded steel tube forward and center sections.
Maximum Speed 317 MPH {510 KmH} at 13,000 ft. {4000m}
Climb to 1000m 1 minute 20 seconds
Climb to 4000m 5 minutes 40 seconds
Range 940 km
Dimensions Wingspan: Given as 10-10.7m {32 ft 1 in}
Length: 8.9m {32 ft}
Height: 3.6m {11ft 10in}
Wing Area: 16 square meters
Weight Unloaded: 1780kg
Loaded: 2250 kg {5040 lb}
Armament IAR-80: 4 Browning FN 7.92mm Machine Guns
61 to be produced in 1936 as immediate replacements for the PWS P10 fighters. Will also begin to replace the 150 PZL P7s currently in service. To be called the PZL P80.