Engine: Bristol Pegasus (670 hp and 720 hp variants)
Dimensions
Length: 9.68 m.
Wing Span: 13.95 m.
Height: 3.3 m.
Max Speed: 304 km/hr
Range: 1,260 km
Maximum Ceiling: 7,300 m
Crew: 3
NOTES
The PZL 23 first flew in 1934 and entered production in 1936. While the Polish variant used the Bristol Pegasus
engine, all export variants (presumably also those which the Latvians could have purchased) were equipped with the
Gnome-Rhone.
Beginning in December 1936 the Latvians began looking for a more modern trainer, suitable for preparing pilots for
the Gloster Gladiator while still being capable of being used for reconnaissance.
While the PZL was one of about six aircraft considered for the role, the decision was made on Feb.9, 1937
to purchase the Hawker Hind.
Sources
- Bruvelis, Edvins Latvijas Aviacijas Vesture