Boeing P-26A information from Profile Publication 14, Air International April 1995 and
Aerofax Minigraph 8.
600 hp.
211 mph/S.L.
234 mph/7,500 ft. (also given at 6,000 ft.)
2360 fpm/S.L
27,400 ft. Service Ceiling.
1 x 0.30 cal./
Combat Weight: 2,935 lb.
Wing Loading at take-off: 19.63 lb./sq. ft.
Power Loading (Max. power at take-off): 4.892 lb./hp.
Very sturdy ( for mid-1930s) and maneuverable aircraft.
Fiat C.R.32 information coms from the Pilot's Manual C.A.156 (1934)
600 cv. (592 hp.)
211 mph/S.L.
209 mph/1km.
207 mph/2km. (215 mph/7,500 ft.)
233 mph/3km. (9,842 ft.)
227 mph/4km.
219 mph/5km.
209 mph/6km.
196 mph/7km.
Climb to 3,280 ft./1'20" (2,460 fpm. avg.)
28,870 ft. Service Ceiling.
Combat Weight 4,078 lb.
C.R,32 Series l: 2 x 7.7 mm/500 rpg.
Wing Loading: 17.14 lb. sq. ft., Power Loading: 6.889 lb/hp.
C.R.32 bis: 2 x 7.7 mm/500 rpg. + 2 x 12.7 mm/350 rpg. (2237 fpm avg. to 1,000 m.) 18.26 & 7.336 lb/hp
C.R.32 ter: 2 x 12.7 mm/350 rpg. (2,027 fpm avg. to 1,000 m.) 18.26 & 7.336
C.R.32 quarter: 2 x 12.7 mm/350 rpg. (2,187 fpm avg. to 1,000 m.) 17.66 & 7.095
Very robust aircraft and arguably the most maneuverable fighter aircraft ever produced.