Although lacking the wing folding and the catapult and arrester gear standard on the FR-1, the XF2R-1 weighed 1,042lb (473 kg) more than its predecessor when it flew for the first time in November 1946. The XT31 drove a propeller with four square-tipped hollow-steel blades which could be fully feathered or reversed to zero blade angle extremely rapidly, the drag of the flatter blade angle serving as an effective air brake for landing.
By comparison with the FR-1, the vertical tail surfaces of the XF2R-1 were enlarged to compensate for the lengthening forward to accommodate the turboprop, but the airframe of the later fighter was similar in most other respects. The XF2R-1 underwent extensive testing at Muroc Dry Lake, but no further development was undertaken.
Span: 42 ft 0 in (12.80 m)
Length: 36 ft 0 in (10.97 m)
Height: 14 ft 0 in (4.27 m)
Wing area: 305 sq.ft (28.33 sq.m)
Loaded weight: 11,000 lb (4,990 kg)
Max speed: 4970 mph (800 kmh) at sea level
Climb: 4,850 ft (1,478 m)/min
Service ceiling: 39,100 ft (11,920 m)."