The new Tiger performance and specifications

Tiger Aircraft LLC was formed to revive, enhance, and build one of the most celebrated airplane designs in general aviation history—the “Tiger.” Today’s Tigers are built in a new facility in Martinsburg, WV constructed specially to build the planes.

Powerplant

Engine                 Lycoming 0-360-A4K @2,700 rpm 180 bhp

Oil Capacity         8.0 qt (7.5 l)

Propeller              Sensenich, two blade, fixed pitch, 76" diameter (1.93 m)

Top speed at sea level 148 kt 274 km/h
Speed (mid-weight cruise) 143 kt 264 km/h
Cruise @ 75% power, cruise altitude 8500 ft 2591 m
Speed 143 kt 264 km/h
Fuel consumption 10.7 gph 40.5 l/h
Endurance 4.7 hr 4.7 hr
Range (with no reserve) 681 nm 1262 km
Range (with 45 min, reserve) 572 nm 1059 km
Rate of climb @ sea level 850 fpm 4.32 m/sec
Service ceiling 13,800 ft 4206 m
Takeoff distance over 50 ft obstacle 1550 ft 473 m
Landing distance over 50 ft obstacle 1120 ft 341 m
Stall speed, flaps down (Vso) 53 kt 98 km/h
Stall speed, flaps up (Vsi) 56 kt 104 km/h
Airframe
Max gross weight on ramp 2400 lb 1089 kg
Empty weight 1500 lb 680 kg
Useful load 900 lb 408 kg
Baggage max weight 120 lb 54 kg
Wing span 31.5 ft 9.6 m
Length 22.0 ft 6.7 m
Height 8.0 ft 2.4 m
Fuel capacity 52.6 gal 199 L
Usable fuel 51.0 gal 193 L