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GRUMMAN AMERICAN AA-1C T-CAT
AA-1C/T-cat AA-1C/T-cat
With Spin Package
Gross Weight 1600 lb 725.8 kg 1600 lb 725.8 kg
Empty Weight 1002 lb 454.5 kg 1010 lb 458.1 kg
Useful Load 598 lb 271.3 kg 590 lb 267.7 kg
Baggage (Maximum) 100 lb 45.4 kg 100 lb 45.4 kg
Seats

2

2
Top Speed at Sea Level 118 kt 218 km/h 115 kt 2l3 km/h
Cruise at 75% Power, Altitude 4500 ft 1372 m 8500 ft 2591 m

    Speed

 112 kt 208 km/h 108 kt 199 km/h

    Fuel Consumption

 6.5 gph 24.6 lt/h 6.5 gph 24.6 lt/h

    Endurance (No reserve)

 3.23 hr 3.23 hr 3.24 hr 3.24 hr

    Range (No reserve)

 358 nm 663 km 335 nm 620 km

    Range (45 min. reserve)

 293 nm 543 km 264 nm 489 km
Rate of Climb at Sea Level 750 fpm 3.81 m/s 670 fpm 3.40 m/s
Service Ceiling 11900 ft 3627 m 9600 ft 2926 m
Take-off distance

    Ground run

 840 ft 256 m 850 ft 259 m

    Over 50 ft (15 m)

      obstacle, total

 1530 ft  466 m 1560 ft 475 m
Landing

    From 50 ft (15 m) obstacle

      height, total

 1125 ft 343 m 1125 ft 343 m

    Ground run

 425 ft 129 m 425 ft 129 m
Stall Speeds

    Flaps down

 52 kt 96 km/h 52 kt 96 km/h

    Flaps up

 54 kt 100 km/h 54 kt 100 km/h
Fuel Capacity, total 24 gal 90.8 lt 24 gal 90.8 lt
Fuel Capacity, useable 22 gal 83.3 1t 22 gal 83.3 1t
Oil Capacity 6 qt 5.7 lt 6 qt 5.7 lt
Engine --Lycoming 0-235-L2C, 115 BHP, 4-cylinder, air-cooled--
Propeller, Sensenich

    Metal, fixed pitch

72" dia/52" pitch

72" dia/52" pitch
Wing Span 24.5 ft 7.5 m 24.5 ft 7.5 m
Wing Area 100.9 ft2 9.4 m2 100.9 ft2 9.4 m2
Length 19,2 ft 5.9 m 19,2 ft 5.9 m
Height 7.6 ft 2.3 m 7.6 ft 2.3 m
      
Reference: Grumman American Aviation Corp. Brochure, SPA77-12, Savannah, Georgia, 1977
Given data is only for information.
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