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1979 CHRISTEN EAGLE I-F – Specifications

Engine

Lycoming AEI0-540-D4B5, 260 hp

Propeller

Sensenich 80BM8-0-66

Wingspan

19 ft. 11 in.

Wing Area

125 sq. ft.

Wing Loading (gross wt)

11.82 lb./sq. ft.

Power Loading (empty wt)

3.76 lb./hp

Length

17 ft. 11 in.

Height

6 ft. 6 in.

Empty Weight

978 lb.

Gross Weight

1478 lb.

Competition Weight

1243 lb. (with 190 lb. pilot)

Useful Load

462 lb.

Baggage Allowance

30 lb.

Fuel Capacity

25 gal. main, 20 gal. aux

Structural Limits (gross wt)

+9g, -6g operational

Top Speed

189 mph

Cruise Speed

162 mph

Stall Speed

58 mph

Never Exceed Speed

210 mph

Rate of Climb

2600 fpm

Roll Rate

187 deg/sec

Vertical Penetration

1600 ft.

Range

325 mi. std., 602 mi. with aux

Inverted Flight Time

Unlimited

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