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1971 Grumman American Trainer AA1A
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| Price: | $18,000 (approx). | |
| Engine make/model: | Lyc O-235 | |
| Horsepower for takeoff: | 108 | |
| TBO hrs.: | 2000 | |
| Fuel type: | 100 | |
| Propeller type: | Fixed | |
| Landing gear type: | Fixed | |
| Max ramp weight (lbs.): | 1500 | |
| Gross weight (lbs.): | 1500 | |
| Max landing weight (lbs.): | 1500 | |
| Empty weight (lbs.): | 1007 | |
| Useful load (lbs.): | 1007 | |
| Payload, full fuel (lbs.): | 349 | |
| Usable fuel (gals.): | 24 | |
| Oil capacity (qts.): | 6 | |
| Wingspan: | 25 ft. 5 in. | |
| Overall length: | 19 ft. 3 in. | |
| Height: | 6 ft. 8 in. | |
| Wing area (sq. ft.): | 100.9 | |
| Wing loading (lbs./sq. ft.): | 12.6 | |
| Power loading (lbs./hp.): | 15 | |
| Wheel track: | 8 ft. 3 in. | |
| Seating capacity: | 2 | |
| Cabin width (in.): | 41 | |
| Cabin height (in.): | 45 | |
| Baggage capacity (lbs.): | 100 | |
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PERFORMANCE
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| Cruise speed (kts.): | ||
| 75% power: | 109 | |
| *65% power: | 105 | |
| *55% power: | 100 | |
| Max range (w/ reserve) (nm): | ||
| 75% power: | 350 | |
| *65% power: | 399 | |
| *55% power: | 471 | |
| Fuel consumption (gph): | ||
| 75% power: | 5.7 | |
| *65% power: | 5.0 | |
| *55% power: | 4.2 | |
| Estimated endurance (65% power w/1 hr reserve) (hrs): | 3.8 | |
| Stall speed (flaps up) (knots): | 55 | |
| Stall speed (flaps down) (knots): | 51 | |
| Best rate of climb (fpm): | 765 | |
| Service ceiling (ft.): | 13,750 | |
| Takeoff ground roll (ft.): | 700 | |
| Landing ground roll (ft.): | 395 | |
| all specs are standard unless noted otherwise | ||
