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| GRUMMAN AMERICAN Tr2 |
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| Basic Price (1975) |
$15,312 |
| Basic IFR Price (1975) |
$21,467 |
| Engine |
Lycoming O-235-C2C, 108 hp |
| TBO |
2,000 hrs |
| Propeller |
Fixed pitch |
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71 in. dia. |
| |
57 in. pitch |
| Length |
19.24 ft. |
| Height |
7.6 ft. |
| Wing span |
24.5 ft. |
| Wing area |
100.92 sq. ft. |
| Wing loading |
15.55 lbs./sq. ft. |
| Seats |
2 |
| Empty weight, IFR equipped |
1,074 lbs. |
| Useful load |
486 lbs. |
| Payload, full fuel and oil, | |
|
342 lbs. |
| Gross weight |
1,560 lbs. |
| Power loading |
14.4 lbs./hp |
| Fuel capacity |
22 gals./132 1bs. |
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| PERFORMANCE |
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| Minimum runway requirement |
1,590 ft. |
| Rate of climb |
660 fpm |
| Service ceiling |
11,550 ft. |
| Maximum speed |
144 mph/125 kts |
| Cruise, 75% power @ | |
|
133 mph/115 kts |
| Miles per gallon @ | |
|
21 sm/18.3 nm |
| Range @ max cruise | |
|
343 sm/298 nm |
| Duration @ max cruise |
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|
3.48 hrs |
| Stall speed (clean) |
62 mph/54 kts |
| Stall speed (flaps down) |
60 mph/52 kts |
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Reference: Collins, R.L., "Grumman American Story, the Aircraft", Flying Magazine, February, 1975 |
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Given data is only for information. |
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