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| GRUMMAN AMERICAN AA-5B TIGER |
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| Basic Price (1975) |
$24,137 |
| Basic IFR Price (1975) |
$31,479 |
| Engine |
Lycoming O-360-A4K, 180 hp |
| TBO |
2,000 hrs |
| Propeller |
Fixed pitch |
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73 in. dia. |
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59 in. pitch |
| Length |
22 ft. |
| Height |
8 ft. |
| Wing span |
31.5 ft. |
| Wing area |
140 sq. ft. |
| Wing loading |
15.7 lbs./sq. ft. |
| Seats |
4 |
| Empty weight, IFR equipped |
1,385 lbs. |
| Useful load |
1,015 lbs. |
| Payload, full fuel and oil, | |
|
692 lbs. |
| Gross weight |
2,400 lbs. |
| Power loading |
13.3 lbs./hp |
| Fuel capacity |
51 gals./306 1bs. |
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| PERFORMANCE |
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| Minimum runway requirement |
1,550 ft. |
| Rate of climb |
850 fpm |
| Service ceiling |
14,600 ft. |
| Maximum speed |
170 mph/148 kts |
| Cruise, 75% power @ | |
|
160 mph/139 kts |
| Miles per gallon @ | |
|
15.1 sm/13.1 nm |
| Range @ max cruise | |
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650 sm/565 nm |
| Duration @ max cruise |
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4.8 hrs |
| Stall speed (clean) |
65 mph/56.5 kts |
| Stall speed (flaps down) |
61 mph/53 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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