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American General Aircraft AG-5B Tiger
Base price: $88,000 (1990*)
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Specifications |
| Powerplant | Lycoming O-360-A4K, |
| | 180 hp at 2,700 rpm |
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2,000 hr |
| Propeller Sensenich, two-blade, |
76-in diameter |
| Length |
22 ft |
| Height |
7.83 ft |
| Wingspan |
31.5 ft |
| Wing area |
l40 sq ft |
| Wing loading |
17.1 lb/sq ft |
| Power loading |
13.3 lb/hp |
| Seats |
4 |
| Cabin length |
7.08 ft |
| Cabin width |
3.33 ft |
| Cabin height |
3.83 ft |
| Empty weight |
1,548 lb |
| Max ramp weight |
2,408 lb |
| Gross weight |
2,408 lb |
| Useful load |
1,089 lb |
| Payload w/full fuel |
783 lb |
| Max takeoff weight |
2,408 lb; utility, 2,058 lb |
| Max landing weight |
2,408 lb |
| Fuel capacity |
51.2 gal (51 gal usable) |
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307 lb (306 lb usable) |
| Oil capacity |
8 qt |
| Baggage capacity |
120 lb |
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Performance |
| Takeoff distance, ground roll |
1,083 ft |
| Takeoff distance over 50-ft obstacle |
1,926 ft |
| Max demonstrated crosswind component |
16 kt |
| Rate of climb, sea level |
850 fpm |
| Max level speed, 8,500 ft |
139 kt |
| Cruise speed/endurance w/45-min rsv, std fuel | |
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@ 75% power, best economy
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139 kt/3.97 hr |
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(64.8 pph/10.8 gph) |
@ 65% power, best economy
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129 kt/5.04 hr |
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(52.8 pph/8.8 gph) |
| Max operating altitude |
13,800 ft |
| Landing distance over 50-ft obstacle |
1,499 ft |
| Landing distance, ground roll |
450 ft |
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Limiting and Recommended Airspeeds |
| Vx (best angle of climb) |
70 KIAS |
| Vy (best rate of climb) |
90 KIAS |
| Va (design maneuvering) |
113 KIAS |
| Vfe (max flap extended) |
104 KIAS |
| Maximum canopy open |
113 KIAS |
| Vno (max structural cruising) |
143 KIAS |
| Vne (never exceed) |
174 KIAS |
| Vr (rotation) |
60 KIAS |
| Vsl (stall, clean) |
56 KIAS |
| Vso (stall, in landing configuration) |
53 KIAS |
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All specifications are based on manufacturer's calculations.
All performance figures are based
on standard day, standard atmosphere,
sea level, gross weight conditions unless otherwise noted. |
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* Price at the time of Reference Magazine (AOPA Pilot) was published. |
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Reference: AOPA Pilot, July 1990 Issue |
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