Grumman American
Tiger
Current market velue: $53,500
Specifications
|
|
Lycoming O-360-A4K,
18O hp at 2,700 rpm
|
|
Propeller
|
McCauley or Sensenich,
76-in. dia
|
|
Length
|
22 ft
|
|
Height
|
7 ft 10 in
|
|
Wingspan
|
31 ft 6 in
|
|
Wing area
|
140 sq ft
|
|
Wing loading
|
17.1 lb/sq ft
|
|
Power loading
|
13 lb/hp
|
|
Seats
|
4
|
|
Empty weight typically
|
1,450 lb
|
|
Max gross weight
|
2,400 lb
|
|
Useful load
|
950 lb
|
|
Payload with full fuel
|
644 lb
|
|
Fuel capacity
|
53 gal (51 usable)
318 lb (306 lb usable)
|
Performance
|
takeoff distance, over
50 ft obstacle
|
1,926 ft
|
|
Max demonstrated crosswind
component
|
16 kt
|
|
Rate of climb, sea level
|
850 fpm
|
|
Cruise speed/endurance w/45-min
rsv, std fuel (fuel consumption) @75% power, best economy
|
139 KTAS/
3.9 hr
|
|
8,500 ft
|
(64.8 pph/10.8 gph)
|
|
Service ceiling
|
13,800 ft
|
|
landing distance over 50-ft
obstacle
|
1,499 ft
|
Limiting and Recommended
Airspeeds
|
VX
(best angle of climb)
|
70 KIAS
|
|
VY
(best rate of climb)
|
90 KlAS
|
|
VA
(design maneuvering)
|
112 KIAS
|
|
VFE
(max flap extended)
|
103 KlAS
|
|
VNO
(max structural cruising)
|
142 KlAS
|
|
VNE
(never exceed)
|
172 KlAS
|
|
VS1
(stall, clean)
|
56 KIAS
|
| VS0 (stall,
landing configuration) |
53 KIAS
|
|
All specifications are based on manufacturer's
calculations.
All performance figures are based on standard day, standard atmosphere,
sea level, maximum gross weight conditions unless otherwise noted.
|
