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Grumman Tiger

 

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Engine make/model: Lyc. O-360-A4K
Horsepower: 180
TBO: 2000
Propeller: Const. spd.
Landing gear type: Tri/Fixed
Gross weight (lbs.): 2400
Empty weight (lbs.): 1294
Useful load (lbs.): 1106
fuel (gals.): 51
Wingspan: 31.5 ft.
Overall length: 22 ft.
Height: 8 ft.
Wing area (sq. ft.): 140
Seating capacity: 4
Cabin width (in.): 40
Cabin height (in.): 45
Baggage capacity (lbs.): 120
PERFORMANCE
Cruise speed (knots):
75% power: 139
65% power: 131
Max range (with reserve) (nm):
75% power: 552
65% power: 578
Fuel consumption (gph):
75% power: 10.8
65% power: 9.7
Estimated endurance
(65% power with 1-hr. reserve):
4 hrs. 30 mins.
Stall speed (gear, flaps down)
(knots): 53
Best rate of climb (fpm): 850
Service ceiling (ft.) 13,850
Takeoff ground roll (ft.): 865
Landing ground roll (ft.): 410

 


Contact the Author:  Bruce J. Elig  CFII/MEI/ATP                                 Last Updated:  21 April, 2008