Grumman Tiger

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  

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