OVERALL DIMENSIONS
Length
Wing Span
Height (Top of tail)
Height (Top of cockpit)
|
25.46 ft. (7.7m)
29 ft. (8.8m)
7.5 ft. (2.3m)
6.23 ft.(1.9m)
|
FUSELAGE DIMENSIONS
Frontal Area
Cockpit Width:
Front Seats
Rear seats
Cockpit Height
Cockpit Length
|
10.02 sq. ft.
44 in.
42 in.
46 in.
78 in.
|
WING DIMENSIONS
Wing Area
Chord
Aspect Ratio
Spar Locations
Airfoil
Dihedral (per panel)
Tip Wash Out
Wing Loading
|
106 sq.ft.
49 in.
7.2
28% & 71% of chord
NACA 65-415
3 degrees
0 degrees
17 lbs/sq.ft.
|
TAIL DIMENSIONS
Horizontal Tail Span
Horz. Tail Chord
Horz. Stab. Mean Chord
Elevator Mean Chord
Horz. Tail Area
Horz. Tail Aspect Ratio
Horz. Tail Thickness
Vertical Tail Area
Vertical Tail Mean Chord
Dorsal Fin
Vertical Fin Thickness
|
10 ft. 3 in. (3.1 m)
3.08 ft. (.9 m)
2.83 ft. (.85m)
14.5 in. ( 37 cm)
19.3 sq.ft.
3.5
12 %
5.91 sq. ft.
2.35 ft.
.33 x 2.5 ft.
10 %
|
FLAPS
Type
Area/Wing
Length (Each)
Chord
|
Plain
15 %
83 in.
15.3 in. @ 28%
|
CONTROL MOVEMENT
Elevator
Ailerons
Rudder
Flaps
|
+25 -16 degrees
+12 -12 degrees
L 24 R 30 degrees
0/12/28 degrees
|
PLACARDED IAS LIMITS
Green Arc
Yellow Arc
White Arc
Red Line
|
58 to 164 mph
164 to 216 mph
55 to 110 mph
216 mph
|
LIMITATIONS
Limit Load Factor
Design Limit Load Factor
V-Maneuver Speed
V-f Flap Ext. Speed
V-ne Never Exceed Speed
|
+2.9 G
-2.2 G
164 mph
110 mph
216 mph
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POWER PLANT
Type
Serial No.
Horsepower
Max RPM
Fuel grade
Propeller (Prince fixed pitch)
|
Lycoming IO-360 A2B
L-2530-51A
200 HP
2700
100/130 LL
P-Tip 68”D X 80”P
|
MAIN LANDING GEAR
Type
Wheels
Tyres
Brakes
Pressure
|
One Piece fixed
Alloy Aluminium
Matco 6”
Air Trac 6.00 x 6
Toe Actuated Disk /
Caliper Hyd.Piston
33 PSI (230 Kpa)
|
NOSE LANDING GEAR
Type
Wheel
Tyre
Pressure
|
Fixed Fabricated Steel
/Aluminium
Free Castoring
Matco 5”
Alloy Alum.
Air Trac 5.00 x 5
29 PSI (200 Kpa)
|
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ir Vent (Pilot) 26. Circuit breakers
