KIS TR-1 SPECIFICATIONS

DIMENSIONS OVERALL
Length
Wing Span
Height (Top of tail)
Height (Top of cockpit)
22 ft.
23 ft.
7.25 ft.
5.65 ft.		 FUSELAGE DIMENSIONS
Frontal Area
Cockpit Width
Cockpit Height
Cockpit Length
9.0 sq. ft.
42 in.
39 in.
65 in.

WING DIMENSIONS
Wing Area
Chord
Aspect Ratio
Spar Location
Airfoil
Dihedral (per panel)
Tip Wash Out
Wing Loading
135 sq.ft.
3.83 ft.
6
30% of Chord
NACA 63(2)-215
2.5 degrees
0 degrees
13.6/14.8/15.6/16.3		 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 Height
Vertical Tail Mean Chord
Dorsal Fin
Vertical Fin Thickness
7.33 ft.
2.08 ft.
1.33 ft.
.75 ft.
15.2 sq.ft.
3.5
12 %
4.09 ft.
.83 ft.
.33 x 2.5 ft.
10 %
FLAPS
Flap Type
Area/Wing
Length (Each)
Chord
Plain
12 %
65 in.
12.5 in. = 28% c
CONTROL MOVEMENT
Elevator
Ailerons
Rudder
Flaps
+25 -16 degrees
+12 -12 degrees
L 24  R 30 degrees
0/12/28		 PLACARDED IAS LIMITS
Green Arc
Yellow Arc
White Arc
Red Line

(Limits in MPH)
55/57/58/58 to 156
156 to 216
50/52/53/55 to 110
215
LIMITATIONS
Limit Load Factor
Design Limit Load Factor
V-Maneuver Speed
V-f Flap Ext. Speed
V-ne Never Exceed Speed
+4.4 G
-2.2 G
145 mph
110 mph
215 mph
MAIN LANDING GEAR
Type

Wheels
Tires

Brakes
One Piece
     Alloy Alum.
Matco 6 x 6
Goodyear 6 x 6
     (13.5 in.dia.)
Toe Actuated Disk /
     Caliper Hyd.Piston		 NOSE LANDING GEAR
Type

Wheel

Tire
Fabricated Steel
   Free Swiveling
Matco 5 x 5
    Alloy Alum.
Goodyear 5 x 5
     (11.5 in. dia.)

ENGINE OPTIONS

Recommended engines include the Limbach 2000 (80hp) or 2400 (92hp), the Continental O-200 (100hp) or recently introduced IO-240 (120hp), and the Lycoming O-235 (118hp).  Other engines of similar weights and power may be suitable for use in the aircraft.  Tri-R Technologies has engineered installations for the recommended engines but is unable to provide details of all possible engine choices.  KIS TR-1 aircraft are flying with many different engines.

Engine Possibilites - CAM 100, Continental - C-85, C-90, O-200, IO-240, Franklin 235, Limbach L2000, Lycoming O-235, O-290, Mosler 80hp, Subaru 135hp.

Factory new engines for the KIS TR-1/1C (Limbach, Continental and Lycoming) can be purchased directly from TRI-R Technologies.  These engines will be offered to kit buyers at large savings.  Good sources of used and rebuilt engines are rebuild facilities and published advertisements in aviation magazines and periodicals.  Trade-A-Plane is an excellent source of ads.

Engine mounts for several different installations are available from Tri-R Technologies as an option.

POWER SPECIFICATIONS
ENGINE

   Limbach  
2000

Continental
0-200

  Lycoming  
0-235

 Continental
IO-240
Power At T.O.
Displacement
Propeller
Power Loading
Weight w/Oil & Access.

80 hp.
1994 c.c.
56 x 44
12.5
180 lbs.

100 hp.
200 c.i.
56 x 44
11.0
230 lbs.

118 hp.
235 c.i.
56 x 44
10.5
275 lbs.

125 hp.
240 c.i.
56 x 44
10
285 lbs.
AIRCRAFT WEIGHTS
Empty Weight(Typical)
Fuel Load 20/20/25/34
Max.Gross Weight
Useful Load
Pilot/Passenger
Baggage


680 lbs.
120 lbs.
1200 lbs.
520 lbs.
400 lbs.
60 lbs.


750 lbs.
120 lbs.
1300 lbs.
550 lbs.
400 lbs.
60 lbs.


788 lbs.
150 lbs.
1400 lbs.
612 lbs.
400 lbs.
60 lbs.


798 lbs.
200 lbs.
1500 lbs.
710 lbs.
400 lbs.
60 lbs.
PERFORMANCE
Maximum Speed-SL
Cruise Speed-SL(75% Pwr)
Stall Speed (Clean)
Stall Speed (Land Config.)
Rate of Climb (Gross Wt.)
Rate of Climb (Solo)
Range at Cruise (+res.)
Service Ceiling


150 mph
135 mph
55 mph
50 mph
650 fpm
900 fpm
550 mi.
14000 ft.


170 mph
155 mph
57 mph
52 mph
900 fpm
1300 fpm
500 mi.
14000 ft.


190 mph
170 mph
58 mph
53 mph
1100 fpm
1600 fpm
575 mi.
14000 ft.


200 mph
180 mph
58 mph
55 mph
1200 fpm
1700 fpm
800+ mi.
15000 ft.