CHART 601. LEADING PARTICULARS AND PRINCIPAL DIMENSIONS (cont)
MODEL PA-23RT-201 PA-28RT-201T
PROPELLER (cont)
Blade Angle, Low Pitch* 14.0° ± 0.2° 13.2 ± .2°
Blade Angle, High Pitch* 29° ± 2° 33 ± 1°
Governor Control and Model Hartzell F-2-7 ( ) Hartzell E-5 or Wood-
ward G210681
LANDING GEAR
Type Hydraulically Retractable Hydraulically Retractable
Shock Strut Type Combination Air-Oil Combination Air-Oil
Fluid Required (Struts, Hydraulic
System and Brakes) MIL-H-5606 MIL-H-5606
Strut Exposure (Exposure under
Static Load):
Nose 2.75 ±.25 in. 2.75 ±.25 in.
Main 2.00 ±.25 in. 2.00 ±.25 in.
Wheel Tread 10 ft. 5.72 in. 10 ft. 5.72 in.
Wheel Base 7 ft. 10.38 in. 7 ft. 10.38 in.
Nose Wheel Travel 30° ± 2° left and right 30° ± 2° left and right
Turning Radius (Min):
Nose Wheel 15 ft. 8.4 in. 15 ft. 8.4 in.
Wing Tip 29 ft. 9.6 in. 29 ft. 9.6 in.
Wheel Nose Cleveland 40-77B or Cleveland 40-77B or
McCauley D-30500, McCauley D-30500,
5:00 x 5 5:00 x 5
Wheel Main Cleveland 40-84, 6:00 x 6 Cleveland 40-84, 6:00 x 6
Brake Type Cleveland 30-55 Cleveland 30-55
Tires, Nose 5:00 x 5, 4 ply rating 5:00 x 5, 4 ply rating
Tires, Main 6:00 x 6, 6 ply rating 6:00 x 6, 6 ply rating
Tire Pressure, Nose 27 psi 27 psi
Tire Pressure, Main 30 psi 30 psi
* MEASURED AT 30 INCH STATlON
6-10-00
Page 6-03
Revised: August 17, 1982
1B20
PIPER AIRCRAFT
PA-28RT-201 / 201T
* MAINTENANCE MANUAL
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