Piper Arrow IV Turbo Maintenance Manual page 44

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