Piper PA-28RT-201T - Page 561

Figure 61-6. Propeller Blade Minor Repair
CHART 6102. PROPELLER SPECIFICATIONS
Hartzell McCauley
Blade Angles
1
Low Pitch (High RPM) 14.0° ± 0.2° 12.5° ± 0.2°
High Pitch (Low RPM) 29.0° ± 2° 27.5° ± 0.5°
1
Measured at 30 inch station.
Propeller RPM Setting Engine Static High RPM 2700 RPM Max.
Propeller Torque Limits Description Required Torque (Dry)
Propeller Mounting Nuts 60-70 foot-pounds (Hartzell)
55-65 foot-pounds (McCauley)
Forward Bulkhead Attach-
ment Bolts 30-35 inch-pounds (Hartzell)
Aft Bulkhead Attachment
Bolts 50-70 inch-pounds
Spinner Attachment Screws 20-25 inch-pounds
Effectivity 61-10-02
PA-28RT-201 Page 61-10
Revised: February 23, 1979
3B5
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL