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Propeller Design Specification Form

On the base of this form AVIA PROPELLER technical staff will advise you the most appropriate AVIA propeller for your aircraft.

(Please complete all blank areas)

Aircraft Model 
Manufacturer:
Max. Take Off Weight: lbs
Engine Model:
Takeoff Power:
 HP   RPM
Max. Continuous:
 HP   RPM
No. of Cylinders:
Gear Ratio, if applicable:
RPM Restrictions: RPM
Desired Propeller:
Fix pitch Ground Adjustable Hydraulic Constant Speed 
Principally designed for:
Climb   Cruise  Allround   Agricultural  Aerobatic 
Configuration: Tractor Pusher
Rotation (view in flight direction):
Single Engine: Righthand Lefthand
Multi Engine:
Left Prop: Righthand Lefthand
Right Prop: Righthand Lefthand
Features: Counterweight Feathering Reversing
Prop Deice Required: Yes No
System Voltage: VDC
Max. Permissible Diameter: inches
Number of Blades:
Hub / Engine Flange Type:
Max. Propeller weight: lbs
Max. Polar Moment of Inertia: lb inch2
Spinner Diameter: inches
Spinner Distance to Flange: inches
spinnerDm.jpg, 6,7kB
Spinner Tip (pointed ore round):
AIRCRAFT DESIGN CONDITIONS
Max. Speed at Sea Level KTAS @ HP @ RPM @
Desired Thrust lbs
Max. Speed KTAS @ ft MSL @ HP @ RPM @
Desired Thrust lbs
VNE: KIAS
Best Climb Rate ft/min @ KIAS
Aircraft data for 1xP Excitation Evaluation
Engine Position: Wing Nose
Angle between the Propeller Axis and Wing Chord deg
Max. Climb: Angledeg @ KTAS @ HP @ RPM
Max. Descent: Angledeg @ KTAS @ HP @ RPM
Max. Yaw: Angledeg @ KTAS @ HP @ RPM
Additional Comments:
Name Address:
First Name:
Last Name:
Company:
Street:
City, State:
ZIP-Code:
Country:
Phone No:
Fax No:
E-mail:


AVIA PROPELLER
Tel: (+420) 296 336 530; -32,    Fax: (+420) 296 336 519
E-Mail: sales@aviapropeller.cz,