AVIA PROPELLER - Propeller design specification form

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:

RPM

Max. Continuous:

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

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

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,