U.S. DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION

TYPE CERTIFICATE DATA SHEET P2BO	TCDS NUMBER P2BO
REVISION: 1
DATE: September 22, 1994
AVIA-Hamilton Standard
Aviation-Ltd.
MODEL/S: VJ8.510	

This Data Sheet, which is part of Type Certificate No. P2BO, prescribes conditions and limitations under which
the product meets the airworthiness requirements of the Federal Aviation Regulations.

Type Certificate Holder 		AVIA-Hamilton Standard
				Aviation Ltd.
				P.O. Box 22
				250 02 Stara Boleslav
				Czech Republic

Type				Constant speed; hydraulic (See Notes 3 and 4)

Engine shaft 			Flanged: 4.25" bolt circle

Hub material 			Steel (forged)

Blade material: 			Aluminum Alloy

Number of blades 		5

Design series 			VJ8.510

Hub	

BLADES
	MAXIMUM
CONTINUOUS
HP/ RPM
KW	
<TAKE OFF>
HP/ RPM
KW	
NOMINAL
DIAMETER	
APPROXIMATE
WEIGHT
	
068-2100	068-1100
CW Rotation	779 2080
580	779/ 2080
580	90.5 in.
230 cm.	186 lbs.
84.5 kg.	

CERTIFICATION BASIS:	The U.S. certification basis determined under Section 21.29 of the FAR and
				Bilateral Airworthiness Agreement between the United States and the Czechl
				Republic is FAR 35, effective February 1, 1965, Amendments 35-1 to 35-6
				inclusive.
TC (IMPORT) NO:
TC APPLICATION DATE: 	May 10, 1990
TC ISSUED:			November 24, 1992

IMPORT REQUIREMENTS:	To be considered eligible for installation on U.S. registered aircraft, each propeller
				to be exported to the United States shall be accompanied by a certificate of
				airworthiness for export or certifying statement endorsed by the exporting
				cognizant civil airworthiness authority which contains the following language:
				(1)   This propeller conforms to its United States type design (Type Certificate
				number P2BO and is in a condition for safe operation.
				(2)   This propeller has been subjected by the manufacturer to a final operational
				check and is in a proper state of airworthiness.
				Reference FAR Section 21.500 which provides for the airworthiness acceptance
				of aircraft engines or propellers manufactured outside the U.S. for which a U.S.
				type certificate has been issued.

				Additional guidance is contained in FAA Advisory Circular 21-23, Airworthiness
				Certification of Civil Aircraft, Engines, Propellers and Related Products, Imported
				into the United States.

				NOTES

NOTE 1:	Hub Model Designation: 	Not applicable
		068-2100

NOTE 2.	Blade Model		Not applicable
		Designation:
		068-1100 (Clockwise Rotation)

NOTE 3:	 Pitch control:		· Propeller Speed Limiter 				065-2600
					· Propeller Speed Hydraulic Regulator 		LUN 7816-8
					· Propeller Electro Hydraulic Actuator 		LUN 7880-01-8

NOTE 4: 	(a) Feathering:		Model incorporates feathering and unfeathering features by means of
					counterweights and motor/pump unit and electro-hydraulic actuator and
					propeller speed hydraulic regulator
		(b) Reversing:		Model incorporates reversing feature. (Maximum reversing angle -24°)

NOTE 5: 	Right- and left-hand 	The approved model is right-hand (clock-wise rotation) tractor when
		models:			viewed from slip stream	
		
NOTE 6: 	Interchangeable blades: 	Not applicable.

NOTE 7:	Accessories -		· Propeller Speed Limiter 				065-2600
		Assemblies of the		· Brush Block Assembly 				LUN 7850-7	
		VJ8.510 Propeller	· Propeller Speed Hydraulic Regulator 		LUN 7816-8
		System:			· Electro-Hydraulic Actuator 			LUN 7880-01-8
					· Auxiliary Pump 				0,7S	LUN 7840-8
					· Pressure Switch 				0,8S	LUN 1492.04-8
					· Timing Relay 					LUN 2601.01-8
					· Timer 						LUN 3193.1-8
					· Propeller 					V510(7)
					· Propeller De-Icing -Electrical three-phase A.C. voltage to leading
					  edge blade heaters.

NOTE 8: 	Shank Fairings: 		Not applicable

NOTE 9:	 Special Limits: 		Life limited components of the AVIA VJ8.510 propeller are
					listed on page 18 of the AVIA Maintenance Manual, 061-
					00.10.

NOTE 10: 	Special Notes: 		(a) Aircraft installations must be approved as part of the
					aircraft type certificate and demonstrate compliance with
					the applicable aircraft airworthiness requirements.

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