DEPARTMENT  OF TRANSPORATION
 FEDERAL AVIATION ADMINISTRATION
		P44GL
	Revision 6
	Hartzell Propeller, Inc.
	HARTZELL
	HC-B5M
	March 9, 1998	

TYPE CERTIFICATE DATA SHEET NO. P44GL

Propellers of models described herein conforming with this data sheet (which is part of  Type Certificate No. P44GL) and other appoved data on file with the Federal Aviation Administration meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Federal Aviation Regulations provided they are installed, operated and maintained as prescribed by the approved manufacturer’s manuals and other approved instructions.

Type Certificate (T.C.) Holder:		Hartzell Propeller, Inc.
					Piqua, Ohio 45356

Type					Constant speed, hydraulic (See NOTES 3 and 4)
Engine Shaft				Special flange (See NOTE 1)
Hub Material				Alloy steel
Blade Material				Aluminum alloy
Number of Blades				Five
Hubs Models				HC-B5MP-3, HC-B5MP-5, HC-B5MA-3, HC-B5MA-5 (See NOTES 1 and 4)
			
			Maximum			Diameter		Approx. Max. Wt. Complete
Blades			Continuous	Takeoff		Limits		        (For Refrence Only)
(see Notes 2 & 6)		HP     RPM	HP     RPM	(See Note 2)	         (See Notes 3 & 7)

HC-B5MP-3
M10282+6		1120   1700    	1198   1700   	111.3"-104.7"   		220 lb.
to M10282+0                               			 	(+6 to +0)  

M10282+0		1120   1700    	1120   1700   	104.7"-98.7" 		215 lb 
to M10282-6                                				(-0 to -6)

M10876+0		1327   1700   	 1500   1700   	111.2"-105.2"  		230 lb.
to M10876-6                                				(-0 to -6)

					HC-B5MP-5, HC-B5MA-3
M11276-0		1327   1700    	1500   1700   	115.2"to 105.2"		254 lb.
to M11276-10						(-0 to -10)

					HC-B5MA-3, HC-B5MA-5
M11276-0		1650   1700    	1650   1700   	115.2"to 105.2"		254 lb.
to M11276-10						(-0 to -10)

						HC-B5MA-3
M11296-0		1650   1700    	1650   1700   	115.2"to 105.2"		255 lb.
to M11296-10						(-0 to -10)

M11296-0		1650   1700    	1650   1700   	118.7"to 108.7"		261 lb.
to M11296-10						(-0 to -10)

Certification Basis:		FAR 35 effective February 1, 1977, with Amendments 35-1 and 35-2 thereto.
				Type Certificate No. P44GL issued November 13, 1975
				Date of Application for T.C.: HC-B5MP-3: Dec. 10, 1973, revised March 8, 1974

Production Basis: 			Production Certificate No. 10

Page No.	1	2	3	
Rev. No,	6	6	1	

P44GL							2						

NOTE 1. Hub Model Designation

HC - B 5 M P - 3 AL

	HC	Hartzell controllable
	B	Identifies basic design
	5	Number of blades
	M  	Hartzell blade shank size
	P  	P denotes special flange with eight 9/16" bolts and four dowels on a 4-1/4" B.C.
		A denotes special flange with twelve 9/16" bolts and two dowels on a 5-1/8" B.C.
	3 	Denotes specific design features (See NOTE 4)
	A 	Denotes minor change not affecting eligibility
		L denotes left hand rotation

NOTE 2. Blade Model Designation

L M 102 82 AB - 2Q

	L	when used denotes left hand rotation
	M	Denotes needle bearing installation in blade shank
	102	Basic diameter in inches for a 3 blade propeller. Add 3.2 in. for 5 blades.
	82	Basic blade model
	AB	A denotes minor change not affecting eligibility
		N denotes shank modification (See NOTE 6)
		S denotes shot peened blade surface
    		B, E, or k denotes deicing boots
	2Q	Number of inches cut off from basic diameter (or added to if preceded by "+")
		Q when used denotes special 1" x 90 deg. factory-bent tip for cutoff diameter

NOTE 3. Pitch Control. 	Approved with the following governors:
			Woodward Model X210XXX or X210X-XXX (weight of governor extra)

NOTE 4. (a)	Feathering. The -3 and -5 models incorporate feathering unfeathering features.

	 (b)	Reversing. The -3 and -5 models are approved for installation as reversing propellers with appropriate reversing controls.

NOTE 5. Left-Hand Models.
	
	The left-hand version of an approved peopeller model is approved at the same rating and diameter as listed for the right-hand model. See NOTES 1 and 2.

							3						P44GL

NOTE 6.	Interchangeability.

		Blades with the suffix "N" in the basic model number may replace those without an "N" either individually or as a set.  When the aircraft Type Certificate or Supplemental Type Certificate specifies blades with an "N" in the basic model number, only the "N" blades may be used.

NOTE 7. Accessories.

	(a)	Propeller Spinner

		(1)	Approved with Hartzell spinners (weight of spinners extra).

	(b)	Propeller deice

		(1)	Approved with Goodrich electrical deicing kit 77-XXX, 67-XXX or 65-XXX when installed in accordance with Goodrich report report no. 59-728( ).
		(2)	Approved with Safeway 6870, 6880 deice boots when installed in accordance with manufacturer's instructions.

NOTE 8. Shank Fairings.
	
	Not applicable.

NOTE 9. Special Limits.

	Not applicable.

NOTE 10. Special Notes. 

	Propeller installation must be approved as part of the aircraft Type Certificate and demonstrate compliance with the applicable aircraft airworthiness requirements.

NOTE 11. Retirement Time. 
	
	(a)  Life Limits and Mandatory Inspections

		(1)  Airworthiness Limitations, if any, are specified in Hartzell Manual 132( ).

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