TCDS P-907

DEPARTMENT OF TRANSPORTATION P-907 FEDERAL AVIATION ADMINISTRATION Revision 19 Hartzell HC-B3Z TYPE CERTIFICATE DATA SHEET NO. P-907 April 20, 2021 Propellers of models described herein conforming with this data sheet (which is part o f Type Certificate No. P-907) and other approved 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 Holder Hartzell Propeller Inc. Piqua, OH 45356 Type Certificate Holder Record Hartzell Propeller Inc. Piqua, OH 45356 Type Constant speed; hydraulic (See NOTES 3 and 4) Engine shaft SAE spline or special flange (See NOTE 1) Hub material Alloy Steel Blade material See “Notes” column in table below Number of blades Three Hub models HC-B3Z20-1, -2; HC-B3Z22-7; HC-B3Z30-2; HC-B3ZF-2 (See NOTES 1, 3 and 4) Maximum Diameter Approx. Max. Wt. Complete Blades Continuous Takeoff Limits (For Reference Only) (See NOTES 2 & 6) HP RPM HP RPM (See NOTE 2) (See NOTES 3 and 7) Notes Hub Models HC-B3Z20-1, -2 9349-0 390 2330 420 2330 93” to 80” 105 lb. Aluminum Alloy to 9349-13 (-0 to -13) 9350-0 390 2330 420 2330 93” to 80” 105 lb. Aluminum Alloy to 9350-13 (-0 to -13) 10151-0 390 2180 400 2180 101” to 90” 108 lb. Aluminum Alloy to 10151-11 (-0 to -11) 10151C-0 390 2180 400 2180 101” to 90” 108 lb. Aluminum Alloy to 10151C-11 (-0 to -11) 10152-5 1/2 450 2300 450 2300 95 1/2” to 88” 119 lb. Aluminum Alloy to 10152-13 (-5 1/2 to -13) 10160-6 450 2300 450 2300 95” to 89” 120 lb. Aluminum Alloy to 10160-12 (-6 to -12) 11451-4 390 1700 390 1700 110” to 100” 122 lb. Aluminum Alloy to 11451-14 (-4 to -14) Hub Model HC-B3Z30-2 9349+1/2 390 2330 420 2330 93 1/2” to 80” 105 lb. Aluminum Alloy to 9349-13 (+1/2 to -13) 9350+1/2 390 2330 420 2330 93 1/2” to 80” 105 lb. Aluminum Alloy to 9350-13 (+1/2 to -13) 10151-0 390 2180 400 2180 101” to 90” 108 lb. Aluminum Alloy to 10151-11 (-0 to -11) 10152-5 1/2 450 2300 450 2300 95 1/2” to 90” 120 lb. Aluminum Alloy to 10152-11 (-5 1/2 to -11) 10160-6 468 2400 468 2400 95” to 90” 121 lb. Aluminum Alloy to 10160-11 (-6 to -11) P-907 Page 2 of 6 Revision 19 Maximum Diameter Approx. Max. Wt. Complete Blades Continuous Takeoff Limits (For Reference Only) (See NOTES 2 & 6) HP RPM HP RPM (See NOTE 2) (See NOTES 3 and 7) Notes Hub Model HC-B3ZF-2 9349-0 300 2070 340 2140 93” to 80” 105 lb. Aluminum Alloy to 9349-13 (-0 to -13) 9350-0 300 2070 340 2140 93” to 80” 105 lb. Aluminum Alloy to 9350-13 (-0 to -13) 10151-0 300 2070 340 2140 101” to 90” 108 lb. Aluminum Alloy to 10151-11 (-0 to -11) 10151C-0 300 2070 340 2140 101” to 90” 108 lb. Aluminum Alloy to 10151C-11 (-0 to -11) 10152-5 1/2 300 2070 340 2140 95 1/2” to 88” 119 lb. Aluminum Alloy to 10152-13 (-5 1/2 to -13) Hub Model HC-B3Z22-7 8447-0 420 2600 420 2600 84” to 78” 95 lb. Aluminum Alloy to 8447-6 (-0 to -6) 8847-0 420 2600 420 2600 84” to 78” 97 lb. Aluminum Alloy to 8847-6 (-0 to -6) 9349-0 390 2330 420 2330 93” to 80” 100 lb. Aluminum Alloy to 9349-13 (-0 to -13) 9350-0 390 2330 420 2330 93” to 80” 100 lb. Aluminum Alloy to 9350-13 (-0 to -13) 10151-0 390 2180 400 2180 101” to 90” 103 lb. Aluminum Alloy to 10151-11 (-0 to -11) 10151C-0 390 2180 400 2180 101” to 90” 103 lb. Aluminum Alloy to 10151C-11 (-0 to -11) 10152-5 1/2 450 2300 450 2300 95 1/2” to 88” 114 lb. Aluminum Alloy to 10152-13 (-5 1/2 to -13) 10160-6 450 2300 450 2300 95” to 90” 115 lb. Aluminum Alloy to 10160-11 (-6 to -11) 11451-4 390 1700 390 1700 110” to 100” 117 lb. Aluminum Alloy to 11451-14 (-4 to -14) Certification Basis: Civil Air Regulations Part 14 effective December 15, 1956. Type Certificate no. P-907 issued October 7, 1958. Date of application for Type Certificate: May 16, 1958. The following models were included under the original certification basis: HC-B3Z30-2; HC-B3Z20-(1,2); HC-B3ZF-2 The following models were added, updated or revised in accordance with 14 CFR Part 35 with amendment 35-1 effective February1, 1965: HC-B3Z22-7 The following models were added, updated or revised under Delegated Option Authorization procedures of 14 CFR Part 21 Subpart J in accordance with 14 CFR Part 35 with amendments 35-1 through 35-6 effective August 18, 1990: HC-B3Z20-(1,2) Production Basis: Production Certificate no. 10 Page 3 of 6 P-907 Revision 19 NOTE 1: Hub Model Designation HC - B 3 Z 30 - 2 D L when used denotes left hand rotation Any other character denotes a minor change not affecting eligibility Denotes specific design features (See NOTE 4) -1: non-feathering with counterweights and spring, governor pressure increases pitch -2: feathering with counterweights, governor pressure decreases pitch -7 non-feathering with counterweights and no spring, governor pressure decreases pitch 20 denotes SAE no. 20 spline 22 denotes French no. 22 spline 30 denotes SAE no. 30 spline F denotes flange with six 1/2” bolts and two 1/2” dowels on a 4” bolt circle Hartzell blade shank size Number of blades Identifies basic design (See NOTE 6) Hartzell Controllable NOTE 2: Blade Model Designation L 101 52 B - 5 ½ R Number when used indicates inches cut off from (or added to if +) basic diameter Q when used denotes special 1” x 90 deg. factory-bent tip. No cutoff permitted. R when used denotes specifically rounded tip for cutoff diameter. Any other character in this location denotes tip shape B or K when used denotes deicing boots C when used denotes a blade twist modification N denotes shank modification (see NOTE 6) R when used denotes a rounded tip for the basic diameter Any other character denotes a minor modification not affecting eligibility Basic model or template Basic diameter rounded to the nearest inch.* L when used denotes left-hand blades * Diameter limits are nominal diameters of the assembled propeller. They do not include the + or – 1/8 inch manufacturing tolerance the FAA allows for propellers with a basic diameter of less than 14 feet. NOTE 3: Pitch Control (a) Approved with Hartzell governors per drawings C-4772. Wt.: 4.5 to 6 lb. (see NOTE 10) B - 1 - 4 Z Governor Model Designation L when used indicates left hand rotation Z when used indicates drive coupling type Any other character denotes a minor change not affecting eligibility Minor adjustment not affecting eligibility Minor adjustment to obtain engine/propeller/governor compatibility Basic body and major parts modification (b) The -1, -2 and -7 models have counterweighted blades and use oil to decrease pitch. (See NOTE 4) (c) Maximum governor output pressure: 350 psi for all propeller models (d) All governors must be approved as part of the aircraft installation regardless of manufacturer. (See NOTE 10) P-907 Page 4 of 6 Revision 19 NOTE 4: Feathering The -1 and -7 models do not feather. The -2 models incorporate feathering and unfeathering features. Reversing Not applicable NOTE 5: Left-Hand Models The left-hand version of an approved propeller model is approved at the same rating and diameter as listed for the right-hand model. (See NOTES 1 and 2) NOTE 6: Interchangeability (a) Blades (1) Only blades listed in the same group of the following listed groups are sufficiently similar aero- dynamically and vibrationwise to permit interchangeability in the same diameter without a flight test. Group (A): 9349, 9350 (2) 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 the letter “N” in the basic model number, the “N” character must be retained in all replacement blade models. For example: Blades without the “N” suffix may be replaced by “N” suffix blades. Blades with the “N” suffix may only be replaced by “N” suffix blades (3) Shot-peened blades may replace non shot-peened blades either individually or as a set (See NOTE 2) (b) Propellers (1) Propeller models listed in this data sheet may replace, but not be replaced by, corresponding propeller models listed in Type Certificate Data Sheet no. P-891. Propeller models listed in this data sheet are interchangeable with corresponding propeller models listed in Type Certificate Data Sheet no. P2EA. Refer to the following tables (read across same row): Prop models on TCDS P-891 may be replaced by Corresponding models on TCDS P-907 HC-93Z20-1 HC-B3Z20-1 HC-93Z20-2 HC-B3Z20-2 HC-93Z30-2 HC-B3Z30-2 HC-93ZF-2 HC-B3ZF-2 Prop models on TCDS P-907 are interchangeable with Corresponding models on TCDS P2EA HC-B3Z20-1 HC-B3W20-1 HC-B3Z20-2 HC-B3W20-2 HC-B3Z30-2 HC-B3W30-2 HC-B3ZF-2 HC-B3WF-2 (c) Governors (See NOTE 3) (1) Hartzell governors with a “Z” suffix in their model designation may be used interchangeably with corresponding governors without the “Z”. For example, the F-6-24Z is a replacement for the F-6-24 and the F-6-24 is a replacement for the F-6-24Z. (2) The Hartzell B-0 is the only model which is interchangeable with the Hamilton Standard 1M12 or 1Q12. Other Hartzell models are not interchangeable with any Hamilton Standard model without modification of the latter. (d) Ice Protection Systems Refer to Hartzell service Letter HC-SL-30-260 for ice protection system component interchangeability Page 5 of 6 P-907 Revision 19 NOTE 7: Accessories (See NOTE 10) (a) Propeller ice protection system (weight of ice protection system extra) (1) Propeller models listed in this data sheet are approved for use with propeller ice protection equipment listed in Hartzell Manual 159 or in other Hartzell type design data. (2) All propeller ice protection equipment must be approved as part of the aircraft installation regardless of manufacturer. (See NOTE 10) (b) Propeller spinner (weight of spinner extra) (1) Approved with Hartzell and other manufacturers’ spinners when listed on Hartzell type design data. (2) All propeller spinners must be approved as part of the aircraft installation regardless of manufacturer. (see NOTE 10) NOTE 8: Shank Fairings Not applicable. NOTE 9: Special Limits Table of Propeller - Engine Combinations Approved Vibrationwise for Use on Normal Category Single Engine Tractor Aircraft The maximum and minimum propeller diameters that can be used from a vibration standpoint are shown below. No reduction below the minimum diameter listed is permissible, since this figure includes the diameter reduction allowable for repair purposes. The engine models listed below are the configurations on the engine type certificate unless specifically stated otherwise. Modifications to the engine or airframe that alter the power of the engine models listed below during any phase of operation have the p otential to increase propeller stresses and are not approved by this list. Such modifications include, but are not limited to, the addition of a turbocharger or turbonormalizer, increased boost pressure, increased compression ratio, increas ed RPM, altered ignition timing, electronic ignition, full authority digital engine controls (FADEC), or tuned induction or exhaust. Also, any change to the mass or stiffness of the crankshaft/counterweight assembly is not approved by this list. Hub Blade Max. Dia. Min. Dia. Model Model Engine Model (inches) (inches) Placards HC-B3Z20 9349 Lycoming R-680-E3A 88 82 none HC-B3Z20 9349 Lycoming R-680-E3B 88 88 none HC-B3Z30 9349 Lycoming IGO-540-B1A Lycoming IGSO-540-B1A 93 ½ 86 none HC-B3Z20 9350 Lycoming R-680-E3A 88 82 none HC-B3Z20 9350 Lycoming R-680-E3B 88 88 none HC-B3Z30 9350 Lycoming IGO-540-B1A Lycoming IGSO-540-B1A 93 ½ 93 ½ none HC-B3Z20 10151 Lycoming GO-480-G1A6, -G1D6 101 95 none HC-B3Z20 HC-B3ZF 10151 Lycoming GSO-480 series with five 3rd order and one 6th order dampers; 7.3:1 compression ratio; 340 HP @ 3400 RPM or less 93 90 none P-907 Page 6 of 6 Revision 19 Hub Blade Max. Dia. Min. Dia. Model Model Engine Model (inches) (inches) Placards HC-B3Z20 10151 Lycoming IGSO-480 series with five 3rd order and one 6th order dampers; 7.3:1 compression ratio; 340 HP @ 3400 RPM or less 93 90 none HC-B3Z30 10151 Lycoming IGSO-540-A1A, -A1E, -A1H, -B1A 93 ½ 90 ½ none HC-B3Z20 10151C Lycoming GO-480-F2D6, -G1D6 101 95 none HC-B3Z30 10152-5 ½ P&WA R-985 with one 4 ½ order and one 9th order crankshaft dampers 95 ½ 95 ½ none HC-B3Z30 10152-7 ½ P&WA R-985 with one 4 ½ order and one 9th order crankshaft dampers 93 ½ 93 ½ Avoid continuous operation between 1600 and 1850 RPM HC-B3Z30 10160-6 P&WA R-985 with one 4 ½ order and one 9th order crankshaft dampers 95 95 Avoid continuous operation between 1600 and 1800 RPM HC-B3Z20 10160-8 Jacobs R-755A2 93 93 none NOTE 10: Propeller installation must be approved as part of the aircraft Type Certificate and demonstrate compliance with the applicable aircraft airworthiness requirements. Propeller models listed herein consist of basic hub and blade models. Most propeller models include additional characters to denote minor changes and specific features as explained in NOTES 1 and 2. Refer to the aircraft Type Certificate Data Sheet for the specific propeller model applicable to the installation. NOTE 11: Special Limits (a) Life Limits and Mandatory Inspections (1) Airworthiness limitations, if any, are stated in Hartzell Manuals 108( ), 114( ) or Service Letter 61( ). The propeller CMACO must evaluate the propeller installation for each new aircraft installation to assess possible changes in the airworthiness limitations. NOTE 12: Special Notes (a) Refer to Hartzell Manual no. 202( ) for overspeed and overtorque limits. (b) Refer to Hartzell Service Letter HC-SL-61-61( ) for overhaul periods. END