TCDS P16EA

DEPARTMENT OF TRANSPORTATION P16EA FEDERAL AVIATION ADMINISTRATION Revision 10 Hartzell HC-92W, BHC-92W March 8, 2005 TYPE CERTIFICATE DATA SHEET NO. P16EA Propellers of models described he rein conforming with this data sheet (which is part of Type Certificate No. P16EA) and other approved data on file with the Federal Avia tion 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 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 Two Hub models HC-92WK-1, -2, -8; HC-92WF-3, -5, -8; BHC-92WF-1, -3, -5; (see NOTES 1 and 4) Maximum Diameter Approx. Max. Wt. Complete Blades Continuous Takeoff Limits (For Reference Only) (see NOTE 2) HP RPM HP RPM (see NOTE 2) (see NOTES 3 and 7) HUB MODELS HC-92WK-1, -8 W8447-0 300 2800 300 2800 84” to 70” 73.0 lb. to W8447-14 (-0 to -14) W8447A-8 250 2800 250 2800 76” to 70” 72.0 lb. to W 8447A-14 (-8 to -14) W8847-0 280 2600 280 2600 88” to 82” 78.0 lb. to W8847-6 (-0 to -6) W9349-0 280 2400 280 2400 92 5/8” to 77 5/8” 82.0 lb. to W9349-15 (-0 to -15) W9350-0 280 2400 280 2400 92 5/8” to 88” 82.0 lb. to W9350-4.6 (-0 to -4.6) W9350-4.6 300 2600 300 2600 88” to 77 5/8” 81.0 lb. to W9350-15 (-4.6 to -15) W9591-0 300 2200 300 2200 95” to 85” 66.0 lb. to W9591-10 (-0 to -10) (for -8D) P16EA, Rev 10 Page 2 of 6 Maximum Diameter Approx. Max. Wt. Complete Blades Continuous Takeoff Limits (For Reference Only) (see NOTE 2) HP RPM HP RPM (see NOTE 2) (see NOTES 3 and 7) HUB MODELS BHC-92WF-1, HC-92WK-2, HC-92WF-3, BHC-92WF-3, HC-92WF-5, BHC-92WF-5 W8447-0 300 2800 300 2800 84” to 70” 74.0 lb. to W8447-14 (-0 to -14) W8447A-8 250 2800 250 2800 76” to 70” 72.0 lb. to W8447A-14 (-8 to -14) W8447-12A 250 2800 250 2800 72” to 68” 72.0 lb. to W8447-16A (-12 to -16) W8447A-12A 250 2800 250 2800 72” to 68” 72.0 lb. to W8447A-16A (-12 to -16) Certification Basis: CAR 14 effective December 15, 1956 with Amendment 14-1 thereto. Type Certificate No. P16EA issued April 3, 1964. Models approved to the original certification basis include HC-92WK-1, -2, -8. The following models were approved under Delegated Option Authorization Procedures of 14 CFR Part 21, Subpart J. Models added, updated or revised in accordance with 14 CFR Part 35 effective February 1, 1965 with amendment 35-1 include the following: HC-92WF-3, BHC-92WF-3 Models added, updated or revised in accordance with 14 CFR Part 35 effective April 3, 1967 with amendments 35-1 and 35-2 include the following: HC-92WK-1, -8, HC-92WF-5, -8, BHC-92WF-5 Models added, updated or revised in accordance with 14 CFR Part 35 effective August 18, 1990 with amendments 35-1 through 35-6 include the following: BHC-92WF-1 Date of application for Type Certificate: February 26, 1964. Production Basis: Production Certificate no. 10 NOTE 1: Hub Model Designation B HC -9 2 W F -2 A G when used denotes special adapter and fan for airship installation L denotes left hand rotation Any other character denotes a minor change not affecting eligibility Denotes specific design features (see NOTE 4) F denotes special flange with six ½” bolts and two ½” dowels on a 4” bolt circle K denotes SAE no. 2 flange with six ½” bolts and four ¾” bushings on a 4-3/4” bolt circle Hartzell blade shank size Number of blades Identifies basic design Hartzell Controllable Indicates dowel location with respect to centerline through blade sockets when viewing hub from flange mounting face (“F” flange hubs only) Blank: 90 and 270 deg. clockwise B: 30 and 210 deg. clockwise Page 3 of 6 P16EA, Rev 10 NOTE 2: Blade Model Designation L W 84 47 A -8 Q Q when used denotes special 1” x 90 deg. factory-bent tip for cutoff diameter A after the dash number indicates a thinner and narrower tip Number of inches cut off from basic diameter A after the model designation denotes 0° sweepback (otherwise sweepback is 1°) B or K denotes deicing boots N denotes shank modification (see NOTE 6) Basic model or template Basic diameter in inches Denotes needle bearing installation in blade shank L when used denotes left hand blade NOTE 3: Pitch Control (a) Approved with Hartzell governors per drawings C-4770 and C-4772. Wt.: 4.5 lb. 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, -3 and -5 models have counterweighted blades and use oil to decrease pitch. The -8 models do not have counterweighted blades and use oil to increase 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) NOTE 4: Feathering and Reversing (a) Feathering The -2 and -5 models incorporate feathering and unfeathering features. The -1, -3, and -8 models do not feather. (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 propeller model is approved at the same rating and diameter as listed for the right-hand model. (See NOTES 1 and 2) P16EA, Rev 10 Page 4 of 6 NOTE 6: Interchangeability (a) Blades (1) 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. (2) Only blades listed in the same groups of the following listed groups are sufficiently similar aerodynamically and vibrationwise to permit interchangeability in the same diameter without a flight test. Group (a) W8447-8 to -14, W8447A-8 to -14 Group (b) W8447-12A to -16A, W8447A-12A to -16A Group (c) W8447-12R to -13R, W8447A-12R to -13R (b) 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 and 1Q12. Other Hartzell models are not interchangeable with any Hamilton Standard model without modification of the latter. (c) Propellers (See NOTES 1 and 2) (1) The following propeller models may replace corresponding propellers listed in Type Certificate Data Sheet P-892 as indicated below. Propellers listed in P-892 are not approved to replace propellers listed in this data sheet. For example (B)HC-92W( ) models using blades with a “W” prefix may replace corresponding (B)HC-92Z( ) models using blades with no prefix. TCDS P16EA TCDS P-892 HC-92WK-1D HC-92ZK-1D BHC-92WF-1D1 BHC-92ZF-1D1 HC-92WK-2B HC-92ZK-2B BHC-92WF-3 BHC-92ZF-3 BHC-92WF-3LG BHC-92ZF-3LG HC-92WK-8D HC-92ZK-8D HC-92WK-8L HC-92ZK-8L NOTE 7: Accessories (a) Propeller anti-icing (weight of anti-icing system extra) (1) Approved with fluid feed boots listed on Hartzell approved type design data when installed in accordance with Hartzell specification H-S-2 or Hartzell Manual no. 133( ). (2) Approved with Hartzell fluid feed equipment on propeller models for which equipment is available. (b) Propeller deicing (weight of deicing system extra) (1) Approved with Goodrich electrical deicing kit 5EXXXX, 7EXXXX, 77-XXX, 67-XXX or 65-XXX when installed in accordance with Goodrich Report no. ATA 30-60-07. (2) Approved with Goodyear Ice Guards (electrical propeller deicer) when installed in accordance with instructions outlined in Goodyear Report no. AP-147 dated October 23, 1961. (3) Approved with ice protection equipment when listed on Hartzell type design data. Page 5 of 6 P16EA, Rev 10 (c) Propeller spinner (weight of spinner extra) Approved with spinners when listed on Hartzell type design data. (d) Propeller Adapter Propeller hub models with -3G or -3LG suffix incorporate a Hartzell pulley adapter P/N C-2987 and Cessna fan P/N 1457210 for use on a Goodyear Airship. Additional weight 21 lb. (When used, combination may be operated to 210 HP at 2800 RPM) 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 propelle r diameters that can be used from a vibrati on 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 c onfigurations on the engine type certificat e unless specifically stated otherwise. Modifications to the engine or airframe that alter the power of the engine models listed be low during any phase of operation have the potential to increase propeller stresses and are not approve d by this list. Such modi fications include, but are not limited to, the addition of a turbocharger or turbonormalizer, increased boost pressure, increas ed compression ratio, increased RPM, altered ignition timing, electronic i gnition, full authority digital engine cont rols (FADEC), or tuned induction or exhaus t. 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-92WF W8447 TCM TSIO-520 and IO-520 series, 7.5 to 1 compression ratio or less, 285 HP at 2700 RPM or less 82 81 none HC-92WK W8447-( )A LYC O-360-A1A, IO-360-B1A 72 70 none HC-92WK W8447-( )R LYC O-360-A1A, IO-360-B1A 72 71 none HC-92WK W8447A LYC IO-360-A1A, -A1D 76 72 Avoid continuous operation between 2250 and 2500 RPM HC-92WK W8447-( )R LYC O-360 and IO-360 series engines, 8.5 to 1 compression ratio or less, 180 HP at 2700 RPM or less 72 71 none HC-92WF W8847 TCM IO-470 series, 8.6 to 1 compression ratio or less, four 6th order dampers, 260 HP at 2625 RPM or less, “Z” engine dowel location 88 88 none HC-92WK W9349 LYC IO-540-A1A5, -B1A5, -B1C5, -E1A5, -E1B5, -G1A5, -G1B5, -G1C5, -G1D5, -G1E5, 280 HP at 2400 RPM 88 88 Do not exceed 23 in. Hg manifold pressure below 2350 RPM HC-92WK W9350 LYC IO-540-A1A5, -B1A5, -B1C5, -E1A5, -E1B5, -G1A5, -G1B5, -G1C5, -G1D5, -G1E5, 300 HP at 2600 RPM 88 88 Do not exceed 23 in. Hg manifold pressure below 2350 RPM P16EA, Rev 10 Page 6 of 6 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 or STC for the specific propeller model applicable to the installation. NOTE 11: Retirement Time (a) Life Limits and Mandatory Inspections (1) Airworthiness limitations, if any, are specified in Hartzell Manuals 105( ), 110( ), 114( ), 119( ) or Service Letter 61( ). NOTE 12: Special Notes Refer to Manual 202( ) for overspeed and overtorque limits. END