TCDS P24EA

DEPARTMENT OF TRANSPORTATION P24EA FEDERAL AVIATION ADMINISTRATION Revision 7 Hartzell HC-A2V, HC-A2MV BHC-A2V, BHC-A2MV November 19, 1998 TYPE CERTIFICATE DATA SHEET NO. P24EA Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P24EA) 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 Constant speed; hydraulic (see NOTES 3 and 4) Engine Shaft Spline shaft, special flange (see NOTE 1) Hub material Alloy steel Blade material Aluminum alloy Number of blades Two Hub models (B)HC-A2(M)VF-(1,2,3), HC-A2(M)VF-6, HC-A2(M)VK-(1,2,3) HC-A2(M)VL-(1,2,6), HC-A2(M)V20-(1,2,3,4,5) (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 (B)HC-A2(M)VF-(1,2,3), HC-A2(M)VF-6, HC-A2(M)VK-(1,2,3), HC-A2(M)V20-(1,2,3,4,5) V7636C-0 225 3000 225 3000 76” to 68” 64.0 lb. to V7636C-8 (-0 to -8) V7636D-0 225 3000 225 3000 76” to 68” 64.0 lb. to V7636D-8 (-0 to -8) V8433-0 260 2625 260 2625 84” to 72” 67.0 lb. to V8433-12 (-0 to -12) V8433S-0 260 2625 260 2625 84” to 72” 67.0 lb. to V8433S-12 (-0 to -12) V8833-0 260 2600 260 2600 88” to 78” 68.0 lb. to V8833-10 (-0 to -10) V9333D-0 260 2400 280 2400 93” to 80” 72.0 lb. to V9333D-13 (-0 to -13) V10133D-0 260 2180 260 2180 101” to 98” 77.0 lb. to V10133D-3 (-0 to -3) V10133D-3 280 2180 280 2180 98” to 95” 77.0 lb. to V10133D-6 (-3 to -6) Weights apply to ( )HC-A2(M)V(F,K)-2 hub models. Subtract 4 lb. for -1 hubs, 2 lb. for -3 hubs and 9 lb. for -6 hubs. For HC-A2(M)V20 hub models, subtract 5 lb. for -1 and -4 hubs and 1 lb. for -2 and -3 hubs. Add 4 lb. for -5 hubs. Page No. 1 2 3 4 5 6 7 Rev. No. 7 4 5 4 4 4 4 P24EA 2 Revision 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-A2(M)VL-(1,2,6) V7636C-0 180 2700 180 2700 76” to 68” 64.0 lb. to V7636C-8 (-0 to -8) V7636D-0 180 2700 180 2700 76” to 68” 64.0 lb. to V7636D-8 (-0 to -8) V8433-0 180 2600 180 2600 84” to 78” 67.0 lb. to V8433-6 (-0 to -6) V8433-8 180 2700 180 2700 76” to 70” 67.0 lb. to V8433-14 (-8 to -14) V8433S-0 180 2600 180 2600 84” to 78” 67.0 lb. to V8433S-6 (-0 to -6) V8433S-8 180 2700 180 2700 76” to 70” 67.0 lb. to V8433S-14 (-8 to -14) V8833-0 180 2600 180 2600 88” to 78” 68.0 lb. to V8833-10 (-0 to -10) Weights apply to HC-A2(M)VL-2 hub models. Subtract 4 lb. for -1 hubs and 9 lb. for -6 hubs. Certification Basis: ( )A2V( ) models: FAR Part 35 with amendments 35-1 and 35-2 effective Feb. 1, 1965 ( )A2MV( ) models: FAR Part 35 with amendments 35-1 through 35-6 effective Aug. 18, 1990 Type Certificate No. P24EA issued April 1, 1966 Date of application for Type Certificate: December 1, 1965 Production Basis: Production Certificate no. 10 3 P24EA Revision 5 NOTE 1. Hub Model Designation ( ) HC A 2 V F - 2 A 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 1/2” bolts and two 1/2” dowels on a 4” bolt circle K denotes SAE # 2 flange with six 1/2” bolts and four 3/4” bushings on a 4-3/4” bolt circle L similar to K except uses 7/16” bolts 20 denotes SAE #20 spline V denotes a double shoulder blade retention system MV denotes a single shoulder blade retention system 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 Blank: 90 and 270 deg. clockwise B: 30 and 210 deg. clockwise NOTE 2: Blade Model Designation L V 84 33 N - 3Q Number of inches cut off from basic diameter Q when used denotes special 1” x 90 deg. factory-bent tip. R when used denotes specifically rounded tip for cutoff diameter. * C or D denotes a dimensional modification from the original design B or K denotes deicing boots R when used denotes a rounded tip for the basic diameter * S when used denotes a square tip for the basic diameter * H denotes hard alloy (see NOTE 6) N denotes a shank modification Basic blade model Basic diameter in inches V denotes a double shoulder blade shank with internal needle bearing MV denotes a single shoulder blade shank with internal needle bearing L when used denotes left hand blade * Some blades which use square or round tip shapes may not contain the letters “S” or “R” in their model designation. These characters are used to distinguish blades when two or more tip shapes are available at the same diameter. P24EA 4 Revision 4 NOTE 3. Pitch Control (a) Approved with Hartzell governors per drawings C-4770 and C-4772. Wt.: 4.5 lb. D - 1 - 4 Governor model designation Minor adjustment not affecting eligibility Minor adjustment to obtain engine/propeller/governor compatibility Basic body and major parts modification (b) Approved with Hoof model 1-000-007 series Wt.: 3.5 lb. (c) Approved with Hamilton Standard models 1A4, 1M12, 1P12, and 1Q12 Wt.: 4.5 lb. (d) Approved with Woodward model X210XXX or X210X-XXX. Wt.: 3.5 lb 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. NOTE 4. (a) Feathering The -2 models incorporate feathering and unfeathering features. (b) Reversing The -3 and -5 models incorporate reversing when used with the appropriate 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. NOTE 6. Interchangeability (a) Blades (1) Blade models 8433 and 8433S are interchangeable. (2) Hard alloy blades may be substituted for the corresponding blade model on seaplanes and amphibious aircraft only. (3) Blades with an “N” suffix, such as (M)V8433N, are interchangeable with corresponding blades without the “N” suffix, provided that all blades in the same propeller are identical. (4) Blades with “M” prefix, such as MV8433N, can be substituted for corresponding blades without the “M” prefix provided that all blades in the same propeller are identical and that the hub model also contains the characters “MV”. Blades without the “M” prefix cannot be substituted for those with the “M” prefix. (b) Propellers (1) Propellers listed in this data sheet may replace corresponding propellers listed in Type Certificate Data Sheets P23EA, P-878 and P-908. (2) Propellers listed in T.C.D.S. nos. P23EA, P-878 and P-908 may not replace propellers listed in this data sheet. (3) In the model designation HC-A2(V,MV)( ), the “A” may be substituted for propeller models with “8” in the same location and “V” or “MV” may be substituted for propeller models with “X” in the same location. (4) In the model designation HC-A2(V,MV)( ), the “MV” may be substituted for “V”, however “V” may not replace “MV”. 5 P24EA Revision 4 NOTE 7. Accessories (a) Propeller anti-icing (1) Approved with fluid feed shoes or Icex boots installed in accordance with Hartzell Special Instruction no. 59A. (2) Approved with Hartzell fluid feed equipment on propeller models for which equipment is available. (3) Approved with Cessna 0850305 slinger ring installed only on Cessna spinner (see item (c)(2) below. (b) Propeller deicing (1) Approved with Goodrich electrical deicing kit 77-XXX or 65-XXX when installed in accordance with BF 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. (c) Propeller spinner (1) Approved with Hartzell spinners. (weight of spinner extra) (2) Approved with Cessna spinner dome 0752006 and bulkhead 0850300 NOTE 8. Shank Fairings Not applicable NOTE 9. Special Limits Table of Propeller - Engine Combinations Approved Vibrationwise foe 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. Hub Blade Max. Dia. Min. Dia. Model Model Engine Model (inches) (inches) Placards HC-A2V V7636C LYC O-290-D2A 74 72 Never exceed 2750 RPM HC-A2V V7636C LYC O-320 76 72 none HC-A2V V7636D LYC O-290-D2A 76 72 none HC-A2V V7636D LYC O-320 76 70 none HC-A2V V7636D LYC O-320-B1A 72 70 none HC-A2V V7636D LYC O-340 76 72 none HC-A2V V8433( )-9Q LYC O-540-A1A5, -A1B5, -A1C5, -A1D5 75 75 none HC-A2V BHC-A2V V8433 TCM O-470-A, -J 84 82 none P24EA 6 Revision 4 Hub Blade Max. Dia. Min. Dia. Model Model Engine Model (inches) (inches) Placards HC-A2V BHC-A2V V8433 TCM O-470-B 84 80 none HC-A2V V8433 TCM O-470-H 84 81 none HC-A2V BHC-A2V V8433 TCM O-470-K, -L 84 78 none HC-A2V V8433 TCM O-470-M 84 78 none HC-A2V V8433 TCM IO-470-D, -E, -F, -S 84 78 none HC-A2V V8433 TCM IO-470-C 84 80 none HC-A2V BHC-A2V V8433 TCM TSIO-470-B 80 78 none HC-A2V V8433 TCM E-185 84 76 Dampened engine only. Do not exceed 2600 RPM at takeoff HC-A2V V8433 TCM E-225 84 80 Do not exceed 2600 RPM at takeoff HC-A2V V8433 LYC O-435-A, -C 78 75 none HC-A2V V8433 LYC O-435-A2, -C1 78 76 none HC-A2V V8433 LYC O-320 72 70 none HC-A2V V8433 LYC O-340, O-340-A1A 72 70 none HC-A2V V8433 LYC O-540-A1A, -A2B 82 80 none HC-A2V V8433 LYC O-540-A1A 77 76 Avoid continuous operation between 2225 and 2275 RPM HC-A2V V8433 LYC O-540-A1A5, -A1B5, -B1A5, -B1B5, -C1A5 77 73 none HC-A2V V8833 TCM E-185 series with one 5th and one 6th order dampers, 7 to 1 compression ratio or less, 225 HP at 2650 RPM or less 84 78 none HC-A2V V8833 TCM E-225 88 86 Avoid continuous operation on the ground between 1400 and 1700 RPM and between 1900 and 2100 RPM. Avoid continuous operation on the ground and in flight between 2450 and 2550 RPM HC-A2V V8833 TCM E-225 series with one 5th and one 6th order dampers, 7 to 1 compression ratio or less, 225 HP at 2650 RPM or less 84 78 none HC-A2V BHC-A2V V8833 TCM O-470-A, -J 88 86 none 7 P24EA Revision 4 Hub Blade Max. Dia. Min. Dia. Model Model Engine Model (inches) (inches) Placards HC-A2V V8833 TCM O-470-E, -K, -L 88 86 none HC-A2V V8833 LYC O-540-A1A5 88 86 Avoid continuous operation between 1950 and 2200 RPM BHC-A2V V8833 TCM O-470-K, -L 88 88 none BHC-A2V V8833 TCM O-470-R 84 78 none 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 Manuals 100( ), 109( ) and 114( ). ....END....