TCDS P-878

Page No. 1 2 3 4 5 6 Rev. No. 25 24 25 24 24 24 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P-878 Revision 25 HARTZELL HC-82X March 6, 1981 TYPE CERTIFICATE DATA SHEET NO. P-878 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. 878) 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. 350 Washington Avenue Piqua, Ohio 45356 Type Constant speed; hydraulic (see Notes 3 and 4) Engine shaft SAE #20 spline, SAE #2 flange, special flange 4" B.C. Hub material Alloy steel Blade material See below Number of blades Two Hubs eligible HC-82XF-1, -2, -3, -6; HC-82XG-1, -2, -6; HC-82XL-1, -2, -6; HC-82X20-1, -3, -5; HC-82-XK-1, -2, -3; HC-82XS-2 (see Notes 1, 3, and 4, and "Blades Eligible.") Blades Eligible Maximum Continuous Takeoff Diameter *Approx. Max. Wt. Complete with Grease, Mounting Bolts, etc. (see Note 2) HP RPM HP RPM Limits (see notes 3 and 7) Blade Construction Hub Models HC-82XF-1, -2, -3, -6; HC-82X20-1, -2, -3, -5; HC-82XK-1, -2, -3 7636C-0 to 7636C-8 225 3000 225 3000 76" - 68" (-0 to -8) 64 lbs. Aluminum alloy 7636D-0 to 7636D-8 225 3000 225 3000 76" - 60" (-0 to 8) 64 lbs. Aluminum alloy 8046-6 to 8046-14 150 2700 150 2700 74" - 66" (-6 to -14) 58 lbs. Special fabric base plastic; stainless steel or brass tipping. 8427+2 to 8427-4 215 2600 215 2600 86" - 80" (+2 to -4) 64 lbs. Special fabric base plastic; stainless steel or brass tipping 8428+2 to 8428-9 250 2600 250 2600 86" - 75" (+2 to -9) 64 lbs. Special fabric base plastic; stainless steel or brass tipping 8428X-0 to 8428X-9 215 or 240 2600 1920 215 260 2600 2180 84" - 75" (-0 to -9) 64 lbs. Special fabric base plastic; stainless steel or brass tipping 8433-0 to 8433-10 260 2625 260 2625 84" - 74" (-0 to -10) 67 lbs. Aluminum alloy 8433S-0 to 8433S-10 260 2625 260 2625 84" - 74" (-0 to -10) 67 lbs. Aluminum alloy P-878 2 Blades Eligible Maximum Continuous Takeoff Diameter *Approx. Max. Wt. Complete with Grease, Mounting Bolts, etc. (see Note 2) HP RPM HP RPM Limits (see notes 3 and 7) Blade Construction Hub Models HC-82XF-1, -2, -3, -6; HC-82X20-1, -2, -3, -5; HC-82XK-1, -2, -3 (cont'd) 8833-0 to 8833-10 240 2600 240 2600 88" - 78" (-0 to -10) 68 lbs. Aluminum alloy 9333C-0 to 9333C-5 260 2330 280 2330 93" - 88" (-0 to -5) 72 lbs. Aluminum alloy 10133D-0 to 10133D-6 260 2180 260 2180 101" - 95" (-0 to -6) 77 lbs. Aluminum alloy 10133D-3 to 10133D-6 280 2180 280 2180 98" - 95" (-3 to -6) 77 lbs. Aluminumm alloy Hub Models HC-82XG-1, -2, -6; HC-82XL-1, -2, -6 7636C-0 to 7636C-8 180 2700 180 2700 76" - 68" (-0 to -8) 64 lbs. Aluminum alloy 7636D-0 to 7636D-8 180 2700 180 2700 76" - 68" (-0 to -8) 64 lbs. Aluminum alloy 8046-6 to 8046-14 150 2700 150 2700 74" - 66" (-6 to -14) 58 lbs. Special fabric base plastic; stainless steel or brass tipping. 8427+2 to 8427-4 86" - 80" (+2 to -4) 64 lbs. Special fabric base plastic; stainless steel or brass tipping. 8428+2 to 8428-9 180 2600 180 2600 86" - 75" (+2 to -9) 64 lbs. Special fabric base plastic; stainless steel or brass tipping. 8428X-0 to 8428X-9 180 2600 180 2600 84" - 75" (-0 to -9) 64 lbs. Special fabric base plastic; stainless steel or brass tipping. 8433-0 to 8433-6 180 2600 180 2600 84" - 78" (-0 to -6) 67 lbs. Aluminum alloy 8433-8 to 8433-14 180 2700 180 2700 76" - 70" (-8 to -14) 67 lbs. Aluminum alloy 8433-0 to 8433S-6 180 2600 180 2600 84" - 78" (-0 to -6) 67 lbs. Aluminum alloy 8433S-8 to 8433S-14 180 2700 180 2700 76" - 70" (-8 to -14) 67 lbs. Aluminum alloy 8833-0 to 8833-10 180 2600 180 2600 88" - 78" (-0 to -10) 68 lbs. Aluminum alloy 9333C-0 to 9333C-5 180 2330 180 2330 93" - 88" (-0 to -5) 72 lbs. Aluminum alloy 10133D-0 to 10133D-6 180 2180 180 2180 101" - 95" (-0 to -6) 77 lbs. Aluminum alloy 3 P-878 Blades Eligible Maximum Continuous Takeoff Diameter *Approx. Max. Wt. Complete with Grease, Mounting Bolts, etc. (see Note 2) HP RPM HP RPM Limits (see notes 3 and 7) Blade Construction Hub Model HC-82XS-2 8046-8 150 2700 150 2700 72" - 66" 58 lbs. Special fabric case plastic; stainless steel or brass tipping. *Weights apply to HC-82XF, K, G, L -2 hub models. Subtract 4 lbs. for -1 hub, 2 lbs. for -3 hubs, and 9 lbs. for -6 hubs. For HC-82X20: Subtract 5 lbs. for -1 hubs, 1 lb. for -2 hubs. Add 2 lbs. for -3 hubs, and 4 lbs. for -5 hubs. Certification basis CAR 14 effective March 5, 1952, as amended by 14-1 and 14-2 Type Certificate No. 878 issued October 8, 1952. Date of application for Type Certificate April 14, 1952. Production basis Production Certificate No. 10 NOTE 1. Hub Model Designation Hub model designation HC - 8 2 X 20 - 2 A Denotes minor change not affecting eligibility L denotes left-hand rotation Denotes specific design features (see Note 4) F denotes special flange, 4" B.C. G denotes SAE No. 2 flange with 3/8" bolts 20 denotes SAE No. 20 spline L denotes SAE No. 2 flange with 7/16" bolts K denotes SAE No. 2 flange with 1/2" bolts and 3/4" bushings Hartzell blade shank size Number of blades Identifies basic design Hartzell controllable NOTE 2. Blade model designation Blade model designation L 93 33 C - 3 Number of inches cut off from basic diameter B denotes deicing boots C denotes dimensional modification from original design D denotes dimensional modification from original design H denotes hard alloy (see Note 6) S denotes square tip Basic model or template Basic diameter in inches Denotes left-hand blade P-878 4 NOTE 3. Pitch Control. Eligible with the following governors: Hartzell Models B-(x)-(x); D-(x)-(x); F-(x)-(x) Weight 4.5 lbs. Hoof Model 1-000-007 series Weight 3.5 lbs. Woodward Model x210xxx or x210x-xxx Hamilton Standard Models 1A4, 1M12, 1P12 and 1Q12 Weight 4.5 lbs. 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. On all models except the -6, oil pressure is used to change the pitch of the blades from high to low pitch. The action is reversed in the -6 model, which has no blade counterweights. NOTE 4. (a) Feathering. The -2 models incorporate feathering and unfeathering features. The -1, -3, and -6 models do not feather. (b) Reversing. The -5 model incorporates reversing but not feathering. NOTE 5. Left-Hand Models. The left-hand version of an approved model propeller is eligible at the same rating and diameter as listed for the right-hand model. See Notes 1 and 2. NOTE 6. Interchangeability. (a) Blades. (1) Hard alloy blades eligible only on seaplanes and amphibious aircraft. (2) 8433A blades are interchangeable with 8433 blades providing all blades in the same propeller are identical. (b) Propellers. Only propellers listed on this data sheet may be replaced by corresponding propellers listed in TC Data Sheet P23GL and P24GL and Type Certificate Data Sheet P-908, provided model designations are the same except that the identifying base design digit "8" (see Note 1) may be replaced by the letter "A" and/or "X" replaced by "V". NOTE 7. Accessories. (a) Propeller Anti-icing (1) Eligible with fluid feed shoes or Icex boots installed in accordance with Hartzell Special Instructions No. 59. (2) Eligible with Hartzell fluid feed equipment on propeller models for which the equipment is available. (3) Eligible with Cessna 0850305 slinger ring installed only on Cessna spinner (see item (b)(2) below). (b) Propeller Deicing (1) Eligible with Goodrich Electrical Propeller Deicer when installed according to instruction given in Goodrich Report 59-728. (2) Eligible with Goodyear Electrical Propeller Deicer when installed according to instruction given in Goodyear Report No. 147 dated October 23, 1961. (c) Propeller Spinner (1) Eligible with Hartzell spinners (weight of spinner extra). (2) Eligible with Cessna spinner dome 0752006 and bulkhead 0850300. NOTE 8. Not applicable. 5 P-878 NOTE 9. 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. Blade Model Engine Model Max. Dia. (Inches) Min. Dia. (Inches) Placards 7636C Lycoming O-290-D2A 74 72 Never exceed 2750 rpm Lycoming O-320 76 72 None 7636D Lycoming O-290-D2A 76 72 None Lycoming O-320 76 70 None Lycoming O-320-B1A 72 70 None Lycoming O-340 76 72 None 8433 Continental O-470-A 84 82 None Continental O-470-B 84 80 None Continental O-470-H 84 81 None Continental O-470-J 84 82 None Continental O-470-K 84 78 None Continental O-470-L 84 78 None Continental O-470-M 84 80 None Continental IO-470-C 84 80 None Continental IO-470-D 80 78 None Lycoming O-320 72 70 None Lycoming O-340 72 70 None Lycoming O-340-A1A 72 70 None Lycoming O-540-A1A 77 76 Avoid continuous operation beteen 2225 and 2275 rpm Lycoming O-540-A1A 82 80 None Lycoming O-540-A1A5, -A1B5 77 73 None Lycoming O-540-A2B 82 80 None Lycoming O-540-B1A5 77 73 None Lycoming O-540-B1B5 77 73 None 8833 Continental O-470-A 88 86 None Continental O-470-E 88 86 None Coontinental O-470-J 88 86 None Continental O-470-K 88 86 None Continental O-470-L 88 86 None Lycoming O-640-A1A5 88 86 Avoid cont. eng. operation between 1950 and 2200 rpm 9333C Lycoming GO-435-C2B, -C2B1 93 91 Avoid cont. eng. operation between 1675 and 2160 rpm, between 2900 and 3200 rpm Lycoming GO-435-C2B, -C2B1 90 88 None Lycoming GO-435-D1 91 89 Avoid cont. eng. operation between 1675 and 2160 rpm, between 2900 and 3200 rpm Lycoming GO-435-D1 90 88 None Lycoming GO-480-B1A 90 88 None Lycoming GO-480-A1A 90 88 None Lycoming GO-430-B, -B1C 90 88 None Continental GO-300-A 90 90 None 10133D Lycoming GO-435-C2B, -C2B1 101 95 Avoid cont. eng. operation between 2600 and 2975 rpm Lycoming GO-480-B1A6 98 92 None Lycoming GO-435-C2B2-6 101 95 None Lycoming GO-435-C2B-6 101 85 None P-878 6 Note 10. Special Note. The word "eligible" as used herein does not signify approval as part of this type certificate. "Eligible" accessories and governors must be approved as part of the aircraft type certificate upon compliance with the applicable aircraft airworthiness requirements. ....END....