TCDS P-884

Page No. 1 2 3 4 Rev. No. 14 13 14 13 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P-884 Revision 14 HARTZELL HC-83X March 6, 1981 TYPE CERTIFICATE DATA SHEET NO. P-884 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. 884) 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, Ohio Type Constant speed; hydraulic (see Notes 3 and 4) Engine shaft SAE No. 20 spline, special flange 4" B.C. Hub material Alloy steel Blade material See below Number of blades Three Hubs eligible HC-83XF-1, -2, -3; HC-83XK-1, -2; HC-83XK20-1, -2. (See Notes 1 and 4 and "Blades Eligible.") Blades Eligible Maximum Continuous Takeoff Diameter *Approx. Max. Wt. Complete (for reference only) (see Note 2) HP RPM HP RPM Limits (see notes 3 and 7) Blade Construction Hub Models HC-83XF-1, -2, -3 7636D-0 to 7636D-6 260 2600 260 2600 76" - 70" (-0 to -6) 83 lbs. Aluminum alloy 8428X-0 to 8428X-9 280 2180 280 2180 84" - 75" (-0 to -9) 87 lbs. Special fabric base plastic; stainless steel or brass tipping 8433-0 to 8433-6 240 2600 240 2600 84" - 78" (-0 to -6) 87 lbs. Aluminum alloy 9333C-0 to 9333C-13 320 2060 340 2180 93" - 80" (-0 to -130) 103 lbs. Aluminum alloy Hub Models HC-83XK-1, -2 8433-0 to 8433-6 250 2600 250 2600 84" - 78" (-0 to -6) 87 lbs. Aluminum alloy Hub Models HC-83X20-1, -2 7636D-0 to 7636D-6 280 2180 295 2180 76" - 70" (-0 to -6) 87 lbs. Aluminum alloy 8428X-0 to 8428X-9 280 2180 280 2180 84" - 75" (-0 to -9) 91 lbs. Special fabric base plastic; stainless steel or brass tipping P-884 2 Blades Eligible Maximum Continuous Takeoff Diameter *Approx. Max. Wt. Complete (for reference only) (see Note 2) HP RPM HP RPM Limits (see notes 3 and 7) Blade Construction Hub Models HC-83X20-1, -2 8433-0 to 8833-6 290 2180 280 2180 84" - 78" (-0 to -6) 91 lbs. Aluminum alloy 8433Z-0 to 8433Z-6 280 2180 280 2180 84" - 78" 91 lbs. Aluminum alloy 8833-0 to 8833-10 280 1925 295 2180 88" - 78" (-0 to -10) 93 lbs. Aluminum alloy 9333C-13 to 9333C-13 320 2060 340 2180 93" - 80" (-0 to -13) 98 lbs. Aluminum alloy *Weights apply to -2 hub models. Subtract 4 lbs. for -1 hubs. Certification basis CAR 14 effective March 5, 1952, as amended by 14-1. Type Certificate No. 884 issued May 5, 1954. Date of application for Type Certificate March 25, 1954. Production basis Production Certificate No. 10 NOTE 1. Hub Model Designation Hub model designation HC - 8 3 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. 20 denotes SAE No. 20 spline x 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 3 P-884 NOTE 2. Blade model designation Blade model designation L 76 36 D - 3 Number of inches cut off from basic diameter H denotes hard alloy (see Note 6) Dimensional modification from original design B denotes deicing boots Basic model or template Basic diameter in inches Denotes left-hand blade NOTE 3. Pitch Control. Eligible with the following governors: Hartzell Models B-(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. NOTE 4. (a) Feathering. The -2 models incorporate feathering and unfeathering features. (b) Reversing. The -3 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. Only blades listed in the same group of the following listed groups are sufficiently similar aerodynamically and vibrationwise to permit interchangeability in the same diameter without a flight test provided all blades in the propeller are the same model. Group (1) 9333C, 9333CH* (2) 8433, 8433H*, 8433Z, 8433A *Hard alloy blades interchangeable only on seaplanes and amphibious aircraft. (b) Propellers. Only propellers listed on this data sheet may be replaced by corresponding propellers listed in TC Data Sheet P-913, provided the propeller model designations are the same except that the identifying base design digit "8" (see Note 1) is replaced by the letter "A". 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. (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 ice guards (electrical propeller deicer) when installed according to instruction given in Goodyear Report No. AP-147 dated October 23, 1961. (c) Propeller Spinner (1) Eligible with Hartzell spinners (weight of spinner extra). NOTE 8. Not applicable. P-884 4 NOTE 9. Table of Propeller-Engine Combinations Approved Vibrationwise for Use on 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 8433 Lycoming GO-435 84 84 None Lycoming GO-435-C2B, -C2B1 84 84 None Lycoming GO-480-A1A 84 84 None Lycoming GO-480-D1A 84 84 None Lycoming GO-480-B, -B1B, -B1C, -B1D 84 84 None Lycoming GO-480-B1A6 84 84 "Avoid continuous operations on ground between 1300 and 1650 and between 2100 and 2500 rpm." Lycoming GO-480-C1B6 86 82 "Avoid continuous operation in flight below 2400 rpm." 9333C Lycoming GO-435-C2B 93 87 None Lycoing GO-435-C2B1 90 90 None Lycoming GO-480-C2C6 93 89 None Lycoming GO-480-A1A6 93 88 None Lycoming GO-480-C1D6 93 89 None Lycoming GSO-480-B1A6 93 88 None Lycoming GSO-480-B1B6 93 88 None Lycoming GSO-480-B2D6 93 91 "Avoid continuous operation between 2800 and 3100 rpm." Lycoming GO-480-F2A 90 87 None Lycoming GO-480-F2A6 93 87 None Lycoming GO-480-F4A6 93 87 None Lycoming GO-480-F4B6 93 87 None 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....