TCDS P-917

Page No. 1 2 3 4 Rev. No. 5 4 4 4 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P-917 Revision 5 TRW Hartzell HC-D2X September 15, 1982 TYPE CERTIFICATE DATA SHEET NO. P-917 Propellers of models described herein conforming with this data sheet (which is a part of type certificate No. P-917) 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 TRW Hartzell Propeller 350 Washington Avenue Piqua, Ohio 45356 Type Ground speed; hydraulic (see Notes 3 and 4) Engine shaft SAE #20 spline Hub material Alloy steel Blade material Aluminum alloy Number of blades Two Hub models eligible HC-D2X20-3, -7, -8 (see Notes 1, 4, and 9) Blades Eligible Maximum Continuous Takeoff Approx. Max. Wt. Complete (for reference only) (See Note 2) HP RPM HP RPM Diameter Limits (See Notes 3 and 7) 8833-0 to 8433-9 225 2600 225 2600 84" - 75" (-0 to -9) 69 lbs. 8433Z-0 to 8433Z-6 225 2600 225 2600 84" - 78" (-0 to -6) 69 lbs. 8833-0 to 8833-4 225 260 2600 or 2180 225 260 2600 2180 88" - 84" (-0 to -4) 75 lbs. 9333C-0 to 9333C-5 260 2180 260 2180 93" - 88" (-0 to -5) 79 lbs. 10133D-0 to 10133D-6 260 2180 260 2180 101" - 95" (-0 to -6) 76 lbs. Certification basis Civil Air Regulations Part 14 effective December 15, 1956 Type Certificate No. 917 issued December 14, 1960. Date of application for Type Certificate December 1, 1960. Production basis Production Certificate No. 10. P-917 2 NOTE 1. Hub Model Designation Hub model designation HC - D 2 X 20 - 3 A Denotes minor change not affecting eligibility L denotes left-hand rotation Denotes specific design features (see Note 4) SAE No. 20 spline Hartzell blade shank size Number of blades Identifies basic design Hartzell controllable A -10 following the hub serial number identifies that oversize tubes are pressed into the spider in order to accommodate worn blade bushings. NOTE 2. Blade Model Designation Blade model designation L 93 33 D H - 4 + Number of inches added to basic diameter - Number of inches cut off from basic diameter Used in an aluminum blade model designation denotes hard alloy Dimensional modification from original design "A" when used with 8433 blades denotes 1° sweepback. Otherwise sweepback is 2°. Basic model or template Basic diameter in inches Denotes left-hand blade NOTE 3. Pitch Control. Eligible with Hartzell manual or constant speed control. Constant speed control includes the Hartzell governor Model A-1. Additional weight of governor is 3.75 lb. (Note: Some installations require a T-drive adapter for the governor. Additional weight of the Hartzell Model C-137 adapter is 2.5 lbs, and of the Hartzell Model C-253 adapter is 2.7 lbs.) NOTE 4. (a) Feathering. Not applicable. (b) Reversing. -3 model incorporates hydraulically controlled reversing. 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. 3 P-917 NOTE 6. Interchangeability. (a) Blades. Only blades listed in the same group of the following list are sufficiently similar aerodynamically and vibrationwise to permit interchangeability in the same diameter without a flight test. Group (a) 8433, 8433Z. Hard and soft alloy aluminum blades of the same model designation are interchangeable but only on seaplanes and amphibious aircraft. Model 8433A blades are interchangeable with 8433 blades provided both blades in the same propeller are identical. (b) Propellers. Only propellers listed in this data sheet are eligible as replacements for corresponding propellers listed in Type Certificate Data Sheet No. P-845 in accordance with Note 6 of P-845. Propellers listed in P-845 are not eligible to replace propellers listed in this data sheet. NOTES 7 Accessories. (a) Propeller deicing (1) Eligible with Goodrich "Icex" shoes, when applied in accordance with Goodrich instructions. Hartzell recommends that the maximum length be limited to .7 x blades radius, measured from center of hub. (b) Propellers spinners (1) Eligible with Hartzell Model D-164 bulkhead assembly, D-163 spinner dome. Additional weight 3 lb. The -3 model has no spinner eligible. (2) Eligible with Goodyear ice guards (electrical propeller deicer) when installed in accordance with instructions outlined in Goodyear Report No. AP-147 dated October 23, 1961. NOTE 8. Not applicable. 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. Hub Model Blade Model Engine Model Max. Dia. (Inches) Min. Dia. (Inches) Placards HC-D2X20 8433 Continental E-185 84 76 Dampened engine only, not to exceed 2600 rpm at takeoff. Franklin 6A8-215-8BF and -9BF 84 84 None Continental E-225 84 82 Not to exceed 2600 rpm at takeoff. Lycoming O-435-A and -C 78 75 None Lycoming O-435-A2 78 76 None Lycoming O-435-C1 78 76 None HC-D2X20 8833 Ranger 6-440-C5 88 88 Avoid continuous operation between 1250 and 1600 and between 1950 and 2200 rpm Continental E-225 88 86 Avoid continuous operation on ground between 1400 and 1700 and also between 1900 and 2100 rpm. Avoid continuous operation on ground and flight between 2450 and 2550 rpm P-917 4 Hub Model Blade Model Engine Model Max. Dia. (Inches) Min. Dia. (Inches) Placards HC-D2X20 9333C Lycoming GO-435-C2 93 91 Avoid continuous ground operation between 1675 and 2150 rpm Lycoming GO-435-C2 90 88 None Lycoming O-435-2-M1 93 93 Avoid continuous ground operation between 1675 and 2150 engine rpm. HC-D2X20 10133D Lycoming GO-435-C2 101 101 Avoid continuous operation between 2600 and 2940 rpm Lycoming GO-435-C2 98 95 None NOTE 10. The word "eligible" as used herein does not signify approval as part of this type certificate. "Eligible" accessories must be approved as part of the aircraft type certificate upon compliance with the applicable aircraft airworthiness requirements. .....END....