TCDS P-913

Page No. 1 2 3 4 Rev. No. 14 14 14 14 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P-913 Revision 14 HARTZELL HC-A3X PHC-A3X May 31, 1984 TYPE CERTIFICATE DATA SHEET NO. P-913 Propellers of models described herein conforming with this data sheet (which is a part of type certificate no. P-913) 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 mauals and other approved instructions. Type Certificate Holder Hartzell Propeller Products Piqua, Ohio 45356 Type Constant speed; hydraulic (see Notes 3 and 4) Engine shaft SAE #2 flange modified, SAE #20 spline Special flange 4" B.C., British S.B.A.C. No. 2 Hub material Alloy steel Blade material Aluminum alloy No. of blades Three Hub models eligible HC-A3XF-2, -4; PHC-A3XF-2; HC-A3XK-2, -4; HC-A3X20-1, -2, -5; HC-A3X21-2 (see Notes 1 and 4.) Blades Eligible Maximum Continuous Takeoff Diameter *Approx. Max. Wt. Complete with grease, mounting bolts, etc. (for reference only) (See NOTE 2) HP RPM HP RPM Limits (See NOTES 3 and 7) 7636D-0 to 7636D-6 336 2800 336 2800 76" - 70" (-0 to -6) 90 lbs. 8433-0 to 8433-10 380 2700 380 2700 84" - 72" (-0 to -12) 94 lbs. 8433-4 to 8433-10 400 2650 400 2650 80" - 74" (-4 to -10) 94 lbs. 8433S-0 to 8433S-12 380 2625 380 2625 84" - 72" (-0 to -12) 94 lbs. 8833-0 to 8833-10 380 2450 380 2450 88" - 78" (-0 to -10) 97 lbs. 9333C-0 to 9333C-13 340 2200 340 2200 93" - 80" (-0 to -13) 100 lbs. *Weights apply to -2 hub models with F or K flange. For SAE No. 20 spline shaft add 3 lbs. For HC-A3X20-5 add 5 lbs. For HC-A3XK-4 subtract 7 lbs. Certification basis CAR 14 effective December 15, 1956. Type Certificate No. P-913 issued February 15, 1960. Date of Application for Type Certificate January 20, 1960. Production basis Production Certificate No. 10. P-914 2 NOTE 1. Hub Model Designation Hub model designation ( ) HC - A 3 X ( ) - ( ) ( ) 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. K denotes SAE No. 2 flange with 1/2" bolts and 3/4" bushings 20 denotes SAE No. 20 spline 21 denotes S.B.A.C. No. 2 spline Hartzell blade shank size Number of blades Identifies basic design Hartzell controllable Blank indicates dowel location with respect to centerline through blade sockets viewing hub from flange mounting face 90° and 270° clockwise P indicates propeller installed with T/C mark on propeller matching T/C mark on engine flange NOTE 2. Blade Model Designation Blade model designation L 84 33 ( ) - ( ) Q Q when used denotes 1° - 90° factory bent tip for cutoff diameter Number of inches cut off from basic diameter A denotes 8433 blades with 1° sweepback in lieu of 2° sweepback If used B denotes deicing boots C denotes modified blade S denotes square tips Basic model or template Basic diameter in inches If used, denotes left hand blade Blade Model 8433-0 incorporates a round tip and blade Model 8433S-0 incorporates a square tip. Blades of reduced length, such as -2, -4, etc., incorporate both round tips and square tips and may or may not be marked with an "S" in the blade model designation, i.e., 8433S-2 incorporates square tips, while 8433-2 may have either round or square tips. NOTE 3. Pitch Control. Eligible with the following governors: Hartzell Models B-(x)-(x), D-(x)-(x) and F-(x)-(x) Wt. 4.5 lb. Hoff Model 1-000-007 Series Wt. 3.5 lb. Woodward Model X210XXX or X210X-XXX Hamilton Standard Models 1A4, 1M12, 1P12 and 1Q12 Wt. 4.5 lb. 3 P-913 The Hartzell B-0 is the only model which is interchangeable with the Hamilton Standard 1M12 and 1Q12. Other Hartzell models are not interchangeble with any Hamilton Standard model without modification of the latter. The HC-A3XK-4 propeller has no counterweights; hence requires a governor to supply oil to increase pitch. The D-(x)-(x) and F-(x)-(x) governors meet this requirement. NOTE 4. (a) Feathering. The -2 model incorporates feathering and unfeathering features. (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) Propellers. Only propellers listed in this data sheet are eligible as replacements for corresponding propellers listed in Type Certificate Data Sheet P-884 in accordance with Note 6 of P-884. Propellers listed in P-884 are not eligible to replace propellers listed in this data sheet. (b) Model 8433A blades are interchangeable with 8433 blades provided all blades in the same propeller are identical. 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 Deicer (1) Eligible with Goodrich deicing kit 77-xxx or 65-xxx when installed according to instruction given in Goodrich Report 59-728. (2) Eligible with Goodyear iceguards (electrical propeller deicer) when installed in accordance with instructions outlined in Goodyear Report No. AP-147 dated October 23, 1961. (c) Propeller Spinner (1) Eligible with Hartzell spinner. (Weight of spinner extra) 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 diamater reduction allowable for repair purposes. Hub Model Blade Model Engine Model Max. Dia. (Inches) Min. Dia. (Inches) Placards HC-A3XF PHC-A3XF 7636D Continental IO-470 series, two 5th order and two 6th order dampers, 8.6:1 compression ratio or less, 260 hp @ 2625 rpm or less. 76¼ 76¼ None HC-A3XK 7636D Lycoming O-540 and IO-540 series, 8.7:1 compression ratio or less, one 6th order and one 5th order damper, 290 hp @ 2575 rpm or less; centerline of one blade in line with #1 crankthrow facing engine from propeller end. 72¼ 70¼ None HC-A3X21 L7636D Bristol Siddeley Gypsy Queen 30 Mk. 2 series, 6.5:1 compression ratio or less, 250 hp @ 2500 rpm or less. 76¼ 75 "Maintain manifold pressure above airspeeds above 140 mph" P-914 4 Hub Model Blade Model Engine Model Max. Dia. (Inches) Min. Dia. (Inches) Placards HC-A3X20 8433 Lycoming GO-435, GO-435-C2B, GO-435-C2B1 84 84 None HC-A3X20 8433 Lycoming GO-480-A1A, -B, -B1B, -B1C, -B1D, -D1A HC-A3X20 8433 Lycoming GO-480-B1A6 84 84 "Avoid continuous operation on ground between 1300 and 1650 and between 2100 and 2500 rpm." HC-A3XK 8433 Lycoming O-540 and IO-540 series, 8.7:1 compression ratio or less, one 6th order and one 5th order damper, 290 hp @ 2775 rpm or less; centerline of one blade in line with #1 crankthrow facing engine from propeller end. 74¼ 72¼ None HC-A3XK 8433 Lycoming IO-540-B1A5 80 77 None HC-A3XK 8433 Lycoming IO-720 series, six 4.0 order, one 3.5 order and one 5.1 order dampers, 8.7:1 compression ratio or less, 4000 hp @ 2650 rpm or less; centerline of one blade must be in line with #1 crankthrow facing engine from propeller end. 77¼ 75¼ "Avoid continuous operation between 1800 and 2000 rpm." PHC-A3XF 8433 Continental IO-470 series, one 5th and one 6th order damper, 7:1 compression ratio or less, 225 hp @ 2600 rpm or less 80.6 78.6 None HC-A3XK PHC-A3XF 8433 Continental IO-470 series, four 6th order dampers, 8.6:1 compression ratio or less, 260 hp @ 2625 rpm or less. 845/8 80 None PHC-A3XF 8433 Continental IO-520 series, two 6th order, one 5th order and one 4th order damper, 8.5:1 compression ratio or less, 285 hp @ 2700 rpm or less. T/C marks must be aligned. 84¼ 84¼ None HC-A3X20 8833 Lycoming GO-480-C1B6 86 82 "Avoid continuous operation in flight below 2400 rpm." HC-A3XF 8833 Continental GIO-470, 8.6:1 compression ratio, .75:1 reduction gear, six heavy 3rd order dampers, 310 hp @ 2300 rpm or less 88¼ 88¼ None HC-A3X20 9333C Lycoming GO-435-C2B 93 87 None HC-A3X20 9333C Lycoming GO-435-C2B1 90 90 None HC-A3X20 9333C Lycoming GO-480, C1D6, -C2C6, -C2D6, -G2D6, -G2F6 93 89 None HC-A3X20 9333C Lycoming GO-480-B1D 90 87 None HC-A3X20 9333C Lycoming GO-480-F2A6 93 87 None HC-A3X20 9333C Lycoming GSO-480-A1A6, GSO-480-B1A6, IGSO-480-A1C6 93 88 None HC-A3X20 9333C Lycoming GSO-480-B2D6 93 91 "Avoid continuous operation between 2800 and 3100 rpm." HC-A3XF 9333C Lycoming GO-480-F4A6, -F4B6 93 87 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.....