TCDS P5EA

Page No. 1 2 3 4 5 Rev. No. 17 16 16 16 16 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P5EA April 17, 2006 Revision 17 McCauley D2AF34C 2AF34C 2AF31C TYPE CERTIFICATE DATA SHEET NO. P5EA Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P5EA) 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 McCauley Propeller Systems 7751 East Pawnee Wichita, KS 67207 Type Constant speed; hydraulic (see NOTES 3 and 4) Engine shaft Special flange 4 in. B.C. Hub material Aluminum alloy Blade material Aluminum alloy No. of blades Two Hubs eligible 2AF31C10 D2AF34C59 D2AF34C303 2AF34C55 D2AF34C60 D2AF34C304 D2AF34C30 D2AF34C61 D2AF34C305 D2AF34C41 D2AF34C65 D2AF34C306 D2AF34C42 D2AF34C71 D2AF34C307 D2AF34C46 D2AF34C81 D2AF34C308 D2AF34C52 D2AF34C91 D2AF34C310 D2AF34C54 D2AF34C301 D2AF34C56 D2AF34C302 Maximum Continuous Takeoff Diameter Limits Approx. Max. Wt. Complete (For Reference Only) Blades HP RPM HP RPM (See Note 2) (See NOTE 3) Hub Models D2AF34C46, D2AF34C59, D2AF34C60, D2AF34C42, D2AF34C91 76C-0 to 225 2800 225 2800 76" - 70" 54 lb., 56.5 lb.*, 59.0 lb.**** 76C-6 (-0 to -6) Hub Models D2AF34C56, D2AF34C61, D2AF34C41 L76C-0 to 225 2800 225 2800 76" - 70" 58 lb. L76C-6 (-0 to -6) Hub Models D2AF34C301, D2AF34C304 76CTA-0 to 225 2800 225 2800 76" - 70" 55.5 lb., 58.5 lb.*** 76CTA-6 (-0 to -6) P5EA 2 Maximum Continuous Takeoff Diameter Limits Approx. Max. Wt. Complete (For Reference Only) Blades HP RPM HP RPM (See Note 2) (See NOTE 3) Hub Model D2AF34C302 L76CTA-0 to 225 2800 225 2800 76" - 70" 60.5 lb. L76CTA-6 (-0 to -6) Hub Models D2AF34C305, D2AF34C307 L78CBA-0 to 225 2800 225 2800 78" - 70" 62.0 lb. L78CBA-8 (-0 to -8) Hub Models D2AF34C303, D2AF34C306 78CAA-0 to 225 2800 225 2800 78" - 70" 56.5 lb. 78CAA-8 (-0 to -8) Hub Models 2AF34C55, D2AF34C30 78FF-0 to 285 2700 285 2700 78" - 72" 57.5 lb. 78FF-6 (-0 to -6) Hub Model D2AF34C52 80GF-0 to 265 2700 265 2700 80" - 72" 60 lb. 80GF-8 (-0 to -8) Hub Model D2AF34C54 84HF-0 to 265 2700 265 2700 84" - 72" 59 lb. 84HF-12 (-0 to -12) Hub Models D2AF34C65, D2AF34C71, D2AF34C81 84JF-0 to 285 2700 285 2700 84" - 72" 62.5 lb., 58 lb.** 84JF-12 (-0 to -12) Hub Model 2AF31C10 84SF-4 to 220 2800 220 2800 80" - 72" 53 lb. 84SF-12 (-4 to -12) Hub Models D2AF34C308, D2AF34C310 90DEA-12 to 225 2800 225 2800 78" - 70" 60.5 lb. 90DEA-20 (-12 to -20) * D2AF34C59/76C and D2AF34C42/76C models weigh 56.5 lb. ** D2AF34C65/84JF and D2AF34C81/84JF models weigh 62.5 lb. and D2AF34C71/84JF weighs 58 lbs. *** D2AF34C301/76CTA weighs 55.5 lb. **** D2AF34C91/76C weighs 59.0 lb. 3 P5EA Certification basis Models D2AF34C46/76C, D2AF34C56/L76C, D2AF34C55/78FF and D2AF34C52/80GF: Civil Air Regulations Part 14 effective December 15, 1956. Models D2AF34C60/76C, D2AF34C61/L76C, D2AF34C54/84HF, D2AF34C59/76C, D2AF34C65/84JF, D2AF34C71/84JF: Civil Air Regulations Part 14 effective December 15, 1956 with Amendment 14-1 thereto. Models D2AF34C81/84JF and 2AF31C10/84SF: Federal Aviation Regulations Part 35 with Amendment 35-1 thereto. All other models: Federal Aviation Regulations Part 35 with Amendments 35-1 and 35-2 thereto. Type Certificate No. P5EA issued July 3, 1962 under Delegation Option Authorization of Part 410 of the Regulations of the Administrator. Date of Application for Type Certificate May 11, 1962. Production basis Production Certificate No. 3 NOTE 1. Hub Model Designation Basic Model Designation D 2 A F 34 C 46 - A Minor change not affecting interchangeability or eligibility Change affecting eligibility. C denotes constant speed. McCauley blade shank size F denotes feathering model. Special flange 4" B.C. Number of blades Indicates dowel location with respect to centerline through blade sockets, viewing hub from flange mounting face. D-90° and 270° clockwise. Blank - 60° and 290° clockwise. NOTE 2. Blade Model Designation Basic model designation S L 76 C - 0 Reduction in inches from basic diameter (as -4, diameter reduced 4 inches to 72 inches.) Blade form characteristics, i.e. activity factor, planform, pitch distribution, etc. On CT[X], CB[X], CA[X] and DE[X] series blades, the suffix letter after "CT", "CB", "CA", and "DE" indicates the blade butt staking dimensions for the actuating pin. Basic design diameter in inches. Indicates left hand blade. Indicates minor change not affecting eligibility or interchangeability. P5EA 4 NOTE 3. Pitch Control. Eligible with the following governors: Woodward Model x,210,xxx Wt. 3.5 lb. McCauley Models DCF290D1/T[X], DCF290D2/T[X], Wt. 3.0 lb. DCFS290D1/T[X], DCF290D2/T[X], DCFU290D1/T[X], DCFU290D2/T[X], DCFUS290D1/T[X], DCFUS290D2/T[X] McCauley Models CF310D1T/[X], CF310D2/T[X], CFU310D1/T[X] Wt. 3.0 lb. CFU310D2/T[X], CFS310D1/T[X], CFS310D2/T[X], CFS310D3/T[X], CFUS310D1/T[X], CFUS310D2/T[X], CFUS310D3/T[X] McCauley Models DCFS310D3/T[X], DCFS310D4/T[X] Wt. 4.0 lb. DCFUS310D3/T[X], DCFUS310D4/T[X] NOTE 4. Feathering. Eligible with full feathering control installed in accordance with the propeller manufacturer's instructions. NOTE 5. Left-Hand Models. The left-hand version of an approved model is eligible at the same rating and diameter limitations as listed for the right-hand model. NOTE 6. Not applicable. NOTE 7. Accessories. (a) Propeller Anti-Icing or Deicing (1) Model 78FF blades eligible with Goodrich 37572 fluid feed shoes 10 inches maximum length, when applied in accordance with McCauley or Beech (Beech Specification BS-388) instruction. (2) Model 78FF blades eligible with Goodyear 4065-2611 iceguards installed per Goodyear Manual AP-147. (3) Model 76C, L76C, 76CTA, L76CTA, 78FF, 80GF, 84HF, 84JF, and 84SF blades eligible with Goodrich 4E1188-3 deicer installed in accordance with Goodrich Report No. 59-728. (b) Spinners (1) Model 2AF34C55/78FF eligible with McCauley plain or anti-icing spinners; reference D-2747 Dome, D-2870 Bulkhead and D-2749 or PD-2749 Installation; D-2793 Dome, D-2801 Bulkhead, and D-2802 or PD-2802 Installation; D-2747 or D-3419 Dome, D-3403 Bulkhead, and D-3404 or PD-3404 Installation; D-3419 Dome, D-2870 Bulkhead, and D-3420 or PD-3420 Installation; D-3461 Dome, D-2801 Bulkhead, and D-3462 or PS-3462 Installation; or D-2793 Dome, D-3830 Bulkhead, and D-3831 Installation. (2) Model 2AF31C10/84SF eligible with McCauley spinner; Reference D-3419 Dome, D-2870 Bulkhead, and D-3420 Installation. (3) Model D2AF34C30/78FF eligible with McCauley plain or anti-icing spinners; Reference D-3419 Dome, D-3956 Bulkhead and D-3953 or PD-3953 Installation, or D-3461 Dome, D-4804 Bulkhead and D-4046 or PD-4046 Installation. 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 diameter reduction allowable for repair purposes. 5 P5EA Hub Blade Engine Damper Max. Dia. Min. Dia. Model Model Engine Model Configuration (Inches) (Inches) Placards D2AF34C42 76C Continental IO-360 Series Two 6th order 76 74 None D2AF34C46 (up to 210 hp. @2800 r.p.m.) or one 4.5 and D2AF34C59 one 6th order D2AF34C60 or D2AF34C91 D2AF34C42 76C Continental TSIO-360 Series Two 6th order 76 72 None D2AF34C46 (up to 210 hp. @2800 r.p.m.) or one 4.5 and D2AF34C59 one 6th order D2AF34C60 or D2AF34C91 D2AF34C301 76CTA Continental IO-360 and Two 6th order 76 75 None or D2AF34C304 TSIO-360 Series (up to or one 4.5 and 210 hp. @ 2800 r.p.m.) one 6th order D2AF34C303 78CAA Continental TSIO-360 Series One 6th and one 76 72 None or D2AF34C306 (up to 210 hp. @2800 r.p.m.) 4.5 order D2AF34C303 78CAA Continental IO-360 Series Two 6th order 78 72 None or D2AF34C306 (up to 210 hp. @2800 r.p.m.) or one 4.5 and one 5th order 2AF34C55 78FF Continental IO-470 Series Two 5th and 78 76 None (up to 260 hp. @2625 r.p.m.) one 6th order D2AF34C52 80GF Continental IO-470 Series Four 6th order or 80 78 None (up to 260 hp. @2625 r.p.m.) two 6th, one 5th and one 4.5 order D2AF34C54 84HF Continental TSIO-470 Series Two 6th, one 5th 82 78 None (up to 260 hp. @2600 r.p.m.) and one 4th order 2AF34C55 78FF Continental IO-520 Series Two 6th, one 5th 78 76 None or D2AF34C30 (up to 285 hp. @2700 r.p.m.) and one 4th order D2AF34C65 84JF Continental IO-470 Series Two 6th, one 5th 84 78 None D2AF34C71 (up to 260 hp. @2625 r.p.m.) and one 4.5 order or D2AF34C81 D2AF34C65 84JF Continental TSIO-520 Series Two 6th, one 5th 81 79 None D2AF34C71 (up to 285 hp. @2700 r.p.m.) and one 4th order or D2AF34C81 2AF31C10 84SF Franklin 6A-350 Series (up Viscous Damper 80 74 None to 220 hp. @2800 r.p.m.) D2AF34C308 90DEA Continental IO-360 Series One 4.5 and one 78 75 None or D2AF34C310 (up to 210 hp. @2800 r.p.m.) 6th order D2AF34C308 90DEA Continental TSIO-360 Series One 4.5 and one 78 75 None or D2AF34C310 (up to 225 hp. @2800 r.p.m.) 6th order 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.....