TCDS P-880

Page No. 1 2 3 4 Rev. No. 30 30 30 30 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P-880 Revision 30 McCAULEY 2A36 B2A36 C2A36 D2A36 July 15, 1985 TYPE CERTIFICATE DATA SHEET NO. P-880 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. 880) 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 Accessory Division Cessna Aircraft Company Vandalia, Ohio 45377 Type Constant speed; hydraulic (see NOTE 3) Engine shaft Special flange 4 in. B.C. Hub material Aluminum alloy Number of blades Two Hubs eligible 2A36C1, 2A36C18, 2A36C23, 2A36C29, 2A36C43, 2A36C82, B2A36C31, C2A36C32, D2A36C31, D2A36C33, D2A36C45 Blades Eligible Maximum Continuous Takeoff Diameter Limits Approx. Maximum Weight Complete (See Note 2) HP RPM HP RPM (See Note 2) (For Reference Only) Hub Models 2A36C1, 2A36C18, 2A36C29, B2A36C31, C2A36C32, D2A36C31, D2A36C33, D2A36C45 90M-0 to 265 2650 265 2650 90" - 70" 60, 62 lb. * 90M-18 (-0 to -18) Hub Models 2A36C23, 2A36C82 84B-0 to 285 2700 285 2700 84" - 78" 62 lb. 84B-6 (-0 to -6) Hub Model 2A36C43 100R-6 to 310 2400 310 2400 94" - 84" 69 lb. 100R-16 (-6 to -16) * Higher weight applies to hub models 2A36C1, 2A36C18. P-880 2 Certification basis Models 2A36C1/90M, 2A36C18/90M, 2A36C29/90M, B2A36C31/90M, C2A36C32/90M, D2A36C31/90M, D2A36C33/90M: Civil Air Regulations Part 14 effective March 5, 1952. Models 2A36C23/84B and D2A36C45/90M: Civil Air Regulations Part 14 effective December 15, 1956. Model 2A36C43/100R: Civil Air Regulations Part 14 effective December 15, 1956 with Amendment 14-1 thereto. Model 2A36C82/84B: Federal Aviation Regulations Part 35 with Amendments 35-1 thereto. Type Certificate No. 880 issued June 10, 1953. The following models were approved under Delegation Option Authorization procedures of Regulations of the Administrator Part 410 on the date shown: D2A35C45/90M April 12, 1961 2A36C23/84B June 18, 1963 2A36C43/100R February 17, 1964 Model 2A36C82/84B was approved August 2, 1965 under Delegation Option Authorization procedures of Federal Aviation Regulations Part 21, Subpart J. Date of Application for Type Certificate April 4, 1953. Production basis Production Certificate No. 3 NOTE 1. Hub Model Designation Basic Model Designation B 2 A 36 C 1 - A Minor change not affecting interchangeability or eligibility Any change affecting eligibility C denotes constant speed model. McCauley blade shank size Special Flange 4" B.C. Number of blades Indicates dowel location with respect to centerline through blade sockets, viewing hub from flange mounting face. Blank - 60° and 240° clockwise B - 0° and 180° clockwiseB - 0° and 180° clockwise C - 120° and 300° clockwiseC - 120° and 300° clockwise D - 90° and 270° clockwise NOTE 2. Blade Model Designation Basic Model Designation 90 M - 0 Reduction in inches from basic design diameter (as -4, diameter reduced 4 inches to 86 inches.) Blade form characteristics, i.e. activity factor, planform, pitch distribution, etc. Basic design diameter in inches. 3 P-880 NOTE 3. Pitch Control. Eligible with the following governor: Woodward Model x,210.xxx Wt. 3.5 lb. Hoof Model 1,000,007 Series Wt. 3.5 lb. Hoof Model 1,604, 014 Wt. 3.5 lb. Garwin Model 34-828 Wt. 3.0 lb. McCauley C290D1/T[X] Wt. 2.8 lb. McCauley C290D2/T[X] Wt. 2.8 lb. Flottorp 1F1 Wt. 3.0 lb. Garwin 34-825 Wt. 3.0 lb. McCauley C290D3/T[X] Wt. 2.8 lb. McCauley C290D4/T[X] Wt. 2.8 lb. NOTE 4. Not applicable. 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) Spinners (1) Eligible with McCauley spinners; D-2838 Dome, D2839 Bulkhead, and D-2845 Installation for 2A36, B2A36, C2A36 Models except 2A36C23; D-2838 Dome, D-2772 Bulkhead, and D-2771 installation for D2A36 Model. (2) Model 2A36C23 eligible with McCauley spinners; D-2820 Shell, D-3291 bulkhead, and D-3290 installation; D-3239 Shell, D-3241 Bulkhead and D-2822 installation; or D-3395 Shell, D-3393 Bulkhead, and D-3396 installation. (3) Model 2A36C82 eligible with McCauley spinner D-3395 Shell, D-3393 Bulkhead, and D-3396 installation. (b) Propeller De-Icing. (1) Model 84B blades are eligible with Goodyear 4065-3542 ice guards when installed with the general requirements of Goodyear Manual AP-147. 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 Blade Crankshaft Damper Max. Dia. Min. Dia. Model Model Engine Model Configuration (Inches) (Inches) Placards *2A36C 84B Continental O-470 & IO-470 ser. (Up to 240 hp. and 2600 r.p.m.) One 6-1/2 & One 9th Order 84 80 None Continental O-, IO-, and TSIO- 470 series (Up to 240 hp. and 2600 r.p.m.) Four 6th Order 84 78 None *2A36C 84B Continental O-, IO-, and TSIO- 470 series (Up to 260 hp. and 2625 r.p.m.) Four 6th Order 84 78 None P-880 4 Hub Blade Crankshaft Damper Max. Dia. Min. Dia. Model Model Engine Model Configuration (Inches) (Inches) Placards Continental O-, IO-, and TSIO- 470 series (Up to 230 hp. and 2650 r.p.m.) One 5th and One 6th or Two 6th Order 84 80 None Continental O-, IO-, and TSIO- 470 series (Up to 240 hp. and 2600 r.p.m.) Two 6-1/2 Order 84 80 None Continental IO-520 series (Up to 285 hp. and 2700 r.p.m.) One 4th, One 5th and Two 6th Order 84 80 None Continental TSIO-520 series (Up to 285 hp. and 2700 r.p.m.) One 4th, One 5th and Two 6th Order 82 80 None 2A36C23 84B Continental IO-520 series (Up to 285 hp. and 2700 r.p.m.) Three 6th and One 4th Order 84 80 None *2A36C 90M Continental O-, IO-, and TSIO- 470 series (Up to 230 hp. and 2600 r.p.m.) Four 6th Order 90 72 None Continental O-, IO-, and TSIO- 470 series (Up to 260 hp. and 2625 r.p.m.) Four 6th Order 90 78 None Continental O-, IO-, and TSIO- 470 series (Up to 240 hp. and 2600 r.p.m.) Four 6th Order 90 78 None Continental O-, IO-, and TSIO- 470 series One 5th and One 6th or 88 80 None (Up to 230 hp. and 2650 r.p.m.) Two 6th Order 90 80 None Continental O-, IO-, and TSIO- 470 series (Up to 240 hp. and 2600 r.p.m.) Two 6-1/2 Order 88 80 None Continental O-, IO-, and TSIO- 470 series (Up to 265 hp. and 2600 r.p.m.) Two 6th Order 90 88 None *2A36C 100R Continental GIO-470 series (Up to 310 hp. and 3200 r.p.m.) Six 3rd Order 90 88 None * Eligible virbrationwise when asterisk is replaced by blank or letter B, C, or D. 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.....