TCDS P11EA

Page No. 1 2 Rev. No. 11 11 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P11EA Revision 3 McCauley 2E34C July 23, 1984 TYPE CERTIFICATE DATA SHEET NO. P11EA Propellers of models described herein conforming with this data sheet (which is part of type certificate no. P11EA) and other approved data on file with the Federal Aviation Administration meet the minimum standards for use in the 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 SAE No. 2 flange modified (six 7/16 in. mounting bolts) Hub material Aluminum alloy Blade material Aluminum alloy Number of blades 2 Hub models eligible 2E34C57 Blades Eligible Max. Continuous Takeoff Diameter Limits Approx. maximum weight complete (for reference only) (See Note 2) HP RPM HP RPM (see Note 2) (See Note 3) 74E-0 to 74E-4 160 2700 160 2700 74" - 70" (-0 to -4) 48 lbs. Certification basis Civil Air Regulations Part 14 effective December 15, 1956. Type Certificate No. P11EA issued February 22, 1963, under Delegation Option Authorization of Part 410 of the Regulations of the Administrator. Date of application for Type Certificate February 22, 1963. Production basis Production Certificate No. 3 NOTE 1. Hub Model Designation Basic model designation 2 E 34 C 53 - A Minor change not affecting interchangeability or eligibility Any change affecting eligibility C denotes Constant Speed McCauley blade shank size E - SAE No. 2 flange modified (6-7/16 in. mounting bolts) Number of blades P11EA 2 NOTE 2. Blade Model Designation Basic model designation 74 E - 0 Reduction in inches from basic design diameter (as -4, diameter reduced 4 inches to 70 inches) Blade form characteristics, i.e. activity factor, planform, pitch distribution, etc. Basic design diameter in inches NOTE 3. Pitch controls. Eligible with the following governors: Woodward Model x, 210, xxx Wt. 3.5 lb. Hoof Model 1,000,007 series Wt. 3.5 lb. McCauley Model C290D1/T(X) Wt. 2.8 lb. McCauley Model C290D2/T(X) Wt. 2.8 lb. McCauley Model C290D3/T(X) Wt. 2.8 lb. McCauley Model 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-2808 Dome, D-3148 Bulkhead and Fillet Assembly, and D-2809 installation. NOTE 8. Not applicable. 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. Hub Model Blade Model Engine Model Max. Dia. (Inches) (Min. Dia. (Inches) Placards 2E34C57 74E Lycoming O-320 series, (up to 160 hp @ 2700 rpm) 74 72.5 None NOTE 10. The word "eligible" as used herein does not signify approval. For approval, compliance with the applicable aircraft airworthiness requirements is required. ....END.....