TCDS P1NM

PAGE 1 2 3 REV. 1 - - DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. P1NM Composite propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P1NM) 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 (TC) HOLDER: Great American Propeller Co. 250 Scottsville Blvd. Jackson, CA 95642 TYPE CERTIFICATE OWNERSHIP RECORD: S&S Propellers Inc. 3681 Sacramento Street San Luis Obispo, CA 93401 Type Fixed Pitch Composite Material Carbon Fiber/Laminated Maple Number of Blades Two Propeller Hub Drilling Hub Dimensions Propeller Weight Engine Manufacturer & TC Takeoff & Maximum Continuance Dia Standard Pitch Mounting Configuration No. of Bolt Holes Dia. of Bolt Holes Bolt Hole Dia. Hub Dia. Hub Thickness Propeller Weight HP RPM (in) (in) (in) (in) (in) (lb) W7448A1-2 Continental (A-40) 40 2575 74 40-56 Taper Shaft 6 0.375 4.375 6 3.5 10.5 W7448A1-2 Continental (A-50) 50 1900 74 40–56 Taper Shaft 6 0.375 4.375 6 3.5 10.5 W7448A1-2 Continental (A-65/O-170) 65 2300 74 40–56 Taper Shaft 6 0.375 4.375 6 3.5 10.5 W7448A1-2 Franklin (4AC-176-B2) 65 2300 74 40–56 SAE-1 Flange 6 0.375 4.375 6 3.5 10.5 W7448A1-2 Lycoming (O-145) 65 2550 74 40–56 SAE-1 Flange 6 0.375 4.375 6 3.5 10.5 W7448A1-2 Continental (A-70) 70 2500 74 40–56 Taper Shaft 6 0.375 4.375 6 3.5 10.5 W7448A1-2 Continental (A-75) 75 2600 74 40–56 Taper Shaft 6 0.375 4.375 6 3.5 10.5 W7448A1-2 Continental (C-75) 75 2275 74 40–56 SAE-1 Flange 6 0.375 4.375 6 3.5 10.5 W7448A1-2 Continental (A-80) 80 2700 74 40–56 Taper Shaft 6 0.375 4.375 6 3.5 10.5 W7448A1-2 Continental (C85) 85 2575 74 40–56 SAE-1 Flange 6 0.375 4.375 6 3.5 10.5 W7448A1-2 Continental (C-90) 90 2550 74 40–56 SAE-1 Flange 6 0.375 4.375 6 3.5 10.5 W7448A1-2 Continental ((A-100) 100 2700 74 40–56 SAE-1 Flange 6 0.375 4.375 6 3.5 10.5 W7448A1-2 Continental (O-200) 100 2750 74 40–56 SAE-1 Flange 6 0.375 4.385 6 3.5 10.5 W7448A1-2 Continental (C-115/125) 125 2550 74 40–56 SAE-2 Flange 6 0.375 4.75 7 4 15.5 W7848A2-2 Continental (C-145/O-300) 145 2700 74 40–56 SAE-2 Flange 6 0.375 4.75 7 4 15.5 W7848A2-2 Franklin (6A4-125-B3) 125 2500 74 40–56 SAE-2 Flange 6 0.375 4.75 7 4 15.5 W7448A1-2 Lycoming (O-235) 118 2600 74 40–56 SAE-1Flange 6 0.375 4.375 6 3.5 10.5 W7848B2-2 Lycoming (O-235) 125 2800 78 40–56 SAE-2 Flange 6 0.375 4.75 7 4 15.5 W7848B2-2 Continental (O-240) 130 2800 78 40–56 SAE-2 Flange 6 0.375 4.75 7 4 15.5 W7848B2-2 Lycoming (O-290) 140 2800 78 40–56 SAE-2 Flange 6 0.4375 4.75 7 4 15.5 W7848B2-2 Lycoming O-290) 140 2800 78 40–56 SAE-2 Flange 6 0.3125 4.75 7 4 15.5 W7848B2-2 Lycoming (O-290) 140 2800 78 40–56 SAE-2 Flange 6 0.500 4.75 7 4 15.5 W7848B2-2 Continental (C-145) 145 2700 78 40–56 SAE-2 Flange 6 0.375 4.75 7 4 15.5 W7848B2-2 Continental (O-300) 145 2700 78 40–56 SAE-2 Flange 6 0.375 4.75 7 4 15.5 W7848B2-2 Lycoming (O-320) 160 2700 78 40–56 SAE-2 Flange 6 0.375 4.75 7 4 15.5 W7848B2-2 Lycoming (O-320) 160 2700 78 40–56 SAE-2 Flange 6 0.4375 4.75 7 4 15.5 W7848B2-2 Lycoming (O-320) 160 2700 78 40–56 SAE-2 Flange 6 0.500 4.75 7 4 15.5 W7848B2-2 Continental (IO-346) 165 2700 78 40–56 SAE-2 Flange 6 0.375 4.75 7 4 15.5 W7848F2-2 Franklin (6A4-150-B3) 150 2600 78 40–56 SAE-3 Flange 8 0.375 5.25 7 4 10.5 W7848F2-2 Franklin (6A4-165-B3) 165 2800 78 40–56 SAE-3 Flange 8 0.375 5.25 7 4 10.5 P1NM Revision 1 Great American Propeller Co. W7400 W7800 March 5, 2019 P-1NM 2 CERTIFICATION BASIS Federal Air Regulations Part 35 including amendment 35-5 dated October 14, 1980, to date of application for Type Certificate dated December 8, 1992. PRODUCTION CERTIFICATE None NOTE 1 Installation These models are for installation on flanged and tapered propeller shafts in accordance with AC 43.131A, Chapter 12, Section 5. (See NOTE 2). Installation of composite propellers on flanged crankshaft must include a front plate of approximately the same area and thickness as the flange and AN bolts conforming to MIL-B-6812. NOTE 2 Model Designation W 74 48 A 1 - 2 Basic Model 2 Leading Edge Type 1 Blade design A Bolt/Hub Configuration 48 Propeller Pitch (inches) 74 Basic Propeller Diameter (inches) W Material: 1/16 Laminated Maple with carbon fiber reinforcement NOTE 3, 4, 5, AND 6 Not applicable. NOTE 7 Spacers S&S crush plates and bolt kits, P/N S&S-SAE-1, S&S-SAE-2, S&S-SAE-3 may be used to comply with (NOTE 1). Taper shaft hubs require S&S Bushing Set P/N A10 or equivalent. NOTE 8 Not applicable. NOTE 9 Special Limits Table of Propeller-Engine Combinations Approved Vibrationwise for use on Normal Category Tractor Aircraft The maximum and minimum propeller diameter 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. Propeller Model Engine Model Maximum Diameter (in) Minimum Diameter (in) Placards W7448A1-2 Continental A – 40 74.5 70 None W7448A1-2 Continental A – 50 74.5 70 None W7448A1-2 Continental A - 65/O-170 74.5 70 None W7448A1-2 Franklin 4AC176-B2 74.5 70 None W7448A1-2 Lycoming O-145 74.5 70 None W7448A1-2 Continental A – 70 74.5 70 None W7448A1-2 Continental A – 75 74.5 70 None W7448A1-2 Continental C – 75 74.5 70 None W7448A1-2 Continental A – 80 74.5 70 None W7448A1-2 Continental C - 85 74.5 70 None W7448A1-2 Continental C - 90 74.5 70 None 3 P-1NM Propeller Model Engine Model Maximum Diameter (in) Minimum Diameter (in) Placards W7448A1-2 Continental A - 100 74.5 70 None W7448A1-2 Continental O - 200 74.5 70 None W7448A1-2 Continental C - 115/125 74.5 70 None W7848B2-2 Continental C-145/O-300 78.5 70 None W7448A1-2 Franklin 4AC-125-B2 74.5 70 None W7448A1-2 Lycoming O-235 74.5 70 None W7848B2-2 Lycoming O-235 74.5 70 None W7848B2-2 Continental O-240 78.5 70 None W7848B2-2 Lycoming O-290 78.5 70 None W7848B2-2 Continental C-145 78.5 70 None W894882-2 Continental O-300 78.5 70 None W7848B2-2 Lycoming O-320 78.5 70 None W7848B2-2 Continental IO-346 78.5 70 None W7848F2-2 Franklin 6A4-150-B2 78.5 70 None W7848F2-2 Franklin 6A4-165-B2 78.5 70 None NOTE 10 Special Notes. The word “eligible” as used herein does not signify approval. For approval compliance with the applicable aircraft airworthiness requirements is necessary. …END…