TCDS P-874

Page No. 1 2 3 4 Rev. No. 20 20 17 19 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P-874 Revision 20 McCauley 1A200 1B200 1C200 1D200 April 21, 2011 TYPE CERTIFICATE DATA SHEET NO. P-874 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. 874) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance with the 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, Kansas 67207 Type Fixed pitch metal Material Aluminum Alloy No. of Blades Two Model Standard No. Dia. Bolt Dia. Pilot Hub Dim. Wt. (lb.) (See Note 2) HP RPM Dia. Pitch Holes Holes Circle Hole Dia. Thick. (Max. Dia.) 1A200/FM 225 2650 90"-78" 100"-40" 8 29/64" 6" 2-1/4" 7" 3-9/16" 43 1B200/HM 225 2650 90"-78" 100"-40" 8 29/64" 6" 3-1/2" 7" 3-9/16" 43 1C200/FC 225 2650 90"-78" 100"-40" 6 1/2" 4" 2-1/4" 7" 3-9/16" 43 1A200/FA 300 2700 90"-78" 100"-40" 6 33/64" 4.75" 2-1/4" 6" 3-9/16" 42 1A200/FAM 180 2700 84"-78" 100"-40" 6 25/64" 4.75" 2-1/4" 6" 3-9/16" 42 1D200/OM 185 2500 90"-84" 64"-34" 6 33/64" 4" 2-1/4" 5-1/4" 3-7/16" 35 1A200/DFA 300 2700 90"-78" 100"-40" 6 33/64" 4.75" 2-1/4" 6" 4-13/16" 45* 1A200/AOM 230 2600 90"-78" 100"-40" 6 33/64" 4" 2-1/4" 5-1/4" 3-7/16" 40 1A200/HFA 290 2700 90"-78" 100"-40" 6 33/64" 4.75" 2-1/4" 6" 5-9/16" 46* 1A200/WFA 290 2700 90"-74" 100"-40" 6 33/64" 4.75" 2-1/4" 6" 3-9/16" 48* * Weight includes integral doweled spacer Takeoff Hub Drilling Hub Dimensions Max. Cont. Certification Basis: Propeller Certification Basis Method of Approval Application Date Approval Date 1A200/FM CAR Part 14 eff Nov 1, 1949 Amdt 14-1 July 27, 1950 September 8, 1950 1B200/HM CAR Part 14 eff Nov 1, 1949 Amdt 14-1 July 27, 1950 September 8, 1950 P-874 2 Rev. 20 1C200/FC CAR Part 14 eff Nov 1, 1949 Amdt 14-1 September 23, 1953 September 23, 1953 Propeller Certification Basis Method of Approval Application Date Approval Date 1A200/FA CAR Part 14 eff Nov 1, 1949 Amdt 14-1 DOA Part 410 of the Regs of the Admin May 16, 1962 May 16, 1962 1A200/FAM CAR Part 14 eff Nov 1, 1949 Amdt 14-1 February 10, 1961 February 10, 1961 1D200/OM CAR Part 14 eff Nov 1, 1949 Amdt 14-1 July 9, 1959 July 9, 1959 1A200/DFA CAR Part 14 eff Dec 15, 1956 Amdt 14-1 DOA Part 410 of the Regs of the Admin July 16, 1964 July 16, 1964 1A200/AOM 14 CFR Part 35, Amdt 35-1 (February 1, 1965) DOA under 14 CFR Part 21, Subpart J November 2, 1965 November 2, 1965 1A200/HFA 14 CFR Part 35, Amdt 35-1 to 35-2 (April 3, 1967) DOA under 14 CFR Part 21, Subpart J April 1, 1974 April 1, 1974 1A200/WFA 14 CFR Part 35, Amdt 35-1 to 35-6 (August 18, 1990) DOA under 14 CFR Part 21, Subpart J April 27, 1998 April 27, 1998 Date of Application for Type Certificate July 27, 1950 Production Basis: Production Certificate No. 3 NOTE 1. Installation . Propeller model 1A200/FM is for use on SAE #4 flanged propeller shaft and must be installed in accordance with McCauley C-1175. Propeller model 1B200/HM is eligible with McCauley hub P/N C-1225 on SAE #20 splined propeller shaft. When hub C-1225 is used, propeller is to be installed in accordance with McCauley Drawing C-1174. Propeller model 1C200/FC is for use on the special Continental Motors Corp. propeller flange and must be installed in accordance with McCauley Drawing C-1530. Propeller model 1A200/FA is for use on SAE #2 modified flange and must be installed in accordance with McCauley Drawing C-2337. Propeller model 1A200/FAM is for use on SAE #2 modified flange and must be installed in accordance with McCauley Drawing C-2720. Propeller models 1A200/AOM and 1D200/OM are for use on the special Continental Motors Corp. propeller flange and must be installed in accordance with McCauley Drawing C-2359. Propeller model 1A200/DFA is for use on SAE #2 modified flange with McCauley P/N B-3434 spacer and must be installed in accordance with McCauley Drawing C-3433. Propeller model 1A200/HFA is for use on SAE #2 modified flange with McCauley P/N B-4585 spacer and must be installed in accordance with McCauley Drawing C-4586. Propeller model 1A200/WFA is for use on SAE #2 modified flange with McCauley P/N B-3637 spacer and must be installed in accordance with McCauley Drawing C-7565. P-874 3 Rev. 20 NOTE 2. Propeller Model Designation . Basic Model Designation Suffix 1A200/ FM 90 47 Inches pitch at .75 radius Propeller diameter in inches FM Denotes SAE No. 4 Flange FC Denotes Special Flange 4" B.C. HM Denotes Special Flange 6" B.C. FA Denotes SAE No. 2 Flange Modified (6-1/2" bolts) DFA Denotes SAE No . 2 Flange Modified (6-1/2" bolts) and B-3434 spacer FAM Denotes SAE No. 2 Flange Modified (6-3/8" bolts) OM Denotes Special Flange 4" B.C.; square tips AOM Denotes Special Flange 4" B.C.; square tips HFA Denotes SAE No. 2 Flange Modified (6-1/2" bolts) and B-4585 spacer WFA Denotes SAE No. 2 Flange Modified (6-1/2" bolts) and B-3637 spacer Basic Design No. NOTES 3, 4, 5, 6, 7, and 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. Propeller Model Engine Model Max. Dia. (Inches) Min. Dia. (Inches) Placards 1A200/FM Continental O-470-11 90 80 None 1B200/HM Continental E-225 90 86 None 1C200/FC Continental O-470-A 90 86 None 1C200/FC Continental O-470-E 90 86 None 1C200/FC Continental O-470-J 90 86 None 1A200/FM Continental E-185 with SAE No. 4 flange and dampered shaft 90 80 None 1A200/FA or 1A200/DFA Lycoming O-360 series (Up to 180 hp and 2700 rpm) 82 78 None 1A200/HFA Lycoming O-360 series (Up to 180 hp and 2700 rpm) 80 79 “Avoid continuous operation while descending between 1700 to 2100 rpm” P-874 4 Rev. 20 Propeller Model Engine Model Max. Dia. (Inches) Min. Dia. (Inches) Placards 1A200/FA or 1A200/DFA Lycoming O-540 & IO-540 with one 5th order and one 6th order crankshaft damper configuration (Up to 260 hp and 2700 rpm) 90 80 None 1A200/FA or 1A200/DFA Lycoming IO-540 series with one 5th order and one 6th order crankshaft damper configuration (Up to 300 hp and 2575 rpm) 90 86 None 1A200/FAM Lycoming O-320 series (Up to 160 hp and 2700 rpm) 82 78 None 1D200/OM Continental GO-300 series (175 hp and 2400 rpm) 90 86 None 1A200/AOM Continental O-470 series with one 5th order and one 6th order crankshaft damper configuration (Up to 230 hp and 2600 rpm 90 86 None NOTE 10. The word “eligible” as used herein does not signify approval. For approval, compliance with the applicable aircraft airworthiness requirements is necessary. …END…