# TCDS P3EA: McCauley Propeller Systems - Type: Type certificate data sheet - Status: Current - Holder: McCauley Propeller Systems - Revision: 24 - Revised: April 17, 2006 - Product: Propeller - Certification basis: Part 14, Part 35, CAR 14 - Data sheet PDF: https://openairdocs.org/files/sha256/1d/5c/1d5c738f96277dfc37a0ce00d2ba6405d08725cdc0c249df770d0c5dca532647 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DEDEE11D959E941686257168006CF21C.0001 - Page: https://openairdocs.org/tcds/P3EA ## Models (10) As the data sheet lists them. - E2A34C - D2A37C - F2A34C - E2A37C - B2A34C - 2A34C - 2A37C - B2A37C - D2A34C - C2A34C ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P3EA Revision 24 McCAULEY 2A34C 2A37C B2A34C B2A37C C2A34C D2A37C D2A34C E2A37C E2A34C F2A34C April 17, 2006 TYPE CERTIFICATE DATA SHEET NO. P3EA Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P3EA) 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, KS 67207 Type Constant speed; hydraulic Engine Shaft Special flange 4 in. B.C. Hub Material Aluminum Alloy No. of Blades Two Hubs Eligible 2A34C22, D2A34C34, D2A34C49, 2A34C50, D2A34C58, F2A34C58, E2A34C64, 2A34C66, D2A34C67, E2A34C70, E2A34C73, D2A34C78, D2A34C98, 2A34C201, 2A34C203, C2A34C204, B2A34C205, 2A34C209, 2A34C210, 2A34C216, 2A34C221, 2A37C223, B2A34C225, 2A34C227, B2A37C228, D2A37C230, D2A37C231, 2A37C232, E2A37C233, E2A37C234, B2A37C238, 2A34C239, 2A34C240 and 2A34C241 Blades Eligible Maximum Continuous Take-Off Diameter Limits Approx. Max. Wt. Complete (For reference only) (See NOTE 2) HP RPM HP RPM (See NOTE 2) (Max. Dia.) Hub Model 2A34C22 84SF-4 to 84SF-12 220 2800 220 2800 80" - 72" (-4 to -12) 47.0 Lbs. Hub Model D2A34C34 84JF-0 to 84JF-12 285 2700 285 2700 84" - 72" (-0 to -12) 51.0 Lbs. Hub Models D2A34C49 and 2A34C50 90A-0 to 90A-18 265 2700 265 2700 90" - 72" (-0 to -18) 52.0 Lbs. Page No. 1 2 3 4 5 6 7 8 9 Rev. No. 24 22 23 23 22 22 22 22 22 P3EA Page 2 of 9 Blades Eligible Maximum Continuous Take-Off Diameter Limits Approx. Max. Wt. Complete (For reference only) (See NOTE 2) HP RPM HP RPM (See NOTE 2) (Max. Dia.) Hub Models D2A34C58, F2A34C58, E2A34C64, 2A34C66, E2A34C70, E2A34C73, D2A34C78 and D2A34C98 90AT-0 to 90AT-12 285 2700 300 2850 90" - 78" (-0 to -12) 52.5 Lbs. * 58.5 Lbs. ** 57.0 Lbs. * with E2A34C64 hub ** with E2A34C70 or E2A34C73 hub Hub Model D2A34C67 76C-0 to 76C-6 225 2800 225 2800 76" - 70" (-0 to -6) 47.0 Lbs. Hub Model 2A34C201 90D[X]-0 to 90D[X]-18 285 2800 300 2850 90" - 72" (-0 to -18) 49.0 Lbs. Hub Model 2A34C203 90DC[X]-0 to 90DC[X]-18 285 2700 300 2850 90" - 72" (-0 to -18) 49.0 Lbs. 90DC[X]-0 to 90DC[X]-18 210 2800 210 2800 80" - 72" (-0 to -18) 49.0 Lbs. Hub Model C2A34C204 90DC[X]-0 to 90DC[X]-18 285 2700 300 2850 90" - 72" (-0 to -18) 49.0 Lbs. Hub Models B2A34C205 and 2A34C227 90DH[X]-0 to 90DH[X]-18 285 2700 300 2850 90" - 72" (-0 to -18) 49.0 Lbs. Hub Models 2A34C209 and 2A34C210 78CC[X]-0 to 78CC[X]-8 225 2800 225 2800 78" - 70" (-0 to -8) * 49.0 Lbs. ** 53.0 Lbs. * with 2A34C209 hub ** with 2A34C210 hub Hub Models 2A34C216 and 2A34C221 90DH[X]-12 to 90DH[X]-20 220 2700 220 2700 78" - 70" (-12 to -20) 53.8 Lbs. Hub Model 2A37C223 90R[X]-0 to 90R[X]-12 285 2700 300 2850 90" - 78" (-0 to -12) 64.0 Lbs. Page 3 of 9 P3EA Blades Eligible Maximum Continuous Take-Off Diameter Limits Approx. Max. Wt. Complete (For reference only) (See NOTE 2) HP RPM HP RPM (See NOTE 2) (Max. Dia.) Hub Model B2A34C225 90DJ[X]-0 to 90DJ[X]-24 285 2700 300 2850 90" - 66" (-0 to -12) 49.0 Lbs. Hub Model B2A37C228 90RD[X]-0 to 90RD[X]-18 300 2700 300 2850 90" - 72" (-0 to -18) 61.0 Lbs. Hub Models D2A37C230, D2A37C231 and 2A37C232 90RE[X]-0 to 90RE[X]-12 285 285 2700 2700 300 300 2700 2850 90" - 78" (-0 to -12) 86" - 78" (-4 to -12) 61.0 Lbs. 61.0 Lbs. Hub Models E2A37C233 and E2A37C234 90RE[X]-8 to 90RE[X]-12 285 2700 300 2850 82" - 78" (-8 to -12) 65.0 Lbs. Hub Model B2A37C238 90RE[X]-0 to 90RE[X]-18 300 2700 300 2850 90” – 72” (-0 to -18) 61.0 Lbs. Hub Model 2A34C239 90DM[X]-15 to 90DM[X]-18 285 2800 285 2800 75” – 72” (-15 to -18) 53.0 Lbs. Hub Model 2A34C240 90 DJ[X]-0 to 90DJ[X]-24 280 2500 280 2500 90” – 66” (-0 to -24) 65.0 Lbs. Hub Model 2A34C241 82PG[X]-6 to 82PG[X]-10 300 2700 300 2700 76” – 72” (-6 to -10) 65.0 Lbs. P3EA Page 4 of 9 Certification Basis Models D2A34C49/90A, 2A34C50/90A and D2A34C58/90A: Civil Air Regulations Part 14 effective December 15, 1956. Models E2A34C64/90AT, 2A34C66/90AT and D2A34C67/76C: Civil Air Regulations Part 14 effective December 15, 1965 with Amendment 14-1 thereto. Models E2A34C70/90AT, E2A34C73/90AT and D2A34C78/90AT: Federal Aviation Regulations Part 35 with Amendment 35-1 thereto. Models 2A34C22/84SF, D2A34C34/84JF, F2A34C58/90AT, D2A34C98/90AT, 2A34C201/90DA, 2A34C203/90DCA, C2A34C204/90DCB, 2A34C209/78CCA, and 2A34C210/78CCA: Federal Aviation Regulations Part 35 with Amendments 35-1 and 35-2 thereto. Model B2A34C205/90DH[X] and 2A34C216/90DH[X]: Federal Aviation Regulations Part 35 effective February 1, 1965 with Amendments 35-1 thru 35-4 thereto. Models 2A34C221/90DH[X] and B2A34C225/90DJ[X]: Federal Aviation Regulations Part 35 effective October 14, 1980 with Amendments 35-1 thru 35-5 thereto. Models 2A37C223/90R[X], 2A34C227/90DH[X], B2A37C228/90RD[X], D2A37C230/90RDB, D2A37C231/90RDC, 2A37C232/90RDB, E2A37C233/90RDB, E2A37C234/90RDC, B2A37C238, 2A34C239/90DM[X], 2A34C240/90DJ[X] and 2A34C241/82PG[X]: Federal Aviation Regulations Part 35 effective August 18, 1990 with Amendments 35-1 thru 35-6 thereto. Type Certificate No. P3EA issued May 11, 1962 under Delegation Option Authorization of Regulations of the Administrator Part 410. Date of application for Type Certificate: March 12, 1962. Production Basis Production Certificate No. 3 Page 5 of 9 P3EA NOTE 1. Hub Model Designation. Basic Model Designation D 2 A 34 C 49 - A Minor change not affecting interchangeability or eligibility. Any change affecting eligibility. The 201 series denotes modified retention system. 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° clockwise C - 120° and 300° clockwise D - 90° and 270° clockwise E - 30° and 210° clockwise F - two alternate locations - 150° and 330° clockwise, or 90° and 270° clockwise NOTE 2. Blade Model Designation. Basic Model Designation S - 90 AT - 0 Reduction in inches from basic design diameter (as -4, diameter reduced 4 inches to 86 inches). Characteristics of blade design (planform, etc.). T signifies tilted blade. Suffix [X] indicates blade butt staking dimensions for the actuating pin. Basic design diameter inches. Indicates minor change not affecting eligibility. P3EA Page 6 of 9 NOTE 3. Pitch Control. With the following governors: Woodward Model x,210,xxx Wt. 3.5 lb. Hoof Model 1,000,007 Series Wt. 3.5 lb. Hoof Model 1,604,014 Series Wt. 3.5 lb. Garwin Model 34-828 Series Wt. 3.0 lb. Hartzell Model F-2-7( ) Wt. 4.5 lb. McCauley Model C290D[X]/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. With McCauley spinners: (1) D-2845 Installation for model 2A34C50. (2) D-2771 Installation for models D2A34C34, D2A34C49 and D2A34C58. (3) D-4082 Installation for model D2A34C58. (4) D-2271 Installation for model D2A34C67. (5) D-4101 Installation for model 2A34C22. (6) D-3290, D-3396 or D-5255 Installation for model 2A37C223. (7) D-5915 Installation for models B2A34C225 and 2A34C227. (8) D-3396 or D-5255 Installation for model B2A37C228. (9) Per McCauley drawing E-7543 for model B2A37C238. (10) Model 2A34C241 with spinner reference McCauley Drawing E-7580 . NOTE 8. Not applicable. NOTE 9. Special Limits: Please reference the airworthiness limitation section of the appropriate Service and Operator's manuals. Table of Propeller-Engine Combinations Approved Vibrationwise for Use on Normal Category Single-Engine Tractor Aircraft The maximum and minimum propeller diameters 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 Crankshaft Damper Configuration Max. Dia. (Inches) Min. Dia. (Inches) Placards D2A34C67 76C Continental I0-360 Series (up to 210 hp. @2800 r.p.m.) Two 6th order, or one 4.5 and one 6th order 76 70 None D2A34C67 76C Continental TSI0- 360 Series (up to 210 hp. @2800 r.p.m.) Two 6th order, or one 4.5 and one 6th order 76 74 None Page 7 of 9 P3EA Hub Model Blade Model Engine Model Crankshaft Damper Configuration Max. Dia. (Inches) Min. Dia. (Inches) Placards 2A34C209 or 2A34C210 78CCA Continental I0-360 Series (up to 210 hp. @2800 r.p.m.) Two 6th order, or one 4.5 and one 6th order 78 72 None D2A34C34 84JF Continental I0-470 Series (up to 260 hp. @2625 r.p.m.) Two 6th, one 5th and one 4.5 order 84 79 None D2A34C34 84JF Continental TSI0- 520 Series (up to 285 hp. @2700 r.p.m.) Two 6th, one 5th and one 4th order 81 79 None 2A34C22 84SF Franklin 6A-335 Series (up to 180 hp. @2800 r.p.m.) Viscous Damper 80 72 None 2A34C22 84SF Franklin 6A-350 Series (up to 220 hp. @2800 r.p.m.) Viscous Damper 80 74 None D2A34C49 or 2A34C50 90A Continental 0-470 and I0-470 Series (up to 260 hp. @2625 r.p.m.) Four 6th order 88 76 None Continental 0-470 and I0-470 Series (up to 230 hp. @2650 r.p.m.) One 5th and one 6th order 88 80 None D2A34C58 2A34C66 E2A34C64 D2A34C78 E2A34C70 E2A34C73 or D2A34C98 90AT Continental 0-470 and I0-470 Series (up to 260 hp. @2625 r.p.m.) Continental 0-470 and I0-470 Series (up to 230 hp. @2650 r.p.m.) Four 6th order One 5th and one 6th order 88 88 76 80 None None 2A34C66 90AT Continental 0-470 Series (up to 190 hp. @2300 r.p.m. max. cont. and 213 hp. @2600 r.p.m. takeoff) Four 6th order 90 80 None P3EA Page 8 of 9 Hub Model Blade Model Engine Model Crankshaft Damper Configuration Max. Dia. (Inches) Min. Dia. (Inches) Placards D2A34C58 D2A34C78 F2A34C58 or D2A34C98 90AT Continental I0-520 Series (up to 285 hp. @2700 r.p.m. maximum continuous and 300 hp. @2850 r.p.m. takeoff) One 4th, one 5th and two 6th order 88 80 None D2A34C58 D2A34C78 or D2A34C98 90AT Continental TSI0- 520 Series (up to 285 hp. @2600 r.p.m. max. continuous & 300 hp. @2700 r.p.m. takeoff) One 4th, one 5th and two 6th order 81.5 80.5 None D2A34C58 2A34C66 D2A34C78 or D2A34C98 90AT Continental TSI0- 520 Series (up to 285 hp. @2700 r.p.m.) One 4th, one 5th and two 6th order 82 80 None D2A34C58 2A34C66 D2A34C78 or D2A34C98 90AT Continental TSI0- 520 Series (up to 285 hp. @2700 r.p.m.) One 4th, one 5th and two 6th order 88 86 None E2A34C64 E2A34C70 or E2A34C73 90AT Continental TSI0- 520 Series (up to 285 hp. @2700 r.p.m.) One 4th, one 5th and two 6th order 82 80 None E2A34C64 E2A34C70 or E2A34C73 90AT Continental I0-520 Series (up to 285 hp. @2700 r.p.m. maximum continuous and 300 hp. @2850 r.p.m. takeoff) One 4th, one 5th and two 6th order 82 80 None 2A34C201 90DA Continental 0-470 Series (up to 230 hp. @2600 r.p.m.) One 5th and one 6th order 82 80 None Page 9 of 9 P3EA Hub Model Blade Model Engine Model Crankshaft Damper Configuration Max. Dia. (Inches) Min. Dia. (Inches) Placards 2A34C201 90DA Franklin 6AS-350 Series (up to 235 hp. @2800 r.p.m. maximum continuous and 250 hp. @2800 r.p.m. takeoff) Viscous damper 88 76 None 2A34C201 90DA Franklin 6A-350-C Series (up to 220 hp @ 2800 rpm takeoff and maximum continuous) Viscous Damper 88 76 None 2A34C203 90DCA Continental I0-360 Series (up to 210 hp. @2800 r.p.m.) One 6th and one 4.5 order 80 74 None 2A34C203 90DCA Continental 0-470 Series (up to 230 hp. @2600 r.p.m.) One 5th and one 6th order 88 80 None C2A34C204 90DCB Continental 0-470 Series (up to 230 hp. @2400 r.p.m.) Two 6th, one 5th and one 4.5 order 82 80 None C2A34C204 90DCB Continental 0-470 Series (up to 230 hp. @2400 r.p.m.) Two 6th, one 5th and one 4.5 order 90 88.5 None NOTE 10. Special Notes. Aircraft installation must be approved as part of the aircraft type certificate upon compliance with the applicable airworthiness requirements. ... END ... ``` ## ADs (13, in force first) - [AD 2006-24-07](https://openairdocs.org/ad/2006-24-07): Propeller blades · Hartzell Propeller BHC-C2Y, HC-A2V, HC-A3V and 52 more. Effective Jan 3, 2007 - [AD 2005-24-09](https://openairdocs.org/ad/2005-24-09): Propeller hubs · McCauley Propeller Systems 2D34C, 3AF32C87, 3AF34C92 and 4 more. Effective Dec 15, 2005 - [AD 2005-14-11](https://openairdocs.org/ad/2005-14-11): Failed propeller blade · Hartzell Propeller BHC-92W, BHC-92ZF-1, BHC-92ZF-3 and 391 more. Effective Aug 17, 2005 - [AD 2003-13-17](https://openairdocs.org/ad/2003-13-17): Propeller blade · Hartzell Propeller BHC-A2V, BHC-C2Y, EHC-G3YF-2 and 81 more. Effective Jul 18, 2003 - [AD 95-09-08](https://openairdocs.org/ad/95-09-08): Cylinder Screw · McCauley Propeller Systems 2A37C. Effective May 19, 1995 - [AD 91-15-04](https://openairdocs.org/ad/91-15-04): Hub · McCauley Propeller Systems 2A34C, 2AF34C55, 2D34C and 5 more. Effective Aug 7, 1991 - [AD 83-24-11 R1](https://openairdocs.org/ad/83-24-11-R1): Retention Threads · McCauley Propeller Systems 2A34C, 2A36C23 and E2A34C. Effective Mar 12, 1986 - [AD 82-27-02 R1](https://openairdocs.org/ad/82-27-02-R1): Shank · McCauley Propeller Systems 2A34C, B2D34C, B2D34CT69 and 7 more. Effective Feb 22, 1983 - [AD 77-16-01](https://openairdocs.org/ad/77-16-01): Actuating Pins · McCauley Propeller Systems 2A34C, 2A36C1, 2A36C18 and 8 more. Effective Aug 9, 1977 - [AD 77-13-17](https://openairdocs.org/ad/77-13-17): Actuating Pins · McCauley Propeller Systems 2A34C, 2AF34C55, 3AF32C75 and 9 more. Effective Jul 6, 1977 - [AD 72-25-07](https://openairdocs.org/ad/72-25-07): Blades · McCauley Propeller Systems E2A34C. Effective Dec 13, 1972 - [AD 68-08-01](https://openairdocs.org/ad/68-08-01): Cylinder Attach Screws · McCauley Propeller Systems 2A34C, 2A36C23, 2A36C29 and 14 more. Effective Jan 21, 1972 - [AD 68-10-03](https://openairdocs.org/ad/68-10-03): Hub Alignment Dowels · McCauley Propeller Systems 2AF34C55, D2A34C and D2AF34C. Effective May 11, 1968 ## STCs approved under this data sheet (6) - [STC SP01222WI](https://openairdocs.org/stc/SP01222WI): Installation of Aircraft Development propeller vortelators.. Aircraft Development Co - [STC SP00582NY](https://openairdocs.org/stc/SP00582NY): Installation of Prop-Guard Polyurethane Protective Tape on the leading edge of metal propellers.. McFarlane Aviation, Inc. - [STC SP00400SE](https://openairdocs.org/stc/SP00400SE): Installation of various propeller electrical de-icer models. SMR Technologies - [STC SP1964SO](https://openairdocs.org/stc/SP1964SO): Installation of replacement electrothermal type de-icing boots.. Thermodyne, Inc - [STC SP1318GL](https://openairdocs.org/stc/SP1318GL): Installation of replacement electrothermal type de-icing boots.. Rapco, Inc - [STC SP1628SO](https://openairdocs.org/stc/SP1628SO): Install H&H Propeller blade activating link P/N H-1935.. Henderson Timothy H --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.