# TCDS P22EA: McCauley Propeller Systems - Type: Type certificate data sheet - Status: Current - Holder: McCauley Propeller Systems - Revision: 8 - Revised: May 24, 2006 - Product: Propeller - Certification basis: Part 21, Part 35 - Data sheet PDF: https://openairdocs.org/files/sha256/2a/65/2a65aecbb61cc7272db7111e01b41392b0efd294eef2a584b50eef0dd68868e8 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C79BEEADDCB1C5FC8625717F004E5A24.0001 - Page: https://openairdocs.org/tcds/P22EA ## Models (10) As the data sheet lists them. - D3AF32C35 - D3AF32C87 - 3AF34C74 - 3AF32C93 - 3AF34C92 - 3AF32C72 - 3AF32C75 - 3AF32C87 - D3AF32C80 - 3AF34C86 ## 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 P22EA Revision 8 McCAULEY 3AF32C D3AF32C 3AF34C May 24, 2006 TYPE CERTIFICATE DATA SHEET NO. P22EA Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P22EA) 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 Propeller Systems 7751 East Pawnee Wichita, KS 67207 Type Certificate Holder Record: Name changed from McCauley Accessory Division, Cessna Aircraft Company, Vandalia, OH 45377 to McCauley Propeller Systems, 7751 East Pawnee, Wichita, KS 67207 May 2006. Type Constant Speed & full feathering; Hydraulic (see NOTES 3 and 4) Engine Shaft Special flange 4 in. B.C. Hub material Aluminum alloy Blade material Aluminum alloy No. of blades Three Hubs eligible D3AF32C35, 3AF32C72, 3AF32C75, 3AF34C74, D3AF32C80, 3AF34C86, 3AF32C87, D3AF32C87, 3AF34C92, 3AF32C93. Maximum Continuous Takeoff Diameter Limits Approx. Max. Wt. Complete Blades HP RPM HP RPM (See Note 2) (Reference only - See NOTE 3) Hub Model 3AF32C72 82N-0 to 285 2700 285 2700 82" - 74" 78.5 lbs. 82N-8 (-0 to -8) Hub Models 3AF32C75, D3AF32C35 82NB-0 to 300 2700 300 2700 82" - 74" 75.0 lbs. 82NB-8 (-0 to -8) Hub Models D3AF32C80, 3AF32C87, D3AF32C87 82NC-0 to 310 2700 310 2700 82" - 74" *75.0 lbs., **79.0 lbs. 82NC-8 (-0 to -8) Hub Model 3AF32C93 82NC-2 to 325 2700 325 2700 80" - 74" 79.0 lbs. 82NC-8 (-2 to -8) Hub Models 3AF34C74, 3AF34C86, 3AF34C92 90LF-0 to 375 2400 375 2400 90" - 84" 83.5 lbs. 90LF-6 (-0 to -6) * With hub model D3AF32C80 Page No. 1 2 3 4 5 Rev. No. 8 7 7 7 7 ** With hub models 3AF32C87, D3AF32C87, 3AF32C93 P22EA Page 2 of 5 Certification basis Models 3AF32C72/82N, 3AF32C75/82NB, 3AF34C74/90LF, D3AF32C80/82NC, D3AF32C80/82NC, 3AF34C86/90LF, 3AF32C87/82NC, and 3AF34C92/90LF: Federal Aviation Regulations Part 35 with Amendment 35-1 thereto. All other models: Federal Aviation Regulations Part 35 with Amendments 35-1 and 35-2 thereto. Type Certificate No. P22EA issued June 7, 1965 under Delegation Option Authorization provisions of Part 21 Subpart J of the Federal Aviation Regulations. Date of Application for Type Certificate April 28, 1965. Production basis Production Certificate No. 3 NOTE 1. Hub Model Designation Basic Model Designation D 3 A F 32 C 72 - A Minor change not affecting interchangeability or eligibility Change affecting eligibility. C denotes constant speed. McCauley blade shank size F denotes feathering model. A denotes special flange 4" B.C. 3 denotes number of blades Indicates dowel location with respect to centerline through blade sockets, viewing hub from mounting face. Blank - 60° and 240° clockwise with No. 1 blade vertical and up. D - 90° and 270° clockwise with No. 1 blade vertical and up. NOTE 2. Blade Model Designation Basic model designation S - 82 NC - 0 Reduction in inches from basic diameter (as -4, diameter reduced 4 inches to 78 inches.) Blade form characteristics, i.e. activity factor, planform, pitch distribution, etc. One or more letters may be used. Basic design diameter in inches. Minor change not affecting interchangeability or eligibility. NOTE 3. Pitch Control . Eligible with the following governors: Woodward Model x,210,xxx Wt. 3.5 lb. McCauley Models CF310D1/T[X], CF310D2/T[X] Wt. 3.0 lb. McCauley Models CFS310D1/T[X], CFS310D2/T[X], Wt. 3.0 lb. CFS310D3/T[X] McCauley Models CFU310D1T/[X], CFU310D2/T[X], Wt. 3.0 lb. McCauley Models CFUS310D1/T[X], CFUS310D2/T[X], Wt. 3.0 lb. CFUS210D3/T[X] McCauley Models DCF290DX/TX, Wt. 3.0 lb. McCauley Models DCFS290DX/TX, DCF310D(X)/T(X) DCFS310D(X)/T(X) Wt. 3.0 lb. McCauley Models DCFU290DX/TX, DCFU310D(X)/T(X) Wt. 3.0 lb. McCauley Models DCFUS290DX/TX, DCFUS310D(X)/T(X) Wt. 3.0 lb. Page 3 of 5 P22EA NOTE 4. Feathering. Eligible with full feathering control installed in accordance with the propeller manufacturer's instructions. 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) Propeller Anti-Icing (1) Model 82N, 82NB, 82NC and 90LF blades eligib le with Goodrich 4E1188-3 deicer installed per Goodrich Report No. 59-728; or with Goodyear 4065-2556 or 4065-2551 iceguard installed per Goodyear Manual AP-147. (2) Model 90LF blade eligible with Goodrich 37572 fl uid feed shoe, 12 inches maximum length, when applied in accordance with McCauley or Goodrich instructions. (3) Model 82NB blade eligible with Goodrich 37572 fluid feed shoe, 10 inches maximum length, when applied in accordance with McCauley or Beech (Beech Specification BS-388) instructions. (b) Spinners (1) Models 3AF32C72/82N, 3AF 32C87/82NC and 3AF32C93/82NC eligible with McCauley plain or anti-icing spinners; reference D-3534 Do me, D-3537 Bulkhead and D-3538 Installation. (2) Models 3AF34C74/90LF and 3AF34C92/90LF eligible with McCauley plain or anti-icing spinner; reference D-3573 Dome, D-3576 Bu lkhead and D-3574 Installation. (3) Model 3AF32C75/82NB eligible with McCauley plain or anti-icing spinner; reference D-3570 Dome, D-3571 Bulkhead, and D-3499 or PD-3499 Installation; or D-3607 Dome, D-3608 Bulkhead, and D-3605 or PD-3605 Installation. (4) Model D3AF32C80/82NC eligible with Mc Cauley spinner; reference D-3651 Dome, D-3652 Bulkhead, and D-3649 Installation. (5) Model 3AF32C86/90LF eligible with Mc Cauley spinner, reference D-3626 Dome, B-3627 Bulkhead, and D-3625 Installation. (6) Model 3AF32C87/82NC eligible with McCaul ey spinner, reference D-3651 Dome, B-3863 Spacer, C-3862 Support, D-3925 Bulkhead, C-4044 Bulkhead adapter and D-4042 Installation. (7) Model D3AF32C35/82NB eligible with McCauley plain or anti-icing spinner; reference D-3570 Dome, D-4151 Bulkhead and D-4068 or PD-4068 Installation; or D-3607 Dome, D-4150 Bulkhead and D-4069 or PD-4069 Installation. 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 diameter reduction allowable for repair purposes. Hub Blade Engine Damper Max. Dia. Min. Dia. Model Model Engine Model Configuration (Inches) (Inches) Placards 3AF32C75 82NB Continental IO-470 Two 6th & Two 5th 80 74 None or D3AF32C80 82NC series (up to 260 hp. Order; or Two 6th, @2625 r.p.m. rating) One 5th & One 4.5 Order 3AF32C93 82NC Continental IO-470 Two 6th and Two 80 74 None or D3AF3287 82NC series (up to 260 hp. 5th order to Two @2625 r.p.m.) 6th, one 5th and one 4.5 Order 3AF32C72 82N Continental IO-520 or Two 6th, One 5th 78 74 None or 3AF32C75 82NB TSIO-520 series (up to & One 4th Order 285 hp. @2700 r.p.m. rating) P22EA Page 4 of 5 Hub Blade Engine Damper Max. Dia. Min. Dia. Model Model Engine Model Configuration (Inches) (Inches) Placards 3AF32C93 82NC Continental IO-520 Two 6th, one 5th 80 74 None series (up to 300 hp. and one 4th Order @2850 r.p.m. takeoff and 285 hp. @2700 r.p.m. max. continuous) D3AF32C87 82NC Continental IO-520 Two 6th, one 5th 80 74 None or 3AF32C87 82NC series (up to 300 hp. and one 4th Order @2850 r.p.m. takeoff and 285 hp. @2700 r.p.m. max. continuous) D3AF32C35 82NB Continental IO-520 Two 6th, One 5th 78 74 None series (up to 285 hp. and one 4th Order @2700 r.p.m.) 3AF32C75 82NB Continental IO-520 or Two 6th, One 5th 80 74 None 3AF32C87 82NC TSIO-520 series (up to & one 4th Order or D3AF32C80 82NC 285 hp. @2700 r.p.m. rating) D3AF32C35 82NB Continental TSIO-520 Two 6th, One 5th 80 74 None series (up to 285 hp. and one 4th Order @2700 r.p.m.) 3AF32C75 82NB Continental TSIO-520 Two 6th, One 5th 80 74 None or 3AF32C87 82NC series (up to 300 hp. & One 4th Order & 2700 r.p.m.) 3AF32C93 82NC Continental TSIO-520 Two 6th & One 80 74 None series (up to 300 hp. 5th and one 4th @2700 r.p.m.) Order 3AF32C93 82NC Continental TSIO-520 Two 6th, one 5th 76.5 74.5 None series (Up to 310 hp. and one 4th Order @2700 r.p.m. and 36 in. manifold pressure) 3AF32C93 82NC Continental TSIO-520 Two 6th, one 5th 78.5 77 "Avoid continuous series (up to 310 hp. and one 4th Order operation below @2700 r.p.m. and 36 in. 2500 r.p.m. above manifold pressure) 33 in. manifold pressure" 3AF32C93 82NC Continental TSIO-520 Two 6th, one 5th 76.5 75 None series (up to 310 hp. and one 4th Order @2700 r.p.m. & 38 in. manifold pressure) 3AF32C93 82NC Continental IO-520 or Two 6th, one 5th 80 74 None TSIO-520 series (up to and one 4th Order 285 hp. @2700 r.p.m.) 3AF34C74 90LF Continental GTSIO-520 Six 3rd Order 88 86 None series (up to 340 hp. @2400 prop. r.p.m. or 3200 engine r.p.m.) Page 5 of 5 P22EA Hub Blade Engine Damper Max. Dia. Min. Dia. Model Model Engine Model Configuration (Inches) (Inches) Placards 3AF34C74 90LF Continental GTSIO-520 Six 3rd Order 90 84 None 3AF34C86 90LF series (up to 340 hp. or 3AF34C92 90LF @3200 engine r.p.m. & 2400 propeller r.p.m. rating) 3AF34C74 90LF Continental GTSIO-520 Six 3rd Order 90 88 None 3AF34C92 90LF series (up to 375 hp. @3400 engine r.p.m. & 2267 propeller r.p.m.) NOTE 10. The word "eligible" as used herein does not signify approval as part of this type certificate. "Eligible" accessories and governors must be approved as part of the aircraft type certificate upon compliance with the applicable aircraft airworthiness requirements. .....END..... ``` ## ADs (6, 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 95-24-05 R1](https://openairdocs.org/ad/95-24-05-R1): Propeller Blade · McCauley Propeller Systems 3AF32C72, 3AF32C75, 3AF32C87 and 7 more. Effective Apr 12, 1996 - [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 ## STCs approved under this data sheet (5) - [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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. 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