# TCDS P11NE: Hamilton Sundstrand Corporation - Type: Type certificate data sheet - Status: Current - Holder: Hamilton Sundstrand Corporation - Revision: 13 - Revised: December 7, 2015 - Product: Propeller - Data sheet PDF: https://openairdocs.org/files/sha256/a6/5f/a65fa2fbd5484d026f67299c951cea38c9efbfd5bd6cab8f1ee436601abcd8e6 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C7DE8AC9118F01F186257F150072C6A2.0001 - Page: https://openairdocs.org/tcds/P11NE ## Models (11) As the data sheet lists them. - 14RF-36 - 14RF-19 - 14RF-21 - 14RF-22 - 14RF-10 - 14RF-35 - 14RF-9 - 14RF-20 - 14RF-24 - 14RF-23 - 14RF-37 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page 1 2 3 4 Rev. 13 13 12 13 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET P11NE TCDS NUMBER P11NE REVISION 13 HAMILTON SUNDSTRAND MODEL/S: 14RF-9 14RF-10 14RF-19 14RF-20 14RF-21 14RF-22 14RF-23 14RF-24 14RF-35 14RF-36 14RF-37 December 7, 2015 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate Number P11NE) 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: Hamilton Sundstrand Corporation One Hamilton Road Windsor Locks, CT 06096-1010 TYPE: Constant speed; hydraulic (see Notes 3 & 4) ENGINE FLANGE: 5.125" Bolt Circle HUB MATERIAL: Aluminum BLADE MATERIAL: Fiberglass covered aluminum spar NUMBER OF BLADES: Four DESIGN SERIES: 14RF See Note 15 for the associated model parts list unique to aircraft applications. BLADE MODELS MAX CONTINUOUS NOMINAL DIAMETER (FT) APPROXIMATE WEIGHT (LB) RIGHT LEFT SHP RPM SHP RPM RFC11E1-6A RFC11E2-6A 2,000 1,313 2,000 1,313 10.5 230.0 RFC11L1-OC RFC11L2-OC 1,870 1,398 1,870 1,398 11.0 232.0 RFC11M1-6A RFC11M2-6A 2,000 1,313 2,000 1,313 10.5 231.0 RFC11N1-6A RFC11N2-6A 2,000 1,313 2,000 1,313 10.5 228.5 RFC11P1-OC RFC11P2-OC 1,870 1,398 1,870 1,398 11.0 230.0 RFC11R1-OC RFC11R2-OC 1,870 1,398 1,870 1,398 11.0 230.0 RFC11T1-OC RFC11T2-OC 1,940 1,398 1,940 1,398 11.0 232.0 RFC11U1-6A RFC11U2-6A 2,000 1,313 2,000 1,313 10.5 228.5 RFC11V1-OC RFC11V2-OC 1,870 1,398 1,870 1,398 11.0 230.0 RFC11W1-OC RFC11W2-OC 1,870 1,398 1,870 1,398 11.0 232.0 RFC11AA1-6A RFC11AA2-6A 2,000 1,313 2,000 1,313 10.5 228.5 RFC11AC1-OC RFC11AC2-OC 1,870 1,398 1,870 1,398 11.0 232.0 RFC11Y1-OC RFC11Y2-OC 1,870 1,398 1,870 1,398 11.0 232.0 RFC11Z1-OC RFC11Z2-OC 1,870 1,398 1,870 1,398 11.0 230.0 RFA12A1 POC 1,750 1,384 1,940 1,384 12.0 270.0 Page 2 of 4 TCDS P11NE CERTIFICATION BASIS: FAR 35 through Amendment 7 dated December 28, 1995. Model 14RF-9/10 14RF-19/20 14RF-21/22 14RF-23/24 14RF-35/36 14RF-37 TC Application Date 06/24/82 04/25/89 08/03/84 04/25/89 05/10/96 04/02/97 TC Issued 12/12/84 05/31/89 08/27/85 05/31/89 05/24/96 09/01/98 PRODUCTION BASIS: Production Certificate No. 14 Propeller assemblies produced under FAA PC14 will have serial numbers in a date code format, YYYYMM#### EASA Production Organization Approval Certificate FR.21G.0001 Propeller assemblies produced under EASA Certificate will have serial numbers in a date code format, FRYYYYMM####. Y: Four digit year; M: Two digit month; #: Four digit incremental number NOTES NOTE 1: HUB MODEL DESIGNATION 1 4 R F - 9 Indicates a specific model designation which defines a complete propeller assembly, including spinner. F denotes flange mounting Blade shank size Number of blades Major model type Special notation – see Note 14 TCDS P11NE Page 3 of 4 NOTE 2: BLADE MODEL DESIGNATION Special notation – See note 14 Blade spinner interface Normal reduction from basic diameter in inches Direction of rotation and tip configuration Structural and operational features (may indicate particular deicing assembly) Basic diameter feet (Diameter limit shown is normal diameter of assembled propeller and does not include the +1/4-inch / 3/16-inch manufacturing tolerance permissible.) Major aerodynamic characteristics Denotes fiberglass blade Hamilton Sundstrand shank size R F C 11 E 1 6 A - Special notation - See Note 13 NOTE 3: PITCH CONTROL: Propeller control specified on approved model parts list. NOTE 4: (a) FEATHERING: Full feathering with propeller control specified on approved model parts list. (b) REVERSING: Full reversing with propeller control specified on approved model parts list. NOTE 5: LEFT-HAND MODELS: The left-hand version of an approved propeller model has the same rating and diameter limitations as listed for the right-hand model. NOTE 6: INTERCHANGEABLE BLADES: Not applicable. NOTE 7: ACCESSORIES: (a) Propeller deicing: Electrical deicing system specified on approved model parts list and installed in accordance with the propeller manufacturer's instructions. (b) Spinners: Spinner specified on approved model parts list. NOTE 8: SHANK FAIRINGS: Not applicable. Page 4 of 4 TCDS P11NE NOTE 9: SPECIAL LIMITS: Airworthiness limitations, if any, are specified in System Maintenance Manual (SMM) P5186 for Model 14RF-9, in SMM P5189 for Model 14RF-21, in SMM P5199 for Model 14RF-19, and in SMM P5208 for 14RF-35, in SMM P5200 for Model 14RF-23, and in SMM 5209 for 14RF-37. NOTE 10: SPECIAL NOTES: Aircraft installations must be approved as part of the aircraft type certificate and demonstrate compliance with the applicable aircraft airworthiness requirements. NOTE 11: LIFE-LIMITED PARTS: See Note 9. NOTE 12: BLADES: (a) The RFC11E1-6A, RFC11M1-6A, RFC11N1-6A, RFC11U1- 6A, and RFC11AA1-6A blades are for the use on the Model 14RF-9 propeller in sets of four. The left-hand versions of these blades are for use on the Model 14RF-10 propellers. (b) The RFC11L1-OC, RFC11P1-OC, RFC11R1-OC, RFC11V1-OC, RFC11W1-OC, RFC11Y1-OC and RFC11Z1-OC blades are for use on the Model 14RF-21 propeller in sets of four. The left-hand version of these blades are for use on the Model 14RF-22 propellers. (c) The RFC11T1-OC and RFC11AC1-OCblades are for use on the Model 14RF-19 and Model 14RF-23 and Model 14RF-35 propellers in sets of four. The left-hand version of these blades are for use on the Model 14RF-20, Model 14RF-24, and Model 14RF-36 propellers. (d) The RFA12A1 POC is for use on the Model 14RF -37 Propeller in sets of 4 only. NOTE 13: SPECIAL NOTATION: This position of the blade model designation normally consists of a hyphen. This hyphen is replaced by a letter to designate a special characteristic. The meaning of these letters is identified below. “P” is used to identify a blade that “as produced or manufactured” met specific requirements. “R” is used to identify a blade that has been reworked to meet specific requriements. NOTE 14: SPECIAL NOTATION: Additional markings may be present at the end of the core part number per instructions for continued airworthiness signifying that the blade, hub or actuator has been reworked to meet specific requirements. NOTE 15: MODEL PARTS LISTS FAA Approved Model Parts Lists (not inclusive) are: PL26524 14RF-1, for application on EMB-120 PL26473 14RF-19, for application on SF-340B PL27764 14RF-21, for application on CN-235 PLK28106 14RF-37, for application on CN-235 …..END…… ``` ## ADs (17, in force first) - [AD 2013-16-10](https://openairdocs.org/ad/2013-16-10): Inspections · Hamilton Standard Division 24PF-303, 24PF-304, 24PF-305 and 41 more. Effective Sep 19, 2013 - [AD 2006-16-01](https://openairdocs.org/ad/2006-16-01): Actuator yokes · Hamilton Sundstrand 14RF-19. Effective Aug 30, 2006 - [AD 2006-10-07](https://openairdocs.org/ad/2006-10-07): Propeller blades of the "+E'' repair configuration · Hamilton Sundstrand 14RF-9. Effective May 22, 2006 - [AD 96-25-20](https://openairdocs.org/ad/96-25-20): Transfer Tube Assemblies · Hamilton Standard Division 6/5500/F-1, 6/5500/F-2, 14RF-19 and 10 more. Effective Feb 7, 1997 - [AD 96-08-01 R1](https://openairdocs.org/ad/96-08-01-R1): Blades · Hamilton Sundstrand 14RF-9. Effective Aug 2, 1996 - [AD 96-08-02](https://openairdocs.org/ad/96-08-02): Blades · Hamilton Standard Division 6/5500/F-1, 6/5500/F-2, 14RF-19 and 10 more. Effective May 9, 1996 - [AD 95-22-12](https://openairdocs.org/ad/95-22-12): Control Unit Servo Ballscrew Internal Spline Assembly · Hamilton Standard Division 6/5500/F-1, 6/5500/F-2, 14RF-19 and 12 more. Effective Nov 24, 1995 - [AD 94-06-05](https://openairdocs.org/ad/94-06-05): Hub · Hamilton Sundstrand 14RF-19, 14RF-21 and 14RF-9. Effective Mar 29, 1994 - [AD 93-06-06](https://openairdocs.org/ad/93-06-06): Control Unit Ballscrew · Hamilton Standard Division 6/5500/F-1, 14RF-19, 14RF-21 and 8 more. Effective Jul 6, 1993 - [AD 2006-12-19](https://openairdocs.org/ad/2006-12-19) (historical): Actuator yokes · Hamilton Sundstrand 14RF-19. Effective Jul 18, 2006 - [AD 96-01-01](https://openairdocs.org/ad/96-01-01) (historical): Blade Taper Bore · Hamilton Standard Division 14RF-19, 14RF-21, 14RF-9 and 9 more. Effective Jan 19, 1996 - [AD 95-05-03](https://openairdocs.org/ad/95-05-03) (historical): Blade · Hamilton Standard Division 14RF-19, 14RF-21, 14RF-9 and 10 more. Effective Mar 23, 1995 - [AD 94-09-06](https://openairdocs.org/ad/94-09-06) (historical): Blade Taper Bore · Hamilton Standard Division 14RF-19, 14RF-21, 14RF-9 and 9 more. Effective May 2, 1994 - [AD 95-18-06 PL](https://openairdocs.org/ad/95-18-06-PL) (historical): Blade Taper Bore · Hamilton Standard Division 14RF-19, 14RF-21, 14RF-9 and 9 more - [AD 95-18-06 R1](https://openairdocs.org/ad/95-18-06-R1) (historical): Blade Taper Bore · Hamilton Standard Division 14RF-19, 14RF-21, 14RF-9 and 9 more - [AD T91-11-51](https://openairdocs.org/ad/T91-11-51) (historical): Loss of control of the propeller system · Hamilton Standard Division 6/5500/F-1, 14RF-19, 14RF-21 and 5 more - [AD T95-18-51](https://openairdocs.org/ad/T95-18-51) (historical): Blade Taper Bore · Hamilton Standard Division 14RF-19, 14RF-21, 14RF-9 and 9 more ## STCs approved under this data sheet (1) - [STC SP00660SE](https://openairdocs.org/stc/SP00660SE): Installation of SMR electrothermal propeller deicer SMR802259-2 as a replacement for Safety electrothermal propeller decier Safeway 802259SW-2.. 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