# TCDS P19EA: Hamilton Standard Division - Type: Type certificate data sheet - Status: Current - Holder: Hamilton Standard Division - Revision: 5 - Revised: September 30, 1977 - Product: Propeller - Certification basis: CAR 14 - Data sheet PDF: https://openairdocs.org/files/sha256/28/90/2890261aa26d9a69c86674c38df2983f2b6aca188c25bddc7a6ced605cd3b3a0 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BC71057056561F058525670F006C9864.0001 - Page: https://openairdocs.org/tcds/P19EA ## Models (3) As the data sheet lists them. - 63E60 - 63EX - 63E50 ## 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 No. 1 2 Rev. No. 5 5 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P19EA Revision 5 HAMILTON STANDARD 63E September 30, 1977 TYPE CERTIFICATE DATA SHEET NO. P19EA Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P19EA) 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 Civil Air Regulations/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 Standard Division United Technologies Corporation Windsor Locks, Connecticut 06096 Type Hydraulically controllable feathering (see Notes 3 and 4) Engine shaft SAE No. 50, 60 or X (X indicates special shaft sizes for foreign installations are eligible.) Hub material Steel Blade material Aluminum alloy Number of blades 3 Hubs eligible 63E50, 63E60, and 63EX (see Note 1) Blades Eligible Maximum Continuous Takeoff Diameter Limits Hub and Blade Weight (See Note 2) HP RPM HP RP M (See Note 2) (Max. Diameter) NOTES 7139-0 to 7139-24 2785 1160 3135 1160 14' 6" - 12' 6" (-0 to -24) 611 lbs. 7140 is the left-hand version of 7139. 5 Certification basis CAR 14 as amended May 3, 1962. Type Certificate No. P19EA issued November 25, 1964. Date of application for Type Certificate July 8, 1963. Production basis Production Certificate No. 14 NOTE 1. Hub Model Designation 6 3 E 60 - 11 Configuration changes (see Note 11.). SAE propeller shaft size Blade shank size Number of blades Major model type P19EA 2 NOTE 2. Blade Model Designation A 7139 B - C Nominal reduction from basic diameter in inches. Operational features (may indicate particular deicing assembly), does not affect eligibility. Aerodynamic and structural features (If used) indicates shank fairing design. Diameter limits shown are nominal diameters of the assembled propeller and do not include the ± 1/8 inch manufacturing tolerance permissible for propellers with basic diameter less than 14 feet or ± 1/4 inch permissible for propellers with basic diameter 14 feet or larger. NOTE 3. Pitch Control. (a) Eligible with Hamilton Standard constant speed control. (b) Eligible with Hamilton Standard direct blade angle (BETA) control. NOTE 4. (a) Feathering. Eligible with full feathering controls installed in accordance with the propeller manufacturer's instructions. (b) Reversing. Eligible with reversing controls installed in accordance with the propeller manufacturer's instructions. NOTE 5. Left Hand Models. The left-hand version of an approved model propeller is eligible at 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. (1) Electric. Eligible only with Hamilton Standard Electric deicing equipment installed in accordance with the propeller manufacturer's instructions.** (2) Fluid. Not applicable. (b) Propeller Spinner. Eligible with spinner supplied by Hamilton Standard. **All rubber deicing accessories shall be installed in accordance with Hamilton Standard instructions regarding the cementing sequence for adhering rubber accessories to aluminum alloy blades. NOTE 8. Shank Fairings. Not applicable. NOTE 8. Special Limits. Not applicable. 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. NOTE 11. CONFIGURATION DIFFERENCES 63E60-11. Original certification propeller. Two low pitch stops and six bolt barrel. None flightworthy. 63E60-13. Same as -11 except three low pitch stops. 63E60-15. Same as -13 except nine bolt barrel. 63E60-17. Same as -15 except no provision for synchrophasing. 63E60-19. Same as -15 except has blade alignment gage provisions. 63E60-21. Same as -17 except has blade alignment gage provisions. 63E60-25. Same as -21 except only one low pitch stop and direct beta (blade angle) control for all operation below the low pitch stop. ....END.... ``` ## ADs None name its models. ## STCs approved under this data sheet (1) - [STC SP00582NY](https://openairdocs.org/stc/SP00582NY): Installation of Prop-Guard Polyurethane Protective Tape on the leading edge of metal propellers.. McFarlane Aviation, Inc. --- 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.