# TCDS P23NE: Airbus Poland S.A. - Type: Type certificate data sheet - Status: Current - Holder: Airbus Poland S.A. - Revision: 2 - Revised: August 16, 2022 - Product: Propeller - Certification basis: Part 21, Part 35 - Data sheet PDF: https://openairdocs.org/files/sha256/69/04/69045fba76890d700c9606fc827b66ac99df98760925723391af3b8f5ec244d9 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4A93FF8BCF0374E9862588A2004E6577.0001 - Page: https://openairdocs.org/tcds/P23NE ## Models (1) As the data sheet lists them. - US-133000 ## 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 3 Rev. No. 2 2 1 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET P23NE TCDS NUMBER P23NE REVISION: 2 Airbus Poland S.A. Model: US-133000 August 16, 2022 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate Number P23NE) 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 (TC) Holder: Airbus Poland Spolka Akcyjna Al. Krakowska 110/114 02-256 Warsaw, Poland Type Certificate Holder Record Panstw owe Zaklady Lotnicze "PZL-Warszawa-Okecie Transferred TC P9EU to Airbus Poland S.A. on June 29, 2022 Type Constant Speed; Hydraulic (see Notes 3 and 4). Engine Flange PZL DRG. Hub Material Steel Blade Material Aluminum Alloy Number of Blades 4 Design Series US-133000 APPROX MAXIMUM Blades MAXIMUM CONTINUOUS < T AKEOFF > NOMINAL WEIGHT COMPLETE (See Note 2) HP RPM HP RPM DIAMETER (Reference Only) US-133500 550 1,435 600 1,540 122" 230 LB (404kw) (445kw) (310 cm) (104kg) Certification basis The U.S. certifi cation basis determined under Section 21.29 of the 14 CFR Part 21 and Bilateral Airworthiness Agreement between the United States and the Polish Central Administration of Civil Aviation (CACA) is FAR 35, effective February 1, 1965, Amendments 35-1 to 35-5, inclusive. The FAA validated this product under U.S. Type Certificate Number P23NE. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of the Polish People's Republic. TC (Import) No. None TC Application Date January 10, 1985 TC Issued January 15, 1991 TC Reissued August 16, 2022 Import requirements: To be considered eligible for in stallation on U.S. registered aircraft, each propeller to be exported to the United States shall be accompanied by a Certificate of Airworthiness for export endorsed by the Polish People's Republic on behalf of the European Community which contains the following language: P23NE 2 (1) This propeller conforms to its United States type design (TC No. P23NE) and is in a condition for safe operation. (2) This propeller has been subjected by the manufacturer to a final operational check and is in a proper state of airworthiness. Reference FAR Section 21.500 which provides for the airworthiness acceptance of aircraft engines or propellers manufactured outside The U.S. for which a U.S. type certificate has been issued. Additional guidance is contained in FAA Advisory Circular 21-23, Airworthiness Certification of Civil Aircraft, Engines, Propellers and Related Products, Imported into the United States. NOTES Note 1. Propeller Model Designation. The serialized number of a complete PZL pr opeller assembly constitutes a model designation. U S - 133 000 / A Suffix denotes major alterations Digits reserved for part numbers (000 - assembly / 500 - blade) Basic model designation Propeller Device NOTE 2. Blade Model Designation: PZL propeller blades ar e identified by a serialized part number only (see Note 1). NOTE 3. Pitch control PZL Gover nor 0719-812-008. (anti clockwise) NOTE 4. (a) Feathering Not applicable (b) Reversing Not applicable NOTE 5. These propellers are designed and manufactured for left hand tractor only. NOTE 6. Interchangeable Blades: Only blades of the same part numbers are interchangeable and may be incorporated in the same propeller. NOTE 7. Accessories (a) Propelle r deicing: Not applicable (b) Spinners: Not applicable NOTE 8. Blade Shank Cuffs Not applicable NOTE 9. Special Limits The propellers listed in this certificate are approved from a vibration standpoint only for use in the engine aircraft combination listed below: PROPELLER MODEL ENGINE MODEL AIRCRAFT MODEL PLACARDS US-133000 PZL-3SR PZL-106 "KRUK" Avoid Continuous Operation (PEZETEL) between 1700 and 1800 RPM. NOTE 10. Special Notes: Aircraft installations must be approved as part of the aircraft type certification and demonstrate compliance with the applicable aircraft airworthiness requirements. 3 P19NE NOTE 11. Service Information. E ach of the documents listed below must state that it is approved by the European Aviation Safety Agency (EASA) or – for approvals made before September 28, 2003 – by the Polish People's Republic. Any such documents are accepted by the FAA and are considered FAA approved. • Service bulletins, • Structural repair manuals, • Vendor manuals, • Aircraft flight manuals, and • Overhaul and maintenance manuals. .....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.