# TCDS P6NE: Hoffmann GmbH & Co. KG - Type: Type certificate data sheet - Status: Current - Holder: Hoffmann GmbH & Co. KG - Revision: 2 - Revised: March 12, 2007 - Product: Propeller - Certification basis: Part 21, Part 35 - Data sheet PDF: https://openairdocs.org/files/sha256/5a/c0/5ac0c445f646ecfa4e9f69a31efc589bb016c0e225df8d9fb91b4dc11ffbff34 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/460300476FDCBDC88625729F006C2802.0001 - Page: https://openairdocs.org/tcds/P6NE ## Models (8) As the data sheet lists them. - HO 4/23 ( ) HM - HO 4/23 ( ) - HO 4/14 ( ) HM - HO 4/27 ( ) - HO 4/27 ( ) HM - HO 4/14 ( ) - HO 4/50 ( ) - HO 4/50 ( ) HM ## 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 REV. 2 2 2 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET P6NE P6NE REVISION NUMBER: 2 HOFFMANN MODEL/S: HO 4/27 () HO 4/27 () HM HO 4/23 () HO 4/23 () HM HO 4/14 () HO 4/14 () HM HO 4/50 () HO 4/50 () HM March 12, 2007 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P6NE) 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 Hoffmann GmbH & Co.KG Kuepferlingstr. 9 D-83022 Rosenheim Federal Republic of Germany TYPE Single piece, fixed-pitch, four-bladed with metal tipping MATERIAL Laminated hard wood NUMBER OF BLADES Four DESIGN SERIES HO 4/27(), HO 4/27()HM, HO 4/23(), HO 4/23()HM, HO 4/14(), HO 4/14()HM, HO 4/50(), HO 4/50()HM MODEL (See Note 2) TAKEOFF & MAX CONT SHP RPM DIA STD. PITCH < HUB DRILLING > NO. OF DIA. OF DIA OF HOLES HOLES BOLT CIRCLE HUB DIMENSION DIA THICKNESS (MINIMUM) APPROX WEIGHT (LBS) HO4/27( )HM 181 2,700 69" 35 - 71" 6 1/2" 4.75" 7.9" 3.9" 23.0 H04/27( ) 181 2,700 69" 35 - 71" 6 1/2" 4.75" 7.9" 3.9" 23.0 HO4/23( )HM 164 2,700 69" 35 - 71" 6 3/8" or 7/16” 4.75" 7.9" 3.5" 22.0 HO4/23( ) 164 2,700 69" 35 - 71" 6 7/16" or 3/8” 4.75" 7.9" 3.5" 22.0 HO4/27( )HM 295 2,575 73" 35 - 71" 6 1/2" 4.75" 8.5" 4.5" 30.0 HO4/27( ) 295 2,575 73" 35 - 71" 6 1/2" 4.75" 8.5" 4.5" 30.0 HO4/14( )HM 101 2,750 65" 20 - 63" 6 3/8" 4.3/8" 7.0" 3.5" 15.5 H04/14( ) 101 2,750 65" 20 - 63" 6 3/8" 4.3/8" 7.0" 3.5" 15.5 HO4/50( )HM 213 2,600 73" 24 - 75" 8 7/16" 6.0" 8.5" 5.0" 30.0 HO4/50( ) 213 2,600 73" 24 - 75" 8 7/16" 6.0" 8.5" 5.0" 30.0 HO4/50( )HM 235 2,575 75" 24 - 75" 8 7/16" 6.0" 8.5" 4.5" 30.0 HO4/50( ) 235 2,575 75" 24 - 75" 8 7/16" 6.0" 8.5" 4.5" 30.0 HO4/27( )HM 235 2,575 75" 35 - 71" 6 1/2” 4 3/4" 7.9" 3.9" 30.0 HO4/27( ) 235 2,575 75" 35 - 71" 6 1/2” 4 3/4” 7.9" 3.9" 30.0 HO4/27( )HM 268 2,600 73" 35 - 71" 6 1/2" 4 3/4” 7.9" 3.5" 30.0 HO4/27( ) 268 2,600 73" 35 - 71" 6 1/2” 4 3/4” 7.9" 3.5" 30.0 Page 2 TCDS P6NE CERTIFICATION BASIS: FAR 21.29, FAR 35 effective February 1, 1965, with Amendments 35-1 to 35-4. Luftfahrt-Bundesamt (LBA) originally type certificated this propeller under its type certificate Number 32.110 / 011. The FAA validated this product under U.S. Type Certificate Number P6NE. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of the Federal Republic of Germany. TC (IMPORT) NO LBA-Data Sheet No. 32.110 / 011, , September 25, 1980, to issue 5 dated November 22, 1994 TC APPLICATION DATE: January 23, 1984 TC ISSUED: May 24, 1984 IMPORT REQUIREMENTS: To be considered eligible for installation 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 LBA on behalf of the European Community which contains the following language: (1) This propeller conforms to its United States type design (Type Certificate Number P6NE) 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. Page 3 TCDS P6NE NOTES NOTE 1. INSTALLATION Installation is to be made with special steel bolts and with/without spacers as required which are either furnished or specified by the propeller manufacturer. NOTE 2: MODEL DESIGNATION: Blank = righthand, tractor D = righthand, pusher Pitch at 0.75 radius measured in cm Basic model = Hoffmann HO 4 / 27( ) ( ) -170 ( ) 128 ( ) L = lefthand, tractor LD = lefthand, pusher Pitch at 0.75 radius measured Blank = normal blade S = narrow blade B = wide blade Propeller diameter in cm Blank = hardwood HM= hardwood fibre reinforced plastic covering(glass fibre, carbon fibre, kevlar, Key number for hub connection (according to list of manufacturer) Number of blades every 50 hours or less, a torque moment check of attaching bolts is required as specified by the propeller manufacturer. - -E N D- - NOTE 3: After first flight, after the first 25 hours and then or hybrid) NOTE 3. Service Information: Each 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 LBA. 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 (1, in force first) - [AD 2000-04-10](https://openairdocs.org/ad/2000-04-10): Propeller Mounting Bolts · Hoffmann HO 27 HM, HO 4/27 ( ) and HO 4/27 ( ) HM. Effective Mar 9, 2000 ## STCs approved under this data sheet (1) - [STC SP01222WI](https://openairdocs.org/stc/SP01222WI): Installation of Aircraft Development propeller vortelators.. Aircraft Development Co --- 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.