# TCDS P19NE: MT-Propeller Entwicklung GmbH - Type: Type certificate data sheet - Status: Current - Holder: MT-Propeller Entwicklung GmbH - Revision: 8 - Revised: July 8, 2021 - Product: Propeller - Certification basis: Part 21, Part 35 - Data sheet PDF: https://openairdocs.org/files/sha256/8c/e2/8ce22f5a76a210fed382a6b10c613b6bd1adc02cef384a6b8986a5904d8a9989 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/65F15764601662218625870C00615523.0001 - Page: https://openairdocs.org/tcds/P19NE ## Models (1) As the data sheet lists them. - MTV-6-( ) ## 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 5 6 7 Rev 7 7 7 7 8 6 6 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET P19NE TCDS NUMBER P19NE REVISION: 8 MT-PROPELLER COMPANY MODEL: MTV-6-( ) DATE: July 8, 2021 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P19NE) 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 MT -Propeller Entwicklung GmbH Flugplatzstrasse 1 D-94348 Atting Germany TYPE Hydraulic constant speed propeller (See Note 3) ENGINE SHAFT See Note 1 of this TCDS HUB MATERIAL Aluminum alloy BLADE MATERIAL Laminated wood composite structure, composite fiber cover, with leading edge and erosion protection HUBS See Note 1 of this TCDS UMBER OF BLADES 3 (three) DESIGN SERIES MTV-6-A, -C, -D, -F, -P, -R HUB- TYPE MTV-6 See Note 1 BLADES See Notes 2 & 6 MAXIMUM CONTINUOUS NOMINAL DIAMETER Max Min BLADE TWIST *) APPROXI- MATE WEIGHT **), ***) HP(kW) RPM HP (kW) RPM inch cm inch cm Min Max lbs. kg -3 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -4 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -5 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 P19NE Page 2 of 7 -6 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -7 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -8 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -9 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -12 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -16 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -23 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -28 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -31 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -49 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 P19NE Page 3 of 7 -51 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -64 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -69 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -80 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -81 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -106 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -112 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -122 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -123 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -125 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 P19NE Page 4 of 7 -129 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 -312 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 160 (120) 180 (134) 135 (101) 153 (114) 177 (132) 2800 2700 2500 2300 2300 69 63 75 75 80 175 160 190 190 203 55 55 55 55 55 140 140 140 140 140 5 5 5 5 5 50 50 50 50 50 30.9 30.9 30.9 30.9 30.9 14 14 14 14 14 *) The limits of the blade twist are defined between .20 and 1.00 blade radius. **) Propellers with the option “Feather” are 7.7 lbs. (3.5 kg) heavier. ***) Propellers with the option “Feather and Reverse” are 9.9 lbs. (4.5 kg) heavier. CERTIFICATION BASIS The U.S. certif ication basis determined under Section 21.29 of the FAR and Bilateral Airworthiness Agreement between the United States and the Federal Republic of Germany is FAR 35, effective February 1, 1965, Amendments 35-1 to 35-7, inclusive. European Aviation Safety Agency (EASA) type certificated this propeller under type certificate EASA P.094. The FAA validated this product under U.S. Type Certificate Number P19NE. 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. 32.130/57, EA SA Type Certificate P.094 since March 14, 2007 TC APPLICATION DATE 10/21/88 TC ISSUED 10/22/89, Revised 08/15/00, 10/15/03, 07/12/05, 03/02/07, 06/19/07 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 P19NE) 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. P19NE Page 5 of 7 NOTES NOTE 1: HUB MODEL DESIGNATION MT V - 6 - F - ( ) - ( ) - ( ) - ( ) - ( ) Small letter: modifications which do not affecting interchangeability Capital letter: modifications which restrict or exclude interchangeability Information about reverse system M: System Mühlbauer Information about reverse Blank: no reverse possible R: reverse system installed Information about feathering Blank: no feathering possible F: feathering system installed Letter designating counterweights: Blank: None or small counterweights for pitch change moments towards low pitch C: Counterweights for pitch change moments towards high pitch Engine Shaft (Flange Type) * Number of basic model Variable pitch propeller MT-Propeller Entwicklung GmbH *Engine shaft (Flange type) A = Bolt circle diameter = 80 mm, 7/16” mounting bolts C = AS-127-D, SAE No, 2 mod., 7/16” mounting bolts D = ARP 502, Type 1 F = AS-127D, SAE No. 1 mod, 3/8” mounting bolts P = Identical to D-Flange except without dowels and uses pilot bore of A-Flange for centering R = Identical to A-Flange except uses 1/2" mounting bolts P19NE Page 6 of 7 NOTE 2: BLADE MODEL DESIGNATION ( ) ( ) 170 - 09 - ( ) Small letter: modifications which do not affecting interchangeability of blade sets Capital letter: modifications which restrict or exclude interchangeability of blade sets Number of blade design, contains construction and aerodynamic data Propeller diameter in cm Sense of rotation (viewed in flight direction) Blank: righthand tractor RD: righthand pusher L: lefthand tractor LD: lefthand pusher Position of pitch change pin Blank: Position for pitch change forces to decrease pitch C: Position for pitch change forces to increase pitch CR: Position for reverse (pitch change forces to increase pitch) CF: Position for feather (pitch change forces to increase pitch) CFR: Position for feather and reverse (pitch change forces to increase pitch) NOTE 3: Pitch Control: Pitch cont rol is accomplished by a standard governor or by the MT-Propeller Hydraulic Propeller Governor Installation, P-480-( ) or P-9( ) ( )-( ) for the reversing option – R(M). Applicable standard governors are published in the FAA-approved list MT-Propeller Service Bulletin No. 14. The P-480-( ) or P-9( ) ( )-( ) is a single acting pump governor, but dual pressure system design enables the hydraulically variable pitch MT-propellers to operate with reverse capability. The P-480-( ) or P-9( ) ( )-( ) governor also incorporates feathering capability. Time Between Overhauls (TBO) for the P-480-( ) or P-9( ) ( )-( ) governor is published in MT-Propeller Service Bulletin No. 1( ). NOTE 4: (a) Feathering: Model incorporates feathering and unfeathering features by means of counterweights and springs with governor operation of P-480-( ) or P-9( ) ( )-( ) governor. (b) Reversing: Model incorporate reversing feature by P-480-( ) or P-9( ) ( )-( ) with additional functions. NOTE 5: Right & Left Hand Models: A version of the approved model with opposite hand rotation is approved at the same rating and diameter limitations. NOTE 6: Interchangeability: See NOTE 1 and NOTE 2. P19NE Page 7 of 7 NOTE 7: Accessories: (a) Propeller Spinners: According to FAA-approved list published in MT-Propeller Service Bulletin No. 13. (b) Propeller Governors: According to FAA-approved list published in MT-Propeller Service Bulletin No. 14. (c) Deicing Systems: According to FAA-approved list published in MT-Propeller Service Bulletin No. 15. NOTE 8: Shank Fairings: Not applicable. NOTE 9: Special Limits: Not applicable. NOTE 10: Special Notes: (a) Aircraft installations must be approved as part of the aircraft type certificate and demonstrate compliance with the applicable aircraft airworthiness requirements. (b) All MTV-6 propellers are to be operated within the limits of MT-Propeller Operation and Installation Manual No. E-124 for non reversible propeller and, E-504 for reversible propeller, and adhere to the TBO-limits shown in MT-Propeller Service Bulletin No. 1( ). (c) Propeller Maintenance, on overhaul, and airworthiness limitations shall be accomplished in accordance with MT-Propeller Overhaul Manual E-220 for non reversible propeller and E- 519 for reversible propeller, latest revision. NOTE 11: 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 (2, in force first) - [AD 2007-26-13](https://openairdocs.org/ad/2007-26-13): Propeller blades · MT-Propeller Entwicklung MT( )( )( )-1( ), MT( )( )( )-2( ), MT( )( )( )-3( ) and 27 more. Effective Jan 31, 2008 - [AD 2006-05-05](https://openairdocs.org/ad/2006-05-05) (historical): Propeller blades · MT-Propeller Entwicklung MTV-1-( ), MTV-12-B, MTV-12-C and 17 more. Effective Apr 10, 2006 --- 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.