TCDS P00036BO

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET P00036BO TCDS NUMBER: P00036BO REVISION: 1 MT PROPELLER COMPANY MODEL: MTV-20 – ( ) DATE: August 20, 2018 Propellers of models described herein confirming with this data sheet (which is part of this Type Certificate No. P00036BO) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certified 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 approved manufacturer’s manual and other approved instructions. TYPE CERTIFICATE HOLDER MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting Germany TYPE Constant speed, Electrical control (See Notes 3 & 4) ENGINE SHAFT See Note 1 of this TCDS HUB MATERIAL Aluminum alloy BLADE MATERIAL Laminated wood composite structure, composite fiber cover, with leading edge erosion protection HUBS: See Note 1 of this TCDS NUMBER OF BLADES 2 (two) DESIGN SERIES MTV-20-B, -C, -D, -AA HUB- TYPE MTV-20 See Note 1 BLADES See Notes 2 & 6 MAXIMUM CONTINUOUS <TAKE OFF> NOMINAL DIAMETER Max Min BLADE TWIST *) APPROXI- MATE WEIGHT **) HP(kW) RPM HP(kW) RPM inch (cm) inch (cm) Min Max lbs. (kg) -02, -11, -14, -15, -18, -20, -21, -22, -25, -26, -27, -29, -33, -34, -35, -37, -42, -43, -45, -46, -50, -52, -55, -58, -61, -62, -63, -65, -66, -67, -102, -103, -104, -109, -121 300 (224) 300 (224) 2700 2200 300 (224) 300 (224) 2700 2200 83 102 (210) (260) 69 69 (175) (175) 5 5 50 50 46 46 (21) (21) *) The limits of the blade twist are defined at 75% blade radius **) MTV-20-AA approximate weight 54 lbs (24.5kg) Page No. 1 2 3 4 Rev. No. 1 1 1 basic TCDS P00036BO Page 2 of 4 CERTIFICATION BASIS: The U.S. certification 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 35-5 , inclu sive for MTV -20-B, Amendments 35-1 to 35-6 inclusive for MTV-20-C and MTV-20-D and Amendments 35-1 to 35-6 inclusive except 35- 39 which is replaced with CS -P 390 amendment 1 dated 16 November 2006 for MTV-20-AA. Luftfahrt-Bundesamt (LBA) originally type certificated this propeller under certificate number 32.130/ 68. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of Germany. EASA issued Type Certificate P.100 for the MTV -20 series propeller. TC (IMPORT) NO. P00036BO TC APPLICATION DATE: September 21, 2017 TC ISSUED November 8, 2017 PRODUCTION BASIS: EASA Production Organization Approval: DE.21G.0008 IMPORT REQUIREMENTS: To be considered eligible for installation on U.S. registered ai rcraft, each propeller to be exported to the United States shall be accompanied by a certificate of airworthiness for export or certifying statement endorsed by the exporting cognizant civil airworthiness authority which contains the following language: (1) This propeller conforms to its United States type design (Type Certificate Number P00036BO) 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 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. TCDS P00036BO Page 3 of 4 NOTES NOTE 1: HUB MODEL DESIGNATION: MT V - 20 - ( ) - ( ) ( ) Small letter: modifications which do not affect interchangeability Capital letter: modifications which restrict or exclude interchangeability Blank: No or small counterweights for pi tch change forces towards fine pitch C: Counterweights for pitch change forces towards high pitch Flange Type * Number of basic model Variable pitch propeller MT-Propeller Entwicklung GmbH * Flange B = AS-127-D, SAE No. 2 mod., 1/2” mounting bolts C = AS-127-D, SAE No. 2 mod., 7/16” mounting bolts D = ARP 502 Type 1 AA = Flange mount for adapter to SAE No. 20 spline NOTE 2: BLADE MODEL DESIGNATION: ( ) 183 - 58 ( ) Small letter: modifications which do not affect 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: right-hand tractor RD: right-hand pusher L: left-hand tractor LD: left-hand pusher TCDS P00036BO Page 4 of 4 NOTES CONTINUED NOTE 3: Pitch Control: Pitch control is accomplished by Control Unit P-120-M (manual) or Control Unit P-120-U (universal (selectable automatic, constant speed & manual control)) or Control Unit P-120-A (automatic (constant speed)) For the control units no TBO or life limits are specified. Service is on condition. NOTE 4: (a) Feathering: Electrical control per Control Units P -120-M, P-120-U and P-120-A (b) Reversing: Not applicable NOTE 5: Right & left hand Models: A version of the approved model wi th opposite hand rotation is approved at the same rating and diameter limitations NOTE 6: Interchangeability: See NOTE 1. 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-20 propellers must be operated within the limits of MT-Propeller Operation and Installation Manual No. ATA 61-01-18 (E-118) and adhere to the TBO-limits shown in Service Bulletin No. 1( ). (c) Propeller Maintenance, or overhaul, and airworthiness limitations shall be accomplished in accordance with MT-Propeller Overhaul Manual No. ATA 61-12-50 (E-250), 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 --