TCDS P00035BO

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET P00035BO TCDS NUMBER: P00035BO REVISION: Basic Avia Propeller LTD. Model: AV-803 Date: May 16, 2016 Propellers of models described herein confirming with this data sheet (which is part of this Type Certificate No. P00035BO) and other approved data on file with the Federal Aviation Administration, meet s the minimum standards for use in certified aircraft in accordance with pertinent aircraft data sheet s 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 Avia Propeller LTD. Beranovych 65/666 199 00 Prague 9 - Letnany Czech Republic TYPE Hydraulic variable pitch, constant speed, feather, reverse propeller Engine Flange See Note 1 Hub Material Aluminum Alloy Blade Material Aluminum Alloy Number of blades 3 (Three) Hub Models see NOTE 1 Design Series AV-803 Hub- Type BLADES (see NOTES 2 & 6) Maximum Continuous HP (kW) RPM * Turbine Installation ** Piston Installation <Takeoff> HP (kW) RPM * Turbine Installation ** Piston Installation Diameter Limits Inch (cm) Approx. Max Wt. Complete (For Reference Only) AV-803-1 ( ) - 412 ( ) - 420 ( ) - 422 ( ) - 423 777* 2080* (580) 360** 1941** (269) 777* 2080* (580) 360** 1941** (269) 98.4 (250) 106.3 (270) 92.9 (236) 83.9 (213) 143 lb. (65 kg) Certification Basis: The U.S. certification basis determined under 14 CFR, § 21.29 and Bilateral Airworthiness Agreement between the United States and the European Aviation Safety Agency is 14 CFR Part 35, effective December 28 , 1995, Amendments 35-1 to 35-7, inclusive. TC (Import) No: EASA Type Certificate P.019 TC Application Date: March1, 2016 TC Issued: May 16, 2016 Page No. 1 2 3 4 5 Rev. No. - - - - - TCDS P00035BO Page 2 of 5 Import Requirements: To be considered eligible for installation on U.S. registered aircraft, each propeller imported into the United States must be accompanied by a certificate of airworthiness for export or a certifying statement endorsed by the exporting cognizant ci vil airworthiness authority . Include the following language in the certifying statement: (1) This propeller conforms to its United States type des ign (Type Certificate Number P00035BO) and is in a condition for safe operation, and (2) The manufacturer has performed a final operation check on this propeller, and it is in a proper state of airworthiness 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. Production Basis: Production Number: CZ.21G.0011 : TCDS P00035BO Page 3 of 5 NOTES NOTE 1: Hub Model Designation A V – 803 – 1 – E – ( ) – ( ) – ( ) – ( ) – ( ) 1 2 3 4 5 6 7 8 9 10 11 Hub 1 Avia Propeller (manufacturer) 2 V – Variable Pitch Propeller 3 Blade Root Type 4 Number of Blade 5 Number of variant of the propeller model 6 Code letter for flange type B = AS 127D, SAE No. 2 mod., ½ inch-20 UNF bolts D = ARP 502 E = ARP 880 K = M14 Flange 7 Code letter for counterweights blank = no or small counterweights for pitch change forces to decrease pitch C = counterweights for pitch change forces to increase pitch 8 Code letter for feather provision blank = no feather position possible F = feather position installed 9 Code letter for reverse provision blank = no reverse position possible R = reverse position installed 10 Code letter for reverse system W = System Walter 11 Code letter for design changes small letter for changes which do not affect interchangeability capital letter for changes which restrict or exclude interchangeability TCDS P00035BO Page 4 of 5 NOTE 2: Blade Model Designation ( ) ( ) 270- 420 ( ) 1 2 3 4 5 Blade 1 Code letter for position of pitch change pin blank = pitch change pin position for pitch change forces to decrease pitch C = pitch change pin position for pitch change forces to increase pitch CF = pitch change pin position for feather provision; pitch change forces to increase pitch CR = pitch change pin position for reverse provision; pitch change forces to increase pitch CFR = pitch change pin position for feather and reverse provision; pitch change forces to increase pitch 2 Code letter for blade design and Installation blank = right-hand tractor RD = right-hand pusher L = left-hand tractor LD = left-hand pusher 3 Propeller diameter in cm 4 Number of blade type (contains design configurations and aerodynamic data) according to the certified hub/blade - combinations 5 Code letter for design changes small letter for changes which do not affect interchangeability of blade set capital letter for changes which restrict or exclude interchangeability of the blade set Note 3: Pitch Control (a) The propellers are approved for flight operation with the propeller speed governors which are listed in Avia Propeller Service Bulletin No. 3 (b) The propellers are approved for flight operation with the propeller overspeed governors which are listed in the appropriate propeller parts list Note 4: Feathering and Reversing (a) The propellers incorporate feathering and unfeathering features when equipped with appropriate mounted instruments (see Note 3 and 7). Blade Feathering is accomplished by: (1) by oil pressure (2) by outweighing moment of counterweights (b) The propellers incorporate reversing feature when equipped with appropriate mounted instruments (see Note 3). Note 5: Left-hand Models The left-hand version of the approved propeller model is eligible at the same rating and diameter limitations as listed for the right-hand model. Note 6: Interchangeability Not applicable Note 7: Accessories (a) Propeller spinners: According to the FAA-approved list published in Avia Propeller Service Bulletin No.2. (b) Propeller accessories including governors: According to the FAA-approved list published in Avia Propeller Service Bulletin No. 3. (c) Propeller de-icing: According to the FAA-approved list published in Avia Propeller Service Bulletin No. 4. TCDS P00035BO Page 5 of 5 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 AV-803 propellers are to be operated within the limits of Avia Propeller Operation and Installation Manuals No. EN-1320, EN-1366 and adhere to the TBO limits shown in Service Bulletin No. 1. (c) Propeller maintenance, overhaul, and airworthiness limitations shall be accomplished in accordance with Avia Propeller Overhaul Manuals No. EN-1291, EN-1367 and EN-1370 latest revision. Note 11: Special Limits Airworthiness Limitations shall be complied with as given in the approved Airworthiness Limitation Section of the Avia Operation and Installation Manuals EN-1320, EN-1366, Overhaul Manuals EN-1291, EN-1367 and Overhaul Manual for Metal Blades EN-1370. The propeller CMACO must evaluate the propeller installation for each new aircraft installation to assess possible changes in the airworthiness limitations. -- END --