# STC SA02474LA - Type: Supplemental type certificate - Status: Current, Reissued - Holder: IKHANA Group Inc. - Description: Re-Life engine nacelles - Status date: November 18, 2020 - Data sheets: A9EA, A9EA, A9EA - Certificate PDF: https://openairdocs.org/files/sha256/97/75/9775124fef673d5990c4f9b3574bc8ce87fa8644b2eaf19794e0087c15bb2b43 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F8C6F1B6E2855C6E862586B6004F17BA.0001 - Page: https://openairdocs.org/stc/SA02474LA ## ADs that name it None. ## Approved models (3) - Viking Air Limited DHC-6-100 (TCDS A9EA) - Viking Air Limited DHC-6-200 (TCDS A9EA) - Viking Air Limited DHC-6-300 (TCDS A9EA) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 1 of 3 Number: SA02474LA IKHANA Group, LLC 37260 Sky Canyon Drive, Hangar 20 Murrieta, California 92563 Part 23 * of the Federal Aviation Regulations. *See Page 3. Original Product Make: Viking Air Limited Type Certificate Number: A9EA Model: DHC-6-100, DHC-6-200, DHC-6-300 Description of Type Design Change: Re-Life engine nacelles in accordance with IKHANA Aircraft Services Drawing List, Document No. ER218-1122, Revision B, dated July 15, 2013, or later FAA approved revision. Install and maintain RWMI DHC-6 Re-Life Nacelles in accordance with IKHAHA Aircraft Services Master Data List, Document No. ER218-1123, Revision NC, dated August 26, 2013, or later FAA approved revision. Limitations and Conditions: Approval of this modification applies to the above noted model airplane series only. This approval should not be extended to other specific airplanes of this model series on which other approved modification are incorporated, unless it is determined that the interrelations between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of the aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. A copy of this STC must be included in the permanent records of each airplane modified in accordance with this STC. (Continued on Sheet 3). Date of Application: April 20, 2012 Date Reissued: March 14, 2014; November 18, 2020 Date of Issuance: September 5, 2013 Date Amended: Title: Manager, Technical & Administrative Support Section Los Angeles ACO Branch FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 2 of 3 Number: SA02474LA United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA02474LA * Limitations and Conditions (Continued) RWMI DHC-6-Re-Nacelles are approved replacements for Viking Air Limited (formerly Bombardier Inc. or De Havilland Inc.) flight controls as listed below: Nacelle Assembly OEM Part Numbers IKHANA Part Number Nacelle Assy, LH C6W1500-11, C6W1500-15, C6W1500-19, C6W1500-23 NR00-W1500-101 Nacelle Assy, RH C6W1500-13, C6W1500-17, C6W1500-21, C6W1500-25 NR00-W1500-103 The safe life service limit of the RWMI DHC-6 Re-Life Nacelle assemblies is 45,000 hours or 90,000 flights, whichever occurs first, from the time in service. All Viking Air Limited, Bombardier Inc., or De Havilland Inc. Service Bulletins for nacelle assemblies also pertain to RWMI DHC-6 Re-Life Nacelle assemblies, as applicable. Any FAA Airworthiness Directives pertaining to Viking Air Limited, Bombardier Inc. or De Havilland Inc. flight control assemblies also pertain to RWMI DHC-6 Re-Life Nacelle assemblies, as applicable. Certification Basis Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the RWMI DHC-6 Re-Life Nacelles is as follows: a. The type certification basis for the DHC -6 series airplanes is shown in TCDS A9EA for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by the change since the reference date of the application, November 9, 2007, is based upon 14 CFR part 23 as amended by Amendment 23- 59. Based on 14 FR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be: Regulations at the latest amendment 23-0 through 23-59 23.29, 23.301, 23.303, 23.305, 23.307, 23.572, 23.574, 23.575, 23.601, 23.603, 23.605, 23.607, 23.609, 23.611, 23.613, 23.619, 23.623, 23.625, 23.627, 23.1529 ………………..END……………….. FAA Form 8110-2 (4/20) Page 3 of 3 ## Every issue (2) - November 18, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/97/75/9775124fef673d5990c4f9b3574bc8ce87fa8644b2eaf19794e0087c15bb2b43) - September 5, 2013: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/17/8d/178d5d8617ae455e301bbd167cb468b65e3c4bf03bd24c06fd8cfe4c3892286d) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.