# STC SA02486LA - Type: Supplemental type certificate - Status: Current, Reissued - Holder: SMR Technologies Inc - Description: Replacement of Socata Leading Edge Assemblies and Pneumatic Deicer - Status date: March 19, 2019 - Data sheets: A60EU - Certificate PDF: https://openairdocs.org/files/sha256/4d/9a/4d9a190fe3f6010b4ff90deb61ea1ab07c7aee2941d41f33bb2ad0d54f868799 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B507B852AFA6D232862585A4003E1AF0.0001 - Page: https://openairdocs.org/stc/SA02486LA ## ADs that name it None. ## Approved models (1) - DAHER AEROSPACE TBM 700 (TCDS A60EU) ## 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 (5/14) Page 1 of This certificate issued to: Part of the Original Product – Type Certificate Number: Make: By Direction of the Administrator Signature Title March 19, 2019 Anthony E. Gallo Manager New York ACO Branch SMR Acquisition, LLC. dba SMR Technologies, Inc. 93 Nettie Fenwick Road Fenwick, WV 26202 SA02486LA Federal Aviation Regulations. 1. Replacement of Socata Leading Edge Assemblies and Pneumatic Deicer in accordance with the FAA Approved SMR Technologies’ Master Drawing List No. MDL-0063, Revision “R” dated May 16, 2018 or later FAA approved revision. 2. This modification must be Maintained in accordance with the Instructions for Continued Airworthiness (ICA), Document No. 11-33-070, Revision 4, dated April 16, 2018. 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person evidence of that permission. 3. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft. DAHER AEROSPACE TBM 700 June 18, 2018 February 4, 2011 December 12, 2013 A60EU 3 FAA Form 8110-2 (5/14) Page 2 of To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): 3 SA02486LA FAA Form 8110-2 (5/14) Page 3 of 3 Date reissued: March 19, 2019 Certification Basis: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for changes that are not significant in FAA Order 8110.48, the certification basis for these modifications are as follows: a. The type certification basis for parts not changed or not affected by the change is shown on TCDS No. A60EU. b. The modification certification basis for parts changed or affected by the change since amendment application date, June 1, 2016, is based on the amendment level in TCDS No. A60EU. ----------END---------- SA02486LA ## Every issue (2) - March 19, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/4d/9a/4d9a190fe3f6010b4ff90deb61ea1ab07c7aee2941d41f33bb2ad0d54f868799) - December 12, 2013: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/5f/d3/5fd3beba8b5f8958f5c4a072b1c87233e7a0ad2ab80a7abb3b9079640b431c90) --- 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.