# STC SR02657LA - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Meeker Aviation Services Ltd, United States - Description: Installation of a Trakkabeam A800 Searchlight on the Aero Pacific AP407UM01 Aft Utility Mount (STC SR00891LA) of the affected helicopters - Applied: February 20, 2014 - Status date: January 17, 2018 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/6f/e8/6fe8c28bff2bf47b9070d10c18e34c06df6ed349f1f8b6d6b34268e425146f67 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D01DA32C1632BE968625821F004A8071.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR02657LA ## ADs that name it (0) None. ## Approved models (10) - Bell Helicopter Textron Canada Limited 206 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206A-1 (OH-58A) ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206B-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 407 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) ## 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. . Certification basis is set forth in Type Certificate Data Sheet H2SW Installation of a Trakkabeam A800 Searchlight on the Aero Pacific AP407UM01 Aft Utility Mount (STC SR00891LA) of the affected helicopters in accordance with Meeker Aviation Services, Ltd, Master Drawing List TRK-110, Revision C, dated November 22, 2017 or later FAA-approved revisions. The associated FAA Approved Rotorcraft Flight Manual Supplement #TRK-107, Revision IR, dated October 27, 2017, or later FAA-approved revisions; and FAA-approved Instructions for Continued Airworthiness #TRK-108, Revision 0, dated July 24, 2017, or later FAA-approved revisions are required. This installation should not be incorporated in any aircraft on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those previously approved modifications will introduce no adverse effect upon the airworthiness of the aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the disposable weight in the fuselage. 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. (Limitations and Conditions continued on page 3) Meeker Aviation Services, Ltd. 2608 Temple Heights Drive Oceanside, California 92056 H2SW Bell 206, 206A, 206B, 206B-1, 206L, 206L-1, 206L-3, 206L- 4 and 407 February 20, 2014 December 12, 2017 January 17, 2018 (Signature) Manager, Systems and Equipment Section, Los Angeles Aircraft Certification Office Branch (Title) Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street) (City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and Zip code) Extent of Authority (if licensing agreement): Signature of grantor (In ink): Limitations and Conditions Instructions for Continued Airworthiness (ICA), TRK-108, Revision 0, or later FAA-accepted revision must be made available to the operator at the time of installation. 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 Bell Models 206, 206A, 206B, 206B-1, 206L, 206L-1, 206L-3, 206L-4 and 407 Series is as follows: a. The type certification basis for Bell Model 206, 206A, 206B, 206B-1, 206L, 206L-1, 206L-3, 206L-4 and 407 series rotorcraft is shown on TCDS H2SW 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 application, February 20, 2014, is based upon part 27 as amended by Amendment 27-30. 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 this modification was determined to be: Regulations at the latest amendment 27-0 through 27-30: 27.301, 27.303, 27.305 27.307, 27.309, 27.321, 27.337, 27.339, 27.561, 27.601, 27.613, 27.619, .625[29-0], 27.1301, 27.1309, 27.1351, 27.1357, 27.1361, 27.1365, 27.1367, 27.1529, 27.1585 ----------END-------- ## Every issue (1) - January 17, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/6f/e8/6fe8c28bff2bf47b9070d10c18e34c06df6ed349f1f8b6d6b34268e425146f67) --- 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.