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FAA STC category

Other aircraft modifications STCs

Current FAA supplemental type certificates outside the principal modification categories. This directory contains 11,384 selected records listed with status Current in the June 30, 2026 FAA DRS snapshot and links every entry to its source.

Showing 5,881–6,000 of 11,384Page 50 of 95
ST10890SC-DOther aircraft modifications

Aft RH Divan Installations in accordance with Data List Report No. F2EX-01038 Revision AG dated 14-Apr-2011, or later FAA approved revision. FAA Approved AFM Supplement, Report 40709-1 dated April 14, 2011 or later FAA approved revision is required. Instructions for Continue Airworthiness, Report ICA-F2EX-01038-501, revision Original, dated 21-Jan-2011 or later FAA approved revision is required.

FAA holder: Dassault Falcon Jet Corp.

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SA2543WEOther aircraft modifications

Installation of Hoskins Model 700801Anti-Collision Light in accordance with FAA sealed Master Eligibility List No. SA2543WE. While the requirements of FAR 23.1401(a), (c), (d), (e) and (f) are met by this installation, the requirements of FAR 23.1401(b) are not met. Since the aircraft was type certificated under airworthiness regulations that contained no Anti-Collision Light Standards for intensity and field of coverage, this installation is accepted. Hoskins FAA approved AFM Supplement (see MEL SA2543WE) is required with this modification.

FAA holder: BF Goodrich Aerospace

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SA2588WEOther aircraft modifications

A Hoskins Model MK III (Twilighter) Anti-Collision Lighting System is installed in accordance with Hoskins Top Drawing 10-0043-1, Revision I as amended on December 21, 1972, or later FAA approved revision. The Anti-Collision Lighting System has been found to meet the Anti-Collision Light Standards of FAR 25.1401 in effect prior to August 11, 1971. Hoskins FAA Approved AFM supplement date December 6, 1972 is required with this modification.

FAA holder: BF Goodrich Aerospace

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SA2630WEOther aircraft modifications

Installation of Hoskins (Pulstar TM) combined Position Anti-Collision Lighting System in accordance with FAA Sealed Hoskins Top Drawings No. 10-202186 or No. 10-202186-1. These Anti-Collision Lighting Systems have been found to meet the Anti-Collision Light Standards of FAR 23.1401, in effect of August 11, 1972. Hoskins FAA Approved AFM supplement dated December 27, 1972 or later FAA Approved Revision is required with this modification.

FAA holder: BF Goodrich Aerospace

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SA362CEOther aircraft modifications

Description of Type Design Change: Install Hoskins Twilighter MK III per Installation Manual and Specification Sheets as amended, dated September 20, 1965. Install Hoskins Twilighter MK IIIB Supplemental Lights per the following required data: Models 310 through 310F and 320 Specification Sheets P/N 65-0025-5 with drawings listed; Models 310G through N and 320-1 through F Specification Sheets P/N 65-0025-6 with drawings listed; Models 401, 401A and 402 Specification Sheets P/N 65-0025-9 with drawing listed; Models 411 and 411A Specification Sheets P/N 65-0025-7 with drawings listed; and Models 421 and 421A Specification Sheets P/N 65-0027-8 with drawings listed.

FAA holder: BF Goodrich Aerospace

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SR01991SEOther aircraft modifications

: Installation of the Mechanical Specialties Scupper Assembly, Part Number 300-101, in accordance with Installation Instructions, document # INST 300-101-100, Revision A, dated April 6, 2009, or later FAA approved revision. Manufactured in accordance with Master Document List 300-101-MDL, Revision A, dated April 9, 2009, or later FAA approved revision. Maintained in accordance with Instructions for Continued Airworthiness, document # 300-101-ICAW, Revision A, dated April 09, 2009, or later FAA approved revision.

FAA holder: Mechanical Specialties Inc

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SA02194SEOther aircraft modifications

Installation of vortex generators on the wings and tail surfaces in accordance with Micro AeroDynamics Drawing Package MA2233, Revision IR, dated September 27, 2010, Installation Manual MA2234, Revision IR, dated September 6, 2011, and Instructions for Continued Airworthiness, MA0666, Rev A, or later FAA approved revisions. NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.

FAA holder: Micro AeroDynamics Inc

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