STC SA00882WI-D
FAA DRS lists SA00882WI-D as Current · Reissued, held by Honeywell International Inc, for Textron Aviation 95-C55, Textron Aviation 95-C55A, and Textron Aviation D55, and 3 more aircraft configurations. Recorded change: Installation of Bendix/King KFC 225 Automatic Flight Control System. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of Bendix/King KFC 225 Automatic Flight Control System.
SA00882WI-D identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.
Applicability
Aircraft named in FAA DRS
Named aircraft: Textron Aviation 95-C55, Textron Aviation 95-C55A, and Textron Aviation D55, and 3 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Textron Aviation 95-C55 and Textron Aviation 95-C55A, and 4 more aircraft configurations model, serial range, and configuration?
- 02Which control configuration, rigging, limitations, and inspections apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related flight controls STCs
Installation of Cyclic Force Trim System in accordance with Premier Aviation, Inc. MDL F00-15000, Rev C, dated December 24, 1996, or later FAA approved revision.
FAA holder: Bell Helicopter Textron Inc.
1. Installation of S-TEC 01298 or 01304 Digital Flight Control System (DFCS), in according with Master Data List 921128, Rev. 11, dated 3-16-11 or later FAA Approved revisions of the above data.
FAA holder: S-TEC Corporation
Installation of the Cessna 182D cowling (upper cowling P/N 0752031-27, lower cowling P/N 0752031-28) with cowl flaps and cowl flap mechanism in accordance with Tom P. O Reilly s Installation Manual, Rev. Orig., Dated 11/7/2008, FAA approved on 2/25/2011 or later FAA approved revision.
FAA holder: O'Reilly Tom Paul
Installation of 40:1 gear ratio wing flap transmissions and related changes in accordance with Colemill Enterprises, Inc., Installation Instructions dated February 16, 1983, or later FAA approved revision. This modification provides and equivalent means of compliance with paragraphs (a)1, (a)2, and (a)4 of AD 82-27-13 and restores the 40 (full) flap travel.
FAA holder: Mike Jones Aircraft Sales Inc.