STC SA378CH
FAA DRS lists SA378CH as Current · Reissued, held by Acron Aviation Inc., for Textron Aviation 65, Textron Aviation 65-80, and Textron Aviation 65-88, and 16 more aircraft configurations. Recorded change: Installation of TCAS I. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of TCAS I.
SA378CH 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 65, Textron Aviation 65-80, and Textron Aviation 65-88, and 16 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 65 and Textron Aviation 65-80, and 17 more aircraft configurations model, serial range, and configuration?
- 02Which configuration, parts, installation data, limitations, and ICAs apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related other aircraft modifications STCs
Operation of airplane on unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index (RON+MON)/ 2 per ASTM Specification D-439. Intermixing with aviation gasoline also approved. Data required: 1. Petersen Drawing No. 1521A dated November 15, 1989, or later FAA Approved revision. 2. Airplane Flight Manual Supplement dated November 22, 2004 or later FAA Approved revision.
FAA holder: Petersen Aviation Inc
Descriptive data pertaining to this design change are considered inadequate for duplication on other products. This approval is limited to the McDonnell Douglas Model DC-9-15 Serial Number 45797 only.
FAA holder: AeroMech Incorporated
Limited to installation on serial number 1017 ONLY.
FAA holder: Innotech Aviation Ltd
Installation of a dual TAWS system in accordance with Pyka MDL 1B07-DL-001-501 Rev. D dated October 29, 2004, or later FAA approved revision. Airplane Flight Manual Supplement 1B07-FM-001 Rev. IR dated November 05, 2004, or later FAA approved revision, is required.
FAA holder: Pyka Aerospace Corp