STC SA00796AT
Current · Reissued · Aircraft · Small Airplane · Rev 09/21/2022 · FAA STC database
Installation of a dual-isolator forward engine mount system View PDF on drs.faa.gov ↗
The STC PDF is authoritative: installation instructions, ICA requirements and limitations.
Applicable aircraft (21)
- A4CE Textron Aviation Inc. · 206
- A4CE Textron Aviation Inc. · 206H
- A4CE Textron Aviation Inc. · 207
- A4CE Textron Aviation Inc. · 207A
- A4CE Textron Aviation Inc. · 210-5 (205)
- A4CE Textron Aviation Inc. · 210-5A (205A)
- A4CE Textron Aviation Inc. · 210
- A4CE Textron Aviation Inc. · 210A
- A4CE Textron Aviation Inc. · 210B
- A4CE Textron Aviation Inc. · 210C
- A4CE Textron Aviation Inc. · 210D
- A4CE Textron Aviation Inc. · 210E
- A4CE Textron Aviation Inc. · 210F
- A4CE Textron Aviation Inc. · 210G
- A4CE Textron Aviation Inc. · 210H
- A4CE Textron Aviation Inc. · 210J
- A4CE Textron Aviation Inc. · 210K
- A4CE Textron Aviation Inc. · 210L
- A4CE Textron Aviation Inc. · 210M
- A4CE Textron Aviation Inc. · 210N
- A4CE Textron Aviation Inc. · 210R
Certification basis — 14 CFR
Specific sections