STC SA03518AT
Historical · Issued · Aircraft · Small Multi-Engine · Rev 11/28/2007 · FAA STC database
Installation of a bonded doubler inside the wing leading edge. View PDF on drs.faa.gov ↗
The STC PDF is authoritative: installation instructions, ICA requirements and limitations.
Applicable aircraft (5)
Certification basis — 14 CFR
Specific sections
- Sec. 111
- Sec. 113
- Sec. 115
- Sec. 117
- Sec. 119
- Sec. 120