STC SE00047AT-D
Current · Issued · Engine · Rev 10/14/1993 · FAA STC database
Modification of turbine exhaust case to provide increased wall thickness for the purpose of improved blade containment. View PDF on drs.faa.gov ↗
The STC PDF is authoritative: installation instructions, ICA requirements and limitations.
Applicable aircraft (6)
Certification basis — 14 CFR
Specific sections
- Sec. 111
- Sec. 113
- Sec. 115
- Sec. 117
- Sec. 119
- Sec. 120