STC SA10407SC
Historical · Reissued · Aircraft · Large Multi-Engine · Rev 03/24/2006 · FAA STC database
Installation of a replacement electrically driven hydraulic pump assembly View PDF on drs.faa.gov ↗
The STC PDF is authoritative: installation instructions, ICA requirements and limitations.
Applicable aircraft (4)
Certification basis — 14 CFR
Specific sections
- Sec. 111
- Sec. 113
- Sec. 115
- Sec. 117
- Sec. 119
- Sec. 120
- § 21.47