STC SA1773SO
Historical · Reissued · Aircraft · Large Airplane · Rev 07/18/2014 · FAA STC database
Installation of a third stand-by attitude gyro and dedicated power supply AIM P/N PE 24-1RM View PDF on drs.faa.gov ↗
The STC PDF is authoritative: installation instructions, ICA requirements and limitations.
Applicable aircraft (3)
Certification basis — 14 CFR
Specific sections
- Sec. 111
- Sec. 113
- Sec. 115
- Sec. 117
- Sec. 119
- Sec. 120
- § 21.47