FAA · Advisory Circular
Reduction of Electrical System Failures Following Aircraft Engine Starting
14 CFR Parts this AC applies to
Derived from the AC's subject series via the FAA's published numbering scheme.
Document overview
Structured fields from the FAA Dynamic Regulatory System (DRS). Full body text lives in the linked PDF.
- Subject
- Reduction of Electrical System Failures Following Aircraft Engine Starting
- Status
- Current
- Office
- AFS-300 | AFS-340
- Cancels
- AC 91-55
- Referenced 14 CFR Parts
- Part 91
- Referenced sections
- Sec. 91.7