FAA · Advisory Circular
Geometry and Dimensional Considerations for Comparative Test and Analysis for Turbine Engine and Auxiliary Power Unit (APU) Replacement, and Repaired Parts
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
- Geometry and Dimensional Considerations for Comparative Test and Analysis for Turbine Engine and Auxiliary Power Unit (APU) Replacement, and Repaired Parts
- Status
- Current
- Office
- AIR-62A
- Referenced 14 CFR Parts
- Part 21, Part 33, Part 43
- Referenced sections
- Sec. 21.303, Sec. 43.13, Sec. 43.15