STC SA00014CH
Historical · Amended · Aircraft · Single-Engine · Rev 11/24/1997 · FAA STC database
Installation of a P&W (Canada) turbopropeller engine (Model PT-6A, -6B, -20, 20A, -20B, or -6/C20) and Hartzell propeller (Model HC-B3TN-3B hub and Model T10282(N)-4R blades). 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