CA.IX.G.K3FAA-S-ACS-7B · Nov 2023Knowledge
How to identify, verify, feather, and secure an inoperative engine.
How to identify, verify, feather, and secure an inoperative engine.
Bottom line
Identifying the failed engine is a two-step process. The failed engine is the side that requires no rudder pressure. After identifying the failed engine, feather that engine and adjust power to maintain descent angle to a landing.
Key numbers
| Number | What it means |
|---|---|
| 400 feet AGL | Checklist |
| 2 to 3 degrees | OEI bank |
| one-half ball diameter | Ball |
FAA references
- PHAK ch. 2 (p. 2-19) — FAA-H-8083-25C (2023)
- PHAK ch. 2 (p. 2-20) — FAA-H-8083-25C (2023)
- FAAP874066 Landing Gear Selected Up, OEI Climb Performance Adequate — FAA-P-8740-66
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