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AI.II.P.R2FAA-S-ACS-25 · Nov 2023Risk management

Loss of directional control.

ACS element text (the applicant demonstrates understanding of)

Loss of directional control.

Bottom line

The VMC noted in practice and demonstration, or in actual OEI operation, could be less or even greater than the published value, depending on conditions and pilot technique. Five to 10 degrees of bank to initially assist the rudder in maintaining directional control in the event of an engine failure, as the pitch attitude for Vyse is established.

FAA references

  1. AFH ch. 13 (pp. 13-29–13-30) — FAA-H-8083-3C
  2. FAA-P-8740-66, Flying Light Twins Safely — FAA-P-8740-66
  3. AFH ch. 13 (p. 13-23) — FAA-H-8083-3C
  4. AFH ch. 13 (pp. 13-26–13-27) — FAA-H-8083-3C
  5. AFH ch. 6 (p. 6-14) — FAA-H-8083-3C
  6. AFH ch. 13 (pp. 13-27–13-28) — FAA-H-8083-3C
  7. RMH ch. 3 (p. 3-7) — FAA-H-8083-2A
  8. PHAK ch. 5 (p. 5-20) — FAA-H-8083-25C (2023)
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