Which option is NOT part of the transition point for a single engine minimum speed landing?

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Prepare for the Mission Helicopter-65E Test with flashcards and multiple choice questions. Each question has hints and explanations. Get ready for your exam!

Multiple Choice

Which option is NOT part of the transition point for a single engine minimum speed landing?

Explanation:
The transition point for a single engine minimum speed landing is defined by three cues you must have ready to move into the landing phase: altitude, airspeed, and straight-line distance to the landing area. You start this transition at about 200 feet AGL, maintain a safe approach speed of roughly 50–60 KIAS to preserve rotor energy and control, and you should have about 1,500 feet of straightaway to stabilize, verify parameters, and set up for the final approach. The distance of 2,000 feet is not part of this standard transition point; the recognized straightaway requirement is 1,500 feet.

The transition point for a single engine minimum speed landing is defined by three cues you must have ready to move into the landing phase: altitude, airspeed, and straight-line distance to the landing area. You start this transition at about 200 feet AGL, maintain a safe approach speed of roughly 50–60 KIAS to preserve rotor energy and control, and you should have about 1,500 feet of straightaway to stabilize, verify parameters, and set up for the final approach. The distance of 2,000 feet is not part of this standard transition point; the recognized straightaway requirement is 1,500 feet.

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