FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 23 > Section 71 - Glide: Single-engine airplanes
section 23.69 |
section 23.73
The maximum horizontal distance traveled in still air, in nautical miles, per 1,000 feet of altitude lost in a glide, and the speed necessary to achieve this must be determined with the engine inoperative, its propeller in the minimum drag position, and landing gear and wing flaps in the most favorable available position.
[Doc. No. 27807, 61 FR 5187, Feb. 9, 1996]
   
Current page: FARs > Part 23 > Section 71 - Glide: Single-engine airplanes
section 23.69 |
section 23.73
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