topics:multi_aerodynamics
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| Both sides previous revision Previous revision Next revision | Previous revision | ||
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topics:multi_aerodynamics [2019/04/28 21:46] evan |
topics:multi_aerodynamics [2019/04/29 00:21] (current) evan [CAR Part 3 (1949)] |
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| * It must be possible to maintain heading ±°20 | * It must be possible to maintain heading ±°20 | ||
| - | FAR Part 23 Requirements | + | ===== FAR Part 23 Requirements ===== |
| <note tip>There is nothing in 14 CFR part 23 that requires a multiengine airplane to maintain altitude while in the takeoff or landing configuration with OEI. (AFH Ch 12)</note> | <note tip>There is nothing in 14 CFR part 23 that requires a multiengine airplane to maintain altitude while in the takeoff or landing configuration with OEI. (AFH Ch 12)</note> | ||
| Line 78: | Line 79: | ||
| type certificated February 4, 1991, or thereafter, the single-engine climb gradient (positive or negative) is | type certificated February 4, 1991, or thereafter, the single-engine climb gradient (positive or negative) is | ||
| simply determined. | simply determined. | ||
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| + | ===== FAR/CAR Regulations Applied to C310R ===== | ||
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| + | ==== CAR Part 3 (1949) ==== | ||
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| + | § 3.83 Stalling speed. **Vso at maximum weight shall not exceed 70 miles per hour (59.5kt)** for (1) single-engine airplanes and (2) **multiengine airplanes which do not have the rate of climb with critical engine inoperative specified in §3.85 (b)**. | ||
| + | |||
| + | (b) Climb with inoperative engine. All muliengine airplanes having a stalling speed Vso greater than 70 miles per hour or a maximum weight greater than 6,000 pounds shall have a **steady rate of climb of at least 0.02 Vso** in feet per minute at an altitude of 5,000 feet with the critical engine inoperative and: | ||
| + | - The remaining engines operating at not more than maximum continuous power, | ||
| + | - The inoperative propeller in the minimum drag position, | ||
| + | - Landing gear retracted, | ||
| + | - Wing flaps in the most favorable position, | ||
| + | - Cowl flaps in the position used in cooling tests specified in §§ 3.581-3.596. | ||
| + | |||
| + | Vso = 72kt = 83mph -> Climb Required: 1.66fpm | ||
topics/multi_aerodynamics.1556488013.txt.gz · Last modified: 2019/04/28 21:46 by evan
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