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--- topics:multi_aerodynamics [2019/04/28 21:47]
evan
+++ topics:multi_aerodynamics [2019/04/29 00:21] (current)
evan [CAR Part 3 (1949)]
@@ Line 79: / Line 79: @@
 type certificated February 4, 1991, or thereafter, the single-engine climb gradient (positive or negative) is
 simply determined.
+===== FAR/CAR Regulations Applied to C310R =====
+==== CAR Part 3 (1949) ====
+§ 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

Evan's CFI Notebook