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Demonstration Stalls

CFI Academy

Heres what they are and what you need to understand about each: Crossed-Control Stall What It Is: This stall occurs when the aircraft is in a skidding turn, typically with ailerons applied in one direction and rudder in the opposite direction (e.g., left aileron, right rudder). 65 knots in a Cessna 172).

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Mastering the Crosswind Landing Technique: Tips for Safer Touchdowns

Pilot's Life Blog

For example, if the wind is blowing directly from the side at 15 knots, the entire 15 knots acts as a crosswind. Understanding this allows you to plan your approach accordingly and choose the best landing technique. The lowered wing counters the wind drift, while the rudder maintains directional control.

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The Starlink era is here—will we regret it?

Air Facts

Weve all seen itnow imagine it on short final with Starlink. Its easy to imagine reading the NTSB report about an influencer on YouTube or Instagram who crashed while livestreaming on final approach (Can I land in a 40-knot crosswind? Ride along and find out!). Kids these days, right? That is why most of us fly, isnt it?

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Step-by-Step Guide: How to Land a Piper Seminole Safely

Pilot's Life Blog

Flight Characteristics The Piper Seminole has predictable handling characteristics, but its twin-engine nature demands more precision during the approach phase. Approach speeds typically range from 80 to 90 knots depending on weight and flap settings, while full flaps are often used to provide the necessary lift during landing.

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Demonstration Stalls

CFI Academy

Here’s what they are and what you need to understand about each: Crossed-Control Stall What It Is: This stall occurs when the aircraft is in a skidding turn, typically with ailerons applied in one direction and rudder in the opposite direction (e.g., left aileron, right rudder). 65 knots in a Cessna 172).

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Garmin Remains Major Player in Display and Autopilot Upgrades for Turbines

Flying Magazine

If an engine fails, the autopilot-based OEI ESP (standing by in the background and detecting the autopilot’s rudder boost has activated) will adjust the PFD’s roll limit indicators from 45 degrees inward to 10 degrees toward the failed engine and 40 degrees on the good engine.

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Stalls in the Pattern

AV Web

Winds were from 290 degrees at 15 knots, gusting to 21 knots. Yet all indications are he succumbed to a simple stall on final approach. On final approach for a third landing and following a Zenith STOL 701 also on final, the accident airplane descended and appeared to be lower than the airplane ahead.