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US FAA issues safety alert over Boeing 737 rudder issue

Aviation News

NTSB issued urgent safety recommendations to Boeing and FAA FAA directs pilots to review Boeing’s procedure for jammed rudder FAA will collect data after incidents.

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The Ercoupe

Plane and Pilot

He was proud of his little bird, with its unique split sliding canopy, no rudder pedals, and a delightful art deco instrument panel. Long before he purchased his very own Boeing 707, actor John Travolta discovered this economical fun flier and began his remarkable aviation career as a proud owner. Push and pull for pitch.

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What Is a Flat Spin?

Pilot Institute

PARE: Power idle, Ailerons neutral, Rudder opposite, Elevator forward. Rudder: Full opposite input to the spin direction. R – Rudder The third step in the spin recovery procedure is to apply the opposite rudder to the direction of the turn. Once the spinning stops, make sure that you bring the rudder back to neutral.

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A Cloud of Confusion

Inspire

Rossier, EAA 472091 This piece originally ran in Robert’s Stick and Rudder column in the July 2024 issue of EAA Sport Aviation magazine. By Robert N.

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What NTSB Reports Say About Impossible Turns and Angle of Attack (Part II)

Air Facts

What NTSB Reports Say About Impossible Turns and Angle of Attack—Part 2: Analysis, Questions Raised, and Next Steps The current emphasis in general aviation (GA) safety is on visual angle of attack (AOA) indicators and impossible turns (return to the airport following engine failure). for several general aviation airplanes.

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Genuine Stall Proficiency

Plane and Pilot

Stalls are feared in general aviation for being a significant factor in a large proportion of accidents. After a thorough ground briefing, on the first power-on stall flight with a student, after clearing the air, I would have the learner do a stall with too much right rudder, enough that the ball was out one width.

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What is a Stall? – When Wings Stop Working

Pilot Institute

Critical Angle of Attack As the AOA increases, the wing generates more lift, but only up to a specific point known as the critical angle of attack, typically around 15-20 degrees for general aviation aircraft (though this can vary depending on the wing design). Level the wings : Use coordinated rudder and aileron inputs.

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