Remove Stability Remove Tail Remove Thrust
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Delta Connection flight received sink rate alert before Toronto Pearson crash

Aerotime

The pilot flyingpulled back the thrust levers, and as a result, over the following 5seconds, N1 decreased from 64% to approximately 43%, where it remained until touchdown. The engine thrust was steady at approximately 43%N1, the TSB report explained. The air speed began to decrease, the TSB report said.

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35 years ago: How a United Airlines crew landed an ‘unflyable’ DC-10

Aerotime

The aircraft was powered by three General Electric CF6 turbofan engines, with one mounted under each wing and a third located above the rear fuselage in the base of the tail. On scanning the engine instruments, it quickly became apparent that the number two tail-mounted engine had failed. The plane entered a descending right-hand turn.

Runway 288
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Understanding Left-Turning Tendencies in Airplanes

Northstar VFR

Left-turning tendencies are primarily caused by four aerodynamic effects:torque, spiraling slipstream, gyroscopic precession, and P-factor (asymmetric thrust).Each As the propeller spins, it creates a spiral pattern of airflow that wraps around the fuselage and strikes the left side of the vertical stabilizer (rudder). The result?

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Delta CRJ-900 Accident In Toronto: Preliminary Report Published

One Mile at a Time

A large portion of the tail section was found on the runway, around 1,680 feet from the threshold, and 235 feet from the main wreckage. Obviously it was gusty, but if youre not able to stabilize an approach, thats when a go around would ordinarily be performed. The right wing came to a rest around 215 feet beyond the main wreckage.

Descent 104
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The Bold, Bulbous Douglas 1015 Cloudster II

Flying Magazine

An unbuilt concept, the Douglas DC-8 Skybus aimed to position two V-12 piston engines in the forward fuselage and link them with two contra-rotating propellers in the tail. A ventral stabilizer doubled as propeller protection in the event of over-rotation or tail strikes.

Drag 133
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Today in Aviation History: First Flight of the Consolidated XP-81

Vintage Aviation News

Around this time, the USAAF was also developing its first jet fighters, but knew that all-jet aircraft at this time were short-ranged and burned fuel quicker than propeller-driven aircraft, and so the optimal design was to feature a propeller-driven engine in the front for long range performance and a jet engine in the tail for high speed in combat.

Thrust 52
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Unbolted in Fairfield (Update on the 2022 Bell 407 GXP Crash)

Fear of Landing

At approximately 30-40 feet agl, the spinning stopped and the helicopter appeared to stabilize for a brief moment before continuing a nose-low, forward descent into the grass north of Runway 28. The operator confirmed that the tail rotor had been installed the day before the accident. As it descended it spun around 2-3 times.

Torque 94