Objective:  Spontaneous recovery is an important determinant of upper extremity recovery after stroke and has been described by the 70% proportional recovery rule for the Fugl-Meyer motor upper extremity (FM-UE) scale. However, this rule is criticized for overestimating the predictability of FM-UE recovery. Our objectives were to develop a longitudinal mixture model of FM-UE recovery, identify FM-UE recovery subgroups, and internally validate the model predictions.

To relate a story which happened at a local airport several years ago. A ferry pilot brought a plane to town at night, tied it down at the rural airport, and was to meet the prospective buyer the next morning. The buyer arrived at the strip early the next morning, and while waiting for the ferry pilot, poked around the locked plane. Eventually something possessed him to rotate the prop through manually. Normally that would not have been a problem, except the magneto switch in the aircraft was "open" in the off position, which meant that both magnetos were hot. This was likely not noticed because not everyone does a magneto "ground" check in the off position during their run-up process. However, if the mixture idle-cutoff were in the cutoff position, there would not be fuel available in the carburetor to ignite, except for some reason (such as the ferry pilot extracting his RON bag in the dark) the mixture was nearly full rich. Normally this might have resulted in the engine firing, or even starting and idling. Again, this morning, things were not normal. The RON bag, extracted in darkness by the ferry pilot not only had bumped the mixture control, but also the throttle, so the aircraft engine faithfully roared to full power. Fortunately the startled prospective buyer did not get hit by the spinning prop. However, again, this was an unusual morning. As the engine roared to life, the tiedown on the right wing broke, and the plane pivoted on the left tiedown and swung approximately 180 degrees until the prop was buried into the fuel tank of an adjacent Cessna. Av gas was all over the place. One thing went right that morning, in that the avgas did not ignite and there was no fireball. Unfortunately, the day was not over, yet. After missing the spinning prop and not getting butchered by the surprise of his life, and then dodging a partially freed airplane, the buyer watched in horror as 40 gallons of avgas was sprayed over a running engine, as it came to a somewhat abrupt stop, the prop buried in someone else's wing. At that point he started running up the hill to the FBO to get help, and collapsed to the ground and died of a heart attack.


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Engines like the Continental A-65 used in Cubs and Champs in the 40s and 50s didn't have mixture controls or idle cutoffs (full rich all the time) and were shutoff by turning off the mags. If a cylinder had a lot of carbon/lead deposits, it would keep running intermittently kadunk kadunk kadunk.

This is a basic question that should be covered by your ground school, flight instructor and your primary training.The vast majority of certified piston-engine airplanes have two (redundant) magnetos for ignition.The mag switch in OFF position grounds the magnetos so they don't produce a spark even when they are turning (like if you pull the prop through a 180 degrees.)The ground wires are called P-Leads. If the ignition switch or one or both P-lead should fail (open the ground circuit) the magneto(s) may be "hot", that is, they can produce a spark in the spark plug and ignite any fuel in the cylinders. This will kick the prop over with great force and possibly hit anyone/anything in the prop arc.By pulling the mixture to cutoff position, starving fuel from the engine to shut it down, you greatly reduce the risk of a surprise/unwanted engine start when the prop is next moved.You might just move the prop level to allow attaching your tow bar after flying, or someone may handle the prop for no reason at all (curious children or just idiots at the airport/airshow/fly-in) and if the engine makes a spark and fuel is available (shut-off carb "rich") there could be an injury, death, and resulting lawsuit.Teach your flying guests, especially children, to never touch the prop unless they are certain it is safe. The key may be left on, or the mixture rich, and accidental starting can occur.Your handy pilot's checklist should have "Mixture - idle cutoff" in the "Before Starting" and "Shutdown" sections. Lastly, never leave a nosewheel towbar connected when you are not moving the airplane. It is very easy to forget it before starting the engine, and ANY PROP STRIKE REQUIRES A PROP INSPECTION AND ENGINE TEARDOWN/INSPECTION. Add "Towbar Stowed" to your preflight checklist.

Spark ignition gasoline and compression ignition diesel engines differ in how they supply and ignite the fuel. In a spark ignition engine, the fuel is mixed with air and then inducted into the cylinder during the intake process. After the piston compresses the fuel-air mixture, the spark ignites it, causing combustion. The expansion of the combustion gases pushes the piston during the power stroke. In a diesel engine, only air is inducted into the engine and then compressed. Diesel engines then spray the fuel into the hot compressed air at a suitable, measured rate, causing it to ignite.

People have often stated that the oxygen sensor installed behind the catalytic converter in a common gasoline engine setup has only one function: to test the health of the catalytic converter. Specifically, that it plays no role in engine mixture control. There is generally no disagreement with the role in catalyst testing. The question: are there any engines where this sensor is used by the engine control computer to modify the fuel mixture or other operating parameters?

Engine management fuel control strategies are among the most closely guarded secrets. Documentation is scarce on the details of how it is done in any given system. That does not mean we are without ways to discover generally how it is done. One piece of evidence we have is the OBDII PID labeled O2BxS2FT. A fuel trim PID for a rear oxygen sensor suggests that the after catalyst sensors are indeed used for fuel control. Experimentation can also reveal how the different OEMS use the sensors. Some systems, Subaru of the late 1990's for example, are unable to maintain mixture control at or near stoiciometric when the pre-catalyst sensor becomes disabled. Others have no problem maintaining fuel control on both banks even when only one rear sensor is operative (1990 Lexus LS400).

Fuel control strategies have changed over the years. In the 1970's and early 1980's system designs tended toward simple direct feedback logic. The mixture sensor sends its signal, the controller adjusts the mixture via changes to the injector on time, combustion happens, and then the sensor reads the new adjusted mixture, and so the feedback cycle continues. This system works but is crude by current standards as it is mediocre when it comes to optimal fuel mileage management and very poor at the fine level of mixture control need by the catalyst for optimal emission control. This is the system design commonly known and quoted among technicians and amateur internet forums. It is where the myth that the rear mixture sensor only tests the catalyst comes from.

Newer designs have changed significantly. This logic type has been labeled "feed forward". It uses Neural Network learning logic and memorized previous engine response parameters to achieve fuel control that gets a clean tailpipe and better power.

 This method uses an air fuel ratio sensors pre-cat and standard O2 sensor post cat. The AFR sensors test for misfire detection, mixture variation among cylinders and exhaust temperature. The rear sensor checks average mixture, catalyst output temp, and for a few seconds when conditions are right monitors catalyst heath. Direct feedback is not used as it is much to slow to keep the mixture in the range needed.

Fuel control logic varies greatly over the years and between manufacturers. Blanket statements about how it is done are unlikely to be supportable. However, one can discern some of how it is done on any given vehicle by watching graphed mixture sensor data on an extended test drive.

I'm wondering what the Johnson recommended fuel mixture would be for my '79 Johnson 35hp outboard. Want to make sure I go with the manufacturers recommendations. Also, what 2-stroke outboard oil brand should I use? I've been doing some reading on this and a lot of people seem to be convinced that the Wally Mart brand is just the Quicksilver brand, relabeled.

I believe if you pull the cover on the motor you will see the rate.If it is a tiller they use to put a white sticker on the inside of the tiller handle with the rate also.50-1 rings a bell but I would not bet on it.

MERCURYs - ANY non-high performance Merc made after 1960 can handle a 50:1 mixture of fuel and oil. Racing motors will need more oil. I run 20:1 in my smaller Merc racers. Newer V6 high performance engines might need more and some require av-gas (100 octane).

POST-1964 JOHNSON/EVINRUDE/GALE - The official stance on 1964 and newer OMC engines is to run them 50:1 and it's a good rule of thumb to follow on the bigger motors. OMC also renegged on the late 1980s 100:1 recommendation on the smaller (4-35hp) motors, bumping them back to 50:1. I've found that the smaller (3, 4, 5, 6hp) motors from post 1964 up into the mid-1970s may appreciate a bit of extra oil as they still have some bronze sleeve bearings. I run 40:1 in my '72 4hp, as I have a pile of holed blocks, burned cranks and twisted rods that were run at 50:1.

1960-1964 JOHNSON/EVINRUDE/GALE - 18hp and up can run at 40:1, as they are mostly jeweled motors at this point. Anything smaller run it at 24:1. Pre 1960 - any size, run it 24:1. If it's used for racing or high performance, double up the oil...

For exemple, on the C 172 G 1000,if during the take off, the air/fuel mixture must be adjusted at 100% when the altitude of flight is between 3000 et 6000 feet, what would be, in principle, the setting of the command of mixture and also the setting for the landing ? thank you for answer . 006ab0faaa

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