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Originally Posted by Hammerhands
I think they mention on that or other episodes about a little propeller that pops out with both engines dead or no gas to provide emergency power for primary controls.
What you're referring to here is often called a RAT, for Ram Air Turbine, or ADG, for Air Driven Generator and will provide for some minimum flight control capability and/or electrical power.
The CRJ has one that will automatically deploy from the right side of the nose of the airplane in flight if both main AC electrical buses lose power (as in the case of a dual engine failure, or some very serious electrical problem). The prop on this thing is very small, about 10" in diameter, and sounds like a little buzz saw when it deploys. I used to flight test these on the RJ (later they developed a model of the ADG that didn't require an inflight test). The test was required every 180 days and it only took about 20 minutes of flying time. We'd go out around midnight, takeoff out of Dulles, shut off the electrical generators and confirm that the ADG deployed and that it provided electrical power (we had the APU running as a backup in case the ADG didn't deploy or didn't work properly).
In the 767, the RAT deploys
only in the case of dual engine failure (
click here for one real life example) and its purpose is to power the flight control portion of the center hydraulic system.
For both of these aircraft, the RAT needs a minimum of 130 kts airspeed to be functional.
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On another episode about an AT-76 that crashed due to icing in Indiana, the accident that caused most of these planes to be shipped to the South, they say that the commuters are/were non-priority at O'Hare behind the internationals. Is that true? Is that due to scheduled landings, schedules, politics, fuel consumption rates?
I often wondered about this when I flew the commuters and now that I'm flying international I've never seen or heard anything that confirms this to be true. Maybe some of our ATC readers can comment.
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Isn’t that little float-plane in the first few pages a little RC float-plane?
I must have missed something. "first few pages" of what?
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Do you get to the casino in Monaco? Have you been one bay over from Nice to Ville-Franche or Beulieu-sur-Mer?
I took the bus to Monaco once (and the train back to Nice) and I walked around and got some pictures, but I didn't go in the casino. Some other crew members told me there's a few just to walk in the place of about 15 Euro.
I'm not familiar with those places, but I've been to Antibbes and Cannes, which are just west of Nice.
Flying in to Nice, we usually land to the Northeast (runway 4L or 4R), but occasionally the winds make a landing the opposite direction necessary. This approach brings us very close in to the beach and the controllers are concerned that we stay out over the water. It's interesting the way they phrase it: "Delta 82, you are cleared for the approach to runway 22 Right. Stay above the water."
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On a little plane you increase the thrust to climb and then adjust the nose. There is an increase in lift due to the angle of attack, but very little of that is due to deflection. Is it the thrust/weight ratio or a change in the magnitude of momentum that makes you think in terms of pulling the stick back to climb? You still drop the nose to gain immediate speed!
Ow, my head hurts!
Airspeed and altitude are interchangeable to some extent. You trade altitude for airspeed, as you note, by lowering the nose and you can trade off excess airspeed to gain altitude also. A flight maneuver that pilots practice in primary training (or was it for the commercial license?...not sure) called a
Chandelle consisted of a course reversal with maximum altitude gain. To get the maximum altitude, you would add power but you would also trade off airspeed until you were right down near stall speed when you rolled out. A good demonstration of the relationship between airspeed and altitude.
In normal flight, we know we need to raise the nose (increase the angle of attack) to climb, but the increased AOA means more drag and that means airspeed will start to bleed off, so we increase power to compensate and to maintain airspeed. If we continue to increase pitch, we will get to a point where it requires more power to go slower due to the increased drag. This is called the
backside of the power curve (the portion of the curve between "stall" and "minimum power airspeed").
If we were to simply increase power in level flight, the plane would begin to accelerate. This acceleration would result in more lift being produced by the wing and the airplane would begin climbing. To avoid this climb we would have to exert more forward pressure on the wheel (or roll in down trim), which is what we would do if, for example, ATC asked us to increase speed from 280 kts to 300 kts.