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hud head clamp
the idea is that you use the eye liner, the three balls on the centre windscreen post, to ensure your head is in the correct spot.
BUT the HUD has a very small angle of view, so very often a small head movement moves the huds display out of the direct and correct line of sight. Not normally a major problem, I find the worst problem, is the very slight lack of infinity, and thus a slight re focus is required. Now thats a problem. |
Knife-Edge - the decision on whether to de-ice is a complicated one. If your a/c had a longish inbound sector the wings would have been well below zero and any rain would freeze on them (known as 'rain ice'). Often an upload of 'warm' fuel (normally well above ambient temperature since it is normally stored underground) will clear the ice. The Ryanair may have had a short inbound sector or uplifted fuel - or both. One hopes that consideration was given to de-icing and I'm sure it was. Normally a combination of experience, indicated wing fuel temperature and a look at the way the rain behaves as it lies on the wing will make the decision. No doubt your Tom Captain made the correct decision:ok:
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The except from the A320 FCOM answers your question:
FWC generates synthetic voice for radio height announcement below 2500 feet. These announcements come through the cockpit loudspeakers even if the speakers are turned off. Predetermined call out The altitude call out uses the following predetermined threshold : height (ft) call out 2500 TWO THOUSAND FIVE HUNDRED OR TWENTY FIVE HUNDRED 2000 TWO THOUSAND 1000 ONE THOUSAND 500 FIVE HUNDRED 400 FOUR HUNDRED 300 THREE HUNDRED 200 TWO HUNDRED 100 ONE HUNDRED 50 FIFTY 40 FORTY 30 THIRTY 20 TWENTY 10 TEN 5 FIVE DH + 100 HUNDRED ABOVE DH MINIMUM Pin programmings allow the operator to select the call outs needed. If aircraft remains at a height that is in the detection zone for a height callout, the corresponding message is repeated at regular intervals. Intermediate call out If time between two consecutive predetermined call outs exceeds a certain threshold, the present height is repeated at regular intervals. The threshold is : 11 seconds above 50 feet 4 seconds below 50 feet The repeating interval is 4 seconds. RETARD announcement The loudspeaker announces RETARD at 20 feet or at 10 feet if autothrust is active and one autopilot is in LAND mode. YS |
Taxi procedures for heavies at TNCM
This is for anyone who has been to TNCM in a heavy, particularly a 747:
What are the real-world taxi procedures for TNCM for heavies? I've been asking around and looking around and I'm still not clear where the heavies turn around. Apparently they all go to taxiway Charlie, then backtrack along the runway to get to the start of runway 9, but I don't know if they take that little taxiway near the 09 end for their 360 to line up, or whether they backtrack all the way to the end of the runway and then turn around in the tiny space provided on the north side. Which procedure is used in real life? Or is the real-world procedure something entirely different? Likewise, for landing, what's the usual procedure for large aircraft? Do they go all the way to the end of 09 and then backtrack to Charlie, or do they stop at that intermediate point where there's a space to turn around, or what? I have quite a bit of difficulty turning a 747 on either spot; with the tiller hard over and lots of brakes on the right side I can just barely squeak by, although the brakes are usually excessively hot on that side by the time I reach the gate. |
Clunky engine noise on 737 ??
Whilst waiting on the spectators balcony at LPMA recently, I watched an Easyjet 737 arrive. As the engines spun down I could hear this god awful clunk with each revolution of the starboard engine. The ground crew didn't seem concerned, neither did the captain when he did a walkaround and gave the fan a spin with his hand (and the clunk was there as he did it).
I've never heard this before. Any ideas on what it might be, and why nobody seemed concerned ? |
I think it's the fan blades making that noise, the blades are seated in the hub but have a small gap in them (presumably for expansion) and you hear a clicking or ticking noise when they move downwards. It is very prominent when a breeze is going through the engine. I will be the first to admit I may be wrong, maybe someone can correct or elaborate for me.
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Aircraft brakes
There is a thread in the flightdeck forum discussing a recent incident at Changi.
It is suggested that pliots can not use braking if the AC is rolling backwards as the result could possibly be an unplanned rotation. :) Is it not possible to apply brakes to the nose gear only to prevent any danger of the aircraft ending up sitting on its tail? |
The vast majority of aircraft only have brakes on the mainwheels. Good idea though.
Regards, BH. |
I was once sitting in the back seat of a C172 parked facing up a bit of a slope. For some reason mein Kapitan released the handbrake before start up and we started to roll backwards towards the clubhouse. He applied the brakes quite heavily and, no doubt assisted by 200lbs of yours truly perched aft of the centre of gravity, we came awfully close to ploughing a narrow furrow with the bottom of the rudder! Not an auspicious start to a jolly...:rolleyes:
The C-17 demo at Farnborough one year included a reverse thrust exit from the runway followed by some enthusiastic braking and a distinct lifting of the nose gear! The crowd loved it.:ok: |
Pushbacks at Paris Orly
Flew out of Orly on Monday night and as we were pushing back I noticed that an AF 321 was being pushed back with the tug attached to the underwing left side undercarriage. I have never seen this before and it looked like an inefficient way of doing it.
Any ideas? |
3 Pilots to Innsbruck?
I recently flew to/from LGW to Innsbruck (LOWI) for a ski-ing holiday with Easyjet on an A319. Both ways the Flight deck crew announced themselves as comprising three members. Normally, of course, there would only be two. Any particular reason? I thought it may be due to being a new-ish route for Easyjet but, moreover combined with the 'interesting' approach to LOWI thus, perhaps they were familiarising pilots to same. Any insider/official explanations?
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You are correct. It is a Category C - ie 'more difficult' airfield - and special simulator training is required. A visit is useful as well and may be a requirement in EasyJet.
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Flaps ???
Hello,
Had some ITVV DVD's for Christmas and a question has just popped into my head (Some 8 weeks later) When the pilots are checking the control surfaces during taxi, why don't they check the flaps and spoilers ?? ie. Why not FULL flaps and then return them to TO configuration. Cheers :ok: Matt |
Windy Landing
I was on a JET2 flight landing at LBA on Sunday (2 March) and the landing was quite bumpy due to wind conditions. Upon touch down we appeared to bank heavily to the right (felt like on one wheel!) and then levelled off. Everyone on board breathed a sigh of relief!
My question is how difficult is it to land in strong winds and are we in any danger from tipping over! As a passenger I feel quite nervous can anyone put my mind at rest? Many thanks.. |
hi PPC,
been a flying instructor many years. we teach for these sort of things but sometimes a stronger than average crosswind gust may just strike when an aircraft is at its most vulnerable...that is just as it flares to land with consequential results but not always fatal nor damaging to aircraft nor passengers. there have been in both light aircraft and large passenger jets crosswind induced accidents....but your chances of being involved in a car accident are still higher.... so relax...and enjoy your flights..when you a$$ is strapped to metal its going to do what its going to do in any event..!!:} safe flying.. the dean. |
upon touch down we appeared to bank heavily to the right (felt like on one wheel!) and then levelled off. PP p.s. should have been landing on Friday night, now that WAS windy!:ok: |
It's very simple.
If the cabin is not secure then we DO NOT land. There is no way around it!! |
Stall Warnings
We all (presumably) know about stick shakers and audible stall warnings that tell when a stall has or is about to occur but what I am confused about is how a stall or potential stall is actually detected.
Is the actual physical stall somehow detected by sensors reading air pressures etc, or does some particularly complicated bit of computer wizardry determine that the aircraft should be stalling "about now" given it's airspeed, configuration and external climatic conditions? |
It is the air sensor on to top of the wing and senses the turbulent air foorewarning a stall
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We all (presumably) know about stick shakers and audible stall warnings that tell when a stall has or is about to occur but what I am confused about is how a stall or potential stall is actually detected. Is the actual physical stall somehow detected by sensors reading air pressures etc, or does some particularly complicated bit of computer wizardry determine that the aircraft should be stalling "about now" given it's airspeed, configuration and external climatic conditions? A stall is an increase in angle of attack to the point of airflow separation, and a big buildup of induced drag and a loss of lift. These things don't happen all at once, necessarily. The key to understanding them is monitoring the angle of attack, and stall warning systems using stick shakers, pushers, etc, do this by sampling the angle of attack. They also sample the position of flight controls such as flaps...because the angle of attack at which the wing stalls will change with the flaps setting as the wing shape and configuration changes. It also takes into account air data information received from an air data computer. How the airplane does this depends on the airplane and the systems in use. Some are very simple, some are not. Some airplanes like the airbus simply won't let the airplane stall due to "laws" built into the system. Some airplanes such as a single engine Cessna may use a small tab or even a simple suction port on the leading edge of the wing to produce a noise, and nothing more...and yet other airplanes don't even do that...they're simply detectable by a buffeting in the airframe or controls. An angle of attack vane may be a movable vane which acts like a weathervane of sorts, or it may simply be a probe with holes that sample the way air flows around it to derive angle information. This is then applied to the aircraft data to determine what the actual angle of attack is (local angle of attack isn't the same as the free airstream, and AoA changes with maneuvering or configuration changes may mean that the AoA isn't the same as what the probe or vane is seeing at any given time...computers correct this). The system in use then takes this information in, and outputs whatever signal is necessary...such as a stick shaker or pusher signal. When the pilots are checking the control surfaces during taxi, why don't they check the flaps and spoilers ?? ie. Why not FULL flaps and then return them to TO configuration. We check all the flight controls after we've set the flaps to their takeoff setting. In cycling the flaps we also move a number of other parts, including the leading edge devices which cycle in stages. We can only test certain things with flaps up, some with flaps out...and we have specific set procedures for everything. In some airplanes, spoilers or aileron augmentation is tested at the same time...happens on our airplane. On others we test them and then test emergency stow systems...some thrust reversers are tested and stowed, and on others, they're not. The primary reason for testing the flight controls is to make sure they're powered, and that they're not locked for any reason. For example, in our airplane, when the flaps are up, the outboard ailerons are locked out. We have to extend the flaps to get the ailerons to work. We're checking for freedom of flight control movement and that our indicators in the cockpit correspond. There's no reason to run the flaps down, especially during ground operations when there's a greater possibility of damage, hitting something, etc. More importantly, we certainly don't want any possibility that they're overextended and a takeoff roll started with them in that dangerous condition. Further, there's no guarantee that simply because they extended before flight, that they'll work when it comes time to land. Especially in a big airplane, moving flaps is a big deal, especially on the ground. Even powering a system, such as electrical or hydraulics, can have severe consequences...or moving a flight control for that matter. What's moved, when, where, and how fast must be carefully considered at all times...especially on the ground. We have flight control surfaces longer than a bus. Our horizontal stabilizer and elevators are bigger than the wings on a DC-3, with a wider span. There's a lot of metal moving out there. The flaps extend down a considerable distance, and there's just no good reason to put them down and then up again. As the engines spun down I could hear this god awful clunk with each revolution of the starboard engine. The ground crew didn't seem concerned, neither did the captain when he did a walkaround and gave the fan a spin with his hand (and the clunk was there as he did it). |
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