Originally Posted by IcePack
(Post 9997880)
Yes agreed it is, but going back to the early 90’s I can remember the AB trainers telling us this fact, when we all wanted a/p off a/t off. We were instructed to to “always” keep the a/t on. This was also because of the variable target speed. (Ground speed mini)
I've had the AT off on windy days where GS mini has adjusted the speed all the way down final. I didn't find it particularly difficult. I'm scanning the ASI anyway- if I'm now a few kt behind the new Vapp, add a bit more power. I think we sometimes confuse what automation can do with what it must do. |
G/S mini is one of those lovely ideas that is great in theory on an average day (like so much of the Airbus)
G/S mini, autothrust on ,is a real pig on a really windy day ,manual thrust Vls +15 sorted . Ride through it all with sensible power setting ,land piece of cake . There’s nothing more terrifying than watching the magenta line children haul the aeroplane around the sky frantically chasing the flight director whilst the auto thrust and g/s mini all operate slightly out of phase with each other and the so called pilot wrestling the stick around |
watching the magenta line children haul the aeroplane around the sky frantically chasing the flight director |
Goodness gracious me. Depending on the surface conditions, if the approach is stabilized, all the P/F has to do is close the throttles when the A/C touches down and a reasonable landing should ensure.
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Those suggesting they might not know it's 3.5g have their head in the clouds.
Worst I've done (and been party to) is 1.7g, and I thought I'd snapped the wings off. I can't imagine how 3.5g must feel. |
Skittles - couldn't agree with you more! I remember sheepishly following my Captain to the fleet manager's office (voluntarily) many years ago because we thought we'd done a REALLY hard landing. He had the data interrogated - surprisingly it was only a 1.4G landing! I was dumbfounded then (as I am now) how some pilots fail to notice a 'true' hard landing.
The FD conversation on this thread is also interesting. I found that only after I'd flown a large Boeing did I truly understand how to fly a FD on final - and it was this; never slavishly follow the FD! Instead take the 'hint' that it's giving, i.e. if it shows a 'fly up' command, just a gentle pitch correction TOWARD it is sufficient to see it immediately come back down towards commanded pitch. While a line instructor, it was something that I tried very hard to instill in new Airbus pilots. As an examiner, I tried to encourage the adoption of same in those who showed a tendency to pitch inappropriately (by simply following the FD like their lives depended on it). As for autothrust - I think the AB certainly does a great job of maintaining speed on 90% of approaches. It's when the 10% of flights encounter seriously gusty conditions that I believe manual thrust comes into its own. Sadly there are an ever-increasing number of airlines who mandate autothrust ON unless it fails - so it becomes harder to fly the aircraft smoothly in those conditions. What to do, what to do? |
I think of the FDs as suggestion bars
And I'm a big advocate for manual thrust on the bus, time and a place etc. Particularly given the response of the a330s ATHR system |
I'm also with Skittles on this one.
The aircraft was planted by the F/O and we had an ACARS reading of 2.1G. Subsequently the Engineers determined that it was only 1.7G because the aircraft looked at the difference between the positive and negative 'G' - apparently.
During the taxi in I was in shock to be honest, as was the F/O. The poor F/O was actually in tears at the gate. I had thought that there must be damage although a post flight walkround revealed nothing to me. We nightstopped for the Engineer to do inspections which revealed nothing amiss. Anyway, how any crew could think that 3.5G is nothing to worry about is beyond me. By the way I was dragged into the office and given a dressing down about allowing an F/O to carry out a night landing off an NPA. Maybe they were correct, although it had never happened before or since. |
I suggest whoever called you into the office never travel on an airline based on the west coast of the Atlantic. Being a copilot at that company must be a very boring job.
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From an engineering point of view, I suspect that if you load a 'plane up to twice its weight, to simulate 2G, then the MLG would be fully compressed. Any further loading beyond that will result in the shock going straight into the airframe, as the shock absorbers are beyond their working range.
Also because the CofG is in front of the MLG, the landing impact will cause the front of the aircraft to drop (lessening the G in the cockpit area.) and cause the rear of the plane to rise, increasing the G forces on the tail. All this rather begs the question of where do you put the Accelerometer to record the forces, or maybe use several of them and take the highest reading. I think for certification reasons all aerobatic airplanes must have both a 5 point seat harness, and a recording G meter. This will have moving needles for +ve and -ve G, and is fitted into the instrument panel. |
I’m sure I remember that back in the day, “crush tape” was fitted to the base of the MLG struts. If it was crushed, it was a heavy landing and inspection was required. (Simples!)
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Originally Posted by cessnapete
(Post 9996168)
RAT5
Unfortunately it’s not just small Airbus operators mandating these SOPs. Apart from the B744, British Airways SOP bans manual control of thrust management on all fleets,at all times during route flying. Never understood the rationale behind crippling pilot skills when all interest should be in keeping those skills sharp. |
scifi
Think you will find that the wings are still carrying a lot of the load in a normal but high ROD landing. Modern airliner struts do not just bottom-out except in extreme overload, they get very stiff in the latter part of their range to avoid destructive structural failure from a high ROD touchdown, esp below normal MLW, although progressive overload damages will occur with the severity of overstress. The "question" of measuring loadings and their interpretation, has also been long understood for airliners. Cheers |
my airline was the first NA carrier to fly the 320 and the 747-400, and, back in the day, the more we got of each, the more the airline's training dept (unofficially, as I remember it) encouraged the occasional use of manual thrust. (so as to maintain FLYING skills). But the airline didnt mandate either, unless required--obviously.
I cant imagine why manual thrust should be prohibited in line training? so, the first time I get to do it is, unsupervised? how about, say, landing in sfo, lets try it there the first time. |
Generally, our rear quarters are calibrated on the safe side of the G meter. On transport aircraft, it is very common for the pilots to note a hard landing before the accelerometers tell their story - i.e., maintenance nearly always has log entries of perceived hard landings that were within parameters rather than the other way round.
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I would agree. However, the danger lies in the unchecked actual overstress. The further operation of this aircraft before being properly heavy landing checked is a criminal act IMO.
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Clue to a serious "event" is that the "rubber jungle" deploys.
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Reading a Load 15 report is a notoriously dark art.
Airbus, in its wisdom, made it hellishly complicated. Interpreting the report is tricky due to the multiple combinations of parameteters and the timings of events. The touchdown point is often difficult to judge from a bunch of digits. It isn't just all about G loading either. In fact Vertical Acceleration coupled with pitch/roll angle play as big a part if not greater in some cases. Most airlines I have worked with leave it to the Captain to determine if a Hard Landing has occurred (a heavy or overweight landing is a completely different animal) however, when an automatic report pops out of the printer we usually get a call just to make sure. In this case I do wonder what was uppermost in the minds of the crew....:suspect: |
Originally Posted by TURIN
(Post 10022843)
It isn't just all about G loading either. In fact Verical Acceleration and pitch/roll angle play as big a part if not greater in some cases.
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Changed it now. Does it make more sense? It's late and i've had gin.
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