AF447 should not be brought in because the crew was overwhelmed. They didn't see anything not even the pitch that resulted fro their actions forget the GPS GS. UAS procedure is based on a philosophy to manage the aircraft speed within a safe band, accuracy is not the purpose nor is it possible. It is similar in Boeing or Airbus. After having applied recommended procedure GPS GS may be referred for awareness but it won't be wise to fine tune anything. Airbus has come out with back up speed(different from B/U SS) obtained by applying lift equation to GW, AOA, CG. It's there in A350 and optionally available on other models. If fitted then it's as simple as AP/FD TCAS. You do nothing. Just Say thank you.
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Originally Posted by itsnotthatbloodyhard
(Post 10479727)
Not in any A330 I’ve ever flown, unless your ‘normal cruise’ is down around F200. For F350, M0.8, ISA+10, 205t (as per AF447), the tables I’m looking at indicate about 95.5% N1. That’s for the CF6 - would the RB211 be that much different? |
It seems as if we are assuming we don't know the actual windspeed, when this can be found by asking the nearest ATC unit for their ground windspeed, then adding the correction of twice that and add 30 degrees to find the wind velocity above 1000 ft.
. |
Just have an idea of the pitch and power you need, it’s not rocket science. Plus on Airbus the thrust would be locked so you don’t even need to worry about it unless you are in a climb or descent. A320: Above FL 300: 80% N1 pitch 2 degrees up between Fl200 and Fl300 : 70% N1 & same pitch Below Fl200 60%: N1 pitch 3 degrees up then 4 up below Fl100. Just some rough value from what I saw during flights. With these I might climb or descent gently but I won’t stall nor overspeed and it gives me time to reach the QRH to do fine tunning. |
scifi, that's pushing too far, it is not a hot air baloon.
The best solution is to at first do nothing and check all the remaining parameters, to be used later as a reference and self-check over and over again. This thread inspires me to include GS in that scan the next time, and it might had prevented a ckup I managed to create in the last session. Having said that, anything additional must be included carefully not to compromise the original underlying skill. |
The best solution is to at first do nothing and check all the remaining parameters Which reminds me of one of my learning events. I was first time left seat ferrying a Twin Otter with a very experiences mentor pilot friend. We were leaving Cairo southbound, and low altitude nav aids were few and far between. This particular Twin Otter did not have a DG at all, it had two slaved RMI's and the magnetic compass (which is not remarkably useful for flying a heading in a Twin Otter). We had noticed on previous legs that the RMI's would drop a flag an quit, seemingly randomly, so becoming useless for flying a heading. We agreed that whomever had a working RMI would fly (no auto pilot, hand flying the whole trip anyway). So, when a half hour into a 9 hour leg, my RMI dropped a flag, I wasn't really eager to surrender flying just yet, I was enjoying myself! My mentor friend was consumed with a marine "Sat Nav" device he had brought on the trip. This was before the days of GPS - the time before magenta lines, so it was charts and heading indicators, other than Bill's occasional fixes on his Sat Nav. He was happy watching the Sat Nav, and probably had little interest in flying anyway, so I kept flying... but how was I going to hold a heading? I could look across at his RMI, but that was not a really good long term solution. As it was a very clear day, I could fly by ground reference for a while, but in that part of the world, sand is sand, so there were not many features to pick on the horizon. So I flew on, taking my time, and thinking. During this period, I found a solution. I considered it, verified it with occasional glances to Bill's RMI, and applied it. I flew a perfect track. Eventually, Bill noticed that my RMI had dropped a flag, he commented without alarm. He asked if I was okay continuing flying, and I said I was. Over the next number of hours, he used the Sat Nav to confirm that my track was right on, and eventually asked me how I was doing it. I told him I'd tell him later. 25 flying hours later, (all but the final leg of which I was offered left seat), and many more RMI failures, I had kept my technique to myself, and he seemed content to ride along, confirming my track, and perfecting his use of the Sat nav for sailing (which interested him more than flying a Twin Otter). We arrived in Maseru and delivered the plane to Air Lesotho. At dinner he finally said: "Okay, you gotta tell me how you were doing that, you were flying perfect tracks for hours with no practical heading indicator." I explained that while flying with the RMI card stopped, I noticed that the RMI slaving meter would show the failing attempts of the remote compass to slave the card. As long as the RMI failed on the heading I wanted to fly, and I kept the slaving meter centered, to plane followed the heading. He quietly smiled. I learned to determine if something was a problem, before doing something to solve it. |
Originally Posted by scifi
(Post 10479916)
It seems as if we are assuming we don't know the actual windspeed, when this can be found by asking the nearest ATC unit for their ground windspeed, then adding the correction of twice that and add 30 degrees to find the wind velocity above 1000 ft.
. Never mind that I've seen wind speed over 150kts without hurricane warnings on the ground. https://www.pprune.org/professional-...nd-studies-14/ |
Yes I should have said A330-300 RR powered is 2.5 degrees and 78% N1 I don’t know anything about the P and W or GE 330’s Smythe—-I’m quoting Pitch attitude on the ADI......not AOA or anything else. |
Originally Posted by Smythe
(Post 10479719)
Just curious..when you state 2.5 degrees, Is this the AoA of the fuselage or the wings?
On the A333. what is the AoA delta between the fuselage and the wings? |
Originally Posted by Rad Alt Alive
Using Airbus FBW procedures as an example,...
Originally Posted by Rad Alt Alive
There is no mention anywhere, in any of our manuals, about accessing the GPS data to determine GS. There is no mention about asking ATC what our GS is. No mention of GS, full stop!
Originally Posted by Rad Alt Alive
I would instead encourage that they just follow the specific manufacturer’s procedures.
"GPS Altitude...Display on MCDU" "Refer to GPS Altitude..." to the extent that it can be used to maintain level flight. "Crosscheck all speed indications..." "Alternate sources may be used to evaluate the data (from the reliable ADR): -GPS altitude -GPS and IRS ground speeds, taking into account altitude and wind effects". Full stop indeed. |
The airspeed unreliable memory items and checklist were developed by Boeing from recommendations / guidelines published by Flight Safety Foundation.
These guidelines included, Procedures should provide information on altitude and power settings that enable crew to maintain the aircrafts flight parameters within normal limits during flight with unreliable airspeed events for all phases of flight. Procedures should address the availability and use of independent alternate sources of airspeed information (e.g. GPS, inertial, angle of attack etc.) Procedures should include memory items for critical immediate action steps The recommendations also provided an Airspeed Unreliable Generic Template, 1. Disconnect Automation - Rationale: automation may be reacting to airspeed indications that may not be correct, so it must be disconnected 2. Stabilse the aircraft with the provided pitch attitude and thrust - Rationale: setting memorised pitch attitude and thrust settings stabilise the aircraft in climb or cruise as applicable. if in a descent, the aircraft should be levelled off and the cruise setting used. There in ends the recommended memory items, reference items of the checklist then direct the amongst other items to set an applicable attitude and thrust. Boeing aircraft this information is found in the QRH PI section. In summary The initial pitch and power settings of the memory items on a Boeing aircraft are designed to keep the aircraft "safe" until such time as the accurate Pitch and Power setting s can be extracted from the QRH PI section. Regarding GPS ground speed, the elephant in the room is GPS jamming, it is becoming more and more prevalent in particular regions of the world so much so that IATA has recently issued an operator alert on the subject. |
Capn Bloggs "GPS Altitude...Display on MCDU" "Refer to GPS Altitude..." to the extent that it can be used to maintain level flight. "Crosscheck all speed indications..." "Alternate sources may be used to evaluate the data (from the reliable ADR): -GPS altitude -GPS and IRS ground speeds, taking into account altitude and wind effects". Full stop indeed. |
Originally Posted by sleeve of wizard
(Post 10480704)
Regarding GPS ground speed, the elephant in the room is GPS jamming, it is becoming more and more prevalent in particular regions of the world..
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Can GPS measure dynamic pressure ?
Did you say no ? There's your answer then. |
Can GPS measure dynamic pressure ? |
Guys if it was a good idea to use GPS or IRS ground speed for unreliable airspeed it would already have been implemented in the unreliable airspeed procedure.
In my home base, it's common to have on final a tail wind of more than 20 kt around 2500 feet AGL and a headwind on landing... The wind speed and direction change dramatically. GPS is a great tool, I used it as my primary nav instrument back in the days flying in the bush; But I would definitely not use it as a primary tool to recover from an unreliable airspeed. |
Originally Posted by Capn Bloggs
(Post 10479246)
Wiggy, I agree.
No, what's the point? When you go UAS, then note your GPS GS. Maintain it until you work out what's going on. If you pull up to 4° and pull the power back to 75% (Flying Stone/737 UAS?) at FL370, you'd better watch that GPS GS closely because it'll be reducing! Precisely, and where the Ethiopians found themselves immediately prior to the final dive: at Vmo. I wonder what the GPS GS was then... Just telling you what my FCOM says. I didn't say anything about "exactly" 250KIAS. 230-270 GPS GS who cares? At least it's not Vmo with full nose down MACS trim while maintaining the UAS "it's safe" memory numbers while your PM comes up with some numbers from the back of the QRH... I agree. My point is that GPS GS is an invaluable aid while doing that, especially down low on approach or after TO when wind effect is low/known. i started this thread to see what proportion of readers realized that GS is not just useful, but makes UAS.an easy exercise. You seem to be one of “ the few” believers! Y |
Originally Posted by FlyingStone
(Post 10478995)
Personally, I'd stick with the approved procedures for unreliable airspeed.
Your GS is 500kts. Are you safe? Could be TAS of either 650 or 350 with a 150kt wind. Neither of which will keep you flying for long at cruising FL. Y |
Originally Posted by pineteam
(Post 10481722)
Guys if it was a good idea to use GPS or IRS ground speed for unreliable airspeed it would already have been implemented in the unreliable airspeed procedure.
In my home base, it's common to have on final a tail wind of more than 20 kt around 2500 feet AGL and a headwind on landing... The wind speed and direction change dramatically. GPS is a great tool, I used it as my primary nav instrument back in the days flying in the bush; But I would definitely not use it as a primary tool to recover from an unreliable airspeed. 2500 ft tailwind 20 airfiel wind headwind 20 So your landing GS will be 20 kts less than V Ref. Say VRef 100, then fly whole approach at 120 GS. Your IAS will be 140 at 2500 and 100 on landing. Just what you were looking for- no? A perfect touchdown speed. Not approx. more commonly one has reducing headwind during final descent. Say 30 kts HW at 1000 ,and 5 kts at touchdown. VRef 100. Fly whole approach at 105 kts. GS. You will land at EXACTLY 100 VRef! this is precision flying- not guesswork. Clearly you use manufacturer Pitch/power tables too to give you a clue but then refine the outcome using GS. |
Originally Posted by wiggy
(Post 10481248)
Good point, yes it is.
Y |
Originally Posted by iceman50
(Post 10480730)
Capn Bloggs Why did you not quote the full Airbus Procedure as what you quoted would be after the stabilization of the aircraft. You can twist anything to make a point! y |
You are not going to get a gps jam just as your birds or ice or whatever it is disables your air data systems. Not going to happen. Its a cinch TAS INCREASES BY 50 kt per 10000. So if the following are at a safe speed at MSL you have all you need is this knowledge MSL 250:kts IAS AND GS FL 100. 250 kts IAS= 300 GS FL200 250 IAS = 350:GS etc etc At FL350 250:kts IAS = 450 kts. If you fly these GS in still Air you are safe. OK - then +/- the wind which is elementary maths. You could fly a whole flight from takeoff to landing using this info and always have safe margins. |
Originally Posted by Iceman
Why did you not quote the full Airbus Procedure as what you quoted would be after the stabilization of the aircraft. You can twist anything to make a point!
In any case, any reader is quite welcome to click on the link I provided (I even gave the page number, for goodness sake) to see what I was getting at. Anyway, fly any way you like. I (and YT! :ok:) will be calling Pineteam's tower for the 3000ft wind and cruising down final looking closely at the GPS speed. A "Reference Groundspeed Approach" I believe they used to call it! :} |
Originally Posted by yanrair
(Post 10482298)
Perfect. 2500 ft tailwind 20 airfiel wind headwind 20 So your landing GS will be 20 kts less than V Ref. Say VRef 100, then fly whole approach at 120 GS. Your IAS will be 140 at 2500 and 100 on landing. Just what you were looking for- no? A perfect touchdown speed. Not approx. more commonly one has reducing headwind during final descent. Say 30 kts HW at 1000 ,and 5 kts at touchdown. VRef 100. Fly whole approach at 105 kts. GS. You will land at EXACTLY 100 VRef! this is precision flying- not guesswork. Clearly you use manufacturer Pitch/power tables too to give you a clue but then refine the outcome using GS. I did not say the wind was 20 kt headwind on ground lol. It usually goes from a strong tailwind around 2500 feet to a crosswind/ light headwind. Anyway I don't deny you should not use the GS as a tool. If you are 200kt GS on short final, something is wrong. But I think it's safer to keep it simple. Pitch and Thrust is all you need to fly safely to the ground. A quick look at the GPS can help but should not be relied on. If for some reasons I have Unreliable airspeed on final, I know with 4 degree pitch and 50% N1 with F3 and gears down on A320 I'm safe. No need to do maths in a critical phase of flight and that's how Airbus expect you to fly in that case according to the QRH. =) |
I have watched this discussion with great interest. Most inputs have been from pilots who have never flown using AoA. I detect the odd Ex Military pilot who supports the use of AoA rather than the ridiculous suggestion of using GS as a substitute for IAS.
I have flown for nearly 40 years using AoA as a primary means to control my aircraft. Although IAS was used throughout, it was totally possible (and practised) to fly and land using AoA, power settings and attitude (aircraft not pilots)! AoA should be displayed in ALL aircraft and its use and relevance taught from initial pilot training right through to a Line Check or Combat Ready. |
Originally Posted by yanrair
(Post 10482298)
Perfect. 2500 ft tailwind 20 airfiel wind headwind 20 So your landing GS will be 20 kts less than V Ref. Say VRef 100, then fly whole approach at 120 GS. Your IAS will be 140 at 2500 and 100 on landing. Just what you were looking for- no? A perfect touchdown speed. Not approx. You are dangerously in error. You say you are flying 120 GS on the whole approach. There is a 20kt tailwind at the top and 20kt headwind at the bottom. That means your IAS will be 100KIAS at the top and 140 at the bottom. Great job shooting your own method in the foot with such a convincing demonstration of how easy it is to get wrong. Good news is you get to practice a stall recovery and a touch and go in one approach. |
Originally Posted by we_were_inverted
(Post 10482539)
Want a great example of an A330 with unreliable to no airspeed, and use of ground speed as a source of information? Youtube ‘Malaysian unreliable airspeed’ ...a Malaysian A330 that departed YBBN with the pitot covers still on. I’m with Dominator2 - give me AoA any day. |
Originally Posted by Capn Bloggs
(Post 10482401)
Cool it, Ice. I never claimed you do that GPS stuff BEFORE the memory items. I merely pointed to evidence that suggests that RAD ALT ALIVE's assertion that GPS isn't mentioned in any manuals appears to be rubbish. Even more concerning is that they appear to be an Airbus driver.
In any case, any reader is quite welcome to click on the link I provided (I even gave the page number, for goodness sake) to see what I was getting at. Anyway, fly any way you like. I (and YT! :ok:) will be calling Pineteam's tower for the 3000ft wind and cruising down final looking closely at the GPS speed. A "Reference Groundspeed Approach" I believe they used to call it! :} Y |
Originally Posted by oggers
(Post 10482600)
You are dangerously in error. You say you are flying 120 GS on the whole approach. There is a 20kt tailwind at the top and 20kt headwind at the bottom. That means your IAS will be 100KIAS at the top and 140 at the bottom. Great job shooting your own method in the foot with such a convincing demonstration of how easy it is to get wrong. Good news is you get to practice a stall recovery and a touch and go in one approach.
should have said fly approach at GS 80 = IAS 100 downwind maybe fly GS 140=IAS 120 point is it works. Now someone mentioned pitch /power which is paramount as a starting point. Agreed 737 it’s 6pitch/60N1 But do need your weight too. Amd on the approach your pitch power change due to headwinds. But you don’t know by how much do you ! GS solves this y |
Originally Posted by scifi
(Post 10479916)
It seems as if we are assuming we don't know the actual windspeed, when this can be found by asking the nearest ATC unit for their ground windspeed, then adding the correction of twice that and add 30 degrees to find the wind velocity above 1000 ft.
. |
The simple fact is that GS can be used in every phase of flight to back up pretty accurately PITCH POWER/WEIGHT /ALTITUDE TABLES provided by OEM. It is possible to fly completely safely an entire flight just by reference to ground speed using two things WIND TAS INCREASE WITH ALTITUDE = 50kts/1000 ft thats it. And if you are caught in a sudden chaotic UAS + SHAKER + MULTIPLE WARNING just maintain current GS PITCH AND POWER. if anyone thinks this doesn’t work get yourself on a sim. Right away. It does. Safe flying Y |
Originally Posted by yanrair
(Post 10484431)
It is possible to fly completely safely an entire flight just by reference to ground speed using two things WIND TAS INCREASE WITH ALTITUDE = 50kts/1000 ft |
[QUOTE][ou are not going to get a gps jam just as your birds or ice or whatever it is disables your air data systems. Not going to happen.
Its a cinch TAS INCREASES BY 50 kt per 10000. So if the following are at a safe speed at MSL you have all you need is this knowledge /QUOTE] is the quote I think. |
Yanrair, if it was a good idea to use GPS in an unreliable airspeed case, aircraft manufacturers would recommend using it.
Read your previous post again: 2 serious mistakes that in real life will put you in a dangerous situation. Don’t try to reinvent the wheel. |
Originally Posted by pineteam
(Post 10484533)
Yanrair, if it was a good idea to use GPS in an unreliable airspeed case, aircraft manufacturers would recommend using it.
Read your previous post again: 2 serious mistakes that in real life will put you in a dangerous situation. Don’t try to reinvent the wheel. OEM plane makers generally don’t teach airlines how to operate in difficult situations. In my last major airline a great deal of the training was developed locally the fact that I made a typo in a previous post that was glaringly obviously a typo does not alter the fact that GS is a pretty foolproof way of avoiding calamity in serious confusing UAS situations with multiple distractions. Over years I have seen pilots flying calmly through situations which, if you don’t believe that GS is a game changer , would be extremely difficult if not fatal. If AF447 had maintained 450 kts and not changed pitch and power we wouldn’t be having the tenth anniversary this week of 300+ deaths. So I am sorry, attempting to use a maths error in an otherwise proven scenario won’t change the science! thanks for pointing out the error though. I wii shortly write an error free version which I will invite you to take apart on a factual basis! y |
GS is a pretty foolproof way of avoiding calamity in serious confusing UAS situations with multiple distractions. If AF447 had maintained 450 kts and not changed pitch and power we wouldn’t be having the tenth anniversary this week of 300+ deaths. It’s quite true that GS has its uses - the ‘Reference GS’ we used to use on approach in Boeings, and the similar GS Mini in the Airbus are good examples. But I don’t agree that GS is the infallible all-purpose solution you seem to believe it is, nor can you justify using it instead of the manufacturer’s procedures. While the two major errors you’ve made so far in your justifications can be dismissed as mere typos or because it was late or something, the fact is you still made them, at zero kts, 1 G, and without the pressure of “sudden chaotic UAS + SHAKER + MULTIPLE WARNING”. It’s not really a great advertisement for what you’re trying to sell. |
Originally Posted by hans brinker
(Post 10480295)
Yeah, I'm sure they would have had an accurate ground wind reading for AF 447.
Never mind that I've seen wind speed over 150kts without hurricane warnings on the ground. https://www.pprune.org/professional-...nd-studies-14/ The wind speed at the time of the pitot tube failure was right in front of the pilots as was the GS. Didn’t need ATC. And the wind is available on every operational flight plan for every leg +/- 5 kts. Had they done nothing which is what is recommended other than maintain existing steady state conditions inc. PITCH. POWER. GS we wouldn’t be having this conversation. y |
Originally Posted by itsnotthatbloodyhard
(Post 10484606)
So is applying the memory items and/or NNCs laid down by the manufacturer. If AF447 had simply not changed pitch or power, with no reference to GS at all, the same would still be true. It’s quite true that GS has its uses - the ‘Reference GS’ we used to use on approach in Boeings, and the similar GS Mini in the Airbus are good examples. But I don’t agree that GS is the infallible all-purpose solution you seem to believe it is, nor can you justify using it instead of the manufacturer’s procedures. The existing steady state conditions are of course proven to work since that’s what you had just before the problem. I repeat if AF 447 for example had done this they could not have stalled or indeed over speeded. But after that you have to use a lot of logic to determine which if any or indeed all parameters are incorrect. And here GS is king. And as we can see here, there are people who don’t believe it! Good luck with that. Y |
Sorry. Someone just asked “ but if AF had just set PITCH POWER etc that should have been enough” It would have been a good start. But pitch/power can be out by significant margins which can over the next few seconds / minutes degrade the condition. Speed can start falling if power say 2% too low say., due to ISA + 20 for example. Nose needs to go up. Speed falls more YOU DONT KNOW THIS unless you notice your ground speed falling below where it was, or lower than flight plan. essentially this is the very point. To sit there allowing the speed to change and knowing it’s happening is - well , not a good idea and can easily lead to loss of control. I’ve seen this technique used successfully in the sim. Over and over and it works with no drama at all. Cheers y |
STEP 4 737 QRH UAS 4 CrosschecktheIRSandFMCgroundspeedand winds to determine airspeed accuracy if indicated airspeed is questionable. |
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