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KelvinD
21st Oct 2017, 22:49
I had thought of that. But then it occurred to me that possibly prior to take off when relevant figures etc were being input into computers etc, if 1 pilot mad a mistake, the other would have have spotted it and pointed it out. Then, providing all was well, during the take off run, if pilot monitoring noticed that pilot flying was not doing a good job of it, he would have either pointed it out or taken direct action. I can only assume from what i have read, all went well, the aircraft departed without hitting anything; no approach lights or localiser antennae were damaged etc

Musician
22nd Oct 2017, 04:49
Mistakes do happen. A web search finds many incidents and accidents, for example:
* https://www.skybrary.aero/index.php/Accident_and_Serious_Incident_Reports:_LOC#Incorrect_Thrust_ Computed
* http://www.ukfsc.co.uk/wp-content/uploads/2016/11/Acc-Incident-IATA-Flight-Crew-Computer-Errors-Case-Studies-Oct-2011.pdf

Meikleour
22nd Oct 2017, 08:37
I-FORD: You have only cited the all engines case regulation. The engine inop. case must also be considered - why do you not cite that also?

DaveReidUK
22nd Oct 2017, 09:19
Not true.

See post #238, where the OP cited both the N and N-1 cases.

Musician
22nd Oct 2017, 10:05
It is considered: "determined under paragraph 25.111" refers to the engine inop case.

Prober
22nd Oct 2017, 20:02
We do not know where V1 was. Almost certainly it had passed some way back and thus there would have been no question of stopping at that rather late point on the runway. It would seem as if there was then a rather dozy rotation which, though looking rather alarming, was, in act, no big deal.

Herod
22nd Oct 2017, 20:31
Prober. Agreed. That's about what I've been trying to say since about page one.

Musician
23rd Oct 2017, 01:41
Was the "rather dozy rotation" a safety issue? That is the open question.

There may have been no danger of damage or injury, but the plane did use some of the safety margins designed into the take-off procedure. Is this an "occurrence" or is it business as usual?

EU regulation on mandatory occurrence reporting, Annex I "Occurrences related to the Operation of the Aircraft", 1. Air Operations, 1.3 "Take-off and landing", (5) "Inability to achieve required or expected performance during take-off, go-around or landing", or (6) "Actual or attempted take-off, approach or landing with incorrect configuration setting": did we see that here or not? Or can we not determine this from the video?

I think this is the reason (well, not the regulation, but the thought behind the regulation) why we have been discussing take-off performance and screen height for the past few days.

biggles61
23rd Oct 2017, 09:31
Flap 1 improved climb

RAT 5
23rd Oct 2017, 12:03
Not from 2000m with options of up to F25 & 26K and a 1.30hr flight. Doubt it. I vote for, as was speculated about on page one, by many, it was a gentlemanly rotation so as not to scare the children on board and give the plane spotters some close up pics.

FullWings
23rd Oct 2017, 12:12
Prober, that makes sense.

When I go flying at work, I try to execute things under my control by SOP. Amongst other things that means taking off with the correct thrust and flap settings from the right place on the runway (and the right runway).

It also means rotating at the right rate from the right speed; I have to say that due to the vagaries of trim, different airframes and environmental conditions there is a certain spread to my efforts and those of my partner-in-crime on the day.

As to the effects? Well, Boeing FCTMs carry interesting diagrams showing slow and under rotation and the difference to 35’, which can be quite noticeable. Both errors cause the the takeoff flight path to be lower, which is undesirable and to be avoided (just to be clear) but not necessarily much more dangerous than normal in the way you might expect just by looking at it from the side.

If the power setting was correct, then stopping from <V1 should be assured. In the event of a thrust loss at V1, the general technique is a slower rotation to a lower pitch attitude - as the acceleration is less from that point there is more time to get it right, plus there might be a little more concentration from all parties.

Past V1 without a failure, in energy terms you are rising above the OEI flightpath with every second that you have AEO. Should you experience a thrust loss when airborne, you will be at V2+ and most likely getting a better climb gradient.

TL;DR: An improper (slow) rotation reduces margins but unless it’s so slow you don’t leave the ground, it’s unlikely to cause an issue, even with a subsequent engine failure. However, you should always aim to follow FCTM guidance as closely as possible (has to be said).

Jwscud
23rd Oct 2017, 21:18
The other side of the slow rotation is that the 738 is prone to tailstrikes, and Ryanair hammer tailstrike awareness in cadets, leading some to err on the slow side of the recommended rotation rate.

I recall RYR training material emphasising 2°/sec where the FCTM states 2-3°/sec with rates slower in longer aircraft. If you are targeting 2°/sec and you undershoot it’s easy to eat a lot of runway. The NG rotation also tends to “stick” at 8-10°NU as the tail enters ground effect.

sprite1
28th Oct 2017, 17:05
This is a gas thread.

TORA is Take-Off Run Available. That means the physical distance of paved runway.

TODA is Take-Off Distance Available. That distance includes TORA plus any published Clearway.

Clearway can be used for take-off perf calculations to attain your 35' Screen Height (Dry).

Yes, it looked unusual. It liked tight. But without a shadow of a doubt, they made 35' by the end of the TODA.

With the way Rwy 27 is, you can bet they had a large V1 to Vr split. But once they had an engine failure at V1, they'd be using all the available TORA remaining to accelerate to Vr and then use the Clearway to get to Screen Height.

Most runways aren't 2000m anymore. Coupled that with the unusual slope characteristics of Runway 27 and 1000m of Clearway and you'll get that type of take-off we see in the video.

My post history will show I hate all things Ryanair. But this is bordering on the ridiculous at this stage.

sprite1
28th Oct 2017, 17:34
A Clearway aids/permits heavier aircraft to use shorter runways that otherwise wouldn't have been allowed, performance wise.
If there was no Clearway at Bristol, Rwy 27, that Ryanair flight would either be pax limited commercially (like BHD) or have to do a tech stop en-route.

I understand from a previous poster this flight was off to the Canaries? Full load?
If that's the case, I can absolutely see how the wheels maybe, apparently, just left the paved surface at the very end. It's the very existence of the 1000m Clearway that allowed them to do it the way we saw in the video.

There was nothing illegal/dangerous/crew error/etc etc about this.

I hope the people writing that this take-off was clearly abnormal are not commercial pilots. Your perf and your knowledge and understanding of it is your bread & butter of flying. On a par with pitch & power. It is absolutely the fundamental thing keeping you alive.

How does one go about closing a thread?

fireflybob
28th Oct 2017, 18:07
I understand from a previous poster this flight was off to the Canaries? Full load?

Previous posts state the destination was Bergerac (France) so not that far - circa one hour's flying time?

If anyone wants to know the ramifications of clearway then fill your boots here!

Clearway (http://www.pprune.org/tech-log/393405-effect-clearway.html?highlight=clearway)

sprite1
28th Oct 2017, 18:26
Ok, fair enough. But then I'd be asking did they tanker round trip etc.

The key to this whole thread though is the fact there is 1000m of Clearway on Rwy 27 that permit the aircraft to basically, how should I put it, scrape off the runway like we saw in the video.

It's all legal etc, regardless of how it looks.

Anyway.

slowjet
29th Oct 2017, 11:05
Sprite, where were you earlier in the thread ? Could have stopped all the ensuing rubbish a lot earlier but it was quite entertaining, in parts. By the way, very neatly articulated.

roving
29th Oct 2017, 13:55
The key to this whole thread though is the fact there is 1000m of Clearway on Rwy 27 that permit the aircraft to basically, how should I put it, scrape off the runway like we saw in the video.

It's all legal etc, regardless of how it looks.


CWY
Description

In aviation, clearway is a term related to the dimension of some runways and it is abbreviated with CWY. A clearway is an area beyond the paved runway, free of obstructions and under the control of the airport authorities. The length of the clearway may be included in the length of the takeoff distance available (TODA). For example, if a paved runway is 2000 m long and there are 400 m of clearway beyond the end of the runway, the takeoff distance available is 2400 m long.


I venture to suggest that for an area to qualify as a "clearway" it has to meet the ordinary meaning of that word, i.e. a way which is clear and unobstructed. As appears from Google maps, in the direction of takeoff on RWY 27 there is indeed a clear and unobstructed area of grassland beyond the runway that appears to meet the description of a clearway. Once the lights/fence/road is reached it is no longer a "clearway' because it is obstructed.

Does that area of grassland stretch 1000 metres beyond the runway?

The Ancient Geek
29th Oct 2017, 14:51
I venture to suggest that for an area to qualify as a "clearway" it has to meet the ordinary meaning of that word, i.e. a way which is clear and unobstructed. As appears from Google maps, in the direction of takeoff on RWY 27 there is indeed a clear and unobstructed area of grassland beyond the runway that appears to meet the description of a clearway. Once the lights/fence/road is reached it is no longer a "clearway' because it is obstructed.

Does that area of grassland stretch 1000 metres beyond the runway?

The lower limit of a clearway is defined by a slope angle (ISTR 1 in 60 but ICBW) which assumes a minimal angle of climb. Bristol is on a hill and the ground beyond 27 falls away rapidly. All you need to do is clear the ILS antennas.

DaveReidUK
29th Oct 2017, 17:59
Does that area of grassland stretch 1000 metres beyond the runway?Probably not. But as your image is of the 09 clearway, not that of 27, it's of no relevance.

sprite1
29th Oct 2017, 19:22
Sprite, where were you earlier in the thread ? Could have stopped all the ensuing rubbish a lot earlier but it was quite entertaining, in parts. By the way, very neatly articulated.

Hah! To be honest, I've been following it from the start and thought it'd be quickly ended by someone else so didn't bother writing. I guess 14 pages is my limit!

FlightDetent
29th Oct 2017, 22:20
I agree in general with sprite1 that what we see is just a distance-limited take off, at the edge of calculated figures. It's not a common occurence and thus looks scary a bit. The video shows them get airborne about 300 m before runway end, all good. Maybe with a small tailwind blow around Vr. With the way Rwy 27 is, you can bet they had a large V1 to Vr split. But once they had an engine failure at V1, they'd be using all the available TORA remaining to accelerate to Vr and then use the Clearway to get to Screen Height. This however needs to be tweaked, for the sake of completeness.

Accelerate to Vr, then pitch up to the unstick attitude and the aircraft gets airborne dozens meters further, at Vlf. From the lift-off, the trajectory continues until 35' height still accelerating to reach V2 concurrently. Now, the geometrical half-way point (equidistant) between getting airborne at Vlf and 35' with V2 must be still inside the paved and designated TORA (TOR<=TORA). That would be applicable for dry runway take-off with 1 ENG inop on a twin, derived from TOR definition JAR 25.113 Subpart B.

Post intended solely as an expansion of what sprite1 contributed above.

Musician
30th Oct 2017, 07:05
Accelerate to Vr, then pitch up to the unstick attitude and the aircraft gets airborne dozens meters further, at Vlf. From the lift-off, the trajectory continues until 35' height still accelerating to reach V2 concurrently. Now, the geometrical half-way point (equidistant) between getting airborne at Vlf and 35' with V2 must be still inside the paved and designated TORA (TOR<=TORA). That would be applicable for dry runway take-off with 1 ENG inop on a twin, derived from TOR definition JAR 25.113 Subpart B.
By this regulation, for all-engine ops, the distance from the start of the run to that half-way point is extended by 15% to yield the take-off run (TOR). You couldn't do that with the flight in the video and still be within TORA. Was that "required or expected performance during take-off"?

P.S.: JAR 25.113 is CS 25.113 now. It still says the same as FAR 25.113.

RAT 5
30th Oct 2017, 07:35
How many pages would this have been if they'd gone grass cutting? Possibly less.

Musician
30th Oct 2017, 08:01
How many pages would this have been if they'd gone grass cutting? Possibly less.
But that's the point, isn't it? That you can have a safety problem even when you haven't experienced any consequences (yet?). They're just easier to pin down when you have consequences to point to, but when you don't, it's debatable that a problem even exists. ("Debatable" = "many pages of posts." :p )

Mikehotel152
30th Oct 2017, 11:05
The other side of the slow rotation is that the 738 is prone to tailstrikes, and Ryanair hammer tailstrike awareness in cadets, leading some to err on the slow side of the recommended rotation rate.

I recall RYR training material emphasising 2°/sec where the FCTM states 2-3°/sec with rates slower in longer aircraft. If you are targeting 2°/sec and you undershoot it’s easy to eat a lot of runway. The NG rotation also tends to “stick” at 8-10°NU as the tail enters ground effect.

In my experience of the latest FR cadets, rotation is, if anything, a little fast for my liking.

FlightDetent
30th Oct 2017, 13:03
@musician: Correct. You are referring to all engine case with +15% margin, which I had purposefully avoided. Only tried to put more detail to spirte1's: lose an engine - use all remaining tarmac to rotate.