If all the passengers ran to the back of a 'plane...

If all the passengers ran to the back of a 'plane...

Author
Discussion

markmullen

15,877 posts

234 months

Tuesday 9th February 2016
quotequote all
I flew Eastern Airways LBA to Southampton on a Jetstream 41 and there was only seven of us on board, plus the 3 man crew, we were arranged around the cabin to balance it out.

Pan Pan Pan

9,898 posts

111 months

Tuesday 9th February 2016
quotequote all
Depending on the aircraft type and number of people, it would not be a matter of space at the rear of the aircraft, but of weight, and could result in a non retrievable condition.
The further aft away from the C of G. the less number of people (weight) would be required to destabilize the aircraft, so even a relatively small number of people doing this could put the aircraft in a non recoverable attitude.
If the passengers stayed at the rear the aircraft (even assuming the elevators were sufficient to counter the weight shift, which would not be the case) the aircraft would enter a nose high attitude so steep, the passengers at the rear would not be able to move forward through the cabin if they wanted to, even using the sides of the seats as a ladder.

anonymous-user

54 months

Tuesday 9th February 2016
quotequote all
I learnt a valuable lesson about tail tipping on the ground, having flown back from France in a Cessna 182 with a rear cabin full of wine.

When we arrived back in the UK, we both got out of the front seats only to discover that without our weight (and the weight of the fuel we'd burned en route) it was not enough to offset the weight aft. I should add that the weight and balance was fine in the air, just not so good once the two well built company directors had got out of the aircraft! Luckily, no damage was done.

Eric Mc

121,994 posts

265 months

Tuesday 9th February 2016
quotequote all
The solution would have been to neck a couple of bottle between you to move the weight from the back to the front.

That might have caused other problems, of course smile

williamp

19,255 posts

273 months

Tuesday 9th February 2016
quotequote all


Sadly even the RAF get it wrong. I think this was because the tail was too heavy wth fuel. Should have been drained first.

ATG

20,570 posts

272 months

Tuesday 9th February 2016
quotequote all
Simpo Two said:
In practice I don't think everyone could 'go to the back' because there wouldn't be room for them all.
Announce there are free peanuts at the back. There'd be a stampede.

ATG

20,570 posts

272 months

Tuesday 9th February 2016
quotequote all
Just possibly to wind us up, I was asked to reach back into the tail and move the luggage forward onto the passengers' laps ... while we were accelerating down the runway on takeoff. Zimbabwe; home of health and safety.

Kermit power

28,642 posts

213 months

Tuesday 9th February 2016
quotequote all
Pan Pan Pan said:
Depending on the aircraft type and number of people, it would not be a matter of space at the rear of the aircraft, but of weight, and could result in a non retrievable condition.
The further aft away from the C of G. the less number of people (weight) would be required to destabilize the aircraft, so even a relatively small number of people doing this could put the aircraft in a non recoverable attitude.
If the passengers stayed at the rear the aircraft (even assuming the elevators were sufficient to counter the weight shift, which would not be the case) the aircraft would enter a nose high attitude so steep, the passengers at the rear would not be able to move forward through the cabin if they wanted to, even using the sides of the seats as a ladder.
confused

Given that most people are capable of climbing a vertical ladder, why would they not be able to move forward through the cabin using the sides of the seats as a ladder? Surely it would have to be accelerating vertically at one hell of a speed for that to be the case?

Brother D

3,719 posts

176 months

Tuesday 9th February 2016
quotequote all
Weirdly on an internal flight last week myself and one other seated in the wingbox area were asked to move to the rear seat rows prior to take off. I could understand myself having over 100Kgs would help with trim, but the other one to move was a tiny asian lady possibly 30Kgs wet.

I do wonder about risks with trim, especially if you have say a rugby club sat in the rear, with say the chess club sat upfront. I don't recall seeing anything in previous partners crew training manual about identifying that scenario?






stain

1,051 posts

210 months

Tuesday 9th February 2016
quotequote all
Concorde was particularly vulnerable to lifting the nose on the ground and happened to us in the hangar once.

Pan Pan Pan

9,898 posts

111 months

Wednesday 10th February 2016
quotequote all
Kermit power said:
Pan Pan Pan said:
Depending on the aircraft type and number of people, it would not be a matter of space at the rear of the aircraft, but of weight, and could result in a non retrievable condition.
The further aft away from the C of G. the less number of people (weight) would be required to destabilize the aircraft, so even a relatively small number of people doing this could put the aircraft in a non recoverable attitude.
If the passengers stayed at the rear the aircraft (even assuming the elevators were sufficient to counter the weight shift, which would not be the case) the aircraft would enter a nose high attitude so steep, the passengers at the rear would not be able to move forward through the cabin if they wanted to, even using the sides of the seats as a ladder.
confused

Given that most people are capable of climbing a vertical ladder, why would they not be able to move forward through the cabin using the sides of the seats as a ladder? Surely it would have to be accelerating vertically at one hell of a speed for that to be the case?
Possibly you have not thought this through? If you have ever been on an airliner, you would see, that the passengers do not consist entirely of fit young athletes, capable of doing the equivalent of free climbing. You might also be aware that just getting off an aircraft after its arrival can take a surprising length of time, owing to the different age /fitness range of the passengers (even though the passengers are standing in essentially in an normal/upright position after leaving their seats)
Even if the passengers consisted entirely of fit young athletes, there would only be room for a small number to climb on the sides of the seats. The floor and overhead would give relatively few points of purchase for anyone trying to climb forward through a cabin at a steep, (if not completely vertical) orientation.
But significantly this is just nonsense, because an aircraft in this condition would have no more than a few seconds in which to correct its pitch angle, How many times have you seen fit young athletes free climb 60 to 80 feet in 3 or 4 seconds on something that is shaking owing to pre stall buffet?
It hopefully would never happen, but the most likely result would be a stall, but without the nose drop which occurs in an aircraft with correct/normal weight distribution. With a lot of weight at the rear, it is more likely a tail slide would occur, which would rip the control surfaces off the aircraft (The control surfaces are not designed, or built to cope with high airflow from the wrong direction) after which, what was left of the aircraft would descend at a high rate into the ground.

Pan Pan Pan

9,898 posts

111 months

Wednesday 10th February 2016
quotequote all
Simpo Two said:
In practice I don't think everyone could 'go to the back' because there wouldn't be room for them all.
It would not be a matter of the `number' of people, but of the weight of those moving to the rear of the aircraft, and whatever distance the distance aft of the c of G they are able to reach. So a relatively small number of people moving to the very rear of the aircraft could be enough to de stabilize the aircraft.

m1dg3

128 posts

154 months

Wednesday 10th February 2016
quotequote all
No idea how this translates to real aircraft but RC aircraft usually have the CoG located a third of the way back on the wing. Moving it as far forward as the leading edge or as far back as the trailing edge makes the plane pretty much uncontrollable. Too far forward and the controls become really sluggish, too far back and it becomes twitchy as hell.

In fact I seem to remember planes like the Eurofighter have the CoG way back to make them more agile and a computer to sort out the inherent instability.

scubadude

2,618 posts

197 months

Wednesday 10th February 2016
quotequote all
m1dg3 said:
In fact I seem to remember planes like the Eurofighter have the CoG way back to make them more agile and a computer to sort out the inherent instability.
Yeah... and computers never go wrong...

xjay1337

15,966 posts

118 months

Wednesday 10th February 2016
quotequote all
scubadude said:
m1dg3 said:
In fact I seem to remember planes like the Eurofighter have the CoG way back to make them more agile and a computer to sort out the inherent instability.
Yeah... and computers never go wrong...
I think it means more that if the FBW systems fail then the plane crashes.
Not if say some other computer systems in the plane fail then it automatically enters a deep dive of death.

J4CKO

41,530 posts

200 months

Wednesday 10th February 2016
quotequote all
Isnt this more of a problem on the ground, in the air the lift of the wing and the tail stabilise the plane, it will make a difference but I dont think it would cause the plane to point skywards and stall, the back of the plane isnt the absolute rear, everyone would be between the wing and the tail, and 150 tonnes of people take up a lot of space, passengers can be dense, but they arent that dense so it wouldnt be like a 150 tonne weight hanging off the tip of the tail, some of that load is meant to be there anyway, i.e. the rear ten rows into which they would all have to clamber.

There is 20 tonnes or so of fuel in the middle of the plane, two massive engines, cargo, luggage etc, also, this wouldn't happen instantly like the Bagram cargo shifting, it would take time and be during level flight based on the question so wouldn't the flight computer just compensate or the pilot notice it and push forward on the stick to counteract ?

Scary thought, the Airbus model 911 !

surveyor

17,817 posts

184 months

Wednesday 10th February 2016
quotequote all
J4CKO said:
Isnt this more of a problem on the ground, in the air the lift of the wing and the tail stabilise the plane, it will make a difference but I dont think it would cause the plane to point skywards and stall, the back of the plane isnt the absolute rear, everyone would be between the wing and the tail, and 150 tonnes of people take up a lot of space, passengers can be dense, but they arent that dense so it wouldnt be like a 150 tonne weight hanging off the tip of the tail, some of that load is meant to be there anyway, i.e. the rear ten rows into which they would all have to clamber.

There is 20 tonnes or so of fuel in the middle of the plane, two massive engines, cargo, luggage etc, also, this wouldn't happen instantly like the Bagram cargo shifting, it would take time and be during level flight based on the question so wouldn't the flight computer just compensate or the pilot notice it and push forward on the stick to counteract ?

Scary thought, the Airbus model 911 !
I think your right. I've heard cabin crew let people move around on smaller plans after takeoff - but they are told to return to their allocated seats for landing.

I recall getting a sleazy flight with only a handful of people before they allocated the seats. They simply asked us to spread ourselves around and not all sit at the front.

BLUETHUNDER

7,881 posts

260 months

Thursday 11th February 2016
quotequote all
The Bagram incident was down to civilian loadmasters not experienced on the tie down procedures of armoured vehicles. Two cougars ( 24 tonnes ) shifted on take off resulting in the catastrophic incident.

Dr Jekyll

23,820 posts

261 months

Thursday 11th February 2016
quotequote all
m1dg3 said:
No idea how this translates to real aircraft but RC aircraft usually have the CoG located a third of the way back on the wing. Moving it as far forward as the leading edge or as far back as the trailing edge makes the plane pretty much uncontrollable.
In engineering/aerodynamic terms an RC aircraft is a real aircraft so translates pretty closely. The aircraft is basically balanced on the wing while flying so the C of G is somewhere on it. Look at a Tiger Moth. One seat between the wings and one behind them. When flown single handed it's always the rear seat that's occupied, the front seat is near enough on the C of G so you can have it occupied or not without upsetting the balance.

Kempus

168 posts

135 months

Thursday 11th February 2016
quotequote all
I'll just leave this here as explains a few things

http://youtu.be/P_0R0eWOKns

Swept wing jets same principle but Cp is further aft due design and Mach Crit.