First Choice Airways 757 Reverse thrust
Joined: Aug 2003
Posts: 361
Likes: 0
From: UK
These pics would say otherwise....
http://www.!!!!!!!!!!!!!!/photos/small/6/9/6/924696.jpg
http://www.!!!!!!!!!!!!!!/photos/small/0/1/4/888410.jpg
http://www.!!!!!!!!!!!!!!/photos/small/1/9/1/857191.jpg
http://www.!!!!!!!!!!!!!!/photos/small/3/6/4/827463.jpg
http://www.!!!!!!!!!!!!!!/photos/small/3/6/5/772563.jpg
http://www.!!!!!!!!!!!!!!/photos/small/0/5/9/762950.jpg
http://www.!!!!!!!!!!!!!!/photos/small/6/9/6/924696.jpg
http://www.!!!!!!!!!!!!!!/photos/small/0/1/4/888410.jpg
http://www.!!!!!!!!!!!!!!/photos/small/1/9/1/857191.jpg
http://www.!!!!!!!!!!!!!!/photos/small/3/6/4/827463.jpg
http://www.!!!!!!!!!!!!!!/photos/small/3/6/5/772563.jpg
http://www.!!!!!!!!!!!!!!/photos/small/0/5/9/762950.jpg
Thread Starter
Joined: Oct 2005
Posts: 24
Likes: 0
From: Bristol, Easton BS5
HFS,
cheers mate, but in january we landed in manchester with 40kts gusting winds (i asked the SFO after the flight). remember the beginning of the year when we had those gale force winds.
reverse thrust wasnt used then, either.
cheers mate, but in january we landed in manchester with 40kts gusting winds (i asked the SFO after the flight). remember the beginning of the year when we had those gale force winds.
reverse thrust wasnt used then, either.

Joined: Sep 1999
Posts: 311
Likes: 6
From: UK
Only idle reverse is used at FCA. So the reverser cowlings will still be seen to be deployed but no increase in thrust. This is deamed because carbon brakes are cheaper than the enhance engine wear. Also with high amounts of reverse, particularly at the slower end of the speed regime there is always a danger of sucking up stones/debris etc. which will potentially cause fundamental damage to an engine.
Hope that answers your question?!
LOC
(SFO for FCA)
Hope that answers your question?!
LOC
(SFO for FCA)
Joined: Sep 2005
Posts: 185
Likes: 0
From: UK
360 degree mason - If it's gusting 40knots mostly down the runway, this will actually help braking, thereby reducing the need for reverse thrust. If it was all across then the runway length and condition would decide if reverse thrust was required, and if there was a tailwind component it would be reversers and hard on the brakes!
Joined: Apr 2005
Posts: 569
Likes: 0
From: Stockholm Sweden
In the technical office, one engineer looks after wheels and brakes and another looks after engines. You have some problem with the brakes wearing out and the wheel man says to the pilots use thrust reverse. Then a reverser fails and the engine man says use the brakes. This used to happen frequently years ago, but nowadays the balance usually swings towards using the brakes. On a normal landing reverse thrust will be selected to idle only and the brakes will stop the aircraft.
Note that the A380 only has two thrust reversers!
Note that the A380 only has two thrust reversers!
Joined: Dec 2003
Posts: 147
Likes: 0
From: South of Watford
Mutt
Yes it is used in the calculations. On the 744 for example using Flap25 and autobrake 2, 2reversers reduce the landing distance by about 200ft, 4 reversers by about 450 feet ( if my memory serves me correctly)
Using autobrake 3 the difference is about 40 ft and 90 ft.
Autobrake 4 and Max have no difference.
Yes it is used in the calculations. On the 744 for example using Flap25 and autobrake 2, 2reversers reduce the landing distance by about 200ft, 4 reversers by about 450 feet ( if my memory serves me correctly)
Using autobrake 3 the difference is about 40 ft and 90 ft.
Autobrake 4 and Max have no difference.
Joined: Dec 2003
Posts: 147
Likes: 0
From: South of Watford
According to Mr Boeing, these will be the achieved landing distances under various conditions, a table is provided to work it out.
The table has a basic landing distance from the runway end and then a series of additions/subtractions depending on aircraft weight, altitude, head/tail wind, temperature, runway slope, speed increments above Vref and 2 or 0 reverse.
Reverse Thrust reduces the Brake Energy but makes lots of noise and vibration doing it.
The table has a basic landing distance from the runway end and then a series of additions/subtractions depending on aircraft weight, altitude, head/tail wind, temperature, runway slope, speed increments above Vref and 2 or 0 reverse.
Reverse Thrust reduces the Brake Energy but makes lots of noise and vibration doing it.
Last edited by Sir Richard; 3rd October 2005 at 15:47.





