Use Of Flap 40 On The B737?

Joined: May 2003
Posts: 198
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From: france
hello ba 146-100,
flaps40 & flaps 30 are both boeing certified normal landing flap configurations. because flap40 generates more lift & a lot more drag, technically the difference is a lower vref( about 4 a 5 knots) for a flap 40 landing resulting in a shorter landing roll. the "price" to pay as nothing in this world is for free, is higher thrust settings on approach, resulting in higher fuelflows & more noise.
your question was: the choise between flap30 & flap40?
it is the captains decision & in accord with company policy:eg,
"preferential landing flaps setting is flap30".(low drag, low noise, lower fuel consumption, the company likes this last assumption)
"flaps40 may be selected for a landing distance available(lda) of 7000ft or less".
"flaps40 is mandatory for an lda of 6000ft or less( is considered a short field)".
"flaps40 is recommended for cat2/3 ( lower deck angle)".
other considerations may include landing weight & runway status, dry, wet or contaminated. it is good operating practice to discuss landing flap setting during the approach briefing, so both pilots agree. i totally agree with captain marvellous summary.hope this answers your question?
flaps40 & flaps 30 are both boeing certified normal landing flap configurations. because flap40 generates more lift & a lot more drag, technically the difference is a lower vref( about 4 a 5 knots) for a flap 40 landing resulting in a shorter landing roll. the "price" to pay as nothing in this world is for free, is higher thrust settings on approach, resulting in higher fuelflows & more noise.
your question was: the choise between flap30 & flap40?
it is the captains decision & in accord with company policy:eg,
"preferential landing flaps setting is flap30".(low drag, low noise, lower fuel consumption, the company likes this last assumption)
"flaps40 may be selected for a landing distance available(lda) of 7000ft or less".
"flaps40 is mandatory for an lda of 6000ft or less( is considered a short field)".
"flaps40 is recommended for cat2/3 ( lower deck angle)".
other considerations may include landing weight & runway status, dry, wet or contaminated. it is good operating practice to discuss landing flap setting during the approach briefing, so both pilots agree. i totally agree with captain marvellous summary.hope this answers your question?
Last edited by blackmail; 28th November 2004 at 13:37.
Joined: Aug 2000
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From: UK
One reason I was told was to give the aircraft more speed stability as at light weights and flap 30 it can be difficult to slow up and speed control is easier on final approach, especially in gusty conditions. I have to say it was not borne out in my experience- I never understood the logic of flying the aeroplane in an unusual configuration in the hardest circumstances only. In windy/sheary weather, if doing a low go around, I would not want that extra drag- I'd rather be climbing away as quickly as possible, and starting at flap 40 did not strike me as a good idea.
Joined: Sep 2004
Posts: 34
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From: Melbourne
My companies policy is flaps 40 for all landings. We must engage flap 40 by 1000ft. Personally i find it easier to land and control the aircraft with a flaps 30.
Reason being: The extra lift created from flap 40 gives you a high nose up attitude and causes a baloon effect just as you flare.
Flap 40 helps on short runways but is seriously not needed. Flap 30 is fine.
Reason being: The extra lift created from flap 40 gives you a high nose up attitude and causes a baloon effect just as you flare.
Flap 40 helps on short runways but is seriously not needed. Flap 30 is fine.
Joined: Sep 2000
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http://www.!!!!!!!!!!!!!!/open.file?i...%3D&static=yes
Believe me you want flaps 40 on this airstrip on a winter day when braking action is poor.
Believe me you want flaps 40 on this airstrip on a winter day when braking action is poor.

Joined: Dec 2000
Posts: 2,132
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From: on the golf course (Covid permitting)
Bantios
Are you sure? In the 737-200 /300 and /400's I flew the opposite was true.
The approach at F30 would be about 2.5deg Nose up vs F40 at 0 deg Nose Up - ie lower nose attitude with Flap 40 set. As for a balloon effect with Flap 40, would have to disagree there also - the greater drag causes for the aircraft to settle quicker than with Flap 30 when you close the thrust levers.
Maybe the 737NG is different?
Reason being: The extra lift created from flap 40 gives you a high nose up attitude and causes a baloon effect just as you flare.
The approach at F30 would be about 2.5deg Nose up vs F40 at 0 deg Nose Up - ie lower nose attitude with Flap 40 set. As for a balloon effect with Flap 40, would have to disagree there also - the greater drag causes for the aircraft to settle quicker than with Flap 30 when you close the thrust levers.
Maybe the 737NG is different?
Joined: Aug 2000
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From: UK
A very large British 747 Classic operator used to do standard full (30) flap landings instead of 25 flap. About 20+ years ago, flaps started falling off, and a Boeing team came over to see why only one very large British operator was so affected. They were not impressed as Boeing were designing the machine for standard flap 25 with 30 available for special circumstances, and stressing the system for that.
I believe the 737 up to -400 was designed this way, with mainly flap 30 intended to be used. It might be worth checking the Boeing manual itself to see if perhaps one of the airline management team is allowing a personal preference to override the manufacturers intention!
I believe the 737 up to -400 was designed this way, with mainly flap 30 intended to be used. It might be worth checking the Boeing manual itself to see if perhaps one of the airline management team is allowing a personal preference to override the manufacturers intention!
Joined: Sep 2000
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look at this
the rwy is 1640 meters long or 5400' feet.
And sometimes the braking action is reported to be towards 20 "my" (poor).
A lot of times it is a calculation whether you can land or not.
A lot of mountains around creates very unstable and rough winds.
You don't want to be without the 40 flap option.
And sometimes the braking action is reported to be towards 20 "my" (poor).
A lot of times it is a calculation whether you can land or not.
A lot of mountains around creates very unstable and rough winds.
You don't want to be without the 40 flap option.
Joined: Sep 2004
Posts: 34
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From: Melbourne
Guys,
I dont know about your airline, but our policy outlines that any runway we land on must be able to stop the plane using a FLAP 15 with MAX auto brakes available. We are not permitted to land on a 5500ft runway, even though the 737 can stop on it.
I dont know about your airline, but our policy outlines that any runway we land on must be able to stop the plane using a FLAP 15 with MAX auto brakes available. We are not permitted to land on a 5500ft runway, even though the 737 can stop on it.
Joined: Aug 2003
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From: S23 28.8 W046 37.8
Hudson, from what I understood, Bantios was saying that if they can't operate with F15 and max auto brake into one particular aiport, they don't at all.
On the other hand, on day-by-day ops, F30 (or 40) is used instead.
Cheers
On the other hand, on day-by-day ops, F30 (or 40) is used instead.
Cheers

Joined: Aug 2000
Posts: 96
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From: London
Personal preference: If the aeroplane is well below 44 tonnes, then i find F40 better for speed stability and you fly the app with a more sensible N1.
I'd rather have the response/spool up from 55ish% at F40 than flying along at 45ish% N1 with F30 at a Vref of 115-120 (esp. in light -500) and the whole thing handling like a rice-pudding....
Flap travel between 40 and 30 is pretty fast anyhow...
Performance-wise (for a G/A) i'd be suprised if there was any significant difference (If there is I'd expect it to be promulgated somewhere..)
As far as gusty conditions go.....well....if you're really light you've got 40ish+kts margin before flap-load relief is required to do its thing...
Notso: point taken about what might be in the Boeing manual...will raise the issue with our TSC....get them to clarify if any doubt.
I'd rather have the response/spool up from 55ish% at F40 than flying along at 45ish% N1 with F30 at a Vref of 115-120 (esp. in light -500) and the whole thing handling like a rice-pudding....
Flap travel between 40 and 30 is pretty fast anyhow...
Performance-wise (for a G/A) i'd be suprised if there was any significant difference (If there is I'd expect it to be promulgated somewhere..)
As far as gusty conditions go.....well....if you're really light you've got 40ish+kts margin before flap-load relief is required to do its thing...
Notso: point taken about what might be in the Boeing manual...will raise the issue with our TSC....get them to clarify if any doubt.
Last edited by Bumblebee; 1st December 2004 at 09:30.

Joined: Aug 2000
Posts: 96
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From: London
HSWL , cheers... how recent was that?...i'd be interested to read it.
btw i'd certainly make a distinction between gusty/strong wind conditions and Windshear proper.....
btw i'd certainly make a distinction between gusty/strong wind conditions and Windshear proper.....
Last edited by Bumblebee; 1st December 2004 at 10:26.
Joined: Sep 2004
Posts: 34
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From: Melbourne
HUDSON
Thankyou for understanding what I am trying to communicate here. This policy is to safegaurd us incase of flap problems (Common on the 737). Most airliners have some sort of landing policy regarding this.
Thankyou for understanding what I am trying to communicate here. This policy is to safegaurd us incase of flap problems (Common on the 737). Most airliners have some sort of landing policy regarding this.





