Go-around A320 Slats /Flaps Jammed
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Go-around A320 Slats /Flaps Jammed
In 320 slats/flaps checklist for go-around it says
1)if slats fault for circuit mantain the config.recommended speed :Max speed -10 knots and for diversion SELECT CLEAN CONFIG.How do we select clean config if our slats are suppose stuck at 3?
2)if flaps fault for diversion it’s says if flaps jammed >0 recommended speed:Max speed-10.
why is there a difference in procedure of slats and flaps?
1)if slats fault for circuit mantain the config.recommended speed :Max speed -10 knots and for diversion SELECT CLEAN CONFIG.How do we select clean config if our slats are suppose stuck at 3?
2)if flaps fault for diversion it’s says if flaps jammed >0 recommended speed:Max speed-10.
why is there a difference in procedure of slats and flaps?
1) Airbus are asking you to move the flaps lever to config zero. The flaps lever position signals flight phase changes to the aircraft systems, and you can still move the lever even though the actual physical slats/flap surfaces might be jammed. For example, with flaps lever set at config 1 or above; go-around mode is available.
2) Can you be more specific with your question?
2) Can you be more specific with your question?
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1) Airbus are asking you to move the flaps lever to config zero. The flaps lever position signals flight phase changes to the aircraft systems, and you can still move the lever even though the actual physical slats/flap surfaces might be jammed. For example, with flaps lever set at config 1 or above; go-around mode is available.
2) Can you be more specific with your question?
2) Can you be more specific with your question?
Last edited by vilas; 1st Aug 2020 at 11:28.
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In 320 slats/flaps checklist for go-around it says
1)if slats fault for circuit mantain the config.recommended speed :Max speed -10 knots and for diversion SELECT CLEAN CONFIG.How do we select clean config if our slats are suppose stuck at 3?
2)if flaps fault for diversion it’s says if flaps jammed >0 recommended speed:Max speed-10.
why is there a difference in procedure of slats and flaps?
1)if slats fault for circuit mantain the config.recommended speed :Max speed -10 knots and for diversion SELECT CLEAN CONFIG.How do we select clean config if our slats are suppose stuck at 3?
2)if flaps fault for diversion it’s says if flaps jammed >0 recommended speed:Max speed-10.
why is there a difference in procedure of slats and flaps?
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The procedure is poorly written. For diversion with slat fault it only says Select clean configuration. It naturally creates a question mark how to do it when slat is jammed. Then if you could do it because it's jammed at zero then why speed restriction of MaX speed-10? In case of Flaps fault it gives two cases, one jammed at zero where you retract slat to zero and then use normal speed and second jammed at >0 where speed is restricted to MAX-10. Obviously the Slat fault is to be taken as Slat jammed>0.
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Hello everyone....
the only reason behind this procedure is DRAG....
Diverting with flaps stuck down causes a lot of drag and fuel burn compared with diversion with slats out & flaps retracted....
the only reason behind this procedure is DRAG....
Diverting with flaps stuck down causes a lot of drag and fuel burn compared with diversion with slats out & flaps retracted....
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There is difference in procedure for flaps jammed =0 and flaps jammed>0 while it is silent on slat>0 why is that?
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Sorry, don’t understand that:
Scenario: you have flaps stuck near 0 and slats normal. You fly the approach with a VAPP of lets say 165kt. You go around. It says max speed -10 and maintain config. So the max speed would be in the red band and something around 190kts. So we accelerate after the go around into the red band to fly a circuit? Correct?
And the other question: slats stuck , procedure done, approach and go around plus diversion. Select clean config. Ok flaps are zero and the slats still out. Max speed will be something with 190kt. The NEW max speed is the speed for the current configuration?So we divert with that speed?
Thanks guys
Scenario: you have flaps stuck near 0 and slats normal. You fly the approach with a VAPP of lets say 165kt. You go around. It says max speed -10 and maintain config. So the max speed would be in the red band and something around 190kts. So we accelerate after the go around into the red band to fly a circuit? Correct?
And the other question: slats stuck , procedure done, approach and go around plus diversion. Select clean config. Ok flaps are zero and the slats still out. Max speed will be something with 190kt. The NEW max speed is the speed for the current configuration?So we divert with that speed?
Thanks guys
Only half a speed-brake
The first sounds alright to me, except one thing.
Vls 60t ~ 135 kt. For Flaps stuck at 0,5 (less than 1 but not fully retracted) and completely operational slats, deltaVapp(failure) is +25 kt and flap-lever position "3".
Vapp = 135+25 = 160 (no further additives because of the large already increment), as you extend the LE devices according to procedure, the Slats will end up at 22° (middle extended dot) called "position 3"
ref: FCOM DSC-27-30-20 "A".
Your MAX SPD per the QRH table is 200 kts. For circuit, the procedure says not to change the configuration and fly @ -10 kt = 190 kt. That would be inside the red, because for "position 3" normally associated with slats = middle dot, flaps = 3rd dot, the barber pole indicates (according to lever position) 185 kt Vfe.
Vls 60t ~ 135 kt. For Flaps stuck at 0,5 (less than 1 but not fully retracted) and completely operational slats, deltaVapp(failure) is +25 kt and flap-lever position "3".
Vapp = 135+25 = 160 (no further additives because of the large already increment), as you extend the LE devices according to procedure, the Slats will end up at 22° (middle extended dot) called "position 3"
ref: FCOM DSC-27-30-20 "A".
Your MAX SPD per the QRH table is 200 kts. For circuit, the procedure says not to change the configuration and fly @ -10 kt = 190 kt. That would be inside the red, because for "position 3" normally associated with slats = middle dot, flaps = 3rd dot, the barber pole indicates (according to lever position) 185 kt Vfe.
Only half a speed-brake
The other question, while rarely rehearsed, I agree the MAX SPD is dynamic.
Assuming Slats stuck just little extended (<1)
the landing conf is S=0,25/F=3 ..... max spd 185
> > > retract one step above max spd -10kt and get S=0,25/F=2 ..... max spd 200
> > > retract one step above max spd -10kt and get S=0,25/F=1 ..... max spd 215
> > > retract one step above max spd -10kt and get S=0,25/F=0 a.k.a. "select clean configuration" = with flap lever at "0" ..... max spd 230
and fly the diversion at 230 -10 kt.
Assuming Slats stuck just little extended (<1)
the landing conf is S=0,25/F=3 ..... max spd 185
> > > retract one step above max spd -10kt and get S=0,25/F=2 ..... max spd 200
> > > retract one step above max spd -10kt and get S=0,25/F=1 ..... max spd 215
> > > retract one step above max spd -10kt and get S=0,25/F=0 a.k.a. "select clean configuration" = with flap lever at "0" ..... max spd 230
and fly the diversion at 230 -10 kt.
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The first sounds alright to me, except one thing.
Vls 60t ~ 135 kt. For Flaps stuck at 0,5 (less than 1 but not fully retracted) and completely operational slats, deltaVapp(failure) is +25 kt and flap-lever position "3".
Vapp = 135+25 = 160 (no further additives because of the large already increment), as you extend the LE devices according to procedure, the Slats will end up at 22° (middle extended dot) called "position 3"
ref: FCOM DSC-27-30-20 "A".
Your MAX SPD per the QRH table is 200 kts. For circuit, the procedure says not to change the configuration and fly @ -10 kt = 190 kt. That would be inside the red, because for "position 3" normally associated with slats = middle dot, flaps = 3rd dot, the barber pole indicates (according to lever position) 185 kt Vfe.
Vls 60t ~ 135 kt. For Flaps stuck at 0,5 (less than 1 but not fully retracted) and completely operational slats, deltaVapp(failure) is +25 kt and flap-lever position "3".
Vapp = 135+25 = 160 (no further additives because of the large already increment), as you extend the LE devices according to procedure, the Slats will end up at 22° (middle extended dot) called "position 3"
ref: FCOM DSC-27-30-20 "A".
Your MAX SPD per the QRH table is 200 kts. For circuit, the procedure says not to change the configuration and fly @ -10 kt = 190 kt. That would be inside the red, because for "position 3" normally associated with slats = middle dot, flaps = 3rd dot, the barber pole indicates (according to lever position) 185 kt Vfe.
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If SLATS are jammed regardless of their position we can safely clean up the FLAPS as the airplane will have no adverse aerodynamics issues even with SLATS psn 3 and FLAPS 0. The opposite is not true, this is why when talking about Slats/Flaps locked we have only one condition which will lead the airplane in ALTN LAW, that is less than 17deg of Slats (less than Flaps position 1) and more than 13deg of FLAPS (At or above CONF2, but it would be more correct to say above Flaps position 1 imho).
In the above scenario the airplane is unable to retain Normal law due to the likelihood to hit easily alpha prot given the reduced stalling AOA and ALTN LAW intervenes without reduced protections to avoid UAS induced by the protections.
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Thanks folks,
so basically, if i stay i keep the setup and the max speed minus 10. When i divert out of the go around i do change the config setting when initiating the go around right? So goaround-flaps?
so basically, if i stay i keep the setup and the max speed minus 10. When i divert out of the go around i do change the config setting when initiating the go around right? So goaround-flaps?
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If You have briefed that in case of go around you would start a diversion then it is according to the type of jam you have as discussed above. If you can clean up, then it will be a normal go around profile with GA/Flaps.
One of the main points to remember of this failure is that you don't want to fly with Flaps extended and no Slats.
Generally speaking Slats/Flaps failure are often practiced in the SIM during takeoff when you do have plenty of fuel and no time pressure at all; actually quite the opposite as burning fuel and decreasing your weight is quite beneficial in that scenario.
Issues start if jams occur during final approach at or just slightly above minimum diversion fuel; that's where an adequate workload management will be essential to get out of troubles, especially if the destination is a short runway.
Only half a speed-brake
Disagree.
Even if in your particular case there is no danger because moving the lever from 3 to 2 retains the same S position at 22 deg and nothing else moves,
nowhere does it say you should retract at the GA initiation. E.g. for go around (and circuit) you retain the approach conf, they say.
It is only for the diversion where you are instructed to clean up >>>> by increasing speed manually to above_Vmax minus 10... and then retracting one notch at a time.
.. that reads to me as the acceleration segment, not the 1st or 2nd of a GA proc.
The normal G/A per SOP has its scope of use. Just because it is not spelled out explicitly does not mean it is perfectly universal.
Even if in your particular case there is no danger because moving the lever from 3 to 2 retains the same S position at 22 deg and nothing else moves,
nowhere does it say you should retract at the GA initiation. E.g. for go around (and circuit) you retain the approach conf, they say.
It is only for the diversion where you are instructed to clean up >>>> by increasing speed manually to above_Vmax minus 10... and then retracting one notch at a time.
.. that reads to me as the acceleration segment, not the 1st or 2nd of a GA proc.
The normal G/A per SOP has its scope of use. Just because it is not spelled out explicitly does not mean it is perfectly universal.
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I posted it before that go around flaps is really applicable to flap full. It has performance issue. Flap3 to 2 or 2 to 1 is done for standardization. This was in Airbus discussion. Here when flaps are stuck between zero to two one step retraction doesn't move anything. Bu you can leave it till deciding to divert. Another issue is if you have to do another instrument approach then what? You do it with landing flap i.e.mostly 3 or retract to 2. Slat jam case it will move flap to 2. As for as diversion is concerned slat jam it asks you to retract flaps but in case of flap jam leave slat as they are. Slat/flap jam is critical during approach because with FPF 60%,80% and 180% for slat, flap, gear you aren't going anywhere. That's why only green fail looks innocuous but if weather is poor then putting gear down requires some consideration. Because you can't divert. In case of goaround would you hold for sometime for weather improvement or keep shooting approaches burning fuel needs some thought.
