Selected Speeds on A320
Why is it that even the VApp is SELECTED in case of failures like Dual hydraulic and Slats/Flaps jammed in the A320.
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I'm only speculating here, but it could be due to the fact of being a high workload situation for the pilot flying, in such case a fixed selected speed is less workload than following a managed target affected by GS MINI.
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To reduce speed, sometimes below maneuvering speed to avoid over speed,or to only reduce speed once the flap is extended and to ensure minimum speeds are maintained when going around or diverting.
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Also because the approach and maneuvering speeds with partial flaps/slats can be different than the FMS target speeds - and the FMS might not necessarily know it.
Bottom line: non standard config - non standard speeds have to be used. |
Boyington is asking why Vapp also flown selected when it can be easily flown managed since we have corrected it in MCDU.fpuentegomez seems to have given logical answer
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i don't see any wording explicitly prohibiting the use of GS mini in mentioned cases once you're in LDG config given VAPP is amended accordingly in MCDU
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Because the autothrust system will not allow the speed to decrease below the manoeuvring speed, if you keep the speed managed.
If you have the flaps stuck at 1+f for example, you'll need flap lever position 2 for landing. (to get the slats extended in position 2) The calculated Vapp will be lower than the manoeuvring speed, so it needs to be selected. |
What exactly do you imply by manoeuvring speed? Do you mean VLS? Thanks.
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F and S speeds are manoeuvring speeds.
Check out the abnormal procedure from the FCTM as it is also explained there. |
sierra_mike
i don't see any wording explicitly prohibiting the use of GS mini in mentioned cases once you're in LDG config given VAPP is amended accordingly in MCDU KingAir1978 Because the autothrust system will not allow the speed to decrease below the manoeuvring speed, if you keep the speed managed. If you have the flaps stuck at 1+f for example, you'll need flap lever position 2 for landing. (to get the slats extended in position 2) The calculated Vapp will be lower than the manoeuvring speed, so it needs to be selected. |
Been a while since I was on the Bus, but...
I always understood a part of the reason for using selected in these instances was due to the fact you were in direct law for landing hence had no autotrim. As GS mini oscillates the speed around the workload is going to increase for the PF as he has to retrim for each change in speed, which isn't something which is regularly practiced on the Bus... Nor is convenient if you are in manual thrust too.. |
Since the QRH recommends use of select speed it takes out the GS mini out of equation. No need to expressly ban GS mini. since we use managed SPD for landing in normal daily ops i would expect airbus to explicitly tell us not to use it if they don't want us to. i.e. as they do for overweight landing procedure "SPEED AT RUNWAY THRESHOLD: VLS" |
Cough
I think in direct law to stay in trim for a fixed Vapp speed is a very valid point. However the new QRH creates an impression that managed speed can be used at Vapp. It only says decelerate to calculated Vapp. sierra_mike As you correctly noted there are some changes to Landing with slats or flaps jam QRH procedure. Following notes have been deleted: 1. Use of selected speed is recommended. 2. Autopilot may be used down to 500ft AGL. 3. ATHR is recommended except B+G LO PR warning. However in VLS greater than VFE next case is retained which can be interpreted as ATHR can be used. Below from QRH: If VLS is greater than VFE NEXT (overweight landing case), the FLAPS lever can be set in the required next position, while the speed is reduced to follow VLS reduction as surfaces extend. The VFE warning threshold should not be triggered. In this case, disconnect the A/THR . A/THR can be re-engaged when the landing configuration is established. |
If VLS is greater than VFE NEXT (overweight landing case), the FLAPS lever can be set in the required next position since we use managed SPD for landing in normal daily ops i would expect airbus to explicitly tell us not to use it if they don't want us to. |
Originally Posted by Chrome
(Post 9917935)
F and S speeds are manoeuvring speeds.
Check out the abnormal procedure from the FCTM as it is also explained there. Unless our fcom's ar different, F &S are min speeds for retraction not manoeuvring. Pro sup 10 VLS is however a manoeuvre speed. 1.13 vs after take off, 30 degree bank turn stall speed increase is approx 1.08, 1.23 vs after retraction of 1 stage, 1.28 vs clean Stall speed increase for 45 degree bank is 1.19, so you've got at least 30 bank avail + 15 over bank at VLS |
I stand corrected. According to Airbus they are manoeuvre speeds but not limitations. It is safe to fly between VLS and Vmax (VMO, VLE, VFE). The required aerodynamic margin is properly ensured. Also in Slat/flap jam Autopliot use upto 500ft. is relocated and not removed.
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Hi LHRPony,
Taken from the FCTM that I have; Abnormal Flaps/Slats Configuration Failure During The Approach ... With A/THR operative, the managed speed target will become the next manoeuvring characteristic speed e.g. S speed when selecting flap lever to 1... |
vilas
My motto is, "I wish I knew what I wish I knew." I am a huge fan of this forum. It is one of the very few places on the sewer of the internet where fresh water is available. Vilas, as a 319/320 pilot, Captain, and Line Check Airman, I always have put great value into your input into this forum. Your correction only adds to that value. |
Thanks mate!
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Cheers Chrome,
So we have fcom defining they are retraction speeds, fctm saying they are man speeds. Genuine question, what manoeuvre margin exists at the f and S? it's defined for VLS,but I haven't come across any definition for manoeuvre margin for f and s. And not wishing to get into a tit for tat, it does also say if their is a discrepancy between fcom and fctm then fcom takes precedence. But as always happy to be corrected. Thanks for your input, always good to rattle these things around and see where we end up. |
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