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-   -   Question for A330 drivers (https://www.pprune.org/tech-log/438284-question-a330-drivers.html)

michelda 2nd January 2011 07:18

Question for A330 drivers
 
Hi guys

I have a small question.....an unfortunately not only one......

ELEC EMER CONF with gen 1 off/inop and engine 2 inop: flaps are not working...
Same configuration but with gen 2 inop/off and engine 1 inop: flaps are working.
Do you know why this difference??
Thanks
Michelda

hetfield 2nd January 2011 07:51

Good morning,

I'm not current on 330, flew A300 for some years.

I guess in emer elc config only SFCC1 is working.
What about hyd systems with one eng inop on 330? Do you still have all three?
Which hyd system drives the flaps?

Maybe there you will find the answer....

spannersatcx 2nd January 2011 14:40

They will once you select land recovery.

michelda 2nd January 2011 15:38

What does it mean??
In both situation you have to push the land recovery pb.
Anyway thanks
Michelda

fantom 2nd January 2011 16:33

Ah...the magic Land Recovery button.

JABBARA 2nd January 2011 19:49

I may have an answer, if you explain how did you come this conclusion?

michelda 2nd January 2011 20:01

Hi Jabarra

I have read from 3.02.24.....

JABBARA 2nd January 2011 20:28

Still I did not understand how did you concluded from 3.02.24, but probabaly I missed some text.

Anyway you are right, and I tried to explain in the following figure

http://i1222.photobucket.com/albums/...g?t=1294003663

michelda 2nd January 2011 20:45

I found this information in emer conf 03.02.24 ( note at the end of procedure)
Your answer can be correct, but in this case what happen in case of eng 1 fault and idg 2 inop???
Thanks for your answer
Michelda

JABBARA 2nd January 2011 21:11


but in this case what happen in case of eng 1 fault and idg 2 inop???
Obviously Flaps and Slats work but at half speed.

Normally FCOM 3.02 pages does not specify the combined failures, but ECAM does. That`s why ECAM steps always reliable at very complex cases resulted from combined failures, which normally pilot cannot do simply as reading from FCOm 3.02.

That`s whay I am interested how did you come to this conclusion as simply reading FCOM 3.02.24 pages.
Can you specify the page no please 3.02.24 P??, pin point please.

ADDED LATER: Disregard my question I found it at 3.02.24 P11. Thanks

hetfield 3rd January 2011 07:55

@JABBARA


#8
Thx, that's what I meant. Same architecture as A300.

Brain Potter 4th January 2011 07:16

I agree with the above comments that with GEN 1 inop and ENG 2 failed; the aircraft will be in EMER ELEC CONFIG with flaps inop.

However, the QRH Summary for EMER ELEC CONFIG assumes that flaps will be available. It gives a VAPP of VREF+5 using FLAP3 with associated landing distances (a factor of 1.2 on a dry runway). I think that with flaps at 0, the delta VREF should be 30 knots with a landing distance factor 1.6 dry. Bearing in mind that the QRH summary is intended to provide the information to apply the landing distance procedure, obviating the need to refer to QRH 2.40, then it appears that the pilots could be led into making an approach 25 knots too slow.

Any thoughts?

JABBARA 4th January 2011 10:01

Brain Potter, a good point you noticed.

A quick answer which comes to my mind

Quote from my post

That`s why ECAM steps always reliable at very complex cases resulted from combined failures, which normally pilot cannot do simply as reading from FCOm 3.02
In your scenario, probably
FCTL FLAPS FAULT/LOCKED
ECAM willl also display, so when calculating Vapp you have to consider its effect as well.

But in any case, since the Vls always represents actual configuration, on the final if you see a Vapp above Vls your speed calculation is correct. If not, this means your speed calculation is wrong. Then simply fly a speed above Vls.


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