A 330 FUEL LEAK PROCEDURE

[JABBARA]

After Air Transat Incident, Airbus made many changes at FUEL LEAK QRH procedure. However I guess still there is a missing point.

Here is the last part of FUEL LEAK [CASE 1] procedure [PRO-ABN-28 P 17/26]:


If leak continues (after engine shutdown):
If the inner tank fuel quantity of the affected side continues to decrease, a leak from the wing may be suspected.
ENGINE RESTART................................................CONSI DER
FUEL LOSS REDUCTION proc................ ................CONSIDER
Refer to PRO-ABN-28 FUEL LOSS REDUCTION.

Question: Since Wing Tank Leakage is suspected, there should have been another Step, why the following step is not there?

INR TK SPLIT (Effected side).................................ON

Any comment?