C-130 problem solved
Discussion
The article below illustrates how a tiny change in a component can have unexpected consequences
http://www.stripes.com/news/us/keesler-technicians...
http://www.stripes.com/news/us/keesler-technicians...
Eric Mc said:
Is this just a C-130J problem or does it effect older variants?
It does say in the article that it (the problem) came about after 2004 in C-130Js Eric.I suppose when we see C-130 we, I certainly, tend to forget that a new engine and fuel system regime changes a lot about a machine's components
It changed the need for underwing tanks for a start
rkem said:
The air con packs in the J are indeed different to the K. More powerful and apparently more noxious!
We also have external tanks as well so I don't know what the last poster meant...
That poster meant that he'd not seen pictures of Js with underwingtanksWe also have external tanks as well so I don't know what the last poster meant...
He had understood that the Js used fuel more efficiently and were not in need of the extra drag
He is sorry if his ignorance was taken as arrogance
The J model has the capability to have the Ext tanks fitted but, owing to it's more efficient engines, does not routinely carry, them unlike the K.
As a K driver I wonder about the lack of 'wing bending relief' operating in this manner and am convinced this is why the J's wing shoulder joints failed so much earlier than those on the K.
As a K driver I wonder about the lack of 'wing bending relief' operating in this manner and am convinced this is why the J's wing shoulder joints failed so much earlier than those on the K.
I didn't know that about the C4; the SOP must have changed since it entered service, so thanks for that.
IIRC on the K, basic wing bending relief was accounted for by ensuring the outboard Mains were heavier by 715 lbs than the inboards and that if carrying fuel in the Aux tanks then it would be used first.
Without reference to the Aircrew Manual I can't remember the relationship(s) between APS (Aircraft Prepared for Service weight), ZFW (Zero Fuel Weight), Fuel Load and the Vno curves (Velocity Normal operating).
IIRC on the K, basic wing bending relief was accounted for by ensuring the outboard Mains were heavier by 715 lbs than the inboards and that if carrying fuel in the Aux tanks then it would be used first.
Without reference to the Aircrew Manual I can't remember the relationship(s) between APS (Aircraft Prepared for Service weight), ZFW (Zero Fuel Weight), Fuel Load and the Vno curves (Velocity Normal operating).
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