I think they did not assume anything - but there is a suspicion that it could be an airframe failure, and that is enough.
On the other hand, don't forget that these are old aircraft, and they were not designed by nor built by the current holder of the certificate (Boeing), so, since the FAA will be heavily influenced by the holder of the certificate, and they in turn might just welcome the opportunity to drop support of this aircraft, and would not be unhappy if they were permanently grounded!
John
JDNSW
1986 110 County 3.9 diesel
1970 2a 109 2.25 petrol
No wonder we don't have a bloody clue what's really going on. OK, I know that most of us are aware of the rising tide of AI fakes, but...
Oh yeah, it has a sponsored section...
JayTee
Nullus Anxietus
Cancer is gender blind.
2000 D2 TD5 Auto: Tins
1994 D1 300TDi Manual: Dave
1980 SIII Petrol Tray: Doris
OKApotamus #74
Nanocom, D2 TD5 only.
Right on rotation one engine fails and breaks off and takes out the second engine.
Or maybe the engine doesn't fail .. maybe it just breaks off. I'm told rotation is one of the highest centripetal loads on everything.
2005 Defender 110
Prelim report :
https://leehamnews.com/wp-content/up...4-UPS-MD11.pdf
MY08 D3 - The Antichrist - "Permagrimace". Turn the key and play the "will it get me home again" lottery.
Yep. Looks like a structural failure. That explains why they grounded the entire type.
MY08 D3 - The Antichrist - "Permagrimace". Turn the key and play the "will it get me home again" lottery.
Yes, it was a structural failure, but was it initiated by :- design, maintenance design, maintenance practices*, or engine vibration outside design parameters.
My guess is the fatigue failure of the mount long predated this flight, which seems to exonerate the engine.
*see the DC-10 crash resulting from unauthorised practice of removing engine plus pylon instead of engine alone.
John
JDNSW
1986 110 County 3.9 diesel
1970 2a 109 2.25 petrol
The report basically says the aft mount failed :
"After initial cleaning of the fracture surfaces, examination of the left pylon aft mount lug
fractures found evidence of fatigue cracks in addition to areas of overstress failure. On the aft
lug, on both the inboard and outboard fracture surfaces, a fatigue crack was observed where
the aft lug bore met the aft lug forward face. For the forward lug's inboard fracture surface,
fatigue cracks were observed along the lug bore. For the forward lug's outboard fracture
surface, the fracture consisted entirely of overstress with no indications of fatigue cracking."
MY08 D3 - The Antichrist - "Permagrimace". Turn the key and play the "will it get me home again" lottery.
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