Oopsie

Joined: May 2015
Posts: 13
Likes: 1
From: US
Here's a clearer view of his approach. Seem like he got alittle antsy with the cyclic w/ the first bounce
https://www.facebook.com/reel/706123948945379
https://www.facebook.com/reel/706123948945379

Joined: Dec 2004
Posts: 379
Likes: 68
From: canada


Joined: Sep 2003
Posts: 2,081
Likes: 189
From: Redding CA, or on a fire somewhere
Joined: Sep 2024
Posts: 21
Likes: 3
From: Florida
Looks like an 8-10 knot tailwind to me. I found the 130 to be a handful. With the skids set so far back, just a very small amount of forward cyclic will pitch it forward when light on the skids, especially with a tailwind. This guy forgot that. I've seen it happen plenty and it happened to me once. You really have to keep flying it when on the ground and slowly lower the collective. The 130 is not a helicopter for low timers.
Joined: Feb 2025
Posts: 1
Likes: 0
From: Jefferson GA
Not necessarily pertinent to this case, I had to guard all the controls in the 350 all the time with passengers aboard. I seldom flew with dual controls (pilot seat on the right front) with a front seat passenger but even in those few cases people equated the cyclic with car steering wheel properties and would push it around, usually forward for more leg clearance. I always wondered if the 350 would go over the nose. Now I know that it could with some power applied..
Even without dual controls, you should guard the collective- the 'critters' might set their bag (and strap) between the seats, often fouling the FFL, pushing it down to shut off or pulling it up from idle to useful power. The twist grip B3s were much much better cockpits.
I loved the 350... except the Lycoming D.
Even without dual controls, you should guard the collective- the 'critters' might set their bag (and strap) between the seats, often fouling the FFL, pushing it down to shut off or pulling it up from idle to useful power. The twist grip B3s were much much better cockpits.
I loved the 350... except the Lycoming D.


Joined: Dec 2006
Posts: 431
Likes: 41
From: yes
This appears to be a dynamic rollover incident due to improper/loss of aircraft control. To be determined is the reason for the improper control inputs (incapacitated pilot, control interference, hydraulic hard-over, control system failure, etc.) A contributing factor appears to be the selected landing direction vs. wind azimuth, which would exacerbate the forward pitch due to the wind’s influence upon the horizontal stabilizer (4” wider on the EC-130 vs. AS-350) and aft landing gear fairing. Potentially, a forward CG could have had increased the susceptibility to the forward roll-over, as the EC-130 has an expanded forward CG range as compared to the AS-350. Of note, is that while the landing gear on the EC-130 gives the appearance of being further aft when compared to the AS-350, they share virtually the same forward point of contact.
Joined: Sep 2024
Posts: 21
Likes: 3
From: Florida
Or you could say they landed downwind.






