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Posted

"bolt was liberated",, never heard it quite put that way b4. We usually just say "it fell apart". Not trying to be funny, so don't jump all over me. All the helicopter experience Mr Robinson has, i cannot understand tho, how he can build helicopters without extensive use of castle nuts and cotter pins (like real helicopters) and he relies on "pal" nuts. Must save what? couple hundred bucks per helicopter and a few hours labor? Likewise on the 206 thomas coupling,, don't understand why they do these things.

Posted (edited)

These are logs and bolts you can check on pre-flight. They should be torque striped per the maintenance manual; however, on some aircraft these torque stripes have worn-off or are otherwise missing. Add it to your list of things to take a better look at.

 

The lower swashplate had four push-pull tube attachment lugs: aft, front left, front right, and front scissor. Push-pull tubes were connected to the aft attachment lug, front right attachment lug, and front scissor attachment lug. However, the front left push-pull tube was not attached to its corresponding lug and the associated attachment bolt assembly was missing, see photo blow.

 

According to the R44 maintenance manual, the assembly consists of a bolt, safety washer, two spacers on either side of the rod end ball bearing, washer, self-locking nut, palnut, and a torque stripe.

 

Remnants of torque striping were observed on the aft attachment lug bolt assembly but not on the forward right or front scissor lug bolt assemblies. The forward left attachment lug was examined for any remnant of a torque stripe but none was found.

 

33_zpsqrweabtl.jpg44_zps6twsz4qj.jpg66_zpsbobbb2xx.jpg

 

Approximately 5 minutes after the pilot departed he told air traffic control that he wanted to return to the airport, but did not specify a reason. The pilot was unable to make it back to the airport and collided with trees, powerlines, and a residence.

77_zpsddo2frre.jpg

Edited by iChris
Posted (edited)

The fatal 2012 Bell 222 mast separation accident (NTSB# CEN10FA291) was caused by a bolt fracture as seen below; however, in the case of this R44, none of the associated attachment bolt assembly was found. Therefore, the cause of the liberation of the attachment bolt with respect the this R44 accident is currently unknown.

 

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Edited by iChris
Posted (edited)

What makes you think it was a design problem?

 

Show me where i said that this accident was caused by a design problem.

 

Watch spike's video.

 

But, since you brought it up, consider the possibilities:

1) the parts were left out upon assembly

2) it fell apart on its own accord

 

3rd ??

Edited by pokey

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