hotrod180 wrote:No STC or field approval required, provided your installation meets certain parameters.
First, check for nutplates in the spar carrythrough.
Then read this, including the policy statement and advisory circulars referred to at the bottom of the page.
https://www.faa.gov/aircraft/gen_av/harness_kits/

hotrod180 wrote:http://www.hookerharness.com/aviation.html
I understand Hooker offers inertia reels but didn't see much about it on their website.
I think that website hasn't been updated in a long time,
might be worth a call to get current info.
Bagarre wrote:hotrod180 wrote:http://www.hookerharness.com/aviation.html
I understand Hooker offers inertia reels but didn't see much about it on their website.
I think that website hasn't been updated in a long time,
might be worth a call to get current info.
It was a few years ago that I checked but the STC that covers the 170 was not for inertia reels.
Compared to the BAS STC, the Hooker modification is VERY invasive. It requires a rather large (5/8ths?) hole drilled and reamed thru the spar fore / aft, a spacer in said hole and an L shaped doubler riveted onto the spar with a dozen or so cherrymax rivets.
Pretty excessive compared to the BAS installation.
It also precludes installing the BAS STC at a later date. The doubler interferes with the BAS bracket and the only way to remove the doubler is to remove the Hooker modification which is to replace the carry thru spar.
Airfoil92 wrote:Bagarre wrote:hotrod180 wrote:http://www.hookerharness.com/aviation.html
I understand Hooker offers inertia reels but didn't see much about it on their website.
I think that website hasn't been updated in a long time,
might be worth a call to get current info.
It was a few years ago that I checked but the STC that covers the 170 was not for inertia reels.
Compared to the BAS STC, the Hooker modification is VERY invasive. It requires a rather large (5/8ths?) hole drilled and reamed thru the spar fore / aft, a spacer in said hole and an L shaped doubler riveted onto the spar with a dozen or so cherrymax rivets.
Pretty excessive compared to the BAS installation.
It also precludes installing the BAS STC at a later date. The doubler interferes with the BAS bracket and the only way to remove the doubler is to remove the Hooker modification which is to replace the carry thru spar.
Yeah that’s a lot of material being drilled out. I guess not having to drill through the skin is their selling point.
bat443 wrote:Just to clarify, if I remember correctly, if the nut plates are installed no additional holes are drilled in the aircraft. For the installation of each BAS bracket two rivets are drilled out and replaced by structural screws in the forward flange of the aft carry through spar. If you do not have the experience or training to do this these rivets should be drilled out by a mechanic as the strength is effected by the fit of the hole. If the nut plates are not installed, according to the BAS notes a 13/32 inch hole is drilled or as an alternate means a 1/2 inch hole in the outer skin. My choice would be the 13/32 inch hole as the outer surface of the carry through spar is not opened. I have installed a couple of BAS shoulder harness kits in 170B's but have no direct experience installing the nut plates. I have had both fixed and inertial locking shoulder harnesses and recommend some type of inertial locking shoulder harness.
Tim
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