![\"\"](\"https:\/\/rv10.mirimar.org\/wp-content\/uploads\/2023\/01\/IMHF0738.jpg\")
<\/a>![\"\"](\"https:\/\/rv10.mirimar.org\/wp-content\/uploads\/2023\/01\/IMHF0740.jpg\")
<\/a>The rear spar bolt was an AN6-11, anchor nut and cotter pin. The wing root fairing supports are held primarily by LP4-3 pull rivets.<\/p>\n<\/p>\n
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<\/p>\n <\/p>\n <\/p>\n <\/p>\n <\/p>\n <\/p>\n <\/p>\n <\/p>\n <\/p>\n Finish configuration of wing root covers required installation of a few system components. The rear spar bolt was an AN6-11, anchor nut and cotter pin. The wing root fairing supports are held primarily by LP4-3 pull rivets. A custom fuel line, filter and shut-off valve from TSFlightline was installed.\u00a0 This configuration should …<\/span> Continue Reading →<\/span><\/a><\/span><\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[10,71],"tags":[],"class_list":["post-12941","post","type-post","status-publish","format-standard","hentry","category-rv-10-build-project","category-section-44-wing-attachment"],"_links":{"self":[{"href":"https:\/\/rv10.mirimar.org\/index.php?rest_route=\/wp\/v2\/posts\/12941","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/rv10.mirimar.org\/index.php?rest_route=\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/rv10.mirimar.org\/index.php?rest_route=\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/rv10.mirimar.org\/index.php?rest_route=\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/rv10.mirimar.org\/index.php?rest_route=%2Fwp%2Fv2%2Fcomments&post=12941"}],"version-history":[{"count":6,"href":"https:\/\/rv10.mirimar.org\/index.php?rest_route=\/wp\/v2\/posts\/12941\/revisions"}],"predecessor-version":[{"id":12974,"href":"https:\/\/rv10.mirimar.org\/index.php?rest_route=\/wp\/v2\/posts\/12941\/revisions\/12974"}],"wp:attachment":[{"href":"https:\/\/rv10.mirimar.org\/index.php?rest_route=%2Fwp%2Fv2%2Fmedia&parent=12941"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/rv10.mirimar.org\/index.php?rest_route=%2Fwp%2Fv2%2Fcategories&post=12941"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/rv10.mirimar.org\/index.php?rest_route=%2Fwp%2Fv2%2Ftags&post=12941"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}<\/a><\/a>A custom fuel line, filter and shut-off valve from TSFlightline was installed.\u00a0 This configuration should allow the filter to be removed for annual inspection without the need to completely drain the tanks.<\/p>\n<\/a><\/a>The massive and high precision bolts (NAS1309-58 and NAS1306-58) were tightened with the nylon insert (AN365-918 and AN365-624) lock nuts and regular\/thin washers to expose sufficient bolt threads.\u00a0 The torques were 100 lb-ft and 20 lb-ft respectively<\/p>\n<\/a><\/a>The Stewart-Warner IE-F-385C (right) fuel sender was attached with NAS180-2-0808 (8-32) hex head bolts and Permatex Aviation Forma-Gasket sealer compound.<\/p>\n<\/a><\/a>Fuel sumping valves were installed and fuel vent lines were fabricated from 1\/4″ stainless tube.<\/p>\n<\/a>Lastly a Garmin GTP59 air temperature probe was installed near the first inspection port.\u00a0 This last run allowed the wire bundles to be consolidated and attached via CPC-24 connector to the fuselage.<\/p>\n","protected":false},"excerpt":{"rendered":"