Here's some pics from a Pre-War Taylorcraft right main landing gear. It failed last winter locally when slow taxiing on skis. Previously no unusual bumps or bangs were noted by the pilot (not me). It appears the MLG diagonal tie strut first separated mid-span followed by outward gear deflection until it reached the limit of the bungee safety cable. Further bending occurred which partially bent and broke the two upper "A" frame tubing. The wing tip never hit and with help the pilot was able to lift the wing and tie the right and left gear together with rope.
Below are pics of Taylorcraft SB 78-001 which recommends inspecting a previously drilled drain hole in the lower MLG strut. If no hole is present then one can be drilled in either of two locations.
However for this gear there was a drilled hole in the location specified in the SB but it went into solid steel and never breached the hollow portion of the strut. Also note the internal corrosion in the strut at the break, as well as at one at the base of one of the "A" tubes. The other is also corroded.
I determined the depth of the hollow strut with a stiff wire then noted that location plus the drilled hole that matched Taylorcraft's specs. Obviously sticking a wire into the hole to inspect for corrosion is useless. I cleaned the hole with brake cleaner and a probe to confirm the blind cavity. Drilling a hole 1/2" further from the gear bolt would have hit the cavity, and so would making one spec'd as the alternative in the SB.
Edit: Note the SB 78-001 was published while the Ferris' were in business. Their gear and maybe others were built to allow a drain from the spec'd hole. Confirming a drain exists by inserting a long wire, applying air pressure, or spraying oil through a small extension might be a good idea.
Gary
Below are pics of Taylorcraft SB 78-001 which recommends inspecting a previously drilled drain hole in the lower MLG strut. If no hole is present then one can be drilled in either of two locations.
However for this gear there was a drilled hole in the location specified in the SB but it went into solid steel and never breached the hollow portion of the strut. Also note the internal corrosion in the strut at the break, as well as at one at the base of one of the "A" tubes. The other is also corroded.
I determined the depth of the hollow strut with a stiff wire then noted that location plus the drilled hole that matched Taylorcraft's specs. Obviously sticking a wire into the hole to inspect for corrosion is useless. I cleaned the hole with brake cleaner and a probe to confirm the blind cavity. Drilling a hole 1/2" further from the gear bolt would have hit the cavity, and so would making one spec'd as the alternative in the SB.
Edit: Note the SB 78-001 was published while the Ferris' were in business. Their gear and maybe others were built to allow a drain from the spec'd hole. Confirming a drain exists by inserting a long wire, applying air pressure, or spraying oil through a small extension might be a good idea.
Gary
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