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Unread 07-28-13, 09:55 PM
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hharney hharney is offline
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The AD 78-09-05 does not require the wings to be removed. Access is gained to the spar and is inspected using an eddy current device (NDI)

The SID that is referred to in the report from AvWeb is the inspection of the attach points of the wings and struts. Because the process requires the bolts to be removed for inspection the inspection is estimated to be very expensive. In order to remove the bolts that attach the wings, the entire tail and boom assembly must be removed first. This is the only method known that will minimize the potential damage that could occur by performing this inspection. If some kind of jig were to be developed that could support the structure maybe the bolts could be safely removed for inspection. To my knowledge no such device exists.

The AD attached is a walk in the park compared to these SID inspections. Although never taken lightly this AD has been performed on many Skymaster's already and may be best to use an experienced shop for the inspection.
Attached Files
File Type: pdf 78-09-05.pdf (325.4 KB, 1882 views)
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Herb R Harney
1968 337C

Flying the same Skymaster for 47 years
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