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Printed page label not indexed. PDF page 13.
pte ete SS ees SL par Sing Ane PR avaH NING »'wds,, ¥3LN]a9 uvdS NO1Ad 1v-\ / ¥aMO1 sealants ee ek ee ie eon ee _ tt tt _ 7 pea it ; SS asie , He IWOIWSHdS © SiaOpen official document at PDF page 13NTSB AAR-79/17: American Airlines DC-10-10 N110AA, Chicago
Printed page label not indexed. PDF page 67.
the pylon upper spar web to the mating structure attachment was inspected and the new sealant was installed after the assembly was lowered from the wing. However, the Safety Board could not determine the extent to which the aft bulkheadOpen official document at PDF page 67NTSB AAR-79/17: American Airlines DC-10-10 N110AA, Chicago
Printed page 70. PDF page 74.
forward flange ~~ and the attaching spar. web and fasteners. 'Require removal of any “sealant which may hide a crack in the: flange area and employ - “eddy-current or other approved techniques to ensure detection of | : such damage.Open official document at PDF page 74NTSB AAR-79/17: American Airlines DC-10-10 N110AA, Chicago