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Printed page label not indexed. PDF page 34.
the unlock limit switch had two DOUGLAS P/N AFA 3210-1 shins, surmounted by a third shim with no reference number and consisting of a thin crumpled piece of metal leaf with numerous folds on the side which had to comeOpen official document at PDF page 34French Commission of Inquiry final report: Turkish Airlines DC-10 TC-JAV, official UK-hosted English translation
Printed page label not indexed. PDF page 39.
observations were made: - The striker P/N 7797-3 located at the end of the lock tube had ten shims, ic: 1 shim P/N ADA 7773-1 & shims PIN ADA 7773-501 1 shim P/N ADA 7773-503 with a total thickness ofOpen official document at PDF page 39French Commission of Inquiry final report: Turkish Airlines DC-10 TC-JAV, official UK-hosted English translation
Printed page label not indexed. PDF page 41.
the view port provided for that purpose. Door of TC-JAV The thickness of the striker shims made any correct adjustment of the lock pins impossible; any attempt to bring the ends of the lock pins to the correct distance ofOpen official document at PDF page 41French Commission of Inquiry final report: Turkish Airlines DC-10 TC-JAV, official UK-hosted English translation
Printed page 46. PDF page 51.
limit warning switch were incorrect. ~ The striker of the unlock limit switch had two shims of Douglas origin, sur- mounted by a shim with no reference and of a quality not to aeronautical standards. During the aircraft's stop atOpen official document at PDF page 51French Commission of Inquiry final report: Turkish Airlines DC-10 TC-JAV, official UK-hosted English translation