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crack growth found on the seven crack samples that provided suitable data. Table 2.--Striation counts on selected cracks from the lap joints along S-4R and S-10L Specimen Estimated number Crack length location of cycles (+/-20%) in_ inches S-4R 28,670 0.105Open official document at PDF page 37NTSB AAR-89/03: Aloha Airlines flight 243, N73711
Printed page 54. PDF page 60.
54 Striation counts of five of the largest fatigue cracks that were present in the upper fastener holes of the section outside the repaired area indicated these cracks grew less than 0.020Open official document at PDF page 60NTSB AAR-89/03: Aloha Airlines flight 243, N73711