What was found
CRACKS ON LONGERONS STA 1022 AND L6L, L5L AND L4L INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00652: CRACKS ON LONGERONS STA 1022 AND L6L, L5L AND L4L INTERNAL STRUCTURE FUSELAGE WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG 201 AND (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON LONGERON STA 1022 5LH. NO CRACK S WERE FOUND PER DCMD/BOEING NDTSPM PART 6, 06-10-01.001. (LP #0850685)