What was found
CRACKED EXAHUST ON EXTERNAL FUSELAGE SKIN BETWEEN LONGERON 20 LT AND 21 LT STA Y=256 TO Y=275. CRACKS ON EXHAUST WAS REPAIRED WITH METHOD 1 POSTERILY WITH METHOD 2 OF ER/A 464964-14MA, REV C, ETI 88-14-237, REV ORIGINAL. FPI WAS ACCOMPLISHED ON WELDED AREAS, NO CRACKS WERE FOUND IAW ETI 88-14--273 AND NDT SPM 08-00-06, PAR 8.