What was found
DURING Q CHECK FOUND THE FUSELAGE FRAME WEB AT BS 260L, LBL 19 WL 276 WITH CRACK L=1.00 W=0.002. REPAIRED THE FUSELAGE FRAME WEB AT BS260L, LBL 19"WL276 WITH CRACK L=1.00" W+0.002" IAW 51-40-2 FIG 1
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING Q CHECK FOUND THE FUSELAGE FRAME WEB AT BS 260L, LBL 19 WL 276 WITH CRACK L=1.00 W=0.002. REPAIRED THE FUSELAGE FRAME WEB AT BS260L, LBL 19"WL276 WITH CRACK L=1.00" W+0.002" IAW 51-40-2 FIG 1