What was found
A 1.75 INCH CRACK IN VERTICAL STAB SKIN LT SIDE FRONT SPAR BELOW ACCESS PANEL 9501. REPAIRED PER SRM 55-30-3 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 1.75 INCH CRACK IN VERTICAL STAB SKIN LT SIDE FRONT SPAR BELOW ACCESS PANEL 9501. REPAIRED PER SRM 55-30-3 FIG 1.