What was found
CHORD ANGLE REMOVED FOR CORROSION DAMAGE STA 110 TO 129, LBL 14 IN. INSTALLED NEW CHORD ANGLE REF DOUGLAS DWG 5911401. CHECK-C 11-22-97 STL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CHORD ANGLE REMOVED FOR CORROSION DAMAGE STA 110 TO 129, LBL 14 IN. INSTALLED NEW CHORD ANGLE REF DOUGLAS DWG 5911401. CHECK-C 11-22-97 STL.