What was found
PIT - DURING Q-1 CHECK, FOUND .25 INCH CRACK AT STA 669 LT (APPROX 12 INCHES UPWARD OF LOWER KEEL T-ANGLE) AT FITTING. INSTALLED DOUBLERS AND REPAIR ANGLES PER SRM 53-03 FIG 11. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-1 CHECK, FOUND .25 INCH CRACK AT STA 669 LT (APPROX 12 INCHES UPWARD OF LOWER KEEL T-ANGLE) AT FITTING. INSTALLED DOUBLERS AND REPAIR ANGLES PER SRM 53-03 FIG 11. (X)