What was found
INSPECTION FOUND A 2" CRACK IN R/H FUSELAGE SKIN AT STA 727E, S24R. REPAIRED IAW SRM 53-00-01, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2" CRACK IN R/H FUSELAGE SKIN AT STA 727E, S24R. REPAIRED IAW SRM 53-00-01, FIGURE 201.