What was found
METAL PEELING UP ON RIGHT OUTBOARD AFT FLAP. / [01] INSPECTED AREA OF DAMAGE ON RH O/B AFT FLAP INBOARD END. DAMAGE MEASURED 8? BY 12?. C/W EA 22-157-02190. REINSPECT EACH CYCLE; PERMANENT REPAIR REQUIRED WITHIN 5 CYCLES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
METAL PEELING UP ON RIGHT OUTBOARD AFT FLAP. / [01] INSPECTED AREA OF DAMAGE ON RH O/B AFT FLAP INBOARD END. DAMAGE MEASURED 8? BY 12?. C/W EA 22-157-02190. REINSPECT EACH CYCLE; PERMANENT REPAIR REQUIRED WITHIN 5 CYCLES.