What was found
NR 2 ENGINE LOWER NACELLE LONGITUDINAL STIFFENER JUST TO THE RT OF THE ICE DOOR IS CRACKED ON THE AFT END. REPAIRED IAW RD8/4-71-016.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 ENGINE LOWER NACELLE LONGITUDINAL STIFFENER JUST TO THE RT OF THE ICE DOOR IS CRACKED ON THE AFT END. REPAIRED IAW RD8/4-71-016.