What was found
(LOG 0631106) CRACK WAS FOUND OF 0.13IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8R & S-9R. RH FUSELAGE FRAME ON STA 867 WAS REPAIRED PER AMDS 2526-01236-02B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(LOG 0631106) CRACK WAS FOUND OF 0.13IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8R & S-9R. RH FUSELAGE FRAME ON STA 867 WAS REPAIRED PER AMDS 2526-01236-02B.