What was found
DURING Q-CHECK, FOUND EXTERNAL FUSELAGE WITH OIL CAN AT BS 901, BETWEEN STRINGER 21 AND 22 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 898.5 TO BS 902.5 BETWEEN STRINGER 21 AND 22 RT DUE TO OIL CAN IAW SRM 53-30-3, FIG 05. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING Q-CHECK, FOUND EXTERNAL FUSELAGE WITH OIL CAN AT BS 901, BETWEEN STRINGER 21 AND 22 RIGHT. REPAIRED FUSELAGE SKIN SECTION FROM BS 898.5 TO BS 902.5 BETWEEN STRINGER 21 AND 22 RT DUE TO OIL CAN IAW SRM 53-30-3, FIG 05. (M)