What was found
(CAN) CRACKED FUSELAGE FRAME AT LT AFT, FLOAT/AFT WING SPAR ATTACHMENT AREA. CRACK IS IN AREA "C" OF WIPAIRE SL REV D. AREA ALREADY REPLACED WITH THE NEWEST VERSION OF TUBING. SUGGEST DRILLING HOLE AT AREA C TO IMPROVE FLEXIBILITY.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) CRACKED FUSELAGE FRAME AT LT AFT, FLOAT/AFT WING SPAR ATTACHMENT AREA. CRACK IS IN AREA "C" OF WIPAIRE SL REV D. AREA ALREADY REPLACED WITH THE NEWEST VERSION OF TUBING. SUGGEST DRILLING HOLE AT AREA C TO IMPROVE FLEXIBILITY.