What was found
FOUND CRACK IN WEB OF INTEGRAL MANHOLE PLATE C 38.2, P 54-55 LT. REPAIR PERFORMED BY CUT BACK CRACKED STIFFENER AND INSTALLING A MILLED STIFFENER IAW RAS /EFW/9000197/2009 ISS A, APPROVED BY EA 6-5310-129179.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CRACK IN WEB OF INTEGRAL MANHOLE PLATE C 38.2, P 54-55 LT. REPAIR PERFORMED BY CUT BACK CRACKED STIFFENER AND INSTALLING A MILLED STIFFENER IAW RAS /EFW/9000197/2009 ISS A, APPROVED BY EA 6-5310-129179.