What was found
WHEN PERFORM EA G-5730-T0384072 P2 STEP 2, REPORT THE CURRENT AIRCRAFT CONFIGURATION TO FEDEX SERVICE ENGINEERING TO REQUEST AIRPLANE JACKING REQUIREMENTS FROM BOEING TO PERFORM THE PERMANENT DOUBLER/TRIPLER REPAIR AS SHOWN IN FIGURE 1. NOTED: NO.1 ENG BOTH FAN COWL REMOVED, FLAP EXTENDED AND MAIN DECK RCB REMOVAL EQUIPMENT INSTALLED. LH WING UPPER SKIN CRACK IN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-50-02-0G FIGURE 1, 51-40-02-0G, 51-10-01-0G,51-20-06-0G, 51-40-05-0G, 51-20-01-0G, 51-40-08-0G, 51-20-05-0G, 51-80-01-0G REV53.0 AND EA G-5730-T0384072 A P2, THIS IS A MAJOR REPAIR PER GMM 6-2-100.