What was found
DURING 100 HOUR CHECK OF THE AIRPLANE (G.LANDING GEAR GROUP, POINT 36) WE DISCOVERED THAT BOLT, PN 400-672 (SECTION IX, CONTROL SYSTEM GROUP, FIGURE NR 63, INDEX NUMBER 90) DAMAGED CHANNEL-TUNEL-RIGHT, PN95599-003 (SECTION II, FUSELAGE GROUP, FIGURE NR 12, INDEX NUMBER 85A)