What was found
DURING LANDING AT ABOUT 100 FEET AN UNCOMMANDED ROCKING OF THE WINGS FROM LEFT TO RIGHT HAPPENED ALL THE WAY DOWN TO TOUCHDOWN.<[01] INTERROGATED FSEU; FOUND F/C 27-51351; T/E FLAP UCM.<BR>PERFORMED FIM TASK FLAP LOAD RELIEF TEST 27-51-830. NO FAULTS;[02] SUSPECT POSSIBLE RUDDER PCU ISSUE; OPENED PANEL 324DR AND INSPECTED MAIN AND STANDBY RUDDER PCU ATTACH POINTS; NO DEFECTS NOTED. RE-INSTALLED PANEL 324DR.;[03] PER MOC; CHECK TENSION ON AILERON CABLES AND ADJUST IF NECESSARY. CHECK AND ADJUSTED AILERON CABLES ACBA-L;ACBA-R;ACBB-L AND ACBB-R PER AMM 27-11-00 AND AMM 27-09-14. STOP AT SUBTASK 27-11-00-820-004; STEP 7 REF. AMM 27-11-00-820-801. RIG PINS A/S-15 A/S-1 AND A/S-1A REMAINED INSTALLED REF. AMM 27-11-00-820-801 FOR DETAILS ON WHERE THEY ARE LOCATED. FOWARD AND AFT E-E BAY ACCESS DOOR REMAINED OPENED DUE TO RIG PINS BEING INSTALLED;[13] C/W AILERON BODY CABLE AA AND AB ADJUSTMENT IAW AMM 27-11-00-820-801. PERFORMED FLIGHT SPOILER SYSTEM TEST PER AMM 27-61-00-730-801 FOUND SPOILERS 2;3;10;AND 11 OUT OF ADJUSTMENT. ADJUSTED SPOILERS 2;3;10 AND 11 PER AMM 27-61-00-820-804. ALL TEST PASSED.;[14] VERIFIED; C/W AILERON BODY CABLE AA AND AB ADJUSTMENT IAW AMM 27-11-00-820-801. PERFORMED FLIGHT SPOILER SYSTEM TEST PER AMM 27-61-00-730-801 FOUND SPOILERS 2;3;10;AND 11 OUT OF ADJUSTMENT. ADJUSTED SPOILERS 2;3;10 AND 11 PER AMM 27-61-00-820-804. ALL TEST PASSED