As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER FLAP 5 TAKEOFF FLAPS WERE RETRACTED TO FLAP 1 POSITION, BUT STOPPED AT FLAP 2 DUE TO FLAP ASYM. REPLACED NR 4 INBD SKEW MECHANISM WITH PART MFG 256A3940-3, NO SN IAW MM 27-59-02. REPLACED SKEW CONTROL ROD IAW IPC 27-59-01-03 ITEM 65. SKEW FUNCTIONAL CHECKED NORMAL IAW MM 27-59-00.