What was found
(CAN) ON FINAL APPROACH, FLAPS WOULD NOT GO FROM 20 TO 25 IAW STANDARD OPERATING PROCEDURE, INCREASED SPEED & LANDED WITHOUT INCIDENT. NIL PAX REACTION, NIL EMER DECLARED WITH ATC. FLAP TE LOAD ALLEVIATION ACTUATOR REPLACED IAW AMM 27-51-30-401. TEST OF THE FLAP ALLEVIATION SYS CARRIED OUT IAM AMM 27-51-00-501, SUBTASK 27-51-00-865-165, CHECKED SERVICEABLE.