What was found
AFTER TAKEOFF FLAPS WOULD NOT RETRACT. FLAP NEEDLES SPLIT AT ABOUT 1 POSITION ON THE INDICATOR. REPLACED RT WING TE FLAP SKEW SENSOR T530 IAW AMM 27-59-01- 201. PERFORMED TEST OF FLAP SKEW SENSOR IAW AMM 27-59-00-501. TEST PASSED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER TAKEOFF FLAPS WOULD NOT RETRACT. FLAP NEEDLES SPLIT AT ABOUT 1 POSITION ON THE INDICATOR. REPLACED RT WING TE FLAP SKEW SENSOR T530 IAW AMM 27-59-01- 201. PERFORMED TEST OF FLAP SKEW SENSOR IAW AMM 27-59-00-501. TEST PASSED.