Narrative:

While slowing for approach to ewr, when flaps were extended from 5 degrees to 10 degrees at speed 180 KTS, autoplt and yoke rolled 2 1/2 degrees left. Autoplt and autothrottle were disengaged and captain took control of aircraft. Leading edge device position was verified (all extended and locked). Flap symmetry verified, fuel balance verified, power lever placement checked. Everything appeared normal. Aircraft was VFR under a broken layer about 20 NM from ewr on ILS runway 4R approach, configured for landing. When flaps were extended to 15 degrees, additional 2 degrees of roll occurred. Decision was made to rebug for flaps 15 degree landing -- and it was normal.

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Original NASA ASRS Text

Title: B737-300 CREW HAD UNCOMMANDED ROLL DURING FLAP EXTENSION AT EWR.

Narrative: WHILE SLOWING FOR APCH TO EWR, WHEN FLAPS WERE EXTENDED FROM 5 DEGS TO 10 DEGS AT SPD 180 KTS, AUTOPLT AND YOKE ROLLED 2 1/2 DEGS L. AUTOPLT AND AUTOTHROTTLE WERE DISENGAGED AND CAPT TOOK CTL OF ACFT. LEADING EDGE DEVICE POS WAS VERIFIED (ALL EXTENDED AND LOCKED). FLAP SYMMETRY VERIFIED, FUEL BAL VERIFIED, PWR LEVER PLACEMENT CHKED. EVERYTHING APPEARED NORMAL. ACFT WAS VFR UNDER A BROKEN LAYER ABOUT 20 NM FROM EWR ON ILS RWY 4R APCH, CONFIGURED FOR LNDG. WHEN FLAPS WERE EXTENDED TO 15 DEGS, ADDITIONAL 2 DEGS OF ROLL OCCURRED. DECISION WAS MADE TO REBUG FOR FLAPS 15 DEG LNDG -- AND IT WAS NORMAL.

Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.