Narrative:

Aircraft departed lan on runway 28L. On flap retraction from 5 degrees to 2 degrees, the amber leading edge disagreement light on the first officer's panel remained illuminated. Airspeed was limited to 180 KTS during abnormal procedure. Airfoil anti-ice was selected on as a leading edge position indication microswitch was suspect. Referenced B727 communication for abnormal procedure, none found. Leading edge panel was referenced to determine actual position of leading edge devices. With flap handle in the 2 degree position, both inboard and outboard flap needles were at 2 degrees, leading edges extended were 2, 3, 6, 7, and the amber leading edge light was illuminated. Dispatch and maintenance control were consulted for additional mechanical and operational considerations, and to determine an appropriate resolution to the indication. Flaps up were selected and verified all flaps and leading edge devices were determined to be retracted. Leading edge disagreement amber light extinguished after approximately 10 mins of airfoil anti-ice application. Flight operated to dtw with all flight control and indications normal in descent and landing.

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Original NASA ASRS Text

Title: A B727-200 ON INITIAL CLB AT 2200 FT HAD THE AMBER LEADING EDGE DISAGREEMENT LIGHT ON. TURNED ON AIRFOIL ANTI-ICE AND RETRACTED FLAPS. AFTER 10 MINS OF AIRFOIL ANTI-ICE OP, LIGHT WENT OUT AND ALL INDICATIONS NORMAL.

Narrative: ACFT DEPARTED LAN ON RWY 28L. ON FLAP RETRACTION FROM 5 DEGS TO 2 DEGS, THE AMBER LEADING EDGE DISAGREEMENT LIGHT ON THE FO'S PANEL REMAINED ILLUMINATED. AIRSPD WAS LIMITED TO 180 KTS DURING ABNORMAL PROC. AIRFOIL ANTI-ICE WAS SELECTED ON AS A LEADING EDGE POS INDICATION MICROSWITCH WAS SUSPECT. REFED B727 COM FOR ABNORMAL PROC, NONE FOUND. LEADING EDGE PANEL WAS REFED TO DETERMINE ACTUAL POS OF LEADING EDGE DEVICES. WITH FLAP HANDLE IN THE 2 DEG POS, BOTH INBOARD AND OUTBOARD FLAP NEEDLES WERE AT 2 DEGS, LEADING EDGES EXTENDED WERE 2, 3, 6, 7, AND THE AMBER LEADING EDGE LIGHT WAS ILLUMINATED. DISPATCH AND MAINT CTL WERE CONSULTED FOR ADDITIONAL MECHANICAL AND OPERATIONAL CONSIDERATIONS, AND TO DETERMINE AN APPROPRIATE RESOLUTION TO THE INDICATION. FLAPS UP WERE SELECTED AND VERIFIED ALL FLAPS AND LEADING EDGE DEVICES WERE DETERMINED TO BE RETRACTED. LEADING EDGE DISAGREEMENT AMBER LIGHT EXTINGUISHED AFTER APPROX 10 MINS OF AIRFOIL ANTI-ICE APPLICATION. FLT OPERATED TO DTW WITH ALL FLT CTL AND INDICATIONS NORMAL IN DSCNT AND LNDG.

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.