Narrative:

Our aircraft was climbing to a cruise altitude of FL330. Both engine anti-ice and airfoil anti-ice were in use. The FMS 'VNAV climb' mode was controling the climb out but approaching FL320, airspeed was decreasing and mach was also rolling back. Both pilots could see that 'climb' thrust was only going to maintain altitude for the moment and that airspeed/mach was continuing to decay. As climb performance continued to deteriorate, and not wanting to increase our angle of attack, the captain disengaged the autoplt and began our descent back down to FL290. As he began the descent out of FL320, the first officer requested the descent with ATC and quickly received it. Aircraft was descended to FL290 where performance was fine. Lesson learned: high gross weight, high altitude, anti-ice on and poor airspeed control (ie, back side of the power curve) can all combine to create a performance barrier which can only be rectified by descending well below the service ceiling and increasing again to cruise mach. The turbulence at FL320 also contributed to our deteriorating climb performance and was a factor in our decision to descend back down to FL290 where it was smooth.

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Original NASA ASRS Text

Title: ATTEMPTED CLB ON THE 'BACKSIDE OF THE PWR CURVE.'

Narrative: OUR ACFT WAS CLBING TO A CRUISE ALT OF FL330. BOTH ENG ANTI-ICE AND AIRFOIL ANTI-ICE WERE IN USE. THE FMS 'VNAV CLB' MODE WAS CTLING THE CLBOUT BUT APCHING FL320, AIRSPD WAS DECREASING AND MACH WAS ALSO ROLLING BACK. BOTH PLTS COULD SEE THAT 'CLB' THRUST WAS ONLY GOING TO MAINTAIN ALT FOR THE MOMENT AND THAT AIRSPD/MACH WAS CONTINUING TO DECAY. AS CLB PERFORMANCE CONTINUED TO DETERIORATE, AND NOT WANTING TO INCREASE OUR ANGLE OF ATTACK, THE CAPT DISENGAGED THE AUTOPLT AND BEGAN OUR DSCNT BACK DOWN TO FL290. AS HE BEGAN THE DSCNT OUT OF FL320, THE FO REQUESTED THE DSCNT WITH ATC AND QUICKLY RECEIVED IT. ACFT WAS DSNDED TO FL290 WHERE PERFORMANCE WAS FINE. LESSON LEARNED: HIGH GROSS WT, HIGH ALT, ANTI-ICE ON AND POOR AIRSPD CTL (IE, BACK SIDE OF THE PWR CURVE) CAN ALL COMBINE TO CREATE A PERFORMANCE BARRIER WHICH CAN ONLY BE RECTIFIED BY DSNDING WELL BELOW THE SVC CEILING AND INCREASING AGAIN TO CRUISE MACH. THE TURB AT FL320 ALSO CONTRIBUTED TO OUR DETERIORATING CLB PERFORMANCE AND WAS A FACTOR IN OUR DECISION TO DSND BACK DOWN TO FL290 WHERE IT WAS SMOOTH.

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.