Narrative:

On climb out at approximately 2000 ft MSL; flaps 5 being retracted to flaps 1; aircraft accelerating; the aircraft went into an uncommanded nose down attitude with climb power selected. Nose up trim selected but slow to respond with a heavy control yoke to bring aircraft to level and climb attitude. As the aircraft began gradual descent; airspeed increased rapidly before PF could disengage autothrottles; flaps 1 overspd occurred by approximately 8 KTS (258 KTS indicated). Once airspeed decreased and flaps retracted; no other flight control problems were evident and no other abnormal indications were present. Flight continued to ZZZ with normal descent approach and landing. Callback conversation with reporter revealed the following information: the reporter stated the uncommanded nose down attitude change was caused by the autoplt stabilizer trim. The flight recorder was removed and established that a 700 ft per min descent was initiated. The reporter stated the autoplt and autothrottle systems were switched off; but a flap overspd occurred by 8 KTS. Once airspeed was decreased and flaps retracted; all flight controls were normal. Maintenance action was replacement of stabilizer trim switch and the low speed jackscrew actuator.

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Original NASA ASRS Text

Title: A B737-400 IN CLB AT 2000 FT; FLAPS RETRACTING FROM 5 TO 1 UNITS; EXPERIENCED UNCOMMANDED NOSE DOWN ATTITUDE WITH CLB POWER. A FLAP OVERSPD OF 8 KTS WAS EXPERIENCED.

Narrative: ON CLBOUT AT APPROX 2000 FT MSL; FLAPS 5 BEING RETRACTED TO FLAPS 1; ACFT ACCELERATING; THE ACFT WENT INTO AN UNCOMMANDED NOSE DOWN ATTITUDE WITH CLB POWER SELECTED. NOSE UP TRIM SELECTED BUT SLOW TO RESPOND WITH A HVY CTL YOKE TO BRING ACFT TO LEVEL AND CLB ATTITUDE. AS THE ACFT BEGAN GRADUAL DSCNT; AIRSPD INCREASED RAPIDLY BEFORE PF COULD DISENGAGE AUTOTHROTTLES; FLAPS 1 OVERSPD OCCURRED BY APPROX 8 KTS (258 KTS INDICATED). ONCE AIRSPD DECREASED AND FLAPS RETRACTED; NO OTHER FLT CTL PROBS WERE EVIDENT AND NO OTHER ABNORMAL INDICATIONS WERE PRESENT. FLT CONTINUED TO ZZZ WITH NORMAL DSCNT APCH AND LNDG. CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING INFO: THE RPTR STATED THE UNCOMMANDED NOSE DOWN ATTITUDE CHANGE WAS CAUSED BY THE AUTOPLT STABILIZER TRIM. THE FLT RECORDER WAS REMOVED AND ESTABLISHED THAT A 700 FT PER MIN DSCNT WAS INITIATED. THE RPTR STATED THE AUTOPLT AND AUTOTHROTTLE SYSTEMS WERE SWITCHED OFF; BUT A FLAP OVERSPD OCCURRED BY 8 KTS. ONCE AIRSPD WAS DECREASED AND FLAPS RETRACTED; ALL FLT CTLS WERE NORMAL. MAINT ACTION WAS REPLACEMENT OF STABILIZER TRIM SWITCH AND THE LOW SPD JACKSCREW ACTUATOR.

Data retrieved from NASA's ASRS site as of January 2009 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.