37000 Feet | Browse and search NASA's Aviation Safety Reporting System |
|
Attributes | |
ACN | 395777 |
Time | |
Date | 199802 |
Day | Fri |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : dfw |
State Reference | TX |
Altitude | agl bound lower : 400 agl bound upper : 400 |
Environment | |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tower : dfw |
Operator | common carrier : air carrier |
Make Model Name | MD-80 Super 80 |
Operating Under FAR Part | Part 121 |
Navigation In Use | Other |
Flight Phase | climbout : takeoff |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : atp |
ASRS Report | 395777 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : commercial pilot : instrument |
Events | |
Anomaly | aircraft equipment problem : less severe other anomaly other |
Independent Detector | aircraft equipment other aircraft equipment : unspecified other flight crewa |
Resolutory Action | other |
Consequence | Other |
Supplementary | |
Primary Problem | Aircraft |
Air Traffic Incident | other |
Narrative:
Reference a feb publication on safety concerning super 80 stick shaker on takeoff. Although no possible violation exists, this debrief is being submitted for safety/trend analysis. On departure, just after rotation, slat disagree light illuminated followed within 1 second by the stick shaker. First officer reduced pitch attitude while I applied maximum power. Stick shaker continued during climb out. At approximately 400 ft afl slat disagree light went out and shaker stopped. Light came back on a few seconds later with shaker on again. Once slats were retracted, light stayed out and no further problems were noted. As stated earlier, after reading safety reports I am concerned about a possible problem with S80 fleet. Had light illuminated a few seconds earlier, V1, some crew members may have decided to abort at very high speed, with the resulting complications.
Original NASA ASRS Text
Title: AN ACR MD80 FLC GOT A STALL WARNING WHEN THE 'SLAT DISAGREE' LIGHT ILLUMINATED AFTER ROTATION DURING THE TKOF.
Narrative: REF A FEB PUB ON SAFETY CONCERNING SUPER 80 STICK SHAKER ON TKOF. ALTHOUGH NO POSSIBLE VIOLATION EXISTS, THIS DEBRIEF IS BEING SUBMITTED FOR SAFETY/TREND ANALYSIS. ON DEP, JUST AFTER ROTATION, SLAT DISAGREE LIGHT ILLUMINATED FOLLOWED WITHIN 1 SECOND BY THE STICK SHAKER. FO REDUCED PITCH ATTITUDE WHILE I APPLIED MAX PWR. STICK SHAKER CONTINUED DURING CLBOUT. AT APPROX 400 FT AFL SLAT DISAGREE LIGHT WENT OUT AND SHAKER STOPPED. LIGHT CAME BACK ON A FEW SECONDS LATER WITH SHAKER ON AGAIN. ONCE SLATS WERE RETRACTED, LIGHT STAYED OUT AND NO FURTHER PROBS WERE NOTED. AS STATED EARLIER, AFTER READING SAFETY RPTS I AM CONCERNED ABOUT A POSSIBLE PROB WITH S80 FLEET. HAD LIGHT ILLUMINATED A FEW SECONDS EARLIER, V1, SOME CREW MEMBERS MAY HAVE DECIDED TO ABORT AT VERY HIGH SPD, WITH THE RESULTING COMPLICATIONS.
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.