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|
Attributes | |
ACN | 322372 |
Time | |
Date | 199512 |
Day | Mon |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : dca |
State Reference | DC |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | MD-80 Series (DC-9-80) Undifferentiated or Other Model |
Operating Under FAR Part | Part 121 |
Flight Phase | landing other |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : atp pilot : instrument pilot : flight engineer pilot : commercial pilot : cfi |
Experience | flight time last 90 days : 300 flight time total : 10000 flight time type : 1000 |
ASRS Report | 322372 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : atp |
Events | |
Anomaly | aircraft equipment problem : less severe non adherence : far other anomaly other |
Independent Detector | other flight crewa |
Resolutory Action | flight crew : overcame equipment problem flight crew : regained aircraft control |
Consequence | Other |
Supplementary | |
Primary Problem | Flight Crew Human Performance |
Air Traffic Incident | other |
Narrative:
Upon landing, our right thrust reverser did not deploy which caused some adverse yaw during deceleration. Not only did the thrust reverser fail to deploy, but as the captain continued to activate the reverser, we seemed to have increased forward thrust. The left thrust reverser functioned normally. Come to find out that maintenance was supposed to secure the right thrust reverser lever in association with the inoperative annunciator light that was placarded inoperative. In the future, I will thoroughly research and read all MEL items that are placarded, whether or not the captain inquires about this, even if it's only a light which is placarded.
Original NASA ASRS Text
Title: AN MD80'S R THRUST REVERSER WAS INOP, BUT ONLY THE ANNUNCIATOR LIGHT WAS PLACARDED BY MAINT. DURING ATTEMPTED USE OF THE INOP THRUST REVERSER, THE FLC EXPERIENCED INCREASING FORWARD THRUST AND YAW.
Narrative: UPON LNDG, OUR R THRUST REVERSER DID NOT DEPLOY WHICH CAUSED SOME ADVERSE YAW DURING DECELERATION. NOT ONLY DID THE THRUST REVERSER FAIL TO DEPLOY, BUT AS THE CAPT CONTINUED TO ACTIVATE THE REVERSER, WE SEEMED TO HAVE INCREASED FORWARD THRUST. THE L THRUST REVERSER FUNCTIONED NORMALLY. COME TO FIND OUT THAT MAINT WAS SUPPOSED TO SECURE THE R THRUST REVERSER LEVER IN ASSOCIATION WITH THE INOP ANNUNCIATOR LIGHT THAT WAS PLACARDED INOP. IN THE FUTURE, I WILL THOROUGHLY RESEARCH AND READ ALL MEL ITEMS THAT ARE PLACARDED, WHETHER OR NOT THE CAPT INQUIRES ABOUT THIS, EVEN IF IT'S ONLY A LIGHT WHICH IS PLACARDED.
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.