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|
Attributes | |
ACN | 112402 |
Time | |
Date | 198905 |
Day | Sun |
Local Time Of Day | 1801 To 2400 |
Place | |
Locale Reference | airport : den |
State Reference | CO |
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 | Medium Large Transport, Low Wing, 2 Turbojet Eng |
Navigation In Use | Other |
Flight Phase | landing other |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : commercial pilot : flight engineer pilot : atp |
Experience | flight time last 90 days : 240 flight time total : 15500 flight time type : 1325 |
ASRS Report | 112402 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : flight engineer pilot : atp |
ASRS Report | 112418 |
Events | |
Anomaly | aircraft equipment problem : critical other anomaly other |
Independent Detector | other flight crewa |
Resolutory Action | flight crew : declared emergency none taken : insufficient time |
Consequence | other |
Supplementary | |
Primary Problem | Aircraft |
Narrative:
About 2-3 seconds after normal landing in denver on 26R at about XA00 pm, we felt tremendous vibration and the aircraft began to veer to the right. Utilized rudder, and later nosewheel steering, to maintain directional control. Braking action was severely reduced, but brought aircraft to a stop near end of runway. Right main gear then collapsed and I initiated the emergency evacuate/evacuation (right side exits and tail cone). The fire crew (through open forward right emergency exit, informed us that there was fuel leakage, so we completed only immediately action items on checklist and left to assist in evacuate/evacuation. It went smoothly. At this point we have no knowledge of cause. Supplemental information from acn 112418: suspect mechanical failure of 'scissor' mechanism which allowed wheels to rotate on or shortly after touchdown. Skidding the dual mains sideways at 100 KTS in my opinion caused the severe shatter and loss of right braking.
Original NASA ASRS Text
Title: ACFT VEERED RIGHT ON ROLLOUT, THEN RIGHT GEAR COLLAPSED. ACFT EVACUATED.
Narrative: ABOUT 2-3 SECONDS AFTER NORMAL LNDG IN DENVER ON 26R AT ABOUT XA00 PM, WE FELT TREMENDOUS VIBRATION AND THE ACFT BEGAN TO VEER TO THE RIGHT. UTILIZED RUDDER, AND LATER NOSEWHEEL STEERING, TO MAINTAIN DIRECTIONAL CONTROL. BRAKING ACTION WAS SEVERELY REDUCED, BUT BROUGHT ACFT TO A STOP NEAR END OF RWY. RIGHT MAIN GEAR THEN COLLAPSED AND I INITIATED THE EMER EVAC (RIGHT SIDE EXITS AND TAIL CONE). THE FIRE CREW (THROUGH OPEN FORWARD RIGHT EMER EXIT, INFORMED US THAT THERE WAS FUEL LEAKAGE, SO WE COMPLETED ONLY IMMEDIATELY ACTION ITEMS ON CHECKLIST AND LEFT TO ASSIST IN EVAC. IT WENT SMOOTHLY. AT THIS POINT WE HAVE NO KNOWLEDGE OF CAUSE. SUPPLEMENTAL INFORMATION FROM ACN 112418: SUSPECT MECHANICAL FAILURE OF 'SCISSOR' MECHANISM WHICH ALLOWED WHEELS TO ROTATE ON OR SHORTLY AFTER TOUCHDOWN. SKIDDING THE DUAL MAINS SIDEWAYS AT 100 KTS IN MY OPINION CAUSED THE SEVERE SHATTER AND LOSS OF RIGHT BRAKING.
Data retrieved from NASA's ASRS site as of August 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.