37000 Feet | Browse and search NASA's Aviation Safety Reporting System |
|
Attributes | |
ACN | 169042 |
Time | |
Date | 199101 |
Day | Sun |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : mtp |
State Reference | NY |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Operator | common carrier : air taxi |
Make Model Name | Small Transport, Low Wing, 2 Turboprop Eng |
Flight Phase | landing other |
Flight Plan | None |
Person 1 | |
Affiliation | company : air taxi |
Function | flight crew : captain oversight : pic |
Qualification | pilot : commercial pilot : instrument pilot : atp pilot : cfi |
Experience | flight time last 90 days : 90 flight time total : 2500 flight time type : 400 |
ASRS Report | 169042 |
Person 2 | |
Affiliation | company : air taxi |
Function | flight crew : first officer |
Qualification | pilot : instrument pilot : commercial |
Events | |
Anomaly | aircraft equipment problem : less severe |
Independent Detector | other flight crewa |
Resolutory Action | none taken : detected after the fact |
Consequence | Other |
Supplementary | |
Primary Problem | Aircraft |
Air Traffic Incident | other |
Narrative:
The flight and approach to landing were normal. The landing of the small transport was also uneventful. Approximately 5 seconds after the landing roll the right wing of the aircraft started to list and get lower. It seemed as though the right tire was flat. After shutting the aircraft down, I noticed that the left strut connecting arm (the scissor arm) was completely cracked. This caused the strut to fully decompress on the left side. After the mechanics investigated it appeared that a stress fracture was already on the strut connecting arm. My recommendation is to preflight carefully and look closely at the strut and strut connecting arm for small cracks and fractures.
Original NASA ASRS Text
Title: STRUCTURAL DAMAGE TO ACFT LEFT STRUT.
Narrative: THE FLT AND APCH TO LNDG WERE NORMAL. THE LNDG OF THE SMT WAS ALSO UNEVENTFUL. APPROX 5 SECS AFTER THE LNDG ROLL THE RIGHT WING OF THE ACFT STARTED TO LIST AND GET LOWER. IT SEEMED AS THOUGH THE RIGHT TIRE WAS FLAT. AFTER SHUTTING THE ACFT DOWN, I NOTICED THAT THE LEFT STRUT CONNECTING ARM (THE SCISSOR ARM) WAS COMPLETELY CRACKED. THIS CAUSED THE STRUT TO FULLY DECOMPRESS ON THE LEFT SIDE. AFTER THE MECHS INVESTIGATED IT APPEARED THAT A STRESS FRACTURE WAS ALREADY ON THE STRUT CONNECTING ARM. MY RECOMMENDATION IS TO PREFLT CAREFULLY AND LOOK CLOSELY AT THE STRUT AND STRUT CONNECTING ARM FOR SMALL CRACKS AND FRACTURES.
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.