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|
Attributes | |
ACN | 866722 |
Time | |
Date | 200912 |
Local Time Of Day | 0601-1200 |
Place | |
Locale Reference | ZZZ.ARTCC |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | B757-200 |
Operating Under FAR Part | Part 121 |
Flight Phase | Cruise |
Flight Plan | IFR |
Component | |
Aircraft Component | Cockpit Window |
Person 1 | |
Function | Pilot Flying Captain |
Experience | Flight Crew Last 90 Days 200 Flight Crew Total 15000 Flight Crew Type 1900 |
Person 2 | |
Function | First Officer Pilot Not Flying |
Experience | Flight Crew Last 90 Days 200 Flight Crew Total 12000 Flight Crew Type 5000 |
Events | |
Anomaly | Aircraft Equipment Problem Critical |
Narrative:
In level cruise; I was up receiving my crew meal when we heard a 'boom' sound. Turning around; I saw that the copilot's windshield had completely shattered. Examining it revealed that the outer pane was affected; but the inner pane was still intact. I initiated a speed reduction and a descent; coordinated with ATC. We ran the checklist for a window failure; which basically resulted in turning off the window heat and determining that the remaining pane was structurally sound. We elected to continue our flight at FL230 and below with a maximum speed of 250 KTS. The procedure did not call for this; but I felt it was an appropriate precaution and had minimal effect on our fuel burn for the remainder of the flight. The landing was uneventful; with the exception of limited visibility through the shattered window pane.
Original NASA ASRS Text
Title: A B757 First Officer's forward windshield outer pane cracked in flight. The aircraft was slowed; descended and proceeded normally to its scheduled destination.
Narrative: In level cruise; I was up receiving my crew meal when we heard a 'boom' sound. Turning around; I saw that the copilot's windshield had completely shattered. Examining it revealed that the outer pane was affected; but the inner pane was still intact. I initiated a speed reduction and a descent; coordinated with ATC. We ran the checklist for a window failure; which basically resulted in turning off the window heat and determining that the remaining pane was structurally sound. We elected to continue our flight at FL230 and below with a maximum speed of 250 KTS. The procedure did not call for this; but I felt it was an appropriate precaution and had minimal effect on our fuel burn for the remainder of the flight. The landing was uneventful; with the exception of limited visibility through the shattered window pane.
Data retrieved from NASA's ASRS site as of April 2012 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.