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|
Attributes | |
ACN | 93015 |
Time | |
Date | 198808 |
Day | Mon |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | atc facility : geg |
State Reference | WA |
Altitude | msl bound lower : 39000 msl bound upper : 39000 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | artcc : zse |
Operator | common carrier : air carrier |
Make Model Name | Large Transport, Low Wing, 2 Turbojet Eng |
Navigation In Use | Other Other |
Flight Phase | cruise other |
Route In Use | enroute : direct enroute other |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : flight engineer pilot : atp |
Experience | flight time last 90 days : 250 flight time total : 9000 flight time type : 900 |
ASRS Report | 93015 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : atp |
Events | |
Anomaly | aircraft equipment problem : critical |
Independent Detector | other flight crewa |
Resolutory Action | flight crew : declared emergency other |
Consequence | faa : investigated |
Supplementary | |
Primary Problem | Aircraft |
Narrative:
Cruising at FL390 copilot's front window suddenly shattered and began arcing (electrically). Captain noticed window visibly bowing inward. Captain flew aircraft and copilot communicated with center and ATC. Captain decided to land at spokane, doubting integrity of shattered window. Copilot relayed intentions to ATC and company. And, with approval from both, began descent. Both pilots donned O2. Shattered window procedure was executed from manual and passenger seatbelt sign illuminated. Captain informed passenger and cabin crew via passenger announcement as to problem and our intentions to land at spokane. Visual approach and landing executed west/O further incident. Upon visual inspection of window, there appeared to be a central point of origin or impact from which exterior pieces of glass were missing and all cracks emminated. We do not know whether something impacted window, but consider it a remote possibility. Have heard of rare instances of birds at high altitudes or perhaps WX balloon. Callback conversation with reporter revealed the following: reporter stated that manual only has procedure that calls for turning off windshield heat. Manufacturer maintains outer pane cracking or shattering does not affect structural integrity, but in this case was a brown streak in middle of inner pane and inward bowing, which seemed unusual with pressurization, so PIC elected to land at nearest suitable. Did not notice if bowing decreased as speed and altitude and pressurization changed. FAA inspector was on scene at arrival and inspected windshield and was satisfied with flight crew action. Did not see anything strike windshield but heard a pop which could have been a strike or just from the glass starting to shatter.
Original NASA ASRS Text
Title: ACR LGT WITH SHATTERED WINDSHIELD MAKES PRECAUTIONARY LNDG AT NEAREST ARPT.
Narrative: CRUISING AT FL390 COPLT'S FRONT WINDOW SUDDENLY SHATTERED AND BEGAN ARCING (ELECTRICALLY). CAPT NOTICED WINDOW VISIBLY BOWING INWARD. CAPT FLEW ACFT AND COPLT COMMUNICATED WITH CENTER AND ATC. CAPT DECIDED TO LAND AT SPOKANE, DOUBTING INTEGRITY OF SHATTERED WINDOW. COPLT RELAYED INTENTIONS TO ATC AND COMPANY. AND, WITH APPROVAL FROM BOTH, BEGAN DSCNT. BOTH PLTS DONNED O2. SHATTERED WINDOW PROC WAS EXECUTED FROM MANUAL AND PAX SEATBELT SIGN ILLUMINATED. CAPT INFORMED PAX AND CABIN CREW VIA PAX ANNOUNCEMENT AS TO PROB AND OUR INTENTIONS TO LAND AT SPOKANE. VISUAL APCH AND LNDG EXECUTED W/O FURTHER INCIDENT. UPON VISUAL INSPECTION OF WINDOW, THERE APPEARED TO BE A CENTRAL POINT OF ORIGIN OR IMPACT FROM WHICH EXTERIOR PIECES OF GLASS WERE MISSING AND ALL CRACKS EMMINATED. WE DO NOT KNOW WHETHER SOMETHING IMPACTED WINDOW, BUT CONSIDER IT A REMOTE POSSIBILITY. HAVE HEARD OF RARE INSTANCES OF BIRDS AT HIGH ALTS OR PERHAPS WX BALLOON. CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING: RPTR STATED THAT MANUAL ONLY HAS PROC THAT CALLS FOR TURNING OFF WINDSHIELD HEAT. MANUFACTURER MAINTAINS OUTER PANE CRACKING OR SHATTERING DOES NOT AFFECT STRUCTURAL INTEGRITY, BUT IN THIS CASE WAS A BROWN STREAK IN MIDDLE OF INNER PANE AND INWARD BOWING, WHICH SEEMED UNUSUAL WITH PRESSURIZATION, SO PIC ELECTED TO LAND AT NEAREST SUITABLE. DID NOT NOTICE IF BOWING DECREASED AS SPEED AND ALT AND PRESSURIZATION CHANGED. FAA INSPECTOR WAS ON SCENE AT ARR AND INSPECTED WINDSHIELD AND WAS SATISFIED WITH FLT CREW ACTION. DID NOT SEE ANYTHING STRIKE WINDSHIELD BUT HEARD A POP WHICH COULD HAVE BEEN A STRIKE OR JUST FROM THE GLASS STARTING TO SHATTER.
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.