THE AIRPLANE HAD BEEN DEICED 2 TIMES BEFORE LEAVING THE GATE. HOWEVER, 35 MINUTES HAD ELAPSED BETWEEN THE 2ND DEICING & TAKEOFF DURING WHICH TIME ICE ACCUMULATED ON THE WING. THIS TIME PERIOD EXCEEDED THE TYPE I DEICING FLUID SAFE HOLDOVER TIME (11 MIN). THE 1ST OFFICER CALLED VR 11 KTS EARLY, AND THE CAPT ROTATED ABOUT 5 KTS EARLY. AFTER LIFTOFF THE AIRPLANE STALLED AND CAME TO REST PARTIALLY INVERTED AND SUBMERGED IN THE BAY. AT THE TIME OF THE ACCIDENT, THE OPERATOR DID NOT REQUIRE A SPECIFIC EXTERIOR INSPECTION FOR ICE CONTAMINATION OF F-28 AIRPLANES DURING PERIODS OF FREEZING PRECIPITATION. ACCIDENT HISTORY SHOWS THAT NONSLATTED, TURBOJET, TRANSPORT-CATEGORY AIRPLANES HAVE BEEN INVOLVED IN A DISPROPORTIONATE NUMBER OF TAKEOFF ACCIDENTS WHERE UNDETECTED UPPER WING ICE CONTAMINATION HAS BEEN CITED AS THE PROBABLE CAUSE OR SOLE CONTRIBUTING FACTOR.
The National Transportation Safety Board determines the probable cause(s) of this accident as follows:
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