FAIRBANKS, AK, USA
N5056Q
de Havilland DHC-3
THE PLT RPRTD THAT BEFORE THE FLT, THE WINGS & STABILIZER WERE SWEPT, LEAVING A LAYER OF 'POLISHED' FROST. FREIGHT WAS LOADED & THE ACFT WAS SERVICED TO BRING THE FUEL LEVEL UP TO 120 GAL. AFTER START, TAXI & RUN-UP, THE PLT BEGAN HIS TAKEOFF FROM THE APPROACH END OF THE 10,300 FT RWY (WITH 35' MP & 2250 RPM). AT ABOUT 100 FT AGL, HE ADJUSTED THE POWER (TO 30' MP & 2000 RPM) & RAISED THE FLAPS TO CLIMB AT 82 KTS. HOWEVER, THE ACFT DID NOT CLIMB & WOULD NOT ACCELERATE IN LEVEL FLT. THE PLT INCREASED THE POWER (TO 31' MP & 2100 RPM), BUT HE BELIEVED THERE WAS A DEFINITE LOSS OF POWER. SUBSEQUENTLY, THE ACFT WAS DAMAGED WHEN THE PLT ABORTED THE TAKEOFF ON SNOW COVERED TERRAIN BEYOND THE END OF THE RWY. NO PRE-ACDNT PART FAILURE OR MALFUNCTION OF THE ACFT OR ENG WAS FOUND. AN INV REVEALED THE ENTIRE ACFT WAS COVERED WITH A COATING OF FROST. COMPANY RECORDS SHOWED THE EMPTY WEIGHT OF THE ACFT WAS 5088 LBS; THE ACFT'S ACTUAL EMPTY WEIGHT WAS 5285 LBS. AN FAA INSPECTOR CALCULATED THAT THE TAKEOFF GROSS WEIGHT EXCEEDED THE MAX LIMIT BY 130 LBS.
FAILURE OF THE PILOT TO REMOVE FROST FROM THE AIRCRAFT. CONTRIBUTING FACTORS WERE: IMPROPER WEIGHT AND BALANCE AND SNOW COVERED TERRAIN.
Source: NTSB Aviation Accident Database
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