ROMULUS, MI, USA
N160FB
CASA C-212-CC
THE CAPT MADE A STEEP, SHORT, FAST VISUAL APPROACH TO THE RUNWAY BEHIND A DEPARTING DC-9. THE EVIDENCE INDICATES THE CAPT PLACED THE POWER LEVERS INTO BETA MODE TO SLOW THE AIRCRAFT RAPIDLY AND MAKE A SHORT FIELD LANDING. AN ASYMMETRIC THRUST CONDITION RESULTED. THE AIRCRAFT WAS VERY CLOSE TO THE GROUND AND THE CAPT COULD NOT RECOVER PRIOR TO IMPACT. IMPACT FORCES WERE SURVIVABLE. HOWEVER, THE FATALITIES WERE ATTRIBUTED TO A POSTCRASH FIRE, LACK OF FIRE-BLOCKING MATERIAL, AND POORLY DESIGNED AIRCRAFT COMPONENTS. THE INVESTIGATION REVEALED INCORRECT SPRINGS INSTALLED IN THE PROPELLERS AND HIGHER THAT NORMAL FUEL FLOW SETTINGS. THE EXAMINATION OF THE CERTIFICATION PROCESS INDICATED INEFFECTIVEMANAGEMENT OF BILATERAL TYPE CERTIFICATION BY THE FAA. (FOR FURTHER INFORMATION, SEE NTSB/AAR-88/08.)
Source: NTSB Aviation Accident Database
Aviation Accidents App
In-Depth Access to Aviation Accident Reports
