Aviation Accident Summaries

Aviation Accident Summary FTW82DA248

FORT WORTH, TX, USA

Aircraft #1

N55276

CESSNA 172P ROBERTSON STOL

Analysis

THE AIRCRAFT WAS EQUIPPED WITH A ROBERTSON STOL KIT. AFTER OPERATING THE AIRCRAFT IN SLOW FLIGHT ABOUT 1/2 HR, THE PILOT ELECTED TO LAND. THE APPROACH WAS FLOWN AT 45 KTS WITH A 500 FT/MIN SINK RATE. POWER WAS ADDED TO ARREST THE SINK RATE JUST BEFORE TOUCHDOWN, BUT REPORTEDLY, TOO MUCH WAS APPLIED AND THE AIRCRAFT BOUNCED AND BALLOONED IN THE AIR. REPORTEDLY, THE PILOT OVERREACTED AND REDUCED TOO MUCH POWER, THEN THE AIRCRAFT BOUNCED AGAIN. AFTER THE SECOND BOUNCE, FULL POWER WAS APPLIED, BUT THE PLANE DRIFTED TO THE LEFT OF THE RUNWAY AND TOUCHED DOWN IN A SOFT AREA. THE NOSE GEAR SHEARED OFF IN THE SOFT TERRAIN AND THE PLANE FLIPPED OVER. THE PILOT STATED THAT HE WAS UNFAMILIAR WITH THE AIRCRAFT'S RESPONSE TO POWER. HE ASSUMED THAT FROM HIS EXPERIENCE IN OTHER MODELS, HE COULD FLY THE STOL MODEL OF THE CESSNA 172.

 

Source: NTSB Aviation Accident Database

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