What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(.4)The airplane was landing on runway 26, a 3,000 foot-long, 50 foot-wide, asphalt runway. A witness observed the airplane touchdown on the runway, still crabbed approximately 30 degrees into the wind. The airplane bounced about 10 feet into the air and began to drift to the south side of the runway. The witness heard full power being applied to the engine, and stated the engine seemed to respond normally. The airplane was observed to climb slightly, roll to the left and descend into trees inverted. The airplane came to rest inverted in a wooded area, about 1,000 feet beyond the approach end of the runway, and 625 feet to left of the runway centerline. Portions of the wreckage, which included the main cabin were consumed by a post crash fire. Examination of the wreckage did not reveal any pre-impact failures of the airframe or engine. Winds reported at airports about 20 miles, east south-east, and 31 miles, south south-west of the accident site, were from 290 degrees at 16 knots with 21 knots gusts, and from 300 degrees at 22 knots with 30 knot gusts, respectively. (-23) pilot attempted to land aircraft at Lehighton, PA, airport (22N) in a strong crosswind. After bounced landing, pilot attempted a go-around but lost control of aircraft. Aircraft landed inverted and pilot was removed from aircraft just prior to beginning of fire. Aircraft received substantial damage and pilot was seriously injured.
As the FAA filed it
(.4)THE AIRPLANE WAS LANDING ON RUNWAY 26, A 3,000 FOOT-LONG, 50 FOOT-WIDE, ASPHALT RUNWAY. A WITNESS OBSERVED THE AIRPLANE TOUCHDOWN ON THE RUNWAY, STILL CRABBED APPROXIMATELY 30 DEGREES INTO THE WIND. THE AIRPLANE BOUNCED ABOUT 10 FEET INTO THE AIR AND BEGAN TO DRIFT TO THE SOUTH SIDE OF THE RUNWAY. THE WITNESS HEARD FULL POWER BEING APPLIED TO THE ENGINE, AND STATED THE ENGINE SEEMED TO RESPOND NORMALLY. THE AIRPLANE WAS OBSERVED TO CLIMB SLIGHTLY, ROLL TO THE LEFT AND DESCEND INTO TREES INVERTED. THE AIRPLANE CAME TO REST INVERTED IN A WOODED AREA, ABOUT 1,000 FEET BEYOND THE APPROACH END OF THE RUNWAY, AND 625 FEET TO LEFT OF THE RUNWAY CENTERLINE. PORTIONS OF THE WRECKAGE, WHICH INCLUDED THE MAIN CABIN WERE CONSUMED BY A POST CRASH FIRE. EXAMINATION OF THE WRECKAGE DID NOT REVEAL ANY PRE-IMPACT FAILURES OF THE AIRFRAME OR ENGINE. WINDS REPORTED AT AIRPORTS ABOUT 20 MILES, EAST SOUTH-EAST, AND 31 MILES, SOUTH SOUTH-WEST OF THE ACCIDENT SITE, WERE FROM 290 DEGREES AT 16 KNOTS WITH 21 KNOTS GUSTS, AND FROM 300 DEGREES AT 22 KNOTS WITH 30 KNOT GUSTS, RESPECTIVELY. (-23) PILOT ATTEMPTED TO LAND AIRCRAFT AT LEHIGHTON, PA, AIRPORT (22N) IN A STRONG CROSSWIND. AFTER BOUNCED LANDING, PILOT ATTEMPTED A GO-AROUND BUT LOST CONTROL OF AIRCRAFT. AIRCRAFT LANDED INVERTED AND PILOT WAS REMOVED FROM AIRCRAFT JUST PRIOR TO BEGINNING OF FIRE. AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE AND PILOT WAS SERIOUSLY INJURED.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N55820 · 1
Matched to the same aircraft by N-number and date.