19980423010379A

Accident · Destroyed

FAA accident report · Beech 58 · Columbus, OH · April 23, 1998

Date
April 23, 1998 · 23:25 local
Place
Columbus, OH
Airport
Port Columbus International
Phase of flight
Final Approach
Operating rules
Air taxi and commuter (Part 135)
Operator
BSYA
Damage
Destroyed
Aircraft
N258B
NTSB investigation
NTSBIAD98FA047
Reported as
Beech 58
Reported engine
Continental IO520CB
People aboard
1
Fatal injuries
1
Pilot’s flight hours
1,250 total23 in this make and model60 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Encountered wake vortex landing behind a 757. Rolled perpendiculer. Lost control crashed and burned. (.4)this was the pilot's first night trip for the company and his fourth stop on a seven leg trip. The previous three legs were reported as uneventful, and had lasted a total of 3 hours and 9 minutes. During arrival at night, the pilot was cleared by ATC to follow a Boeing 757 on final approach for runway 10R. He was cautioned three times about possible wake turbulence from the Boeing 757 and he confirmed that he had the jet in sight. A witness reported observing the aircraft roll 90 degrees perpendicular to the runway into a steep descending nose low attitude and collide with the terrain while in close trail behind the 757. Radar data showed that the accident airplane stayed above the flight path of the Boeing 757 3 to 5 miles out. The Boeing 757 touched down about 1,000 feet down the runway, while the accident airplane flew a steeper approach and impacted the runway about 700 feet from the approach end. According to the pilot's evaluation form dated April 8, 15 days before the accident, the pilot was counseled not to, 'dive f or the runway toward the end of the approach.' According to advisory circular dated October 1, 1991, when landing behind la larger aircraft-same runway, stay at or above the larger aircraft's final approach flightpath-note touchdown point-land beyond it. The reported winds ar the time of the accident was calm. Examination of the engine and airframe did not disclose any evidence of mechanical malfunction. (-23) see narrative #IAD98FA047

As the FAA filed it

ENCOUNTERED WAKE VORTEX LANDING BEHIND A 757. ROLLED PERPENDICULER. LOST CONTROL CRASHED AND BURNED. (.4)THIS WAS THE PILOT'S FIRST NIGHT TRIP FOR THE COMPANY AND HIS FOURTH STOP ON A SEVEN LEG TRIP. THE PREVIOUS THREE LEGS WERE REPORTED AS UNEVENTFUL, AND HAD LASTED A TOTAL OF 3 HOURS AND 9 MINUTES. DURING ARRIVAL AT NIGHT, THE PILOT WAS CLEARED BY ATC TO FOLLOW A BOEING 757 ON FINAL APPROACH FOR RUNWAY 10R. HE WAS CAUTIONED THREE TIMES ABOUT POSSIBLE WAKE TURBULENCE FROM THE BOEING 757 AND HE CONFIRMED THAT HE HAD THE JET IN SIGHT. A WITNESS REPORTED OBSERVING THE AIRCRAFT ROLL 90 DEGREES PERPENDICULAR TO THE RUNWAY INTO A STEEP DESCENDING NOSE LOW ATTITUDE AND COLLIDE WITH THE TERRAIN WHILE IN CLOSE TRAIL BEHIND THE 757. RADAR DATA SHOWED THAT THE ACCIDENT AIRPLANE STAYED ABOVE THE FLIGHT PATH OF THE BOEING 757 3 TO 5 MILES OUT. THE BOEING 757 TOUCHED DOWN ABOUT 1,000 FEET DOWN THE RUNWAY, WHILE THE ACCIDENT AIRPLANE FLEW A STEEPER APPROACH AND IMPACTED THE RUNWAY ABOUT 700 FEET FROM THE APPROACH END. ACCORDING TO THE PILOT'S EVALUATION FORM DATED APRIL 8, 15 DAYS BEFORE THE ACCIDENT, THE PILOT WAS COUNSELED NOT TO, 'DIVE F OR THE RUNWAY TOWARD THE END OF THE APPROACH.' ACCORDING TO ADVISORY CIRCULAR DATED OCTOBER 1, 1991, WHEN LANDING BEHIND LA LARGER AIRCRAFT-SAME RUNWAY, STAY AT OR ABOVE THE LARGER AIRCRAFT'S FINAL APPROACH FLIGHTPATH-NOTE TOUCHDOWN POINT-LAND BEYOND IT. THE REPORTED WINDS AR THE TIME OF THE ACCIDENT WAS CALM. EXAMINATION OF THE ENGINE AND AIRFRAME DID NOT DISCLOSE ANY EVIDENCE OF MECHANICAL MALFUNCTION. (-23) SEE NARRATIVE #IAD98FA047

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.