19980512008959A

Accident · Substantial damage

FAA accident report · Beech A23-24 · Holbrook, AZ · May 12, 1998

Date
May 12, 1998 · 11:00 local
Place
Holbrook, AZ
Airport
Holbrook Municipal Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N6092N
NTSB investigation
NTSBLAX98LA155
Reported as
Beech A2324
Reported engine
Lycoming IO360A2B
People aboard
2
Fatal injuries
0
Pilot’s flight hours
632 total554 in this make and model14 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.

Landing wind gust forced A23 off runway. Exceeded crosswing component. (.4)the pilot was attempting to land when he encountered a strong wind gust that turned the aircraft about 15 degrees to the right. He attempted a go-around, but was unable to gain altitude or maintain directional control. The aircraft collided with terrain and continued to slide forward. All three landing gear separated from the aircraft and both wing tips were torn off. The propeller struck the ground and the aircraft came to rest in an upright position about 120 degrees from the runway heading. The reported winds at the time of the accident were from 210 degrees at a velocity of 18 knots gusting to 23 knots. The pilot reported no mechanical malfunction with the aircraft prior to the accident.

As the FAA filed it

LANDING WIND GUST FORCED A23 OFF RUNWAY. EXCEEDED CROSSWING COMPONENT. (.4)THE PILOT WAS ATTEMPTING TO LAND WHEN HE ENCOUNTERED A STRONG WIND GUST THAT TURNED THE AIRCRAFT ABOUT 15 DEGREES TO THE RIGHT. HE ATTEMPTED A GO-AROUND, BUT WAS UNABLE TO GAIN ALTITUDE OR MAINTAIN DIRECTIONAL CONTROL. THE AIRCRAFT COLLIDED WITH TERRAIN AND CONTINUED TO SLIDE FORWARD. ALL THREE LANDING GEAR SEPARATED FROM THE AIRCRAFT AND BOTH WING TIPS WERE TORN OFF. THE PROPELLER STRUCK THE GROUND AND THE AIRCRAFT CAME TO REST IN AN UPRIGHT POSITION ABOUT 120 DEGREES FROM THE RUNWAY HEADING. THE REPORTED WINDS AT THE TIME OF THE ACCIDENT WERE FROM 210 DEGREES AT A VELOCITY OF 18 KNOTS GUSTING TO 23 KNOTS. THE PILOT REPORTED NO MECHANICAL MALFUNCTION WITH THE AIRCRAFT PRIOR TO THE ACCIDENT.

NTSB investigation

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