19980208001009A

Accident · Substantial damage

FAA accident report · Beech C23 · Minneapolis, MN · February 8, 1998

Date
February 8, 1998 · 14:40 local
Place
Minneapolis, MN
Airport
Flying Cloud Airport
Phase of flight
Go Round (Aborted VFR)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N18766
NTSB investigation
NTSBCHI98LA092
Reported as
Beech C23
Reported engine
Lycoming O360A4K
Fatal injuries
0
Pilot’s flight hours
225 total112 in this make and model2 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.

Bounced propoised landing. Began go around yaw and rolled left. Strcuk hangar fence and ditch. Torque and p factors/ (-23) it appears that Mr. Burstad improperly executed a "go-around" which precipitated the accident. Based on Mr. Brustad's testimony, he was not fully prepared for a "straight-in" clearance to rwy 18 at fcm. He was high and configured the aircraft for landing. On landing, the aircraft bounced twice. He elected to go-around. He retracted flaps to zero, added power, and lost directional control. The right wing of the aircraft struck a hangar which caused Mr. Brustad to lose complete aircraft control. The aircraft then struck power lines, a chain link fence and ditch, coming to rest on a highway.

As the FAA filed it

BOUNCED PROPOISED LANDING. BEGAN GO AROUND YAW AND ROLLED LEFT. STRCUK HANGAR FENCE AND DITCH. TORQUE AND P FACTORS/ (-23) IT APPEARS THAT MR. BURSTAD IMPROPERLY EXECUTED A "GO-AROUND" WHICH PRECIPITATED THE ACCIDENT. BASED ON MR. BRUSTAD'S TESTIMONY, HE WAS NOT FULLY PREPARED FOR A "STRAIGHT-IN" CLEARANCE TO RWY 18 AT FCM. HE WAS HIGH AND CONFIGURED THE AIRCRAFT FOR LANDING. ON LANDING, THE AIRCRAFT BOUNCED TWICE. HE ELECTED TO GO-AROUND. HE RETRACTED FLAPS TO ZERO, ADDED POWER, AND LOST DIRECTIONAL CONTROL. THE RIGHT WING OF THE AIRCRAFT STRUCK A HANGAR WHICH CAUSED MR. BRUSTAD TO LOSE COMPLETE AIRCRAFT CONTROL. THE AIRCRAFT THEN STRUCK POWER LINES, A CHAIN LINK FENCE AND DITCH, COMING TO REST ON A HIGHWAY.

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 N18766 · 1

Matched to the same aircraft by N-number and date.