N172GA

Substantial
None

BEECH 1900CS/N: UB-11

Accident Details

Date
Monday, April 30, 2018
NTSB Number
CEN18LA164
Location
Sioux Falls, SD
Event ID
20180509X25604
Coordinates
43.581943, -96.741943
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Failure of the right main landing gear drag brace bolt for reasons that could not be determined based on the available information.

Aircraft Information

Registration
Make
BEECH
Serial Number
UB-11
Engine Type
Turbo-prop
Model / ICAO
1900CB190
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
19
FAA Model
1900C

Registered Owner (Current)

Name
ALPINE AVIATION INC
Address
1177 ALPINE AIR WAY
City
PROVO
State / Zip Code
UT 84601-8270
Country
United States

Analysis

On April 29, 2018, about 2230 central daylight time, a Beech 1900C, N172GA, was substantially damaged when the right main landing gear collapsed as the airplane started to taxi for takeoff at Joe Foss Field Airport (FSD), Sioux Falls, South Dakota. The airline transport pilot was not injured. The airplane was registered to and operated by Alpine Aviation, doing business as Alpine Air Express, under the provisions of Title 14 Code of Federal Regulations Part 135 as a non-scheduled domestic cargo flight. Visual meteorological conditions prevailed at the airport at the time of the accident, and an instrument flight rules flight plan had been filed. The flight was originating from FSD, and was destined for Rapid City Regional Airport (RAP), Rapid City, South Dakota.

According to Federal Aviation Administration (FAA) inspectors, the airplane had just moved forward to taxi for takeoff when the right main landing gear collapsed. A postaccident examination of the airplane revealed the right main landing gear drag brace bolt failed at the wing forward attach point. The drag brace bolt was not retained for further examination. The strut pivoted aft when the airplane moved forward, and the landing gear collapsed. The aft center wing lower spar cap was dented and deformed up to 0.090". Further examination found pitting corrosion on the spar cap.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN18LA164