N44508

Substantial
None

BURR EXPRESS 2000 RGS/N: 0101RG

Accident Details

Date
Friday, May 29, 2015
NTSB Number
WPR15LA179
Location
Glendale, AZ
Event ID
20150605X64827
Coordinates
33.522777, -112.290557
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A collapse of the left main landing gear for reasons that could not be determined based on the available information.

Aircraft Information

Registration
Make
BURR
Serial Number
0101RG
Engine Type
Turbo-prop
Year Built
2008
Model / ICAO
EXPRESS 2000 RG
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
EXPRESS 2000 RG

Registered Owner (Current)

Name
AEROMANIA LLC
Address
5641 RED BLUFF
City
CHEYENNE
State / Zip Code
WY 82009
Country
United States

Analysis

On May 29, 2015, about 1542 mountain standard time, a Burr Express 2000 RG, N44508, experienced a landing gear collapse during the landing roll at Glendale Municipal Airport (GEU) in Glendale, Arizona. The private pilot and one passenger were uninjured, and the airplane sustained substantial damage to the rudder and elevators. The airplane was registered to, and operated by, the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed and no flight plan was filed. The flight departed from GEU at about 1500.

The pilot reported that he landed the airplane onto the runway normally. He applied beta thrust to decelerate the airplane and started to brake lightly. Suddenly, the left main landing gear collapsed and the airplane swerved to the left. The airplane departed the runway surface and the left wing impacted a runway sign. It traversed along the dirt when the right landing gear collapsed and the tail impacted the ground before sliding to a rest.

During a postaccident examination by a Federal Aviation Administration Inspector it was revealed that the left main landing gear actuator heim rod failed where the threads meet the rod end. Given the location of the heim rod, the inspector was unable to view the fracture surface while the component was installed on the airplane. In addition, the inspector noted that the hydraulic line to the gear actuator was ripped.

The National Transportation Safety Board Investigator-in-charge attempted to obtain the heim rod for further examination, however, the pilot had already repaired the airplane and the part was no longer available.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR15LA179