N7508L

Substantial
None

Schweizer 269CS/N: S1417

Accident Details

Date
Tuesday, August 20, 2002
NTSB Number
DEN02LA098
Location
Broomfield, CO
Event ID
20020903X01502
Coordinates
39.908611, -105.117225
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

maintenance personnel's failure to secure the landing skid oleo strut bolt during the last 50-hour inspection, causing the left rear skid to collapse and the tail rotor to strike the ground.

Aircraft Information

Registration
Make
SCHWEIZER
Serial Number
S1417
Engine Type
Reciprocating
Year Built
1989
Model / ICAO
269CH269
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
269C

Registered Owner (Current)

Name
BRUEGGER SHANNON B
Address
496 COW CREEK RD
City
LANCE CREEK
State / Zip Code
WY 82222
Country
United States

Analysis

On August 20, 2002, approximately 1120 mountain daylight time, a Schweizer 269C, N7508L, operated by Rotors of the Rockies, was substantially damaged when the left rear landing skid collapsed during a practice autorotation at Jefferson County Airport, Broomfield, Colorado. The commercial pilot receiving instruction and the commercial flight instructor were not injured. Day visual meteorological conditions prevailed at the time, and no flight plan had been filed for the instructional flight being conducted under Title 14 CFR Part 91. The flight originated at Broomfield at an undetermined time.

According to the flight instructor's accident report, the student was practicing autorotations in preparation for taking his rotorcraft-helicopter practical flight test the following day. They had successfully performed two "full down" autorotations. As the student completed the third autorotation, they heard a loud noise and the helicopter settled toward the left rear, enough that the tail rotor struck the asphalt taxiway. Postaccident inspection disclosed that the bolt that attaches the left rear oleo strut to the crossbeam was missing. The tail rotor blades were damaged, the tail rotor driveshaft was twisted, and the splined end was separated from the main transmission. The skids and fuselage bottom were not damaged.

According to maintenance records, the helicopter had accrued 5.1 hours since the last 50-hour inspection, at which time the landing gear struts had been overhauled and the skid shoes replaced.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN02LA098