N7452F

Substantial
None

Hughes 269CS/N: 760522

Accident Details

Date
Sunday, October 26, 2003
NTSB Number
SEA04LA011
Location
Hillsboro, OR
Event ID
20031103X01856
Coordinates
45.423889, -122.941108
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's selection of unsuitable terrain for a practice auto rotation landing. A contributing factor was the soft terrain.

Aircraft Information

Registration
Make
HUGHES
Serial Number
760522
Engine Type
Reciprocating
Model / ICAO
269C
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
269C

Registered Owner (Current)

Name
REEP NIC K
Address
11904 BARRETT RD
City
YAKIMA
State / Zip Code
WA 98908-8508
Country
United States

Analysis

On October 26, 2003, approximately 1215 Pacific standard time, a Hughes 269C helicopter, N7452F, registered to and being operated/flown by a commercially rated flight instructor, sustained substantial damage during a nose down event following a low altitude auto-rotation landing at the Stark's Twin Oaks Airpark, Hillsboro (7S3), Oregon. Both the flight instructor and the pilot under instruction were uninjured. Visual meteorological conditions existed and no flight plan had been filed. The flight, which was instructional, was operated under 14CFR91, and originated from the Hillsboro airport (HIO), Hillsboro, Oregon, at 1145 on the morning of the accident.

The instructor reported to an inspector assigned to the Hillsboro Federal Aviation Administration's Flight Standards District Office that he was in control of the helicopter, which was moving forward in a hover at a "brisk walk." He initiated a demonstration of an auto-rotation while in the forward hover to a grassy area slightly east of the runway environment and upon touchdown, the helicopter's skids encountered soft terrain and dug in and the helicopter rocked forward up onto the toes of the skids. Immediately thereafter, the main rotor blades contacted the ground and the helicopter came to rest on the forward skid toes and the main rotor mast. The instructor reported that there was no mechanical malfunction with the helicopter at the time of the event and the terrain at the selected site for the auto-rotation was soft.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA04LA011