N552CS

Substantial
Minor

Enstrom F-28CS/N: 437

Accident Details

Date
Saturday, November 23, 2002
NTSB Number
DEN03LA018
Location
Morrison, CO
Event ID
20021203X05550
Coordinates
39.641666, -105.166664
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
1
Total Aboard
2

Probable Cause and Findings

the pilot not maintaining clearance from the telephone lines during landing. Factors contributing to the accident were the pilot not being able to see the telephone lines, the low altitude, and the dark night.

Aircraft Information

Registration
N552CS
Make
ENSTROM
Serial Number
437
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
F-28CEN28
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
5264 WCR 16 3/4
Status
Deregistered
City
LONGMONT
State / Zip Code
CO 80504
Country
United States

Analysis

On November 22, 2002, at 1830 mountain standard time, an Enstrom F-28C helicopter, N552CS, piloted by a private pilot, sustained substantial damage when it made a hard landing in a ditch along a road near Morrison, Colorado. Prior to the hard landing, the helicopter's tail rotor struck telephone lines during a landing attempt. Night visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted without a flight plan under the provisions of 14 CFR Part 91. The pilot reported minor injuries. The passenger on board reported no injuries. The flight originated at Longmont, Colorado, at 1800.

In his written statement, the pilot said he was approaching a landing area, located just east of a restaurant, from the south. The pilot said that during the approach he could not see the lighted flag on top of the restaurant, thus he could not determine the wind direction or velocity for landing. He said he executed a go around and began maneuvering so that he could approach the landing area from the east. The pilot said that at the "northern most point of the go around, a tail rotor strike was felt." The pilot immediately put the helicopter down on a road.

An examination of the wreckage showed the left skid broken upward. The right skid was bent upward and the bottom fuselage, aft of the pilot seat, was crushed upward. Both tail rotor blades were bent near mid span. Both main rotor blades were bent and twisted. Control continuity was confirmed. An examination of the helicopter's systems revealed no anomalies.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN03LA018