N72DCSCHWEIZER 269C2011-07-03 NTSB Accident Report

Substantial
None

SCHWEIZER 269CS/N: S1624

Summary

On July 03, 2011, a Schweizer 269C (N72DC) was involved in an incident near Katy, TX. All 1 person aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The pilot's failure to maintain adequate rotor rpm during a low-altitude maneuvering flight.

The helicopter pilot was flying between six and seven feet above the ground, at an airspeed of 20 knots, over a field of rice to cross-pollinate the crop. The pilot stated that he encountered a low rotor rpm situation and the helicopter started to settle. As soon as the helicopter descended, the landing skid became tangled in the rice plants, the helicopter impacted the rice field, and came to rest on its side. During the collision with terrain, the tail boom and main rotor separated from the fuselage. An examination of the helicopter and its systems, conducted by a Federal Aviation Administration inspector, revealed no preimpact mechanical failures or malfunctions.

This incident is documented in NTSB report CEN11CA442. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N72DC.

Accident Details

Date
Sunday, July 3, 2011
NTSB Number
CEN11CA442
Location
Katy, TX
Event ID
20110703X00318
Coordinates
29.727222, -95.899719
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain adequate rotor rpm during a low-altitude maneuvering flight.

Aircraft Information

Registration
Make
SCHWEIZER
Serial Number
S1624
Engine Type
Reciprocating
Year Built
1992
Model / ICAO
269CH269
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
DYLAN AVIATION LLC
Address
518 SCHOOL ST
Status
Deregistered
City
HOUMA
State / Zip Code
LA 70360-4568
Country
United States

Analysis

The helicopter pilot was flying between six and seven feet above the ground, at an airspeed of 20 knots, over a field of rice to cross-pollinate the crop. The pilot stated that he encountered a low rotor rpm situation and the helicopter started to settle. As soon as the helicopter descended, the landing skid became tangled in the rice plants, the helicopter impacted the rice field, and came to rest on its side. During the collision with terrain, the tail boom and main rotor separated from the fuselage. An examination of the helicopter and its systems, conducted by a Federal Aviation Administration inspector, revealed no preimpact mechanical failures or malfunctions.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN11CA442