N3623T

Substantial
None

Schweizer 269C S/N: S1567

Accident Details

Date
Friday, January 12, 1996
NTSB Number
FTW96LA095
Location
SAN YGNACIO, TX
Event ID
20001208X05137
Coordinates
27.129295, -99.330513
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

Failure of the rotor drive system clutch assembly (separation of the swedge ball from the end of the clutch control cable), which resulted in disengagement of the rotor drive system, while the helicopter was in lateral movement at low altitude.

Aircraft Information

Registration
N3623T
Make
SCHWEIZER
Serial Number
S1567
Engine Type
Reciprocating
Year Built
1991
Model / ICAO
269C H269
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
ADKINS FLITE CENTER INC
Address
10244 FM 1346
Status
Deregistered
City
ADKINS
State / Zip Code
TX 78101-9705
Country
United States

Analysis

On January 12, 1996, at 0930 central standard time, a Schweizer 269C, N3623T, sustained substantial damage during a forced landing near San Ygnacio, Texas. The commercial helicopter pilot and his passenger were not injured. The aircraft was registered to and operated by Smith Helicopters under Title 14 CFR Part 91. The flight originated from a private airstrip near San Ygnacio, Texas, at 0900. Visual meteorological conditions prevailed for the local flight and no flight plan was filed.

The pilot reported that he heard a loud "bang" while hovering sideways at approximately 12 MPH at 70 feet out of ground effect. He responded by applying the right anti torque pedal to straighten the helicopter, however the helicopter did not respond to pedal inputs. According to the pilot, the engine produced high RPM, but the tail rotor and main rotor RPM decreased. The pilot initiated an autorotation. The pilot further reported that, during touchdown with lateral movement, the helicopter rolled over coming to rest on its right side. The tail boom, the engine mount, and the skids sustained substantial damage, and the tail rotor separated from the helicopter.

Inspection of the aircraft revealed that the swedged ball on the end of the clutch control cable had separated, which allowed the rotor drive system's clutch assembly to disengage.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW96LA095