N96161

Substantial
None

Bell TH-13T S/N: 3547

Accident Details

Date
Sunday, June 30, 1996
NTSB Number
CHI96LA223
Location
MANDAN, ND
Event ID
20001208X05943
Coordinates
46.820358, -100.880111
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 clearance from known transmission lines. A factor relating to this accident was the sunglare which hindered the pilot's ability to see the transmission lines.

Aircraft Information

Registration
Make
BELL
Serial Number
3547
Engine Type
Reciprocating
Model / ICAO
TH-13T
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
TH-13T

Registered Owner (Current)

Name
SCOTTS HELICOPTER SERVICES INC
Address
PO BOX 92
City
LE SUEUR
State / Zip Code
MN 56058
Country
United States

Analysis

On June 30, 1996, at 1320 central daylight time, a Bell TH-13T, N96161, operated by a commercial pilot, sustained substantial damage when while performing an aerial application, 18 miles northwest of Mandan, North Dakota, it struck some high line utility wires. The helicopter subsequently impacted the terrain. Visual meteorological conditions prevailed at the time of the accident. The aerial application flight was being conducted under 14 CFR Part 137. No flight plan was on file, and the pilot reported no injuries. The local flight originated at Mandan, North Dakota.

In his written statement, the pilot said he was spot spraying pasture land with pesticide when he "turned into the sun heading east to follow a ravine. The sun was just right in the sky and was glaring off my bubble were I could not see the power lines until I was too close." When the pilot did see the power lines he "pulled back and to the left to avoid them." The helicopter's lower outside cabin struck the lines and the helicopter "went into the ground tail first."

The Federal Aviation Administration (FAA) inspector who examined the wreckage at the site found the helicopter resting in the bottom of a ravine, beneath the power lines, oriented on a 270 degree heading. The cockpit bubble windscreen had separated from the frame and was broken. The aircraft frame which formed the cockpit was broken in several places. The pilot's seat was undamaged. The tail boom had broken at mid-span. The aft section of the boom and tail rotor was resting 40 feet south of the main wreckage. The boom exhibited upward bending at the points where it broke. Both tail rotor blades showed cuts in the leading edges at approximately mid-span. The forward frame, which held the engine and transmission, was twisted and bent. Both main rotor blades showed cuts on the inboard leading edges, approximately 5 feet outboard of the hub. There were also cuts on the blades' leading edges 3 feet inboard from the tips. Flight control continuity was established. No anomalies with the engine, engine controls or transmission were found.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI96LA223