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WPR13LA429

2013-09-29 · Santa Maria, California, United States · Minor · 1 aircraft · Status: Completed

Current FAA registration · N38113

Make / Model
TEXAS HELICOPTER CORP OH-13E/M74
Engine
LYCOMING VO-435 SERIES (260 hp)
Seats / Engines
1 seats · 1 engine
Last airworthiness date
19780126
ADS-B equipped
Yes — Mode-S A46198

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's inadequate monitoring of the environment and failure to maintain clearance from transmission wires during a low-altitude maneuver.

Factual narrative

On September 29, 2013, about 0930 Pacific daylight time, a Texas Helicopter Corp OH-13/M74, N38113, was substantially damaged when it struck power transmission wires and impacted the ground near Santa Maria, California. The commercial pilot, the sole occupant, received minor injuries. R & S Crop Dusters, Inc., was operating the helicopter under the provisions of 14 Code of Federal Regulations Part 137. Visual meteorological conditions prevailed for the local aerial application flight, which had originated from a nearby staging area approximately 10 minutes before the accident. A flight plan had not been filed. The pilot reported that before he began his first application run, he flew overhead scouting the designated field for hazards and noted the power line. On his first pass, he had a "momentary lapse" and flew through the wires. The biggest wire shattered the cabin's main Plexiglass bubble and struck the main rotor mast. Both push-pull flight control tubes were compromised just above the swashplate. The helicopter fell to the ground and came to rest upright on its landing skids. The pilot reported no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation. The pilot reported that before he began his first aerial application run, he flew overhead to scout the designated field for hazards and noted a power line near the field. He stated that he had a "momentary lapse" during his first application pass and flew through the wires, which shattered the cabin's main Plexiglass bubble and struck the main rotor mast. Both push-pull flight control tubes were compromised just above the swashplate. The helicopter fell to the ground and came to rest upright on its landing skids. The pilot reported no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Personnel issues-Psychological-Attention/monitoring-Monitoring environment-Pilot - C
  • — Environmental issues-Physical environment-Object/animal/substance-Wire-Response/compensation

Verbatim from NTSB's published report. Source file NTSB_2013_WPR13LA429.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.