N414RX

Substantial
Fatal

AIRBUS HELICOPTERS EC 130 T2S/N: 8909

Accident Details

Date
Tuesday, October 7, 2025
NTSB Number
WPR26FA008
Location
Sacramento, CA
Event ID
20251007201802
Coordinates
38.558524, -121.452480
Aircraft Damage
Substantial
Highest Injury
Fatal
Fatalities
1
Serious Injuries
2
Minor Injuries
0
Uninjured
0
Total Aboard
3

Aircraft Information

Registration
Make
AIRBUS HELICOPTERS
Serial Number
8909
Engine Type
Turbo-shaft
Year Built
2021
Model / ICAO
EC 130 T2
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
8
FAA Model
EC 130 T2

Registered Owner (Current)

Name
REACH AIR MEDICAL SERVICES LLC
Address
2360 BECKER BLVD
City
SANTA ROSA
State / Zip Code
CA 95403-8270
Country
United States

Analysis

On October 6, 2025, about 1905 Pacific daylight time, an Airbus Helicopters EC-130 T2, N414RX, was substantially damaged when it was involved in an accident in Sacramento, California. The pilot and flight paramedic sustained serious injuries; the flight nurse succumbed to her injuries 4 days after the accident. The helicopter was operated as a Title 14 Code of Federal Regulations Part 135 air medical flight.

The helicopter departed UC Davis Medical Center Tower II Heliport (3CLO), Sacramento, California, with a planned destination of Mc Clellan Airfield (MCC), Sacramento, California. The flight paramedic reported that shortly after takeoff she noticed the power had gone out and the helicopter was autorotating towards U.S. Route 50. She made a mayday call on the company radio frequency.

Subsequently, the helicopter came to rest on its left side in the eastbound lanes of U.S. Route 50, about 1,600 ft north of 3CLO. A main rotor blade ground impression was observed on the residential side of the fence that enclosed the highway. Furthermore, a section of the outer portion of the main rotor blade was discovered embedded in the roof of a detached garage on a residential home located next to the highway.

A review of ADS-B data revealed that the total accident flight was about 26 seconds. The data showed the helicopter departed the helipad and climb to a maximum altitude of about 500 ft mean sea level. Shortly thereafter, the helicopter was in descent for the final 11 seconds of the flight.

Postaccident examination revealed that the helicopter’s fuselage and main rotor blades sustained substantial damage. The helicopter was recovered and retained for further examination.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR26FA008