N105TV

MINR
None

EUROCOPTER AS 350 B2S/N: 2279

Accident Details

Date
Tuesday, May 22, 2012
NTSB Number
WPR12IA248
Location
Seattle, WA
Event ID
20120605X33610
Coordinates
47.466945, -122.335281
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

Failure of maintenance personnel to ensure that the tail rotor pitch change link bolt was properly secured, which resulted in an in-flight separation of the bolt and subsequent vibration.

Aircraft Information

Registration
N105TV
Make
EUROCOPTER
Serial Number
2279
Year Built
1989
Model / ICAO
AS 350 B2

Registered Owner (Historical)

Name
PYLON AVIATION HOLDINGS LLC
Address
16192 COASTAL HWY
Status
Deregistered
City
LEWES
State / Zip Code
DE 19958-3608
Country
United States

Analysis

On May 22, 2012, about 1430 Pacific daylight time, a Eurocopter AS-350 B2, N105TV, sustained minor damage following an in-flight separation of a tail rotor pitch change link bolt while maneuvering near the Seattle-Tacoma International Airport (SEA), Seattle, Washington. The airline transport pilot and aerial photographer crewmember were not injured. The helicopter was registered to KING Broadcasting Company, Seattle, Washington, and operated as an electronic news gathering flight under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and a company flight plan was activated for the flight that originated from Boeing Field (BFI), Seattle, Washington, about 1415. The pilot's planned destination was Seattle Private Number One Heliport (WN01).

The pilot reported that he had just entered a slow orbit, about 1,200 feet above the ground, when the helicopter experienced what he described as a severe vibration. The vibration was continuous and so severe that the pilot diverted to BFI for landing. He reported that just before landing, with full right pedal inputs, the helicopter entered a slow turn to the left, which continued until touchdown on the taxiway.

The pilot reported that a postincident examination of the helicopter revealed damage to the tail boom assembly and support structure. He reported the exam also revealed that one of the tail rotor pitch change link bolts (to the pitch arm) was missing and likely released during the flight, which resulted in an asymmetrical pitch between the two tail rotor blades and subsequent vibration.

The accident flight followed a 100-hour maintenance inspection that concluded earlier that day. The inspection included maintenance and service to the tail rotor assembly. The pilot reported that the pitch change link bolt (to pitch arm) was not correctly tightened and secured while in maintenance and subsequently loosened and released during the flight.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR12IA248