N410QX

Unknown
None

Bombardier DHC-8-401S/N: 4053

Accident Details

Date
Saturday, March 2, 2002
NTSB Number
SEA02IA044
Location
Boise, ID
Event ID
20020312X00331
Aircraft Damage
Unknown
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
73
Total Aboard
73

Probable Cause and Findings

The partial failure of one of the number two hydraulic system elevator hydraulic lines, leading to the loss of fluid and pressure in that system during cruise flight. This loss resulted in reliance upon the sole remaining activation system (number one hydraulic) to operate the rudder.

Aircraft Information

Registration
N410QX
Make
BOMBARDIER
Serial Number
4053
Year Built
2001
Model / ICAO
DHC-8-401

Registered Owner (Historical)

Name
AVIATION MARKETING GROUP INC
Address
1076 WESSINGTON MANOR LN
Status
Deregistered
City
FORT MILL
State / Zip Code
SC 29715-7850
Country
United States

Analysis

On March 1, 2002, approximately 1840 mountain standard time, a Horizon Airlines Bombardier DHC-8-401, N410QX, experienced a failure of the number two hydraulic system during en route cruise to Boise, Idaho. The airline transport pilot, his first officer, the two flight attendants, and the 69 passengers were not injured, and the aircraft did not sustain any damage. The 14 CFR Part 121 scheduled passenger flight, which departed Seattle-Tacoma International Airport, Seattle, Washington, about two hours earlier, was being operated in visual meteorological conditions. The flight, which was on an IFR flight plan, eventually landed at its destination around 1900. There was no emergency evacuation.

According to the flight crew, during en route cruise, they noticed the number two hydraulic system quantity beginning to decrease. As they began to run the appropriate checklist, they noticed the illumination of several hydraulic system caution lights. Eventually, the number two system lost pressurization, and the rudder became dependent upon the sole remaining system (hydraulic system number one) for its movement. After the landing gear was extended manually, the aircraft landed without further incident, but it had to be towed from the runway, as the failure of the number two system rendered the nose wheel steering inoperable.

It was later discovered that the number two system hydraulic line to the elevator had failed, leading to a loss of pressure in the number two system. The reason for the failure could not be positively determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA02IA044