N41NE

Unknown
None

Fairchild SA227-ACS/N: 741B

Accident Details

Date
Friday, January 18, 2008
NTSB Number
ANC08IA033
Location
Dutch Harbor, AK
Event ID
20080411X00456
Coordinates
53.906944, -166.549163
Aircraft Damage
Unknown
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The disengagement of the rudder control cable and loose rudder cable retaining pins. A factor contributing to the accident was a wind gust.

Aircraft Information

Registration
N41NE
Make
FAIRCHILD
Serial Number
741B
Year Built
1989
Model / ICAO
SA227-AC

Registered Owner (Historical)

Name
PENINSULA AIRWAYS INC DBA
Address
6100 BOEING AVE
Status
Deregistered
City
ANCHORAGE
State / Zip Code
AK 99502-1000
Country
United States

Analysis

On January 18, 2008, about 1245 Alaska standard time, a Fairchild SA227-AC airplane, N41NE, had a rudder malfunction after encountering a severe wind gust during taxi for takeoff at the Dutch Harbor Airport, Dutch Harbor, Alaska. The airplane was being operated by Peninsula Airways Inc., Anchorage, Alaska, as an instrument flight rules (IFR) nonscheduled cargo flight under Title 14, CFR Part 121. The airline transport certificated pilot and the first officer were not injured. Visual meteorological conditions prevailed at the departure airport, and an instrument flight rules flight plan was filed and activated. The airplane departed Dutch Harbor, and landed at the Ted Stevens International Airport, Anchorage, without incident.

In a written statement, the pilot reported that during taxi for takeoff at Dutch Harbor, the airplane encountered a 68 knot wind gust. He said that they returned to the gate to examine the rudder because this airplane model has a history of rudder damage when encountering extreme wind gusts. Finding no damage, they elected to continue the flight. During initial climb after takeoff, the pilot said there was little, if any, left rudder control. The flight continued to the destination and landed without incident.

The airplane was examined by an FAA air safety inspector. From the pilot's position, the rudder is controlled by a cable which makes a 180 degree turn toward the tail via two phenolic pulleys. Each of the pulleys has two guard pins (P/N: NAS427W18), which keep the cable from jumping off the pulleys if the cable becomes slack. During the inspection, the inspector reported that the cable had jumped off the upper pulley, disabling the rudder system. She noted that the pulley's guard pin was retracted, and did not prevent the cable from being dislodged. The guard pin is a hollow roll pin with a perforated and deformed end, giving it a spring action which secures the pin after passing through the holes on either side of the pulley bracket. She said there are no current service difficulty reports on file for the pins, and they do not have any service life limits.

During an examination of all the same model airplanes in the operator's fleet, maintenance personnel found several guard pins that had come loose and retracted from their respective brackets. According to the director of maintenance for the operator, it appears that the pin's locking action becomes weakened by repeated use. The operator elected to replace all the pins in the operator's fleet, and submitted a service difficulty report to the FAA.

As a result of this incident, the manufacturer has published service letters 226-SL-037, 227-SL052, and CC7-SL-045. The service letters require at the next scheduled access that the pins be inspected, and that all pins (P/N NAS427K18) be replaced with pins (P/N NAS427W18), and secured with cotter pins (P/N MS24665-132).

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC08IA033