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Last updated: 31 July 2021
Datum:Freitag 26 Juni 1998
Flugzeugtyp:Silhouette image of generic C130 model; specific model in this crash may look slightly different
Lockheed L-100-30 Hercules
Fluggesellschaft:Lynden Air Cargo
Kennzeichen: N402LC
Werknummer: 4698
Baujahr: 1976
Besatzung:Todesopfer: 0 / Insassen: 5
Fluggäste:Todesopfer: 0 / Insassen: 0
Gesamt:Todesopfer: 0 / Insassen: 5
Sachschaden: schwer beschädigt
Konsequenzen: Repaired
Unfallort:Hog River Airport, AK (   USA)
Flugphase: Landung (LDG)
Flug von:Fairbanks International Airport, AK (FAI/PAFA), USA
Flug nach:?
A Lockheed Hercules transport plane, N402LC, sustained substantial damage during landing at the Hog River Airport, a private airport about 40 miles north of Huslia, Alaska. The airplane was being operated as an instrument (IFR) cross-country cargo flight when the accident occurred. The flight originated at the Fairbanks International Airport, Alaska, about 12:47.
The captain indicated he flew over runway 30 to inspect the runway, and observe the wind sock, which is located at the north end of the runway. The wind direction from the wind sock, a comparison of the airplane's airspeed, and ground speed indication from a global positioning system receiver (GPS), revealed variable wind conditions that were less than 10 knots. The captain decided to land toward the north, and planned to touch down in the first few hundred feet of the approach end of runway 30. During the landing flair, the airplane floated slightly, and then touched down about 1,200 feet beyond the approach end of the runway. After touch down, the captain lowered the nose of the airplane, and brought the engines into reverse. As the airplane decelerated, it drifted slightly to the left, but the captain indicated he did not notice any collision with any objects. After the airplane was parked, the crew noticed damage to the leading edge of the left wing, about 18 inches inboard from the tip.

An inspection of the leading edge revealed a collision with about a 3 inch diameter tree. The wing received aft crushing, damage to a wing nose rib, and slight denting of the wing spar web. The airplane has a wing span of 132 feet, 7 inches. The wing is 15 feet, 3 inches above the ground.

Probable Cause:

PROBABLE CAUSE: "The pilot's failure to maintain proper alignment of the airplane during the landing roll."

Accident investigation:
Investigating agency: NTSB
Status: Investigation completed
Duration: 1 year and 8 months
Accident number: ANC98LA085
Download report: Summary report



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This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
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