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Last updated: 16 November 2019
Statuts:Enquête Officielle
Date:vendredi 26 juin 1998
Heure:14:03
Type/Sous-type:Silhouette image of generic C130 model; specific model in this crash may look slightly different
Lockheed L-100-30 Hercules
Compagnie:Lynden Air Cargo
Immatriculation: N402LC
Numéro de série: 4698
Année de Fabrication: 1976
Equipage:victimes: 0 / à bord: 5
Passagers:victimes: 0 / à bord: 0
Total:victimes: 0 / à bord: 5
Dégats de l'appareil: Substantiels
Conséquences: Repaired
Lieu de l'accident:Hog River Airport, AK (   Etats-Unis d'Amérique)
Phase de vol: A l'atterrissage (LDG)
Nature:Cargo
Aéroport de départ:Fairbanks International Airport, AK (FAI/PAFA), Etats-Unis d'Amérique
Aéroport de destination:?
Détails:
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:
cover
Investigating agency: NTSB
Status: Investigation completed
Duration: 1 year and 8 months
Accident number: ANC98LA085
Download report: Summary report

Sources:
» NTSB


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Les informations ci-dessus ne représentent pas l'opinion de la 'Flight Safety Foundation' ou de 'Aviation Safety Network' sur les causes de l'accident. Ces informations prélimimaires sont basées sur les faits tel qu'ils sont connus à ce jour.
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