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Aviation safety reports, made easier to study

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NTSB Report

June 26, 1998 · Lockheed L-382G · N402LC

Huslia, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 26, 1998
Injury Outcomes
No injuries (5 uninjured)
Location
Huslia, AK
Aircraft
Lockheed L-382G
Tail Number
N402LC
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC98LA085

A transport category cargo airplane was landing on a remote, private airport. The runway was 4,300 feet long, and varied between 100 and 80 feet wide. The captain indicated the wind conditions were light and variable. He landed toward the north, and planned to touch down in the first few hundred feet of the approach end of the runway. 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. The left wing collided with a 3 inch diameter tree, and 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.

NTSB Probable Cause

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

Full Narrative

On June 26, 1998, about 1403 Alaska daylight time, a Lockheed L-382G airplane, 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 under Title 14 CFR Part 121, when the accident occurred. The airplane was registered to, and operated by Lynden Air Cargo LLC. The crew of the airplane, consisting of the captain, first officer, flight engineer, and two load masters, were not injured. Visual meteorological conditions prevailed. A IFR flight plan was filed. The flight originated at the Fairbanks International Airport, Fairbanks, Alaska, about 1247. The chief pilot for the operator reported the airport has a gravel runway that is oriented on a 300/120 degree heading. The runway is 4,300 feet long, and varies between 100 and 80 feet wide. 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.

Flight

Event TypeAccident
Event Time14:03 AKDT
Nearest AirportHOGRIVER (0nm)
Runway30
Runway Length4300 ft
Runway Width80 ft
Flight Plan FiledIFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftLockheed L-382G
Tail NumberN402LC
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 121
Engines4
Engine TypeTurboprop
Engine DetailsAllison · T-56 · Turboprop · 4500
Seats5

People & Injuries

Injury SummaryNo injuries (5 uninjured)
Fatal0
Serious0
Minor0
Uninjured5
Total5
Crew 1Age 54 · First Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility50 sm
CeilingNone
Temperature / Dew Point61 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data