ANC01LA081

NTSB accident investigation · Lockheed L-382G · Lake Minchumina, AK · July 2, 2001

Accident · No injuriesLimited investigationFinal report
Date
July 2, 2001, 08:50 local (16:50 UTC)
Place
Lake Minchumina, AK
Injuries
4 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N401LCLockheed L-382G
Weather
Visual (VMC) · Day
Status
Completed · report June 3, 2002
Report
Approved by Office Director
NTSB office
Alaska Regional Office
Parties
Federal Aviation Administration
FAA report
20010702017079A
Case key
52632

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

The flight crew's improper recovery from a bounced landing. Factors associated with the accident were the selection of an unsuitable landing area, and a rough/uneven landing surface.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Dragged wing,rotor,pod,float or tail/skidLanding - flare/touchdown
Unsuitable terrain or takeoff/landing/taxi area - selectedFlightcrewFactor
Terrain condition - rough/unevenFactor
Recovery from bounced landing - improperFlightcrewCause

Analysis

The crew of the arriving cargo flight flew over the airport to inspect the runway conditions, and subsequently elected to use runway 20, a 4,200 feet long, 90 feet wide, gravel runway. The crew noted that the runway surface had a number of frost-heaves that had developed during the past winter. During the initial landing touchdown, the airplane "skipped" as the main wheels touched on the crest of one of the frost-heaves. The airplane became airborne, floated slightly, touched again about 750 feet beyond the approach end of the runway. During the second landing flare, the main landing gear wheels touched on the downhill side of a second frost-heave, which allowed the tail of the airplane to contact the gravel runway. The captain characterized the second touchdown as within acceptable limits, but with a slightly nose high attitude. A postflight inspection by the crew discovered a 4 feet by 2 feet puncture on the belly of the airplane, just forward of the main cargo door.

Factual narrative

On July 2, 2001, about 0850 Alaska daylight time, a Lockheed L-382G airplane, N401LC, sustained substantial damage during landing at the Lake Minchumina Airport, Lake Minchumina, 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 a load master, were not injured. Visual meteorological conditions prevailed, and an IFR flight plan was filed. The flight originated at the Ted Stevens International Airport, Anchorage, Alaska, about 0800.

During a telephone conversation with the National Transportation Safety Board investigator-in-charge on July 2, the director of operations for the operator reported the airport has a gravel runway that is oriented on a 020/200 degree heading. He added that the captain flew over the airport to inspect the runway conditions, and subsequently elected to use runway 20. He said that the runway is 4,200 feet long, 90 feet wide, and that the gravel runway had a number of frost-heaves that have developed during the past winter. The director of operations said that the captain was making an approach to runway 20, and on initial touchdown the airplane "skipped" as the main wheels touched down on the crest of one of the frost-heaves. He said that the airplane became airborne, floated slightly, and then touched down about 750 feet beyond the approach end of the runway. During the second landing flare, the main landing gear wheels touched on the downhill side of a second frost-heave, which allowed the tail of the airplane to contact the gravel runway. The captain characterized the second touchdown as within acceptable limits, but with a slightly nose high attitude. After touchdown, the captain lowered the nose of the airplane, brought the engines into reverse, and completed the landing. After landing rollout, the airplane was taxied to parking. A postflight inspection by the crew discovered a 4 feet by 2 feet puncture on the belly of the airplane, just forward of the main cargo door.

Aircraft

Registration
N401LC
Reported as
Lockheed L-382G
Category
Airplane
Serial number
4606
Airframe hours
31,652.8
Engine
Allison 501-D22A, 4,368 horsepower, turbo prop
Damage
Substantial damage
Flight
Part 121
Registered owner
Lynden Air Cargo LLC
Airworthiness certificate
Standard, Normal
Last inspection
Continuous airworthiness · April 10, 2001 · 285.7 hours before
Departed
ANC · Anchorage, AK
Destination
MHM · Lake Minchumina, AK
Flight plan
IFR
Airport
MHM · Minchumina, runway 20, 4,200 × 90 ft, gravel

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew · 4

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
37
Injuries
None
Certificate
Airline transport
Airplane ratings
Single-engine sea, Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Last flight review
January 31, 2001
Seat
Left
Flight hours
15,000 total · 2,200 in this make and model · 11,000 as pilot in command · 200 in the last 90 days · 70 in the last 30 days · 7 in the last 24 hours
Role
Co-pilot
Injuries
None
Role
Flight engineer
Injuries
None
Role
Other flight crew
Injuries
None

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
55 °F, dew point 46 °F
Altimeter
30.14 inHg

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N401LC · 2

Matched to the same aircraft by N-number and date.