ANC07LA032

NTSB accident investigation · Beech D18S · Levelock, AK · April 26, 2007

Accident · No injuriesLimited investigationFinal report
Date
April 26, 2007, 11:20 local (19:20 UTC)
Place
Levelock, AK
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N502CKBeech D18S
Weather
Visual (VMC) · Day
Status
Completed · report November 29, 2007
Report
Approved by Office Director
NTSB office
Alaska Regional Office
Parties
Anchorage FSDO-03
FAA report
20070426007529A
Case key
65645

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

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Probable cause

The NTSB’s determination of the probable cause, and any contributing factors.

The pilot's misjudged flare, which precipitated a hard landing, and damage to the main landing gear, resulting in a main landing gear collapse during the landing roll. A factor contributing to the accident was the overload failure of the main landing gear atachment.

Analysis

The airline transport certificated pilot was conducting a non-scheduled, domestic cargo flight under Title 14, CFR Part 135. The pilot reported that during the landing roll the right main landing gear collapsed, causing the airplane to exit the right side of the runway. An FAA air safety inspector who visited and photographed the site, said the airplane landed hard on the gravel runway threshold, became airborne again, and touched down about 300 feet down the runway. The inspector photographed main landing gear impact marks on the runway threshold. The marks were several inches deep, 3-6 feet in length, and had gravel sprayed forward and to each side of the track. The tracks began again about 300 feet down the runway. The tracks veered sharply off the right side of the runway, and terminated at the wreckage. The inspector provided a hand-drawn sketch of the marks with approximate distances. The airplane received damage to the landing gear attaching points, right wing, and fuselage.

Factual narrative

On April 26, 2007, about 1120 Alaska daylight time, a Beech D18S airplane, N502CK, sustained substantial damage when the right main landing gear collapsed after landing at the Levelock Airport, Levelock, Alaska. The airplane was being operated by Air Supply Alaska, Kenai, Alaska, as a visual flight rules (VFR) non-scheduled cargo flight under Title 14, CFR Part 135, when the accident occurred. The solo airline transport certificated pilot was not injured. Visual meteorological conditions prevailed, and a VFR flight plan was filed. The flight departed the Kenai Airport, Kenai, about 1025.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on April 27, the pilot said about 200 feet into the landing roll he heard the gear warning horn activate, and saw the gear in-transit light illuminate. He said the right main landing gear collapsed, and the airplane exited the runway. The pilot said the left gear sheared off as it encountered soft terrain on the side of the runway. He said the airplane sustained damage to right wing and the fuselage. The pilot reported that there were known problems with the landing gear prior to the accident.

On April 30, the NTSB IIC met with the FAA aviation safety inspector who visited, and photographed the accident site. He said the airplane landed hard on the runway threshold, became airborne again, and touched down about 300 feet down the runway. The runway is gravel, and the inspector provided photographs that showed impact marks from the main landing gear on the runway threshold. The marks were several inches deep, 3-6 feet in length, and had gravel sprayed forward and to each side of the track. The tracks began again about 300 feet down the runway, with the left main landing gear touching first, followed by the right main landing gear, and then the nose wheel. The tracks veered sharply off the right side of the runway, and terminated at the wreckage. The inspector provided a hand-drawn sketch of the marks with approximate distances.

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.

Hard landingLanding - flare/touchdown
Flare - misjudgedPilot in commandCause
Gear collapsedLanding - roll
Landing gear,main gear attachment - overloadFactor
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - rough/uneven

Aircraft

Registration
N502CK
Reported as
Beech D18S
Category
Airplane
Serial number
A366
Airframe hours
17,654
Engine
Airesearch TPE331-1-101B, 625 horsepower, turbo prop
Damage
Substantial damage
Flight
Part 135
Operator
Air Supply Alaska
Registered owner
Aero Equipment LLC
Airworthiness certificate
Standard, Normal
Departed
PAEN · Kenai, AK
Destination
9Z8 · Levelock, AK
Flight plan
Company VFR
Airport
9Z8 · Levelock, runway 01, 3,281 × 59 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

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
55
Injuries
None
Certificates
Airline transport, Flight instructor
Airplane ratings
Multi-engine land, Single-engine sea, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Last flight review
January 1, 2007
Seat
Left
Flight hours
13,013 total · 685 in this make and model · 12,230 as pilot in command · 236 in the last 90 days · 52 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
350° at 10 knots
Visibility
50 statute miles
Lowest ceiling
None
Temperature
45 °F

FAA reports on this event · 1

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