N333WD

Substantial
None

Cessna 310L S/N: 310-002

Accident Details

Date
Monday, May 25, 1998
NTSB Number
CHI98LA174
Location
WHEELING, IL
Event ID
20001211X10026
Coordinates
42.130374, -87.920265
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
5
Total Aboard
5

Probable Cause and Findings

the collapse of the left main landing gear for undetermined reasons.

Aircraft Information

Registration
Make
CESSNA
Serial Number
310-002
Engine Type
Reciprocating
Year Built
1966
Model / ICAO
310L C310
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
6
FAA Model
310L

Registered Owner (Current)

Name
WOELBING AVIATION LLC
Address
5619 NICHOLSON RD
City
FRANKSVILLE
State / Zip Code
WI 53126-9439
Country
United States

Analysis

On May 25, 1998, at 1201 central daylight time, a Cessna 310L, N333WD, was substantially damaged when the left main gear collapsed during a landing roll on runway 30R (4397' x 50', dry, asphalt) at the Palwaukee Municipal Airport, Wheeling, Illinois. The airline transport pilot, private pilot rated student, and three passengers reported no injuries. The instructional 14 CFR Part 91 flight was operating in visual meteorological conditions. A VFR flight plan was on file. The flight departed from Muskegon County Airport, Muskegon, Michigan, at 1115.

According to the instructor's written statement, the dual student had flown the instrument approach and had relinquished the controls to him for the landing on runway 30R. The instructor stated that a normal landing was made and the aircraft rolled approximately 1,500' to 2,000' when the left landing gear collapsed. The pilot stated that the aircraft slid to the left, came to rest, and everyone evacuated the aircraft.

An Air Traffic Controller at the Palwaukee Air Traffic Control tower reported that the landing appeared normal and the airplane traveled approximately 2,000' down the runway prior to the gear collapsing.

Post crash investigation showed that the bellcrank assembly was sheared at both connection points of the strut assembly for the left main gear. A Federal Aviation Administration inspector stated, in a written report, that the fracture of the bellcrank assembly was clean, with no signs of stress, corrosion or previous damage.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI98LA174