N218LG

MINR
None

CESSNA 402BS/N: 402B0218

Accident Details

Date
Monday, September 10, 2012
NTSB Number
ERA12IA559
Location
Opa-Locka, FL
Event ID
20120911X40823
Coordinates
25.907499, -80.278053
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The pilot’s turning the airplane too sharply while exiting the runway, which resulted in the failure of the right main landing gear bellcrank due to an overstress fracture.

Aircraft Information

Registration
N218LG
Make
CESSNA
Serial Number
402B0218
Engine Type
Reciprocating
Year Built
1972
Model / ICAO
402BC402
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
WAYMAN AVIATION SERVICES INC
Address
14351 NW 41ST AVE
Status
Deregistered
City
OPA LOCKA
State / Zip Code
FL 33054-2328
Country
United States

Analysis

On September 10, 2012, about 1650 eastern daylight time, a Cessna 402B, N218LG, landed at Opa-Locka Executive Airport (OPF), Miami, Florida, and after clearing the runway, the right main landing gear collapsed. The airline transport-rated pilot and two passengers were not injured. The airplane sustained minor damage. The airplane was registered to and operated by Waymen Aviation Services Inc. under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed and no flight plan was filed. The flight originated from OPF at 1600.

The pilot stated that, while turning left off of the active runway after landing, the airplane "began veering to the left," and the right main landing gear subsequently collapsed. The right main landing gear was examined by a Federal Aviation Administration inspector, and he confirmed the damage to the right main landing gear assembly.

The landing gear bellcrank was sent to the NTSB materials laboratory for examination. The bellcrank consisted of a long arm, approximately 7.5 inches long, and a short arm, approximately 2.1 inches long, with a 105-degree included angle between the two. The end of each arm was shaped in the form of a clevis. One of the clevis knuckles on the long bellcrank arm was fractured. The fracture surface had a rough appearance and was at an angle to the longitudinal axis of the clevis arm, consistent with an overstress fracture. No other anomalies were noted with the landing gear.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA12IA559