N661R

Substantial
None

CESSNA 310B S/N: 35033

Accident Details

Date
Monday, August 21, 1995
NTSB Number
NYC95LA201
Location
MONTICELLO, NY
Event ID
20001207X04360
Coordinates
41.649028, -74.679672
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

fatigue failure of the right main landing gear during the landing, which resulted in a gear collapse, loss of directional control, and subsequent collision with an embankment.

Aircraft Information

Registration
N661R
Make
CESSNA
Serial Number
35033
Engine Type
Reciprocating
Model / ICAO
310B C310
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
CRAMER ALLAN E
Address
26 OLD MOUNTAIN RD
Status
Deregistered
City
PORT JERUIS
State / Zip Code
NY 12771
Country
United States

Analysis

On August 21, 1995, about 1550 eastern daylight time, a Cessna 310B, airplane, N661R, was substantially damaged when it collided with terrain during the landing, at the Monticello Airport, Monticello, New York. The private pilot and passenger were not injured. Visual meteorological conditions prevailed for the personal flight that departed from Sussex, New Jersey. There was no flight plan for the flight conducted under 14 CFR Part 91.

In the NTSB form 6120.1/2, the pilot stated:

". . .At touchdown on runway 01, the right wheel fell off. . . .Upon leaving blacktop, airplane spun around and stopped beside runway. . . .Upon examination of wheel and strut, a weld broke causing wheel to fall off. . . ."

The pilot reported that the airplane came to rest in a large embankment.

Additionally, the right main landing gear assembly was examined by the National Transportation Safety Board Metallurgist Lab, Washington, District of Columbia. The metallurgist's factual report stated: "Examination of the fracture faces on the received pieces revealed features typical of fatigue cracking adjacent to the inner surface of the weld. The fatigue cracking initiated from multiple origins located at the inboard and outboard sides of the strut assembly. . . .Subsequent examination of the fracture faces revealed no evidence of corrosion pitting either at the fatigue crack origins or in any other areas of the fracture."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC95LA201