N7648Q

Substantial
None

Cessna 310QS/N: 31000427

Accident Details

Date
Tuesday, May 9, 2000
NTSB Number
LAX00LA188
Location
MESA, AZ
Event ID
20001212X21036
Coordinates
33.460834, -111.728332
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the overload fracture and separation of the right main landing gear attachment.

Aircraft Information

Registration
N7648Q
Make
CESSNA
Serial Number
31000427
Engine Type
Reciprocating
Year Built
1971
Model / ICAO
310QC310
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
QUALITY AIRCRAFT SALES LLC
Address
2650 AIRPORT RD
Status
Deregistered
City
CENTERVILLE
State / Zip Code
TN 37033-5921
Country
United States

Analysis

On May 9, 2000, about 0935 mountain standard time, a Cessna 310Q, N7648Q, experienced a right main landing gear collapse during landing roll at Falcon Field Airport, Mesa, Arizona. Perez Electric, Inc., was operating the airplane under the provisions of 14 CFR Part 91. The private pilot, the sole occupant, was not injured; the airplane sustained substantial damage. The personal cross-country flight departed from Brackett Field, La Verne, California, about 0740 with a planned destination of Falcon Field. Visual meteorological conditions prevailed, and a flight plan had not been filed.

In a written statement, the pilot reported that he performed a normal approach and landing on runway 22L. During the landing rollout, he eased back pressure on the control yoke and retracted the wing flaps. Upon application of brake pressure, the right main landing gear collapsed. The right wing dropped, resulting in the airplane veering to the right. The airplane continued to the right, off the runway, and came to rest in a dirt field. The airplane incurred damage to the right wing and horizontal stabilizer.

The Safety Board's Materials Laboratory examined the right main landing gear attachment. The materials specialist stated that the threaded rod/bolt fractured in overstress. The part had a classical "cup-cone" shape with shear lips at the edges and adjacent threads were also cracked. The nut side was deformed and flattened as was the mating corner of the opposite piece.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX00LA188