N4974U

Substantial
None

Cessna 210ES/N: 21058674

Accident Details

Date
Monday, February 16, 2004
NTSB Number
IAD04LA011
Location
Pittsburgh, PA
Event ID
20040224X00227
Coordinates
40.354167, -79.930000
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The owner/pilot-mechanic's failure to comply with an airworthiness directive, which resulted in a fatigue fracture to the left main landing gear saddle.

Aircraft Information

Registration
N4974U
Make
CESSNA
Serial Number
21058674
Engine Type
Reciprocating
Model / ICAO
210EC210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
YUHASCHEK JOSEPH
Address
11900 PENNSIDE RD
Status
Deregistered
City
ALBION
State / Zip Code
PA 16401-8520
Country
United States

Analysis

On February 16, 2004, at 1426 eastern standard time, a Cessna 210E, N4974U, was substantially damaged while landing at Allegheny County Airport (AGC), Pittsburgh, Pennsylvania. The certificated commercial pilot and the passenger were not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight, conducted under 14 CFR Part 91.

According to the pilot, who was also the airplane's owner and mechanic, the left main landing gear would not extend into a down and locked position. The pilot decided to land with the right main and nose landing gear in the down and locked position, and the left main landing gear "hanging." Upon touchdown, the left main landing gear collapsed, and the airplane slid off the left side of the runway.

According to a Federal Aviation Administration (FAA) inspector, a post-accident examination of the airplane revealed that the left main landing gear saddle was fractured.

The landing gear saddle was the subject of an Airworthiness Directive (AD), AD 76-14-07 R2. The AD required replacement of the landing gear saddle, and after 1,200 hours of service on the new part, annual dye penetrant inspections. The FAA inspector's review of the airframe logbook revealed that the part was replaced in 1976, and was due for its first dye penetrant inspection in 1986. There were no records in the logbook to indicate that an annual inspection of the part had ever been performed.

The landing gear saddle was submitted to the Safety Board Materials Laboratory for examination. According to the engineer's factual report, the saddle fracture surfaces exhibited features consistent with fatigue. There was also no visual evidence of any dye penetrant on the part.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# IAD04LA011