N5870M

Substantial
None

CESSNA 340S/N: 3400058

Accident Details

Date
Saturday, September 9, 2017
NTSB Number
CEN17LA351
Location
McKinney, TX
Event ID
20170914X44755
Coordinates
33.176387, -96.589164
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the bell crank pivot bolt which resulted in the left main landing gear collapse. Contributing to the accident was the lack of landing gear inspections in accordance with the airplane manufacturer's maintenance manuals.

Aircraft Information

Registration
Make
CESSNA
Serial Number
3400058
Engine Type
Reciprocating
Year Built
1972
Model / ICAO
340C340
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
6
FAA Model
340

Registered Owner (Current)

Name
MCDONALD BRIAN L
Address
PO BOX 1896
City
VAN ALSTYNE
State / Zip Code
TX 75495-1896
Country
United States

Analysis

On September 9, 2017, about 1500 central daylight time, a twin-engine Cessna 340 airplane, N5870M, experienced a gear collapse after landing at the McKinney National Airport (KTKI), McKinney, Texas. The commercial rated pilot and passenger were not injured, and the airplane was substantially damaged. The airplane was registered to and operated by Holubar Properties, Inc., McKinney, Texas, under the provisions of 14 Code of Federal Regulations Part 91 as a cross-country flight. Visual meteorological conditions prevailed at the time.

A Federal Aviation Administration (FAA) inspector reported that the airplane landed on runway 36, and during the rollout, the left main landing gear collapsed. An examination of the airplane noted revealed substantial damage to the airplane's aileron, and the left gear down-lock and bell crank pivot bolt were broken.

A review of the Cessna 340 maintenance manual revealed that the landing gear system is to be disassembled/inspected after 20 years (or 10,000 landings) and every 10 years/5,000 landings after the initial inspection. Additionally, the maintenance manual indicates that the main landing gear bell crank pivot bolt to be inspected for wear, every 3 years (or 500 landings) after an initial inspection at 3 years or 1,000 landings.

A review of the airplane maintenance records did not reveal an entry were the landing gear inspections had been accomplished. The records revealed the airframe had accumulated 5,799.3 hours at the time of the last annual inspection, that was dated September 1, 2016.

The pilot did not return a completed Pilot/Operator Aircraft Accident form (NTSB 6120.1).

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN17LA351