N225TA

MINR
None

Beech 58 S/N: TH-64

Accident Details

Date
Tuesday, March 14, 2000
NTSB Number
MIA00IA104
Location
MEMPHIS, TN
Event ID
20001212X20691
Coordinates
35.030788, -90.010543
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

failure of the right main landing gear's dynamic brake relay, that resulted in the motor driving the gearbox past prescribed limits, resulting in a bent connecting rod, and failure of the gear to extend.

Aircraft Information

Registration
Make
BEECH
Serial Number
TH-64
Engine Type
Reciprocating
Year Built
1970
Model / ICAO
58 BE58
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
6
FAA Model
58

Registered Owner (Current)

Name
N225TA LLC
Address
4440 BAY CREEK RD
City
LOGANVILLE
State / Zip Code
GA 30052-7390
Country
United States

Analysis

On March 14, 2000, about 1620 central standard time, a Beech 58, N225TA, registered to and operated by Flight Express Inc., as a Title 14 CFR Part 135 on demand air taxi flight, had a right main landing gear collapse during the landing rollout at Memphis International Airport, Memphis, Tennessee. Visual meteorological conditions prevailed and an instrument flight rules flight plan was filed. The aircraft received minor damage and the airline transport-rated pilot, the sole occupant, was not injured. The flight originated the same day from Fort Smith, Arkansas, about 1457.

The pilot stated that after the flare, and during the landing rollout he felt the right wing begin to sink, and the airplane started to turn to the right. The pilot further stated that he pulled back on the yoke, and applied left aileron, and noted that he had a green landing gear light. He said he was about to apply power to go around, but he saw that the propeller was damaged, and seconds later the right wing contacted the runway. The airplane then exited the north side of the runway. According to an FAA inspector, company maintenance personnel examined the right main landing gear and found that a dynamic brake relay which provides a momentary surge of reverse current to the landing gear for positive stopping, once the gear has reached either a full up, or a full down position, was found to be defective. This defective part allowed the motor to drive the gearbox past prescribed limits, inducing a bend into the right main gear connecting rod. Once gear down had been selected, the rod had a compression load, which caused it to bend even further, and not extend the 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# MIA00IA104