N414HF

Substantial
None

CESSNA 414S/N: 414-0389

Accident Details

Date
Saturday, June 18, 2022
NTSB Number
ERA22LA282
Location
Jasper, GA
Event ID
20220623105310
Coordinates
34.453472, -84.457222
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the owner to comply with a service bulletin, which resulted in the failure of the left main landing gear torque tube due to fatigue cracking.

Aircraft Information

Registration
Make
CESSNA
Serial Number
414-0389
Engine Type
Reciprocating
Model / ICAO
414C414
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
7
FAA Model
414

Registered Owner (Current)

Name
N414HF LLC
Address
PO BOX 756
City
JASPER
State / Zip Code
GA 30143-0756
Country
United States

Analysis

On June 18, 2022, about 1730 eastern daylight time, a Cessna 414, N414HF, was substantially damaged when it was involved in an accident near Jasper, Georgia. The commercial pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight.

The pilot reported that after touchdown on runway 34 the left main landing gear collapsed. The airplane skidded to the left, departed the runway surface, and struck a taxiway sign. The pilot also reported that he had “3 green” indications before touchdown, and the landing was “smooth and straight.”

An inspector with the Federal Aviation Administration (FAA) responded to the accident site and examined the wreckage. The inspector reported that the left wing sustained substantial damage to the lower structure. The landing gear was collapsed, and the left main landing gear torque tube was fractured.

After recovery of the wreckage to the ramp, maintenance personal removed the fractured torque tube, and it was forwarded to the National Transportation Safety Board Materials Laboratory for further examination. The examination revealed the presence of multiple fatigue cracks near the weld between the boss arm and the tube body. The opposite-facing fatigue cracks propagated inward from the outer and inner surfaces, consistent with reverse bending at this location. The cracks initiated from multiple crack initiation sites.

Cessna Multi-engine Service Bulletin (SB) MEB09-2, dated May 11, 2009, addressed the issue of main landing gear torque tube failure. The service bulletin stated that noncompliance could result in fatigue failure of the torque tube. The SB required replacement of the tube at 4,000 hours of time in service. According to the owner, the airplane total time was 5,000 hours, and the torque tube was original to the airplane. The service bulletin was not included in an FAA Airworthiness Directive.

An FAA fact sheet titled “Service Bulletins and the Aircraft Owner,” stated in part:

“Are Service Bulletins Mandatory?

The short answer is – it depends. If you are operating your aircraft under 14 CFR part 91, a service bulletin is advisory, and compliance is not mandatory unless it is included in an Airworthiness Directive. Keep in mind that even when a service bulletin is not mandatory, you should always pay attention to it as a means to ensure your safety….”

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA22LA282