N1837M

Substantial
None

CURTISS WRIGHT C-46FS/N: 22388

Accident Details

Date
Wednesday, July 3, 2013
NTSB Number
ANC13LA063
Location
Fairbanks, AK
Event ID
20130711X55743
Coordinates
64.808891, -147.853881
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 right main landing gear side brace due to fatigue, which resulted in a collapse of the right main landing gear.

Aircraft Information

Registration
Make
CURTISS WRIGHT
Serial Number
22388
Engine Type
Reciprocating
Year Built
1944
Model / ICAO
C-46FC46
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
65
FAA Model
C-46F

Registered Owner (Current)

Name
EVERTS AIR FUEL INC
Address
PO BOX 60908
City
FAIRBANKS
State / Zip Code
AK 99706-0908
Country
United States

Analysis

On July 2, 2013, about 1600 Alaska daylight time, a twin-engine Curtiss Wright, C-46F airplane, N1837M, sustained substantial damage while taxiing to parking at the Fairbanks International Airport, Fairbanks, Alaska. The commercial certificated captain and the airline transport certificated first officer were not injured. The airplane was registered to and operated by Evert's Air Fuel, under the provisions of Title 14 Code of Federal regulations Part 91, as a visual flight rules (VFR) maintenance test flight. Visual meteorological conditions prevailed, and no flight plan had been filed.

The operator reported that during the maintenance test flight, the flight crew moved the landing gear handle to the "down" position, but did not observe the three green landing gear down-and-lock lights illuminate. After cycling the landing gear "several" times they observed a gear down-and-locked indication in the cockpit. After landing, while taxiing to parking, the right main landing gear collapsed, and the right wing and aileron sustained substantial damage.

A postaccident examination, of the landing gear system revealed that both inner and outer tubes of the right landing gear side brace, separated near the fuselage attach forging. The fractured main landing gear side brace assembly was sent to the NTSB's Materials Laboratory in Washington, D.C. for examination.

A senior Safety Board metallurgist reported that a magnified optical examination of the landing gear side brace assembly fracture surfaces revealed ratchet marks, arrest lines, and flat fracture regions consistent with fatigue propagation. No obvious discontinuities such as porosity or undercutting were visually noted in the weld adjacent to the fracture. A complete copy of the NTSB's materials laboratory factual report is included in the public docket for this accident.

In the recommendation section of the NTSB Accident/Incident Reporting Form 6120.1, the operator stated that the accident may have been prevented if the flight crew would have shut down the airplane clear of the runway, and had the landing gear inspected before taxiing to parking. They also noted, that three green down-and-lock lights illuminated is the normal indication for a positive lock.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC13LA063