N28119

Substantial
None

BELLANCA 17 31S/N: 78-31146

Accident Details

Date
Friday, March 21, 2014
NTSB Number
WPR14LA142
Location
Salt Lake City, UT
Event ID
20140321X05050
Coordinates
40.776943, -111.962219
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 right main landing gear extension spring to maintain adequate pressure, which allowed the landing gear to collapse during the landing roll. 

Aircraft Information

Registration
Make
BELLANCA
Serial Number
78-31146
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
17 31
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
17-31ATC

Registered Owner (Current)

Name
PAGE GREGORY G
Address
6094 N HIGHWAY 121
City
ROOSEVELT
State / Zip Code
UT 84066-5105
Country
United States

Analysis

On March 20, 2014 about 2045 mountain daylight time, a Bellanca 17-31ATC, N28119, sustained substantial damage after the landing gear collapsed at the Salt Lake City International Airport (SLC), Salt Lake City, Utah. The pilot, the sole occupant, was not injured; the airplane sustained substantial damage to the right wing aileron. The airplane was registered to, and operated by, the pilot under the provision of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, and no flight plan was filed. The flight originated from the Roosevelt Municipal Airport (74V), Roosevelt, Utah at about 1950.

The pilot reported that during the approach he conducted his usual pre-landing checklist, which included verifying the landing gear position and indicator lights four separate times. He conducted a normal, uneventful landing. During the landing roll the landing gear warning indication light activated and the right main landing gear green indicator light extinguished. The right wing dropped to the runway and the airplane slid before coming to a rest just off of the runway surface.

Postaccident examination of the landing gear by a mechanic and the pilot revealed that the right main landing gear extension spring appeared to be compressed; when tested, it produced 19-20 pounds of pressure. The extension springs from the nose and left landing gear assemblies were also removed and tested; they both produced about 40 pounds of pressure.

The pilot reported that he subsequently purchased and tested three new springs, all of which produced about 44 pounds of pressure. The new springs were installed on the airplane and no further landing gear anomalies were noted.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR14LA142