N14TG

Substantial
None

PIPER PA 31PS/N: 31P-7400190

Accident Details

Date
Saturday, October 12, 2013
NTSB Number
WPR14LA051
Location
Calexico, CA
Event ID
20131114X31956
Coordinates
32.667221, -115.517501
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The pilot’s failure to maintain the proper pitch attitude during the landing, which resulted in the nose landing gear contacting the surface hard and then separating from the airplane.

Aircraft Information

Registration
N14TG
Make
PIPER
Serial Number
31P-7400190
Engine Type
Turbo-shaft
Model / ICAO
PA 31PM600
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
TVPX AIRCRAFT SOLUTIONS INC TRUSTEE
Address
39 E EAGLE RIDGE DR STE 201
Status
Deregistered
City
NORTH SALT LAKE
State / Zip Code
UT 84054-2533
Country
United States

Analysis

On October 12, 2013, at 1500 Pacific daylight time, a Piper PA-31P, N14TG, experienced a nose gear separation during the landing roll at the Calexico International Airport, Calexico, California. The commercial pilot and two passengers were not injured. The forward fuselage was substantially damaged. The airplane was registered to and operated by Flying Bull Aviation under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed and no flight plan was filed. The flight originated from El Cajon, California, at 1425.

The pilot reported that he set-up for a straight in approach to runway 8. The approach was normal and the prelanding checklist was completed. The pilot stated that he was targeting 90 KIAS for touchdown, but the airspeed was slightly fast approaching the runway so he pulled the power back to idle and flared. The airplane was unresponsive when he pulled up the nose as the airplane settled on the main landing gear. The nosewheel abruptly sheared off upon surface contact and the airplane nosed down and slid about 1,000 feet down the runway before coming to rest.

The pilot further reported that there are known problems controlling the nose attitude in the landing configuration between 90 KIAS and the recommended landing speed around 80 KIAS. Both these speeds are above the stalling speed, but too slow to respond to pilot action regarding elevator control.

Post accident examination of the nose gear strut found that the housing was ruptured and the strut was broken. Further examination revealed no evidence of preimpact mechanical malfunction or failure that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR14LA051