N2148J

Substantial
None

PIPER PA 28RT-201TS/N: 28R-7931012

Accident Details

Date
Sunday, July 27, 2014
NTSB Number
CEN14LA474
Location
Houston, TX
Event ID
20140903X23040
Coordinates
29.597778, -95.164169
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The landing gear’s failure to extend for reasons that could not be determined based on the available evidence.

Aircraft Information

Registration
N2148J
Make
PIPER
Serial Number
28R-7931012
Engine Type
Turbo-shaft
Year Built
1978
Model / ICAO
PA 28RT-201TM600
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
575 ED BEEGLES LN
Status
Deregistered
City
GREELEY
State / Zip Code
CO 80631-9021
Country
United States

Analysis

On July 27, 2014, about 1830 central daylight time, a Piper PA-28RT-201T airplane, N2148J, was substantially damaged during landing rollout at Ellington Airport (EFD), Houston, Texas. The pilot was not injured. The airplane was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed during the flight, which departed without a flight plan from La Porte Municipal Airport (T41), La Porte, Texas about 1715.

While departing from T41, the pilot noted the landing gear unsafe light (red) was illuminated after retracting the landing gear. After extending the landing gear using emergency extension procedures, the right main landing gear light (green) did not illuminate. The pilot accomplished a low approach and received a visual report of his landing gear condition from tower personnel at Scholes Airport (GLS), Galveston, Texas, who informed him the landing gear appeared to be down. The pilot proceeded from GLS to EFD for landing. During rollout at EFD, the right main landing gear collapsed, damaging the right aileron.

Following the accident, a mechanic replaced the landing gear hydraulic pump, solenoids, and springs. After these components were replaced, the landing gear operated normally during ground testing. These maintenance actions were performed without the awareness or approval of the Federal Aviation Administration inspector conducting the investigation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN14LA474