N4816T

Substantial
None

Piper PA-28-200RS/N: 28R-7235114

Accident Details

Date
Wednesday, August 20, 2003
NTSB Number
SEA03LA174
Location
Nampa, ID
Event ID
20030903X01445
Coordinates
43.580276, -116.520835
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Landing gear collapse for undetermined reasons during the landing roll. On ground collision with a runway light was a factor.

Aircraft Information

Registration
Make
PIPER
Serial Number
28R-7235114
Engine Type
Reciprocating
Year Built
1972
Model / ICAO
PA-28-200RP28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28R-200

Registered Owner (Current)

Name
BULLDOG AIR LLC
Address
3511 SILVERSIDE RD STE 105
City
WILMINGTON
State / Zip Code
DE 19810-4902
Country
United States

Analysis

On August 20, 2003, approximately 1230 mountain daylight time, a Piper PA-28-200R, N4816T, registered to and being flown by a private pilot, sustained substantial damage during a gear collapse on landing roll at Nampa, Idaho. The pilot was uninjured. Visual meteorological conditions existed and no flight plan had been filed. The flight, which was personal, was operated under 14CFR91, and originated from Kemmerer, Wyoming, approximately 0950 on the morning of the accident.

The pilot reported that prior to executing an approach and landing to runway 29, he verified that he had a three green indication for the landing gear being down and locked. While rolling out on the 5,000 foot long asphalt runway and having decelerated to about 10 miles per hour, the right main landing gear began to collapse. As the aircraft departed the right side of the runway it impacted a runway light. The nose gear collapsed and the propeller struck the ground.

An airframe and powerplant mechanic removed the aircraft from the accident site to the facility of Skyline Aircraft Maintenance, Nampa, Idaho. The mechanic reported that a retraction test was accomplished to the aircraft's gear system. The aircraft's landing gear was cycled using an electric power pack and Piper's automatic free-fall system. During the retraction tests, the aircraft's landing gear down-locks and micro switches were found set within manufacturer's limits. The mechanic further stated that in his opinion, "all areas of the landing gear system were in an airworthy condition and functioning properly."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA03LA174