N31998

Substantial
None

Piper PA-32RT-300TS/N: 32R7887019

Accident Details

Date
Wednesday, April 16, 2003
NTSB Number
DEN03LA065
Location
St. George, UT
Event ID
20030428X00587
Coordinates
37.091388, -113.592224
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

the pilot's improper flare technique, resulting in a hard landing that caused the nose landing gear down-lock to fail and the gear to collapse. A contributing factor was the unfavorable wind.

Aircraft Information

Registration
Make
PIPER
Serial Number
32R7887019
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
PA-32RT-300TP32T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
7
FAA Model
PA-32RT-300T

Registered Owner (Current)

Name
LANCE GROUP LLC
Address
1248 S HIGHWAY 191
City
MOAB
State / Zip Code
UT 84532-3101
Country
United States

Analysis

On April 15, 2003, approximately 1920 mountain daylight time, a Piper PA-32RT-300T, N31998, owned and operated by the pilot, was substantially damaged during a hard landing at St. George Municipal Airport, Utah. The private pilot, two pilot certificated passengers, and a third passenger were not injured. Visual meteorological conditions prevailed, and no flight plan had been filed for the business flight being conducted under Title 14 CFR Part 91. The flight originated at Long Beach, California, approximately 1720 Pacific daylight time.

According to the pilot, he made a normal straight-in approach to runway 34 and "crossed the fence at about 80 to 90 knots." Just before touchdown, the airplane "ballooned" and touched down "a little harder than normal." The nose gear collapsed and the airplane skidded to a halt about 1,300 feet down the runway.

The nose landing gear down-lock was removed and, along with an exemplar down-lock, was sent to NTSB's materials laboratory for examination. According to its report, the down-lock "contained a fracture that intersected the hook portion." Microscopic examination revealed "a river pattern that pointed to the inner bend area of the hook, indicating that this was the origin of the fracture. The fracture face contained features typical of overstress separation, with no evidence of a preexisting (fatigue) crack. The origin area of the fracture contained no evidence of mechanical or corrosion damage. However, contact wear was noted in the throat of the hook."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN03LA065