N4386G

Substantial
None

Piper PA-46-310PS/N: 46-8508037

Accident Details

Date
Sunday, July 6, 2003
NTSB Number
DEN03LA123
Location
Englewood, CO
Event ID
20030708X01040
Coordinates
39.567222, -104.849998
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 improper flare which resulted in a hard landing. Contributing factors were the out-of-calibration waste gate actuator, a blown tire, and the airport sign.

Aircraft Information

Registration
N4386G
Make
PIPER
Serial Number
46-8508037
Engine Type
Reciprocating
Year Built
1985
Model / ICAO
PA-46-310PPA46
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
JENSEN STEPHEN D
Address
7620 AUTO CLUB CIR
Status
Deregistered
City
BLOOMINGTON
State / Zip Code
MN 55438-2839
Country
United States

Analysis

On July 6, 2003, at 1052 mountain daylight time, a Piper PA-46-310P, N4386G, was substantially damaged when it ran off the side of the runway during takeoff at Centennial Airport, Englewood, Colorado. The private pilot and his two passengers were not injured. Day visual meteorological conditions prevailed, and an instrument flight plan had been filed for the cross-country flight being operated under Title 14 CFR Part 91. The flight was originating at the time of the accident.

The pilot was cleared for takeoff on runway 17L and was instructed to maintain runway heading. In his accident report, the pilot said that after lifting off, he aborted the takeoff "due to poor airplane performance" and "landed very hard." The left main tire blew out and the airplane departed the left side of the runway and struck a taxiway sign. The left wing was bent, the tire was blown out, and the landing gear door was damaged.

According to a report submitted by Straight Flight, a Centennial Airport repair facility, the engine was functionally tested and the manifold pressure was found to be "3 [inches] low at full takeoff power," and the engine was producing "approximately 95-97 [per cent] full power at the takeoff setting." An adjustment to the wastegate actuator raised the manifold pressure to the correct setting.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN03LA123