N6898Y

Substantial
Serious

Piper PA-60-602P S/N: 60-8265010

Accident Details

Date
Tuesday, July 7, 1998
NTSB Number
FTW98LA303
Location
BEAUMONT, TX
Event ID
20001211X10574
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
2
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The pilot's failure to maintain control of the airplane while attempting to return to the airport. Factors were the open baggage compartment door and the pilot's diverted attention to the open door.

Aircraft Information

Registration
N6898Y
Make
PIPER
Serial Number
60-8265010
Engine Type
Reciprocating
Year Built
1982
Model / ICAO
PA-60-602P AEST
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
W H WATKINS COMPANY
Address
HWY 6 WEST
Status
Deregistered
City
BATESVILLE
State / Zip Code
MS 38606
Country
United States

Analysis

On July 7, 1998, at 0635 central daylight time, a Piper PA-60-602P twin engine airplane, N6898Y, was substantially damaged when it impacted trees and terrain while attempting to return to land at the Jefferson County Airport, near Beaumont, Texas. The non-instrument rated private pilot/owner and his passenger were seriously injured. The airplane was registered to the W.H. Watkins Company, of Batesville, Mississippi. Visual meteorological conditions prevailed for the Title 14 CFR Part 91 personal flight for which an IFR flight plan was filed. The flight, which was destined for the Panola County Airport, near Batesville, Mississippi, was originating at the time of the accident.

According to personnel at the airport, an IFR flight plan was filed and a clearance was received for the 337 nautical mile flight. After departure from runway 12, approximately 200 feet above the ground, the pilot reported that a door had opened in flight and he was returning to the airport. The airplane impacted trees and terrain approximately one mile from the approach end of runway 30.

Examination of the wreckage by FAA inspectors who responded to the accident site revealed that the door for the unpressurized baggage compartment, which is located on the left side of fuselage, aft of the fuel cell, had damage consistent with an open door. The FAA inspector stated that physical evidence and ground signatures at the accident site revealed that the airplane impacted the ground at a high rate of descent, at relatively low forward speed. At the time of impact, the airplane was configured with the landing gear and flaps extended.

According to FAA records, the private pilot obtained his private pilot certificate on December 2, 1994. Additionally, the pilot had accumulated a total of 1,850 flight hours at the time of his last FAA medical examination on January 24, 1997. The pilot's level of experience in the accident airplane could not be determined; however, the investigation revealed that the 1982 model airplane was purchased by the company 4 months prior to the accident.

Despite several attempts to obtain a completed NTSB Form 6120.1/2, the pilot did not return the requested form.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW98LA303