N101KT

Substantial
Serious

Hughes 269A S/N: 960663

Accident Details

Date
Friday, July 31, 1998
NTSB Number
CHI98LA293
Location
SALINA, KS
Event ID
20001211X10536
Coordinates
38.809497, -97.610916
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

inadequate maintenance which failed to detect corrosion in the fuel injector system and the fuel pump. Factors related to the accident were the low altitude and airspeed at which the loss of engine power occurred.

Aircraft Information

Registration
N101KT
Make
HUGHES
Serial Number
960663
Model / ICAO
269A

Registered Owner (Historical)

Name
KANSAS STATE UNIVERSITY SALINA
Address
2409 SCANLAN AVE
Status
Deregistered
City
SALINA
State / Zip Code
KS 67401
Country
United States

Analysis

On July 31, 1998, at 1240 central daylight time (cdt), a Hughes 269A, N101KT, registered to Kansas State University Salina, of Salina, Kansas, was substantially damaged following a loss of engine power and subsequent autorotation at the Salina Municipal Airport. The airline transport rated pilot received serious injuries. The 14 CFR Part 91 flight was operating in visual meteorological conditions without a flight plan. The flight originated at the Salina Muncipal Airport shortly before the accident.

An annual inspection had just been completed on the helicopter and the pilot was performing a maintenance test flight at the time of the accident. The pilot reported that he had made several takeoffs and landings without incident. He reported that he made a departure into the wind and at an altitude of about 300 feet above the ground with an airspeed of 50 miles per hour, the engine lost power. The pilot continued to report, "Autorotation into wind was carried out. Because of low altitude and low speed and the turn to miss obstacles, was unable to perform a normal autorotational landing." The helicopter impacted the terrain and nosed over.

A post accident engine run was conducted under the supervision of inspectors from the Federal Aviation Administration Wichita, Kansas, Flight Standards District Office. The engine was power washed to remove debris from the accident. The engine driven fuel pump, injection unit, oil filter adapter, and ignition vibrator were damaged during the accident. These components were removed from the engine and replaced with like parts prior to starting the engine. The engine started and ran. Inspection of the fuel pump which was removed revealed "heavy corrosion throughout the fuel pump. ... The fuel pump was white with corrosion throughout most of the interior of the pump." The inspectors also reported the fuel injector unit had a "white corrosion powder" in most every port and opening. Water was present in several locations; however, the water could have been a result of the power washing. The fuel injector finger screen was corroded on the external side of the screen.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI98LA293