Wichita Falls – Conway

The twin-engine turbojet airplane was attempting to land on a runway with standing water when the accident occurred. Before the landing attempt, the pilot was told that the runway was wet from a recent rain shower. Witnesses reported seeing the airplane on the runway traveling at a high speed and then increase engine power to abort the landing with about 1/4 of the runway remaining. The surviving passenger reported that the runway was "soaked and shiny with water." He stated that the airplane landed hard and fishtailed during the landing roll. During the aborted landing the airplane impacted a jet-blast deflector located off the departure end of the runway. The airplane then proceeded through the airport perimeter fence and impacted a residential structure before coming to a stop. The airplane and residential structure were destroyed during a postaccident fire. An examination of the airframe and engines did not reveal any anomalies associated with a preimpact failure or malfunction. The airplane was not equipped with thrust reversers or an anti-skid braking system. Radar track data analysis indicated that when the airplane was about 1/4 mile from the end of the runway it was approximately 16 knots above its target landing reference speed (Vref) and had a descent rate of 1,150 feet per minute. The runway was 4,875 feet long. The calculated landing distance for a runway with standing water is 4,789 feet.

Flight / Schedule

Wichita Falls – Conway

Registration

N771HR

MSN

500-0206

Year of Manufacture

1974

Date

June 30, 2007 at 02:50 PM

Type

CRASH

Flight Type

Private

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Conway Arkansas

Region

North America • United States of America

Coordinates

35.0892°, -92.4398°

Crash Cause

Human factor

Narrative Report

On June 30, 2007 at 02:50 PM, Wichita Falls – Conway experienced a crash involving Cessna 500 Citation, operated by IHR Administrative Services, with the event recorded near Conway Arkansas.

The flight was categorized as private and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.

2 people were known to be on board, 2 fatalities were recorded, 0 survivors were identified or estimated. This corresponds to an estimated fatality rate of 100.0%.

Crew on board: 1, crew fatalities: 1, passengers on board: 1, passenger fatalities: 0, other fatalities: 1.

The listed crash cause is human factor. The twin-engine turbojet airplane was attempting to land on a runway with standing water when the accident occurred. Before the landing attempt, the pilot was told that the runway was wet from a recent rain shower. Witnesses reported seeing the airplane on the runway traveling at a high speed and then increase engine power to abort the landing with about 1/4 of the runway remaining. The surviving passenger reported that the runway was "soaked and shiny with water." He stated that the airplane landed hard and fishtailed during the landing roll. During the aborted landing the airplane impacted a jet-blast deflector located off the departure end of the runway. The airplane then proceeded through the airport perimeter fence and impacted a residential structure before coming to a stop. The airplane and residential structure were destroyed during a postaccident fire. An examination of the airframe and engines did not reveal any anomalies associated with a preimpact failure or malfunction. The airplane was not equipped with thrust reversers or an anti-skid braking system. Radar track data analysis indicated that when the airplane was about 1/4 mile from the end of the runway it was approximately 16 knots above its target landing reference speed (Vref) and had a descent rate of 1,150 feet per minute. The runway was 4,875 feet long. The calculated landing distance for a runway with standing water is 4,789 feet.

Aircraft reference details include registration N771HR, MSN 500-0206, year of manufacture 1974.

Geospatial coordinates for this crash are approximately 35.0892°, -92.4398°.

Fatalities

Total

2

Crew

1

Passengers

0

Other

1

Crash Summary

The twin-engine turbojet airplane was attempting to land on a runway with standing water when the accident occurred. Before the landing attempt, the pilot was told that the runway was wet from a recent rain shower. Witnesses reported seeing the airplane on the runway traveling at a high speed and then increase engine power to abort the landing with about 1/4 of the runway remaining. The surviving passenger reported that the runway was "soaked and shiny with water." He stated that the airplane landed hard and fishtailed during the landing roll. During the aborted landing the airplane impacted a jet-blast deflector located off the departure end of the runway. The airplane then proceeded through the airport perimeter fence and impacted a residential structure before coming to a stop. The airplane and residential structure were destroyed during a postaccident fire. An examination of the airframe and engines did not reveal any anomalies associated with a preimpact failure or malfunction. The airplane was not equipped with thrust reversers or an anti-skid braking system. Radar track data analysis indicated that when the airplane was about 1/4 mile from the end of the runway it was approximately 16 knots above its target landing reference speed (Vref) and had a descent rate of 1,150 feet per minute. The runway was 4,875 feet long. The calculated landing distance for a runway with standing water is 4,789 feet.

Cause: Human factor

Occupants & Outcome

Crew On Board

1

Passengers On Board

1

Estimated Survivors

0

Fatality Rate

100.0%

Known people on board: 2

Operational Details

Schedule / Flight

Wichita Falls – Conway

Flight Type

Private

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Region / Country

North America • United States of America

Aircraft Details

Registration

N771HR

MSN

500-0206

Year of Manufacture

1974