Salina - Phoenix

Upon landing at the completion of a cross country flight, the captain of the turbojet aircraft employed aerodynamic braking and thrust reverse to slow the airplane to about 60 knots. The captain was allowing the airplane to roll toward the end of the runway where the owner/copilot's hanger was located. With about 4,000 feet of runway remaining, the captain applied the brakes. No braking action was noted. The airplane continued off the end of the runway, through a fence and block wall into a parking lot where the left wing of the airplane was severed. A post crash fire consumed about half of the airplane. Emergency braking procedures were not employed. The crew reported that the were unable to shut down the engines. The copilot lacked experience in the aircraft and crew coordination during the approach, landing, and emergency was ineffective. The airplane traveled about 11,000 feet from point of touchdown to point of rest. Examination of the braking and hydraulic systems failed to pinpoint a malfunction.

Flight / Schedule

Salina - Phoenix

Registration

N169RF

MSN

306-45

Year of Manufacture

1969

Date

November 7, 1992 at 10:26 PM

Type

CRASH

Flight Type

Private

Flight Phase

Landing (descent or approach)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Phoenix-Sky Harbor Arizona

Region

North America • United States of America

Coordinates

33.4661°, -111.9949°

Crash Cause

Human factor

Narrative Report

On November 7, 1992 at 10:26 PM, Salina - Phoenix experienced a crash involving Rockwell Sabreliner 60, operated by Halford R. Price, with the event recorded near Phoenix-Sky Harbor Arizona.

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.

8 people were known to be on board, 0 fatalities were recorded, 8 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.

Crew on board: 2, crew fatalities: 0, passengers on board: 6, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is human factor. Upon landing at the completion of a cross country flight, the captain of the turbojet aircraft employed aerodynamic braking and thrust reverse to slow the airplane to about 60 knots. The captain was allowing the airplane to roll toward the end of the runway where the owner/copilot's hanger was located. With about 4,000 feet of runway remaining, the captain applied the brakes. No braking action was noted. The airplane continued off the end of the runway, through a fence and block wall into a parking lot where the left wing of the airplane was severed. A post crash fire consumed about half of the airplane. Emergency braking procedures were not employed. The crew reported that the were unable to shut down the engines. The copilot lacked experience in the aircraft and crew coordination during the approach, landing, and emergency was ineffective. The airplane traveled about 11,000 feet from point of touchdown to point of rest. Examination of the braking and hydraulic systems failed to pinpoint a malfunction.

Aircraft reference details include registration N169RF, MSN 306-45, year of manufacture 1969.

Geospatial coordinates for this crash are approximately 33.4661°, -111.9949°.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

Upon landing at the completion of a cross country flight, the captain of the turbojet aircraft employed aerodynamic braking and thrust reverse to slow the airplane to about 60 knots. The captain was allowing the airplane to roll toward the end of the runway where the owner/copilot's hanger was located. With about 4,000 feet of runway remaining, the captain applied the brakes. No braking action was noted. The airplane continued off the end of the runway, through a fence and block wall into a parking lot where the left wing of the airplane was severed. A post crash fire consumed about half of the airplane. Emergency braking procedures were not employed. The crew reported that the were unable to shut down the engines. The copilot lacked experience in the aircraft and crew coordination during the approach, landing, and emergency was ineffective. The airplane traveled about 11,000 feet from point of touchdown to point of rest. Examination of the braking and hydraulic systems failed to pinpoint a malfunction.

Cause: Human factor

Occupants & Outcome

Crew On Board

2

Passengers On Board

6

Estimated Survivors

8

Fatality Rate

0.0%

Known people on board: 8

Operational Details

Schedule / Flight

Salina - Phoenix

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

N169RF

MSN

306-45

Year of Manufacture

1969