Bournemouth - Bournemouth

After the second overshoot, the aircraft entered the circuit, and was cleared for a touch-and-go landing on Runway 17. The final approach was described as 'steep' and was flown with full (45°) flap. After a short ground run, the pilot under training opened the throttles, and. at about 80 knots, rotated the aircraft with the flaps still at the full (45 degree) setting. Shortly after becoming airborne, there was a loss of power, accompanied by vibration or buffeting; the aircraft yawed and rolled to the right, and the airspeed started to decay. The pilot under training then retracted the flaps to 30°, and, at this point, the instructor took control, closed the throttles, and landed the aircraft on the grass on a heading of about 200° magnetic. The aircraft than ran across the south western taxiway, through the airfield perimeter fence, across a public road, at which point the undercarriage collapsed, before finally coming to rest in an adjacent field. Both fuel tanks were ruptured by the impact with the fence posts, but there was no fire. The crew, who were uninjured, shut off the fuel cocks, switched off the electrics, and vacated the aircraft through the main entry door. The emergency services responded to this incident very quickly, and had arrived at the crash scene by the time the crew vacated the aircraft.

Flight / Schedule

Bournemouth - Bournemouth

Registration

G-OFRL

MSN

414A-0220

Year of Manufacture

1979

Date

May 15, 1984 at 02:27 PM

Type

CRASH

Flight Type

Training

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Crash Location

Bournemouth-Hurn Dorset

Region

Europe • United Kingdom

Crash Cause

Human factor

Narrative Report

On May 15, 1984 at 02:27 PM, Bournemouth - Bournemouth experienced a crash involving Cessna 414 Chancellor, operated by Flight Refuelling, with the event recorded near Bournemouth-Hurn Dorset.

The flight was categorized as training and the reported phase was takeoff (climb) at a airport (less than 10 km from airport) crash site.

3 people were known to be on board, 0 fatalities were recorded, 3 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: 1, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is human factor. After the second overshoot, the aircraft entered the circuit, and was cleared for a touch-and-go landing on Runway 17. The final approach was described as 'steep' and was flown with full (45°) flap. After a short ground run, the pilot under training opened the throttles, and. at about 80 knots, rotated the aircraft with the flaps still at the full (45 degree) setting. Shortly after becoming airborne, there was a loss of power, accompanied by vibration or buffeting; the aircraft yawed and rolled to the right, and the airspeed started to decay. The pilot under training then retracted the flaps to 30°, and, at this point, the instructor took control, closed the throttles, and landed the aircraft on the grass on a heading of about 200° magnetic. The aircraft than ran across the south western taxiway, through the airfield perimeter fence, across a public road, at which point the undercarriage collapsed, before finally coming to rest in an adjacent field. Both fuel tanks were ruptured by the impact with the fence posts, but there was no fire. The crew, who were uninjured, shut off the fuel cocks, switched off the electrics, and vacated the aircraft through the main entry door. The emergency services responded to this incident very quickly, and had arrived at the crash scene by the time the crew vacated the aircraft.

Aircraft reference details include registration G-OFRL, MSN 414A-0220, year of manufacture 1979.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

After the second overshoot, the aircraft entered the circuit, and was cleared for a touch-and-go landing on Runway 17. The final approach was described as 'steep' and was flown with full (45°) flap. After a short ground run, the pilot under training opened the throttles, and. at about 80 knots, rotated the aircraft with the flaps still at the full (45 degree) setting. Shortly after becoming airborne, there was a loss of power, accompanied by vibration or buffeting; the aircraft yawed and rolled to the right, and the airspeed started to decay. The pilot under training then retracted the flaps to 30°, and, at this point, the instructor took control, closed the throttles, and landed the aircraft on the grass on a heading of about 200° magnetic. The aircraft than ran across the south western taxiway, through the airfield perimeter fence, across a public road, at which point the undercarriage collapsed, before finally coming to rest in an adjacent field. Both fuel tanks were ruptured by the impact with the fence posts, but there was no fire. The crew, who were uninjured, shut off the fuel cocks, switched off the electrics, and vacated the aircraft through the main entry door. The emergency services responded to this incident very quickly, and had arrived at the crash scene by the time the crew vacated the aircraft.

Cause: Human factor

Occupants & Outcome

Crew On Board

2

Passengers On Board

1

Estimated Survivors

3

Fatality Rate

0.0%

Known people on board: 3

Operational Details

Schedule / Flight

Bournemouth - Bournemouth

Flight Type

Training

Flight Phase

Takeoff (climb)

Crash Site

Airport (less than 10 km from airport)

Region / Country

Europe • United Kingdom

Aircraft Details

Registration

G-OFRL

MSN

414A-0220

Year of Manufacture

1979