No fatalities

Performance Loss After Takeoff Leads to Forced Landing; Occupants Uninjured (VH-AOX)

Port Macquarie, AustraliaTakeoff (climb)

On April 13, 1985, a Piper PA-31-350 Navajo Chieftain (registration VH-AOX) operated by Oxley Airlines was involved in an aviation accident near Port Macquarie, Australia during takeoff. No fatalities were reported. Investigators recorded the probable cause as: No fault was subsequently found with the engines or systems of the aircraft which might have explained the reported loss of performance. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Source recordUpdated 2026-07-04Data APIEditorial standards

A pilot reported a propeller pitch noise change and performance loss after takeoff. Despite raising gear and flaps, the aircraft failed to climb. A forced landing was executed off the runway; all nine occupants escaped uninjured.

Event Description

Shortly after becoming airborne, the pilot noticed a substantial change in propeller pitch noise accompanied by a loss of performance. Insufficient runway remained for a straight-ahead landing. The pilot raised the landing gear and flaps, but the aircraft did not climb and airspeed decayed below the safe single-engine speed. The takeoff attempt was abandoned, and a forced landing was conducted off the end of the runway.

Accident Details

The rear fuselage impacted heavily on a dirt bank 78 meters beyond the runway threshold. The aircraft then passed through a fence and slid for an additional 78 meters before coming to rest. All nine occupants exited the aircraft uninjured.

Official Findings

No fault was found with the engines or systems that could explain the reported loss of performance. Calculations indicated the aircraft's takeoff weight was close to the maximum allowable, and its center of gravity was aft of the rear limit. Several passengers noted that the aircraft rotated sharply to an unusually high nose attitude as it became airborne. The pilot's decision to raise the flaps upon perceiving the power loss was contrary to the emergency procedures for the aircraft type, which likely resulted in a sink and further reduction in airspeed.

Probable cause

No fault was subsequently found with the engines or systems of the aircraft which might have explained the reported loss of performance. Calculations indicated that the weight of the aircraft at the time of take-off was close to the maximum allowable, but the centre of gravity was aft of the rear limit. Several of the passengers indicated that the aircraft rotated sharply to an unusually high nose attitude as it became airborne. The pilot's action in raising the flap when he perceived the power loss was contrary to the emergency procedures for the type, and probably resulted in sink and a further reduction in airspeed.

Frequently asked questions

What happened in the 13 Apr 1985 Piper PA-31-350 Navajo Chieftain accident near Port Macquarie, Australia?

A pilot reported a propeller pitch noise change and performance loss after takeoff. Despite raising gear and flaps, the aircraft failed to climb. A forced landing was executed off the runway; all nine occupants escaped uninjured.

Were there any fatalities in the 13 Apr 1985 Piper PA-31-350 Navajo Chieftain accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 13 Apr 1985 involved a Piper PA-31-350 Navajo Chieftain, registration VH-AOX, operated by Oxley Airlines, at Port Macquarie, Australia.

What was the probable cause of the accident?

No fault was subsequently found with the engines or systems of the aircraft which might have explained the reported loss of performance. Calculations indicated that the weight of the aircraft at the time of take-off was close to the maximum allowable, but the centre of gravity was aft of the rear limit. Several of…