The Hawker H25B taxied to runway 23 at EGPE Inverness Airport and commenced the take-off roll, covering 849 m which represented 46 % of the available runway. Liftoff was achieved at 141 kt. Ambient conditions were 17 °C with a wind of 2 kt from 269°, giving a 2 kt head-wind component and a 1 kt cross-wind component.

A left-hand pattern entry was flown for 2 nm, completed in 36 seconds, before turning onto the left-hand crosswind leg for a further 1 nm in 23 seconds.

The aircraft then executed a downwind turn covering 4 nm with a measured angle to the runway of 47.3°, and proceeded on the downwind leg for 5 nm in 107 seconds.

A base-leg turn followed, spanning 4 nm and recorded at an angle of 45.7° to the runway, after which the base leg itself was flown for 2 nm in 59 seconds.

A final turn of less than 1 nm was completed in 29 seconds, positioning the aircraft for the final approach.

During the descent phase the aircraft reduced altitude from 876 ft AGL to 57 ft AGL over a period of 72 seconds.

The final approach to runway 23 was flown with the aircraft meeting the stabilisation gates, preparing for touchdown.

Touchdown occurred on runway 23, whose total length is 1,866 m. The threshold speed was recorded at 110 kt, and the aircraft touched down after 305 m of rollout at 99 kt with a vertical speed of minus 289 fpm. Alignment on touchdown was perfect, and the local weather remained 16 °C with a wind of 2 kt from 269°, providing a 2 kt head-wind and 1 kt cross-wind.

Runway rollout distance measured 774 m, representing 42 % of the runway, and alignment during rollout was described as very good.

In total the flight covered 20 nm, required 8 (unspecified units) of time, and consumed 101 kg of fuel.