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MY FS FLIGHTS
Flight Score
Improve the takeoff
The rudder input is a changing profile through the roll rather than one that is held. So the demand on your right foot starts large at power application, eases as speed builds and the rudder gains authority, then jumps again at rotation.
Read more in Improve Your Take-OffsStart to finish · 18 stages, 16 scored
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Two stabilised approach gates, each with six checks at 1,000 ft and 500 ft above the runway.
Side view — the last 2,351 m of the approach.
Plan view — the first 2,351 m of the 3,054 m runway, to the same scale as the side view.
Touched down 886 m past the threshold — beyond the full-score zone. The arrival was smooth.
The rest of the report
The Avro Vulcan B2 aircraft took off from runway 02 at EGXW RAF Waddington, covering a distance of 806 meters, which was 30% of the runway length. The takeoff roll was completed in a relatively short time, and the aircraft lifted off at a speed of 159 knots. The local weather conditions at the time of departure were characterized by a temperature of 18 degrees Celsius, with a wind speed of 12 knots at an angle of 40 degrees. This resulted in a crosswind of 4 knots and a headwind of 11 knots.
As the aircraft climbed away from RAF Waddington, it began its enroute climb, which started overhead the airbase. The climb took the aircraft from an altitude of 1,269 feet above sea level to 44,406 feet above sea level, an increase of 43,137 feet in just 16 minutes. This climb phase covered a distance of 66 nautical miles. The enroute level cruise phase followed, during which the aircraft flew at a steady altitude for a prolonged period of 930 minutes, covering a distance of 3,556 nautical miles.
The enroute descent phase began when the aircraft started its descent from an altitude of 46,083 feet above sea level to 1,781 feet above sea level, a decrease of 44,302 feet in just 16 minutes. This descent phase covered a distance of 115 nautical miles. The final approach to runway 13 at FHAW RAF Ascension Island was made from the west, with the aircraft heading 116.0 degrees at an altitude of 1,525 feet above ground level and a distance of 4 nautical miles from the runway threshold.
The landing on runway 13 at FHAW RAF Ascension Island was completed successfully, with the aircraft touching down at a speed of 135 knots. The touchdown point was 470 meters beyond the touchdown zone, and the touchdown rate was fair at -225 feet per minute. The runway touchdown position was slightly misaligned from the centerline by 3.7 meters. The local weather conditions at the time of landing were characterized by a temperature of 26 degrees Celsius, with a wind speed of 17 knots at an angle of 141 degrees. This resulted in a crosswind of 7 knots and a headwind of 16 knots.
The total landing distance was 2,271 meters, which was 74% of the runway length. The runway rollout alignment was very good, indicating a smooth and controlled landing. The taxiing to the parking from the runway took just 1 minute, covering a distance of less than 1 nautical mile. The total flight distance was 3,746 nautical miles, and the flight duration was 451 minutes. Notably, the aircraft used zero kilograms of fuel during the flight.
The Avro Vulcan B2 aircraft successfully landed at FHAW RAF Ascension Island, achieving a score of 91.4%. The final approach to runway 13 was initiated from the west, heading 116.0° at a distance of 4 nautical miles and an altitude of 1,525 feet above ground level.
Upon landing, the aircraft touched down on the runway, with the threshold speed being slightly above the target at 152 knots. The touchdown point was located 470 meters beyond the designated touchdown zone, which may indicate a slight deviation from the intended landing spot. However, the touchdown speed of 135 knots was considered good, indicating a controlled descent.
The aircraft's touchdown rate of -225 feet per minute was fair, suggesting that the pilot may have been able to improve the rate of descent to achieve a smoother landing. Additionally, the runway touchdown position was slightly misaligned by 3.7 meters from the centerline, which may have been due to factors such as wind or pilot error.
The local weather conditions at the time of landing were characterized by a temperature of 26°C and a wind speed of 17 knots from 141°. The crosswind component was 7 knots, while the headwind component was 16 knots, which may have affected the aircraft's approach and landing.
The total landing distance of 2,271 meters was 74% of the runway length, indicating that the aircraft was able to stop within a reasonable distance. The runway rollout alignment was very good, suggesting that the pilot was able to maintain control of the aircraft during the rollout phase.
Overall, the landing was considered successful, with the aircraft achieving a good touchdown speed and a controlled rollout. However, there were some minor deviations from the intended landing spot and a slightly high touchdown rate, which may indicate areas for improvement in the pilot's technique.
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