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MY FS FLIGHTS
Flight Score
Departure
Smooth your pitch and roll inputs during the climb so the g force stays close to 0.8 g instead of spiking.
What happened: During the third climb segment the g force swung to 0.8 g, well outside the steady level flight band.
Watch for: Watch the g-meter and keep it settled near the normal one g climb band.
Arrival
Reduce power earlier on approach to be at 144 kt by the stabilisation gate, not just by the threshold.
What happened: The approach was too fast at the stabilisation gate, crossing the threshold at 110 kt against a VREF of 144 kt.
Watch for: Airspeed indicator against 144 kt at the stabilisation gate.
See Arrival Approach
Preparing for a stable approach will give you time to decide on whether to attempt the landing or going around. Too much altitude with a high sink rate will result in carrying too much speed onto the runway. Configuring flaps and the gear late also won't help the speed decay.
Read more in The Stabilised ApproachStart to finish · 9 stages, 9 in the score
Events
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From brake release to the end of the climb, against time, then the takeoff point by point.
Lifted off at 147 kt with 9.8° of pitch. Climb 3 averaged 293 kt, 32 kt over its 261 kt target.
Two traces from brake release: the airspeed on top, and below it the pitch, which is how far the nose is above the horizon. The figure at liftoff is the pitch then. The shaded stretch is Climb 3, the part of the climb scored on holding the climb speed.
The takeoff, point by point
Side view from the start of the roll to the end of Climb 3 at 884 ft.
Reached 35 ft with 1,930 m of runway left; gear up at 30 ft, inside the 400 ft that gets full marks; then climbing at 3,240 fpm on average to 884 ft.
The takeoff from the side: the height above the runway against the distance along it. The numbers along the runway are the speeds reached at each point. Lifting off in the amber last quarter of the runway costs marks for the roll length. The gear-up ring is coloured by its mark. The shaded stretch is Climb 3, scored on its average speed against the target.
Plan view the roll down the 3,056 m runway.
Rolled from 646 m in, never more than 1.2 m off the centreline, in 14 kn of crosswind from the left. Airborne 29 % of the way down the runway, before the 75 % line.
The roll from above, with your left at the top. The line is where the wheels went, and "widest" is the furthest you drifted off the centreline. Lifting off before the amber 75 % line gets full marks for the roll length. The arrow beside the runway is the crosswind, pointing the way the air was moving, so it pushed the aircraft that way.
One stabilised approach gate: seven checks where the approach path is 300 ft above the runway. The 1,000 ft gate was not assessed, because the approach did not join final that far out. These checks are the approach's score.
At the 300 ft gate: no landing flap set, sink rate more than 600 fpm beyond what the glideslope needed, centreline more than 1° off, wings more than 10° from level and speed more than 17 kt above the approach speed of 144 kt.
The approach, gate by gate
Over the threshold
Touchdown
The flare strayed well off the target profile. The aircraft was flown onto the runway - pitch changed 0.4° and the descent was barely arrested. Touchdown was 99 m past the threshold. Start the flare with progressive back pressure rather than one pull, and keep it coming.
No wind recorded: nothing to correct for. Touched down with the nose 4° right of the track, 10° of bank.
The wind is the one recorded at the landing, split along the runway (headwind or tailwind) and across it. To hold the centreline in a crosswind the nose points a little into wind - the crab - and is straightened with rudder just before the wheels touch, often with the into-wind wing lowered to stop the drift. These are the nose against the direction you were actually moving, and the wings, at the moment of touchdown. Shown for reading; not marked.
Side view — the last 1,524 m of the approach.
Crossed the threshold at 103 ft, 53 ft above the 50 ft target; began the flare late, at 5 ft. Touched down 99 m in, 206 m short of the ideal 305 m.
The last stretch of the approach and the touchdown, from the side. The height is stretched so that the last few feet show: 80 ft top to bottom, against 1,524 m across. The dashed line is the ideal, 50 ft over the threshold and down 305 m in. The flare ring is where you began raising the nose, and "descent slowed" is where the sink came off; the figures beside them are the sink rate, pitch and speed at that point.
Sink and pitch — through the flare, lined up with the side view.
The sink stayed between 3,770 fpm and 10,320 fpm from the flare to the runway. The nose came up 1.3° on the way down.
Lined up with the side view above, so a point on one sits under the same point of the other. On top, how fast you were coming down: 0 is level, and −600 is 600 ft a minute down. Below, the pitch. In a flare the nose comes up and the descent slows towards 0. The figure at the touchdown line is your touchdown rate.
Plan view — the full 1,524 m runway, to the same scale as the side view.
Touched down 7.5 m left of the centreline.
The runway from above, with your left at the top. Touching down inside the green bracket scores full marks for the distance. The shaded part is the rollout, up to where it ended.
The 99 m touchdown sits inside the full-score zone.
The rest of the report
A F-35A Lightning II departed RAAF Base Amberley, rolling down runway 15 and accelerating to liftoff speed of 148 knots in a distance of 883 meters, which accounted for 29% of the available runway. The aircraft lifted off into a local weather scenario characterized by a temperature of 30 degrees Celsius and a moderate wind of 15 knots from an 85-degree bearing. This resulted in a crosswind component of 15 knots and a headwind component of 4 knots, which presented a manageable challenge for the pilots.
As the F-35A Lightning II transitioned from the takeoff phase to the climb phase, it began to ascend into the local atmosphere. The pilots maintained control of the aircraft, navigating through the wind conditions and making adjustments as necessary to ensure a stable and efficient climb. The aircraft's advanced avionics and flight control systems played a crucial role in this phase, allowing the pilots to optimize the climb profile and minimize fuel consumption.
The F-35A Lightning II completed its short flight, covering a total distance of 1 nautical mile in approximately 2 minutes. During this time, the aircraft consumed 791 kilograms of fuel, a relatively efficient performance considering the short duration of the flight. The pilots successfully completed the flight, demonstrating the aircraft's capabilities in a variety of operating conditions.
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