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IT-AUTOFLIGHT: Difference between revisions
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A set vertical speed is being tracked. | A set vertical speed is being tracked. | ||
G/S (2) | ;G/S (2) | ||
A glideslope is being tracked. | A glideslope is being tracked. | ||
SPD CLB (4) | ;SPD CLB (4) | ||
A set indicated airspeed or mach number is being held by varying pitch angle in order to climb. The autothrottle is commanded to hold the thrust limit. | A set indicated airspeed or mach number is being held by varying pitch angle in order to climb. The autothrottle is commanded to hold the thrust limit. | ||
SPD DES (4) | ;SPD DES (4) | ||
A set indicated airspeed or mach number is being held by varying pitch angle in order to descend. The autothrottle is commanded to hold idle thrust. | A set indicated airspeed or mach number is being held by varying pitch angle in order to descend. The autothrottle is commanded to hold idle thrust. | ||
FPA (5) | ;FPA (5) | ||
A set flight path angle is being tracked. | A set flight path angle is being tracked. | ||
FLARE (6) | ;FLARE (6) | ||
The aircraft is flared for touchdown during and autoland. | The aircraft is flared for touchdown during and autoland. | ||
ROLLOUT (6) | ;ROLLOUT (6) | ||
Those is lowered at a user configurable rate and then held on the ground via light forward pressure during rollout. | Those is lowered at a user configurable rate and then held on the ground via light forward pressure during rollout. | ||
T/O CLB (7) | ;T/O CLB (7) | ||
The takeoff speed (V2+10) is being held by varying pitch angle. The autothrottle is commanded to hold the thrust limit. | The takeoff speed (V2+10) is being held by varying pitch angle. The autothrottle is commanded to hold the thrust limit. | ||
G/A CLB (7) | ;G/A CLB (7) | ||
The set go around speed (takeoff speed or current speed, whichever is higher) is being held by varying pitch angle. The autothrottle is commanded to hold the thrust limit. | The set go around speed (takeoff speed or current speed, whichever is higher) is being held by varying pitch angle. The autothrottle is commanded to hold the thrust limit. | ||