| 摘要 |
The present invention concerns a method for the detection and adjustments of angular excursion of the aircraft wing flaps, comprising the use of at least a devices pair (30, 40) with a first device (30) that can be positioned on a flap (20), and a second device (40) that can be positioned on the trailing edge of said wing in line with said first device, a system for automated or operator-based reading of the angular excursion data as visualized in the cockpit; a dedicated device for the adjustment of the flap inclination;
Being carried out the following steps:
- Positioning the first device (30) on a wing flap (20), and the second device (40) on the trailing edge of the wing in line with said first device;
- Moving the relevant flap until the first and second devices provide the same inclination data;
- Verifying the coherence between the inclination data and the zero as visualized in the cockpit and the flap;
- Comparing the value of the difference between the values provides by the first and second device with the value as visualized in the cockpit. |
