180 |
Lift coefficient increment due to full-span double flap (main flap slotted). |
Aero F.01.01.09 |
180 |
Lift coefficient increment due to full-span slotted flaps. |
Aero F.01.01.08 |
180 |
Wing lift coefficient increment at zero angle of attack due to deployment of plain trailing-edge flaps at low speeds. |
97011 |
180 |
Wing lift coefficient increment at zero angle of attack due to deployment of trailing-edge split flaps at low speeds. |
0 85679 996 3 |
180 |
Wing lift coefficient increment at zero angle of attack due to deployment of leading-edge devices at low speeds. |
96032 |
180 |
Wing lift coefficient increment at zero angle of attack due to deployment of double-slotted or triple-slotted flaps at low speeds. |
95021 |
180 |
Wing lift increment at zero angle of attack due to deployment of single-slotted flaps at low speeds. |
93019 |
180 |
Maximum lift of wings with leading-edge devices and trailing-edge flaps deployed. |
92031 |
180 |
Maximum lift of wings with trailing-edge flaps at low speeds. |
91014 |
180 |
Lift coefficient increment at low speeds due to full-span split flaps. |
74009 |