Left/Right Aileron Failure
This is a work in progress
The indicated aileron flight control surface is inoperative. The REUs and/or hydraulic actuators or EBHAs on the indicated ailerons are inoperative resulting in a damped bypass (float) or jammed position.
A loss of one or both ailerons will result in reduced lateral (roll) control effectiveness and reduced ground roll braking effectiveness.
- Fuel Burn: Increased.
- Steep Approach: Unavailable.
To view the FCS Synoptic Legend, refer to 03-13-190, FCS Synoptic Legend.
- Autopilot . . . OFF
- Airspeed . . . 285 KCAS / 0.90M maximum
- ROLLTRIM . . . Neutralize roll control forces
- Airplane . . . Land as soon as practicable
- If additional roll trim is required:
a. Landing Controllability Check . . . Perform
- Approach and Landing
a. Runway . . . Select runway based on minimum crosswind (less than 10 knots)
b. Airspeed . . . Maintain VREF minimum until touchdown
c. Landing . . . Lower nose wheels to runway without delay
Refer to 03-13-10, Landing Controllability Check
Gulfstream GVII-G500 Airplane Flight Manual, Revision 1, August 31, 2018