Gulfstream Aerospace G650 manuals

This document is a supplement to the Gulfstream G650 Airplane Flight Manual, specifically for aircraft with serial numbers 6001 and subsequent that do not have ASC 134. It provides updated limitations, procedures, and performance information that supersede the basic manual.

• Applies to G650 airplanes SN 6001 and subsequent without ASC 134.
• Limits operating envelope to below 250 KCAS / 0.925M unless in an emergency.
• Maximum altitude with rudder or yaw damper inoperative is 20,000 ft.
• Maximum operating limit speed is 250 KCAS / 0.925M, except for emergencies.
• Revised procedures for rudder failure include immediate autopilot disconnection.
• Maintain airspeed below 200 KCAS to reduce roll oscillations during rudder failure.
• Landing should be performed as soon as practicable in case of rudder failure.
• Use smooth roll inputs to minimize lateral-directional oscillations.