What is the go-around minimum fuel quantity per wing tank and the associated nose-up pitch angle?

• A. 600 LBS per wing tank at 10 degrees nose up
• B. 600 LBS per wing tank at 5 degrees nose up
• C. 500 LBS per wing tank at 10 degrees nose up
• D. 700 LBS per wing tank at 15 degrees nose up

Answer: (A)

When performing a go-around, you must have enough fuel to execute the maneuver and reach a safe altitude with a contingency reserve, while adopting an attitude that gives you a reliable climb. The standard training value for a go-around is 600 pounds in each wing tank, which ensures symmetric fuel distribution and sufficient total fuel to climb and manage the procedure without running low on reserves. The associated nose-up pitch of 10 degrees is chosen to produce a solid, controlled climb: it lifts the nose enough to achieve a positive climb rate and avoid stalling or losing airspeed, while staying within safe handling limits for the aircraft during the transition from approach to climb. A smaller pitch like 5 degrees would yield a gentler climb that might not meet the required climb gradient; a larger pitch or more fuel per wing would unnecessarily bias the aircraft toward a steeper climb or heavier weight without added safety benefit.