How is load distribution and center of gravity managed for the UH-60 when carrying external cargo or passengers?

How is load distribution and center of gravity managed for the UH-60 when carrying external cargo or passengers?

• A. Ensure proper weight distribution, balance, and CG within limits; adjust ballast or fuel as necessary; verify with load diagrams.
• B. Use flight-time estimates to guess CG and frequently change ballast during flight.
• C. CG does not matter when external cargo is strapped to the aircraft.
• D. Balance is achieved by distributing passengers evenly around the cabin only after landing.

Answer: (B)

Managing load distribution and center of gravity for the UH-60 with external cargo or passengers starts with staying within published weight and balance limits for the specific configuration. Before flight, the crew uses the load diagrams to place external loads, passengers, crew, and fuel so the forward and aft CG stay within limits and the aircraft remains within its maximum takeoff weight. If the diagram calls for it, ballast or fuel adjustments are made to precisely tune the CG, and this is verified against the official data so handling remains predictable and safe. The key is knowing the exact configuration and keeping the CG within limits throughout the flight, rather than guessing where the CG is or changing ballast on a whim. Relying on flight-time estimates to determine CG or making frequent in-flight ballast changes undermines stability and control. External loads and passenger distribution do shift the CG, so proper planning and verification against the load diagram are essential. CG matters for stability and control in hover, conversion to forward flight, and landing, so balancing is done during the planning and flight, not after the aircraft is on the ground.

Managing load distribution and center of gravity for the UH-60 with external cargo or passengers starts with staying within published weight and balance limits for the specific configuration. Before flight, the crew uses the load diagrams to place external loads, passengers, crew, and fuel so the forward and aft CG stay within limits and the aircraft remains within its maximum takeoff weight. If the diagram calls for it, ballast or fuel adjustments are made to precisely tune the CG, and this is verified against the official data so handling remains predictable and safe. The key is knowing the exact configuration and keeping the CG within limits throughout the flight, rather than guessing where the CG is or changing ballast on a whim. Relying on flight-time estimates to determine CG or making frequent in-flight ballast changes undermines stability and control. External loads and passenger distribution do shift the CG, so proper planning and verification against the load diagram are essential. CG matters for stability and control in hover, conversion to forward flight, and landing, so balancing is done during the planning and flight, not after the aircraft is on the ground.