Beechcraft King Air 360

This document is a FAA Approved Airplane Flight Manual Supplement for the Beechcraft Super King Air 350, 350C, 360, and 360C airplanes, specifically addressing modifications made under the CenTex Aerospace Halo 350 Increased Gross Weight conversion. The supplement provides critical information regarding the increased maximum takeoff weight, which is now 15,950 pounds, allowing for an additional payload capacity of approximately 950 pounds. It includes essential operational limitations, emergency procedures, and performance data that pilots must be familiar with when operating these modified aircraft. The information is designed to supplement the basic Pilot Operating Handbook (POH) and should be used in conjunction with it for comprehensive operational guidance.

• Maximum Takeoff Weight: 15,950 pounds
• Maximum Ramp Weight: 16,050 pounds
• Maximum Landing Weight: 15,000 pounds
• Maneuvering Speed (VA): 179 KCAS
• Emergency Descent Speed: 182 knots
• One-Engine Inoperative Best Rate-of-Climb Speed (VYSE): 135 knots
• Maximum Operating Speed (VMO): 245 knots up to 24,000 feet