Beechcraft King Air 100 — Emergency Procedures

This document serves as the Emergency Procedures manual for the Beechcraft King Air A-100, published in 1990. It is designed for pilots operating this aircraft model, providing critical information on handling emergencies that may arise during flight operations. The manual outlines various emergency scenarios, including engine failures, fires, and emergency descent procedures, along with specific actions to take in each situation. Pilots should familiarize themselves with these procedures to ensure safety and effective response in emergencies.

• Maximum Take-Off Weight: 11,500 lbs
• Maximum Cross Wind: 25 knots
• Fuel Capacity: 470 U.S. gallons
• Emergency Descent Airspeed: 156 knots
• Engine Failure Below Take-Off Speed: Power IDLE, Brakes AS REQUIRED