Section V: Operating Limitations

	Table of Contents Introduction 5-2 Minimum crew 5-2 Instrument Markings 5-2 Fuel 5-2  Emergency Fuels 5-2 Engine Operating Limits 5-2  In-Flight Shutdown 5-2  Exhaust Gas Temperature (EGT) 5-2  Compressor Inlet Temperature (CIT) 5-5  Engine Speed (RPM) 5-5  Oil Pressure 5-5  Exhaust Nozzle Position (ENP) 5-5 Maximum Weight 5-5 Load Factor Limits 5-8 Flight Envelope Limits 5-8  Maximum Mach 5-8  Airspeed 5-8  Angle of Attack 5-10  Altitude 5-10  High Altitude Turns 5-10 Prohibited Maneuvers 5-10 Simulated Single-Engine Flight 5-10 Rate of Descent 5-16 Center of Gravity 5-16  Pitch Trim Indications While Subsonic 5-16  Pitch Trim Indications While Supersonic 5-17 Aircraft Systems Limitations 5-17  Surface Limiter 5-17  Stability Augmentation System 5-17  Autopilot 5-17  Fuel System 5-17  Anticollision Lights 5-17  Canopy 5-17  Landing Gear 5-18  Tires 5-18  Brakes 5-23  Drag Chute 5-23  Flight Without Pressure Suit 5-23