Section 2. Operating Limits 01 July 2020
Engine Starting
Maximum Torque Starter Limit: Seconds
Takeoff / Max % Wait Sec, Min, Min, Min after each start/motoring attempt
Transient % ( Seconds) Maximum ITT to °C for Sec (Do Not Attempt Restart)
Torque above % is indicative of a system malfunction Maximum Oil Pressure PSI
Maximum ITT Minimum Oil Temperature °C
Idle °C Minimum Battery Voltage V
Takeoff/Max °C Pressurization
Transient to °C ( Seconds) Normal Above 18,000 Ft MSL ± PSI
N1 Overpressurization Safety Valve Opens PSI
Idle to % Ground, % (Min) Flight Fuel
Np Normal Recovery Fuel Pounds
Idle to % Minimum Fuel Pounds ( Pounds Solo)
Takeoff / Max %, (% ± % PMU Off) Emergency Fuel Pounds
Avoid stabilized ground operations from to % Np Minimum Fuel for Acrobatics Pounds per side
Oil Pressure Runway
Takeoff / Max to PSI Minimum Landing Distance Available (LDA) Feet, or heavy weight flaps landing distance plus Feet, whichever is greater
Acrobatics / Spins to PSI Minimum Runway Width Feet
Acrobatics / Spins (Idle) to PSI ( Sec) Winds
Oil Temp Maxmimum Crosswinds
Takeoff / Max to °C Dry Runway Knots
Transient to °C ( Min) Wet Runway Knots
Maximum Fuel Flow Icy Runway Knots
All phases of flight PPH Touch-and-go Knots
Prohibited Maneuvers Formation Takeoff / Landing Knots
Stalls Maximum Tailwind Component for Takeoff Knots
Spins Maximum Wind with Canopy Open Knots
Aggrivated Acceleration Limits
Spins with the PCL Symmetric Clean to Gs
Spins with the , , or extended Symmetric Gear / Flaps to Gs
Spins with the Asymmetric Clean to Gs
Spins below feet pressure altitude Asymmetric Gear / Flaps to Gs
Spins above feet pressure altitude Intentional Spin Entry
Abrupt maneuvers Minimum Altitude for Entry Feet MSL
Aerobatic maneuvers, spins, or stalls with greater than pounds fuel imbalance Minimum Cloud Clearance Feet above clouds
slides Icing
Airspeed Limitations Maximum Icing Band Feet
Max Airspeed Gear and/or Flaps KIAS Maximum Icing Type
Max Operating Speed KIAS or Mach Temperature
Full rudder deflection above KIAS will exceed the limits of the rudder control system. Ground operation is limited to ambient temperatures of to °C