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 |