-
Ground operation is limited to ambient temperatures of _______ to _______ degrees C
-23 to 43 degrees C
-
Maximum Icing Band/Icing Type __________ Feet / __________
5,000 Feet / light rime
-
Minimum Altitude for Entry ________ Feet MSL
13,500 Feet MSL
-
Minimum Cloud Clearance _________ Feet above the clouds
7,000 Feet
-
Symmetric Clean ______ to ______ Gs
-3.5 to 7.0 Gs
-
Symmetric Gear/Flaps ________ to ________ Gs
0 to 2.5 Gs
-
Asymmetric Clean ______ to ______ Gs
-1.0 to 4.7 Gs
-
Asymmetric Gear/Flaps _______ to ______ Gs
0 to 2.0 Gs
-
Dry Runway ______ Knots
25 Knots
-
Wet Runway ______ Knots
10 Knots
-
Icy Runway _____ Knots
5 Knots
-
Touch-and-Go ________ Knots
20 Knots
-
Formation Takeoff/Landing _______ Knots
15 Knots
-
Maximum Tailwind Component for Takeoff _______ Knots
10 Knots
-
Maximum Wind with Canopy Open ________ Knots
40 Knots
-
Minimum Runway Length _________ Feet
4,000 Feet
-
Minimum Runway Width ___________ Feet
75 Feet
-
Normal Recovery Fuel ___________ Pounds
200 Pounds
-
Minimum Fuel _______ Pounds ( _______ Pounds Solo)
150 Pounds ( 200 Pounds Solo)
-
Emergency Fuel ________ Pounds (______ Pounds Solo)
100 Pounds ( 100 Pounds Solo)
-
Minimum Fuel for Aerobatics _______ Pounds per side
150 Pounds
-
Normal Above 18,000 Ft MSL _________ (+-) ________ PSI
3.6 (+-) 0.2 PSI
-
Over-pressurization Valve Opens ____________ PSI
4.0 PSI
-
Starter Limit : ________ Seconds
20 Seconds
-
Wait ____ Sec, ____ Min, ____ Min, ____ Min after each start attempt
30 Sec, 2 Min, 5 Min, 30 Min
-
Maximum ITT _______ degrees C for ____ sec (Do Not Attempt Restart)
1000 degrees C for 5 Sec
-
Maximum Oil Pressure ____________ PSI
200 PSI
-
Minimum oil temperature ________ degrees C
-40 degrees C
-
Minimum Battery Voltage _________ V
23.5 V
-
Max Airspeed Gear and/or Flaps ______ KIAS
150 KIAS
-
Max Operating Speed __________ KIAS or ______ Mach
316 KIAS or 0.67 Mach
-
Full rudder deflection above KIAS will exceed the limits of the rudder control system
150 KIAS
-
__________ Stalls
Inverted
-
__________ Spins
Inverted
-
Aggravated ___________
spins past 2 turns
-
Spins with the PCL ____________
above idle
-
Spins with the ____________, ___________, or ___________ extended
landing gear , flaps , or speed brake
-
Spins with the ________________
PMU off
-
Spins below __________ feet pressure altitude
10,000 feet
-
Spins above __________ feet pressure altitude
22,000 feet
-
Abrupt ____________________ maneuvers
cross-controlled ( snap)
-
Aerobatic maneuvers, spins or stalls with greater than _____ pounds fuel imbalance
50 pounds
-
______________ slides
Tail
-
Maximum Torque
Takeoff/Max _____%
Transient _______% ( _____ Seconds)
Torque above _____% is indicative of system malfunction
-
Maximum ITT
Idle ____ degrees C
Takeoff/ Max ______ degrees C
Transient ______ degrees C(Up to____ Seconds)
- 750 degrees C
- 820 degrees C
- 870 degrees C & 20 Seconds
-
N1
Idle ____ to _____% Ground, _____ % (Min Flight)
60 to 61% 67%
-
Np
Idle ______ to _______ %
Takeoff/Max ______%, (_____ % (+-) ___% PMU off)
Avoid stabilized ground operations from _____ to _____ % Np
- 46 to 50%
- 100% (100% (+-) 2%
- 62 to 80%
-
Oil Pressure
Takeoff/Max _____ to _______ PSI
Aerobatics / Spins _______ to _______ PSI
Aerobatics / Spins (Idle) ______ to ______ PSI (___ Sec)
- 90 to 120 PSI
- 40 TO 130 PS
- I15 TO 40 PSI (5 Sec)
-
Oil Temp
Takeoff/Max _______ to _______ degrees C
Transient _____ to _______ degrees C (______ minutes)
- 10 to 105 degrees C
- 106 to 110 degrees C ( 10 minutes)
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