T-6 Ops Limits

Maximum Torque (Takeoff/Max): __________ %

100

Maximum Torque (Transient): __________ % ____________ seconds

132, 20

Maximum Torque: Torque above ___________ % is indicative of a system malfunction.

102%

Maximum ITT: (Idle) _____ °C

750

Maximum ITT: (Takeoff/Max) _____ °C

820

Maximum ITT: (Transient) _____ to _°C (__ Seconds)

821, 870, 20

N₁ Idle _____ to _____% Ground

60, 61, 67

Nₚ (Idle) ______ to ______ %

46, 50

Nₚ (Takeoff/Max) ______ %

100, 100 ± 2

Avoid stabilized ground operations from ____ to ____ % Nₚ

62, 80

Oil Pressure (Takeoff/Max) _____ to _____ PSI

90, 120

Oil Pressure (Aerobatics/Spins) _____ to _____ PSI

40, 130

Oil Pressure (Aerobatics/Spins Idle) _____ to _____ PSI

15, 40

Oil Temp (Takeoff/Max) _____ to _____ °C

10, 105

Oil Temp (Transient) _______to ________ °C (_______ Min)

106, 110, 10

Maximum Fuel Flow All phases of flight ______ PPH

799

Prohibited Maneuvers 1. _____________ Stalls

Inverted

Prohibited Maneuvers 2. _____________ Spins

Inverted

Prohibited Maneuvers 3. Aggravated __________________________________

spins past 2 turns

Prohibited Maneuvers 4. Spins with the PCL __________________________________

above idle

Prohibited Maneuvers 5. Spins with the _____________________

landing gear flaps speed brake

Prohibited Maneuvers 6. Spins with the ____________________

PMU off

Prohibited Maneuvers 7. Spins below ______________ feet pressure altitude

10,000

Prohibited Maneuvers 8. Spins above ______22,000______ feet pressure altitude

22,000

Prohibited Maneuvers 9. Abrupt ___________________________ maneuvers

cross-controlled (snap)

10. Aerobatic maneuvers, spins, or stalls with greater than______________ pounds fuel imbalance

50

Prohibited Maneuvers 11. __________ slides

Tail

Airspeed Limitations: Max Airspeed Gear and/or Flaps __________ KIAS

150

Airspeed Limitations: Max Operating Speed __________ KIAS or ___________ Mach

316, 0.67

Airspeed Limitations: Full rudder deflection above __________ KIAS will exceed the limits of the rudder control system.

150

Starting: Starter Limit _______ Seconds

20

Starting: Wait ______

30 Sec, 2 min, 5 min, 30 min

Maximum ITT _________ to __________ ⁰C for __________ Sec

871 1000 5

Starting: Maximum Oil Pressure _______ PSI

200

Starting: Minimum Oil Temperature _______ °C

-40

Starting: Minimum Battery Voltage _______ V

23.5

Pressurization: Normal above 18,000

3.6 ± 0.2

Pressurization: Overpressurization Safety Valve Opens _________ PSI

4.0

Fuel: Normal Recovery Fuel ___________ Pounds

200

Fuel: Minimum Fuel _________ Pounds (_________ Pounds Solo)

150, 200

Fuel: Emergency Fuel __________ Pounds

100

Fuel: Minimum Fuel for Aerobatics ____________ Pounds per side

150

Minimum Landing Distance Available (LDA) ___________Feet, or

Oil Temp heavy weight flaps ________ landing distance plus __________ Feet, whichever is greater

4,000, up, 500

Minimum Runway Width _______ Feet

75

Maximum Crosswinds: Dry Runway _________ Knots

25

Maximum Crosswinds: Wet Runway _________ Knots

10

Maximum Crosswinds: Icy Runway _________ Knots

5

Maximum Crosswinds: Touch-and-Go _________ Knots

20

Maximum Crosswinds: Formation Takeoff/Landing _________ Knots

15

Maximum Crosswinds: Maximum Tailwind Component for Takeoff _________ Knots

10

Maximum Crosswinds: Maximum Wind with Canopy Open _________ Knots

40

Acceleration Limits: Symmetric Clean __________ to ___________ Gs

-3.5, 7.0

Acceleration Limits: Symmetric Gear/Flaps __________ to ___________ Gs

0, 2.5

Acceleration Limits: Asymmetric Clean __________ to ___________ Gs

-1.0, 4.7

Acceleration Limits: Asymmetric Gear/Flaps __________ to ___________ Gs

0, 2.0

Minimum Altitude for Entry _________ Feet MSL

13,500

Minimum Cloud Clearance _________ Feet above clouds

7,000

Maximum Icing Band ________ Feet

5,000

Icing: Maximum Icing Type ___________

Light Rime

Temperature: Ground operation is limited to ambient temperatures of _______ to _______ °C

-23, 43