T-6 Ops Limits Flashcards
Maximum Torque
Takeoff / Max ____%
Transient ____% (____ Seconds)
Torque above ____% is indicative of a system malfunction.
100
132, 20
102
Maximum ITT
Idle ____C
Takeoff / Max ____C
Transient ____ to ____C (____ Seconds)
750
820
821,870,20
N1
Idle ____ to ____% Ground, ____% (Min) Flight
60,61,67
Np
Idle ____ to ____%
Takeoff Max ____%, (____% +- ____% PMU Off)
Avoid stabilized ground operations from ____ to ____% Np
46,50
100,100,2
62,80
Oil Pressure
Takeoff / Max ____ to ____ PSI
Aerobatics / Spins ____ to ____ PSI
Aerobatics / Spins (Idle) ____ to ____ PSI (____ Sec)
90,120
40,130
15,40,5
Oil Temp
Takeoff / Max ____ to ____ *C
Transient ____ to ____ *C (____ Min)
10,105
106,110,10
Maximum Fuel Flow
All phases of flight ____ PPH
799
Prohibited Maneuvers
1. ____ Stalls
2. ____ Spins
3. Aggravated ____
4. Spins with the PCL ____
5. Spins with the ____, ____, or ____ extended
6. Spins with the ____
7. Spins below ____ feet pressure altitude
8. Spins above ____ feet pressure altitude
9. Abrupt ____ maneuvers
10. Aerobatic maneuvers, spins, or stalls with greater than ____ pounds fuel imbalance
11. ____ Slides
Inverted
Inverted
spins past 2 turns
above idle
landing gear, flaps, speed brake
PMU off
10,000
22,000
cross-controlled (snap)
50
Tail
Airspeed Limitations
Max Airspeed Gear and/ or Flaps ____ KIAS
Max Operating Speed ____ KIAS or ____ Mach
Full rudder deflection above ____ KIAS will exceed the limits of the rudder control system
150
316,0.67
150
Starting
Starter Limit: ____ Seconds
Wait ____ Sec, ____ Min, ____ Min, ____ Min after each start/ motoring attempt
Maximum ITT ____ to ____ *C for ____ Sec (Do Not Attempt Restart)
Maximum Oil Pressure ____ PSI
Minimum Oil Temperature ____ *C
Minimum Battery Voltage ____ V
20
30,2,5,30
871, 1,000, 5
200
-40
23.5
Pressurization
Normal Above 18,000 Ft MSL ____ +- ____ PSI
Overpressurization Safety Valve Opens ____ PSI
3.6, 0.2
4.0
Fuel
Normal Recovery Fuel ____ Pounds
Minimum Fuel ____ Pounds (____ Pounds Solo)
Emergency Fuel ____ Pounds
Minimum Fuel for Aerobatics ____ Pounds per Side
200
150,200
100
150
Runway
Minimum Landing Distance Available (LDA) ____ Feet, or heavy weight flaps ____ landing distance plus ____ Feet, whichever is greater
Minimum Runway Width ____ Feet
4,000, up, 500
75
Winds
Dry Runway ____ Knots
Wet Runway ____ Knots
Icy Runway ____ Knots
Touch-and-Go ____ Knots
Formation Takeoff / Landing ____ Knots
Maximum Tailwind Component for Takeoff ____ Knots
Maximum Wind with Canopy Open ____ Knots
25
10
5
20
15
10
40
Acceleration Limits
Symmetric Clean ____ to ____ Gs
Symmetric Gear/ Flaps ____ to ____ Gs Asymmetric Clean ____ to ____ Gs Asymmetric Gear/ Flaps ____ to ____ Gs
-3.5, 7.0
0, 2.5
-1.0, 4.7
0, 2.0
