T6 Ops Limits Flashcards

1
Q

Engine
Maximum Torque

Takeoff/Max __%

A

Takeoff/Max 100%

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2
Q

Engine
Maximum Torque

Transient __% to __% (__Seconds)

A

Transient 100% to 107% (5 Seconds)

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3
Q

Engine
Maximum Torque

Torque above __% is indicative of system malfunction

A

Torque above 107% is indicative of system malfunction

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4
Q

Engine
Maximum ITT

Idle __°C

A

Idle 750°C

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5
Q

Engine
Maximum ITT

Takeoff/Max __°C

A

Takeoff/Max 820°C

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6
Q

Engine
Maximum ITT

Transient __ to __°C (__ Seconds)

A

Transient 821 to 870°C (20 Seconds)

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7
Q

Engine
N1

Idle __ to __% Ground __% (Min) Flight

A

Idle 60 to 61% Ground, 67% (Min) Flight

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8
Q

Engine
Np

Idle __ to __%

A

Idle 46 to 50%

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9
Q

Engine
Np

Takeoff/Max __%, (__% ± __% PMU Off)

A

Takeoff/Max 100%, (100% ± 2% PMU Off)

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10
Q

Engine
Np

Avoid Stabalized Ground Operations From __ to __% Np

A

Avoid Stabalized Ground Operations From 62 to 80% Np

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11
Q

Engine
Oil Pressure

Takeoff/Max __ to __ PSI

A

Takeoff/Max 90 to 120 PSI

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12
Q

Engine
Oil Pressure

Acrobatics/Spins __ to __ PSI

A

Acrobatics/Spins 40 to 130 PSI

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13
Q

Engine
Oil Pressure

Acrobatics/Spins (Idle) __ to __ PSI (__ Sec)

A

Acrobatics/Spins (Idle) 15 to 40 PSI (5 Sec)

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14
Q

Engine
Oil Temp

Takeoff/Max __ to __°C

A

Takeoff/Max 10 to 105°C

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15
Q

Engine
Oil Temp

Transient __ to __°C (10 Min)

A

Transient 106 to 110°C (10 Min)

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16
Q

Engine
Maximum Fuel Flow

All Phases of Flight __ PPH

A

All Phases of Flight 799 PPH

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17
Q

Prohibited Manuvers

  1. __ Stalls
A
  1. Inverted Stalls
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18
Q

Prohibited Manuvers

  1. __ Spins
A
  1. Inverted Spins
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19
Q

Prohibited Manuvers

  1. Aggravated __
A
  1. Aggravated spins past 2 turns
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20
Q

Prohibited Manuvers

  1. Spins with the PCL __
A
  1. Spins with the PCL above idle
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21
Q

Prohibited Manuvers

  1. Spins with __, __, or __ extended
A
  1. Spins with landing gear, flaps, or speed brake extended
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22
Q

Prohibited Manuvers

  1. Spins with the __
A
  1. Spins with the PMU off
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23
Q

Prohibited Manuvers

  1. Spins below __ feet pressure altitude
A
  1. Spins below 10,000 feet pressure altitude
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24
Q

Prohibited Manuvers

  1. Spins above __ feet pressure altitude
A
  1. Spins above 22,000 feet pressure altitude
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25
Q

Prohibited Manuvers

  1. Abrupt __ manuvers
A
  1. Abrupt cross-controlled (snap) manuvers
26
Q

Prohibited Manuvers

  1. Acrobatics manuvers, spins, or stalls with greater than __ pounds fuel imbalance
A
  1. Acrobatics manuvers, spins, or stalls with greater than 50 pounds fuel imbalance
27
Q

Prohibited Manuvers

  1. __ slides
A
  1. Tail slides
28
Q

Airspeed Limitations

Max Airspeed Gear and/or Flaps __ KIAS

A

Max Airspeed Gear and/or Flaps 150 KIAS

29
Q

Airspeed Limitations

Max Operating Speed __ KIAS or __ Mach

A

Max Operating Speed 316 KIAS or 0.67 Mach

30
Q

Airspeed Limitations

Full rudder defection above __ KIAS will exceed the limits of the rudder control system.

A

Full rudder defection above 150 KIAS will exceed the limits of the rudder control system.

31
Q

Starting

Starter Limit: __ Seconds

A

Starter Limit: 20 Seconds

32
Q

Starting

Wait __ Sec, __ Min, __ Min, __ Min after each start/monitoring attempt

A

Wait 30 Sec, 2 Min, 5 Min, 30 Min after each start/monitoring attempt

33
Q

Starting

Maximum ITT __ to __ for __ Sec (Do Not Attempt Restart)

A

Maximum ITT 871 to 1,000 °C for 5 Sec (Do Not Attempt Restart)

34
Q

Starting

Maximum Oil Pressure __ PSI

A

Maximum Oil Pressure 200 PSI

35
Q

Starting

Minimum Oil Temperature __ °C

A

Minimum Oil Temperature -40 °C

36
Q

Starting

Minimum Battery Voltage __ V

A

Minimum Battery Voltage 23.5 V

37
Q

Pressurization

Normal above 18,000 Ft MSL 3.6±0.2 PSI

A

Normal above 18,000 Ft MSL __±__ PSI

38
Q

Pressurization

Overpressurization Safety Valve Opens 4.0 PSI

A

Overpressurization Safety Valve Opens __ PSI

39
Q

Fuel

Normal Recovery Fuel __ Pounds

A

Normal Recovery Fuel 200 Pounds

40
Q

Fuel

Minimum Fuel __ Pounds (__ Pounds Solo)

A

Minimum Fuel 150 Pounds (200 Pounds Solo)

41
Q

Fuel

Emergency Fuel 100 Pounds

A

Emergency Fuel __ Pounds

42
Q

Fuel

Minimum Fuel for Acrobatics __ Pounds per side

A

Minimum Fuel for Acrobatics 150 Pounds per side

43
Q

Runway

Minimum Landing Distance Available (LDA) __, or heavy weight flaps __ landing ground rools plus __ Feet, whichever is greater

A

Minimum Landing Distance Available (LDA) 4,000 Feet, or heavy weight flaps up landing ground rools plus 500 Feet, whichever is greater

44
Q

Runway

Minimum Runway Width 75 Feet

A

Minimum Runway Width __ Feet

45
Q

Maximum Crosswinds

Dry Runway __ Knots

A

Dry Runway 25 Knots

46
Q

Maximum Crosswinds

Wet Runway __ Knots

A

Wet Runway 10 Knots

47
Q

Maximum Crosswinds

Icy Runway __ Knots

A

Icy Runway 5 Knots

48
Q

Maximum Crosswinds

Touch-and-Go __ Knots

A

Touch-and-Go 20 Knots

49
Q

Maximum Crosswinds

Formation Takeoff/Landing 15 Knots

A

Formation Takeoff/Landing __ Knots

50
Q

Maximum Crosswinds

Maximum Tailwind Component for Takeoff 10 Knots

A

Maximum Tailwind Component for Takeoff __ Knots

51
Q

Maximum Crosswinds

Maximum Wind with Canopy Open __ Knots

A

Maximum Wind with Canopy Open 40 Knots

52
Q

Acceleration Limits

Symmetric Clean __ to __ Gs

A

Symmetric Clean -3.5 to 7.0 Gs

53
Q

Acceleration Limits

Asymptomatic Clean __ to __ Gs

A

Asymptomatic Clean -1.0 to 4.7 Gs

54
Q

Acceleration Limits

Symmetric Gear/Flaps __ to __ Gs

A

Symmetric Gear/Flaps 0 to 2.5 Gs

55
Q

Acceleration Limits

Asymmetric Clean __ to __ Gs

A

Asymmetric Clean -1.0 to 4.7 Gs

56
Q

Acceleration Limits

Asymmetric Gear/Flaps __ to __ Gs

A

Asymmetric Gear/Flaps 0 to 2.0 Gs

57
Q

Intentional Spin Entry

Minimum Altitude for Entry __ Feet MSL

A

Minimum Altitude for Entry 13,500 Feet MSL

58
Q

Intentional Spin Entry

Minimum Cloud Clearance __ above clouds

A

Minimum Cloud Clearance 7,000 Feet above clouds

59
Q

Icing

Maximum Icing Band __ Feet

A

Maximum Icing Band 5,000 Feet

60
Q

Icing

Maximum Icing Type __

A

Maximum Icing Type light rime

61
Q

Temperature

Ground Operation is limited to ambient temperatures of __ to __°C

A

Ground Operation is limited to ambient temperatures of -23 to 43°C