Op limits T-6A Flashcards

1
Q

Maximum Torque - Takeoff / Max

A

100 %

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2
Q

Maximum Torque - Transient (percent/seconds)

A

132 % ( 20 seconds)

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3
Q

Maximum Torque - Torque above ____ indicative of system malfunction

A

102 %

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4
Q

Maximum ITT - Idle

A

750 degrees Celcius

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5
Q

Maximum ITT - Takeoff/Max

A

820 degrees Celcius

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6
Q

Maximum ITT - Transient (Degrees/seconds)

A

821 to 870 degrees Celcius (up to 20 seconds)

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7
Q

N₁ - Idle, Ground (percent)

A

60 to 61 %, 67%

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8
Q

Np - idle (percent)

A

46 to 50 %

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9
Q

Np - takeoff/max (percent)

A

100% ( 100% +/- 2% PMU off)

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10
Q

Np - avoid stabilized ground operations (percent)

A

62 to 80%

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11
Q

Oil pressure - takeoff/max

A

90 to 120 PSI

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12
Q

Oil pressure - aerobatics/spins

A

40 to 130 PSI

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13
Q

Oil pressure - Aerobatics/spins Idle (Psi/seconds)

A

15 to 40 PSI (5 sec)

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14
Q

Oil Temp - takeoff/max

A

10 to 105 degrees Celcius

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15
Q

Oil Temp - Transient (degrees/minutes)

A

106 to 110 degrees Celcius (10 minutes)

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16
Q

Prohibited Maneuvers (stalls)

A

Inverted

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17
Q

Prohibited Maneuvers (Spins)

A

Inverted

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18
Q

Prohibited Maneuvers -Aggravated

A

Spins past 2 turns

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19
Q

Prohibited Maneuvers - Spins with the PCL

A

above idle

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20
Q

Prohibited Maneuvers with what (extended)

A

landing gear, flaps, or speed brake

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21
Q

Prohibited Maneuvers - Spins with the

A

PMU off

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22
Q

Prohibited Maneuvers - spins below (feet)

A

10,000 feet pressure altitude

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23
Q

Prohibited Maneuvers - spins above (feet)

A

22,000 feet pressure altitude

24
Q

Prohibited Maneuvers - abrupt “blank” maneuvers

A

cross-controlled (snap)

25
Q

Prohibited Maneuvers - Aerobatic, spins, or stalls with greater than “blank” pounds fuel imbalance

A

50 pounds

26
Q

Prohibited Maneuvers - “blank” slides

A

Tail slides

27
Q

Airspeed Limitations - Max airspeed gear and/or flaps

A

150 KIAS

28
Q

Airspeed Limitations - Max Operating speed (KIAS/Mach)

A

316 KIAS or .67 mach

29
Q

Airspeed Limitations - full rudder deflection above blank KIAS will exceed the limits of the rudder control system

A

150 KIAS

30
Q

Starting - Starter Limit

A

20 seconds

31
Q

Starting - Wait

A

30 sec, 2 minutes, 5 min, 30 min after each start/motoring

32
Q

Starting - Maximum ITT (Degrees/seconds)

A

871 to 1000 degrees celcius for 5 seconds

33
Q

Starting - Maximum Oil pressure

A

200 PSI

34
Q

Starting - Minimum Oil temperature

A

-40 degrees celcius

35
Q

Starting - Minimum Battery Voltage

A

23.5 V

36
Q

Fuel - Normal recovery fuel

A

200 pounds

37
Q

Fuel - Minimum Fuel

A

150 pounds (200 Pounds solo)

38
Q

Fuel - Emergency Fuel

A

100 Pounds

39
Q

Fuel - Minimum Fuel Aerobatics

A

150 Pounds per side

40
Q

Runway - Minimum Landing distance available (LDA) Blank feet or heavy weight flaps blank landing distance plus blank feet whichever is greater

A

4000 feet, up, 500 feet

41
Q

Runway - Minimum runway width blank feet

A

75 feet

42
Q

Winds Max Crosswinds - Dry Runway

A

25 Knots

43
Q

Winds Max Crosswinds - Wet Runway

A

10 Knots

44
Q

Winds Max Crosswinds - Icy Runway

A

5 Knots

45
Q

Winds Max Crosswinds - Touch- and-go

A

20 Knots

46
Q

Winds - Maximum tailwind component for Takeoff

A

10 Knots

47
Q

Winds - Maximum Wind with Canopy Open

A

40 Knots

48
Q

Acceleration Limits - Symmetric Clean (Gs)

A

-3.5 to 7.0 Gs

49
Q

Acceleration Limits - Symmetric Gear/Flaps (Gs)

A

0 to 2.5 Gs

50
Q

Acceleration Limits - Asymmetric Clean (Gs)

A

-1.0 to 4.7 Gs

51
Q

Acceleration Limits - Asymmetric Gear/Flaps (Gs)

A

0 to 2.0 Gs

52
Q

Intentional Spin Entry - Minimum Altitude for Entry

A

13,500 Feet MSL

53
Q

Intentional Spin Entry - Minimum Cloud Clearance

A

7000 Feet above clouds

54
Q

Icing - Maximum Icing Band/Icing type

A

5000 feet/ light rime

55
Q

Temperature - Ground operation is limited to ambient temperatures of

A

-23 to 43 Degrees celcius