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T-6 BOLDFACE/Ops Limits > Ops Limits > Flashcards

Ops Limits Flashcards

1
Q

Maximum Torque: Takeoff/Max:

A

100%

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2
Q

Transient Max Torque

A

101-107% (5 Seconds)

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3
Q

Torque above ______ is indicative of a system malfunction

A

107%

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4
Q

Max ITT @ Idle (deg Celcius)

A

760 C

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5
Q

Max ITT @ Takeoff/Max

A

820 C

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6
Q

Max ITT Transient

A

821 - 870 C (20 Seconds)

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7
Q

N1 Idle on Ground

A

60-61%

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8
Q

N1 Min in Flight

A

67% (Min) Flight

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9
Q

Np @ Idle

A

46-50%

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10
Q

Np Takeoff / Max

A

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

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11
Q

Avoid stabilized ground ops from _____ to ____ % Np

A

62-80%

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12
Q

Oil Pressure Takeoff/Max

A

90-120 PSI

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13
Q

Oil Pressure Aerobatics/Spins

A

40-130 PSI

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14
Q

Oil Pressure Aerobatics/Spins (Idle)

A

15-40 PSI (5 seconds)

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15
Q

Oil Temp Takeoff/Max

A

10-105 C

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16
Q

Oil Temp Transient

A

106-110 C (10 Min)

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17
Q

Max fuel Flow All Phases of Flight

A

799 PPH

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18
Q

Prohibited Stalls

A

Inverted

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19
Q

Prohibited Spins

A

Inverted

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20
Q

Prohibited Aggravated __________

A

Spins past 2 turns

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21
Q

Spins prohibited with the PCL ___________________

A

Above idle

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22
Q

Spins prohibited with _________, _________, or _________ extended

A

landing gear, flaps, or speed brake

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23
Q

Spins prohibited with the _______________

A

PMU off

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24
Q

Spins prohibited below _________ feet pressure altitude

A

10,000

25
Q

Spins prohibited above _________ feet pressure altitude

A

22,000

26
Q

Abrupt __________________ maneuvers are prohibited

A

cross-controlled (snap)

27
Q

Aerobatic maneuvers, spins, or stalls with greater than _________ pounds fuel imbalance

A

50

28
Q

___________ slides prohibited

A

Tail

29
Q

Max Airspeed Gear and/or Flaps _______ KIAS

A

150

30
Q

Max Operating Speed _______ KIAS or ______ Mach

A

316 KIAS or 0.67 Mach

31
Q

Full rudder deflection above ______ KIAS will exceed the limits of the rudder control system

A

150

32
Q

Starter Limit (seconds)

A

20

33
Q

Wait _____ Sec, ______ Min, ______ Min, _______ Min after each start/motoring attempt

A

30, 2, 5, 30

34
Q

Maximum ITT (degrees C) for _________ Sec (Do not attempt restart)

A

871 to 1,000 C for 5 Sec

35
Q

Maximum Starting Oil Pressure ___________ PSI

A

200

36
Q

Minimum Starting Oil Temp

A

-40 C

37
Q

Minimum Starting Battery Voltage ______ V

A

23.5

38
Q

Normal Recovery Fuel _____ Pounds

A

200

39
Q

Minimum Fuel Duel (Pounds)

A

150

40
Q

Minimum Fuel Solo (Pounds)

A

200

41
Q

Emergency Fuel (Pounds)

A

100

42
Q

Min Fuel for Aerobatics: ________ pounds per side

A

150

43
Q

Minimum Landing Distance Available (LDA)_____Feet, or heavy flaps _____ landing distance plus ______ feet, whichever is greater

A

4,000 ft, up, 500

44
Q

Minimum Runway Width

A

75 Feet

45
Q

Max Crosswinds Dry Runway

A

25 Knots

46
Q

Max Crosswinds Wet Runway

A

10 Knots

47
Q

Max Crosswinds Icy Runway

A

5 Knots

48
Q

Max Crosswinds Touch-and-Go

A

20 Knots

49
Q

Max Tailwind Component for Takeoff

A

10 Knots

50
Q

Acceleration Limit Symmetric Clean ______ to ______ Gs

A

-3.5 to 7.0

51
Q

Acceleration Limit Symmetric Gear / Flaps ______ to ______ Gs

A

0 to 2.5 Gs

52
Q

Acceleration Limit asymmetric Clean ______ to ______ Gs

A

-1.0 to 4.7 Gs

53
Q

Acceleration Limit asymmetric Gear/Flaps ______ to ______ Gs

A

0 to 2.0 Gs

54
Q

Intentional Spin Entry - Minimum Altitude for Entry _________ Feet MSL

A

13,500

55
Q

Intentional Spin Entry - Minimum Cloud Clearance ________ Feet above clouds

A

7,000

56
Q

Maximum Icing Band (Feet)

A

5,000 ft

57
Q

Maximum Icing Type

A

Light rime

58
Q

Ground Operation Limited to Ambient Temps of ______ to ______ C

A

-23 to 43 C

T-6 BOLDFACE/Ops Limits (2 decks)

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