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T-6 > Ops Limits > Flashcards

Ops Limits Flashcards

1
Q

Maximum Torque

A

Takeoff / Max 100%

Transient 132% (20 seconds)

Torque above 102% is indicative of engine system malfunction.

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2
Q

Maximum ITT

A

Idle 750°C

Takeoff / Max 820°C

Transient 821 to 870 °C (Up to 20 Seconds)

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3
Q

N1

A

Idle 60 to 61 %

Ground, 67% (Min) Flight

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4
Q

Np

A

Idle 46 to 50%

Takeoff / Max 100%, (100% +/- 2% PMU Off)

Avoid stabilized ground operations from 62 to 80% Np

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5
Q

Oil Pressure

A

Takeoff / Max 90 to 120 PSI

Aerobatics / Spins 40 to 130 PSI

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

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6
Q

Oil Temp

A

Takeoff / Max 10 to 105°C

Transient 106 to 110°C (10 Minutes)

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7
Q

__________ Stalls

A

Inverted

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8
Q

_________ Spins

A

Inverted

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9
Q

Aggravated ____________

A

Spins past 2 turns

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10
Q

Spins with the PCL __________

A

above idle

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11
Q

Spins with the ______, _______, or ________ extended.

A

Landing gear, flaps, or speed brake

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12
Q

Spins with the ________.

A

PMU off

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13
Q

Spins below _________ feet pressure altitude.

A

10,000

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14
Q

Spins above _________ feet pressure altitude.

A

22,000

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15
Q

Abrupt _________________ maneuvers.

A

Cross- controlled (snap)

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16
Q

Aerobatics maneuvers, spins, or stalls with greater than _____ pounds fuel imbalance.

A

50

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17
Q

__________ slides

A

Tail

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18
Q

Max airspeed year and / or flaps ______ KIAS

A

150

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19
Q

Max operating speed ______ KIAS or _____ Mach

A

316 or .67

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20
Q

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

A

150

21
Q

Starter limit: ______ Seconds

A

20

22
Q

Wait ____ Sec, _____ Min, _____ Min, _____ Min after each start / motoring attempt.

A

30, 2, 5, 30

23
Q

Maximum ITT _____ to _____ °C for ____ Sec ( Do not attempt Restart)

A

871 to 1000

24
Q

Maximum oil pressure _____ PSI

A

200

25
Q

Minimum oil temperature ______ °C

A

-40

26
Q

Minimum battery voltage ______ V

A

23.5

27
Q

Normal above 18,000 ft MSL ____ +/- _____ PSI

A

3.6 0.2

28
Q

Overpressurization safety valve opens ___ PSI

A

4.0

29
Q

Normal recovery fuel _____ pounds

A

200

30
Q

Minimum fuel _____ pounds (_____ pounds solo)

A

150 200

31
Q

Emergency fuel ________ pounds

A

100

32
Q

Minimum landing distance available (LDA) _________ feet or heavy weight flaps ____ landing distance plus ______ feet, whichever is greater.

A

150 200 100

33
Q

Minimum fuel for aerobatics _______ pounds per side

A

150

34
Q

Dry runway _____ knots

A

25

35
Q

Wet runway _____ knots

A

10

36
Q

Icy runways ______ knots

A

5

37
Q

Touch-and-go ____ knots

A

20

38
Q

Formation takeoff / landing ______ knots

A

15

39
Q

Maximum tailwind component for takeoff _____ knots

A

10

40
Q

Maximum wind with canopy open_____ knots

A

40

41
Q

Symmetric clean ______ to _______ Gs

A

-3.5 to 7.0

42
Q

Symmetric gear / flaps ______ to _____ Gs

A

0 to 2.5

43
Q

Asymmetric clean _____ to _____ Gs

A

-1.0 to 4.7

44
Q

Asymmetric gear / flaps ____ to _____ Gs

A

0 to 2.0

45
Q

Minimum altitude for entry ________ feet MSL

A

13,500

46
Q

Minimum cloud clearance _______ feet above the clouds

A

7,000

47
Q

Maximum icing band / icing type ______ feet / ___________.

A

5,000

Light rime

48
Q

Ground operation is limited to ambient temperatures of ______ to ______ °C

A

-23 to 43

T-6 (2 decks)

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