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T-6 Study Material > OPS Limits > Flashcards

OPS Limits Flashcards

1
Q

Takeoff/Max Torque

A

100

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2
Q

Max Transient Torque

A

132% for 20 sec

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3
Q

Torque above ____ % is indicative of a system malfunction.

A

102

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4
Q

Idle Max ITT

A

750 C

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5
Q

Take/Max ITT

A

820 C

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6
Q

Transient ITT Range + Time

A

821 C to 870 C for 20 sec

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7
Q

Idle N1

A

60 to 61% Ground, 67% in flight

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8
Q

Idle Np

A

46 to 50%

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9
Q

Takeoff/Max Np

A

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

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10
Q

Avoid stabilized ground ops from ___ to ___ Np.

A

62 to 80%

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11
Q

Takeoff/Max Oil PX

A

90 to 120 PSI

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12
Q

Aero/Spins Oil PX

A

40 to 130 PSI

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13
Q

Aero/Spins (idle) oil PX

A

15 to 40 PSI (5 sec)

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14
Q

Takeoff/Max Oil Temp

A

10 to 105 C

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15
Q

Transient Oil Temp

A

106 to 110 C (10 Sec)

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16
Q

Maximum fuel Flow all phases of flight

A

799 PPH

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17
Q

Prohibited maneuvers

A
  1. Inverted Stalls
  2. Inverted Spins
  3. Aggravated spins past 2 turns
  4. Spins with PCL above idle
  5. Spins with the flaps, landing gear, or speed brake extended
  6. Spins with the PMU off.
  7. Spins below 10,000 feet pressure altitude
  8. Spins above 22,000 feet pressure altitude
  9. Abrupt cross-controlled(snap) maneuvers
  10. Aero maneuvers, spins, or stalls with greater then 50 lbs fuel imbalance.
  11. Tail Slides
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18
Q

Max airspeed gear/flaps

A

150 kias

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19
Q

Max operating speed

A

316 kias or .67 mach

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20
Q

Full rudder deflection above __ will exceed the limits of the rudder control system

A

150 kias

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21
Q

Starter limit:

A

20 sec

22
Q

Wait ___, ___, ___, ___, after each start/motoring attempt

A

30 sec, 2 min, 5 min, 30 min

23
Q

Max ITT ___ to ___ C for ___ sec
(Do not attempt restart)

A

871 to 1000 C for 5 sec

24
Q

Max oil PX at start

A

200 PSI

25
Q

Minimum Oil Temp at start

A

-40 C

26
Q

Minimum battery voltage at start

A

23.5 V

27
Q

Normal Pressurization above 18,000 ft msl

A

3.6 +/- 0.2 PSI

28
Q

Over pressurization Safety valve opens

A

4.0 PSI

29
Q

Normal Recovery Fuel

A

200 lbs

30
Q

Minimum fuel

A

150 lbs

31
Q

Minimum fuel Solo

A

200 lbs

32
Q

Emergency fuel

A

100 lbs

33
Q

Minimum fuel for Aero

A

150 lbs per side

34
Q

Minimum landing distance available ___ft or heavy weight flaps __ landing dist plus ___ ft + (_______)

A

4000ft , up , 500 ft +
(Whichever is greater)

35
Q

Minimum runway width

A

75 ft

36
Q

Max crosswinds Dry

A

25 kts

37
Q

Max crosswinds Wet

A

10 kt

38
Q

Max crosswinds Icy

A

5 kt

39
Q

Max crosswinds Touch and Go

A

20 kt

40
Q

Max crosswinds formation t/o or ldg

A

15 kt

41
Q

Max tailwind component for t/o

A

10 kt

42
Q

Max wind with canopy open

A

40 kt

43
Q

Acceleration limits symmetric clean

A

-3.5 to 7.0 Gs

44
Q

Acceleration limits Symmetric Gear/Flaps

A

0 to 2.5 Gs

45
Q

Acceleration limits Asymmetric clean

A

-1 to 4.7 Gs

46
Q

Acceleration limits Asymmetric Gear/Flaps

A

0 to 2.0 Gs

47
Q

Minimum altitude for intentional spin entry

A

13,500 ft msl

48
Q

Minimum cloud clearance for spin entry ___ ft above clouds

A

7,000 ft

49
Q

Max icing band

A

5,000 ft

50
Q

Max icing type

A

Light rime

51
Q

Ground ops is limited to ambient temperatures of

A

-23 to 43 C

T-6 Study Material (6 decks)

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