T-6 Boldface and Ops Limits

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71 Terms

1
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Emergency Engine Shutdown on the Ground

PCL - OFF

FIREWALL SHUTOFF HANDLE - PULL

2
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Abort

PCL - IDLE

BRAKES - AS REQUIRED

3
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Engine Failure Immediately After Takeoff (Sufficient Runway Remaining Straight Ahead)

AIRSPEED - 110 KNOTS (MINIMUM)

PCL - AS REQUIRED

EMER LDG GR HANDLE - PULL (AS REQUIRED)

4
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Engine Failure During Flight

ZOOM/GLIDE - 125 KNOTS (MINIMUM)

PCL - OFF

INTERCEPT ELP

5
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Immediate Airstart (PMU NORM)

PCL - OFF

STARTER SWITCH - AUTO/RESET

PCL - IDLE, ABOVE 13% N1

6
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Uncommanded Power Changes / Loss of Power / Uncommanded Propeller Feather

PCL - MID RANGE

PMU SWITCH - OFF

PROP SYS CIRCUIT BREAKER (left front console) - PULL, IF Np STABLE BELOW 40%

7
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Inadvertent Departure From Controlled Flight

PCL - IDLE

CONTROLS - NEUTRAL

ALTITUDE - CHECK

8
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Fire in Flight, If Fire is Confirmed

PCL - OFF

FIREWALL SHUTOFF HANDLE - PULL

9
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PHYSIOLOGICAL SYMPTOMS

BOS PUSH MAN - PRESS ON

10
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OBOGS Failure / Overtemp / Physiological Symptoms/ OXY CRIT Annunciator

GREEN RING - PULL (AS REQUIRED)

DESCENT BELOW 10,000 FEET MSL - INITIATE

OBOGS SUPPLY LEVER - OFF (BOTH)

11
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Eject

EJECTION HANDLE - PULL

12
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Maximum Torque (Takeoff/Max): __________ %

100

13
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Maximum Torque (Transient): _____ % to____% _____ seconds

101, 107, 5

14
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Maximum Torque: Torque above ___________ % is indicative of a system malfunction.

107

15
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Maximum ITT: (Idle) _____ °C

750

16
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Maximum ITT: (Takeoff/Max) _____ °C

820

17
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Maximum ITT: (Transient) _____ to _°C (__ Seconds)

821, 870, 20

18
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N₁ Idle _____ to _____% Ground, ____% (Min) Flight

60, 61, 67

19
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Nₚ (Idle) ______ to ______ %

46, 50

20
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Nₚ (Takeoff/Max) ___ %(___%±__% PMU Off)

100, 100 ± 2

21
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Avoid stabilized ground operations from ____ to ____ % Nₚ

62, 80

22
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Oil Pressure (Takeoff/Max) _____ to _____ PSI

90, 120

23
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Oil Pressure (Aerobatics/Spins) _____ to _____ PSI

40, 130

24
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Oil Pressure (Aerobatics/Spins Idle) _____ to _____ PSI (___Sec)

15, 40, 5

25
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Oil Temp (Takeoff/Max) _____ to _____ °C

10, 105

26
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Oil Temp (Transient) _______to ________ °C (_______ Min)

106, 110, 10

27
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Maximum Fuel Flow All phases of flight ______ PPH

799

28
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Prohibited Maneuvers 1. _____________ Stalls

Inverted

29
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Prohibited Maneuvers 2. _____________ Spins

Inverted

30
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Prohibited Maneuvers 3. Aggravated __________________________________

spins past 2 turns

31
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Prohibited Maneuvers 4. Spins with the PCL __________________________________

above idle

32
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Prohibited Maneuvers 5. Spins with the _____________________extended

landing gear, flaps, speed brake

33
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Prohibited Maneuvers 6. Spins with the ____________________

PMU off

34
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Prohibited Maneuvers 7. Spins below ______________ feet pressure altitude

10,000

35
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Prohibited Maneuvers 8. Spins above ______22,000______ feet pressure altitude

22,000

36
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Prohibited Maneuvers 9. Abrupt ___________________________ maneuvers

cross-controlled (snap)

37
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10. Aerobatic maneuvers, spins, or stalls with greater than______________ pounds fuel imbalance

50

38
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Prohibited Maneuvers 11. __________ slides

Tail

39
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Airspeed Limitations: Max Airspeed Gear and/or Flaps __________ KIAS

150

40
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Airspeed Limitations: Max Operating Speed __________ KIAS or ___________ Mach

316, 0.67

41
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Airspeed Limitations: Full rudder deflection above __________ KIAS will exceed the limits of the rudder control system.

150

42
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Starting: Starter Limit _______ Seconds

20

43
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Starting: Wait ______

30 Sec, 2 min, 5 min, 30 min

44
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Maximum ITT _________ to __________ ⁰C for __________ Sec

871, 1000, 5

45
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Starting: Maximum Oil Pressure _______ PSI

200

46
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Starting: Minimum Oil Temperature _______ °C

-40

47
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Starting: Minimum Battery Voltage _______ V

23.5

48
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Pressurization: Normal above 18,000

3.6 ± 0.2

49
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Pressurization: Overpressurization Safety Valve Opens _________ PSI

4.0

50
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Fuel: Normal Recovery Fuel ___________ Pounds

200

51
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Fuel: Minimum Fuel _________ Pounds (_________ Pounds Solo)

150, 200

52
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Fuel: Emergency Fuel __________ Pounds

100

53
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Fuel: Minimum Fuel for Aerobatics ____________ Pounds per side

150

54
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Minimum Landing Distance Available (LDA) ___________Feet, or

Oil Temp heavy weight flaps ________ landing distance plus __________ Feet, whichever is greater

4,000, up, 500

55
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Minimum Runway Width _______ Feet

75

56
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Maximum Crosswinds: Dry Runway _________ Knots

25

57
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Maximum Crosswinds: Wet Runway _________ Knots

10

58
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Maximum Crosswinds: Icy Runway _________ Knots

5

59
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Maximum Crosswinds: Touch-and-Go _________ Knots

20

60
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Maximum Crosswinds: Formation Takeoff/Landing _________ Knots

15

61
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Maximum Crosswinds: Maximum Tailwind Component for Takeoff _________ Knots

10

62
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Maximum Crosswinds: Maximum Wind with Canopy Open _________ Knots

40

63
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Acceleration Limits: Symmetric Clean __________ to ___________ Gs

-3.5, 7.0

64
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Acceleration Limits: Symmetric Gear/Flaps __________ to ___________ Gs

0, 2.5

65
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Acceleration Limits: Asymmetric Clean __________ to ___________ Gs

-1.0, 4.7

66
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Acceleration Limits: Asymmetric Gear/Flaps __________ to ___________ Gs

0, 2.0

67
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Minimum Altitude for Entry _________ Feet MSL

13,500

68
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Minimum Cloud Clearance _________ Feet above clouds

7,000

69
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Maximum Icing Band ________ Feet

5,000

70
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Icing: Maximum Icing Type ___________

Light Rime

71
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Temperature: Ground operation is limited to ambient temperatures of _______ to _______ °C

-23, 43