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T-6A Texan II > Boldface and Ops Limits > Flashcards

Boldface and Ops Limits Flashcards

1
Q

Emergency Engine Shutdown on the Ground

A

PCL - OFF

FIREWALL SHUTOFF HANDLE - PULL

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2
Q

Abort

A

PCL - IDLE

BRAKES - AS REQUIRED

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3
Q

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

A

AIRSPEED - 110 KNOTS (MINIMUM)
PCL - AS REQUIRED
EMER LDG GR HANDLE - PULL (AS REQUIRED)

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4
Q

Engine Failure During Flight

A

ZOOM/GLIDE - 125 KNOTS (MINIMUM)
PCL - OFF
INTERCEPT ELP

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5
Q

Immediate Airstart (PMU NORM)

A

PCL - OFF
STARTER SWITCH - AUTO/RESET
PCL - IDLE, ABOVE 13% N1

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6
Q

Uncommanded Power Changes / Loss of Power / Uncommanded Propeller Feather

A

PCL - MID RANGE
PMU SWITCH - OFF
PROP SYS CIRCUIT BREAKER (left front console) - PULL, IF Np STABLE BELOW 40%

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7
Q

Inadvertent Departure From Controlled Flight

A

PCL - IDLE
CONTROLS - NEUTRAL
ALTITUDE - CHECK

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8
Q

Fire in Flight

A

PCL - OFF

FIREWALL SHUTOFF HANDLE - PULL

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9
Q

OBOGS Inoperative

A

GREEN RING - PULL (AS REQUIRED)

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10
Q

Eject

A

EJECTION HANDLE - PULL

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11
Q

Takeoff / Max Torque

A

100%

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12
Q

Transient Torque

A

131%, 20 seconds

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13
Q

Torque above ____ is indicative of a system malfunciton

A

102%

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14
Q

Maximum Idle ITT

A

750 C

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15
Q

Maximum Takeoff ITT

A

820 C

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16
Q

Maximum Transient ITT

A

870 C, 20 seconds

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17
Q

Idle N1 Range

A

60-61%

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18
Q

Ground N1 Min for Flight

A

67%

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19
Q

Idle Np

A

46-50%

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20
Q

Takeoff / Max Np

A

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

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21
Q

Avoid stabilized ground ops

A

62-80%

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22
Q

Takeoff Oil Pressure

A

90-120 psi

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23
Q

Aerobatics / Spins Oil Pressure

A

40-130 psi

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24
Q

Aerobatics / Spins (IDLE) Oil Pressure

A

15-40 psi for 5 sec

25
Q

Takeoff / Max Oil Temp

26
Q

Transient Oil Temp

A

106-110 C for 10 min

27
Q

Prohibited Maneuvers

A

Inverted Stalls
Inverted Spins
Aggravated spins past 2 turns
Spins with the PCL above idle
Spins with the landing gear, flaps, or speed brake extended
Spins with the PMU off
Spins below 10,000 feet pressure altitude
Spins above 22,000 feet pressure altitude
Abrupt cross-controlled (snap) maneuvers
Aerobatic maneuvers, spins, or stalls with greater than 50 pounds fuel imbalance
Tail slides

28
Q

Max Airspeed Gear and/or Flaps

29
Q

Max Operating Speed

A

316 KIAS or 0.67 Mach

30
Q

Full Rudder Deflection above ____ will exceed the limits of rudder control system

31
Q

Starter Limit

A

20 seconds

32
Q

Wait ____ after each start attempt

A

30 sec, 2 min, 5 min, 30 min

33
Q

Maximum Starting ITT

A

1,000 C for 5 sec

34
Q

Maximum Starting Oil Pressure

35
Q

Minimum Starting Oil Temperature

36
Q

Minimum Starting Battery Voltage

37
Q

Normal Pressurization above 18,000 ft MSL

A

3.6 +/- 0.2 psi

38
Q

Overpressurization Valve Opens

39
Q

Normal Recovery Fuel

A

200 pounds

40
Q

Minimum Fuel (Solo)

A

150 pounds (200 pounds solo)

41
Q

Emergency Fuel (Solo)

A

100 pounds (100 pounds solo)

42
Q

Minimum Fuel for Aerobatics

A

150 pounds per side

43
Q

Minimum Runway Length

A

4,000 feet

44
Q

Minimum Runway Width

45
Q

Max Dry Crosswinds

46
Q

Max Wet Crosswinds

47
Q

Max Icy Crosswinds

48
Q

Max Touch-and-Go Crosswinds

49
Q

Max Formation Takeoff/Landing Crosswinds

50
Q

Max Tailwind for Takeoff

51
Q

Max Wind with Canopy Open

52
Q

Symmetric Clean Acceleration

A

-3.5 to 7.0 Gs

53
Q

Symmetric Gear/Flaps Acceleration

A

0 to 2.5 Gs

54
Q

Asymmetric Clean Acceleration

A

-1.0 to 4.7 Gs

55
Q

Asymmetric Gear/Flaps Acceleration

A

0 to 2.0 Gs

56
Q

Minimum Altitude for Spin Entry

A

13,500 feet MSL

57
Q

Minimum Cloud Clearance for Spin Entry

A

7,000 feet above clouds

58
Q

Maximum Icing Band/Type

A

5,000 feet / light rime

59
Q

Ground Ops Ambient Temperature Limits

A

-23 to 43 C

T-6A Texan II (1 decks)

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