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 - OFF
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 - 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 Failure/ Overtemp/ Physio Symptoms

A

GREEN RING - PULL (AS REQUIRED)
DESCENT BELOW 10,000 FEET MSL - INITIATE
OBOGS SUPPLY LEVER - OFF

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10
Q

Eject

A

EJECTION HANDLE - PULL

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11
Q

Maximum Torque
Takeoff/Max ______%

A

100

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12
Q

Maximum Torque
Transient _________% (_____ Seconds)

A

132, 20

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13
Q

Maximum Torque
Torque above ___% is indicative of sys malfunction

A

102

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14
Q

Maximum ITT
Idle ____ *C

A

750

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15
Q

Maximum ITT
Takeoff/Max ___*C

A

820

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16
Q

Maximum ITT
Transient ___ to ___ *C (___ Seconds)

A

821, 870, 20

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17
Q

N1
Idle ___ to ___% Ground, ___% (Min) Flight

A

60, 61, 67

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18
Q

NP
Idle ___ to ___%

A

46, 50

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19
Q

NP
Takeoff/Max ___%,(___% +/- ___% PMU off)

A

100, 100, 2

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20
Q

NP
Avoid stabilized ground operations from ___ to ___ % Np

A

62, 80

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21
Q

Oil Pressure
Takeoff/ Max ___ to ___ PSI

A

90, 120

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22
Q

Oil Pressure
Aerobatics/Spins ___ to ___ PSI

A

40, 130

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23
Q

Oil Pressure
Aerobatics/Spins (Idle) ___ to ___ PSI (___ Sec)

A

15, 40, 5

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24
Q

Oil Temp
Takeoff/Max ___ to ___ *C

A

10, 105

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25
Q

Oil Temp
Transient ___ to ___ *C (___ Min)

A

106, 110, 10

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26
Q

All phases of flight ___ PPH

A

799

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27
Q
  1. _________ Stalls
A

Inverted

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28
Q
  1. _________ Spins
A

Inverted

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29
Q
  1. Aggravated ___________________
A

spins past 2 turns

30
Q
  1. Spins with the PCL ____________
A

above idle

31
Q
  1. Spins with the _______,_______, or ______ extended
A

landing gear, flaps, speed brake

32
Q
  1. Spins with the _________
A

PMU off

33
Q
  1. Spins below _______ feet pressure altitude
A

10,000

34
Q
  1. Spins above ________ feet pressure altitude
A

22,000

35
Q
  1. Abrupt _________ maneuvers
A

cross-controlled (snap)

36
Q
  1. Aerobatic maneuvers, spins, or stalls with greater than _____ pounds fuel imbalance
A

50

37
Q
  1. _______ Slides
A

Tail

38
Q

Max airspeed Gear and/or Flaps _______KIAS

A

150

39
Q

Max operating Speed _______KIAS or ________ mach

A

316, 0.67

40
Q

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

A

150

41
Q

Starter limit: ______ Seconds

A

20

42
Q

Wait ___ Sec, ___ Min, ___Min, ___ Min after each start/motoring attempt

A

30, 2, 5, 30

43
Q

Maximum ITT___ to ___ *C for ___ Sec (Do not Attempt Restart)

A

871, 1,000, 5

44
Q

Maximum Oil Pressure ___ PSI

A

200

45
Q

Minimum Oil Temperature ___ *C

A

-40

46
Q

Minimum Batter Voltage ___V

A

23.5

47
Q

Normal Above 18,000 Ft MSL ___ +/- ___ PSI

A

3.6, 0.2

48
Q

Overpressurization Safety Valve Opens ___ PSI

A

4.0

49
Q

Normal Recovery Fuel ___ Pounds

A

200

50
Q

Minimum Fuel ___ Pounds (___ Pounds Solo)

A

150, 200

51
Q

Emergency Fuel ____ Pounds

A

100

52
Q

Minimum Fuel for Aerobatics ___ Pounds per side

A

150

53
Q

Minimum landing distance available (LDA) ___ feet, or heavy weight flaps ___ landing distance plus ___ feet, whichever is greater

A

4,000, up, 500

54
Q

Minimum Runway width ____ Feet

A

75

55
Q

Maximum Crosswinds
Dry Runway ___ Knots

A

25

56
Q

Maximum Crosswinds
Wet Runway ___ Knots

A

10

57
Q

Maximum Crosswinds
Icy Runway ___ Knots

A

5

58
Q

Maximum Crosswinds
Touch and Go ___ Knots

A

20

59
Q

Maximum Crosswinds
Formation Takeoff/ Landing ___ Knots

A

15

60
Q

Maximum Crosswinds
Maximum tailwind component for takeoff ___ knots

A

10

61
Q

Maximum wind with canopy open ___ Knots

A

40

62
Q

Symmetric clean ___ to ___ Gs

A

-3.5, 7.0

63
Q

Symmetric Gear/ Flaps ___ to ___ Gs

A

0, 2.5

64
Q

Asymmetric Clean ___ to ___ Gs

A

-1.0, 4.7

65
Q

Asymmetric Gear/Flaps ___ to ___ Gs

A

0, 2.0

66
Q

Minimum altitude for entry ____ Feet MSL

A

13,500

67
Q

Minimum cloud clearance ____ feet above clouds

A

7,000

68
Q

Maximum Icing Band ____ Feet

A

5,000

69
Q

Maximum Icing type ____

A

Light Rime

70
Q

Ground Operation is limited to ambient temperatures of ___ to ___ *C

A

-23, 43