Boldface Ops Limits Flashcards

1
Q

Engine Fire During Ground OperationS

A

THROTTLES - CUTOFF

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2
Q

Engine Fire During Flight

If engine fire switchlight remains illuminated, L or R FIRE DET FAIL illuminates, fire warning test fails, or fire conditions persist:

A

THROTTLE IDLE

THROTTLE - CUTOFF
ENGINE FIRE SWITCH - PUSH
BOTTLE ARMED SWITCH - PUSH

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3
Q

Smoke Or Fumes In Aircraft

A

OXYGEN MASKS - DON / 100%

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4
Q

Pitch Trim/Roll Trim/Rudder Trim Runaway

A

TRIM INT & A/P DISENGAGE SWITCH - PUSH AND HOLD

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5
Q

Low Cabin Pressure

A

OXYGEN MASKS - DON / 100%

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6
Q

Engine:
Thrust Setting: Takeoff
Time Limit (Minutes):

A

5 (1)

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7
Q

Engine:
Thrust Setting: Maximum Continuous
Time Limit (Minutes):

A

Continuous

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8
Q

Engine:
Thrust Setting: Idle
Time Limit (Minutes):

A

Continuous

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9
Q

Engine:
Thrust Setting: Takeoff
Maximum Observed ITT degrees C:

A

700

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10
Q

Engine:
Thrust Setting: Maximum Continuous
Maximum Observed ITT degrees C:

A

680

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11
Q

Engine:
Thrust Setting: Idle
Maximum Observed ITT degrees C:

A

580

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12
Q

Engine:
Thrust Setting: Starting (4)
Maximum Observed ITT degrees C:

A

550 - 600 4 SEC
600 - 700 2 SEC
700 - 720 1 SEC

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13
Q

Engine:
Thrust Setting: Transient
Maximum Observed ITT degrees C:

A

(720 2 SEC Max)

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14
Q

Engine:
Thrust Setting: Takeoff
N2%:

A

96

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15
Q

Engine:
Thrust Setting: Miximum Continuous
N2%:

A

96

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16
Q

Engine:
Thrust Setting: Idle
N2%:

A

52 (Min)

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17
Q

Engine:
Thrust Setting: Transient
N2%:

A

96

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18
Q

Engine:
Thrust Setting: Takeoff
N1%:

A

104

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19
Q

Engine:
Thrust Setting: Maximum Continuous
N1%:

A

104

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20
Q

Engine:
Thrust Setting: Transient
N1%:

A

106

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21
Q

Engine:
Thrust Setting: Takeoff
Oil Pressure (2) PSI:

A

60 to 83

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22
Q

Engine:
Thrust Setting: Maximum Continuous
Oil Pressure (2) PSI:

A

60 to 83

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23
Q

Engine:
Thrust Setting: Idle
Oil Pressure (2) PSI:

A

40 (Min)

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24
Q

Engine:
Thrust Setting: Transient
Oil Pressure (2) PSI:

A

95 for 90 SEC

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25
Q

Engine:
Thrust Setting: Takeoff
OilTemperature (degrees C):

A

10 to 121

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26
Q

Engine:
Thrust Setting: Maximum Continuous
OilTemperature (degrees C):

A

10 to 121

27
Q

Engine:
Thrust Setting: Idle
OilTemperature (degrees C):

A

-40 to 121

28
Q

Engine:
Thrust Setting: Starting
OilTemperature (degrees C):

A

-40 (Min)

29
Q

Engine:
Thrust Setting: Transient
OilTemperature (degrees C):

A

135 (Max) (15 MIN Max)

30
Q

(2) Normal Flight: Normal oil pressure is ___ to ___ PSI at N2 speeds above ___%. Oil pressure below ___ PSIis undesirable and should be tolerated only for the safe recovery of the flight, preferably at reduced power setting. Oil Pressure below ___ PSI is unsafe.

A
60
83
60
60
40
31
Q

(3) Under cold starting conditions, oil pressure between ___ PSI and ___ PSI is limited to ___ seconds.

A

83
95
90

32
Q

(4) The ITT during ground starts should normally not exceed ___ degrees C.

A

550

33
Q

Normal hydraulic pressure ___ to ___ PSI

A

1350 to 1550

34
Q

Normal nitrogen pressure ___ to ___ PSI

A

1350 to 1650

35
Q

Normal oxygen pressure ___ to ___ PSI

A

1600 to 1850

36
Q

Min battery voltage for battery start ___ volts

A

22

37
Q

Max gen load prior to starting second engine ___ amps

A

150

38
Q

Motoring of the starter is limited to:
First, ___ seconds then ___ minutes cooling.
Second, ___ seconds then ___ minutes cooling.
Third, ___ seconds then ___ minutes cooling.

A

30 5
30 15
30 60

39
Q

Emergency Fuel / Minimum Fuel ___ lbs / ___ lbs

A

300 / 500

40
Q

Maximum Fuel Imbalance - T.O./Touch & Go ___ lbs

A

100

41
Q

Max Fuel Imbalance - Flight ___ lbs

A

300

42
Q

Max Fuel Imbalance - Landing ___ lbs

A

300

43
Q

Fuel crossfeed with 2 engines operating is limited to level flight with less than ___ lbs of fuel remains in the wing tank supplying fuel.

A

600

44
Q

Max Ramp Weight ___ lbs

A

16,300

45
Q

Max Takeoff Weight ___ lbs

A

16,100

46
Q

Max Landing Wieght ___ lbs

A

15,700

47
Q

Extend flaps to 10 degrees ___ KIAS

A

200

48
Q

Extend flaps >10 degrees ___ KIAS

A

170

49
Q

Flaps extended > 10 degrees ___ KIAS

A

165

50
Q

Aircraft if limited to ___ KIAS or ___ MACH, whichever is less

A

330 .78

51
Q

Landing Gear/Lights ___ KIAS / FL ___

A

200 200

52
Q

Wipers ___ KIAS

A

200

53
Q

Tire ___ Knots GS

A

165

54
Q

Max Tailwind ___ Knots

A

10

55
Q

Max Crosswind (Dry)___ Knots

A

25

56
Q

Max Crosswind (Wet)___ Knots

A

15

57
Q

Max Crosswind (Icy)___ Knots

A

10

58
Q

Max Operating Altitude FL ___

A

410

59
Q

Yaw Damper required operable for flight above FL ___

A

280

60
Q

Do not use autopilot below ___ FT AGL

A

200

61
Q

Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above ___ degrees C OAT/SAT

A

10

62
Q

Do not operate surface anti-ice systems in flight at ram air temperatures above ___ degrees C.

A

10

63
Q

To ensure proper wing anti-ice operations, the throttles must be kept at ___% N2 minimum.

A

70