Ops Limits Flashcards

1
Q

Thrust Setting: Takeoff: Time Limit

A

5 (1) Time limit starts when throttles first advanced for takeoff thrust

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2
Q

Thrust Setting: Takeoff: Maximum Observed ITT

A

700

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3
Q

Thrust Setting: Takeoff: N2 %

A

96

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4
Q

Thrust Setting: Takeoff: N1 %

A

104

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5
Q

Thrust Setting: Takeoff: Oil Pressure (PSI)

A

60 to 83

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6
Q

Thrust Setting: Takeoff: Oil Temperature (C)

A

10 to 121

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7
Q

Thrust Setting: Max Continuous: Time Limit

A

Continuous

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8
Q

Thrust Setting: Max Continuous: Max Observed ITT (C)

A

680

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9
Q

Thrust Setting: Max Continuous: N2 %

A

96

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10
Q

Thrust Setting: Max Continuous: N1 %

A

104

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11
Q

Thrust Setting: Max Continuous: Oil Pressure (PSI)

A

60 to 83

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12
Q

Thrust Setting: Max Continuous: Oil Temp (C)

A

10 to 121

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13
Q

Thrust Setting: Idle: Time Limit

A

Continuous

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14
Q

Thrust Setting: Idle: Max Observed ITT (C)

A

580

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15
Q

Thrust Setting: Idle: N2 %

A

52 (Min)

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16
Q

Thrust Setting: Idle: Oil Pressure (PSI)

A

40 (Min)

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17
Q

Thrust Setting: Idle: Oil Temperature (C)

A

-40 to 121

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18
Q

Thrust Setting: Starting: Max Observed ITT (C)

A

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

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19
Q

Thrust Setting: Starting: Oil Temperature (C)

A

-40 (Min)

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20
Q

Thrust Setting: Transient: Max Observed ITT (C)

A

(720 2 SEC Max)

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21
Q

Thrust Setting: Transient: N2 %

A

96

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22
Q

Thrust Setting: Transient: N1 %

A

106

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23
Q

Thrust Setting: Transient: Oil Pressure (PSI)

A

95 for 90 SEC

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24
Q

Thrust Setting: Transient: Oil Temperature (C)

A

135 (Max)

15 MIN Max

25
Q

Normal flight: Normal oil pressure is…

A

60 to 83 PSI at N2 speeds above 60%.

26
Q

Oil pressure below ___ PSI is undesirable and …

A

60 PSI; … should be tolerated only for the safe recovery of the flight.

27
Q

Oil pressure between ___ PSI and ___ PSI is limited to ___ 90 seconds.

A

83; 95; 90

28
Q

The ITT during ground starts should normally not exceed ___ C

A

550

29
Q

Normal hydraulic pressure

A

1350 to 1550 PSI

30
Q

Normal nitrogen pressure

A

1350 to 1650 PSI

31
Q

Normal oxygen pressure

A

1600 to 1850 PSI

32
Q

Min battery voltage for battery start

A

22 volts

33
Q

Max gen load prior to starting second engine

A

150 amps

34
Q

Motoring of the starter is limited to:

A

First, 30 seconds then 5 minutes cooling.
Second, 30 seconds then 15 minutes cooling.
Third, 30 seconds then 60 minutes of cooling.

35
Q

Emergency fuel / Minimum Fuel

A

300 lbs / 500 lbs

36
Q

Max Fuel Imbalance - T.O./Touch & Go

A

100 lbs

37
Q

Max Fuel Imbalance - Flight

A

300 lbs

38
Q

Max Fuel Imbalance - Landing

A

300 lbs

39
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

40
Q

Max Ramp Weight

A

16,300 lbs

41
Q

Max Takeoff Weight

A

16,100 lbs

42
Q

Max Landing Weight

A

15,700 lbs

43
Q

Extend flaps to 10 degrees

A

200 KIAS

44
Q

Extend flaps > 10 degrees

A

170 KIAS

45
Q

Flaps extended > 10 degrees

A

165 KIAS

46
Q

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

A

330; .78

47
Q

Landing Gear/Lights ___ KIAS / FL ___

A

200; 200

48
Q

Wipers

A

200 KIAS

49
Q

Tire

A

165 Knots GS

50
Q

Max Tailwind

A

10 Knots

51
Q

Max Crosswind (Dry)

A

25 Knots

52
Q

Max Crosswind (Wet)

A

15 Knots

53
Q

Max Crosswind (Icy)

A

10 Knots

54
Q

Max Operating Altitude

A

FL410

55
Q

Yaw Damper required operable for flight above

A

FL280

56
Q

Do not use autopilot below ___ FT AGL

A

200

57
Q

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

A

10

58
Q

Do not operate surface anti-ice systems in flight at ram air temperatures above __ (C)

A

10

59
Q

To ensure proper wing anti-ice operation, the throttles must be kept at __ % N2 minimum

A

70