Ops Limits Flashcards

1
Q

Takeoff Thrust Time Limit

A

5 Minutes

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2
Q

Takeoff Thrust Maximum Observed ITT (C)

A

700

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3
Q

Takeoff Thrust N2 (%)

A

96

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4
Q

Takeoff Thrust N1 (%)

A

104

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5
Q

Takeoff Thrust Oil Pressure (PSI)

A

60 to 83

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6
Q

Takeoff Thrsut Oil Temperature (C)

A

10 to 121

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7
Q

Maximum Continuous Thrust Time Limit

A

Continuous

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8
Q

Maximum Continuous Thrust Max Obesebed ITT (C)

A

680

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9
Q

Maximum Continuous Thrust N2 (%)

A

96

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10
Q

Maximum Continuous Thrust N1 (%)

A

104

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11
Q

Maximum Continuous Thrust Oil Pressure (PSI)

A

60 to 83

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12
Q

Maximum Continuous Oil Temperature (C)

A

10 to 121

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13
Q

Idle Thrust Time Limit

A

Continuous

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14
Q

Idle Thrust Max Observed ITT (C)

A

580

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15
Q

Idle Thrust N2 (%)

A

52 (min)

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16
Q

Idle Thrust Oil Pressure (PSI)

A

40 (min)

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17
Q

Idle Thrust Oil Temperature (C)

A

-40 to 121

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18
Q

Starting Max Observed ITT (C)

A

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

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19
Q

Starting Oil Temperature (C)

A

-40 (min)

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20
Q

Transient Max Observed ITT (C)

A

720 (2 SEC Max)

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21
Q

Transient N2 (%)

A

96

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22
Q

Transient N1 (%)

A

106

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23
Q

Transient Oil Pressure (PSI)

A

95 for 90 SEC

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24
Q

Transient Oil Temp (C)

A

135 (MAX) (15 MIN MAX)

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25
Q

Normal Oil Pressure Range

A

60 to 83 PSI at N2 speeds above 60%

26
Q

Undesireable Oil Pressure

A

Below 60 PSI

27
Q

Unsafe Oil Pressure

A

40 PSI

28
Q

Cold Starting Oil Pressure

A

83 to 95 PSI (90 SEC)

29
Q

Ground Start Normal ITT Limit

A

550 C

30
Q

Normal Hydraulic Pressure

A

1350 to 1550 PSI

31
Q

Normal Nitrogen Pressure

A

1350 to 1650 PSI

32
Q

Normal Oxygen Pressure

A

1600 to 1850 PSI

33
Q

Minimum Battery Voltage for battery start

A

22 Volts

34
Q

Max Gen Load Prior to Starting Second Engine

A

150 Amps

35
Q

Motoring Starter Limits

A

First, 30 Seconds then 5 minutes cooling
Second, 30 seconds then 15 minutes cooling
Thirst, 30 seconds, then 60 minutes cooling

36
Q

Emergency Fuel

A

300 lbs

37
Q

Min Fuel

A

500 lbs

38
Q

Max Fuel Imabalance T.O. / Touch and Go

A

100 lbs

39
Q

Max Fuel Imbalance - Flight

A

300 lbs

40
Q

Max Fuel Imbalance - Landing

A

300 lbs

41
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

42
Q

Max Ramp Weight

A

16,300 lbs

43
Q

Max Takeoff Weight

A

16,100 lbs

44
Q

Max Landing Weight

A

15,700 lbs

45
Q

Extend flaps to 10 degrees

A

200 KIAS

46
Q

Extend Flaps > 10 Degrees

A

170 KIAS

47
Q

Flaps extended > 10 degrees

A

165 KIAS

48
Q

Aircraft speed limit

A

330 KIAS or .78 MACH, whichever is less

49
Q

Landing Gear/Lights Max Speed and Altitude

A

200 KIAS / FL 200

50
Q

Wipers Max Airspeed

A

200 KIAS

51
Q

Tire Max Ground Speed

A

165 Knots GS

52
Q

Max Tailwind

A

10 Knots

53
Q

Max Crosswind (Dry)

A

25 knots

54
Q

Max Crosswind (Wet)

A

15 knots

55
Q

Max Crosswind (Icy)

A

10 knots

56
Q

Max Operating Altitude

A

FL 410

57
Q

Yam Damper required operable for flight above___

A

FL 280

58
Q

Do not use autopilot below ___

A

200 FT AGL

59
Q

Anti-ice systems Ground Ops Max Temperature

A

10 C

60
Q

Anti-ice systems in flight max Ram Air Temp

A

10 C

61
Q

Proper Wing Anti-Ice operation minimum N2

A

70%