OPS LIMITS Flashcards

1
Q

Time Limit (Minutes)
Takeoff Thrust Setting

A

5

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2
Q

Time Limit (Minutes)
Maximum Continuous Thrust Setting

A

Continuous

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3
Q

Time Limit (Minutes)
Idle Thrust Setting

A

Continuous

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4
Q

Maximum Observed ITT *C
Takeoff Thrust Setting

A

700

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5
Q

Maximum Observed ITT *C
Maximum Continuous Thrust Setting

A

680

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6
Q

Maximum Observed ITT *C
Idle Thrust Setting

A

580

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7
Q

Maximum Observed ITT *C
Starting Thrust Setting

A

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

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8
Q

Maximum Observed ITT *C
Transient Thrust Setting

A

720 2 SEC Max

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9
Q

N2%
Takeoff Thrust Setting

A

96

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10
Q

N2%
Maximum Continuous Thrust Setting

A

96

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11
Q

N2%
Idle Thrust Setting (Min)

A

52

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12
Q

N2%
Transient Thrust Setting

A

96

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13
Q

N1%
Takeoff Thrust Setting

A

104

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14
Q

N1%
Maximum Continuous Thrust Setting

A

104

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15
Q

N1%
Transient Thrust Setting

A

106

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16
Q

Oil Pressure PSI
Takeoff Thrust Setting

A

60 to 83

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17
Q

Oil Pressure PSI
Maximum Continuous Thrust Setting

A

60 to 83

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18
Q

Oil Pressure PSI
Idle Thrust Setting (Min)

A

40

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19
Q

Oil Pressure PSI
Transient Thrust Setting

A

95 for 90 SEC

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20
Q

Oil Temperature (*C)
Takeoff Thrust Setting

A

10 to 121

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21
Q

Oil Temperature (*C)
Maximum Continuous Thrust Setting

A

10 to 121

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22
Q

Oil Temperature (*C)
Idle Thrust Setting

A

-40 to 121

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23
Q

Oil Temperature (*C)
Starting Thrust Setting (Min)

A

-40

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24
Q

Oil Temperature (*C)
Transient Thrust Setting

A

135 (Max)
(15 MIN Max)

25
Q

Normal Flight: Normal oil pressure is ___ to ___PSI at N2 speeds above ___%. Oil pressure below ___PSI is 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

26
Q

Under cold starting conditions, oil pressure between ___PSI and ___PSI is limited to ___seconds.

A

83
95
90

27
Q

The ITT during ground starts should normally not exceed ___*C

A

550

28
Q

Normal Hydraulic Pressure (PSI)

A

1350 to 1550

29
Q

Normal Nitrogen Pressure (PSI)

A

1350 to 1650

30
Q

Normal Oxygen Pressure (PSI)

A

1600 to 1850

31
Q

Min battery voltage for battery start (volts)

A

22

32
Q

Max gen load prior to starting second engine (amps)

A

150

33
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

34
Q

Emergency Fuel / Minimum Fuel (lbs)

A

300 / 500

35
Q

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

A

100

36
Q

Max Fuel Imbalance - Flight (lbs)

A

300

37
Q

Max Fuel Imbalance - Landing (lbs)

A

300

38
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

39
Q

Max Ramp Weight (lbs)

A

16,300

40
Q

Max Takeoff Weight (lbs)

A

16,100

41
Q

Max Landing Weight (lbs)

A

15,700

42
Q

Extend flaps to 10 degrees (KIAS)

A

200

43
Q

Extend flaps > 10 degrees (KIAS)

A

170

44
Q

Flaps extended > 10 degrees (KIAS)

A

165

45
Q

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

A

330
.78

46
Q

Landing Gear/Lights ___ KIAS / FL ___

A

200
200

47
Q

Wipers ___ KIAS

A

200

48
Q

Tire ___ Knots GS

A

165

49
Q

Max Tailwind __ Knots

A

10

50
Q

Max Crosswind (Dry) ___ Knots

A

25

51
Q

Max Crosswind (Wet) ___ Knots

A

15

52
Q

Max Crosswind (Icy) ___ Knots

A

10

53
Q

Max Operating Altitude FL ___

A

410

54
Q

Yaw Damper required operable for flight above FL ___

A

280

55
Q

Do not use autopilot below ___ FT AGL

A

200

56
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

57
Q

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

A

10

58
Q

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

A

70