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
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.
60 83 60 60 40
26
Under cold starting conditions, oil pressure between ___PSI and ___PSI is limited to ___seconds.
83 95 90
27
The ITT during ground starts should normally not exceed ___*C
550
28
Normal Hydraulic Pressure (PSI)
1350 to 1550
29
Normal Nitrogen Pressure (PSI)
1350 to 1650
30
Normal Oxygen Pressure (PSI)
1600 to 1850
31
Min battery voltage for battery start (volts)
22
32
Max gen load prior to starting second engine (amps)
150
33
Motoring of the starter is limited to: First, ___ seconds then ___ minutes cooling. Second, ___ seconds then ___ minutes cooling. Third, ___ seconds then ___ minutes cooling.
30 5 30 15 30 60
34
Emergency Fuel / Minimum Fuel (lbs)
300 / 500
35
Maximum Fuel Imbalance - T.O./Touch & Go (lbs)
100
36
Max Fuel Imbalance - Flight (lbs)
300
37
Max Fuel Imbalance - Landing (lbs)
300
38
Fuel crossfeed with 2 engines operating is limited to level flight with less than ___ lbs of fuel remains in the wing tank supplying fuel.
600
39
Max Ramp Weight (lbs)
16,300
40
Max Takeoff Weight (lbs)
16,100
41
Max Landing Weight (lbs)
15,700
42
Extend flaps to 10 degrees (KIAS)
200
43
Extend flaps > 10 degrees (KIAS)
170
44
Flaps extended > 10 degrees (KIAS)
165
45
Aircraft is limited to ___ KIAS or ___ MACH, whichever is less.
330 .78
46
Landing Gear/Lights ___ KIAS / FL ___
200 200
47
Wipers ___ KIAS
200
48
Tire ___ Knots GS
165
49
Max Tailwind __ Knots
10
50
Max Crosswind (Dry) ___ Knots
25
51
Max Crosswind (Wet) ___ Knots
15
52
Max Crosswind (Icy) ___ Knots
10
53
Max Operating Altitude FL ___
410
54
Yaw Damper required operable for flight above FL ___
280
55
Do not use autopilot below ___ FT AGL
200
56
Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above ___ *C OAT/SAT
10
57
Do not operate surface anti-ice systems in flight at ram air temperatures above ___ *C.
10
58
To ensure proper wing anti-ice operation, the throttles must be kept at ___% N2 minimum.
70