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T-1 Air Force Fundamentals > Operating Limitations > Flashcards

Operating Limitations Flashcards

1
Q

Takeoff Thrust Setting Max Time Limit (Minutes)

A

5 minutes

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2
Q

Takeoff Maximum Observed ITT (Celsius)

A

700 Degrees

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3
Q

Takeoff Max N2 %

A

96%

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4
Q

Takeoff Max N1 %

A

104%

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5
Q

Takeoff Oil Pressure (PSI)

A

60 to 83 PSI

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6
Q

Takeoff Oil Temperature (Celsius)

A

10 to 121

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7
Q

Maximum Continuous Max Observed ITT (Celsius)

A

680 Degrees

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8
Q

Maximum Continuous Max N2 %

A

96%

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9
Q

Max Continuous Max N1%

A

104%

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10
Q

Maximum Continuous Max Oil Pressure (PSI)

A

60 to 83

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11
Q

Maximum Continuous Max Oil Temperature (Celsius)

A

10 to 121 Degrees

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12
Q

Idle Max Observed ITT (Celsius)

A

580 Degrees

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13
Q

Idle Minimum N2%

A

52%

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14
Q

Idle Min Oil Pressure (PSI)

A

40

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15
Q

Idle Max Oil Temperature (Celsius)

A

-40 to 121

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16
Q

Starting Max Observed ITTs (Celsius)

A

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

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17
Q

Cold Start Conditions Oil Pressure Range (PSI)

A

83 - 95 (90 SEC)

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18
Q

The ITT for ground starts should not normally exceed:

A

550 Degrees C

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19
Q

Starting Min Oil Temperature (Celsius)

A

-40 Degrees

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20
Q

Transient Max Observed ITT (Celsius)

A

720 Degrees (2 SEC MAX)

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21
Q

Transient Max N2%

A

96%

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22
Q

Transient Max N1 %

A

106%

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23
Q

Transient Max Oil Pressure (PSI)

A

95 PSI for 90 SEC

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24
Q

Transient Max Oil Temperature (Celsius)

A

135 Degrees for 15 MIN

25
Normal Oil Pressure is _____ to _____ PSI at N2 speeds above _____ %
60 to 83 PSI. 60% N2
26
Oil Pressure below _____ PSI is undesirable and should be tolerated only for safe recovery of the flight , preferable at reduced power setting
60 PSI
27
Oil Pressure below _____ PSI is unsafe
40 PSI
28
Normal Hydraulic Pressure
1350 to 1550 PSI
29
Normal Nitrogen Pressure
1350 to 1650 PSI
30
Normal Oxygen Pressure
1600 to 1850 PSI
31
Min Battery Voltage for Battery Start
22 Volts
32
Max Gen Load prior to starting second engine
150 Amps
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
300 lbs / 500 lbs
35
Maximum Fuel Imbalance - T.O./Touch & Go
100 lbs
36
Max Fuel Imbalance - Flight
300 lbs
37
Max Fuel Imbalance - Landing
300 lbs
38
Fuel cross feed with 2 engines operating is limited to level flight with less than ____ lbs of fuel remains in the wing tank supplying fuel
600 lbs
39
Max Ramp Weight
16,300 lbs
40
Max Takeoff Weight
16,100 lbs
41
Max Landing Weight
15,700 lbs
42
Extend Flaps to 10 degrees
200 KIAS
43
Extend Flaps > 10 degrees
170 KIAS
44
Flaps Extended > 10 degrees
165 KIAS
45
Aircraft’s is limited to ____ KIAS or ____ MACH, whichever is less.
330 KIAS/.78 MACH
46
Landing Gear/Lights
200 KIAS / FL 200
47
Max Wipers Speed
200 KIAS
48
Max Tire Ground Speed
165 Knots GS
49
Max Tailwind
10 Knots
50
Max Crosswind (Dry)
25 Knots
51
Max Crosswind (Wet)
15 Knots
52
Max Crosswind (Icy)
10 Knots
53
Max Operating Altitude
FL 410
54
Yaw Damper required operable for flight above _____
FL 280
55
Do not use autopilot below _____
200 FT AGL
56
Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above _____ OAT/SAT
10 C
57
Do not operate surface anti-ice systems in flight at ram air temperatures above _____
10 C
58
To ensure proper wing anti-ice operation, the throttles must be kept at _____ minimum
70% N2

T-1 Air Force Fundamentals (8 decks)

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