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T-38 Class > Boldface and Ops Limits > Flashcards

Boldface and Ops Limits Flashcards

1
Q

Abort

A

THROTTLES - IDLE
WHEEL BRAKES - AS REQUIRED

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2
Q

Engine Failure/ Fire Warning During Takeoff, Takeoff Continued

A

THROTTLES - MAX
FLAPS - 60%
AIRSPEED - ATTAIN SETOS MINIMUM

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3
Q

Tire Failure During Takeoff, Takeoff Continued

A

GEAR - DO NOT RETRACT

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4
Q

Fire Warning During Flight (Affected Engine)

A

TRHOTTLE - IDLE
THROTTLE - OFF, IF FIRE LIGHT REMAINS ON
IF FIRE IS CONFIRMED - EJECT

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5
Q

Ejection

A

EJECTION HANDLE - PULL

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6
Q

Alternate Airstart/Loss of Thrust (Low Altitude)

A

THROTTLES(S) - MAX
SPEED BRAKE - CONFIRM CLOSED

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7
Q

Single-Engine Go-Around

A

THROTTLES(S) - MAX
FLAPS - 60%
AIRSPEED - ATTAIN FINAL APPROACH SPEED MINIMUM

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8
Q

Start EGT
(Ground Steady State)

A

925(Max)845

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9
Q

Start Fuel Flow
(Ground Steady State)

A

***360 (Max)

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10
Q

Idle RPM%
(Ground Steady State)

A

46-50

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11
Q

Idle Nozzle Position
(Ground Steady State)

A

77-92

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12
Q

Idle Fuel Flow
(Ground Steady State)

A

400-600

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13
Q

Idle Oil Pressure
(Ground Steady State)

A

5-20

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14
Q

Military EGT
(Ground Steady State)

A

630-650

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15
Q

Military RPM
(Ground Steady State)

A

99-101

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16
Q

Military Nozzle Position
(Ground Steady State)

A

0-20

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17
Q

Military Fuel flow
(Ground Steady State)

A

2100-2700

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18
Q

Military Oil Pressure
(Ground Steady State)

A

20-55

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19
Q

Military Time duration
(Ground Steady State)

A

5

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20
Q

Max EGT
(Ground Steady State)

A

630-650

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21
Q

Max RPM%
(Ground Steady State)

A

99-101

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22
Q

Max Nozzle Position
(Ground Steady State)

A

50-85

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23
Q

Max Oil pressure
(Ground Steady State)

A

20-55

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24
Q

Max time duration
(Ground Steady State)

A

5

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25
Q

Start EGT
(Flight Steady State)

A

925

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26
Q

Start Fuel Flow
(Flight Steady State)

A

360

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27
Q

Idle Fuel Flow
(Flight Steady State)

A

200

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28
Q

Idle Oil Pressure
(Flight Steady State)

A

5 min

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29
Q

Military EGT
(Flight Steady State)

A

630-650

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30
Q

Military RPM%
(Flight Steady State)

A

99-104

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31
Q

Military Nozzle Position
(Flight Steady State)

A

0-20

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32
Q

Military Oil Pressure
(Flight Steady State)

A

20-55

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33
Q

Military Time Duration
(Flight Steady State)

A

30 min

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34
Q

Max EGT
(Flight Steady State)

A

630-650

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35
Q

Max RPM %
(Flight Steady State)

A

99-104

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36
Q

Max Nozzle Position
(Flight Steady State)

37
Q

Max Oil Pressure
(Flight Steady State)

38
Q

Max Time Duration
(Flight Steady State)

39
Q

Idle (Ground) RPM%
(Fluctuation Limits)

40
Q

Idle (Ground) Nozzle Position
(Fluctuation Limits)

A

None Allowed

41
Q

Idle (Ground) Fuel Flow
(Fluctuation Limits)

42
Q

Idle (Ground) Oil Pressure
(Fluctuation Limits)

43
Q

Mil and AB (Ground) RPM%
(Fluctuation Limits)

44
Q

Mill and AB (Ground)
Nozzle Position
(Fluctuation Limits)

45
Q

MIL and AB (Ground)
Fuel Flow
(Fluctuation Limits)

46
Q

MIL and AB (Ground)
Oil Pressure
(Fluctuation Limits)

47
Q

MIL and AB (Flight) RPM
(Fluctuation Limits)

48
Q

MIL and AB (Flight) Nozzle Position
(Fluctuation Limits)

49
Q

MIL and AB (Flight) Fuel Flow
(Fluctuation Limits)

50
Q

MIL and AB (Flight) Oil Pressure
(Fluctuation Limits)

51
Q

Abort start if EG reaches _____*C to preclude exceeding temperature limits.

52
Q

Abort aircraft during ground start if EGT exceeds _____*C momentarily.

53
Q

Total fluctuations in EGT of ___C(+/-____C) are acceptable if the average EGT is between ____C and ____C

A

15
7.5
630
650

54
Q

Maximum allowable transient RPM _____%

55
Q

Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within ____ seconds.

56
Q

During engine state the indicated fuel flow may momentarily transit above ____LB/HR after advancing the throttle to idle during engine sequence but should return to equal to or less than _____ LB/HR prior to EGT rise during actual engine start.

57
Q

Do not exceed ____ minutes in military power with oil pressure above ___ PSI.

58
Q

If a sudden change of ____ PSI or greater in oil pressure indicaiton occurs at anu atabilized RPM, follow engine oil system malfunction precedures

59
Q

Airspeed
Flaps 1% - 45%: ____KCAS

60
Q

Airspeed
Flaps 46% - 60%: ____KCAS

61
Q

Airspeed
Flaps Over 60%: ____KCAS

62
Q

Airspeed
Canopy: ___ KCAS

63
Q

Airspeed
Gear/Gear Doors:___KCAS

64
Q

Airspeed
Nose Wheel Steering:___GS

65
Q

Airspeed
Main Wheel Tire: ____ GS

66
Q

Airspeed
Nose Wheel Tire:___GS

67
Q

Load Factor
3500 Max Sym G

A

-2.3 to +5.7

68
Q

Load Factor
3500 Max Asym G

69
Q

Load Factor
3000 Max Sym G

A

-2.4 to +5.9

70
Q

Load Factor
3000 Max Aysm G

71
Q

Load Factor
2000 Max Sym G

A

-2.6 to +6.5

72
Q

Load Factor
2000 Max Asym G

73
Q

Load Factor
1000 Max Sym G

A

-2.9 to +7.2

74
Q

Load Factor
1000 Max Asym G

75
Q

Extension/retraction of landing gear at bank angles greater than ___* or at load factors greater than ____G can result in overstress failure of the main landing gear sidbrace trunnion.

76
Q

Hydraulic Pressure
Min PSI

77
Q

Hydraulic Pressure
Max PSI

78
Q

Hydraluic Pressure
Normal Range _____ PSI to ______ PSI

A

2850 to 3200

79
Q

Oxygen Pressure
Normal Range ___PSI to ___PSI

80
Q

WSSP Limitations
Sym ___ to____

81
Q

WSSP Limitations
Asym ___ to ____

82
Q

WSSP Limitations
Normal Capacity ___LBS

83
Q

Airspeed Limits:
Max ____ KCAS

84
Q

Airspeed Limits:
SB Open/Turbulence ____KCAS

85
Q

Airspeed Limits:
Abrupt Control: ____KCAS

86
Q

DASH-1 Prohibited Maneuvers:
1.

A

Vertical Stalls

87
Q

DASH-1 Prohibited Maneuvers:
2.

A

Intentional Spins

88
Q

DASH-1 Prohibited Maneuvers:
3.

A

Continuous aileron rolls at other than 1.0g and/or greater than 3.4 stick deflection.

T-38 Class (13 decks)

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