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UPT > T-38 Ops limits > Flashcards

T-38 Ops limits Flashcards

1
Q

Ground / Start EGT

A

925 (Max) 845

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2
Q

Ground / Idle EGT

A

None

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3
Q

Ground / Military EGT

A

630-650

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4
Q

Ground / (Max) Afterburner EGT

A

630-650

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5
Q

Flight / Start EGT

A

925 (Max)

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6
Q

Flight / Idle EGT

A

None

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7
Q

Flight / Military EGT

A

630-650

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8
Q

Flight / (Max) Afterburner EGT

A

630-650

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9
Q

Fluctuation Limits / Idle (Ground) EGT

A

None

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10
Q

Fluctuation Limits / MIL and AB (Ground)/(Flight) EGT

A

15 (+-7.5) if the average EGT is between 630-650

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11
Q

Ground / Start RPM

A

None

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12
Q

Ground / Idle RPM

A

46-50

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13
Q

Ground / Military RPM

A

99-101

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14
Q

Ground / (Max) Afterburner RPM

A

99-101

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15
Q

Flight / Start RPM

A

None

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16
Q

Flight / Idle RPM

A

None

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17
Q

Flight / Military RPM

A

99-104

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18
Q

Flight / (Max) Afterburner RPM

A

99-104

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19
Q

Fluctuation Limits / Idle (Ground) RPM

A

46-50

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20
Q

Fluctuation Limits / MIL and AB (Ground) RPM

A

99-101

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21
Q

Fluctuation Limits / MIL and AB (Flight) RPM

A

+-1

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22
Q

Ground / Start Nozzle Position

A

None

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23
Q

Ground / Idle Nozzle Position

A

77-92

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24
Q

Ground / Military Nozzle Position

A

0-20

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25
Q

Ground / (Max) Afterburner Nozzle Position

A

50-85

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26
Q

Flight / Start Nozzle Position

A

None

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27
Q

Flight / Idle Nozzle Position

A

None

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28
Q

Flight / Military Nozzle Position

A

0-20

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29
Q

Flight / (Max) Afterburner Nozzle Position

A

50-85

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30
Q

Fluctuation Limits / Idle (Ground) Nozzle Position

A

None Allowed

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31
Q

Fluctuation Limits / MIL and AB (Ground) Nozzle Position

A

+-3

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32
Q

Fluctuation Limits / MIL and AB (Flight) Nozzle Position

A

+-3

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33
Q

Ground / Start Fuel Flow

A

360 (Max)

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34
Q

Ground / Idle Fuel Flow

A

400-600 (Std Day)

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35
Q

Ground / Military Fuel Flow

A

2100-2700 (Sea Level)

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36
Q

Ground / (Max) Afterburner Fuel Flow

A

None

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37
Q

Flight / Start Fuel Flow

A

360 (Max)

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38
Q

Flight / Idle Fuel Flow

A

200 (Min) (Std Day)

39
Q

Flight / Military Fuel Flow

40
Q

Flight / (Max) Afterburner Fuel Flow

41
Q

Fluctuation Limits / Idle (Ground) Fuel Flow

42
Q

Fluctuation Limits / MIL and AB (Ground) Fuel Flow

43
Q

Fluctuation Limits / MIL and AB (Flight) Fuel Flow

44
Q

Ground / Start Oil Pressure

A

*****Do not advance throttle above idle without positive (>0) indication of oil pressure. During cold weather, oil pressure may exceed limitations. This is normal indication as long as the oil pressure continues to decrease as engine oil warms. Do not exceed (5) minutes in military power with oil pressure above (55) PSI. If a sudden change of (10) PSI of greater in oil pressure indication occurs at any stabilized RPM, follow engine oil system malfunction procedures in Section III of the Dash-1.

45
Q

Ground / Idle Oil Pressure

46
Q

Ground / Military Oil Pressure

47
Q

Ground / (Max) Afterburner Oil Pressure

48
Q

Flight / Start Oil Pressure

A

*****Do not advance throttle above idle without positive (>0) indication of oil pressure. During cold weather, oil pressure may exceed limitations. This is normal indication as long as the oil pressure continues to decrease as engine oil warms. Do not exceed (5) minutes in military power with oil pressure above (55) PSI. If a sudden change of (10) PSI of greater in oil pressure indication occurs at any stabilized RPM, follow engine oil system malfunction procedures in Section III of the Dash-1.

49
Q

Flight / Idle Oil Pressure

50
Q

Flight / Military Oil Pressure

51
Q

Flight / (Max) Afterburner Oil Pressure

52
Q

Fluctuation Limits / Idle (Ground) Oil Pressure

53
Q

Fluctuation Limits / MIL and AB (Ground) Oil Pressure

54
Q

Fluctuation Limits / MIL and AB (Flight) Oil Pressure

55
Q

Ground / Start Time Duration

56
Q

Ground / Idle Time Duration

57
Q

Ground / Military Time Duration

58
Q

Ground / (Max) Afterburner Time Duration

59
Q

Flight / Start Time Duration

60
Q

Flight / Idle Time Duration

61
Q

Flight / Military Time Duration

62
Q

Flight / (Max) Afterburner Time Duration

63
Q

Fluctuation Limits / Time Duration (Idle) (MIL and AB)

64
Q

Maximum allowable transient RPM

65
Q

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

66
Q

Airspeed: Flaps 1%-45%

67
Q

Airspeed: Flaps 46%-60%

68
Q

Airspeed: Flaps Over 60%

69
Q

Airspeed: Canopy

70
Q

Airspeed: Gear / Gear Doors

71
Q

Airspeed: Nose Wheel Steering

72
Q

Airspeed: Main Wheel Tire

A

221 Kts GS

73
Q

Airspeed: Nose Wheel Tire

A

174 Kts GS

74
Q

Sym G: 3500 lbs

A

-2.3 to +5.7

75
Q

Sym G: 3000 lbs

A

-2.4 to +5.9

76
Q

Sym G: 2500 lbs

A

-2.6 to +6.5

77
Q

Sym G: 2000 lbs

A

-2.9 to +7.2

78
Q

Asym G: 3500 lbs

79
Q

Asym G: 3000 lbs

80
Q

Asym G: 2500 lbs

81
Q

Asym G: 2000 lbs

82
Q

Extension / retraction of the landing gear at bank angles greater than ____ degrees or at a load greater than _____ G can result in overstress failure of the main landing gear side brace trumnion.

83
Q

Hydraulic Pressure Min PSI

84
Q

Hydraulic Pressure Max PSI

85
Q

Hydraulic Pressure Normal Range

A

2850 PSI to 3200 PSI

86
Q

Oxygen Pressure Normal Range

A

50 PSI to 120 PSI

87
Q

WSSP Limitations: Sym G

88
Q

WSSP Limitations: Asym G

89
Q

WSSP Normal Capacity

90
Q

WSSP Airspeed Limits: Max

91
Q

WSSP Airspeed Limits: SB Open / Turbulence

92
Q

WSSP Airspeed Limits: Abrupt Control

93
Q

Prohibited Maneuvers

A
  1. Vertical Stalls
  2. Intentional Spins
  3. Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection.

UPT (16 decks)

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