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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

A

None

40
Q

Flight / (Max) Afterburner Fuel Flow

A

None

41
Q

Fluctuation Limits / Idle (Ground) Fuel Flow

A

+-25

42
Q

Fluctuation Limits / MIL and AB (Ground) Fuel Flow

A

+-50

43
Q

Fluctuation Limits / MIL and AB (Flight) Fuel Flow

A

+-50

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

A

5-20

46
Q

Ground / Military Oil Pressure

A

20-55

47
Q

Ground / (Max) Afterburner Oil Pressure

A

20-55

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

A

5 (Min)

50
Q

Flight / Military Oil Pressure

A

20-55

51
Q

Flight / (Max) Afterburner Oil Pressure

A

20-55

52
Q

Fluctuation Limits / Idle (Ground) Oil Pressure

A

+-2

53
Q

Fluctuation Limits / MIL and AB (Ground) Oil Pressure

A

+-2

54
Q

Fluctuation Limits / MIL and AB (Flight) Oil Pressure

A

+-2

55
Q

Ground / Start Time Duration

A

None

56
Q

Ground / Idle Time Duration

A

None

57
Q

Ground / Military Time Duration

A

5

58
Q

Ground / (Max) Afterburner Time Duration

A

5

59
Q

Flight / Start Time Duration

A

None

60
Q

Flight / Idle Time Duration

A

None

61
Q

Flight / Military Time Duration

A

30

62
Q

Flight / (Max) Afterburner Time Duration

A

15

63
Q

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

A

None

64
Q

Maximum allowable transient RPM

A

107

65
Q

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

A

10

66
Q

Airspeed: Flaps 1%-45%

A

300 KCAS

67
Q

Airspeed: Flaps 46%-60%

A

240 KCAS

68
Q

Airspeed: Flaps Over 60%

A

220 KCAS

69
Q

Airspeed: Canopy

A

50 KCAS

70
Q

Airspeed: Gear / Gear Doors

A

240 KCAS

71
Q

Airspeed: Nose Wheel Steering

A

65 Kts GS

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

A

0 to +4.1

79
Q

Asym G: 3000 lbs

A

0 to +4.3

80
Q

Asym G: 2500 lbs

A

0 to +4.7

81
Q

Asym G: 2000 lbs

A

0 to +5.0

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.

A

45, 1.5

83
Q

Hydraulic Pressure Min PSI

A

1500

84
Q

Hydraulic Pressure Max PSI

A

3200

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

A

0 to +4.0

88
Q

WSSP Limitations: Asym G

A

0 to +3.0

89
Q

WSSP Normal Capacity

A

140 LBS

90
Q

WSSP Airspeed Limits: Max

A

400 KCAS

91
Q

WSSP Airspeed Limits: SB Open / Turbulence

A

350 KCAS

92
Q

WSSP Airspeed Limits: Abrupt Control

A

240 KCAS

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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