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T-38 > Ops Limits > Flashcards

Ops Limits Flashcards

1
Q

EGT (C) Ground Steady State (Start)

A

*925 (Max) 845

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2
Q

EGT (C) Ground Steady State (Idle)

A

N/A

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3
Q

EGT (C) Ground Steady State (Military)

A

630-650

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4
Q

EGT (C) Ground Steady State (Max/Afterburner)

A

630-650

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5
Q

RPM (%) Ground Steady State (Start)

A

N/A

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6
Q

RPM (%) Ground Steady State (Idle)

A

46-50

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7
Q

RPM (%) Ground Steady State (Military)

A

99-101

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8
Q

RPM (%) Ground Steady State (Max/Afterburner)

A

99-101

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9
Q

Nozzle Position (%) Ground Steady State (Start)

A

N/A

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10
Q

Nozzle Position (%) Ground Steady State (Idle)

A

77-92

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11
Q

Nozzle Position (%) Ground Steady State (Military)

A

0-20

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12
Q

Nozzle Position (%) Ground Steady State (Max/Afterburner)

A

50-85

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13
Q

Fuel Flow (LB/HR) Ground Steady State (Start)

A

***360 (max)

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14
Q

Fuel Flow (LB/HR) Ground Steady State (Idle)

A

400-600 (Std Day)

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15
Q

Fuel Flow (LB/HR) Ground Steady State (Military)

A

2100-2700 (Sea Level)

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16
Q

Fuel Flow (LB/HR) Ground Steady State (Max/afterburner)

A

N/A

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17
Q

Oil Pressure (PSI) Ground Steady State (Start)

A
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18
Q

Oil Pressure (PSI) Ground Steady State (Idle)

A

5-20

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19
Q

Oil Pressure (PSI) Ground Steady State (Military)

A

20-55

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20
Q

Oil Pressure (PSI) Ground Steady State (Max/Afterburner)

A

20-55

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21
Q

Time Duration (Minutes) Ground Steady State (Start)

A

N/A

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22
Q

Time Duration (Minutes) Ground Steady State (Idle)

A

N/A

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23
Q

Time Duration (Minutes) Ground Steady State (Military)

A

5

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24
Q

Time Duration (Minutes) Ground Steady State (Max/Afterburner)

A

5

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25
Q

EGT (C) Flight Steady State (Start)

A

*925 (Max)

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26
Q

EGT (C) Flight Steady State (Idle)

A

N/A

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27
Q

EGT (C) Flight Steady State (Military)

A

630-650

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28
Q

EGT (C) Flight Steady State (Max/Afterburner)

A

630-650

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29
Q

RPM (%) Flight Steady State (Start)

A

N/A

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30
Q

RPM (%) Flight Steady State (Idle)

A

N/A

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31
Q

RPM (%) Flight Steady State (Military)

A

99-104

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32
Q

RPM (%) Flight Steady State (Max/Afterburner)

A

99-104

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33
Q

Nozzle Position (%) Flight Steady State (Start)

A

N/A

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34
Q

Nozzle Position (%) Flight Steady State (Idle)

A

N/A

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35
Q

Nozzle Position (%) Flight Steady State (Military)

A

0-20

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36
Q

Nozzle Position (%) Flight Steady State (Max/Afterburner)

A

50-85

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37
Q

Fuel Flow (LB/HR) Flight Steady State (Start)

A

***360 (Max)

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38
Q

Fuel Flow (LB/HR) Flight Steady State (Idle)

A

200 (Min) (Std Day)

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39
Q

Fuel Flow (LB/HR) Flight Steady State (Military)

A

N/A

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40
Q

Fuel Flow (LB/HR) Flight Steady State (Max/Afterburner)

A

N/A

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41
Q

Oil Pressure (PSI) Flight Steady State (Start)

A
42
Q

Oil Pressure (PSI) Flight Steady State (Idle)

A

5 (Min)

43
Q

Oil Pressure (PSI) Flight Steady State (Military)

A

20-55

44
Q

Oil Pressure (PSI) Flight Steady State (Max/Afterburner)

A

20-55

45
Q

Time Duration (Minutes) Flight Steady State (Start)

A

N/A

46
Q

Time Duration (Minutes) Flight Steady State (Idle)

A

N/A

47
Q

Time Duration (Minutes) Flight Steady State (Military)

A

30

48
Q

Time Duration (Minutes) Flight Steady State (Max/Afterburner)

A

15

49
Q

EGT (C) Fluctuation Limits (Within Steady State Limits) (Idle Ground)

A

N/A

50
Q

EGT (C) Fluctuation Limits (Within Steady State Limits) (Mil and AB Ground)

A

**

51
Q

EGT (C) Fluctuation Limits (Within Steady State Limits) (Mil and AB Flight)

A

**

52
Q

RPM (%) Fluctuation Limits (Within Steady State Limits) (Idle Ground)

A

46-50

53
Q

RPM (%) Fluctuation Limits (Within Steady State Limits) (Mil and AB Ground)

A

99-101

54
Q

RPM (%) Fluctuation Limits (Within Steady State Limits) (Mil and AB Flight)

A

+/-1

55
Q

Nozzle Position (%) Fluctuation Limits (Within Steady State Limits) (Idle Ground)

A

None Allowed

56
Q

Nozzle Position (%) Fluctuation Limits (Within Steady State Limits) (Mil and AB Ground)

A

+/-3

57
Q

Nozzle Position (%) Fluctuation Limits (Within Steady State Limits) (Mil and AB Flight)

A

+/-3

58
Q

Fuel Flow (LB/HR) Fluctuation Limits (Within Steady State Limits) (Idle Ground)

A

+/-25

59
Q

Fuel Flow (LB/HR) Fluctuation Limits (Within Steady State Limits) (Mil and AB Ground)

A

+/-25

60
Q

Fuel Flow (LB/HR) Fluctuation Limits (Within Steady State Limits) (Mil and AB Flight)

A

+/-25

61
Q

Oil Pressure (PSI) Fluctuation Limits (Within Steady State Limits) (Idle Ground)

A

+/-2

62
Q

Oil Pressure (PSI) Fluctuation Limits (Within Steady State Limits) (Mil and AB Ground)

A

+/-2

63
Q

Oil Pressure (PSI) Fluctuation Limits (Within Steady State Limits) (Mil and AB Flight)

A

+/-2

64
Q

Time Duration (Minutes) Fluctuation Limits (Within Steady State Limits) (Idle Ground)

A

N/A

65
Q

Time Duration (Minutes) Fluctuation Limits (Within Steady State Limits) (Mil and AB Ground)

A

N/A

66
Q

Time Duration (Minutes) Fluctuation Limits (Within Steady State Limits) (Idle Ground)

A

N/A

67
Q

EGT: *Abort start if EGT reaches ____ to preclude exceeding temperature limits. Abort aircraft during ground start if EGT exceeds ____ momentarily** Total fluctuations in EGT of ___ (+/- ___) are acceptable if the average EGT is between ____ and ____

A 
845 (C)
925 (C)
15 (C)
7.5 (C)
630 (C)
650 (C)
68
Q

RPM: Maximum allowable transient RPM ____

A

107%

69
Q

Nozzle Position: Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within ___ seconds

A

10

70
Q

Fuel Flow:***During engine start the indicated fuel flow may momentarily transit above ___ LB/HR after advancing the throttle to idle during engine start sequence but should return to equal to or less than ____ LB/HR prior to EGT rise during actual engine start

A

360

360

71
Q

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

A

5
55
10

72
Q

Airspeed: Flaps 1%-45%

A

300 KCAS

73
Q

Airspeed: Flaps 46%-60%

A

240 KCAS

74
Q

Airspeed: Flaps Over 60%

A

220 KCAS

75
Q

Airspeed: Canopy

A

50 KCAS

76
Q

Airspeed: Gear/Gear Door

A

240 KCAS

77
Q

Airspeed: Nose Wheel Steering

A

65 Kts GS

78
Q

Airspeed: Main Wheel Tire

A

221 (14 ply) KtsGS

195 (12 ply) Kts GS

79
Q

Airspeed: Nose Wheel Tire

A

174 Kts GS

80
Q

Hydraulic Pressure: Min PSI

A

1500

81
Q

Hydraulic Pressure: Max PSI

A

3200

82
Q

Hydraulic Pressure: Normal Range

A

2850 to 3200

83
Q

WSSP Limitations: Sym

A

0 to +4.0

84
Q

Airspeed Limits: Max

A

400 KCAS

85
Q

Load Factor (Max Sym G): Fuel (LBS) 3500

A

-2.3 to +5.7

86
Q

Load Factor (Max Sym G): Fuel (LBS) 3000

A

-2.4 to +5.9

87
Q

Load Factor (Max Sym G): Fuel (LBS) 2000

A

-2.6 to +6.5

88
Q

Load Factor (Max Sym G): Fuel (LBS) 1000

A

-2.9 to +7.2

89
Q

Load Factor (Max Asym G): Fuel (LBS) 3500

A

0 to +4.1

90
Q

Load Factor (Max Asym G): Fuel (LBS) 3000

A

0 to +4.3

91
Q

Load Factor (Max Asym G): Fuel (LBS) 2000

A

0 to +4.7

92
Q

Load Factor (Max Asym G): Fuel (LBS) 1000

A

0 to +5.0

93
Q

Caution: Extension/retraction of landing gear at bank angles greater than ____ or at load factor greater than _____G can result in overstress failure of the main landing gear sidebrace trunnion

A

45 degrees

1.5

94
Q

Oxygen Pressure ___PSI to ___ PSI

A

50 to 120

95
Q

WSSP Limitations: Asym

A

0 to +3.0

96
Q

WSSP Limitations: Normal Capacity (LBS)

A

140

97
Q

Airspeed Limits: SB Open/ Turbulence

A

350 KCAS

98
Q

Airspeed Limits: Abrupt Control

A

240 KCAS

99
Q

DASH-1 Prohibited Maneuvers (1)

A

Vertical Stalls

100
Q

DASH-1 Prohibited Maneuvers (1)

A

Intentional Spins

101
Q

DASH-1 Prohibited Maneuvers (1)

A

Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection

T-38 (8 decks)

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