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T-38 > Boldface / Ops Limits > Flashcards

Boldface / 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

THROTTLE - 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

THROTTLE(S) - MAX

SPEED BRAKE - CONFIRM CLOSED

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7
Q

Single-Engine Go-Around

A

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

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8
Q

EGT (Ground)

Start: ____ (Max) ____

A

925, 845

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9
Q

EGT (Ground)

Military

A

630-650

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10
Q

EGT (Ground)

Max/Afterburner

A

630-650

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11
Q

EGT (Flight)

Start: ____ (Max)

A

925

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12
Q

EGT (Flight)

Military

A

630-650

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13
Q

EGT (Flight)

Max/Afterburner

A

630-650

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14
Q

RPM (Ground)

Idle

A

46-50

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15
Q

RPM (Ground)

Military

A

99-101

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16
Q

RPM (Ground)

Max/Afterburner

A

99-101

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17
Q

RPM (Flight)

Military

A

99-104

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18
Q

RPM (Flight)

Max/Afterburner

A

99-104

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19
Q

RPM (Fluctuation)

Idle (Ground)

A

46-50

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20
Q

RPM (Fluctuation)

MIL/AB (Ground)

A

99-101

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21
Q

RPM (Fluctuation)

MIL/AB (Flight)

A

+/- 1

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22
Q 
Nozzle Position (Ground)
Idle
A

77-92

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23
Q 
Nozzle Position (Ground)
Military
A

0-20

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24
Q 
Nozzle Position (Ground)
Max/Afterburner
A

50-85

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25
Q 
Nozzle Position (Flight)
Military
A

0-20

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26
Q 
Nozzle Position (Flight)
Max/Afterburner
A

50-85

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27
Q 
Nozzle Position (Fluctuation)
Idle (Ground)
A

None Allowed

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28
Q 
Nozzle Position (Fluctuation)
MIL/AB (Ground)
A

+/- 3

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29
Q 
Nozzle Position (Fluctuation)
MIL/AB (Flight)
A

+/- 3

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30
Q 
Fuel Flow (Ground)
Start: \_\_\_\_ (Max)
A

360

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31
Q 
Fuel Flow (Ground)
Idle: \_\_\_\_ - \_\_\_\_ (STD Day)
A

400, 600

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32
Q 
Fuel Flow (Ground)
MIL: \_\_\_\_ - \_\_\_\_ (Sea Level)
A

2100, 2700

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33
Q 
Fuel Flow (Flight)
Start: \_\_\_\_ (Max)
A

360

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34
Q 
Fuel Flow (Flight)
Idle: \_\_\_ (Min) (STD Day)
A

200

35
Q 
Fuel Flow (Fluctuation)
Idle (Ground)
A

+/- 25

36
Q 
Fuel Flow (Fluctuation)
MIL/AB (Ground)
A

+/- 50

37
Q 
Fuel Flow (Fluctuation)
MIL/AB (Flight)
A

+/- 50

38
Q 
Oil Pressure (Ground)
Idle
A

5-20

39
Q 
Oil Pressure (Ground)
Military
A

20-55

40
Q 
Oil Pressure (Ground)
Max/Afterburner
A

20-55

41
Q 
Oil Pressure (Flight)
Idle: \_\_\_\_ (Min)
A

5

42
Q 
Oil Pressure (Flight)
Military
A

20-55

43
Q 
Oil Pressure (Flight)
Max/Afterburner
A

20-55

44
Q 
Oil Pressure (Fluctuation)
Idle (Ground)
A

+/- 2

45
Q 
Oil Pressure (Fluctuation)
MIL/AB (Ground)
A

+/- 2

46
Q 
Oil Pressure (Fluctuation)
MIL/AB (Flight)
A

+/- 2

47
Q

Time (Duration)

Ground - Military

A

5

48
Q

Time (Duration)

Ground - Max/AB

A

5

49
Q

Time (Duration)

Flight - Military

A

30

50
Q

Time (Duration)

Flight - Max/AB

A

15

51
Q

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

A

845, 925, 15, 7.5, 630, 650

52
Q

RPM: Maximum allowable transient RPM ____ %.

A

107

53
Q

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

A

10

54
Q

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

A

360, 360

55
Q

Oil Pressure: Do not advance throttle above idle without a 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 ____ 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

56
Q

Airspeed

Flaps 1%-45%

A

300

57
Q

Airspeed

Flaps 46%-60%

A

240

58
Q

Airspeed

Flaps over 60%

A

220

59
Q

Airspeed

Canopy

A

50

60
Q

Airspeed

Gear/Gear Doors

A

240

61
Q

Ground Speed

Nose Wheel Steering

A

65

62
Q

Ground Speed

Main Wheel Tire

A

221

63
Q

Ground Speed

Nose Wheel Tire

A

174

64
Q

Load Factor

3500# - Sym

A

-2.3 to +5.7

65
Q

Load Factor

3000# - Sym

A

-2.4 to +5.9

66
Q

Load Factor

2000# - Sym

A

-2.6 to +6.5

67
Q

Load Factor

1000# - Sym

A

-2.9 to +7.2

68
Q

Load Factor

3500# - Asym

A

0 to +4.1

69
Q

Load Factor

3000# - Asym

A

0 to +4.3

70
Q

Load Factor

2000# - Asym

A

0 to +4.7

71
Q

Load Factor

1000# - Asym

A

0 to +5.0

72
Q

Caution: Extension/retraction of landing gear at bank angles greater than ____* or at load factors greater than ____ G can result in over stress failure of the main landing gear sidebrace trunnion.

A

45, 1.5

73
Q

Hydraulic Pressure

Minimum PSI

A

1500

74
Q

Hydraulic Pressure

Maximum PSI

A

3200

75
Q

Hydraulic Pressure

Normal Range PSI

A

2850-3200

76
Q

Oxygen Pressure

Normal Range PSI

A

50-120

77
Q

WSSP Limits

Sym G

A

0 to +4.0

78
Q

WSSP Limits

Asym G

A

0 to +3.0

79
Q 
WSSP Limits
Normal Capacity (LBS)
A

140

80
Q

Airspeed Limits

Max

A

400

81
Q

Airspeed Limits

SB Open / Turbulence

A

350

82
Q

Airspeed Limits

Abrupt Control

A

240

83
Q

Dash-1 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.

T-38 (7 decks)

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