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T-38 > Boldface/Ops Limits > Flashcards

Boldface/Ops Limits Flashcards

1
Q

Tire Failure During Takeoff, Takeoff Continued

A

GEAR-DO NOT RETRACT

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2
Q

Time Duration Ground Steady State Start

A

NONE

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3
Q

RPM Flight Steady State (Max)/Afterburner

A

99-104%

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4
Q

EGT Ground Steady State Start

A

925 (Max) 845 deg C

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5
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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6
Q

EGT Ground Steady State Military

A

630-650 deg C

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7
Q

EGT Ground Steady State (Max)/Afterburner

A

630-650 deg C

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8
Q

Alternate Airstart/Loss of Thrust (Low Altitude)

A

THROTTLE(S)-MAX

SPEED BRAKE-CONFIRM CLOSED

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9
Q

EGT Flight Steady State (Max)/Afterburner

A

630-650 deg C

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10
Q

EGT Flight Steady State Start

A

925 (Max) deg C

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11
Q

EGT Flight Steady State Military

A

630-650 deg C

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12
Q

Ejection

A

EJECTION HANDLE-PULL

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13
Q

RPM Ground Steady State Idle

A

46-50%

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14
Q

RPM Ground Steady State Military

A

99-101%

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15
Q

RPM Ground Steady State (Max)/Afterburner

A

99-101%

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16
Q

Engine Failure/Fire Warning During Takeoff, Takeoff Continued

A

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

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17
Q

RPM Flight Steady State Military

A

99-104%

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18
Q

RPM Fluctuation Limits (Within Steady State Limits)

A

46-50%

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19
Q

Abort

A

THROTTLES-IDLE

WHEEL BRAKES-AS REQUIRED

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20
Q

Airspeed Canopy

A

50 KCAS

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21
Q

Nozzle Position Ground Steady State Military

A

0-20%

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22
Q

RPM Fluctuation Limits (Within Steady State Limits) MIL and AB (Ground)

A

99-101%

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23
Q

Load Factor (3000 lbs) Max Sym G

A

-2.4 to +5.9 Gs

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24
Q

Nozzle Position Ground Steady State (Max)/Afterburner

A

50-85%

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25
Q

Nozzle Position Flight Steady State Military

A

0-20%

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26
Q

Nozzle Position Flight Steady State (Max)/Afterburner

A

50-85%

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27
Q

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

A

None Allowed

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28
Q

Time Duration Flight Steady State Idle

A

NONE

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29
Q

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

A

+/-3

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30
Q

Airspeed Flaps 1%-45%

A

300 KCAS

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31
Q

Nozzle Position Ground Steady State Idle

A

77-92%

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32
Q

Airspeed Flaps Over 60%

A

220 KCAS

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33
Q

Airspeed limits max? Airspeed limits SB open/turbulence? Airspeed abrupt control?

A

400 KCAS
350 KCAS
240 KCAS

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34
Q

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

A

+/-3

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35
Q

Fuel Flow Flight Steady State Military

A

NONE

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37
Q

Airspeed NWS

A

65 Kts GS

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38
Q

Airspeed Main Wheel Tire

A

221 Kts GS

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38
Q

Load Factor (3500 lbs) Max Sym G

A

-2.3 to +5.7 Gs

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39
Q

Load Factor (2000 lbs) Max Sym G

A

-2.6 to +6.5 Gs

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40
Q

Airspeed Nose Wheel Tire

A

174 Kts GS

41
Q

Load Factor (1000 lbs) Max Sym G

A

-2.9 to +7.2 Gs

42
Q

Load Factor (3000 lbs) Max Asym G

A

0 to +4.3 Gs

43
Q

Airspeed Gear/Gear Doors

A

240 KCAS

45
Q

Load Factor (2000 lbs) Max Asym G

A

0 to +4.7 Gs

46
Q

Load Factor (1000 lbs) Max Asym G

A

0 to +5.0 Gs

46
Q

Fuel Flow Flight Steady State (Max)/Afterburner

A

NONE

47
Q

What is the hydraulic pressure min PSI?

A

1500 psi

48
Q

Fuel flow fluctuation limits (within Steady State limits) MIL and AB (Flight)

A

+/-50 lbs/ hr

49
Q

RPM Fluctuation Limits (Within Steady State Limits) MIL and AB (Flight)

A

+/-1

50
Q

What is the hydraulic pressure max PSI?

A

3200 psi

51
Q

Airspeed Flaps 46%-60%

A

240 KCAS

53
Q

What is oxygen pressure normal range?

A

50 to 120 psi

54
Q

WSSP Sym limitations? Asym limitations? Normal capacity?

A

0 to +4.0
0 to +3.0
140 lbs

55
Q

Time Duration Ground Steady State Idle

A

NONE

56
Q

What are the 3 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.
57
Q

What is the max bank angle for extension/retraction of the landing gear?

A

45 deg

58
Q

EGT Fluctuation Limits (Within Steady State Limits) IDLE (Ground)

A

NONE

59
Q

What is the max load factor for extension/retraction of the landing gear?

A

1.5 G

60
Q

Time Duration Flight Steady State Start

A

NONE

61
Q

Fuel flow ground Steady State start?

A

360 (max) lbs/hr

62
Q

Fuel flow ground Steady State idle?

A

400-600 lbs/hr (std day)

62
Q

Fuel flow ground Steady State Military?

A

2100-2700 (sea level) lbs/hr

63
Q

What is the hydraulic normal range?

A

2850 to 3200 psi

64
Q

Fuel flow flight Steady State start?

A

360 (Max) lbs/hr

64
Q

Fuel flow flight Steady State idle?

A

200 (Min) (Std Day) lbs/hr

65
Q

Fuel flow fluctuation limits (within Steady State limits) Idle (Ground)

A

+/-25 lbs/hr

66
Q

Fuel flow fluctuation limits (within Steady State limits) MIL and AB (Ground)

A

+/-50 lbs/hr

67
Q

Oil pressure ground Steady State idle?

A

5-20 psi

69
Q

Oil pressure ground Steady State (max)/afterburner?

A

20-55 psi

70
Q

Oil pressure Flight Steady State IDLE?

A

5 (Min)

71
Q

Oil pressure Flight Steady State Military?

A

20-55 psi

72
Q

Oil pressure Flight Steady State (Max)/Afterburner?

A

20-55 psi

73
Q

Nozzle Position Flight Steady State Idle

A

NONE

74
Q

Oil pressure fluctuation limits (within Steady State limits) (all cases)

A

+/-2 psi

75
Q

Time duration ground Steady State Military

A

5 min

76
Q

Time duration ground Steady State (Max) Afterburner

A

5 Min

77
Q

Time duration Flight Steady State military

A

30 min

78
Q

Time duration Flight Steady State (Max)/Afterburner

A

15 Min

80
Q

Abort start if EGT reaches what temperature (to preclude exceeding temperature limits)?

A

845 deg C

80
Q

Nozzle Position Ground Steady State Start

A

NONE

81
Q

What is the max allowable transient RPM?

A

107%

82
Q

What total EGT fluctuations are acceptable and in what case?

A

15 deg C (plus or minus 7.5 deg C) if average EGT is between 630 and 650 deg C

83
Q

Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within what?

A

10 seconds

84
Q

Oil pressure ground Steady State Military?

A

20-55 psi

85
Q

Indicated fuel flow should return to equal to or less than what prior to EGT rise during actual engine start?

A

360 lb/hr

87
Q

RPM Ground Steady State Start

A

NONE

88
Q

Do not exceed oil pressure limits in military power with oil pressure above what for how long?

A

55 psi

5 min

89
Q

Execute the engine oil system malfunction procedures in Section III of the DASH 1 if you have a sudden change in oil pressure of what?

A

10 psi or greater

93
Q

Abort aircraft during ground start if EGT exceeds what momentarily?

A

925 deg C

96
Q

EGT Flight Steady State Idle

A

NONE

97
Q

Load Factor (3500 lbs) Max Asym G

A

0 to +4.1 Gs

98
Q

Single-Engine Go-Around

A

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

99
Q

Time Duration Fluctuation Limits (Within Steady State Limits) (any)

A

NONE

100
Q

RPM Flight Steady State Start

A

NONE

101
Q

RPM Flight Steady State Idle

A

NONE

102
Q

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

A

None Allowed

103
Q

Fuel Flow Ground Steady State (Max)/Afterburner

A

NONE

104
Q

Nozzle Position Flight Steady State Start

A

NONE

107
Q

EGT Ground Steady State IDLE

A

NONE

T-38 (19 decks)

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