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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 (*C)

A

925(Max) 845

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9
Q

EGT - Ground Military (*C)

A

630-650

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10
Q

EGT - Ground (MAX)/Afterburner (*C)

A

630-650

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11
Q

EGT - Flight Start (*C)

A

925 (Max)

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12
Q

EGT - Flight Military (*C)

A

630-650

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13
Q

EGT - Flight (Max)/Afterburner (*C)

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 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 Limits - Idle (Ground)

A

46-50

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20
Q

RPM Fluctuation Limits - MIL and AB (Ground)

A

99-101

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21
Q

RPM Fluctuation Limits - MIL and 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 Fluctuation Limits - Idle (Ground)

A

None Allowed

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28
Q

Nozzle Fluctuation Limits - MIL and AB (Ground)

A

+/- 3

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29
Q

Nozzle Fluctuation Limits - MIL and AB (Flight)

A

+/- 3

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30
Q

Fuel Flow - Ground Start (LB/HR)

A

360 (Max)

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31
Q

Fuel Flow - Ground Idle (LB/HR)

A

400-600 (Std Day)

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32
Q

Fuel Flow - Ground MIL (LB/HR)

A

2100-2700

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33
Q

Fuel Flow - Flight Start (LB/HR)

A

360 (Max)

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34
Q

Fuel Flow - Flight Idle (LB/HR)

A

200 (Min)(Std Day)

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35
Q

Fuel Flow Fluctuation Limits Idle (Ground) (LB/HR)

A

+/- 25

36
Q

Fuel Flow Fluctuation Limits MIL and AB (Ground) (LB/HR)

A

+/- 50

37
Q

Fuel Flow Fluctuation Limits MIL and AB (Flight) (LB/HR)

A

+/- 50

38
Q

Oil Pressure - Ground Idle (PSI)

A

5-20

39
Q

Oil Pressure - Ground Military (PSI)

A

20-55

40
Q

Oil Pressure - Ground (Max)/Afterburner (PSI)

A

20-55

41
Q

Oil Pressure - Flight Idle (PSI)

A

5 (Min)

42
Q

Oil Pressure - Flight Military (PSI)

A

20-55

43
Q

Oil Pressure - Flight (Max)/Afterburner (PSI)

A

20-55

44
Q

Oil Pressure Fluctuation Limits - Idle (Ground) (PSI)

A

+/- 2

45
Q

Oil Pressure Fluctuation Limits - MIL and AB (Ground) (PSI)

A

+/- 2

46
Q

Oil Pressure Fluctuation Limits - MIL and AB (Flight)

A

+/- 2

47
Q

Time Duration - Military (Ground) (Minutes)

A

5

48
Q

Time Duration - (Max)/Afterburner (Ground) (Minutes)

A

5

49
Q

Time Duration - Military (Flight) (Minutes)

A

30

50
Q

Time Duration - (Max)/Afterburner (Flight) (Minutes)

A

15

51
Q

Abort start if EGT reaches ___C to preclude going over limits. Abort aircraft during ground start if EGT exceeds ___C

A

845, 925

52
Q

Maximum allowable transient RPM ___%

A

107

53
Q

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

A

10

54
Q

Fuel flow may momentarily transit above ___LB/HR after advancing 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

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 … follow engine oil system malfunction procedures in Section III of the -1.

A

5, 55, 10

56
Q

Airspeed - Flaps 1% - 45%

A

300 KCAS

57
Q

Airspeed - Flaps 46% - 60%

A

240 KCAS

58
Q

Airspeed - Flaps Over 60%

A

220 KCAS

59
Q

Airspeed - Canopy

A

50 KCAS

60
Q

Airspeed - Gear / Gear Doors

A

240 KCAS

61
Q

Airspeed - Nose Wheel Steering

A

65 KCAS

62
Q

Airspeed - Main Wheel Tire (14 ply)

A

221 Kts GS

63
Q

Airspeed - Main Wheel Tire (12 ply)

A

195 Kts GS

64
Q

Airspeed - Nose Wheel Tire

A

174 Kts GS

65
Q

Hydraulic Pressure Min PSI

A

1500

66
Q

Hydraulic Pressure Max PSI

A

3200

67
Q

Hydraulic Pressure Normal Range (PSI)

A

2850-3200

68
Q

Oxygen Pressure Normal Range (PSI)

A

50-120

69
Q

Max Sym G 3500 Lbs

A

-2.3 to +5.7

70
Q

Max Sym G 3000 Lbs

A

-2.4 to +5.9

71
Q

Max Sym G 2000 Lbs

A

-2.6 to +6.5

72
Q

Max Sym G 1000 Lbs

A

-2.9 to +7.2

73
Q

Max Asym G 3500 Lbs

A

0 to +4.1

74
Q

Max Asym G 3000 Lbs

A

0 to +4.3

75
Q

Max Asym G 2000 Lbs

A

0 to +4.7

76
Q

Max Asym G 1000 Lbs

A

0 to +5.0

77
Q

Extension/Retraction of landing gear at bank angles greater than __* or at load factors greater than 1.5 G can result in overstress failure of the main landing gear sidebrace trunnion.

A

45*, 1.5 G

78
Q

WSSP Sym G Limits

A

0 to +4.0

79
Q

WSSP Asym G Limits

A

0 to +3.0

80
Q

WSSP Normal Capacity (Lbs)

A

140 LBS

81
Q

WSSP Max Airspeed

A

400 KCAS

82
Q

WSSP SB Open/Turbulence Airspeed

A

350 KCAS

83
Q

WSSP Abrupt Control Airspeed

A

240 KCAS

84
Q

DASH-1 Prohibited Maneuver 1

A

Vertical Stalls

85
Q

DASH-1 Prohibited Maneuver 2

A

Intentional Spins

86
Q

DASH-1 Prohibited Maneuver 3

A

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

87
Q

Total Fluctuations in EGT of __ (+/-__) are acceptable if the average EGT is between ___C and ___C

A

15, 7.5, 630, 650

T-38 (10 decks)

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