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T38 > BF/OL > Flashcards

BF/OL 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 Steady State

Start

A

925 (Max) 845

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9
Q

EGT: Ground Steady State

Military

A

630-650

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10
Q

EGT: Ground Steady State

AB

A

630-650

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11
Q

EGT: Flight Steady State

Start

A

925

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12
Q

EGT: Flight Steady State

Military

A

630-650

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13
Q

EGT: Flight Steady State

AB

A

630-650

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14
Q

RPM: Ground Steady State

Idle

A

46-50

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15
Q

RPM: Ground Steady State

Military

A

99-101

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16
Q

RPM: Ground Steady State

AB

A

99-101

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17
Q

RPM: Flight Steady State

Military

A

99-104

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18
Q

RPM: Flight Steady State

AB

A

99-104

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19
Q

RPM: Fluctuation Limits

Idle

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 Steady State

Idle

A

77-92

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23
Q

Nozzle Position: Ground Steady State

Military

A

0-20

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24
Q

Nozzle Position: Ground Steady State

AB

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

AB

A

50-85

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27
Q

Nozzle Position: Fluctuation Limits

Idle (Ground)

A

None allowed

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28
Q

Nozzle Position: Fluctuation Limits

MIL and AB (Ground)

A

+/- 3

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29
Q

Nozzle Position: Fluctuation Limits

MIL and AB (Flight)

A

+/- 3

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30
Q

Fuel Flow: Ground Steady State

Start

A

360

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31
Q

Fuel Flow: Ground Steady State

Idle

A

400-600

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32
Q

Fuel Flow: Ground Steady State

Military

A

2100-2700

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33
Q

Fuel Flow: Flight Steady State

Start

A

360

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34
Q

Fuel Flow: Flight Steady State

Idle

A

200 (min) (Std Day)

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35
Q

Fuel Flow: Fluctuation Limits

Idle

A

+/-25

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36
Q

Fuel Flow: Fluctuation Limits

MIL and AB (Ground)

A

+/- 50

37
Q

Fuel Flow: Fluctuation Limits

MIL and AB (Flight)

A

+/-50

38
Q

Oil Pressure: Ground Steady State

Idle

A

5-20

39
Q

Oil Pressure: Ground Steady State

Military

A

20-55

40
Q

Oil Pressure: Ground Steady State

AB

A

20-55

41
Q

Oil Pressure: Flight Steady State

Idle

A

5 (min)

42
Q

Oil Pressure: Ground Steady State

Mil

A

20-55

43
Q

Oil Pressure: Ground Steady State

AB

A

20-55

44
Q

Oil Pressure: Fluctuation Limits

Idle

A

+/-2

45
Q

Oil Pressure: Fluctuation Limits

MIL and AB (Ground)

A

+/-2

46
Q

Oil Pressure: Fluctuation Limits

MIL and AB (Flight)

A

+/-2

47
Q

Time Duration: Ground Steady State

MIL

A

5

48
Q

Time Duration: Ground Steady State

AB

A

5

49
Q

Time Duration: Flight Steady State

MIL

A

30

50
Q

Time Duration: Flight Steady State

AB

A

15

51
Q

Abort start if EGT reaches ___ to preclude exceeding temp limits.

A

845

52
Q

Abort aircraft during ground start if EGT exceeds ___ momentarily

A

925

53
Q

Total fluctuations in EGT of ___ (+/-___) are acceptable if the average EGT is between ___ and ___.

A

15, 7.5, 630, 650

54
Q

Maximum allowable transient RPM ___

A

107%

55
Q

Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within ___ sec

A

10

56
Q

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 to or less than ___ prior to EGT rise during actual engine start

A

360, 360

57
Q

Do not exceed __ min in military power with oil pressure above __ PSI

A

5, 55

58
Q

A sudden change of __ PSI or greater is considered a problem

A

10

59
Q

Max Airspeed for flaps 1-45%

A

300kts

60
Q

Max Airspeed for flaps 46-60%

A

240kts

61
Q

Max Airspeed for flaps over 60%

A

220kts

62
Q

Max Airspeed for canopy

A

50

63
Q

Max Airspeed for gear/gear doors

A

240

64
Q

Max Airspeed for nose wheel steering

A

65

65
Q

Max Airspeed for Main wheel tire (14 ply)

A

221

66
Q

Max Airspeed for main wheel tire (12 ply)

A

195

67
Q

Max Airspeed for nose wheel tire

A

174

68
Q

Max Sym G for 3500

A

-2.3 to +5.7

69
Q

Max Sym G for 3000

A

-2.4 to +5.9

70
Q

Max Sym G for 2000

A

-2.6 to +6.5

71
Q

Max Sym G for 1000

A

-2.9 to +7.2

72
Q

Max Asym G for 3500

A

0 to +4.1

73
Q

Max Asym G for 3000

A

0 to +4.3

74
Q

Max Asym G for 2000

A

0 to +4.7

75
Q

Max Asym G for 1000

A

0 to +5.0

76
Q

Extension/retraction limits of landing gear:
___ deg
___ G

A

45, 1.5

77
Q

Min Hydraulic Pressure

A

1500

78
Q

Max Hydraulic Pressure

A

3200

79
Q

Normal Hydraulic Pressure range

A

2850-3200

80
Q

Normal O2 Pressure range

A

50-120

81
Q

WSSP Limits: Sym

A

0 to +4.0

82
Q

WSSP Limits: Asym

A

0 to +3.0

83
Q

WSSP Limits: Normal Capacity

A

140 lbs

84
Q

WSSP Airspeed Limits: Max

A

400

85
Q

WSSP Airspeed Limits: SB Open/Turbs

A

350

86
Q

WSSP Airspeed Limits: Abrupt Control

A

250

87
Q

Dash-1 Prohibited Maneuver 1

A

Vertical Stalls

88
Q

Dash-1 Prohibited Maneuver 2

A

Intentional Spins

89
Q

Dash-1 Prohibited Maneuver 3

A

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

T38 (6 decks)

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