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T-38 Ops Limits > Ops Limits > Flashcards

Ops Limits Flashcards

1
Q

EGT max/AB (Ground steady state)

A

630-650

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2
Q

EGT mil (Ground steady state)

A

630-650

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3
Q

EGT start (flight steady state)

A

925 max

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4
Q

EGT mil (FLT steady state)

A

630-650

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5
Q

EGT max/AB (FLT steady state)

A

630-650

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6
Q

Abort start when EGT reaches ____

A

845

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7
Q

Abort AC during ground start if EGT reaches _____

A

925

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8
Q

Total fluctuations in EGT of ______ are acceptable if EGT is between ___ and ____

A

15 (+/- 7.5), 630-650

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9
Q

RPM idle (Ground steady state)

A

46-50

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10
Q

RPM mil (Ground steady state)

A

99-101

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11
Q

RPM max/AB (Ground steady state)

A

99-101

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12
Q

RPM mil (FLT steady state)

A

99-104

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13
Q

RPM max/AB (FLT steady state)

A

99-104

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14
Q

RPM fluctuations idle

A

46-50

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15
Q

RPM fluctuations mil/max (GRD)

A

99-101

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16
Q

RPM fluctuations mil/max (FLT)

A

+/- 1

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17
Q

Nozzle idle (Ground steady state)

A

77-92

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18
Q

Nozzle mil (Ground steady state)

A

0-20

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19
Q

Nozzle max/AB (Ground steady state)

A

50-85

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20
Q

Nozzle mil (FLT steady state)

A

0-20

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21
Q

Nozzle max/AB (FLT steady state)

A

50-85

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22
Q

Nozzle fluctuations idle GRD

A

None allowed

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23
Q

Nozzle fluctuations mil/AB (GRD)

A

+/- 3

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24
Q

Nozzle fluctuations mil/AB (FLT)

A

+/- 3

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25
Q

Fuel flow start (Ground steady state)

A

360

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26
Q

Fuel flow idle (Ground steady state)

A

400-600

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27
Q

Fuel flow mil (Ground steady state)

A

2100-2700

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28
Q

Fuel flow start (FLT steady state)

A

360 (max)

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29
Q

Fuel flow idle (FLT steady state)

A

200

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30
Q

Oil pressure idle (Ground steady state)

A

5-20

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31
Q

Oil pressure mil (Ground steady state)

A

20-55

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32
Q

Oil pressure max/AB (Ground steady state)

A

20-55

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33
Q

Oil pressure idle (FLT steady state)

A

5 (min)

34
Q

Oil pressure mil (FLT steady state)

A

20-55

35
Q

Oil pressure max/AB (FLT steady state)

A

20-55

36
Q

Fuel flow idle fluctuations (GRD)

A

+/- 25

37
Q

Fuel flow fluctuations mil/AB (GRD)

A

+/- 50

38
Q

Fuel flow fluctuations mil/AB (FLT)

A

+/- 50

39
Q

Oil pressure fluctuations idle (GRD)

A

+/-2

40
Q

Oil pressure fluctuations mil/max GRD

A

+/-2

41
Q

Oil press fluctuations mil/max FLT

A

+/-2

42
Q

Time durations mil (Ground steady state)

A

5

43
Q

Time durations max/AB (Ground steady state)

A

5

44
Q

Time durations mil (FLT steady state)

A

30

45
Q

Time durations max/AB (FLT steady state)

A

15

46
Q

EGT start (Ground steady state)

A

925 (max) 845

47
Q

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

A

10

48
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 ______ LB/HR prior to EGT rise during actual engine start

A

360 / 360

49
Q

Do not exceed ___ minutes in military power with oil pressure above ________. If a sudden change of _______ or greater in oil pressure indication occurs at any stabilized RPM, follow engine oil system malfunction procedures in Section III of DASH 1

A

5 / 55 PSI / 10 PSI

50
Q

Flaps 1% - 45%

A

300 KCAS

51
Q

Flaps 46% - 60%

A

240 KCAS

52
Q

Flaps over 60%

A

220 KCAS

53
Q

Canopy

A

50 KCAS

54
Q

Gear / gear doors

A

240 KCAS

55
Q

Nose wheel steering

A

65 kts GS

56
Q

Main wheel tire

A

214 (14 ply) kts GS

195 (12 ply) kts GS

57
Q

Nose wheel tire

A

174 kts GS

58
Q

Min PSI hydraulic pressure

A

1500

59
Q

Max PSI hydraulic pressure

A

3200

60
Q

Normal range hydraulic pressure

A

2850 PSI to 3200 PSI

61
Q

WSSP Sym

A

0 to +4.0

62
Q

WSSP Asym

A

0 to +3.0

63
Q

WSSP normal capacity

A

140 LBS

64
Q

Airspeed limits Max

A

400 KCAS

65
Q

Airspeed limits SB open / turbulence

A

350 KCAS

66
Q

Airspeed limits abrupt control

A

240 KCAS

67
Q

DASH-1 prohibited maneuvers

1.

A

Vertical stalls

68
Q

DASH-1 prohibited maneuvers

2.

A

Intentional Spins

69
Q

DASH-1 prohibited maneuvers

3.

A

Continuous aileron rolls (more than one complete roll) will be accomplished only at 1.0 G and 3/4 or less stick deflection.

70
Q

Oxygen pressure normal range

A

50 PSI to 120 PSI

71
Q

Load factor 3500 Sym G

A

-2.3 to +5.7

72
Q

Load factor 3000 Sym G

A

-2.4 to +5.9

73
Q

Load factor 2000 Sym G

A

-2.6 to +6.5

74
Q

Load factor 1000 Sym G

A

-2.9 to 7.2

75
Q

Load factor 3500 Asym G

A

0 to +4.1

76
Q

Load factor 3000 Asym G

A

0 to +4.3

77
Q

Load factor 2000 Asym G

A

0 - +4.7

78
Q

Load factor 1000 Asym G

A

0 to +5.0

79
Q

Caution: Extension / retraction of landing gear at bank angles greater than _____ degrees or at load factors greater than _____ G can result in overs tress failure of the main landing gear sidebrace trunnion

A

45 / 1.5

80
Q

Maximum allowable transient RPM ______ %

A

107

T-38 Ops Limits (1 decks)

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