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T-38 ENJJPT 21-01 > Ops Limits > Flashcards

Ops Limits Flashcards

1
Q

Start EGT °C
Ground
* ____ (MAX) ____

A

925

845

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2
Q

Start Fuel Flow LB / HR
Ground
*** ____ (MAX)

A

360

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3
Q

Idle RPM %

Ground

A

46 - 50

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4
Q

Idle Nozzle Position %

Ground

A

77 - 92

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5
Q

Idle Fuel Flow LB / HR
Ground
____ - ____ (Std Day)

A

400 - 600

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6
Q

Idle Oil Pressure PSI

Ground

A

5 - 20

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7
Q

Military EGT °C

Ground

A

630 - 650

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8
Q

Military RPM %

Ground

A

99 - 101

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9
Q

Military Nozzle Position %

Ground

A

0 - 20

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10
Q

Military Fuel Flow LB / HR
Ground
____ - _____ (Sea Level)

A

2100 - 2700

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11
Q

Military Oil Pressure PSI

Ground

A

20 -55

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12
Q

Military Time Duration (Minutes)

Ground

A

5

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13
Q

(MAX) / Afterburner EGT °C

Ground

A

630 - 650

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14
Q

(MAX) / Afterburner RPM %

Ground

A

99 - 101

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15
Q

(MAX) / Afterburner Nozzle Position %

Ground

A

50 - 85

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16
Q

(MAX) / Afterburner Oil Pressure PSI

Ground

A

20 - 55

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17
Q

(MAX) / Afterburner Time Duration (Minutes)

Ground

A

5

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18
Q

Start EGT °C
Flight Steady State
* ____ (MAX)

A

925

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19
Q

Start Fuel Flow LB / HR
Flight Steady State
*** ____ (MAX)

A

360

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20
Q

Idle Fuel Flow LB / HR
Flight Steady State
____ (Min) (Std Day)

A

200

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21
Q

Idle Oil Pressure PSI
Flight Steady State
____ (Min)

A

5

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22
Q

Military EGT °C

Flight Steady State

A

630 - 650

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23
Q

Military RPM %

Flight Steady State

A

99 - 104

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24
Q

Military Nozzle Position %

Flight Steady State

A

0 - 20

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25
Q

Military Oil Pressure PSI

Flight Steady State

A

20 - 55

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26
Q

Military Time Duration (Minutes)

Flight Steady State

A

30

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27
Q

(MAX) / Afterburner EGT °C

Flight Steady State

A

630 - 650

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28
Q

(MAX) / Afterburner RPM %

Flight Steady State

A

99 - 104

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29
Q

(MAX) / Afterburner Nozzle Position %

Flight Steady State

A

50 - 85

30
Q

(MAX) / Afterburner Oil Pressure PSI

Flight Steady State

A

20 - 55

31
Q

(MAX) / Afterburner Time Duration (Minutes)

Flight Steady State

A

15

32
Q 
Idle (Ground) RPM %
Fluctuation Limits (Within Steady State Limits)
A

46 - 50

33
Q 
Idle (Ground) Fuel Flow LB / HR
Fluctuation Limits (Within Steady State Limits)
A

±25

34
Q 
Idle (Ground) Oil Pressure PSI
Fluctuation Limits (Within Steady State Limits)
A

±2

35
Q 
MIL and AB (Ground) RPM %
Fluctuation Limits (Within Steady State Limits)
A

99 - 101

36
Q 
MIL and AB (Ground) Nozzle Position %
Fluctuation Limits (Within Steady State Limits)
A

±3

37
Q 
MIL and AB (Ground) Fuel Flow LB / HR
Fluctuation Limits (Within Steady State Limits)
A

±50

38
Q 
MIL and AB (Ground) Oil Pressure PSI
Fluctuation Limits (Within Steady State Limits)
A

±2

39
Q 
MIL and AB (Flight) RPM %
Fluctuation Limits (Within Steady State Limits)
A

±1

40
Q 
MIL and AB (Flight) Nozzle Position %
Fluctuation Limits (Within Steady State Limits)
A

±3

41
Q 
MIL and AB (Flight) Fuel Flow LB / HR
Fluctuation Limits (Within Steady State Limits)
A

±50

42
Q 
MIL and AB (Flight) Oil Pressure PSI
Fluctuation Limits (Within Steady State Limits)
A

±2

43
Q

EGT: * Abort start if EGT reaches _____ °C to preclude exceeding temperature limits. Abort aircraft during ground start if EGT exceeds ____°C momentarily

A

845

925

44
Q

EGT: ** Total fluctuations in EGT of ____°C (+/- ___°C) are acceptable if the average EGT is between _____°C and ____°C

A

15; 7.5
630
650

45
Q

RPM: Maximum allowable transient RPM ____ %

A

107

46
Q

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

A

10

47
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

48
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 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

49
Q

Flaps 1% - 45% Airspeed

A

300 KCAS

50
Q

Flaps 46 - 60% Airspeed

A

240 KCAS

51
Q

Flaps Over 60% Airspeed

A

220 KCAS

52
Q

Canopy Airspeed

A

50 KCAS

53
Q

Gear / Gear Doors Airspeed

A

240 KCAS

54
Q

Nose Wheel Steering

A

65 Kts GS

55
Q

Main Wheel Tire

A

221 (14 ply) Kts GS

195 (12 ply) Kts GS

56
Q

Nose Wheel Tire

A

174 Kts GS

57
Q

Hydraulic Pressure min PSI

A

1500

58
Q

Hydraulic Pressure max PSI

A

3200

59
Q

Hydraulic Pressure Normal Range

A

2850 PSI to 3200 PSI

60
Q

WSSP Limitations:
Sym
Asym
Normal Capacity

A

0 to +4.0
0 to +3.0
140 LBS

61
Q

WSSP Airspeed limits:
MAX
SB Open / Turbulence
Abrupt Control

A

400 KCAS
350 KCAS
240 KCAS

62
Q

DASH -1 Prohibited Maneuvers 1.

A

Vertical Stalls

63
Q

DASH -1 Prohibited Maneuvers 2.

A

Intentional Spins

64
Q

DASH -1 Prohibited Maneuvers 3.

A

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

65
Q

Oxygen Pressure Normal Range

A

50 PSI to 120 PSI

66
Q

Load Factor Fuel 3500 LBS

A

MAX Sym G -2.3 to +5.7

MAX Asym G 0 to +4.1

67
Q

Load Factor Fuel 3000 LBS

A

MAX Sym G -2.4 to +5.9

MAX Asym G 0 to +4.3

68
Q

Load Factor Fuel 2000 LBS

A

MAX Sym G -2.6 to +6.5

MAX Asym G 0 to +4.7

69
Q

Load Factor Fuel 1000 LBS

A

MAX Sym G -2.9 to +7.2

MAX Asym G 0 to +5.0

70
Q

Caution: Extension / retraction of landing gear at bank angles greater than ___° or at load factors greater than ___ G can result in overstress failure of the main landing gear side brace trunnion.

A

45

1.5

T-38 ENJJPT 21-01 (19 decks)

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