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ENJJPT T38 > Ops Limits > Flashcards

Ops Limits Flashcards

1
Q

EGT is in

A

Celsius

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2
Q

RPM is in

A

%

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3
Q

Nozzle position is in

A

%

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4
Q

Fuel Flow is in

A

LB / HR

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5
Q

Oil Pressure is in

A

PSI

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6
Q

Time Duration is in

A

Minutes

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7
Q

Ground
Start EGT

A

*925 (Max)
845

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8
Q

Ground
Start Fuel Flow

A

***360 (Max)

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9
Q

Ground
Start Oil Pressure

A

four asterixes (it won’t let me type them out)

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10
Q

Ground
Idle RPM

A

46-50

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11
Q

Ground
Idle Nozzle Position

A

77-92

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12
Q

Ground
Idle FF

A

400-600 (Std Day)

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13
Q

Ground
Idle Oil P

A

5-20

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14
Q

Ground
Military EGT

A

630-650

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15
Q

Ground
Military RPM

A

99-101

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16
Q

Ground
Military Nozzle Position

A

0-20

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17
Q

Ground
Military FF

A

2100-2700 (Sea Level)

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18
Q

Ground
Military Oil P

A

20-55

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19
Q

Ground
Military Time Duration

A

5

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20
Q

Ground
(Max) / Afterburner EGT

A

630-650

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21
Q

Ground
(Max) / Afterburner RPM

A

99-101

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22
Q

Ground
(Max) / Afterburner Nozzle Position

A

50-85

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23
Q

Ground
(Max) / Afterburner Oil P

A

20-55

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24
Q

Ground
(Max) / Afterburner Time Duration

A

5

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25
Q

Flight Steady State
Start EGT

A

*925 (Max)

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26
Q

Flight Steady State
Start FF

A

***360 (Max)

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27
Q

Flight Steady State
Start Oil P

A

four asterixes (it won’t let me type them)

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28
Q

Flight Steady State
Idle FF

A

200 (Min)(Std Day)

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29
Q

Flight Steady State
Idle Oil P

A

5 (Min)

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30
Q

Flight Steady State
Military EGT

A

630-650

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31
Q

Flight Steady State
Military RPM

A

99-104

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32
Q

Flight Steady State
Military Nozzle Position

A

0-20

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33
Q

Flight Steady State
Military Oil P

34
Q

Flight Steady State
Military Time Duration

35
Q

Flight Steady State
(Max) / Afterburner EGT

36
Q

Flight Steady State
(Max) / Afterburner RPM

37
Q

Flight Steady State
(Max) / Afterburner Nozzle Position

38
Q

Flight Steady State
(Max) / Afterburner Oil P

39
Q

Flight Steady State
(Max) / Afterburner Time Duration

40
Q

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

41
Q

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

A

None Allowed

42
Q

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

43
Q

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

44
Q

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

45
Q

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

46
Q

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

47
Q

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

48
Q

Fluctuation Limits (Within Steady State Limits)
MIL and AB (Ground) Oil P

49
Q

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

50
Q

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

51
Q

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

52
Q

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

53
Q

Fluctuation Limits (Within Steady State Limits)
MIL and AB (Flight) Oil P

54
Q

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

A

845C, 925C

55
Q

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

A

15C, 7.5, EGT, 630C, 650C

56
Q

RPM
Maximum allowable transient RPM ___ %

57
Q

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

58
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 to or less than ___ LB/HR prior to EGT rise during actual engine start.

59
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 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 the DASH 1.

A

5, 55 PSI, 10 PSI

60
Q

Airspeed
Flaps 1%-45%

61
Q

Airspeed
Flaps 46%-60%

62
Q

Airspeed
Flaps Over 60%

63
Q

Airspeed
Canopy

64
Q

Airspeed
Gear / Gear Doors

65
Q

Airspeed
Nose Wheel Steering

66
Q

Airspeed
Main Wheel Tire

A

221 Kts GS

67
Q

Airspeed
Nose Wheel Tire

A

174 Kts GS

68
Q

Load Factor
Fuel (LBS) 3500
Max Sym G

A

-2.3 to +5.7

69
Q

Load Factor
Fuel (LBS) 3500
Max Asym G

70
Q

Load Factor
Fuel (LBS) 3000
Max Sym G

A

-2.4 to +5.9

71
Q

Load Factor
Fuel (LBS) 3000
Max Asym G

72
Q

Load Factor
Fuel (LBS) 2000
Max Sym G

A

-2.6 to +6.5

73
Q

Load Factor
Fuel (LBS) 2000
Max Asym G

74
Q

Load Factor
Fuel (LBS) 1000
Max Sym G

A

-2.9 to +7.2

75
Q

Load Factor
Fuel (LBS) 1000
Max Asym G

76
Q

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

77
Q

Hydraulic Pressure
Min PSI:
Max PSI:
Normal Range:

A

1500
3200
2850 PSI to 3200 PSI

78
Q

Oxygen Pressure
Normal Range:

A

50 PSI to 120 PSI

79
Q

WSSP Limitations
Sym:
Asym:
Normal Capacity:

A

0 to +4.0
0 to +3.0
140 LBS

80
Q

Airspeed Limits
Max:
SB Open / Turbulence:
Abrupt Control:

A

400 KCAS
350 KCAS
240 KCAS

81
Q

DASH -1 Prohibited Maneuvers
1.
2.
3.

A
  1. Vertical Stalls
  2. Intentional Spins
  3. Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection

ENJJPT T38 (5 decks)

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