T-38 Ops Limits

Front 1

Ground Steady State:Start: EGT (*C) ____(Max)____

Back 1

925, 845

Front 2

Ground Steady State:Militar: EGT (*C) ____-____

Back 2

630,650

Front 3

Ground Steady State:(Max)/Afterburner: EGT (*C) ____-____

Back 3

630,650

Front 4

Ground Steady State:Idle:RPM% ___-___

Back 4

46, 50

Front 5

Ground Steady State:Military:RPM% ___-___

Back 5

99, 101

Front 6

Ground Steady State:(Max)/Afterburner:RPM% ___-___

Back 6

99, 101

Front 7

Ground Steady State:Idle:Nozzle Position% ___-___

Back 7

77, 92

Front 8

Ground Steady State:Military:Nozzle Position% ___-___

Back 8

0, 20

Front 9

Ground Steady State:(Max)/Afterburner:Nozzle Position% ___-___

Back 9

50, 85

Front 10

Ground Steady State:Start:Fuel Flow (Lb/hr): ____(Max)

Back 10

360

Front 11

Ground Steady State:Idle:Fuel Flow (Lb/hr): ___-___(Std Day)

Back 11

400, 600

Front 12

Ground Steady State:Military:Fuel Flow (Lb/hr): ___-___ (Seal Level)

Back 12

2100, 2700

Front 13

Ground Steady State:Idle:Oil P (psi) ___-___

Back 13

5, 20

Front 14

Ground Steady State:Military:Oil P (psi) ___-___

Back 14

20, 55

Front 15

Ground Steady State:(Max)/Afterburner: Oil P (psi) ___-___

Back 15

20, 55

Front 16

Ground Steady State:Military:Time Duration (mins) ___

Back 16

5

Front 17

Ground Steady State:Military:Time Duration (mins) ___

Back 17

5

Front 18

Flight Steady State:Start:EGT(*C) ___(Max)

Back 18

925

Front 19

Flight Steady State:Military:EGT(*C) ___-___

Back 19

630, 650

Front 20

Flight Steady State:(Max)/Afterburner:EGT(*C) ___-___

Back 20

630, 650

Front 21

Flight Steady State:Military:RPM% ___-___

Back 21

99, 104

Front 22

Flight Steady State:(Max)/Afterburner:RPM% ___-___

Back 22

99, 104

Front 23

Flight Steady State:Military:Nozzle Position% ___-___

Back 23

0, 20

Front 24

Flight Steady State:(Max)/Afterburner:Nozzle Position% ___-___

Back 24

50, 85

Front 25

Flight Steady State:Start:Fuel Flow (lb/hr) ___(Max)

Back 25

360

Front 26

Flight Steady State:Idle:Fuel Flow (lb/hr) ___ (Min)(Std Day)

Back 26

200

Front 27

Flight Steady State:Idle:Oil P (psi) ___(min)

Back 27

5

Front 28

Flight Steady State:Military:Oil P (psi) ___-___

Back 28

20, 55

Front 29

Flight Steady State:(Max)/Afterburner:Oil P (psi) ___-___

Back 29

20, 55

Front 30

Flight Steady State:Military:Time Duration (mins) ___

Back 30

30

Front 31

Flight Steady State:(Max)/Afterburner:Time Duration (mins) ___

Back 31

15

Front 32

Fluctuation Limits (Within Steady State Limits):Idle:RPM% ___-___

Back 32

46, 50

Front 33

Fluctuation Limits (Within Steady State Limits):MIL and AB(Ground):RPM% __-___

Back 33

99, 101

Front 34

Fluctuation Limits (Within Steady State Limits):MIL and AB(Flight): RPM% +- ___

Back 34

1

Front 35

Fluctuation Limits (Within Steady State Limits):Idle(Ground):Nozzle Position% _____

Back 35

none allowed

Front 36

Fluctuation Limits (Within Steady State Limits):MIL and AB(Ground):Nozzle Position% +- ___

Back 36

3

Front 37

Fluctuation Limits (Within Steady State Limits):MIL and AB(Flight):Nozzle Position% +- ___

Back 37

3

Front 38

Fluctuation Limits (Within Steady State Limits):Idle(Ground):Fuel Flow (lb/hr) +- ___

Back 38

25

Front 39

Fluctuation Limits (Within Steady State Limits):MIL and AB(Ground):Fuel Flow (lb/hr) +- ___

Back 39

50

Front 40

Fluctuation Limits (Within Steady State Limits):Mil and AB(Flight):Fuel Flow (lb/hr) +- ___

Back 40

50

Front 41

Fluctuation Limits (Within Steady State Limits):Idle(Ground):Oil P (psi) +- ___

Back 41

2

Front 42

Fluctuation Limits (Within Steady State Limits):MIL and AB(Ground):Oil P (psi) +- ___

Back 42

2

Front 43

Fluctuation Limits (Within Steady State Limits):MIL and AB(Flight):Oil P (psi) +- ___

Back 43

2

Front 44

Abort Start if EGT reaches ____ *C to preclude exceeding temperature limits.

Back 44

845

Front 45

Abort aircraft during ground start if EGT exceeds ___ *C momentarily

Back 45

925

Front 46

Total fluctuation in EGT of ___ *C (+- ___*C) are acceptable if the average EGT is between ___*C and ___*C

Back 46

15, 7.5, 630, 650

Front 47

RPM: Maximum allowable transient RPM ___%

Back 47

107

Front 48

Nozzle Position:Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within ___ secconds

Back 48

10

Front 49

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

Back 49

360, 360

Front 50

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 ___ PSI.

Back 50

5, 55

Front 51

If a sudden change of ___ PSi or greater in oil pressure indications occurs at any stabilized RPM, follow engine oil sysmtem malfunction procedures in Section III of Dash 1

Back 51

10

Front 52

Flaps 1%-45% _____ KCAS

Back 52

300

Front 53

Flaps 46%-60% _____ KCAS

Back 53

240

Front 54

Flaps Over 60% _____ KCAS

Back 54

220

Front 55

Canopy ____ KCAS

Back 55

50

Front 56

Gear/Gear Doors ____ KCAS

Back 56

240

Front 57

Nose Wheel Steering ____ KCAS

Back 57

65

Front 58

Main Wheel Tire (14 ply) ____ KCAS

Back 58

204

Front 59

Main Wheel Tire (12 ply) ____ KCAS

Back 59

195

Front 60

Nose Wheel Tire ____ KCAS

Back 60

174

Front 61

3500 lbs: Max Sym G ___to___

Back 61

-2.3, +5.7

Front 62

3000 lbs: Max Sym G ___to___

Back 62

-2.4, +5.9

Front 63

2000 lbs: Max Sym G ___to___

Back 63

-2.6, +6.5

Front 64

1000 lbs: Max Sym G ___to___

Back 64

-2.9, +7.2

Front 65

3500 lbs: Max Asym G ___to___

Back 65

0, +4.1

Front 66

3000 lbs: Max Asym G ___to___

Back 66

0, +4.3

Front 67

2000 lbs: Max Asym G ___to___

Back 67

0, +4.7

Front 68

1000 lbs: Max Asym G ___to___

Back 68

0, +5.0

Front 69

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 trunion

Back 69

45, 1.5

Front 70

Oxygen Pressure Normal Range ___ PSI to ___ PSI

Back 70

50, 120

Front 71

Hydraulic Pressure Min PSI ____

Back 71

1500

Front 72

Hydraulic Pressure Max PSI ____

Back 72

3200

Front 73

Hydraulic Pressure Normal Range ____ PSI to ____ PSI

Back 73

2850, 3200

Front 74

WSSP Limitations: Sym: ___to___

Back 74

0, +4.0

Front 75

WSSP Limitations: Asym: ___to ___

Back 75

0, +3.0

Front 76

WSSP Limitations: Normal Capacity ___LBS

Back 76

140

Front 77

Airspeed Limits: Max ____KCAS

Back 77

400

Front 78

Airspeed Limits: SB Open/Turbulence ___KCAS

Back 78

350

Front 79

Airspeed Limits: Abrupt Control ___KCAS

Back 79

240

Front 80

Dash-1 Prohibited Maneuvers:1

Back 80

Vertical Stalls

Front 81

Dash-1 Prohibited Maneuvers:2

Back 81

Intentional Spins

Front 82

Dash-1 Prohibited Maneuvers:3

Back 82

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