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82 Cards in this Set
- Front
- Back
Ground Steady State:Start: EGT (*C) ____(Max)____
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925, 845
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Ground Steady State:Militar: EGT (*C) ____-____
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630,650
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Ground Steady State:(Max)/Afterburner: EGT (*C) ____-____
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630,650
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Ground Steady State:Idle:RPM% ___-___
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46, 50
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Ground Steady State:Military:RPM% ___-___
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99, 101
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Ground Steady State:(Max)/Afterburner:RPM% ___-___
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99, 101
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Ground Steady State:Idle:Nozzle Position% ___-___
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77, 92
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Ground Steady State:Military:Nozzle Position% ___-___
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0, 20
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Ground Steady State:(Max)/Afterburner:Nozzle Position% ___-___
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50, 85
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Ground Steady State:Start:Fuel Flow (Lb/hr): ____(Max)
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360
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Ground Steady State:Idle:Fuel Flow (Lb/hr): ___-___(Std Day)
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400, 600
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Ground Steady State:Military:Fuel Flow (Lb/hr): ___-___ (Seal Level)
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2100, 2700
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Ground Steady State:Idle:Oil P (psi) ___-___
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5, 20
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Ground Steady State:Military:Oil P (psi) ___-___
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20, 55
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Ground Steady State:(Max)/Afterburner: Oil P (psi) ___-___
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20, 55
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Ground Steady State:Military:Time Duration (mins) ___
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5
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Ground Steady State:Military:Time Duration (mins) ___
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5
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Flight Steady State:Start:EGT(*C) ___(Max)
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925
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Flight Steady State:Military:EGT(*C) ___-___
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630, 650
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Flight Steady State:(Max)/Afterburner:EGT(*C) ___-___
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630, 650
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Flight Steady State:Military:RPM% ___-___
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99, 104
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Flight Steady State:(Max)/Afterburner:RPM% ___-___
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99, 104
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Flight Steady State:Military:Nozzle Position% ___-___
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0, 20
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Flight Steady State:(Max)/Afterburner:Nozzle Position% ___-___
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50, 85
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Flight Steady State:Start:Fuel Flow (lb/hr) ___(Max)
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360
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Flight Steady State:Idle:Fuel Flow (lb/hr) ___ (Min)(Std Day)
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200
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Flight Steady State:Idle:Oil P (psi) ___(min)
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5
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Flight Steady State:Military:Oil P (psi) ___-___
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20, 55
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Flight Steady State:(Max)/Afterburner:Oil P (psi) ___-___
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20, 55
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Flight Steady State:Military:Time Duration (mins) ___
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30
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Flight Steady State:(Max)/Afterburner:Time Duration (mins) ___
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15
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Fluctuation Limits (Within Steady State Limits):Idle:RPM% ___-___
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46, 50
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Fluctuation Limits (Within Steady State Limits):MIL and AB(Ground):RPM% __-___
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99, 101
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Fluctuation Limits (Within Steady State Limits):MIL and AB(Flight): RPM% +- ___
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1
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Fluctuation Limits (Within Steady State Limits):Idle(Ground):Nozzle Position% _____
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none allowed
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Fluctuation Limits (Within Steady State Limits):MIL and AB(Ground):Nozzle Position% +- ___
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3
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Fluctuation Limits (Within Steady State Limits):MIL and AB(Flight):Nozzle Position% +- ___
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3
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Fluctuation Limits (Within Steady State Limits):Idle(Ground):Fuel Flow (lb/hr) +- ___
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25
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Fluctuation Limits (Within Steady State Limits):MIL and AB(Ground):Fuel Flow (lb/hr) +- ___
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50
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Fluctuation Limits (Within Steady State Limits):Mil and AB(Flight):Fuel Flow (lb/hr) +- ___
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50
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Fluctuation Limits (Within Steady State Limits):Idle(Ground):Oil P (psi) +- ___
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2
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Fluctuation Limits (Within Steady State Limits):MIL and AB(Ground):Oil P (psi) +- ___
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2
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Fluctuation Limits (Within Steady State Limits):MIL and AB(Flight):Oil P (psi) +- ___
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2
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Abort Start if EGT reaches ____ *C to preclude exceeding temperature limits.
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845
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Abort aircraft during ground start if EGT exceeds ___ *C momentarily
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925
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Total fluctuation in EGT of ___ *C (+- ___*C) are acceptable if the average EGT is between ___*C and ___*C
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15, 7.5, 630, 650
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RPM: Maximum allowable transient RPM ___%
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107
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Nozzle Position:Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within ___ secconds
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10
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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
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360, 360
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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.
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5, 55
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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
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10
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Flaps 1%-45% _____ KCAS
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300
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Flaps 46%-60% _____ KCAS
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240
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Flaps Over 60% _____ KCAS
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220
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Canopy ____ KCAS
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50
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Gear/Gear Doors ____ KCAS
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240
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Nose Wheel Steering ____ KCAS
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65
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Main Wheel Tire (14 ply) ____ KCAS
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204
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Main Wheel Tire (12 ply) ____ KCAS
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195
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Nose Wheel Tire ____ KCAS
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174
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3500 lbs: Max Sym G ___to___
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-2.3, +5.7
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3000 lbs: Max Sym G ___to___
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-2.4, +5.9
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2000 lbs: Max Sym G ___to___
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-2.6, +6.5
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1000 lbs: Max Sym G ___to___
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-2.9, +7.2
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3500 lbs: Max Asym G ___to___
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0, +4.1
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3000 lbs: Max Asym G ___to___
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0, +4.3
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2000 lbs: Max Asym G ___to___
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0, +4.7
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1000 lbs: Max Asym G ___to___
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0, +5.0
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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
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45, 1.5
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Oxygen Pressure Normal Range ___ PSI to ___ PSI
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50, 120
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Hydraulic Pressure Min PSI ____
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1500
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Hydraulic Pressure Max PSI ____
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3200
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Hydraulic Pressure Normal Range ____ PSI to ____ PSI
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2850, 3200
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WSSP Limitations: Sym: ___to___
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0, +4.0
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WSSP Limitations: Asym: ___to ___
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0, +3.0
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WSSP Limitations: Normal Capacity ___LBS
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140
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Airspeed Limits: Max ____KCAS
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400
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Airspeed Limits: SB Open/Turbulence ___KCAS
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350
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Airspeed Limits: Abrupt Control ___KCAS
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240
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Dash-1 Prohibited Maneuvers:1
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Vertical Stalls
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Dash-1 Prohibited Maneuvers:2
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Intentional Spins
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Dash-1 Prohibited Maneuvers:3
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Continuous aileron rolls (more than one complete roll) will be accomplished only at 1.0 G and 3/4 or less stick deflection.
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