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77 Cards in this Set
- Front
- Back
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Max EGT (Start)
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925ºC (abort start at 845ºC)
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Normal EGT (Military)
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630 - 650ºC
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Normal EGT (Afterburner)
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630 - 650ºC
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EGT Flux Lmt
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15ºC (±7.5ºC)
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Ground RPM (Idle)
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46 - 50%
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Ground RPM (Military)
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99 - 101%
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Ground RPM (Afterburner)
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99 - 101%
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Flight RPM (Military)
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99 - 104%
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Flight RPM (Afterburner)
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99 - 104%
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RPM Flux (Idle, Ground)
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46 - 50%
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RPM Flux (MIL and AB Ground)
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99 - 101%
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RPM Flux (MIL and AB Flight)
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±1%
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NOZ (Idle, Ground)
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77 - 92%
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NOZ (Military, Ground)
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0 - 20%
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NOZ (AB, Ground)
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50 - 85%
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NOZ (MIL, Flight)
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0 - 20%
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NOZ (AB, Flight)
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50 - 85%
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NOZ Flux (Idle, Ground)
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None Allowed
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NOZ Flux (MIL and AB, Ground)
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±3%
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NOZ Flux (MIL and AB, Flight)
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±3%
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FF, Ground (Start)
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360 (Max)
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FF, Ground (Idle)
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400 - 600 (Std Day)
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FF, Ground (Military)
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2100 - 2700 (Sea Level)
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FF, Flight (Start)
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360 (Max)
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FF, Flight (Idle)
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200 (Min) (Std Day)
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FF, Flux (Ground, Idle)
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±25
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FF, Flux (Ground, MIL and AB)
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±50
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FF, Flux (Flight, MIL and AB)
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±50
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Oil Press, Ground (Idle)
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5 - 20 PSI
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Oil Press, Ground (MIL)
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20 - 55 PSI
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Oil Press, Ground (AB)
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20 - 55 PSI
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Oil Press, Flight (Idle)
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5 PSI (Min)
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Oil Press, Flight (MIL)
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20 - 55 PSI
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Oil Press, Flight (AB)
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20 - 55 PSI
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Oil Press, Flux (Ground, Idle)
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±2 PSI
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Oil Press, Flux (Ground, MIL and AB)
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±2 PSI
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Oil Press, Flux (Flight, MIL and AB)
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±2 PSI
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Time Duration, Ground (MIL)
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5 MIN
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Time Duration, Ground (AB)
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5 MIN
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Time Duration, Flight (MIL)
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30 MIN
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Time Duration, Flight (AB)
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15 MIN
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AS, Flaps 1%-45%
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300 KCAS
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AS, Flaps 46%-60%
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240 KCAS
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AS, Flaps Over 60%
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220 KCAS
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AS, Canopy
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50 KCAS
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AS, Gear/Gear Doors
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240 KCAS
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AS, Nose Wheel Steering
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65 Kts GS
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AS, Main Wheel Tire, 14 ply
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204 Kts GS
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AS, Main Wheel Tire, 12 ply
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195 Kts GS
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AS, Nose Wheel Tire
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174 Kts GS
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Hyd Press, Min
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1500 PSI
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Hyd Press, Max
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3200 PSI
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Hyd Press, Normal Range
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2850 - 3200 PSI
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WSSP, Capacity
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140 LBS
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WSSP, Sym
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0 to +4.0
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WSSP, Asym
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0 to +3.0
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WSSP, AS, Max
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400 KCAS
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WSSP, AS, SB Open/Turb
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350 KCAS
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WSSP, AS, Abrupt Control
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240 KCAS
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Oxygen Press, Normal Range
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50 to 120 PSI
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Extension/retraction of landing gear at bank angles greater than ____ º or at load factors greater than ____ G can result in overstress failure of the main landing gear sidebrace trunion.
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45º, 1.5G
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Max Sym G, 3500 LBS
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-2.3 to +5.7
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Max Asym G, 3500 LBS
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0 to +4.1
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Max Sym G, 3000 LBS
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-2.4 to +5.9
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Max Asym G, 3000 LBS
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0 to +4.3
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Max Sym G, 2000 LBS
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-2.6 to +6.5
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Max Asym G, 2000 LBS
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0 to +4.7
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Max Sym G, 1000 LBS
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-2.9 to +7.2
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Max Asym G, 1000 LBS
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0 to +5.0
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Abort start if EGT reaches ____ ºC to preclude exceeding temperature limits.
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845ºC
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Abort aircraft during ground start if EGT exceeds ____ ºC momentarily.
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925ºC
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Maximum allowable transient RPM ____ %.
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107%
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Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within ____ seconds.
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10 seconds
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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 LB/HR and 360 LB/HR
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Do not exceed ____ minutes in military power with oil pressure above ____ PSI.
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5 MIN, 55 PSI
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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.
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10 PSI
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DASH-1 Prohibited Manuevers
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1. Vertical Stalls
2. Intentional Spins 3. Continuous aileron rolls (more than one complete roll) will be accomplished only at 1.0 G and 3/4 or less stick deflection. |
