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77 Cards in this Set

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