Boldface / Ops Limits Flashcards
Abort
THROTTLES - IDLE
WHEEL BRAKES - AS REQUIRED
Engine Failure / Fire Warning During Takeoff, Takeoff Continued
THROTTLES - MAX
FLAPS - 60 %
AIRSPEED - ATTAIN SETOS MINIMUM
Tire Failure During Takeoff, Takeoff Continued
GEAR - DO NOT RETRACT
Fire Warning During Flight (Affected Engine)
THROTTLE - IDLE
THROTTLE - OFF, IF FIRE LIGHT REMAINS ON
IF FIRE IS CONFIRMED - EJECT
Ejection
EJECTION HANDLE - PULL
Alternate Airstart / Loss of Thrust (Low Altitude)
THROTTLE(S) - MAX
SPEED BRAKE - CONFIRM CLOSED
Single-Engine Go-Around
THROTTLE(S) - MAX
FLAPS - 60 %
AIRSPEED - ATTAIN FINAL APPROACH SPEED MINIMUM
EGT (Ground)
Start: ____ (Max) ____
925, 845
EGT (Ground)
Military
630-650
EGT (Ground)
Max/Afterburner
630-650
EGT (Flight)
Start: ____ (Max)
925
EGT (Flight)
Military
630-650
EGT (Flight)
Max/Afterburner
630-650
RPM (Ground)
Idle
46-50
RPM (Ground)
Military
99-101
RPM (Ground)
Max/Afterburner
99-101
RPM (Flight)
Military
99-104
RPM (Flight)
Max/Afterburner
99-104
RPM (Fluctuation)
Idle (Ground)
46-50
RPM (Fluctuation)
MIL/AB (Ground)
99-101
RPM (Fluctuation)
MIL/AB (Flight)
+/- 1
Nozzle Position (Ground) Idle
77-92
Nozzle Position (Ground) Military
0-20
Nozzle Position (Ground) Max/Afterburner
50-85
Nozzle Position (Flight) Military
0-20
Nozzle Position (Flight) Max/Afterburner
50-85
Nozzle Position (Fluctuation) Idle (Ground)
None Allowed
Nozzle Position (Fluctuation) MIL/AB (Ground)
+/- 3
Nozzle Position (Fluctuation) MIL/AB (Flight)
+/- 3
Fuel Flow (Ground) Start: \_\_\_\_ (Max)
360
Fuel Flow (Ground) Idle: \_\_\_\_ - \_\_\_\_ (STD Day)
400, 600
Fuel Flow (Ground) MIL: \_\_\_\_ - \_\_\_\_ (Sea Level)
2100, 2700
Fuel Flow (Flight) Start: \_\_\_\_ (Max)
360
Fuel Flow (Flight) Idle: \_\_\_ (Min) (STD Day)
200
Fuel Flow (Fluctuation) Idle (Ground)
+/- 25
Fuel Flow (Fluctuation) MIL/AB (Ground)
+/- 50
Fuel Flow (Fluctuation) MIL/AB (Flight)
+/- 50
Oil Pressure (Ground) Idle
5-20
Oil Pressure (Ground) Military
20-55
Oil Pressure (Ground) Max/Afterburner
20-55
Oil Pressure (Flight) Idle: \_\_\_\_ (Min)
5
Oil Pressure (Flight) Military
20-55
Oil Pressure (Flight) Max/Afterburner
20-55
Oil Pressure (Fluctuation) Idle (Ground)
+/- 2
Oil Pressure (Fluctuation) MIL/AB (Ground)
+/- 2
Oil Pressure (Fluctuation) MIL/AB (Flight)
+/- 2
Time (Duration)
Ground - Military
5
Time (Duration)
Ground - Max/AB
5
Time (Duration)
Flight - Military
30
Time (Duration)
Flight - Max/AB
15
EGT: Abort start if EGT reaches ____C to preclude exceeding temperature limits. Abort aircraft during ground start if EGT exceeds ____C momentarily. Total fluctuations in EGT of ____C (+/- ____C) are acceptable if the average EGT is between ____C and ____C.
845, 925, 15, 7.5, 630, 650
RPM: Maximum allowable transient RPM ____ %.
107
Nozzle Position: Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within ____ seconds.
10
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 or less than ____ LB/HR prior to EGT rise during actual engine start.
360, 360
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. 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.
5, 55, 10
Airspeed
Flaps 1%-45%
300
Airspeed
Flaps 46%-60%
240
Airspeed
Flaps over 60%
220
Airspeed
Canopy
50
Airspeed
Gear/Gear Doors
240
Ground Speed
Nose Wheel Steering
65
Ground Speed
Main Wheel Tire
221
Ground Speed
Nose Wheel Tire
174
Load Factor
3500# - Sym
-2.3 to +5.7
Load Factor
3000# - Sym
-2.4 to +5.9
Load Factor
2000# - Sym
-2.6 to +6.5
Load Factor
1000# - Sym
-2.9 to +7.2
Load Factor
3500# - Asym
0 to +4.1
Load Factor
3000# - Asym
0 to +4.3
Load Factor
2000# - Asym
0 to +4.7
Load Factor
1000# - Asym
0 to +5.0
Caution: Extension/retraction of landing gear at bank angles greater than ____* or at load factors greater than ____ G can result in over stress failure of the main landing gear sidebrace trunnion.
45, 1.5
Hydraulic Pressure
Minimum PSI
1500
Hydraulic Pressure
Maximum PSI
3200
Hydraulic Pressure
Normal Range PSI
2850-3200
Oxygen Pressure
Normal Range PSI
50-120
WSSP Limits
Sym G
0 to +4.0
WSSP Limits
Asym G
0 to +3.0
WSSP Limits Normal Capacity (LBS)
140
Airspeed Limits
Max
400
Airspeed Limits
SB Open / Turbulence
350
Airspeed Limits
Abrupt Control
240
Dash-1 Prohibited Maneuvers
- Vertical Stalls
- Intentional Spins
- Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection.