Boldface/Ops Limits Flashcards
Tire Failure During Takeoff, Takeoff Continued
GEAR-DO NOT RETRACT
Time Duration Ground Steady State Start
NONE
RPM Flight Steady State (Max)/Afterburner
99-104%
EGT Ground Steady State Start
925 (Max) 845 deg C
Fire Warning During Flight (Affected Engine)
THROTTLE-IDLE
THROTTLE-OFF, IF FIRE LIGHT REMAINS ON
IF FIRE IS CONFIRMED-EJECT
EGT Ground Steady State Military
630-650 deg C
EGT Ground Steady State (Max)/Afterburner
630-650 deg C
Alternate Airstart/Loss of Thrust (Low Altitude)
THROTTLE(S)-MAX
SPEED BRAKE-CONFIRM CLOSED
EGT Flight Steady State (Max)/Afterburner
630-650 deg C
EGT Flight Steady State Start
925 (Max) deg C
EGT Flight Steady State Military
630-650 deg C
Ejection
EJECTION HANDLE-PULL
RPM Ground Steady State Idle
46-50%
RPM Ground Steady State Military
99-101%
RPM Ground Steady State (Max)/Afterburner
99-101%
Engine Failure/Fire Warning During Takeoff, Takeoff Continued
THROTTLES-MAX
FLAPS-60%
AIRSPEED-ATTAIN SETOS MINIMUM
RPM Flight Steady State Military
99-104%
RPM Fluctuation Limits (Within Steady State Limits)
46-50%
Abort
THROTTLES-IDLE
WHEEL BRAKES-AS REQUIRED
Airspeed Canopy
50 KCAS
Nozzle Position Ground Steady State Military
0-20%
RPM Fluctuation Limits (Within Steady State Limits) MIL and AB (Ground)
99-101%
Load Factor (3000 lbs) Max Sym G
-2.4 to +5.9 Gs
Nozzle Position Ground Steady State (Max)/Afterburner
50-85%
Nozzle Position Flight Steady State Military
0-20%
Nozzle Position Flight Steady State (Max)/Afterburner
50-85%
Nozzle Position Fluctuation Limits (Within Steady State Limits) Idle (Ground)
None Allowed
Time Duration Flight Steady State Idle
NONE
Nozzle Position Fluctuation Limits (Within Steady State Limits) MIL and AB (Ground)
+/-3
Airspeed Flaps 1%-45%
300 KCAS
Nozzle Position Ground Steady State Idle
77-92%
Airspeed Flaps Over 60%
220 KCAS
Airspeed limits max? Airspeed limits SB open/turbulence? Airspeed abrupt control?
400 KCAS
350 KCAS
240 KCAS
Nozzle Position Fluctuation Limits (Within Steady State Limits) MIL and AB (Flight)
+/-3
Fuel Flow Flight Steady State Military
NONE
Airspeed NWS
65 Kts GS
Airspeed Main Wheel Tire
221 Kts GS
Load Factor (3500 lbs) Max Sym G
-2.3 to +5.7 Gs
Load Factor (2000 lbs) Max Sym G
-2.6 to +6.5 Gs
Airspeed Nose Wheel Tire
174 Kts GS
Load Factor (1000 lbs) Max Sym G
-2.9 to +7.2 Gs
Load Factor (3000 lbs) Max Asym G
0 to +4.3 Gs
Airspeed Gear/Gear Doors
240 KCAS
Load Factor (2000 lbs) Max Asym G
0 to +4.7 Gs
Load Factor (1000 lbs) Max Asym G
0 to +5.0 Gs
Fuel Flow Flight Steady State (Max)/Afterburner
NONE
What is the hydraulic pressure min PSI?
1500 psi
Fuel flow fluctuation limits (within Steady State limits) MIL and AB (Flight)
+/-50 lbs/ hr
RPM Fluctuation Limits (Within Steady State Limits) MIL and AB (Flight)
+/-1
What is the hydraulic pressure max PSI?
3200 psi
Airspeed Flaps 46%-60%
240 KCAS
What is oxygen pressure normal range?
50 to 120 psi
WSSP Sym limitations? Asym limitations? Normal capacity?
0 to +4.0
0 to +3.0
140 lbs
Time Duration Ground Steady State Idle
NONE
What are the 3 prohibited maneuvers?
- Vertical Stalls
- Intentional Spins
- Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection.
What is the max bank angle for extension/retraction of the landing gear?
45 deg
EGT Fluctuation Limits (Within Steady State Limits) IDLE (Ground)
NONE
What is the max load factor for extension/retraction of the landing gear?
1.5 G
Time Duration Flight Steady State Start
NONE
Fuel flow ground Steady State start?
360 (max) lbs/hr
Fuel flow ground Steady State idle?
400-600 lbs/hr (std day)
Fuel flow ground Steady State Military?
2100-2700 (sea level) lbs/hr
What is the hydraulic normal range?
2850 to 3200 psi
Fuel flow flight Steady State start?
360 (Max) lbs/hr
Fuel flow flight Steady State idle?
200 (Min) (Std Day) lbs/hr
Fuel flow fluctuation limits (within Steady State limits) Idle (Ground)
+/-25 lbs/hr
Fuel flow fluctuation limits (within Steady State limits) MIL and AB (Ground)
+/-50 lbs/hr
Oil pressure ground Steady State idle?
5-20 psi
Oil pressure ground Steady State (max)/afterburner?
20-55 psi
Oil pressure Flight Steady State IDLE?
5 (Min)
Oil pressure Flight Steady State Military?
20-55 psi
Oil pressure Flight Steady State (Max)/Afterburner?
20-55 psi
Nozzle Position Flight Steady State Idle
NONE
Oil pressure fluctuation limits (within Steady State limits) (all cases)
+/-2 psi
Time duration ground Steady State Military
5 min
Time duration ground Steady State (Max) Afterburner
5 Min
Time duration Flight Steady State military
30 min
Time duration Flight Steady State (Max)/Afterburner
15 Min
Abort start if EGT reaches what temperature (to preclude exceeding temperature limits)?
845 deg C
Nozzle Position Ground Steady State Start
NONE
What is the max allowable transient RPM?
107%
What total EGT fluctuations are acceptable and in what case?
15 deg C (plus or minus 7.5 deg C) if average EGT is between 630 and 650 deg C
Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within what?
10 seconds
Oil pressure ground Steady State Military?
20-55 psi
Indicated fuel flow should return to equal to or less than what prior to EGT rise during actual engine start?
360 lb/hr
RPM Ground Steady State Start
NONE
Do not exceed oil pressure limits in military power with oil pressure above what for how long?
55 psi
5 min
Execute the engine oil system malfunction procedures in Section III of the DASH 1 if you have a sudden change in oil pressure of what?
10 psi or greater
Abort aircraft during ground start if EGT exceeds what momentarily?
925 deg C
EGT Flight Steady State Idle
NONE
Load Factor (3500 lbs) Max Asym G
0 to +4.1 Gs
Single-Engine Go-Around
THROTTLE(S)-MAX
FLAPS-60%
AIRSPEED-ATTAIN FINAL APPROACH SPEED MINIMUM
Time Duration Fluctuation Limits (Within Steady State Limits) (any)
NONE
RPM Flight Steady State Start
NONE
RPM Flight Steady State Idle
NONE
Fluctuation Limits (Within Steady State Limits) Idle (Ground)
None Allowed
Fuel Flow Ground Steady State (Max)/Afterburner
NONE
Nozzle Position Flight Steady State Start
NONE
EGT Ground Steady State IDLE
NONE
