Ops Limits Flashcards
Start EGT °C
Ground
* ____ (MAX) ____
925
845
Start Fuel Flow LB / HR
Ground
*** ____ (MAX)
360
Idle RPM %
Ground
46 - 50
Idle Nozzle Position %
Ground
77 - 92
Idle Fuel Flow LB / HR
Ground
____ - ____ (Std Day)
400 - 600
Idle Oil Pressure PSI
Ground
5 - 20
Military EGT °C
Ground
630 - 650
Military RPM %
Ground
99 - 101
Military Nozzle Position %
Ground
0 - 20
Military Fuel Flow LB / HR
Ground
____ - _____ (Sea Level)
2100 - 2700
Military Oil Pressure PSI
Ground
20 -55
Military Time Duration (Minutes)
Ground
5
(MAX) / Afterburner EGT °C
Ground
630 - 650
(MAX) / Afterburner RPM %
Ground
99 - 101
(MAX) / Afterburner Nozzle Position %
Ground
50 - 85
(MAX) / Afterburner Oil Pressure PSI
Ground
20 - 55
(MAX) / Afterburner Time Duration (Minutes)
Ground
5
Start EGT °C
Flight Steady State
* ____ (MAX)
925
Start Fuel Flow LB / HR
Flight Steady State
*** ____ (MAX)
360
Idle Fuel Flow LB / HR
Flight Steady State
____ (Min) (Std Day)
200
Idle Oil Pressure PSI
Flight Steady State
____ (Min)
5
Military EGT °C
Flight Steady State
630 - 650
Military RPM %
Flight Steady State
99 - 104
Military Nozzle Position %
Flight Steady State
0 - 20
Military Oil Pressure PSI
Flight Steady State
20 - 55
Military Time Duration (Minutes)
Flight Steady State
30
(MAX) / Afterburner EGT °C
Flight Steady State
630 - 650
(MAX) / Afterburner RPM %
Flight Steady State
99 - 104
(MAX) / Afterburner Nozzle Position %
Flight Steady State
50 - 85
(MAX) / Afterburner Oil Pressure PSI
Flight Steady State
20 - 55
(MAX) / Afterburner Time Duration (Minutes)
Flight Steady State
15
Idle (Ground) RPM % Fluctuation Limits (Within Steady State Limits)
46 - 50
Idle (Ground) Fuel Flow LB / HR Fluctuation Limits (Within Steady State Limits)
±25
Idle (Ground) Oil Pressure PSI Fluctuation Limits (Within Steady State Limits)
±2
MIL and AB (Ground) RPM % Fluctuation Limits (Within Steady State Limits)
99 - 101
MIL and AB (Ground) Nozzle Position % Fluctuation Limits (Within Steady State Limits)
±3
MIL and AB (Ground) Fuel Flow LB / HR Fluctuation Limits (Within Steady State Limits)
±50
MIL and AB (Ground) Oil Pressure PSI Fluctuation Limits (Within Steady State Limits)
±2
MIL and AB (Flight) RPM % Fluctuation Limits (Within Steady State Limits)
±1
MIL and AB (Flight) Nozzle Position % Fluctuation Limits (Within Steady State Limits)
±3
MIL and AB (Flight) Fuel Flow LB / HR Fluctuation Limits (Within Steady State Limits)
±50
MIL and AB (Flight) Oil Pressure PSI Fluctuation Limits (Within Steady State Limits)
±2
EGT: * Abort start if EGT reaches _____ °C to preclude exceeding temperature limits. Abort aircraft during ground start if EGT exceeds ____°C momentarily
845
925
EGT: ** Total fluctuations in EGT of ____°C (+/- ___°C) are acceptable if the average EGT is between _____°C and ____°C
15; 7.5
630
650
RPM: Maximum allowable transient RPM ____ %
107
Nozzle Position: Following rapid throttle movements, nozzle position should stabilise 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 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
Flaps 1% - 45% Airspeed
300 KCAS
Flaps 46 - 60% Airspeed
240 KCAS
Flaps Over 60% Airspeed
220 KCAS
Canopy Airspeed
50 KCAS
Gear / Gear Doors Airspeed
240 KCAS
Nose Wheel Steering
65 Kts GS
Main Wheel Tire
221 (14 ply) Kts GS
195 (12 ply) Kts GS
Nose Wheel Tire
174 Kts GS
Hydraulic Pressure min PSI
1500
Hydraulic Pressure max PSI
3200
Hydraulic Pressure Normal Range
2850 PSI to 3200 PSI
WSSP Limitations:
Sym
Asym
Normal Capacity
0 to +4.0
0 to +3.0
140 LBS
WSSP Airspeed limits:
MAX
SB Open / Turbulence
Abrupt Control
400 KCAS
350 KCAS
240 KCAS
DASH -1 Prohibited Maneuvers 1.
Vertical Stalls
DASH -1 Prohibited Maneuvers 2.
Intentional Spins
DASH -1 Prohibited Maneuvers 3.
Continuous aileron rolls at other than 1.0g and/or greater than 3/4 stick deflection.
Oxygen Pressure Normal Range
50 PSI to 120 PSI
Load Factor Fuel 3500 LBS
MAX Sym G -2.3 to +5.7
MAX Asym G 0 to +4.1
Load Factor Fuel 3000 LBS
MAX Sym G -2.4 to +5.9
MAX Asym G 0 to +4.3
Load Factor Fuel 2000 LBS
MAX Sym G -2.6 to +6.5
MAX Asym G 0 to +4.7
Load Factor Fuel 1000 LBS
MAX Sym G -2.9 to +7.2
MAX Asym G 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 overstress failure of the main landing gear side brace trunnion.
45
1.5