| Condition | Engine | |||||
|---|---|---|---|---|---|---|
| EGT °C |
RPM % |
Nozzle Position % |
Fuel Flow LB / HR |
Oil Pressure PSI |
Time Duration (Minutes) |
|
| Ground Steady State | ||||||
| Start | * (Max) | *** (Max) | **** | |||
| Idle | - | - | - (Std Day) | - | ||
| Military | - | - | - | - (Sea Level) | - | |
| (Max) / Afterburner | - | - | - | - | ||
| Flight Steady State | ||||||
| Start | * (Max) | *** (Max) | **** | |||
| Idle | (Min) (Std Day) | (Min) | ||||
| Military | - | - | - | - | ||
| (Max) / Afterburner | - | - | - | - | ||
| Fluctuation Limits (Within Steady State Limits) | ||||||
| Idle (Ground) | - | None Allowed | ± | ± | ||
| MIL and AB (Ground) |
** | - | ± | ± | ± | |
| MIL and AB (Flight) | ** | ± | ± | ± | ± | |
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.
RPM: Maximum allowable transient RPM %.
Nozzle Position: Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within seconds.
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 to or less than LB/HR prior to EGT rise during actual engine start.
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.
| Airspeed | Load Factor | |||
|---|---|---|---|---|
| Flaps 1% - 45% | KCAS | Fuel (LBS) | Max Sym G | Max Asym G |
| Flaps 46% - 60% | KCAS | 3500 | to | to |
| Flaps Over 60% | KCAS | 3000 | to | to |
| Canopy | KCAS | 2000 | to | to |
| Gear / Gear Doors | KCAS | 1000 | to | to |
| Nose Wheel Steering | Kts GS | 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 sidebrace trunnion. | ||
| Main Wheel Tire | Kts GS | |||
| Nose Wheel Tire | Kts GS | |||
| Hydraulic Pressure | Oxygen Pressure | ||||
|---|---|---|---|---|---|
| Min PSI | Max PSI | Normal Range | PSI to PSI | ||
| Normal Range | PSI to PSI | ||||
| WSSP Limitations: | Sym to | Asym to | Normal Capacity LBS |
| Airspeed Limits: | Max KCAS | SB Open / Turbulence KCAS | Abrupt Control KCAS |