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Su-25T Frogfoot Emergency Procedures
Immediate Action Procedures
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6 procedures
- 1Affected throttleIDLE
- 2Affected fuel cockCLOSE
- 3Fire warningMONITOR for extinguish
- 4Remaining engineMILITARY POWER
- 5If fire persists after 30 secprepare to EJECT
- 6Airspeedmaintain > 300 km/h
- 7Land immediately at nearest suitable airfield
- 1Failed engine throttleIDLE then CLOSE fuel cock
- 2Remaining engineMILITARY POWER
- 3Airspeedmaintain > 300 km/h
- 4Asymmetric thrustCORRECT with rudder
- 5Declare emergencyadvise ATC intentions
- 6Land at nearest suitable airfield
- 1Both throttlesIDLE
- 2Airspeedmaintain 350-400 km/h (best glide)
- 3Relight attemptadvance throttle to IDLE gate, monitor for restart
- 4MAYDAYDECLARE on guard frequency
- 5If restart fails below 1,500 m AGLEJECT immediately
- 6K-36D seatzero-zero capable, eject early
- 1Hydraulic pressureCHECK gauges (Hyd 1 / Hyd 2)
- 2Control forcesEXPECT increased resistance on affected system
- 3Flight controlsuse caution, avoid abrupt inputs
- 4Landing gearuse emergency extension if primary system fails
- 5Brakesuse emergency brake system
- 6Approach speedADD 20-30 km/h margin
- 7Land as soon as practical
- 1Throttle(s)IDLE
- 2Affected fuel cock(s)CLOSE
- 3FireMONITOR for extinguish
- 4Flight controlsCHECK for damage / asymmetry
- 5If fire not extinguished within 30 secEJECT
- 6If controllableclimb above 300 m AGL before ejecting
- 7Eject if fire spreading or aircraft uncontrollable
- 1AirspeedREDUCE below 900 km/h if possible
- 2AircraftFLY WINGS LEVEL
- 3AltitudeCLIMB above 100 m AGL minimum
- 4Canopy jettison handlePULL (seat fires through canopy if needed)
- 5Ejection handlePULL firmly between legs
- 6Seat fires automaticallydo not interfere with sequence
- 7On ground: harness release and move clear of aircraft
FLIGHT2.23.0Checklist
Su-25T FrogfootDCS WORLD · Emergency Procedures · 6procedures · 40 steps
Engine Fire - In Flight7 steps
| 01 | Affected throttleIDLE | |
| 02 | Affected fuel cockCLOSE | |
| 03 | Fire warningMONITOR for extinguish | |
| 04 | Remaining engineMILITARY POWER | |
| 05 | If fire persists after 30 secprepare to EJECT | |
| 06 | Airspeedmaintain > 300 km/h | |
| 07 | Land immediately at nearest suitable airfield |
Engine Failure - Single Engine6 steps
| 01 | Failed engine throttleIDLE then CLOSE fuel cock | |
| 02 | Remaining engineMILITARY POWER | |
| 03 | Airspeedmaintain > 300 km/h | |
| 04 | Asymmetric thrustCORRECT with rudder | |
| 05 | Declare emergencyadvise ATC intentions | |
| 06 | Land at nearest suitable airfield |
Dual Engine Flameout6 steps
| 01 | Both throttlesIDLE | |
| 02 | Airspeedmaintain 350-400 km/h (best glide) | |
| 03 | Relight attemptadvance throttle to IDLE gate, monitor for restart | |
| 04 | MAYDAYDECLARE on guard frequency | |
| 05 | If restart fails below 1,500 m AGLEJECT immediately | |
| 06 | K-36D seatzero-zero capable, eject early |
Hydraulic Failure7 steps
| 01 | Hydraulic pressureCHECK gauges (Hyd 1 / Hyd 2) | |
| 02 | Control forcesEXPECT increased resistance on affected system | |
| 03 | Flight controlsuse caution, avoid abrupt inputs | |
| 04 | Landing gearuse emergency extension if primary system fails | |
| 05 | Brakesuse emergency brake system | |
| 06 | Approach speedADD 20-30 km/h margin | |
| 07 | Land as soon as practical |
Battle Damage / Uncontrolled Fire7 steps
| 01 | Throttle(s)IDLE | |
| 02 | Affected fuel cock(s)CLOSE | |
| 03 | FireMONITOR for extinguish | |
| 04 | Flight controlsCHECK for damage / asymmetry | |
| 05 | If fire not extinguished within 30 secEJECT | |
| 06 | If controllableclimb above 300 m AGL before ejecting | |
| 07 | Eject if fire spreading or aircraft uncontrollable |
Ejection7 steps
| 01 | AirspeedREDUCE below 900 km/h if possible | |
| 02 | AircraftFLY WINGS LEVEL | |
| 03 | AltitudeCLIMB above 100 m AGL minimum | |
| 04 | Canopy jettison handlePULL (seat fires through canopy if needed) | |
| 05 | Ejection handlePULL firmly between legs | |
| 06 | Seat fires automaticallydo not interfere with sequence | |
| 07 | On ground: harness release and move clear of aircraft |