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MSFS 2024 · Airliner
McDonnell Douglas MD-82 Emergency Procedures
Immediate Action Procedures
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12 procedures
- 1ThrottleIDLE
- 2If fire warning ceases and damage is not suspectedCONTINUE ENGINE OPERATION AT CAPTAIN'S DISCRETION
- 3Fuel LeverOFF
- 4Engine Fire HandlePULL
- 5Fire AgentDISCHARGE
- 6If ENG Fire light remains illuminated after 30 secDISCHARGE REMAINING BOTTLE AGENT
- 7Pneumatic CrossfeedCLOSE
- 8Aux or Trans Hydraulic PumpAS REQUIRED
- 9Fuel Tank Pumps and X-FeedAS REQUIRED
- 10Electrical LoadsCHECKED
- 11When takeoff thrust no longer required, Air Conditioning Shutoff Switch - OVERRIDE
- 12AC Supply Switch (affected engine)OFF
- 1ThrottleIDLE
- 2Fuel Control LeverOFF
- 3Pneumatic CrossfeedCLOSE
- 4Aux or Trans Hydraulic PumpAS REQUIRED
- 5Fuel Tank Pumps and X-FeedAS REQUIRED
- 6Electrical LoadsCHECKED
- 7When takeoff thrust no longer required, Air Conditioning Shutoff Switch - OVERRIDE
- 8AC Supply Switch (affected engine)OFF
- 9Restricted rudder may result after applying maximum rudder due to asymmetric thrust; centering the rudder pedals momentarily during deceleration may allow the rudder throw limiter to return to the speed-scheduled position
- 1Emergency Power SwitchON
- 2ENG IGN SwitchOVRD
- 3ThrottlesIDLE
- 4Airspeed - OPTIMUM GLIDE SPEED (190 kt at 80,000 lb to 270 kt at 160,000 lb, clean)
- 5Battery SwitchON / LOCKED
- 6START Pump SwitchON
- 7All FUEL BOOST Pump SwitchesON
- 8ENG ANTI-ICE SwitchesON
- 9FUEL X-FEED LeverON
- 10If both engines start - RESTORE SYSTEMS AND LAND AT NEAREST SUITABLE AIRPORT
- 11If neither engine starts - APU START, FUEL LEVERS OFF, THEN ON AFTER 20 SECONDS, REPEAT UNTIL AN ENGINE STARTS
- 1EMER PWR SwitchON
- 2Battery SwitchON
- 3CABIN PRESS Control LeverMANUAL
- 4AC BUS XTIE SwitchOPEN
- 5Galley PowerOFF
- 6L GEN (or APU) SwitchRESET / ON (NORMAL)
- 7R GEN (or APU) SwitchRESET / ON (NORMAL)
- 8Generator OperationCHECK
- 9If generator operation not normal - L AND R GEN SWITCHES OFF, APU WINDMILL START IF AVAILABLE
- 10Prior to landingONE AC SUPPLY SWITCH OFF
- 1Master WarningPUSH TO RESET
- 2APU Fire Control SwitchOFF AND AGENT ARM
- 3If the APU does not shut downPULL APU CONTROL CB (OVERHEAD PANEL B-21)
- 4If APU fire warning persistsAPU FIRE AGENT NO. 1 OR NO. 2 DISCHARGE
- 5If APU FIRE warning remains on after 30 seconds2ND APU FIRE AGENT DISCHARGE
- 6APU Master SwitchOFF
- 7APU DoorsAUTO
- 1Stabilizer Trim Switch (left side center pedestal)STOP
- 2If the stabilizer continues to run awayPRIMARY SYSTEM (RED GUARDED SWITCH) RESTORE
- 3TrimMAINTAIN WITH PRIMARY SYSTEM
- 4AUTOPILOT and ALTERNATE LONGITUDINAL TRIM C-Bs (Upper EPC D9, D10 and D11) - PULL
- 1Oxygen Masks and InterphoneON AND 100 PERCENT
- 2Crew CommunicationsESTABLISHED
- 3Manual Cabin Alt ControlFULL FORWARD AND MANUALLY LOCKED
- 4Pneumatic X-Feed ValvesCLOSED
- 5Air Conditioning Supply SwitchesAUTO
- 6Passenger Oxygen MaskDEPLOYED
- 7Master Warning LightRESET
- 8Radio Rack SwitchFAN
- 9If requiredINITIATE EMERGENCY DESCENT
- 1Speed BrakesEXTEND
- 2ThrottlesIDLE
- 3DescendMACH 0.80 TO 0.82 / 320-340 KIAS
- 4Altitude SelectLEVEL OFF ALTITUDE ARMED
- 5IgnitionOVRD
- 6Seat Belt SwitchON
- 7Autopilot / AutothrottlesOFF
- 8Transponder7700
- 9ATCNOTIFY
- 10AltimetersFL180 OR TRANSITION ALTITUDE
- 11If structural integrity is in doubtAVOID HIGH IAS AND ABRUPT MANEUVERS
- 1PUSH DSCH SwitchPUSH
- 2TimeNOTE
- 3Second Halon bottle discharges automatically 5 minutes after release of the PUSH DSCH switch
- 4Diversion - START IMMEDIATELY TO THE NEAREST SUITABLE AIRPORT, DO NOT DELAY
- 5The aircraft must land within 78 minutes after activation of bottle 1
- 1Oxygen Masks, Goggles and InterphoneON AND 100 PERCENT
- 2Crew CommunicationsESTABLISHED
- 3Radio Rack SwitchVENTURI
- 4Cabin Altitude (Pressure) Control LeverMANUAL AND LOCK IN EXISTING POSITION
- 5AC Cross Tie SwitchOPEN
- 6R GEN Control Switch (or R APU Bus Switch) if power sourceOFF
- 7If smoke continues - R GEN CONTROL SWITCH BACK ON, THEN L GEN CONTROL SWITCH OFF
- 8If smoke disappearsPROCEED TO ISOLATION CHECKLIST
- 9CabinDEPRESSURIZE PRIOR TO LANDING
- 1Tower (time permitting)CALL
- 2Parking BrakesSET
- 3SPD BRK / SPOILER LeverRETRACTED
- 4Flaps28 DEG
- 5Fuel LeversOFF
- 6EMER PWR SelectorON
- 7Command EvacuationEVACUATE, THREE TIMES
- 8EMER LTS SwitchON
- 9Engine Fire HandlesPULL
- 10Fire Bottles (if required)DISCHARGE
- 11APU FIRE CONT Switch (if APU operating)OFF AND AGENT ARM
- 12Cockpit Voice Recorder C-B (Upper EPC F6)PULL
- 1CallSTALL, FULL POWER
- 2Full power - APPLY (if ground contact is imminent, throttles fully forward)
- 3Autopilot - DISCONNECT, be alert to counteract an excessive nose-up trim condition
- 4Wings - LEVEL, adjust pitch to minimize altitude loss or obtain obstacle clearance
- 5Above FL250 - ACCEPT ALTITUDE LOSS WHILE ACCELERATING, MAINTAIN EXISTING CONFIGURATION
- 6Below FL250 - EXTEND SLATS IF CLEAN, ACCELERATE TO THE MINIMUM SPEED FOR THE CONFIGURATION, THEN ADJUST CONFIGURATION AS DESIRED
FLIGHT2.22.0Checklist
McDonnell Douglas MD-82MSFS 2024 · Emergency Procedures · 12procedures · 105 steps
Engine Fire / Severe Damage / Separation12 steps
| 01 | ThrottleIDLE | |
| 02 | If fire warning ceases and damage is not suspectedCONTINUE ENGINE OPERATION AT CAPTAIN'S DISCRETION | |
| 03 | Fuel LeverOFF | |
| 04 | Engine Fire HandlePULL | |
| 05 | Fire AgentDISCHARGE | |
| 06 | If ENG Fire light remains illuminated after 30 secDISCHARGE REMAINING BOTTLE AGENT | |
| 07 | Pneumatic CrossfeedCLOSE | |
| 08 | Aux or Trans Hydraulic PumpAS REQUIRED | |
| 09 | Fuel Tank Pumps and X-FeedAS REQUIRED | |
| 10 | Electrical LoadsCHECKED | |
| 11 | When takeoff thrust no longer required, Air Conditioning Shutoff Switch - OVERRIDE | |
| 12 | AC Supply Switch (affected engine)OFF |
Engine Failure / Inflight Shutdown9 steps
| 01 | ThrottleIDLE | |
| 02 | Fuel Control LeverOFF | |
| 03 | Pneumatic CrossfeedCLOSE | |
| 04 | Aux or Trans Hydraulic PumpAS REQUIRED | |
| 05 | Fuel Tank Pumps and X-FeedAS REQUIRED | |
| 06 | Electrical LoadsCHECKED | |
| 07 | When takeoff thrust no longer required, Air Conditioning Shutoff Switch - OVERRIDE | |
| 08 | AC Supply Switch (affected engine)OFF | |
| 09 | Restricted rudder may result after applying maximum rudder due to asymmetric thrust; centering the rudder pedals momentarily during deceleration may allow the rudder throw limiter to return to the speed-scheduled position |
Loss of All Engines11 steps
| 01 | Emergency Power SwitchON | |
| 02 | ENG IGN SwitchOVRD | |
| 03 | ThrottlesIDLE | |
| 04 | Airspeed - OPTIMUM GLIDE SPEED (190 kt at 80,000 lb to 270 kt at 160,000 lb, clean) | |
| 05 | Battery SwitchON / LOCKED | |
| 06 | START Pump SwitchON | |
| 07 | All FUEL BOOST Pump SwitchesON | |
| 08 | ENG ANTI-ICE SwitchesON | |
| 09 | FUEL X-FEED LeverON | |
| 10 | If both engines start - RESTORE SYSTEMS AND LAND AT NEAREST SUITABLE AIRPORT | |
| 11 | If neither engine starts - APU START, FUEL LEVERS OFF, THEN ON AFTER 20 SECONDS, REPEAT UNTIL AN ENGINE STARTS |
Loss of Both Engine Generators10 steps
| 01 | EMER PWR SwitchON | |
| 02 | Battery SwitchON | |
| 03 | CABIN PRESS Control LeverMANUAL | |
| 04 | AC BUS XTIE SwitchOPEN | |
| 05 | Galley PowerOFF | |
| 06 | L GEN (or APU) SwitchRESET / ON (NORMAL) | |
| 07 | R GEN (or APU) SwitchRESET / ON (NORMAL) | |
| 08 | Generator OperationCHECK | |
| 09 | If generator operation not normal - L AND R GEN SWITCHES OFF, APU WINDMILL START IF AVAILABLE | |
| 10 | Prior to landingONE AC SUPPLY SWITCH OFF |
APU Fire7 steps
| 01 | Master WarningPUSH TO RESET | |
| 02 | APU Fire Control SwitchOFF AND AGENT ARM | |
| 03 | If the APU does not shut downPULL APU CONTROL CB (OVERHEAD PANEL B-21) | |
| 04 | If APU fire warning persistsAPU FIRE AGENT NO. 1 OR NO. 2 DISCHARGE | |
| 05 | If APU FIRE warning remains on after 30 seconds2ND APU FIRE AGENT DISCHARGE | |
| 06 | APU Master SwitchOFF | |
| 07 | APU DoorsAUTO |
Runaway Stabilizer Trim4 steps
| 01 | Stabilizer Trim Switch (left side center pedestal)STOP | |
| 02 | If the stabilizer continues to run awayPRIMARY SYSTEM (RED GUARDED SWITCH) RESTORE | |
| 03 | TrimMAINTAIN WITH PRIMARY SYSTEM | |
| 04 | AUTOPILOT and ALTERNATE LONGITUDINAL TRIM C-Bs (Upper EPC D9, D10 and D11) - PULL |
Cabin Altitude Warning / Rapid Decompression9 steps
| 01 | Oxygen Masks and InterphoneON AND 100 PERCENT | |
| 02 | Crew CommunicationsESTABLISHED | |
| 03 | Manual Cabin Alt ControlFULL FORWARD AND MANUALLY LOCKED | |
| 04 | Pneumatic X-Feed ValvesCLOSED | |
| 05 | Air Conditioning Supply SwitchesAUTO | |
| 06 | Passenger Oxygen MaskDEPLOYED | |
| 07 | Master Warning LightRESET | |
| 08 | Radio Rack SwitchFAN | |
| 09 | If requiredINITIATE EMERGENCY DESCENT |
Emergency Descent11 steps
| 01 | Speed BrakesEXTEND | |
| 02 | ThrottlesIDLE | |
| 03 | DescendMACH 0.80 TO 0.82 / 320-340 KIAS | |
| 04 | Altitude SelectLEVEL OFF ALTITUDE ARMED | |
| 05 | IgnitionOVRD | |
| 06 | Seat Belt SwitchON | |
| 07 | Autopilot / AutothrottlesOFF | |
| 08 | Transponder7700 | |
| 09 | ATCNOTIFY | |
| 10 | AltimetersFL180 OR TRANSITION ALTITUDE | |
| 11 | If structural integrity is in doubtAVOID HIGH IAS AND ABRUPT MANEUVERS |
Cargo Fire and Smoke Detector Loop Light5 steps
| 01 | PUSH DSCH SwitchPUSH | |
| 02 | TimeNOTE | |
| 03 | Second Halon bottle discharges automatically 5 minutes after release of the PUSH DSCH switch | |
| 04 | Diversion - START IMMEDIATELY TO THE NEAREST SUITABLE AIRPORT, DO NOT DELAY | |
| 05 | The aircraft must land within 78 minutes after activation of bottle 1 |
Electrical Smoke / Fire / Fumes9 steps
| 01 | Oxygen Masks, Goggles and InterphoneON AND 100 PERCENT | |
| 02 | Crew CommunicationsESTABLISHED | |
| 03 | Radio Rack SwitchVENTURI | |
| 04 | Cabin Altitude (Pressure) Control LeverMANUAL AND LOCK IN EXISTING POSITION | |
| 05 | AC Cross Tie SwitchOPEN | |
| 06 | R GEN Control Switch (or R APU Bus Switch) if power sourceOFF | |
| 07 | If smoke continues - R GEN CONTROL SWITCH BACK ON, THEN L GEN CONTROL SWITCH OFF | |
| 08 | If smoke disappearsPROCEED TO ISOLATION CHECKLIST | |
| 09 | CabinDEPRESSURIZE PRIOR TO LANDING |
Emergency Evacuation12 steps
| 01 | Tower (time permitting)CALL | |
| 02 | Parking BrakesSET | |
| 03 | SPD BRK / SPOILER LeverRETRACTED | |
| 04 | Flaps28 DEG | |
| 05 | Fuel LeversOFF | |
| 06 | EMER PWR SelectorON | |
| 07 | Command EvacuationEVACUATE, THREE TIMES | |
| 08 | EMER LTS SwitchON | |
| 09 | Engine Fire HandlesPULL | |
| 10 | Fire Bottles (if required)DISCHARGE | |
| 11 | APU FIRE CONT Switch (if APU operating)OFF AND AGENT ARM | |
| 12 | Cockpit Voice Recorder C-B (Upper EPC F6)PULL |
Stall Recovery6 steps
| 01 | CallSTALL, FULL POWER | |
| 02 | Full power - APPLY (if ground contact is imminent, throttles fully forward) | |
| 03 | Autopilot - DISCONNECT, be alert to counteract an excessive nose-up trim condition | |
| 04 | Wings - LEVEL, adjust pitch to minimize altitude loss or obtain obstacle clearance | |
| 05 | Above FL250 - ACCEPT ALTITUDE LOSS WHILE ACCELERATING, MAINTAIN EXISTING CONFIGURATION | |
| 06 | Below FL250 - EXTEND SLATS IF CLEAN, ACCELERATE TO THE MINIMUM SPEED FOR THE CONFIGURATION, THEN ADJUST CONFIGURATION AS DESIRED |