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27 Cards in this Set
- Front
- Back
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Engine fire or failure in flight |
Condition lever - fuel cutoff Propeller lever - feather Fire fuel valve - pull closed Fire extinguisher, if required - actuate |
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Engine fire on ground |
Condition lever - fuel cutoff Firewall fuel valve - pull closed Igntion and engine start switch - starter only Fire extinguisher, if required - actuate |
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Engine failure during takeoff (at or below V1) |
Power levers - ground fine Brakes - Maximum (or as required to achieve stopping distance) |
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Engine failure during takeoff (at or abouve V1) |
Vr speed - rotate to approximately 8° Landing gear (when positive climb established) - Up Airspeed - Maintain V2 to 400 ft agl Propeller (inoperative engine) - Verify feathered |
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Engine failure in flight below air minimum control speed (Vmca) |
Reduce power on operative engine as required to maintain control Lower nose to accelerate above Vmca |
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Oil pressure low (L or R Oil Pres Lo Annunciator) |
Oil pressure gage - Comfirm below 60 Psi If confirmed - Secure engine or land at the nearest suitable airport using the minimum power required to sustain flight |
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Propeller collision during ground operation |
If maximum braking and maximum reverse are insufficient and a collision is imminent: Power levers - Ground fine or Idle Condition levers - Fuel cutoff |
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Fuel pressure low (L or R fuel pres Lo Annunciator) |
Standby pump (failed side) - On |
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Electrical smoke or fire |
Oxygine control - Comfirm on Crew - Don mask, and goggles (if installed) *Mask selector switch - emerg (if installed) or 100% *Purge valve (if installed) - Open Headsets - Don Mic selector switches - Oxygen mask
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Environmental system smoke or fumes |
Oxygine control - Comfirm on Crew - Don mask, and goggles (if installed) *Mask selector switch - emerg (if installed) or 100% *Purge valve (if installed) - Open Headsets - Don Mic selector switches - Oxygen mask |
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Cabin door or cargo door unlocked Annunciator |
All occupants - seated with seat belts securely fastened |
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Emergency descent |
Power levers - Idle Propeller levels - set 1700 RPM Flaps - 17° Landing gear control - DN Airspeed - 180 Knots |
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Glide |
Landing gear control - Up Flaps - Up Pripellers - feathered Airspeed - 140 Knots |
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Single inverter or AC bus failure (L or R AC Bus Annunciator) |
AC Bus switch (failed side) - Off, then on. |
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Single inverter failure followed by a second inverter or AC bus failure (L or R AC Bus Annunciators) |
Attitude/Heading Control - Use standby attitude indicator and compass |
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Duel inverter failure (L or R AC Bus Annunciators) |
Attitude/Heading Control - Use standby attitude indicator and compass |
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Duel generator failure (L and R DC Gen Annunciator) |
Instrument emergency lights (if required) - On Generators - Reset, then on
If either generator will reset: Do not exceed 100% load on operating generator
If neither generator will reset: Non-essential equipment - Off |
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Unscheduled electric elevator trim |
Airplane Attitude - Maintain (using elevator control) Control wheel disconnect switch- Depress fully (pitch trim off Annunciator - Illuminated) |
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Unscheduled rudder boost activation |
Control wheel disconnect switch - Depress and Hold (1st level) Rudder boost/Yaw control test switch - Off If contition persists: Rudder boost circuit breaker - Pull |
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Use of Oxygen |
Oxygen control - Comfirm on Cabin Oxygen control - Pull on Crew - Don mask Mask selector switch - Set *inflatable type harness - Normal *Strap type harness - Normal (100% at cabin altitude above 20 000 feet) Headsets - Don Mic selector switches - Oxygen mask
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Cabin decompression (Cab Alt Hi Annunciator) |
Oxygen control - Comfirm on Cabin Oxygen control - Pull on Crew - Don Mask Mask selector switch - set *inflatable type harness - Normal *Strap type harness - Normal (100% at cabin altitude above 20 000 feet) Headsets - Don Mic selector switches - Oxygen mask |
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High differential pressure (Cab Diff Hi Annunciator) |
Bleed Air Valves - Envir off |
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Bleed Air line failure (L or R BL Air fail Annunciator) |
Bleed air valve (affected side) - Cycle to envir off and back to open
If Envir fail Annunciator extinguishes, continue opertation. If Annunciator remains illuminated: Bleed air valve (affected side) - Envir off |
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In-flight activation of GPWS warning |
In IMC or at NIGHT: Wings - level Airspeed - 122 KIAS Power - Max allowable Gear and flaps - Retract Continue climb at 122 kias until all visual and aural warnings cease |
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Emergency exit |
Escape hatch handle - Pull |
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Spins |
Control collumn - Full forward, ailerons neutral Full rudder - Opposite the direction of spin Power levers - Idle Rudder - neutralize when rotation stops Execute a smooth pullout |
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Emergency Airspeeds 17 120 Pounds |
One engine inoperative best angle of climb (Vxse) - 122 knots One engine inoperative best rate of climb (Vyse) - 128 Knots (Decrease 2 kts per 5000 ft) One engine inoperative En-route climb (Venr) - 123 knots Air minimum control speeds (Vmca) - flap up - 92 knots Flap 17° - 92 knots Emergency descent - 180 knots Maximum range glide - 140 knots |
