Memory Items Flashcards
Engine Failure in Flight
Affected Engine Condition Lever - Cut Off Propeller Lever - Feather Firewall Fuel Valve - Pull Closed Fire Extinguisher - Actuate
In- Flight Activation of GPWS Warning (GPWS Annunciator and Continuous “Pull UP, Pull UP” Voice Message)
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
In Day VMC
Evaluate Flight path with respect to terrain
Take action as necessary to recover safe terrain clearance
Electrical Smoke or Fire
Oxygen Control - Confirm ON Crew - Don Mask and Goggles -Mask Selector Switch - Emergency - Purge Valve - Open Headsets - Don Mic Selector Switches - Oxygen Mask
Engine Failure during Take off at or below V1
Power Lever - Ground Fine
(Do not use reverse thrust with one engine inoperative)
Brakes - Maximum or as required to achieve stopping distance
Spins
Intentional Spins are prohibited. If an unintentional spin is encountered perform the following procedure immediately - the longer the delay, the more difficult recovery will become. Steps 1 through 3 should be done AGGRESSIVELY and SIMULTANEOUSLY. The full forward position of the control column may be reduced slightly, if required to prevent the airplane for exceeding the 90 degree nose down (inverted) attitude
Control Column - Full Forward, Ailerons Neutral
Full Rudder - Opposite the direction of spin
Power Levers - IDLE
Rudder - Neutralize when rotation stops
Execute smooth pullout
Dual Generator Failure (L and R DC GEN Annunciators)
Instruments Emergency lights - 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
Use of Oxygen
Oxygen Control - Confirm ON Cabin Oxygen Control - Pull ON Crew - Don Mask Mask Selector Switch - SET - Inflatable type harness - Normal - Strap Type Harness - Normal (100% at cabin altitudes above 20,000 ft) Headsets - DON Mic Selector Switch - Oxygen Mask
Oil Pressure low (L or R OIL PRESS LO Annunciator)
Oil Pressure Gauge -
60-90PSI is undesirable. Do not exceed 2000Ft-lbs Torque for completion of flight.
Confirm below 60 PSI
if Confirmed - Secure engine or land at nearest suitable airport using minimum power required to sustain flight
Vmca
92
Vyse
128
Bleed Air Line Failure (L or R BL AIR FAIL Annunciator)
Bleed Air Valve (Affected Engine) INST & ENVIR OFF
Cabin Door or Cargo door Annuciator
All Occupants - Seated with seat belts securely fastened
Glide
Landing Gear Control - Up
Flaps - Up
Propellers - Feathered
Airspeed 140 Knots
Single Inverter Failure followed by a second Inverter or AC bus Failure (L or R AC BUS Failure)
Attitude/Heading Control - Use standby attitude indicator and Compass
Environmental System Smoke or Fumes
Oxygen Control - Confirm ON Crew - Don Mask and Goggles -Mask Selector Switch - Emergency - Purge Valve - Open Headsets - Don Mic Selector Switches - Oxygen Mask
Fuel Press Low (L or R FUEL PRESS LOW Annunciator)
Standby Pump (Failed Side) - ON
Environmental Failure (L or R ENVIR FAIL Annunciator)
Bleed Air Valve (Affected Side) - Cycle to ENVIR OFF and back to OPEN
if ENVIR FAIL Annunciator Extinguishes, Continue Operation. If Annunciator remains Illuminated
Bleed Air Valve (affected side) - ENVIR OFF
Engine Fire on Ground
Affected Engine - Fuel Cut off
Firewall Fuel valve - Pull Closed
Ignition and Engine Start Switch - Starter only
Fire Extinguisher, if required - Actuate
Propeller Collision during ground operation
If maximum braking and maximum reverse are insufficient and collision is imminent
Power Levers - Ground Fine or Idle
Condition Levers - Fuel Cut off
Emergency Descent
180
Venr
123
Cabin Decompression (CAB ALT HI Annuciator)
Oxygen Control - Confirm ON Cabin Oxygen Control - Pull ON Crew - Don Mask Mask Selector Switch - SET - Inflatable type harness - Normal - Strap Type Harness - Normal (100% at cabin altitudes above 20,000 ft) Headsets - DON Mic Selector Switch - Oxygen Mask
High Pressure Differential (CAB DIFF HI Annunciator)
Bleed Air Valves - ENVIR OFF
Engine Failure at or above V1 Take off continued
Vr Speed (Rotate to approximately 8 degrees
Landing Gear (when positive climb established) - Up
Airspeed - Maintain V2 to 400ft AGL
Propeller (inoperative engine) Verify Feathered\
Do not retard the failed engine power lever until the Auto feather system has completely stopped propeller rotation.
Airspeed @ 400 ft AGL….Accelerate to VENR Climb speed
Flaps….UP
Power Reduce to MCP
Bleed Valve (Operative engine) ….OFF
Climb to 1500 ft and accomplish checklist
Emergency Descent
Power Levers - Idle Propeller Levers Set 1700 RPM Flaps - 17 Degrees Landing Gear Control - Down Airspeed - 180 Knots
Dual Inverter Failure (L and R AC BUS Annunciator)
Attitude/Heading Control - Use Standby Attitude Indicator and Compass
Vxse
122
Max Glide Range
140
Engine Failure in flight below Vmca
Reduce power on operative engine to maintain control
Lower Nose to accelerate above Vmca
Unscheduled Electric Elevator Trim
Airplane Attitude - Maintain (Using Elevator Control)
Control Wheel Disconnect Switch (Depress Fully, Pitch Trim OFF Annunciator - Illuminated)
Unscheduled Rudder Boost Activation
Control Wheel Disconnect Switch - Depress and Hold (1st Level)
Rudder Boost/Yaw Control test switch - OFF
If condition persists
Rudder boost Circuit Breaker - Pull
Single Inverter or AC Bus Failure (L or R Bus Annunciators
AC BUS Switch (Failed Side) - OFF, then ON
(AC Bus Annunciator - Extinguished) if not checklist
