Memory Items Flashcards
Engine Fire/Failure in Flight
Affected engine:
- Condition lever - FUEL CUTOFF
- Prop lever - FEATHER
- Firewall valve - CLOSE (EXTINGUISHER PUSH) and (CLOSED) - ILLUMINATED
- Fire extinguisher (if fire warning persists) - ACTUATE (DISCHARGED) - ILLUMINATED
EMERGENCY ENGINE SHUTDOWN ON THE GROUND
- Condition levers - FUEL CUTOFF
- Prop levers - FEATHER
- Firewall valves - CLOSE (EXTINGUISHER PUSH) and (CLOSED) - ILLUMINATED
- Master switch (gang bar) - OFF
- Battery bus switch - EMER OFF
- ESIS power - OFF
ENGINE FAILURE DURING TAKEOFF AT/BELOW V1 - TAKEOFF ABORTED
- Power Levers - GROUND FINE
2. Brakes - MAXIMUM (or as required to achieve desired stopping distance)
ENGINE FAILURE DURING TAKEOFF AT/ABOVE V1 - TAKEOFF CONTINUED
- VR speed - ROTATE TO APPROXIMATELY 10° PITCH ATTITUDE
- Gear - UP (When positive climb established)
- Airspeed - MAINTAIN V2 TO 400 ft AGL AND CLEAR OF OBSTACLES
- Prop (inoperative engine) - VERIFY FEATHERED
ENGINE FAILURE IN FLIGHT BELOW Vmca
- Power - REDUCE AS REQUIRED TO MAINTAIN CONTROL
2. Nose - LOWER TO ACCELERATE ABOVE Vmca
GLIDE (BOTH ENGINES INOPERATIVE)
- Landing Gear - UP
- Flaps - UP
WARNING: Do not feather second engine propeller if a No Starter Assist air start is to be conducted. Air starts with a windmilling propeller will result in lower starting temperatures. Refer to Abnormal Procedures for Air Start Procedures. - Prop Levers - FEATHERED
- Airspeed - 135 KTS
DUAL GENERATOR FAILURE [L DC GEN] and [R DC GEN]
- Instrument emergency lights (if required) - ON
- Generator - RESET, THEN ON
If either generator will reset: - Operating generator loadmeter - MONITOR
If neither generator resets: - ECS mode - OFF
- Cockpit/Cabin blower - AUTO
- Non-essential equipment - OFF
UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION
- Aircraft attitude - MAINTAIN WITH ELEVATOR CONTROL
2. AP/Trim disconnect - DEPRESS FULLY (Pitch Trim OFF) - ILLUMINATED
UNSCHEDULED RUDDER BOOST ACTIVATION
- AP/Trim disconnect - DEPRESS/HOLD (FIRST LEVEL)
- Rudder boost - OFF
If condition persists: - YD/AP DISC (on Flight Guidance Panel) - PULL DOWN
SPINS
If a spin is entered inadvertently:
- Control column - FULL FORWARD - AILERONS NEUTRAL
- Rudder - APPLY FULL OPPOSITE SPIN DIRECTION
- Power levers - REDUCE TO IDLE ON BOTH ENGINES
These action should be accomplished as nearly simultaneously as possible
- RUDDER - NEUTRALIZE - HOLD UNTILE ROTATION STOPS
- Execute smooth pullout
ELECTRICAL SMOKE OR FIRE
WARNING: Dissipation of smoke is not sufficient evidence that a fire has been extinguished. If it cannot be visually confirmed that no fire exists, land at the nearest suitable airport.
- Oxygen mask(s) - DON
- Mask selector switch - EMERG
- Mic switch(es) - OXY
ENVIRONMENTAL SYSTEM SMOKE OR FUMES
Oxygen:
- Crew mask - DON
- Mask selector switch - EMERG
- Mic selector - OXY
AIRSTAIR/CARGO DOOR UNLOCKED
WARNING: Do not attempt to check the security of the airstair door or cargo door in flight. Remain as far from the door as possible with seat belts securely fastened.
If the [DOOR UNLOCKED] Illuminates, of If An Unlatched Airstair Door/Cargo Door is Suspected:
- All occupants - SEATED WITH SEAT BELTS SECURELY FASTENED
EMERGENCY DESCENT
- Power levers - IDLE
- Prop levers - FULL FORWARD
- Flaps - APPROACH/202 KTS MAX
- Landing gear - DOWN/184 KTS MAX
- Airspeed - 184 KTS MAX
OXYGEN USE
Crew System:
- Crew mask - DON
- Mic Switches - OXYGEN MASK
PRESSURIZATION LOSS [CABIN ALT HI]
- Oxygen mask(s) - DON
- Mic switch(es) - OXYGEN MASK
- Passenger manual drop out - PULL ON [PASS OXYGEN ON] - ILLUMINATED
- Descent - AS REQURED
WARNING: The highest recommended cabin altitude for sustained flight is 25,000 ft.
HIGH DIFFERENTIAL PRESSURE
- Bleed air valve switches - ENVIR OFF
- Oxygen
(crew and passengers) - AS REQUIRED - Descend as required
AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE
- Passenger manual dropout - PULL ON
BLEED AIR FAILURE
If illuminated during flight:
- Bleed air valve switch
(affected engine) - PNEU/ENVIR OFF
AUTOPILOT MISTRIM [E] or [A]
WARNING: Intentional or automatic disengagement of the autopilot without restraining the control wheel during mistrim condition will produce a significant airplane response in the direction of the mistrim force.
If a Mistrim Indication continues for more than a few seconds:
- Flight controls - HOLD FIRMLY
(Control forces may exceed 25 lbs) - AP - DISENGAGE
AUTOPILOT TRIM FAIL [TRIM]
- Flight controls - HOLD FIRMLY
2. AP - DISENGAGE
AUTOPILOT AUTOMATIC DISENGAGEMENT
If an Automatic Disengagement occurs:
- Maintain airplane control
- AP/TRIM disconnect - DEPRESS TO 1st LEVEL TO CANCEL HORN
EGPWS in IMC or NIGHT
- Wings - LEVEL
- Power - MAX ALLOWABLE
- Pitch - INCREASE
- Promptly and smoothly increase pitch toward an initial pitch attitude of 20° to 25°
- Adjust as required to avoid continuous buffeting and/or stall warning
- Adjust to maintain 125 KIAS - Gear and Flaps - UP
TAWS+ in IMC or NIGHT
- Autopilot - DISENGAGE
- Wings - LEVEL
- Power - MAX ALLOWABLE
- Pitch - INCREASE
- Promptly and smoothly increase pitch toward an initial pitch attitude of 20° to 25°
- Adjust as required to avoid continuous buffeting and/or stall warning
- Adjust to maintain 125 KIAS - Gear and Flaps - UP
ENG FIRE ON GROUND
- Condition Lever - FUEL CUTOFF
- Firewall Fuel Valve - CLOSE (EXTINGUISHER PUSH AND CLOSED) - ILLUMINATED
- Starter Switch - STARTER ONLY
- Fire Extinguisher [if fire warning persists] - ACTUATE [DISCHARGED] - ILLUMINATED
