Memory Emergencies Flashcards

1
Q

Takeoff Abort

A

Captain
First Officer
Call “Abort, my airplane” and assume control of aircraft
Remove feet from rudder pedals and respond, “Your airplane”
POWER levers-FLIGHT IDLE then DISC
Brakes- apply maximum brakes. Maintain directional control with rudder and nose wheel steering
Maintain wings level with the ailerons as appropriate to the wind
Stop Aircraft (clear of the runway if practical) and evaluate the decision

Direct FO to request emergency equipment, if required
Request emergency equipment, if directed

If passengers or crew are in immediate danger, call for “Emergency Evacuation Checklist”
Accomplish the Emergency Evacuation Checklist on the IAC

If engine failure or fire occurs, call for “Engine Shutdown/Fire on Ground Checklist”
Accomplish the Engine Shutdown/Fire on Ground Checklist on the IAC

If evacuation not required, call for “Takeoff Abort Checklist”
Accomplish the Takeoff Abort Checklist in the E&A (Emergency & Abnormal)

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2
Q

Engine Start Abort

A

___ Condition Lever: FUEL OFF
Start SELECT switch: CENTER
Call for Engine Start Abort Checklist

Engine start shall be aborted if:
Engine ITT approaches or exceeds 920C
NH is not in the green arc within 70 seconds of selecting Condition Lever to START & FEATHER
Engine Oil Pressure fails to reach 44 psi by start SELECT switch reset

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3
Q

Roll Control Abort

A

Autopilot: DISENGAGE
If control still jammed:
ROLL DISC handle: Pull and turn 90 degrees
Control wheels: Both pilots attempt roll control
Aircraft control: Pilot with free controls flies aircraft
Call for Roll Control Jam Checklist

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4
Q

Pitch Control Abort

A

Autopilot: DISENGAGE
Retain flap setting and approximate airspeed at time of jam
If control still jammed: Both pilots attempt to control by force against jam
If unable to overcome jam:
Control Column Force: Relax
PITCH Disconnect handle: Pull and turn 90 degrees
Control Column: Both pilots attempt pitch control
Aircraft Control: Pilots with free control column
Call for Pitch Control Jam Checklist

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5
Q

O2 Mask Donning Procedure

A

When detecting a situation which could introduce smoke or fumes in the flight deck, shall state “Smoke-Don Mask” or
When detecting a situation results in loss of cabin pressure above 10,000 MSL, shall state “Oxygen-Don Mask”

Headset: Remove
O2 Mask: Don

If smoke or fumes are present
Regulator (if required): EMERGENCY (pressurizes mask to prevent smoke from entering)
Communications: Establish
Headset: ON
HOT mic: OFF (use interphone switch for crew comms)
MASK/MIC switch: MASK

After donning emergency equipment call for the appropriate checklist
(Ie. aircraft fire or smoke, smoke warning, and cabin press warning checklists)

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6
Q

Engine Failure/Fire During Takeoff

A

Pilot Flying
Pilot Monitoring

If engine fails after V1 on the runway:
Maintain direction control with rudder and accelerated to Vr
At Vr call “Rotate”
Rotate to Flight Director 10 degrees up

If engine fails in flight:
Roll wings level with ailerons, adjust pitch to 10 up, and apply rudder pressure to maintain coordination
After rotation when positive rate of climb is indicated “Positive Rate”
When positive rate is seen or heard “Gear Up”
Select gear up when directed
Climb at 10 in PITCH HOLD (Minimum speed V2 and use TCS as required)

At Acceleration Height
At Acceleration Height “Acceleration Height”
When Acceleration Height is indicated or heard, level off to accelerate, Do Not Descend “Push ALT”
Push ALT

At/above V2+10 “Flap retract speed” Above V2+10 “Flaps zero”
Select FLAPS lever incrementally to 0 when directed

At the appropriate VSE for conditions (Open Bug or Solid Bug) “Single-engine Climb Speed” Accelerate and resume climb at appropriate VSE “Push IAS, Set [VSE/VSE(ICE)]
Push IAS, set VSE or VSE (ICE), verify ALT is set and ALT SEL

Call for “Engine Failure or Fire Checklist”
Conduct Engine Failure or Fire Checklist from IAC

Note: If the prop does not autofeather, or if the condition requires immediate action the Engine Failure Checklist (IAC) should be called for immediately, regardless of altitude

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7
Q

Engine Failure During Approach

A

Pilot Flying
Pilot Monitoring

“Engine Failure Checklist” or “Engine Fire Checklist”
Accomplish Engine Failure or Fire Checklist on IAC immediately

After completing IAC checklist:
Accomplish canceling approach prior to the MAP, Single-engine missed approach, or continue for landing as appropriate

Continue to land only if the gear has been extended AND landing is assured provided the approach is stable, no compounding mechanical or environmental conditions, and both pilots agree landing is assured

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8
Q

Engine Failure During Missed Approach or Single-Engine Missed Approach

A

Pilot Flying
Pilot Monitoring

Accomplish Missed Approach Procedure according to Normal Procedures

If engine fails during missed approach (only)
Do not allow airspeed to decay below Open Bug
“Max Power” if positive rate of climb is not obtained
After gear is up and flight guidance set call “Engine Failure Checklist”
Accomplish Engine Failure Checklist on IAC immediately to feather propeller
Climb at 10 pitch up to acceleration height (Minimum speed is Open Bug or Solid Bug as appropriate) Do Not Descend

Above 1,000’ AFE
If autopilot is desired “Push Autopilot”
Push AP if commanded

At Acceleration Height (2,000’ above approach minimums or first level-off altitude whichever is lower)
“Acceleration Height”
Level off to accelerate, Do Not Descent “Push ALT”
Push ALT

At/above Open Bug +10
“Flap Retract Speed”
“Flaps zero”
Select flaps incrementally to 0 degrees when directed

At appropriate VSE for conditions (Derived from tFDP or iBugs/Data Card)
“Single-engine climb speed”
Accelerate and resume climb at appropriate VSE for conditions “Push IAS, Set [VSE/VSE(ICE)]”
Push IAS, set VSE or VSE(ICE), Verify MAP Altitude is set and verify ALT SEL
If practical set Open and Solid Bugs to VSE speeds

IF EGPWS “PULL-UP” Warning Occurs
Maintain appropriate VSE speed
If below 500’ AGL and necessary to avoid ground contact
“500 feet”
Advance power past detent to full travel “Max Power”
Verify Power levers set to maximum forward travel
When clear of obstacles, reduce power back to detent
Verify power levers returned to detent

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9
Q

EGPWS Responses

A

Excessive Glideslope Deviation
“GLIDESLOPE” Callout = Maneuver aircraft to re-establish glideslope

Altitude Loss after Takeoff or Low Go-around
“DON’T SINK” Callout = Arrest descent or re-establish positive climb
“TOO LOW-TERRAIN” Callout = Increase climb rate or maneuver to increase terrain separation

Insufficient Terrain Clearance for Existing Configuration or Speed
“TOO LOW-TERRAIN” Callout = Maneuver to obtain more terrain separation
“TOO LOW-GEAR” Callout = Accomplish Missed Approach
“TOO LOW-FLAPS” Callout = Accomplish Missed Approach

Excessive Descent Rate or Excessive Closure to Terrain
“SINK RATE, SINK RATE” Callout = Reduce descent rate until alter stops (usually 1,000fpm)
“TERRAIN, TERRAIN” Callout (maybe “PULL UP”) = Stop any descent and climb as necessary
“CAUTION TERRAIN, CAUTION TERRAIN” or “CAUTION OBSTACLE, CAUTION OBSTACLE” Callout = Climb or turn to avoid terrain/obstacle conflict
“TERRAIN, TERRAIN—PULL UP” or “OBSTACLE, OBSTACLE—PULL UP” Callout = Missed Approach (execute windshear/EGPWS recovery)

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10
Q

Takeoff Procedures–Windshear/EGPWS Recovery

A

Pilot Flying
Pilot Monitoring

Either pilot calls “Windshear” or EGPWS PULL-UP Warning

Maintain 15 degrees pitch up (V2 + 10)
Do not change gear or flap configuration
Leave power at NTOP

If Aircraft is Descending or “PULL UP” Warning
Increase pitch to maintain V2 (DO NOT SLOW TO STICK SHAKER)
Monitor airspeed, VSI, and Radio altimeter
If descent “Sink Rate”
If airspeed slows below V2 “Airspeed”

If Below 500’ AGL and Necessary to Avoid Ground Contact
“Max Power”
Verify Power levers set to maximum forward travel
Maintain V2

After Stabilized Climb is Established
When positive rate of climb is noted “Positive Rate”
When positive rate is seen or hear “Gear Up”
Select landing gear up

When climb is established and clear of obstacles
Reduce pitch to transition to normal climb
Reduce power levers to detent (If Max Power used)

At Acceleration Height
“Acceleration Height”
Above acceleration height resume normal after takeoff procedures
Resume normal after takeoff procedures

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11
Q

Missed Approach Procedures–Windshear/EGPWS Recovery

A

Pilot Flying
Pilot Monitoring

Either pilot calls “Windshear” or EGPWS PULL-UP Warning

“Missed Approach”
Press G/A Button on Power Lever (disconnects autopilot)
Rotate to Flight Director (10 nose up)
Position hands below Power levers to assist power applications
After initiation rotation, advance Power levers to detent “Check Power”
Ensure Power levers set to detent and conditions levers to MAX (1020 RPM)

If Aircraft is Descending or “PULL UP” Warning Continues
Increase pitch to maintain Open Bug or Sold Bug (DO NOT SLOW TO STICK SHAKER)
Monitor airspeed, VSI, and Radio altimeter
If descent is noted “Sink Rate”
If airspeed slows below V2 “Airspeed”

If Below 500’ AGL and Necessary to Avoid Ground Contact
“Max Power”
Verify Power levers set to maximum forward travel
Maintain V2

After Stabilized Climb is Established
When positive rate of climb is noted “Positive Rate”
When positive rate is seen or hear “Gear Up”
Select landing gear up

When climb is established
When pitch is 10 degrees “Flaps one notch up”
Select flaps on notch up when directed
When positive rate of climb is noted “Positive Rate”
“Gear up”
Select landing gear up
Climb at Solid Bug for normal two engine climb

At Acceleration Height
“Acceleration Height”
Above acceleration height accelerate to climb Bug Speed + 10 then resume normal after takeoff procedures
Resume normal after takeoff procedures

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12
Q

Stall Warning Recovery

A

Pilot Flying
Pilot Monitoring

At first indication of stall “Stall Warning”

Immediately and simultaneously reduce pitch until stick shaker stops, reduce bank to 20 max, increase power by advancing Power Levers as required
Guard controls, if pitch exceeds 10 degrees “Pitch Down”, ensure Power Levers st and Condition Levers Max (1020), verify airspeed increases

Maintain reduced pitch and increased power until airspeed increases to Low Speed Cue + 10 kts minimum
If airspeed decays below Low Speed Cue + 10 kts “Airspeed”
Maintain Low Speed Cue +10 kts minimum and smoothly raise pitch to level flight

If on approach bellow 1,000’ AFE accomplish missed approach
If on approach above 1,000’ AFE consider cancelling the approach and or executing missed approach
Otherwise return to desired flight path

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13
Q

Fire or Smoke and/or SMOKE Warning (in flight)

A

O2 masks: DON/100%
BOOM/MASK switch: MASK/establish comms
BLEEDs 1 & 2 (both): First Officer OFF
Proceed with IAC Aircraft Fire or Smoke and/or SMOKE warning (In Flight) Checklist

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14
Q

Propeller Ground Range Lights Cycling

A
POWER Lever(s): Advance
Propeller Ground Range Lights Cycling Checklist: ACCOMPLISH
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