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P-Ocho > EPs > Flashcards

EPs Flashcards

1
Q

Smoke, Fire, or Fumes

A
  1. Alert crew, execute firefighting duties - Alerted (PM/MSN)
  2. Oxygen masks and regulators - ON/100%, as required (ACW)
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2
Q

CONFIG (Landing)

A

Landing Configuration - Check (FLT)

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3
Q

Max T/O Crosswind (all flaps, wet)

A

25 knots

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4
Q

Windshear Conditions

A

Unacceptable flight path deviations, recognized as uncommanded changes from normal steady state flight conditions below 1,000 feet AGL in excess of any of the following conditions:

a. 15 knots indicated airspeed.
b. 500 fpm vertical speed.
c. 5° pitch attitude.
d. One dot displacement from the glideslope.
e. Unusual thrust lever position for a significant period of time.

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5
Q

Engine (1,2) OVERHEAT

A
  1. Autothrottle - Disengage (PF)
  2. Thrust lever (affected engine) - Confirm - Close (PF)
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6
Q

Max T/O Crosswind (flaps 1,5 dry)

A

35

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7
Q

Ground Evacuation

A
  1. Ground/Tower - Notify (CP)
  2. PARKING BRAKE - Set (P)
  3. SPEED BRAKE lever - DOWN (P)
  4. FLAP lever - 30 (CP)
  5. Pressurization mode selector - MAN (CP)
  6. Outflow VALVE switch - Hold in OPEN until the outflow VALVE position indicates fully open (CP)
  7. EWMU - OFF (CP)
  8. Engine start levers/FUEL CONTROL switches (both) - CUTOFF (P)
  9. Engine and APU fire switches (all) - Override and pull (P)
  10. Advise the cabin to evacuate (CP)

Note When lowering the airstair on battery power, extension will take longer.

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8
Q

Fire APU

A
  1. Choose one:
    a. INSIDE the aircraft:
    (1) APU fire switch - Pull, rotate to the stop until BOTTLE DISCHARGE illuminates (ACW)
    (2) APU switch - OFF (ACW)
    b. OUTSIDE the aircraft:
    (1) APU fire control handle - Pull down (ACW)
    (2) BOTTLE DISCHARGE switch - Push left (ACW)
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9
Q

Upset Recovery conditions

A

An aircraft upset as defined by one or more of the following occurring:

  1. Any stall indication (including buffet or stick shakers).
  2. The aircraft pitch attitude is unintentionally more than 25° nose high.
  3. The aircraft pitch attitude is unintentionally more than 10° nose low.
  4. The aircraft bank angle is unintentionally greater than 65°.
  5. Within above parameters but flying at airspeeds/attitudes inappropriate for the conditions.
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10
Q

Windshear Escape

A
  1. Autothrottle - Disengage (PF)
  2. Autopilot - Disengage (PF)
  3. Pitch - 15° initially, then follow flight director TO/GA guidance, if available (PF)
  4. Roll - Wings level (PF)
  5. Thrust levers - Maximum (PF)
  6. Speedbrake Lever - DOWN (PF)
  7. TO/GA switch (either) - Press (PF)
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11
Q

Engine Fire on the Ground

A
  1. Engine Start Lever/Fuel Cutoff Switch (affected engine) - Cutoff (PM)
  2. Engine Fire Switch - Pull and rotate to the stop until bottle discharge (PM)
  3. Engine Fire Switch - Pull and rotate to the other stop until bottle discharge (PM)
    - > Proceed to the Ground Evacuation Checklist
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12
Q

Runaway Stabilizer

A
  1. Control column - Hold firmly (PF)
  2. Autopilot - Disengage (PF)
  3. AT- disengage
  4. Control column/thrust levers- ctrl pitch attitude and a/s
  5. Main electric stabilizer trim- reduce control column forces
  6. If the runaway continues:
    a. STAB TRIM CUTOUT switches (both) - CUTOUT (PM)
  7. If the runaway continues:
    a. Stabilizer trim wheel - Grasp and hold (PM)
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13
Q

Engine Limit, Surge, or Stall

A
  1. Autothrottle - Disengage (PF)
  2. Thrust lever (affected engine) - Confirm - Retard until indications stay within limits or the thrust lever is closed (PF)
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14
Q

TCAS - RA

A
  1. Autothrottle - As required (PF)
  2. Autopilot - As req (PF)
  3. Pitch - Adjust to satisfy RA (PF)
  4. Roll - Continue planned lateral path (PF)
  5. Thrust levers - As required (PF)
  6. Flaps - Set (PM)
  7. LANDING GEAR - UP, as required (PM)
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15
Q

Prohibited Operations

A
  1. Intentional spins, stalls, aerobatics, steep dives (not associated with an Emergency Descent), or maneuvers resulting in abrupt accelerations.
  2. Use of auto land.
  3. Load factor greater than 2.0 g’s with asymmetric thrust.
  4. Holding and on-station mission operations in icing with flaps extended.
  5. Use of Mission Limit Mode.
  6. Uninterrupted rudder deflections across the neutral position (commonly referred to as rudder reversals). Approximately zero sideslip and yaw must be established at neutral rudder.
  7. Rapid rudder check or rapid release to neutral after abrupt rudder input.
  8. Alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g., large sideslip angles).
  9. Uninterrupted rapid wheel inputs across the neutral position at roll rates greater than 10 degrees per second.
  10. Inflight auxiliary fuel transfer functions FWD > AFT and AFT > FWD, except to prevent or correct a cg limit exceedance.
  11. Flight beyond stick shaker or initial buffet (whichever occurs first).
  12. Intentional single engine or simulated single engine maneuvers, except as required for an FCF.
  13. Use of tactical fuel flow margin.
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16
Q

Engine Tailpipe Fire

A
  1. Engine Start Lever/Fuel Cutoff Switch (affected engine) - Cutoff (P)
17
Q

Emergency Descent

A
  1. Emergency Descent - Announce (FLT)
  2. Condition 5 - Set (FLT)
  3. Descent - Initiate (PF)
  4. ENGINE START switches (both) - CONT (PM)
  5. Thrust levers (both) - Close (PF)
  6. Speed brake - FLIGHT DETENT (PF)
  7. Target Speed - Vmo/Mmo (PF)
18
Q

Upset Recovery

A
  1. Autothrottle - Disengage (PF)
  2. Autopilot - Disengage (PF)
  3. Pitch - Reduce AOA (PF)
  4. Roll - Wings level (PF)
  5. Thrust - As required to prevent overspeed, ground contact, or undesired pitch up (PF)
  6. SPEED BRAKE lever - As required (PF)
19
Q

Aborted Start conditions

A
  1. The N1 or N2 does not increase or increases very slowly after the EGT increases.
  2. There is no oil pressure indication by the time that the engine is stable at idle.
  3. The EGT does not increase within 10 seconds after the engine start lever/FUEL CONTROL switch is moved to IDLE.
  4. The EGT quickly nears or exceeds the start limit.
  5. Engine torching.
20
Q

EGPWS Conditions

A
  1. Activation of the aural EGPWS warnings.
    a. “PULL UP.”
    b. “TERRAIN TERRAIN PULL UP.”
    c. “OBSTACLE OBSTACLE PULL UP.”
  2. Other situations resulting in unacceptable flight toward terrain.
21
Q

Airspeed Unreliable or IAS Disagree

A
  1. Autothrottle - Disengage
  2. Autopilot - Disengage
  3. F/D switches (both) - OFF
  4. Initially set the following gear up pitch attitude and thrust:
    a. Flaps extended - 10° and 80% N1
    b. Flaps up - 4° and 75% N1
22
Q

EGPWS Warning

A
  1. Autothrottle - Disengage
  2. Autopilot - Disengage (PF)
  3. Pitch - 20° initially (PF)
  4. Roll - Wings level (PF)
  5. Thrust levers (both) - Maximum
  6. Speedbrake Lever - DOWN (PF)
  7. If terrain remains a threat, continue to increase pitch up to: (PF)
    a. Pitch Limit Indicator
    b. Stick Shaker
    c. Initial buffet
  8. Monitor radio altimeter for sustained or increasing terrain separation (PF)
  9. When clear of terrain, slowly decrease pitch attitude and recover to appropriate airspeed and configuration (PF)
23
Q

Max Landing Crosswind (wet)

A

30 knots

24
Q

Aborted Takeoff

A
  1. Autothrottles - Disengage (PF)
  2. Thrust levers (both) - Close (PF)
  3. Brakes - Verify RTO or Max Manual (PF)
  4. Speed brake lever - Up (PF)
  5. Reverse Thrust - Apply (PF)
25
Q

FIRE - ENG (1,2) or Engine Severe Damage or Separation

A
  1. Autothrottle - Disengage (PF)
  2. Thrust lever (affected engine) - Confirm - Close (PF)
  3. Engine start lever/FUEL CONTROL switch (affected engine) - Confirm - CUTOFF (PM)
  4. Engine fire switch (affected engine) - Confirm - Pull (PM)
  5. If fire indications exist:
    a. Engine fire switch - Rotate to the stop and hold until BOTTLE DISCHARGE illuminates (PM)
  6. If after 30 seconds, fire indications persist:
    a. Engine fire switch - Rotate to the other stop and hold until BOTTLE DISCHARGE illuminates (PM)
26
Q

Airspeed Unreliable or IAS Disagree Conditions

A

Airspeed Unreliable: The pitch attitude is not consistent with the phase of flight, altitude, thrust and weight, or noise or low frequency buffeting is experienced. IAS DISAGREE: Indicates the pilot’s and copilot’s airspeed indications disagree by more than 5 knots for 5 continuous seconds.

27
Q

WEAPON RELEASE

A
  1. MASTER ARM switch - DISARM (PM)
  2. Mission Crew - Notify (PM)
28
Q

Max T/O and Landing Crosswind (contaminated)

A

15 knots

29
Q

Loss of Thrust on Both Engines

A
  1. ENGINE START switches (both) - FLT (PM)
  2. Engine start levers/FUEL CONTROL switches (both) - CUTOFF (PM)
  3. When EGT decreases:
    a. Engine start levers/FUEL CONTROL switches (both) - IDLE/detent/IDLE (PM)
  4. If EGT reaches 975°C or there is no increase in EGT within 30 seconds:
    a. Engine start levers/FUEL CONTROL switches (affected engine) - Confirm - CUTOFF, then IDLE/detent/IDLE, repeat as required (PM)

At or above FL270, set airspeed above 275 knots. Failure to achieve the appropriate airspeed may limit N2 preventing a successful restart.

30
Q

TCAS - TA

A
  1. If traffic is sighted, maneuver as required (PF)
31
Q

CABIN ALTITUDE, DON OXYGEN, Rapid Depressurization

A
  1. Oxygen masks/regulators - ON, 100% (ACW)
    a. CREW/PASS OXYGEN PASS switch - ON (PM)
  2. Crew communications - Establish, as required (FLT, TC/OBS)
32
Q

CONFIG (Takeoff)

A

Takeoff Configuration - Check (FLT)

33
Q

Airspeed Unreliable Conditions

A
  1. Speed/altitude information not consistent with pitch attitude and thrust setting.
  2. SPD failure flag.
  3. SPD LIM failure flag.
  4. IAS DISAGREE alert.
  5. Blank or fluctuating airspeed display.
  6. Variation between pilot and co-pilot airspeed indications.
  7. Radome damage or loss.
  8. Overspeed warning.
  9. Simultaneous overspeed and stall warnings.
34
Q

Max Landing Crosswind (dry)

A

35 knots

35
Q

Ditching

A

Alert crew time to impact - Alerted (PM)

36
Q

Max Tailwind

A

15 knots

P-Ocho (11 decks)

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