Disengage autopilot Disconnect autothrottle(s) Aggressively apply maximum thrust Simultaneously roll wings level and rotate to an initial pitch attitude of 20° Retract speedbrakes If terrain remains a threat, continue rotation up to the pitch limit indicator or stick shaker or initial buffet ------------------------------ Do not change gear or flap configuration until terrain separation is assured Monitor radio altimeter for sustained or increasing terrain separation When clear of the terrain, slowly decrease pitch attitude and accelerate

QRH - Memory Items Flashcards by Michelle Powell

Aborted Engine Start

(memory items)

FUEL CONTROL switch (effected side)

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Dual Eng Fail/Stall

(memory items)

Condition:
Engine speed for both engines is below idle.

1) FUEL CONTROL switches

CUTOFF, the RUN

2) RAM AIR TURBINE switch

## Push and hold for 1 second

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() ENG AUTOSTART

(memory items)

Condition:
Autostart did not start the engine
Fuel control switch is in RUN at low engine RPM with autostart switch OFF

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Eng Lim/Surge/Stall conditions?

(5)

Engine indications are abnormal

Eng indications are quickly nearing or show an exceedance

Abnormal eng noises, possibly with airframe vibrations

No response to TL movement or response is abnormal

Flames in the engine inlet or exhaust

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Eng Lim/Surge/Stall memory items?

(memory items)

1) A/T ARM switch (affected side)
Confirm———–OFF

2) Thrust lever (affected side)
Confirm——–Retard until eng. indications stay within limits or TL is idle
——————————

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Eng. Severe Damage/Sep

(memory items)

Conditions:
Airframe vibrations with abnormal engine indications
Engine separation

A/T ARM switch (affected side)
Confirm———–OFF

Thrust lever
(affected side)
Confirm———–Idle

FUEL CONTROL switch
(affected side)
Confirm——-CUTOFF

Eng. Fire switch
(affected side)
Confirm———-Pull
——————————

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FIRE ENG L/R

(memory items)

In Flight:

A/T ARM switch (affected side)
Confirm———–OFF

Thrust lever
(affected side)
Confirm———–Idle

FUEL CONTROL switch
(affected side)
Confirm——-CUTOFF

Eng. Fire switch
(affected side)
Confirm———-Pull

IF FIRE ENG msg shows:

Eng. fire switch
(affected side)—-Rotate to the stop and hold for 1 sec.
—————————-

On Ground:
No memory items

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STABILIZER

(memory items)

Conditions:
Stabilizer movement without signal to trim
Stabilizer has failed

STAB cutout switches (both)———-CUTOUT

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Airspeed Unreliable

(memory items)

Autopilot disc switch - Push

A/T ARM switches (both)—————OFF

F/D switches
(both)—————OFF

Gear up pitch and thrust:

Flaps extended:
10 degrees 85 % N1

Flaps up:
4 degrees + 70 % N1

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What is the objective of the Airspeed Unreliable NNC?

To identify a reliable airspeed indication if possible

To continue flight using the Flight With Unreliable Airspeed table in the Perf. Inflight Ch.

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What is reliable in Airspeed Unreliable NNC?

Attitude
N1
Ground Speed
RA

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Which EICAS msg could may show for Airspeed Unreliable?

(11 incl. 4x Pitot)

AIRSPEED LOW

GND PROX SYS

HEAT PITOT C

HEAT PITOT L

HEAT PITOT R

HEAT PITOT L+C+R

OVERSPEED

SGL SOURCE AIR DATA

SGL SOURCE DISPLAYS

WINDSHEAR SYS

AIR DATA SYS

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CABIN ALTITUDE

(memory items)

Don oxygen masks

Establish crew comm

Check cabin alt + rate

IF cabin altitude is uncontrollable:

SUPRNMRY OXYGEN switch——————-Push to ON and hold 1 sec

WITHOUT DELAY
Descend to lowest safe altitude or 10000’ whichever is higher

To descend:
TL idle

Extend speedbrakes

IF structural integrity is in doubt limit airspeed and avoid high maneuvering loads.

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ENG FUEL VALVE L,R

On ground

(No memory items)

Do not attempt engine start

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Conditions for Eng In-Flight Start ?

(3)

All of the following are true:

There is N1 rotation

There was NO engine fire

There is NO abnormal airframe vibrations

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SPEEDBRAKE EXTENDED - conditions?

(3)

one or more:

RA between 15-800’

Flap lever in landing setting

TL not idle

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CONFIG GEAR condition

Gear not down and locked and:

Below 800’ RA and TL near idle
or
Flaps in landing pos.

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CONFIG SPOILERS condition?

One of these:

Speedbrak lever is not down during Takeoff

Speedbrake lever is extended beyond ARMED in flight with climb thrust or greater

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PF Stall maneuver?

Initiate recovery:

Smoothly apply nose down elevator
to reduce the angle of attack until
buffet or stick shaker stops

Continue recovery:

Roll in the shortest direction to
wings level if needed
*Advance thrust levers as needed
*Retract the speedbrakes
*Do not change gear or flap
configuration, except:
*During liftoff, if flaps are up, call
for flaps 1

Complete recovery:

*Check airspeed and adjust thrust as
needed
*Establish pitch attitude
*Return to desired flight path
*Re-engage the autopilot and
autothrottle, if desired

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GPWS maneuver (PF)

Disengage autopilot
Disconnect autothrottle(s)
Aggressively apply maximum* thrust
Simultaneously roll wings level and rotate
to an initial pitch attitude of 20°
Retract speedbrakes
If terrain remains a threat, continue rotation
up to the pitch limit indicator or stick
shaker or initial buffet
——————————
Do not change gear or flap configuration
until terrain separation is assured
Monitor radio altimeter for sustained or
increasing terrain separation
When clear of the terrain, slowly decrease
pitch attitude and accelerate

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Rejected Takeoff above 80 kts conditions?

Fire or Fire Warning
Engine Failure
PWS Warning
Airplane unsafe or unable to fly

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Rejected Takeoff maneuver - Captain

Without delay:

Simultaneously close thrust levers,
disconnect autothrottles, and apply
maximum manual wheel brakes or
verify operation of RTO autobrakes.

If RTO autobrakes is selected, monitor
system performance and apply manual
wheel brakes if the AUTOBRAKE
message is displayed or deceleration is
not adequate.

Apply reverse thrust up to the
maximum amount consistent with
conditions.

Verify the speedbrakes are extended.

Continue maximum braking until
certain the airplane can stop on the
runway.

When stopping is assured:

Start movement of the reverse thrust
levers to reach the reverse idle detent
before taxi speed.

After the engines are at reverse idle,
move the reverse thrust levers to full
down

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Climb RA in LDG config maneuver?

Study These Flashcards

Disengage the autopilot and
disconnect the autothrottle.

Advance
thrust levers forward to ensure
maximum thrust is attained and call for
FLAPS 20. Smoothly adjust pitch to
satisfy the RA command. Follow the
planned lateral flight path unless visual
contact with the conflicting traffic
requires other action.

Pilot Monitoring
Verify maximum thrust set. Position
flap lever to 20 detent.

PM - Verify a positive rate of climb on the
altimeter and call “POSITIVE RATE.”

Verify a positive rate of climb on the
altimeter and call “GEAR UP.”

Historically upset definitions?

Pitch + 25 nose up Pitch + 10 nose down Bank + 45 degrees less than the above parameters but flying at an airspeed inappropriate for the conditions

What is the "new" upset definition?

Any time an airplane is diverting from the intended airplane state.

Stall condition suspected parameters?

Stick shaker Buffet Lack of pitch authority Lack of roll control Inability to stop descent

Nose High Recovery?

*Recognize and confirm the developing situation. *Disengage autopilot *Disconnect autothrottle Recover *Apply nose down elevator. Apply as much elevator as needed to obtain a nose down pitch rate. *Apply appropriate nose down stabilizer trim* *Reduce thrust *Roll (adjust bank angle) to obtain a nose down pitch rate* Complete the recovery: *When approaching the horizon, roll to wings level *Check airspeed and adjust thrust *Establish pitch attitude

Nose Low Recovery maneuver?

Recognize and confirm the developing situation. * Disengage autopilot * Disconnect autothrottle Recover * Recover from stall, if needed * Roll in the shortest direction to wings level. If bank angle is more than 90 degrees, unload and roll* Complete the recovery: * Apply nose up elevator * Apply nose up trim, if needed* * Adjust thrust and drag, if needed

In regards to windshear what are Unacceptable flight deviations?

Uncontrolled changes away from normal steady flight below 1000' AGL: 15 kts IAS 500 fpm VS 5 degrees pitch 1 dot displ. from GS Unusual thrust lever position for a significant period of time

Windshear Escape maneuver (PF) Manual Flight

*Disengage autopilot *Push either TO/GA switch *Aggressively apply maximum* thrust *Disconnect autothrottle(s) *Simultaneously roll wings level and rotate toward an initial pitch attitude of 15° *Retract speedbrakes *Follow flight director TO/GA guidance (if available)** ** do not exceed PLI

For ECL do you need to read aloud or visually confirm items that are complete (green)?

No, call "__Checklist Complete" PF visually confirm CHECKLIST COMPLETE indication "Checklist complete"

What does the CI recommend in case of Single ECL malfunction?

Confirm that the control position or system condition is correct as stated in the checklist step, then use the item override key (ITEM OVRD) to complete the step. Continue to use ECL.

What does the CI recommend for Multiple ECL malfunctions?

Discontinue use of the ECL and use the backup checklist (QRH or equivalent) for the remainder of the flight. Use the EICAS alert messages, but disregard the checklist icons on the EICAS message list. Do not combine the use of ECL and QRH. If the CHKL INCOMPLETE NORM or CHKL NON-NORMAL messages show, confirm that the appropriate checklist has been completed using the QRH or equivalent, then ignore the message.

Can you combine ECL and QRH?

Name the Miscellaneous NNC's

Ditching Overweight Landing

What does a rectangle icon mean [ ]

Precedes all EICAS alert messages that have: Procedural steps Notes Other info

EICAS alert messages without rectangle icons are?

Informational, have no procedural steps or notes, or the action is obvious (such as OVERSPEED).

Checklists printed in bold type?

Quick Action Index checklists

Checklists in upper case (autobrake)

Annunciated by EICAS or other indication

Checklists in upper and lower case?

Not annunciated

Are memory items identified i ECL's?

What is the primary purpose of the non-normal menu for ECL's?

To access unannunciated checklists and condition statements for EICAS alert msg's without rectangle icons

What can the non-normal menu also be used for in ECL's?

Access EICAS alert checklists with a rectangle icon to allow review of the checklist.

What must the PM do with closed loop (sensed) checklist items?

Check off any open loop (not sensed) items and verify that all closed loop items are green

According to CI, what are some the cases when a checklist is started without an icon?

Unannunciated checklist Non-normal condition occurring more than once in a flight (CHKL RESET) Checklist opened only for review CHKL opened by accident

What can you do if you have opened a ECL either by accident, for review or the condition no longer exists and checklist was not completed? To force it back to inactive state?

Select CHKL OVRD key on bottom of the checklist page Otherwise it can remain active

What does the CHKL OVRD also override?

Notes collected on Notes page Inhibited checklists Deferred items at the end of normal checklists

Should you use the CHKL OVRD to pause a checklist?

No, close the ECL. It will stay active and available via the non-normal key

What colour does a line item become if ITEM OVRD is selected?

Cyan

According to CI when should the PF call for the checklist? (3)

Flight path under control Not in critical phase of flight (Takeoff or landing) All memory items are complete

When is the verbal confirmation required during non-normal in flight?

A/T arm switch Thrust lever Fuel control switch Eng, APU, Cargo fire arm switch Gen Drive disconnect switch *not for Dual Eng/Fail/Stall

Is confirmation needed for non-normal checklist on the ground?

What are consequential messages on EICAS?

Result of doing a non-normal checklist Shown for crew awareness Rectangle removed Like "do not accomplish the following checklist" for QRH reading in ECL Consequential checklist will be inhibited checklists

In special situations with multiple failures what should the crew consider to do first in terms of checklist priority?

Consider doing memory items first

According to CI when must the crew land at the nearest suitable airport?

Instructed by NNC Fire or smoke continues Only 1 AC poser source (main, APU or backup gen) Any other situation determined by the crew to have significantly adverse effect on safety if flight is continued

Are there any NNC for loss of engine indication, vibrations or oil qty?

How many times should you attempt to reset a switch in when directed by NNC?

Only once per flight. For any additional attempts in NNC select ITEM OVRD

QRH - Memory Items Flashcards

(58 cards)