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FedEx 767 QRH > QRH Rev 11 - Maneuvers > Flashcards

QRH Rev 11 - Maneuvers Flashcards

1
Q

QRH Rev 11 - (Non-Norm) Man 2.2 - RTO

Before 80 knots, reject the takeoff for any of the following:

A

Before 80 knots, reject the takeoff for any of the following:

Fire or fire warning
Engine Failure
Airplane is unsafe or unable to fly
Predictive wind shear alert

Master caution
Takeoff configuration Light
System malfunction
Tire malfunction
Airplane slow to accelerate
Open side window
Unusual noise or vibration
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2
Q

QRH Rev 11 - (Non-Norm) Man 2.2 - RTO

Above 80 knots and prior to V1, the takeoff should be rejected for any of the following:

A

Fire or fire warning
Engine failure
Airplane is unsafe or unable to fly
Any wind shear alert or warning

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3
Q

QRH Rev 11 - (Non-Norm) Man 2.2 - RTO

List the steps for the Captain in the Rejected Takeoff Procedure:

A

WITHOUT DELAY:

  • Simultaneously 1) close the thrust levers, 2) disengage the auto-throttles, 3) 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 AUTOBRAKES light illuminates or deceleration is not adequate.
  • Raise SPEEDBRAKE lever.
  • Apply reverse thrust up to maximum amount consistent with conditions.
  • Continue maximum braking until 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 le-vers to full down.

CALL FOR RTO CHECKLIST

CONSIDER:

  • Fuse plugs melting
  • Clear runway
  • Remote Parking
  • Wind Direction (Fire)
  • Alert fire equipment
  • Advise ground crew of hot brakes
  • Supernumeraries (remain seated or evacuate)
  • what caused RTO?… checklist?
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4
Q

QRH Rev 11 - (Non-Norm) Man 2.10 - Windshear

What are the indications an airplane is encountering a windshear?

A

• Uncontrolled flight path deviations from normal steady state flight conditions below 1,000 feet AGL, in excess of any of the following:

  • 15 knots indicated airspeed.
  • 500 FPM vertical speed.
  • 5 degrees pitch attitude.
  • 1 dot displacement from the glideslope.
  • Unusual thrust lever position for a significant period of time.

• Windshear Immediate-Alert Warning (two-tone siren followed by “WINDSHEAR, WINDSHEAR, WINDSHEAR”).

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5
Q

QRH Rev 11 - (Non-Norm) Man 2.11 - Windshear

Wind-shear Escape Maneuver steps with flight director guidance - Manual Flight

A
  • Disconnect autopilot.
  • Push either go-around switch.
  • Aggressively apply maximum thrust.
  • Disconnect autothrottle.
  • Roll wings level and rotate toward an initial pitch attitude of 15°.
  • Retract speedbrakes.
  • Follow flight director GA guidance (if available).

Once through wind-shear, proceed with go-around maneuver to clean up.

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6
Q

QRH Rev 11 - (Non-Norm) Man 2.11 - Windshear

Wind-shear Escape Maneuver steps with flight director guidance - Automatic Flight

A
  • Push either go-around switch.
  • Verify TO/GA mode annunciation.
  • Verify GA thrust.
  • Retract speedbrakes.
  • Monitor system performance.

Once through the wind-shear, perform go-around maneuver to clean up.

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7
Q

QRH Rev 11 - (Non-Norm) Man 2.1 - Aprch to Stall Recovery

Approach to Stall Recovery Steps - PF

A

Initiate the recovery:
• Hold the control column firmly.
• Disconnect autopilot and auto-throttle.
• Smoothly apply nose down elevator to reduce the angle of attack until buffet or stick shaker stops.
Nose down sta-bilizer trim may be needed.

Continue the 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 the recovery:
• Check airspeed and adjust thrust as needed.
• Establish pitch attitude.
• Return to the desired flight path.
• Re-engage the autopilot and auto-throttle if desired.

WARNING: if the control column does not provide the needed response, stabilizer trim may be necessary.

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8
Q

QRH Rev 11 - (Non-Norm) Man 2.1 - Aprch to Stall Recovery

Approach to stall recovery - Steps (PM):

A
  • Monitor altitude and air-speed.
  • Verify all required actions have been done and call out any omissions.
  • Call out any trend toward terrain contact.
  • Set the FLAP lever as directed.

WARNING: if the control column does not provide the needed response, stabilizer trim may be necessary.

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9
Q

QRH Rev 11 - (Non-Norm) Man 2.2 - RTO

List the steps for the FO in the Rejected Takeoff Procedure:

A

VERIFY ACTIONS AS FOLLOWS:

  • Thrust levers closed.
  • Autothrottle disengaged.
  • Maximum brakes applied.
  • Verify speedbrake lever UP, call “Spoilers Deployed”. If speed-brake lever not UP call “No Spoil-ers”.
  • Reverse thrust applied. When both REV indications are green, call “REVERSERS NORMAL”.
  • If there is no REV indication(s) or the indication(s) stays amber, call “NO REVERSER LEFT EN-GINE”, or “NO REVERSER RIGHT ENGINE”, or “NO RE-VERSERS”.
  • Call out any omitted action items
  • Call out 60 knots.
  • Communicate the reject decision to the control tower as soon as practical.

GO TO QRH - RTO CHECKLIST

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10
Q

QRH Rev 11 - (Non-Norm) Man 2.4 - Terrain Avoidance / GPWS

When can the below glideslope deviation alert be canceled or inhibited?

A

Cancel the below glideslope deviation alert for any of these conditions:

  • Localizer or backcourse approach.
  • Circling approach from an ILS.
  • When conditions require a deliberate approach below glideslope.
  • Unreliable glideslope signal.
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11
Q

QRH Rev 11 - (Non-Norm) Man 2.4 - Terrain Avoidance / GPWS

When is the one time, during a terrain/GPWS caution, that the alert may be treated as cautionary and the approach continued?

A

In daylight/VMC conditions and positive verification is made that no obstacle or terrain hazard exists.

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12
Q

QRH Rev 11 - (Non-Norm) Man 2.4 - Terrain Avoidance / GPWS

What is the response for a “Terrain avoidance / GPWS alert - Pilot Flying (PF)..?

A
  • Disconnect autopilot.
  • Disconnect autothrottle.
  • Aggressively apply maximum thrust.
  • Simultaneously roll wings level and rotate to an initial pitch atti-tude of 20°.
  • Retract speedbrakes.
  • If terrain remains a threat, con-tinue rotation up to the pitch lim-it indicator or stick shaker or initial buffet.… Do not change gear or flap settings
    … Do not use flight director
    … Monitor radio altimeters for increasing terrain separation
    … When clear of terrain, decrease pitch and accelerate.
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13
Q

QRH Rev 11 - (Non-Norm) Man 2.4 - Terrain Avoidance / GPWS

What is the response for a “Terrain avoidance / GPWS alert - Pilot Monitoring (PM)..?

A

• Verify maximum thrust.
• Verify all required actions have been completed - call out any omissions.
• Monitor vertical speed and altitude.
- radio altitude for terrain clearance .
- barometric altitude for a minimum safe altitude.
• Call out any trend toward terrain contact.

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14
Q

QRH Rev 11 - (Non-Norm) Man 2.6 - Traffic Avoidance / Res Advisory

Take the following actions for a “Traffic Advisory” - PF and PM

A
  • Look for traffic using traffic display as a guide.
  • Call out any conflicting traffic.
  • If traffic is sighted, maneuver as re-quired.
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15
Q

QRH Rev 11 - (Non-Norm) Man 2.6 - Traffic Avoidance / Res Advisory

LIST the actions to take for a Resolution Advisory (RA) (except a climb in landing configuration) - PF:

A
  • Disengage the autopilot
  • Disengage the autothrottle.
  • Smoothly adjust pitch and thrust to satisfy the RA command.
  • Follow the planned lateral flight path unless visual contact with the traffic requires other action.
  • Attempt to establish visual contact. Call out any conflicting traffic.
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16
Q

QRH Rev 11 - (Non-Norm) Man 2.6 - Traffic Avoidance / Res Advisory

LIST the actions to take for a Resolution Advisory (RA) (except a climb in landing configuration) - PM:

A

Attempt to establish visual contact. Call out any conflicting traffic.

17
Q

QRH Rev 11 - (Non-Norm) Man 2.6 - Traffic Avoidance / Res Advisory

LIST the actions to take for a “Climb In Landing Configuration” Resolution Advisory” - PF:

A
  • Disengage the autopilot.
  • Disengage the auto-throttle.
  • Advance thrust levers forward to maximum thrust.
  • Call for FLAPS 20.
  • Smoothly adjust pitch to satisfy the RA command.
  • Follow the planned lateral flight path unless visual contact with traffic requires other action.… Verify a positive rate of climb on the altimeter and call “GEAR UP.”
    … Attempt to establish visual contact.
    … Call out any conflicting traffic.
18
Q

QRH Rev 11 - (Non-Norm) Man 2.6 - Traffic Avoidance / Res Advisory

LIST the actions to take for a “Climb In Landing Configuration” Resolution Advisory - PM

A
  • Verify maximum thrust set.
  • Position flap lever to 20 detent.
  • Verify a positive rate of climb on the altimeter and call “POSITIVE RATE.”
  • Set the landing gear lever to UP.
  • Attempt to establish visual contact.
  • Call out any conflicting traffic.
19
Q

QRH Rev 11 - (Non-Norm) Man 2.6 - Traffic Avoidance / Res Advisory

When should a “DESCEND” RA not be followed?

A

When issued below 1,000’ AGL

20
Q

QRH Rev 11 - (Non-Norm) Man 2.8 - Upset Recovery

List the indicators of a “stalled airplane”:

A
  • Stick shaker
  • Buffet that can be heavy at times
  • Lack of pitch authority
  • Lack of roll control
  • Inability to stop a descent.
21
Q

QRH Rev 11 - (Non-Norm) Man 2.8 - Upset Recovery

List the “Historical Upset Airplane Conditions”:

A
  • Pitch attitude greater than 25 degrees nose up, or
  • Pitch attitude greater than 10 degrees nose down, or
  • Bank angle greater than 45 degrees, or
  • Flying at an airspeed inappropriate for the conditions.
22
Q

QRH Rev 11 - (Non-Norm) Man 2.8 - Upset Recovery

What is the “new definition” of an Airplane Upset Condition?

A

any time an airplane is diverting from the intended airplane state. Can involve any or all of the following:

  • Pitch or roll angle deviations
  • Inappropriate airspeeds for the conditions.
23
Q

QRH Rev 11 - (Non-Norm) Man 2.8 - Upset Recovery

“Nose High Recovery” steps - PF

A
  • Disconnect autopilot.
  • Disconnect autothrottle.
  • Apply nose down elevator 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.
24
Q

QRH Rev 11 - (Non-Norm) Man 2.8 - Upset Recovery

“Nose High Recovery” steps - PM

A
  • Call out attitude, airspeed and altitude throughout the recovery.
  • Verify all required actions have been completed and call out any omissions.
25
Q

QRH Rev 11 - (Non-Norm) Man 2.8 - Upset Recovery

“Nose Low Recovery” steps - PF

A 
• Disconnect autopilot.
• Disconnect autothrottle
• Recover from stall, if required.
• Roll in the shortest direction to wings level (unload and roll if bank angle is more than 90°).
• Recover to level flight:
    - Apply nose up elevator.
    - Apply nose up trim, if required.
    - Adjust thrust and drag as required.
26
Q

QRH Rev 11 - (Non-Norm) Man 2.8 - Upset Recovery

“Nose Low Recovery” steps - PM

A
  • Call out attitude, airspeed and altitude throughout the recovery.
  • Verify all required actions have been completed and call out any omissions.
27
Q

QRH Rev 11 - (Non-Norm) Man 2.11 - Windshear

Windshear encountered during takeoff roll - actions -PF

A

*** If windshear is encountered prior to V1, there may not be sufficient runway remaining to stop if an RTO is initiated at V1.

  • At VR, rotate at a normal rate toward a 15 degree pitch attitude.
  • Once airborne, per-form the Windshear Escape Maneuver.
28
Q

QRH Rev 11 - (Non-Norm) Man 2.11 - Windshear

Windshear encountered “near the normal rotation speed” - actions - PF

A

*** If windshear is encountered near the normal rotation speed and air-speed suddenly decreases, there may not be sufficient runway left to accelerate back to normal takeoff speed.

If there is insufficient run-way left to stop:

  • initiate a normal rotation at least 2,000 feet before the end of the runway (even if airspeed is low.)
  • Higher than normal attitudes may be required to lift off in the remaining runway.
  • Ensure maximum thrust is set.
29
Q

QRH Rev 11 - (Flt Pat) Man 3.3 - Eng Fail at V1 (V1 Cut)

Engine Failure at V1 (V1 Cut) Maneuver - List the steps for both seats:

A
  • PF - - PM -
                                                                                     “V1… Engine Failure… Rotate” (Begin takeoff rotation)
2 deg/sec… 12.5/deg)
(V2 x V2+15 kts)
(15 deg bank if < V2+15 kts)
(Establish climb, then Flt Dir)
                                                                                 “Positive Rate”   “Gear Up” 
                                                                                 (Raises gear handle)
(Adjust pitch to V2 & pos climb)
(Follow Flt Dir)
(Confirm good track)
(Trim into good engine) (Above 400 ft. RA)… “LNAV” 
                               or “Heading Select”
                                                                                 “Engaged”
                                                                                 (Notify ATC) (At Acceleration Height - normally 1000 ft. AFE),               “Clear the Master Caution”  “Vertical Speed 0 to +200”  “Set Top Bug”  “Autopilot On”   “What’s the problem?”
                                                                                           “(PM states the actual condition)”
                                                                                             (ie: “Engine severe damage - no N1”) “QRC”
                                                                                           (FO runs QRC) (Clean up on schedule)
                                                                                           “QRC complete”
                                                                                           “Standing by XX checklist” (QRH) At Flaps Up Maneuvering Speed:
“VNAV” or “FLCH, Top Bug”
“Select and Set Max Continuous”
“Select and Execute ENG OUT”
 “QRC” (if not previously accomplished) 
                                                                                               “Standing by XX checklist” (QRH) “After Takeoff Checklist”  (when QRH Checklist 
is complete to the Deferred Items.)
                                                                                                (Accomplishes After TO Checklist) “Recruise the FMS.”                                                                    
                                                                                                 (Recruises the FMS)
*DOWNWIND*
(Establish roles:)
      PF - Aviate, Communicate
      PM - Monitor PF, QRH, FMS
“In Range checklist” 
“Flaps 1” 
“Approach checklist” 
      (Brief approach)
      (Brief SE specifics for approach)
      (Brief Single Engine GA)

BASE LEG
“Flaps 5” (base leg)

GLIDE SLOPE ALIVE
“Gear down”
“Flaps 20”
“Before Landing checklist”
“Speed following” (if hand flying)
“Give me 5 clicks of trim into my XX engine”
(Set final approach speed) (VREF20 + wind additive)
(Adjust thrust) (4.5 fuel flow)
At 1,000’ “Stable” or “Not stable”
(If “not stable” identify condition)
At 500’ - “Cleared to land, Rwy XX”
At 50’ AGL: (Autopilot off NLT 50’ AGL)

SINGLE ENGINE GA
(Push GA switch)
“Go Around, Flaps 5” (for a flaps 20 appch)
(Verify rotation to GA attitude)
(Verify max thrust reference) ( GA GA in FMAs)
(Verify rotation to GA attitude)
(Verify Max Thrust reference)
(Verify GA GA in FMAs)
(Thrust set to max thrust reference)
“Thrust Set”
“Positive rate” “Positive Rate”
“Gear up… check missed approach altitude.”
“Set” ( verify missed approach alt is set)
400’ AGL
“Heading select” (or) “LNAV”
(Select Heading SEL / LNAV)
Acceleration Height (norm 1,000’)
“VNAV”
“Autopilot On” (select AP on)
(Must have pitch and roll mode for AP on)
(Retract flaps on schedule)
(If flaps remaining at 5 or 1, select SPD Intervene)
and set a bug speed)

At FLAPS UP MANEUVER SPEED
“Select and set max continuous thrust”
(Press CON on TMSP)
(Move thrust lever to CON thrust)
“After TO checklist”
(Do After TO checklist)
“FUEL CONFIG checklist” (if required)

30
Q

QRH Rev 11 - (Flt Pat) Man 3.8 - Visual Pattern

List the sequence for a “Visual Pattern” beginning at “Downwind”:

A

ENTERING DOWNWIND:

  • Flaps 5.
  • 1,500’ AFE
  • 2 NM from runway

DOWNWIND PRIOR TO BASE TURN:

  • Gear down.
  • Flaps 20. (One engine landing flaps)
  • Speedbrakes armed.
  • Begin descent (2-2.5 nm past runway threshold)

BASE:

  • Landing flaps (2 engine)
  • Before Landing checklist.

FINAL APPROACH - Stabilized

  • 2-2.5 nm from threshold.
  • 700-500’ stabilized on profile.

FedEx 767 QRH (2 decks)

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