Memory Items and Manouvers

Question 1

ABORTED ENGINE START QRH- 7.1

Answer 1

• FUEL CONTROL switch (affected side)…………………CUTOFF

Question 2

CABIN ALTITUDE or Rapid Depressurization QRH- 2.1

Answer 2

• Don the oxygen masks
• Establish crew communications
• Check the cabin altitude and rate
• If the cabin altitude is uncontrollable
  
  • If PAX:
    
    • PASS OXY switch - Push and hold for 1 second
  • Emergency descent - Initiate
  • Thrust levers (both) - Idle
  • Speedbrake - UP
• If structural damage is not suspected:
  
  • Target speed - VMO/MMO
• If strutural damage is suspected:
  
  • Target speed - At or less than current IAS
  • Limit airspeed and avoid high manouvering loads
• If JA605F:
  
  • SPeedbrakes may autostow to 50% at 320kts. Do not override until speed less than 315kts
• Transponder - 7700
• Descend to the lowest safe altitude or 10,000ft whichever is higher

Question 3

Dual Engine Failure QRH 7.3

Answer 3

• ENG START selectors (both)………………………………………….FLT
• Thrust levers (both)…………………………………………………………Idle
• FUEL CONTROL switches (both)………….CUTOFF then RUN
• IF engine appears stalled OR EGT approaches the maximum EGT limit (960’c) of the Standby Engine Indicator:
  
  • Repeat above step as needed

Question 4

Engine Limit or Surge or Stall QRH 7.7

Answer 4

• A/T ARM switch - OFF
• Until engine indications stay within limits or the thrust lever is at idle
• Thrust lever (affected side) - Confirm - Retard

Question 5

ENGINE FIRE or Engine Severe Damage or Separation QRH 8.2

Answer 5

• A/T ARM switch - OFF
• Thrust lever (affected side) - Confirm - Idle
• Fuel control switch (affected side) - Confirm - CUTOFF
• Engine fire switch (affected side) - Confirm - Pull
• If the engine fire warning light is illuminated:
  
  • Engine fire switch (affected side) - Rotate to the stop and hold for 1 second
• If after 30 seconds the engine fire warning light stays illuminated:
  
  • Engine fire switch (affected side) - Rotate to the other stop and hold for 1 second

Question 6

UNSCHD STAB TRIM QRH 9.1

Answer 6

STAB TRIM CUT OUT switches (both) - CUT OUT

Question 7

Airspeed Unreliable QRH 10.1

Answer 7

• Check the pitch attitude and thrust
• If pitch attitude or thrust is not normal for phase of flight:
  
  • Autopilot disengage SW - Push to disengage
  • Autothrottle disconnect SW - Push to disconnect
  • F/D switches (both) - OFF
  • Establish normal pitch attitude and thrust setting for phase of flight

Question 8

AUTOMATIC UNLOCK QRH 1.1

Answer 8

• FLT DK DOOR lock selector - Rotate to DENY and hold for 1 second

Question 9

Non-normal Flow

Answer 9

• Checklist- Non Normal
• EICAS
• Checklist- Normal
• ATC- Wx & App info- STBY INTENTIONS
• Intentions-Advise
• ATC- Clearance
• Advise Company
• Set CDU- RTE Check
• LDG ALT
• LDG Dist
• RECALL
• LDG setup (Flap, App SPD, Auto-brakes, set your side)
• Set Own side- APP brief, SPDS
• Descent Checklist
• Approach checklist

Question 10

FCC Fail

Answer 10

• Lose- ADI, HSI (Not blank, just lose F/D on ADI & Track info on HSI)
• NO LAND 3 appears on ASA
• ACTION- “Left ADI/ HSI blank, check Right side”
• “Right side normal” “You have control (Modes)”
• “______ FCC Fault, FLT DIR (C,R)”
• “Left ADI, HSI normal, I have control”
• “You have control”
• “Check EICAS message”
• INTENTION
• CONTACT COMPANY TO ADVISE

Question 11

ADC Fail

Answer 11

• ASI- Blanks, 260 set on SPD
• ALT- Blanks
• VSI- Blanks
• ‘L ENG EEC MODE’ ‘R ENG EEC MODE’
• ACTION- “Air SPD, Altimeter, Vertical SPD failure, check Right side”
• “Right side normal” “You have control (Modes)”“______
• ADC Fail, ____ ADC SW ALTN
• “AIRSPEED_____, ALT______, VS______”
• “Same as right side”“Left Side back on normal, I have control” “You have control”
• “Check EICAS message”. “L & R ENG EEC MODE”“ENG EEC MODE CHECKLIST”
• “Check EICAS MSG”
• “Left ADC FAIL, now flying with RIGHT ADC, non RVSM, Contact ATC and advise Unable RVSM request next highest level to FL290”
• “Contact company advise situation, request fuel figures for FL______”

Question 12

Go-Around

Answer 12

• “Go Around” ( GA SW push)
• “3 GA, Flap 20” “Flap 20, Positive” “Gear Up” “F/D ON” (If rejected LDG) “Gear Up”, Gears Up”
• @ OR ABV 400ft”LNAV/ HDG SEL” “LNAV/ HDG SEL”
• @1500ft”Set CLB Thrust”
• @ ALT CAP”SPD, ALT CAP”“SPD Set to VREF+60”@ VREF + 20” A/S Checked, Flap 5” “Flap 5, Flap 5” A/S checked, Flap 1” “Flap 1, Flap 1”
• “ATO CHECKLIST”
• “Check Weather/ APP INFO”
• “Request RV ILS”
• “Set CDU, ILS RWY ___, INTC CF___ , CRS ___, MAP _____ft”
• “VREF 30 is ____ Bug set”
• “RV ILS ____, procs same as before”“Check Recall”
• “Descent & APP checklist”

Question 13

Rejected Take-Off

Answer 13

• THRUST LEVERS- CLOSE (Disconnect A/T if BLW 80kts)
• VERIFY OPERATION OF AUTOBRAKES OR APPLY MAXIMUM ALLOWABLE BRAKING
• MAXIMUM ALLOWABLE REVERSE THRUST
• (If speed brake lever did not move UP automatically) SPEEDBRAKE LEVER UP
• Continue maximum braking till A/C is decelerated sufficiently
• When flight is not continued perform after LDG procedures
• When flight is continued see T/O weight limit by brake temp as described in chapter 2

Question 14

GPWS Warning (‘PULL UP’, ‘TERRAIN TERRAIN PULL UP’ or ‘OBSTACLE OBSTACLE PULL UP’)

Answer 14

• Disengage A/P
• Disconnect A/T
• Aggressively apply maximum thrust
• Simultaneously roll wings level and rotate to an initial pitch atttude of 20’
• Set the SPEEDBRAKE lever to DOWN
• If terrain remains a threat, continue rotation up to pitch limit indicator, stick shaker or initial buffet
• Do not change flap or gear configuration until terrain separation is assured
• Monitor RADALT for sustained or increasing terrain separation
• When clear of terrain, slowly decrease pitch attitude and accelerate
• FLIGHT AT STICK SHAKER MAY BE REQ’D
• DO NOT USE F/D COMMANDS

Question 15

Windshear Escape Maneuver MANUAL FLIGHT

Answer 15

• Disengage A/P
• Push G/A switch
• Aggressively apply MAX thrust
• Disconnect A/T
• Simultaneously ROLL wings LVL and rotate toward an initial pitch ATT of 15’
• Speedbrake lever DOWN
• Follow FD guidance (If avail)
• Do not change GEAR & FLAP config until WS no longer a factor
• Monitor VS and ALT
• Do not attempt to regain lost A/S until WS no longer a factor

Question 16

Windshear Escape Maneuver AUTOMATIC FLIGHT

Answer 16

• Push either G/A switch
• Verify GA mode annunciation
• Verify thrust levers advance to GA power
• Speedbrake Lever DOWN
• Monitor system performance
• Do not change GEAR & FLAP config until WS no longer a factor
• Monitor VS and ALT
• Do not attempt to regain lost A/S until WS no longer a factor
• IF GA MODE UNAVAIL FLY MANUALLY!

Question 17

ENG Failure in Final APP?

Answer 17

• Advance operating ENG to GA position
• Retract to Flaps 20
• Maintain VREF 30+10kts (Equivalent to VREF Flap 20)
• DECIDE GA or CONTINUE
• GA - Maintain VREF 30+10kts & execute GA proc (Flap5, “positive” gear up)
• CONTINUE - Maintain SPD conduct OEI LDG.

Question 18

RA

Answer 18

• If manoeuvring is Req’d
• A/P- DISENGAGE
• A/T- DISCONNECT
• Smoothly adjust pitch & thrust to satisfy RA command
• If stick shaker occurs, accomplish stall recovery procedure-
• f high speed buffet occurs, relax pitch force to reduce buffet but continue the manoeuvre
• Do not use F/D commands until clear of conflict

Question 19

CLB RA in LDG CONFIG

Answer 19

• A/P - DISENGAGE
• A/T- DISCONNECT
• Thrust levers FULL FORWARD
• Call “Flaps 20”
• Smoothly adjust pitch to satisfy the RA command
• “POSITIVE” “GEAR UP”

Question 20

Nose HIGH Recovery

Answer 20

• Recognize & Confirm situtation
• DISENGAGE A/P & DISCONNECT A/T
• Apply as much FULL DOWN ELEVATOR
• Apply appropriate nose down TRIM
• REDUCE Thrust
• ROLL to obtain nose down pitch rate
• Complete recovery
• When approaching HORIZON, roll wings LVL
• Check A/S & adjust Thrust
• Establish pitch ATT

Question 21

Nose LOW Recovery

Answer 21

• Recognize & Confirm
• DISENGAGE A/P & DISCONNECT A/T
• RECOVER from Stall (if req’d)
• ROLL in shortest direction to wings LVL
• RECOVER to LVL flight-
• Apply nose up elevator
• Apply nose up trim if required
• Adjust thrust and drag as req’d

Question 22

What is an UPSET defined as?

Answer 22

• >25’ Nose UP
• >10’ Nose DOWN
• AOB> 45’
• A/S inappropriate for conditions

Question 23

Approach to Stall or Stall Recovery

Answer 23

• Initiate the Recovery
• Hold control column firmly
• Disengage A/P disconnect A/T
• Smoothly apply NOSE DOWN elevator to reduce AOA until buffet or stick shaker stops (Trim may be req’d)
• Continue the Recovery
• ROLL in shortest direction to wings LVL
• ADVANCE thrust
• SPEEDBRAKE DOWN
• Do not change Gear & Flap except during liftoff if Flaps are UP call for Flaps 1
• Complete the Recovery
• Check A/S and adjust thrust as req’d
• Establish pitch ATT
• Return to desired flight path
• Re-engage A/P & A/T if desired

Question 24

Aborted Engine Start

Answer 24

• No EGT increase by 25 sec after fuel cont switch is moved to run
• No N1 rotation by 30 seconds after N2 is stabalized at idle
• EGT quickly or near exceeds the start limit
• Oil pressure indication is not normal by time the engine is stabalized at idle

Question 25

What are the two indications A/C is in WIndshear?

Answer 25

* 1) "WINDSHEAR, WINDSHEAR, WINDSHEAR" * Immediate alert * Excessive Windshear at A/P current position * Enabled BLW 1,500ft RAD ALT * Detection begins at rotation * 2) Unacceptable flight path deviations

Question 26

What are Unacceptable flight path deviations?

Answer 26

* Uncontrolled changes from normal steady state flight conditions BLW 1,000ft AGL in excess of: * 15 KIAS * VS 500fpm * 5' pitch ATT * 1 dot displacement from GS * Unusual thrust lever position for a significant amount of time

Question 27

Steep turn method?

Answer 27

* Cabin sign ON * VOR mode (PF) * A/S=250kts * DES & APP Check * PWR- 66% (280t-61%) * ATT- 2- 2.5' ROLLING INTO TURN (Use fast slow pointer if 250kts bugged) * ADD PWR- 3% (280t-64%) * ATT- 2.5- 3' ROLLING OUT OF TURN * 15' to go start rollout * PWR- 66% (280t-61%) * ATT- 2- 2.5'

Question 28

"GO AROUND WINDSHEAR AHEAD"

Answer 28

* Enabled during APP BLW 1,200ft AGL * Windshear within 1.5 nm & DIRECTLY ahead of plane * If WX not selected on HSI, PWS symbology will auto pop up * Shows position & size only when HSI in VOR,APP,MAP,CTR MAP mode * Perform Windshear escape maneuver

Question 29

"WINDSHEAR AHEAD, WINDSHEAR AHEAD"

Answer 29

* Enabled during T/O BLW 1,200ft * Windshear within 3nm & DIRECTLY ahead of plane * If WX not selected on HSI, PWS symbology will auto pop upshows position & size only when HSI in VOR,APP,MAP,CTR MAP mode * Prior to V1 - REJECT * After V1 - Rotate at normal rate to 15' after airborne perform Windshear escape maneuver * IF WINDSHEAR ENCOUNTERED AND A/S DECREASES AND NOT ENOUGH ROOM TO STOP * Initiate normal rotation at least 2,000ft before end of RWY even if A/s low * Higher than normal pitch ATT may be req'd * Ensure MAX thrust set