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AJX Study > Memory Items and Manouvers > Flashcards

Memory Items and Manouvers Flashcards

1
Q

ABORTED ENGINE START QRH- 7.1

A
  • FUEL CONTROL switch (affected side)…………………CUTOFF
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2
Q

CABIN ALTITUDE or Rapid Depressurization QRH- 2.1

A
  • 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
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3
Q

Dual Engine Failure QRH 7.3

A
  • 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
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4
Q

Engine Limit or Surge or Stall QRH 7.7

A
  • A/T ARM switch - OFF
  • Until engine indications stay within limits or the thrust lever is at idle
  • Thrust lever (affected side) - Confirm - Retard
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5
Q

ENGINE FIRE or Engine Severe Damage or Separation QRH 8.2

A
  • 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
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6
Q

UNSCHD STAB TRIM QRH 9.1

A

STAB TRIM CUT OUT switches (both) - CUT OUT

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7
Q

Airspeed Unreliable QRH 10.1

A
  • 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
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8
Q

AUTOMATIC UNLOCK QRH 1.1

A
  • FLT DK DOOR lock selector - Rotate to DENY and hold for 1 second
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9
Q

Non-normal Flow

A
  • 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
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10
Q

FCC Fail

A
  • 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
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11
Q

ADC Fail

A
  • 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______”
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12
Q

Go-Around

A
  • “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”
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13
Q

Rejected Take-Off

A
  • 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
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14
Q

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

A
  • 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
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15
Q

Windshear Escape Maneuver MANUAL FLIGHT

A
  • 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
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16
Q

Windshear Escape Maneuver AUTOMATIC FLIGHT

A
  • 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!
17
Q

ENG Failure in Final APP?

A
  • 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.
18
Q

RA

A
  • 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
19
Q

CLB RA in LDG CONFIG

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

Nose HIGH Recovery

A
  • 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
21
Q

Nose LOW Recovery

A
  • 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
22
Q

What is an UPSET defined as?

A
  • >25’ Nose UP
  • >10’ Nose DOWN
  • AOB> 45’
  • A/S inappropriate for conditions
23
Q

Approach to Stall or Stall Recovery

A
  • 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
24
Q

Aborted Engine Start

A
  • 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
25
Q

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

A
  • 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
26
Q

What are Unacceptable flight path deviations?

A
  • 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
27
Q

Steep turn method?

A
  • 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’
28
Q

“GO AROUND WINDSHEAR AHEAD”

A
  • 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
29
Q

“WINDSHEAR AHEAD, WINDSHEAR AHEAD”

A
  • 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

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