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Things to keep Reviewing frequently Flashcards

1
Q

What’s the CPT communication with the GND Crew?

A
  1. Ground, FD
  2. Confirm:
    1. Bypass pin is inserted
    2. All Doors+Hatches are closed AND
    3. Ground eq. is removed
  3. Standby for Push/ Cleared P/S. P/B Set
  4. P/B released, Time XX
  5. Are we cleared to start Eng. No 1/2?
  6. P/B set. Cleared to disconnect towbar+bypass pin, advise when clear.
  7. Two good starts, cleared to disconnect headset, hand signals on L/R with the pin.
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2
Q

Final CDU Preflight. Who does what?

A

CPT

FO

  1. Perf INIT Page
    1. Call out OPT masses
    2. OPT ZFW <> eFL eZFW
    3. Call FMC GW <>OPT GW
    4. EXEC
  2. Read OPT T/O Perf lines
  3. N1 Limit Page
    1. TMD<>Derate<>ATRT<>N1
  4. T/O REF Page
    1. ​OPT Flap
    2. OPT C/G
    3. OPT STAB<>FMC STAB
    4. Set STAB (hand)
    5. Call+Set Vspeeds (VFY)
    6. OPT MFRA - Set PFD
  5. OPT Land Dispatch CALC
  6. Sign and Send
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3
Q

Takeoff Brief

A

Done by PF

Standard Items

  1. This is a 8200/800/700,SFP A/C
  2. LHS/RHS T/O
  3. RWY __
  4. Flaps _
  5. NADP _
  6. EOSID

===NON STD===

Inside

  1. Full Thrust
  2. Wet Speeds
  3. Bleeds OFF
  4. A/I ON
  5. MEL/CDL

Outside

  1. Adv WX/ RWY Cond
  2. EOSID
  3. A/P eng alt (if <> 1000’)
  4. T/O alternate
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4
Q

What is the Emergency Brief?

A

CP

F/O

Above 80 kts I will only reject the T/O for:

  1. Fire / Fire WARN
  2. ENG Failure
  3. PWS WARN
  4. Airplane “unsafe” or “unable to fly”

Before V1, if I call “STOP” I will:

  1. Simult. Close Thr Lev & diseng A/T
  2. Apply MAX MAN BRK -OR- verify operation of RTO A/BRKs
  3. Manually raise S/B lev.
  4. Apply Max REV thr. & stop the a/c.
  5. I will set the P/B

If you call “STOP” I will:

  1. Note BRK ON Spd.
  2. Call S/B UP/NOT UP
  3. Call THR REV Norm/Abn. Indications
  4. Verify your actions are complete and call out any omissions
  5. Call 100/80/60+RWY DIST REM
  6. Call “A/B Disarm”
  7. Select F40 when P/B is set
  8. Inform ATC of reject

We will ID the failure and carry out any drills as appropriate. If we decide to EVAC the A/C we will read and do the EVAC CX. If time permits, I will pull the CVR C/B.

If the call

  1. >400’ AGL, verify HDG SEL & complete Memory items
  2. @ MFRA, BUG UP & retr. Flaps on sched.
  3. @FUNL, sel. LVL CHG, confirm MCT, eng. AP & clb. To MSA
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5
Q

What is the DALTA Setup and Brief?

A
  1. Q-DAF-PLN-MOBITA
    1. ​QNH - preselect
    2. Des + FCST (250/100 + Trans LVL + Alt Restr R1)
    3. ARR - select APP
    4. FIX page (3*FL, 10, 4/5, 4.2+ABM)
    5. PROG 4/4 (if RNP, set 0.3)
    6. LEGS - set H+V restr. (<10 nm 180B)
    7. NAVAIDS+CRS
    8. Minima
    9. OPT - populate
    10. Brief
      1. MSA+TAlt
      2. Chart - top strip+LAlt
      3. G/A
      4. QTSAVNG - Double Brief
        1. ​QNH + Minima
        2. T - cold t. corr
        3. Sequence of config
        4. AFDS+A/T modes
        5. V - actions if Visual (think profiles RCL F/Ds, etc.)
        6. N - actions if Not Visual
        7. G - landing gate
        8. CXL
    11. ​INIT REF - OPT, LW, Hold Fuel, Land Flap, Vref, A/BRK
    12. T/A - Taxi and Apron
  2. Take back CTL
  3. DES C/X (VSD ON)
  4. CC - 10 minutes?
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6
Q

What is the Captain’s T/O brief?

A

PBS-SS-EA

  1. Packs
  2. Bleeds
  3. Speeds
  4. SID
  5. Stop ALT
  6. EOSID
  7. Adv WX
  8. +REVIEWED after F/O challenge
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7
Q

What’s in a RIBETS brief and when do you do it?

A

Done after the ATC clearence and mini-brief and PFs pre-flt scanflow complete.

  1. TEM
  2. Route check - Routing (OFP No.+SID/STAR), Tot. Distance, Fuel at destination. Execute
  3. Instrument crosscheck - Clocks, PFD (QNH,ALT,MFRA,F/D, Flags?), SBY instruments (set)
  4. Brief for T/O
  5. Emergency brief
  6. Taxi out routing (Hotspots, etc.)
  7. SID brief (on FIX page)
    1. (Legs page, from chart to PLAN mode,
    2. Trans ALT
    3. SPD/ALT restrictions (stop alt, 220 in first turn if no speed specified, +250/100)
    4. WPT sequencing
    5. EOSID procedure
    6. RNAV contingency
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8
Q

How do you do sidestep manoeuvre?

A
  1. Disconnect - AFDS (PF)
  2. Deselect - (PM) Detune ILS freq from both NAVs
  3. Recycle - (PM) F/Ds
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9
Q

What are the areas of Resp when A/C is Moving under its own power?

A
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10
Q

What are the areas of Resp when A/C NOT Moving under its own power?

A
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11
Q

What is the Pre-FLight sequence?

(i.e. what do you need to do before you get airborne?

A
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12
Q

FD Safety + Prelim FD Procedure PF Flow

A
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13
Q

Pre-FLT Procedure PF flows

A
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14
Q

Final FD Prep Flows

A
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15
Q

After Start Flows

A
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16
Q

Before TO Flows

A
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17
Q

ATOCx flows

A
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18
Q

10 Checks flows

A

+ No SMKG to ON on the way down after the PA

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19
Q

G/A Flows

A

G/A datums for level off ~3* NU/ 230 kts/ 52% N1 (?)

Consider combining LNAV/HDG SEL w Flaps 5 call to avoud overspeed of Flaps

If OEI

  1. G/A, F1
  2. Set G/A Thr
  3. Wait for -1 speed
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20
Q

Landing Flow

A
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21
Q

Taxi in flows

A
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22
Q

Transit/Shutdown Flows

A
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23
Q

Secure Flows

A
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24
Q

When can you NOT use ATRT from the OPT?

A

If ATRT Calculated, select FULL rated thrust when:

  1. A-SKD / REV INOP*.
  2. (EEC) in ALTN*.
  3. Snow, Slush, Ice or Standing water
  4. L/G extended*.
  5. Potential W/S.
  6. Bleeds OFF T/O*.
  7. Prohibited by the Airfield brief*.
  8. De/anti-iced (+min 24k)**.
  9. XWC>10 knots* (if no ATRT - next highest FULL).
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25
Q

What is the ATC INT L/O procedure?

A
  1. ALT HLD
  2. MCP ALT “SET” - “FLXXX, CX”
  3. “LVL CHG”
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26
Q

What’s the correct AFDS eng. sequence?

A
  1. Call for Roll/Pitch modes on MCP
  2. Follow F/D
  3. Roll
  4. Pitch
  5. eng. A/P. Verify on FMA “CMD B”
  6. eng A/T. Verify on FMA “A/T engaged”
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27
Q

Fuel Crossfeed procedure?

A

If IMBAL alert is displayed, PF instructs, PM does

  1. Determine no Fuel leak
  2. (CTR Tank OFF)
  3. X-Feed ON
  4. Low side pumps off
  5. KG Diff / FF per side =>iPad timer
  6. at time , reverse procedure. if OEI, leave X-Feed ON
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28
Q

How do you intercept G/S from Above?

A
  1. Establish on LOC
  2. Set on MCP AD elev. + 1000’ + LVL CHG + Thr IDLE
  3. Set F5, Bug F5 + 10 speed (max), can go to F10
  4. If above G/S by 8nm - SPD BRK
  5. Arm APP when 1• above G/S. Need to capture G/S by 5nm (all conditions)
  6. At G/S capture, stow SPD BRK (or ARM), bug F10 spd and set MAA
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29
Q

Take-off, AEO

A
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30
Q

Take-off, engine fail @V1

A
  1. GND - Rudder only to maint C/L
  2. LIFTOFF/AIR - Rudder + Aileron - Maint HDG + Center Aileron. Slower rotation. Keep ND in scan for C/L tracking. Put TRK line on Dashed white line (C/L). Ask PM to match your Wind Corr HDG.
  3. Follow FDs
  4. 400’ - HDG Sel + state Malf + Memory As
  5. MFRA - Bug Up, Retr Flaps. Stay level to accelerate (IVSI + ALT). Nose DN as SPD Up + Less rudder + Trim (small bank towards LIVE eng. + bank towards LIVE acceptable)
  6. FUNL - LVL CHG, MCT, AP B, clb to MSA at -UP. Trim 3-5 units towards operating Engine. Ask for a hold at EOSID fix and LNAV
  7. QRH
  8. ATOCX
  9. PIOSEE-NITS-PA-OEILCx
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31
Q

GLS approach, AEO, VIZ>5K

A

GLS/ ILS - Fail passive?

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32
Q

GLS OEI

A
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33
Q

ILS approach AEO

A
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34
Q

ILS approach OEI

A
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35
Q

Instrument approach using VNAV AEO

A
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36
Q

Instrument approach using V/S AEO

A
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37
Q

Instrument approach using VNAV OEI

A
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38
Q

Instrument approach using V/S OEI

A
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39
Q

Circling approach

A
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40
Q

Circling approach OEI

A
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41
Q

Visual traffic pattern AEO

A
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42
Q

Visual traffic pattern OEI

A
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43
Q

Circuit training

A
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44
Q

Describe the PIOSEE process

A
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45
Q

Describe the CTL DUB Profile

A
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46
Q

Describe the CTL Generic Profile

A
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47
Q

Describe the CTL STN Profile

A
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48
Q

Describe the OEI ILS APP Profile

A
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49
Q

Describe the ILS CAT I APP Profile AEO

A
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50
Q

Describe the Normal Landing profile

A
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51
Q

Describe the NPA VNAV APP profile

A
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52
Q

Describe the NPA V/S APP Profile

A
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53
Q

Describe the Raw Data ILS Profile

A
  1. Platform altitude - F5/5*/55%
  2. Use trend vector for C/L intercept on LOC
  3. G/S alive - G/D, F15. LCx to Flaps
  4. G/S 1/2 dot - F30/F40, complete LCx
  5. G/S capture - set MAA, 2.5*, 57% (RoD = 5*G/S)

Raw data ILS improves Hand<>Eye coordination

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54
Q

Describe the normal Takeoff Profile

A
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55
Q

Describe the Descent Profile

A
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56
Q

Describe the ILS CAT I APP Profile OEI

A
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57
Q

Describe the DUB NADP Profile

A
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58
Q

Describe the EFATO Profile

A
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59
Q

Describe the NADP 1 Profile

A
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60
Q

Describe the NADP 2 Profile

A
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61
Q

Describe the G/A 2 Engines Profile

A

Set thrust FWD (good airmanship)

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62
Q

Describe the Climb and LEVEL OFF profile

A
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63
Q

Engine Inoperative Cruise/Driftdown profile. Describe it

A
  1. ENG fail > Just “look” at the Rudder + Trim
  2. A/T OFF, set MCT (fm ENG OUT)
  3. Recall items (if required)
  4. Maint CRZ FL until slowing down (minutes). Start QRH
  5. Set ALT and SPD in MCP (fm ENG OUT)
  6. LVL CHG. Sel QNH on SBY
  7. ATC (Pan pan / Mayday) + HDG SEL (if req.)
  8. QRH (relight)
  9. Accelerate to OEI LRC speed on rem eng once level
  10. PIOSEE-NITS-PA
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64
Q

Approach to Stall or Stall Recovery maneuver

A

Pitch-Roll-Thrust

  1. Hold CC
  2. Disco All
  3. ND until buffet stops
  4. Roll (ailerons only) ShDir to W/L (when approaching horizon)
  5. Thrust and SpBrk (check down, tactile)
  6. Don’t change config
  7. Check IAS, thrust, pitch att. - Rebuild - Include PLIs in scan to avoid secondary stall!
  8. Return to normal flight - add thrust when above yellow speed bar.
  • Maintain lateral control with aileron only
  • Don’t use F/D
  • Higher alt-higher thrust settings. Need to bring power quicker as slower to accelerate
  • If high thrust - reduce to reduce AoA

Do all recoveries from approach to stall as if an actual stall has occurred.

Immediately do below at the first indication of stall (buffet or stick shaker).

Note: Do not use F/D guidance

Pilot Flying

Pilot Monitoring

Initiate recovery:

  • Hold the CC firmly.
  • A/P + A/T OFF
  • Smoothly ND elevator until buffet or stick shaker stops. (Roll 45-60*; Rudder)
    (ND STAB may be needed)
  • PM Monitor H and V.
  • PM Verify actions and call out omissions.
  • PM Call out any trend toward terrain contact.

Continue recovery:

  • Roll in SD to W/L if needed.**
  • Advance thrust as needed.
  • S/BRK Stow.
  • Do not change config, except during liftoff, if FU => F1. Do not follow F/D
  • PM As above + Set the FLAP

Complete the recovery:

  • Check V and adjust thrust
  • Establish Pitch ATT.
  • Return to the desired flight path (CMD HDG, ALT, SPD).
  • Re-engage A/T and A/P.
  • PM As above

WARNING: *If the control column does not provide the needed response, stabilizer trim may be needed. Excessive use of pitch trim can aggravate the condition, or can result in loss of control or in high structural loads.

WARNING: ** Excessive use of pitch trim or rudder can aggravate the condition, or can result in loss of control or in high structural loads.

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65
Q

RTO, how do you do

A

As briefed in EMERG brief, additionally:

  • CPT - PA to CC when stopped either:
    • “Cabin Crew Standby” - if not immediately life-threatening, but EVAC may become necessary
      • 2*“THIS IS AN EMERGENCY, EVACUATE THE AIRCRAFT USING ALL AVAILABLE EXITS.”
    • “NO 1 TO THE FLIGHT DECK” - no EVAC - NITS
  • If FIRE - during Memory actions - for F/O - rotate the fire switch to the stop and hold for 1 second, then immediately rotate to discharge the remaining bottle. DO NOT wait 30 seconds on the ground.
  • Look at the door panel before leaving the cockpit - if doors are not opening repeat evacuation command
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66
Q

How would you react to the GPWS Cautions below:

  • SINK RATE
  • TERRAIN
  • DON’T SINK
  • TOO LOW FLAPS/GEAR
  • TOO LOW TERRAIN
  • GLIDESLOPE
  • BANK ANGLE
  • CAUTION OBSTACLE/TERRAIN
  • CAUTION TERRAIN
  • AIRSPEED LOW
A

Correct the flight path or the airplane configuration.

G/S alert can be inhibited for LOC approach/CTL from an ILS/ conditions - deliberate APP below G/S (day VMC only)/ Unreliable G/S signal (day VMC)

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67
Q

How would you react and what manouever would you accomplish for a GPWS

  • “PULL UP”, “OBSTACLE OBSTACLE PULL UP”
  • OR Other situations resulting in unacceptable flight toward terrain.
A

Do not use F/D

Pilot Flying

Pilot Monitoring

  • A/P + A/T OFF
  • Aggressively MAX THR
  • {Roll W/L, +20° NU}
  • S/BRK stow.
  • If terrain remains a threat, continue rotation up to PLI/ shaker/initial buffet.
  • Assure maximum* thrust.
  • Verify all needed actions have been completed and call out any omissions.
  • Do not change gear or flap configuration until terrain separation is assured.
  • Monitor RADALT for sustained or increasing terrain separation.
  • When clear of terrain, slowly decrease pitch attitude and accelerate.
  • Monitor V/S and H (radio for terrain and baro for MSA)
  • Call out any trend toward terrain contact.
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68
Q

How would you manoeuver for a TCAS TA?

A

Look for traffic using traffic display as a guide. Call out any conflicting traffic

If traffic is sighted, maneuver if needed.

Note: Maneuvers based solely on a TA can result in reduced separation and are not recommended.

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69
Q

How would you manoeuver for a TCAS RA?

A

Normal Config

  • Disco All + Adjust

Landing Config

  1. Disco All
  2. Max Thrust
  3. ASk for F15
  4. Gear Up on (+) RoC

WARNING: Do not follow a DESCEND (fly down) RA issued below 1000 feet AGL.

  • For RA, except a climb in landing configuration
    • If maneuvering is needed, A/T + A/P off , follow the planned lateral flight path unless visual contact with the conflicting traffic requires other action.
  • For Climb RA in landing configuration

​Pilot Flying

  • A/P + A/T OFF
  • Thrust levers - maximum + FLAPS 15.
  • @ + RoC - Call Gear UP
  • Smoothly follow RA unless visual contact requires other action.

Pilot Monitoring

  • Verify maximum thrust set. Position flap lever to 15 detent.
  • Verify a (+) + “GEAR UP.”
  • Verify “POSITIVE RATE.”
  • Set the gear lever to UP.

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

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70
Q

Nose High UA recovery

A

Pitch - Thrust - Roll

  1. Disco ALL - XCX SBY ADI
  2. Unload (elev ND/trim/Roll 45-60 lift vector) + Roll to W/L (maint. +G)
  3. Reduce thrust
  4. Limit AoB to 70*
  5. Increase Thrust when above amber speed bar
  6. Approaching horizon - coordinated roll to W/L and slightly nose low attitude
  7. Adjust thrust and pitch
  • Use minimal pitch trim during initial recovery.
  • Careful use of rudder to aid roll only if roll control is ineffective and the airplane is not stalled.
  • These actions assume that the airplane is not stalled. Stalled condition if
    • Stick shaker
    • Buffet that can be heavy at times
    • Lack of pitch authority
    • Lack of roll control
    • Inability to stop a descent.
  • If stalled, first recover from the stall - ND elevator until recovery is complete and stick shaker stops.

Pilot Flying

Pilot Monitoring

Recognize and confirm the developing situation

A/P + A/T OFF Recover:

  • ND Elevator as much as needed to obtain a ND pitch rate
  • Apply appropriate nose down stabilizer trim*
  • Reduce thrust
  • Roll (adjust bank angle) to obtain a nose down pitch rate*

Complete the recovery:

  • Approaching the horizon, roll W/L
  • Check V and adjust thrust
  • Establish pitch ATT.
  • Call out ATT, V and H throughout the recovery.
  • Verify all actions have done and call out any continued deviation.

WARNING: * Excessive use of pitch trim or rudder can aggravate an upset, result in loss of control, or result in high structural loads.

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71
Q

Nose Low UA recovery

A

Roll - Pitch - Thrust (drag)

  1. Disco ALL- XCX SBY ADI
  2. Recover from the stall, if needed
  3. Reduce Thrust+SpBrk (if needed)
  4. Roll to W/L (reduce Thr if high AoB)
  5. AoB
    1. >90* neutral/fwd yoke pressure + Top Rudder (pitch-roll-thrust)
    2. <60* - Back pressure
  6. Adjust Thrust and Drag as needed
  7. INVERTED - Unload + Roll, then PULL
  • Need to be prompt and gentle (high energy, overstressing airframe). Don’t be agressive!
  • Use minimal pitch trim during initial recovery.
  • Careful use of rudder to aid roll only if roll control is ineffective and the airplane is not stalled.
  • These actions assume that the airplane is not stalled. Stalled condition if
    • Stick shaker
    • Buffet that can be heavy at times
    • Lack of pitch authority
    • Lack of roll control
    • Inability to stop a descent.
  • If stalled, first recover from the stall - ND elevator until recovery is complete and stick shaker stops.

Pilot Flying

Pilot Monitoring

Recognize and confirm the developing situation

A/P + A/T OFF Recover:

  • Recover from stall, if needed
  • Roll in the shortest to W/L. If AoB> 90*, unload and roll.*

Complete the recovery:

  • Apply NU elevator
  • Apply NU trim, if needed*
  • Adjust thrust and drag, if needed.
  • Call out ATT, V and H throughout the recovery.
  • Verify actions have been done and call out any continued deviation.

WARNING: * Excessive use of pitch trim or rudder can aggravate an upset, result in loss of control or result in high structural loads.

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72
Q

How would you manoeuver for a Windshear Caution “MONITOR RADAR DISPLAY” alert?

A

Maneuver as needed to avoid the windshear.

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73
Q

How would you manoeuver for a Windshear Warning

“WINDSHEAR AHEAD, WINDSHEAR AHEAD”?

A
  1. DISCO AP
  2. TOGA + Max Thrust + chk S/Brk Retracted
  3. THR FULL FWD+DISCO AT
  4. Roll+Pitch to 15*
  5. (Follow F/D)
  6. Do NOT change configuration
  7. Rebuild - set thrust to 90%, Config?/ Bug Up?/ Reset Brain

PM

Verify Thrust, Actions, Call out Altitude (RA) / V/S, Terrain, Speed changes

Windshear during takeoff roll:

  • before V1, reject takeoff
    • < 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, perform W/S Escape.
    • Near the normal rotation speed and airspeed suddenly decreases, there may not be sufficient runway left to accelerate back to normal takeoff speed. If there is insufficient runway left to stop, initiate a normal rotation at least 600 meters before the end of the runway, even if airspeed is low. Higher than normal attitudes may be needed to lift off in the remaining runway. Ensure maximum thrust is set.
  • after V1, perform W/S Escape

Predictive windshear warning during approach
(“GO–AROUND, WINDSHEAR AHEAD” aural) - W/S Escape / normal G/A

Windshear encountered in flight - W/S Escape

​Note: The following are indications the airplane is in windshear:

  • “WINDSHEAR, WINDSHEAR, WINDSHEAR”
  • unacceptable flight path deviations.
    • Note: Unacceptable flight path deviations below 1000 feet AGL, in excess
      • 15 KIAS
      • 500 fpm V/S
      • 5° pitch ATT
      • 1 dot displacement from the G/S
      • unusual thrust lever position for a significant period of time.

Pilot Flying

Pilot Monitoring

MANUAL FLIGHT

  • A/P OFF.
  • TO/GA switch.
  • Aggressively apply maximum thrust*
  • A/T OFF
  • {Roll W/L, Rotate 15° NU}.
  • S/BRK STOW.
  • Follow F/D TO/GA guidance (if available) **
  • Verify maximum* thrust.
  • Verify all needed actions have been completed and call out any omissions.

AUTOMATIC FLIGHT

  • Push either TO/GA switch***
  • Verify TO/GA FMAs.
  • Verify G/A thrust.
  • S/BRK STOW.
  • Monitor system performance****
  • Verify GA* thrust.
  • Verify all needed actions have been completed and call out any omissions.

MANUAL OR AUTOMATIC FLIGHT

  • Do not change flap or gear configuration until W/S is no longer a factor.
  • Monitor V/S and H.
  • Do not attempt to regain lost V until W/S is no longer a factor.
  • Monitor vertical speed and altitude.
  • Call out any trend toward terrain contact, descending flight path, or significant airspeed changes.

Note: **Do not exceed the Pitch Limit Indication.

Note: *** If TO/GA is not available, disengage autopilot and autothrottle and fly manually.

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74
Q

Circling approach

A
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75
Q

Aborted Engine Start, what do you do and what are the conditions to abort?

A
  1. Engine start lever (affected engine) . . . . CUTOFF

Captain is PF, so he calls for Memory Items, his area of responsibility?

Conditions to abort:

  1. No N1 rotation before the engine start lever is raised to IDLE detent.
  2. No oil pressure indication by the time the engine is stabilized at idle.
  3. No increase in EGT within 15 seconds of raising the engine start lever to IDLE detent.
  4. No increase in, or a very slow increase in N1 or N2 after EGT indication.
  5. EGT rapidly approaching or exceeding the start limit.
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76
Q

Airspeed Unreliable

A

10.1

Condition: Airspeed or Mach indications are suspected

to be unreliable. (Items which might indicate unreliable airspeed are listed in the Additional Information section.)

  1. Autopilot (if engaged) . . . . . . . . . . . . .Disengage
  2. Autothrottle (if engaged). . . . . . . . . . .Disengage
  3. F/D switches (both) . . . . . . . . . . . . . . . . . . OFF
  4. Set the following gear up pitch attitude and thrust:
  • Flaps extended . . . . . . . . . . 10° and 80% N1
  • Flaps up . . . . . . . . . . . . . . . . 4° and 75% N1

###

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77
Q

APU FIRE

A

8.1

Condition: Fire is detected in the APU.

1 APU fire switch. . . Confirm. . . .Pull, rotate to the

stop, and hold for 1 second

2 APU switch. . . . . . . . . . . . . . . . . . . . . . . . OFF

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78
Q

CABIN ALTITUDE WARNING ( )

or

Rapid Depressurization ( )

A

2.1

Condition: One or more of these occur:

  • A cabin altitude exceedance
  • In flight, the intermittent cabin altitude/configuration warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates.

  1. Don oxygen masks and set regulators to 100%. :
  2. ### Establish crew communications.
  3. Pressurization mode selector . . . . . . . . . . . . MAN
  4. ### Outflow VALVE switch . . . . . . . . . . Hold in CLOSE until the outflow VALVE indication shows fully closed :

If cabin altitude is uncontrollable: :

  1. ### Passenger signs. . . . . . . . . . . . . . . . . . . . ON
  2. ### PASS OXYGEN switch . . . . . . . . . . . . . . . . ON

►►Go to the Emergency Descent cx ( )

■ ■ ■ ■

:

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79
Q

EMERG Descent

A

0.1

Condition: One or more of these occur:

  • Cabin altitude cannot be controlled
  • A rapid descent is needed.

1 The pilot flying will advise the cabin crew, on the PA : system, of impending rapid descent or confirm that : the Emergency Descent PA has been made by PRAM. The pilot monitoring will advise ATC and obtain the area altimeter setting

2 Passenger signs. . . . . . . . . . . . . . . . . . . . . . ON

  1. ## Without delay, descend to the lowest safe altitude or 10,000 feet, whichever is higher.
  2. ENGINE START switches (both) . . . . . . . . . CONT
  3. Thrust levers (both) . . . . . . . . . Reduce thrust to

minimum or as needed for anti-ice

  1. Speedbrake. . . . . . . . . . . . . . . . FLIGHT DETENT

If structural integrity is in doubt, limit speed as much as possible and avoid high maneuvering loads.

  1. Set target speed to Mmo/Vmo.
    - - - - - - - - - - - - - - - - - - - - - - -
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80
Q

ENGINE FIRE ( )

or

Engine Severe Damage or Separation ( )

A

8.2

Condition: One or more of these occur:

  • Engine fire warning
  • Airframe vibrations with abnormal engine indications
  • Engine separation.
  1. Autothrottle (if engaged) . . . . . . . . . . .Disengage
  2. Thrust lever

(affected engine) . . . . . . Confirm. . . . . . . Close

  1. Engine start lever

(affected engine) . . . . . . Confirm. . . . . CUTOFF

  1. Engine fire switch

(affected engine) . . . . . . Confirm. . . . . . . . Pull

To manually unlock the engine fire switch, press the override and pull.

  1. ## If the engine fire switch or ENG OVERHEAT light is illuminated:
    • Engine fire switch. . . . . Rotate to the stop and

hold for 1 second

If after 30 seconds the engine fire switch or ENG OVERHEAT light stays illuminated:

  • Engine fire switch. . . . . . . .Rotate to the

other stop and hold for 1 second

- - - - - - - - - - - - - - - - - - - - - - -

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81
Q

Engine Limit or Surge or Stall

A

7.2

Condition: One or more of these occur:

  • Engine indications are abnormal
  • Engine indications are rapidly approaching or exceeding limits
  • Abnormal engine noises are heard, possibly with airframe vibration
  • There is no response to thrust lever movement or the response is abnormal
  • Flames in the engine inlet or exhaust are reported.
  1. Autothrottle (if engaged) . . . . . . . . . . .Disengage
  2. Thrust lever (affected engine) . . . . Confirm. . . . . Retard until engine indications stay within limits or the thrust lever is closed
    - - - - - - - - - - - - - - - - - - - - - - -
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82
Q

ENGINE OVERHEAT

ENG 1 OVERHEAT / ENG 2 OVERHEAT

A

8.6

Condition: An overheat is detected in the engine.

  1. Autothrottle (if engaged) . . . . . . . . . . .Disengage
  2. Thrust lever (affected engine) . . . . . . Confirm. . . . . . . Close
  3. If the ENG OVERHEAT light stays illuminated:

►►Go to the ENGINE FIRE ( ) or Engine Severe Damage or Separation checklist on page 8.2

■ ■ ■ ■

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83
Q

Engine FIRE or Severe damage OR separation

A

8.2

Condition: One or more of these occur:

  • Engine fire warning
  • Airframe vibrations with abnormal engine indications
  • Engine separation.
  1. Autothrottle (if engaged) . . . . . . . . . . .Disengage
  2. Thrust lever

(affected engine) . . . . . . Confirm. . . . . . . Close

  1. Engine start lever

(affected engine) . . . . . . Confirm. . . . . CUTOFF

  1. Engine fire switch

(affected engine) . . . . . . Confirm. . . . . . . . Pull

To manually unlock the engine fire switch, press the override and pull.

  1. ## If the engine fire switch or ENG OVERHEAT light is illuminated:
    • Engine fire switch. . . . . Rotate to the stop and

hold for 1 second

If after 30 seconds the engine fire switch or ENG OVERHEAT light stays illuminated:

  • Engine fire switch. . . . . . . .Rotate to the

other stop and hold for 1 second

- - - - - - - - - - - - - - - - - - - - - - -

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84
Q

Landing config

A

Assure correct airplane landing configuration

■ ■ ■ ■

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85
Q

Loss Of Thrust On Both Engines

A

7.6

Condition: Both of these occur:

  • Both engines have a loss of thrust
  • Both ENG FAIL alerts show.

Objective: To restart at least one engine.

  1. ENGINE START switches (both) . . . . . . . . . . FLT
  2. Engine start levers (both) . . . . . . . . . . . CUTOFF
  3. ## When EGT decreases:

Engine start levers (both) . . . . . . IDLE detent

  1. ## If EGT reaches a redline or there is no increase in EGT within 30 seconds:

Engine start lever

(affected engine) . . . . Confirm. . . . . CUTOFF,

then IDLE detent

If EGT again reaches a redline or there is no increase in EGT within 30 seconds, repeat as needed.

86
Q

Rapid depressurisation

A

2.1

Condition: One or more of these occur:

  • A cabin altitude exceedance
  • In flight, the intermittent cabin altitude/configuration warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates.

  1. Don oxygen masks and set regulators to 100%. :
  2. ### Establish crew communications.
  3. Pressurization mode selector . . . . . . . . . . . . MAN
  4. ### Outflow VALVE switch . . . . . . . . . . Hold in CLOSE until the outflow VALVE indication shows fully closed :

If cabin altitude is uncontrollable: :

  1. ### Passenger signs. . . . . . . . . . . . . . . . . . . . ON
  2. ### PASS OXYGEN switch . . . . . . . . . . . . . . . . ON

►►Go to the Emergency Descent cx ( )

■ ■ ■ ■

####

87
Q

Runaway Stabilizer ( )

A

9.1

Condition: Uncommanded stabilizer trim movement occurs continuously or in a manner not appropriate for flight conditions.

  1. Control column. . . . . . . . . . . . . . . . . Hold firmly
  2. Autopilot (if engaged) . . . . . . . . . . . . .Disengage
  3. Autothrottle (if engaged). . . . . . . . . . .Disengage
  4. Control column and

thrust levers . . . . . . . . . . . Control airplane pitch

attitude and airspeed

  1. Main Electric

Stabilizer trim. . . . . . . . . . . . . . .Reduce control

column forces

  1. ## If the runaway stops after the autopilot is disengaged:

Do not re-engage the autopilot or autothrottle.

■ ■ ■ ■

  1. ## If the runaway continues after the autopilot is disengaged:

STAB TRIM cutout

switches (both) . . . . . . . . . . . . . . . . CUTOUT

If the runaway continues:

Stabilizer trim wheel. . . . . . . . . . Grasp and hold

88
Q

Take-off configuration

A

Assure correct airplane takeoff configuration.
- - - - - - - - - - - - - - - - - - - - - - -
■ ■ ■ ■

89
Q

WARNING HORN (INTERMITTENT)

or

WARNING LIGHT - CABIN ALTITUDE OR TAKEOFF CONFIGURATION

A

15.2

Left Forward Panel Right Forward Panel

TAKEOFF CONFIG / CABIN ALTITUDE / CABIN ALTITUDE / TAKEOFF CONFIG

Condition: One of these occurs:

  • In flight, at an airplane flight altitude above 10,000 feet MSL, the intermittent warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates
  • On the ground, the intermittent warning horn sounds or a TAKEOFF CONFIG light (if installed and operative) illuminates when advancing the thrust levers to takeoff thrust.

  1. ## If the intermittent warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates in flight at an airplane flight altitude above 10,000 feet MSL:

Don the oxygen masks and set the regulators to 100%.

Establish crew communications.

►►Go to the CABIN ALTITUDE WARNING ( ) or Rapid Depressurization ( ) checklist on page 2.1

■ ■ ■ ■

  1. ## If the intermittent warning horn sounds or a TAKEOFF CONFIG light (if installed and operative) illuminates on the ground when advancing the thrust levers to takeoff thrust:

Assure correct airplane takeoff configuration.

■ ■ ■ ■

90
Q

NNC

Which chapter is

Miscellaneous?

A

0

91
Q

NNC

Which chapter is

Airplane General, Emergency Eq., Doors, Windows?

A

1

92
Q

NNC

Which chapter is

Air Systems?

A

2

93
Q

NNC

Which chapter is

Anti-ice, Rain?

A

3

94
Q

NNC

Which chapter is

Auto-Flight?

A

4

95
Q

NNC

Which chapter is

Comms?

A

5

96
Q

NNC

Which chapter is

Electrics?

A

6

97
Q

NNC

Which chapter is

APU, Engines?

A

7

98
Q

NNC

Which chapter is

Fire Protection?

A

8

99
Q

NNC

Which chapter is

Flight Controls?

A

9

100
Q

NNC

Which chapter is

Flight Instruments, Displays?

A

10

101
Q

NNC

Which chapter is

Flight Management, Navigation?

A

11

102
Q

NNC

Which chapter is

Fuel?

A

12

103
Q

NNC

Which chapter is

Landing Gear?

A

14

104
Q

NNC

Which chapter is

Warning Systems?

A

15

105
Q

What checklist would you ask for as PF when you see ANTI-SKID INOP light on the Main panel? What are the implications?

A

“Antiskid INOP” QRH CX, 14.1, “My radios”

  1. NW on GND
  2. S/BRK Manually raise
  3. Man BRK as you slow down, increase effort, do not pump brakes
106
Q

What checklist would you ask if the L/G lever does not come up? When would you do it? Would you clean up?

A

“L/G lever will not move up” QRH CX 14.14, “My radios”

Do it after cleaned up, enroute, and > MSA.

After, do VNAV, Set STD, ATOCx

107
Q

What CX would you ask for if you have a HYD pump low pressure?

A

“HYD pump low pressure” QRH CX 13.1, “My Radios”

108
Q

What CX would you ask for if you have HYD SYS A failure? What are the implications?

A

“Loss of System A” QRH CX 13.3, “My Radios”

L/G free fall, Slow roll, REV slow on Eng 1

109
Q

What CX would you ask for if you have HYD SYS B failure? What are the implications?

A

“Loss of System B” QRH CX 13.6, “My Radios”

ALTN flap Extension, delay setting bug until flaps are at position, REV slow, Roll slow

110
Q

What CX would you ask for if you have F/CTL low Pressure indication?

A

“FLT CTL low pressure” QRH CX, 9.8, “My Radios”

111
Q

What do you do if you see “DSPLY SOURCE 1/2” in bottom left corner of PFD? What does it mean? Which CX would you call for?

A

DEU Failure 1/2, “Display Source” QRH CX 10.16+”My radios”

+

“EEC Alternate mode” QRH CX 7.14

112
Q

What do you do if you see “Start Valve Open” in top right corner of Upper DU?

A

“Start Valve Open” QRH CX 7.38, “My Radios”

113
Q

What do you do if you see “LOW OIL PRESSURE” in top right corenr of UPPER DU?

A

“ENGINE LOW OIL PRESSURE” QRH CX 7.28, “My Radios”

114
Q

What CX do you ask for if you see the “SPEEDBRAKE DO NOT ARM” Light?

A

“Speedbrake do not arm” QRH CX 9.22, “My Radios”

115
Q

What are the specifics of a SRA approach and how do you fly it?

A
  • If Radio fail - G/A
  • Fixes - /10 , /exp. DES point
  • Mins = Baro => Revised MDA
  • Use HDG sel + V/S
  • Leave platform alt. in LDG config
  • PM - alt vs dist callouts + “Approaching DES” 2nm to go
  • Gear Down, F15 1nm before DES
  • LDG Flap 0.5nm to DES
116
Q

What are the specifics of a Timed NPA approach and how do you fly it?

A
  • Can only fly it if it exists in FMC DB
  • Use LNAV and VNAV (VNAV only if MAPt is at or before RWY THR point AND/OR G/P angle is in LEGS)
  • Config @ 5nm to go
  • IAF @ F1, max 220
  • Inbound @ F5, Max 180
117
Q

What are the specifics of a Visual approach and how do you fly it?

A
  • Create RX point in FMC w 3* G/P. Make it a hard altitude
  • Use LNAV and VNAV
  • When cleared visual APP - DIR to RX point
  • Do not turn final unless +/- 400’ of profile
  • Land gate Land alt + 500’ (set as Baro min). GPWS “500” acts as “minimums” call
118
Q

Describe the complete CLB,CRZ and DES profile and actions and trigger points

A
119
Q

Rapid depressurisation

A

2.1

Condition: One or more of these occur:

  • A cabin altitude exceedance
  • In flight, the intermittent cabin altitude/configuration warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates.

  1. Don oxygen masks and set regulators to 100%. :
  2. ### Establish crew communications.
  3. Pressurization mode selector . . . . . . . . . . . . MAN
  4. ### Outflow VALVE switch . . . . . . . . . . Hold in CLOSE until the outflow VALVE indication shows fully closed :

If cabin altitude is uncontrollable: :

  1. ### Passenger signs. . . . . . . . . . . . . . . . . . . . ON
  2. ### PASS OXYGEN switch . . . . . . . . . . . . . . . . ON

►►Go to the Emergency Descent cx ( )

■ ■ ■ ■

:
Captain (PF)Co-Pilot (PM)

Mask – On + communications - Establish

Assumes PF role

Emergency descent - Initiate

Mask – On + communications - Establish

Assumes PNF role

MAN + CLOSE

If cabin altitude is uncontrollable:

signs + oxygen - ON

Emergency descent - Initiate

120
Q

Pilot incapacitation, what do you do?

A
  1. Ask Qs (2Q and out)
  2. Take CTL, check position of switches
  3. “ATTEND” + “N1 to the F/D”
  4. ATC - Mayday
  5. F/AID
  6. Re-organise for Landing (PIOSEE-NITS-PA) - NRST suitable
  7. ATC - advise stopping on RWY and medical assistance
  8. Autoland
  9. ATC - RV req.
  10. Start APU
  11. Land - Stop, APU on busses, shutdown engines, medical onboard
121
Q

Crosswind landing, what’s the procedure?

A

De-Crab during flare

  1. Downwind rudder during flare (20’) to eliminate crab and align with C/L
  2. Upwind aileron for W/L
  3. Crossed controls maintained during landing
122
Q

What are your Speed and altitude gates during approach and landing?

A
  1. @35nm /FL100 / 250kts
  2. @20nm/ 5000‘aal / 250 decelerating (800fpm or less to be slowing down)
  3. @15nm / 4000‘aal / UP speed or F1 speed
  4. @10nm 3-2-1 (10nm rule) / 3000’aal / 200kts / F1
  5. 9nm / 190 kts
  6. 8nm / 180 kts
  7. G/S capture / F5 speed
  8. 7nm / 170 kts
  9. 6nm / 160 kts
  10. 5nm /150 kts
  11. 1000/500’ gates - on profile w LCX complete to Lights
123
Q

What do you do if during descent you’re above or below profile?

A

Below Profile

  • Use V/S until you INTCPT VNAV profile, then VNAV

Above Profile

  • >FL100
  • *LVL CHG/VNAV SPD INTV** - Increase speed (max 330/.81) + update FMC speed target (for big changes) OR S/BRK out (small changes)
  • Use LVL CHG, not VNAV. ​Limited by 250/FL100 so 250/S/BRK OR 220/F5/S/BRK (assess) THEN 180/F10/S/BRK

(Don’t ARM APP when high on G/S)

124
Q

What’s the preferred mode for small altitude changes

A

VNAV

125
Q

When visual and with AFDS on, what’s the correct sequence to transition to Visual landing?

A
  1. A/T off. Stabilise N1 at correct APP setting
  2. Push shoulders back. Look at TDZ point. Memorise
  3. Disco A/P. From now on you only make small changes!
126
Q

ENG fail on final. What do you do?

A
  1. Need to be quick w Rudder (+Yoke)
  2. Thr levers - both FWD (57% to 82%). Rudder towards live engine. Keep C/L with feet, W/L with aileron
  3. Keep V>Vref if keep land flap. If retr to F15 - Bug Vref +20 (white bug)
  4. Leave F15 until MFRA if G/A
  5. Pitch 2.5*-3* for G/S. Fly top bug + 5kts
  6. EGPWS flap override
  7. Field length OK?
  8. Flare for F15?
  9. Delay Recall items until on GND and full stop. Is it a fire ? EVAC? Taxi on our own? Fire brigade? Ask ATC to visually confirm
  10. NITS-PA
127
Q

How do you do the rotation manoeuvre?

A
  1. @ “Rotate” - look at end of the runway. Count to 4s when lifting the nose - MORE
  2. When the nose starts rising, reduce BP - LESS
  3. @4s/8-10* “Dead band” Increase BP - MORE
  4. After the Dead Band - decrease BP - LESS
  5. Pause at 15* and follow F/Ds

whole manoeuvre takes 6s @ 2.5*/s rotation rate

If Xwind

  1. Keep C/L with rudder - increase aileron into wind w speed for W/L up to 1.5 units
  2. Once airborne - slowly neutralise rudder + aileron
128
Q

What’s the correct sequence for trimming?

A
  1. Pitch
  2. Thrust
  3. Trim to maintain ATT
  4. Release to assess trim

Change in thrust = Change in Pitch + change in trim

129
Q

What 2 conditions have to be met before you can order to “Set STD”?

A
  1. Cleared above TA (to a FL)
  2. A/C is > 3000’ aal
130
Q

What checklist would you call for if you have

Engine vibrations (only)

?

A

QRH [High Engine Vibration]

+

“My Radios”

131
Q

What checklist would you call for if you have

N1 and N2 and EGT decreasing

?

A

QRH [Engine Failure or Shutdown]

+

“My Radios”

132
Q

What checklist would you call for if you have

No response to thrust lever movement

?

A

QRH [Engine Limit or Surge or Stall]

+

“My Radios”

133
Q

What checklist would you call for if you have

Unusual engine noises

?

A

QRH [Engine Limit or Surge or Stall]

+

“My Radios”

134
Q

What checklist would you call for if you have

N1 or N2 fluctuating up/down

?

A

QRH [Engine Limit or Surge or Stall]

+

“My Radios”

135
Q

What checklist would you call for if you have

N1, N2 or EGT near or exceeding limit

?

A

QRH [Engine Limit or Surge or Stall]

+

“My Radios”

136
Q

What checklist would you call for if you have

N1 or N2 zero RPM

?

A

QRH [ENGINE FIRE or Engine Severe Damage or Separation]

+

“My Radios”

137
Q

What checklist would you call for if you have

FIRE WARNING

?

A

QRH [ENGINE FIRE or Engine Severe Damage or Separation]

+

“My Radios”

138
Q

What checklist would you call for if you have

OVERHEAT

?

A

QRH [ENGINE OVERHEAT]

+

“My Radios”

139
Q

What calls would you make

to the ATC and the Cabin

for a Wheel well fire?

A
  • ATC: PAN call (Mayday?) + Request inspection of RWY + Request towing + Inspection of landing gear by
    tower
    • Cabin: Prepare cabin crew and pax for evacuation upon landing
140
Q

What calls would you make

to the ATC and the Cabin

for a Door lights & Depressurisation?

A
  • ATC: Advise ATC
    • Cabin: Advise cabin crew, Supply oxygen to pax
      needing it, If cabin door: direct
      pax away from door.
141
Q

What calls would you make

to the ATC and the Cabin

for a Emergency descent?

A
  • ATC: Mayday call + Medical assistance in function of cabin report
    • Cabin: Cabin report (No. of wounded pax, No. of pax needing oxygen) + Give diversion &
      remaining flight time
142
Q

What calls would you make

to the ATC and the Cabin

for a Loss of both IDGs?

A
  • ATC: PAN call, Mayday if busses can not be restored + Radar vectors + Possible loss of all communications
    • Cabin: Advise cabin crew + No lights in cabin + Pressurization problems + Diversion
143
Q

What calls would you make

to the ATC and the Cabin

for a Transfer bus off?

A
  • ATC: PAN call + Advise possible brake problems
    • Cabin: Advise cabin crew + Some cabin lights are U/S
144
Q

What calls would you make

to the ATC and the Cabin

for a Electrical fire & Smoke?

A
  • ATC: Mayday call + Radar vectors for immediate landing
    • Cabin: Advise cabin crew + request to locate smoke source if applicable
145
Q

What calls would you make

to the ATC and the Cabin

for a Flaps up Landing?

A
  • ATC: Advise ATC high speed
  • Cabin: Advise cabin crew
146
Q

What calls would you make

to the ATC and the Cabin

for a Asymmetrical trailinq edge flaps?

A
  • ATC: PAN call
  • Cabin: Advise cabin crew
147
Q

What calls would you make

to the ATC and the Cabin

for a Jammed Stabiliser?

A
  • ATC: PAN call, high speed start of approach
  • Cabin: Advise cabin crew (pitch movements)
148
Q

What calls would you make

to the ATC and the Cabin

for a Loss of System A+B (Manual reversion)?

A
  • ATC: Mayday call + Request to keep runway free for LDG
  • Cabin: Prepare cabin crew and pax for evacuation upon landing
149
Q

What calls would you make

to the ATC and the Cabin

for a Loss of System A?

A
  • ATC: Advise ATC, May be committed to land
    due to fuel status (unable to retract the qear)
  • Cabin: Advise cabin crew
150
Q

What calls would you make

to the ATC and the Cabin

for a Loss of System B?

A
  • ATC: Advise ATC, longer final 20 nm (2min to extend Flaps)
  • Cabin: Advise cabin crew
151
Q

What calls would you make

to the ATC and the Cabin

for an lnextinguishable APU FIRE?

A
  • ATC: Mayday call + Confirm fire by ATC
  • Cabin: Prepare cabin crew and pax for evacuation upon landing
152
Q

What calls would you make

to the ATC and the Cabin

for an lnextinguishable ENG FIRE?

A
  • ATC: Mayday call
  • Cabin: Prepare cabin crew and pax for evacuation upon landing
153
Q

What calls would you make

to the ATC and the Cabin

for an Eng failure?

A
  • ATC: PAN call
  • Cabin: Advise cabin crew
154
Q

EGPWS “Obstacle, Obstacle”/ “Pull Up” manouever

A

PF

  1. DISCO all
  2. Aggresively Full FWD Throttles
  3. S/BRK retracted
  4. Rotate to 20* NU first (Roll + Pitch)
  5. If needed - rotate up to PLI/Stick Shaker/Initial Buffet
  6. Include Radalt in Scan
  7. Do NOT change configuration
  8. Rebuild

PM

  1. Assure MAx Thrust
  2. Verify actions are complete
  3. Monitor V/S and ALT (radalt)
  4. Call out trend toward terrain conflict
155
Q

What are the Pitch Datums for a G/A AEO (OEI)

for 60t A/C?

A
  • (154kts) 15-18* (12-13*) / G/A Thrust - 90% (>90%)
156
Q

What are the Pitch Datums for a G/S Intercept AEO (OEI)

for 60t A/C?

A
  • @ G/D F15 (160kts): 2.5* (3*) / 52% (70%)
  • F30 (152kts): 1* / 57% (84%?)
  • F40 (144kts): 0* / 62% (??%)

Pitch for Rate, Thrust for speed

Flaps = Balooning

Thrust - Attitude - Trim

157
Q

What are the Pitch Datums for a Level Flight AEO (OEI)

for 60t A/C?

A
  • >FL100 6-2-8,
  • @ FU (204kts): 5.6* / 58% (70%)
  • @F1 (184kts): 5.6* / 60% (80%)
  • @F5 (164kts): 6* / 60% (80%)
    Platform F5 - 5* / 55%
  • @ G/D F15 (154kts): 6* / 70% (92%)

Flaps = Balooning

Thrust - Attitude - Trim

158
Q

Describe how you land a 737-800?

A

Scan Technique

ATT (1/0)- SPD - ATT (1/0) - VSI - ATT (1/0) - THR (57% F30/ 63% F40)

Below 500’ becomes

OUT - SPD - OUT - THR

  1. DISCO A/T first - stabilise N1
  2. Push back in your seat
  3. DISCO A/P last - only small corrections from now on! When back on profile , return to datums
  • ‘1000’ - 75/25 split. Aiming point should be 35-40% up the bottom of the Windscreen
  • ‘500’ 50/50. Don’t overcorrect for PAPIs close in!
  • >‘200’ 25/75
  • ‘100’ - 100% outside
  • ‘50’ - Look at far end of RWY
  • >‘20’ - Check ATT +2-3* to ~5*NU (visual manoeuver) (-1* for every 5kts above Vref). Flare higher if RoD higher.
  • ‘10’ -Close gradually THR and HOLD (all flare 4-8s)
  • T/D @ around 150fpm
  • On GND after stopping assured - transition to manual braking smoothly

Bounce Recovery

  • Shallow - reestablish OR hold pitch AND add thrust as required to check RoD
  • Big bounce - G/A. MAN G/A THR. Maint Gear + Flap until (+) RoC
159
Q

What is a rejected landing and how do you recover from it?

A

G/A below minima, but before T/D. 30’ lost in manoeuver.

  • G/A as usual. Might have to Manually advance to G/A the THR (TOGA sw inhibited near GND or on GND)
160
Q

What is a balked landing and how do you execute it?

A

Occurs when G/A after T/D but before REV selected

  • DISCO A/P + A/T + advance to G/A thrust + SpBrk Down
  • Maintain Flap config until climbing away unless sufficient RWY rem to select F15
  • Rotate to 15* = maintain Vref or higher
  • Follow G/A procedure
161
Q

Describe the CTL STN RNP 04 profile

A
162
Q

How do you do Steep turns on the 737-800?

A
  1. Use 35-35* AoB
  2. Add PITCH for ALT (larger Nose Up for larger deviations) - 1-2*
  3. Add THR (+5%) for SPD (as you go past 30* or you see spd trend vector)
  4. Rollout 15* before HDG
  5. Decrease THR
  6. Decrease PITCH
163
Q

What’s the Crosswind takeoff technique on the 737-800?

A
  1. Visualise W/V. Tilt yoke slightly towards wind to help visualise (Rudder away fm wind, yoke toward wind)
  2. On GND - maint C/L with Rudder
    (slippery RWY PM - Symmetrical thrust)
  3. Begin T/O roll with Yoke centered - gradually increase displacement into wind only enought to maintain wings level. Use as much aileron as you need (unless perf limited)
  4. At liftoff - crossed controls - Wind will pick up upwind wing - more aileron required. Airborne and established in a crab - slowly neutralise conrols
  5. Use higher thrust setting on gusty/windy days
164
Q

What’s the Crosswind Landing technique on the 737-800?

A

2 used - De-Crab During Flare and T/D in a Crab (wet)

  1. Whenever a crab is maintained during X-Wind APP, offset F/Deck on the upwind side of C/L so that Main gear touches in the center of the RWY
  2. Maintain W/L and track the point in (1)
  3. While flaring (20’) - downwind rudder to align with C/L and aileron for W/L
  4. Both MLGs touch down at the same time
  5. Keep Upwind aileron throughout rollout
165
Q

Take off profile using VNAV 737NG

A
166
Q

Take off profile using VNAV 737 MAX

A
167
Q

GA and MApp (all approaches)

A
168
Q

How do you perform Non-standard G/A

A
  1. Look at your altitude/speed and Flap setting first
  2. Altitude (is MAA set?)
    1. > MAA - no TO/GA
      1. Flaps
    3. >F15 - G/A, F15 and Normal G/A.
      Set thrust FWD
      Note Speed Restrictions, leave flaps if needed
    4. - leave them as they are. Note Speed Restrictions, leave flaps if needed
  3. (Gear Up) on (+) RoC
  4. Do not turn before MAPt
  5. >400’ - select roll mode
  6. Tune radios for MAPP
  7. Bug UP
  • If MAN G/A - ask for F/D first, before calling for Roll Mode

Thrust UP - Gear UP - Roll UP (MAPt) - Bug UP - Clean UP - Radios <>

169
Q

What is the standard Pitch + Thrust for Climbout (no F/Ds) at fixed climb thrust (60t)?

A
  1. Rotate to 15-18* / V2 - V2+20
  2. Bug Up - 8* / Accelerating to -UP
  3. Climbing 12.5* / -UP speed
  4. Accelerate to 250 - 6* / Accelerate to 250
  5. Climbing - 10* // 250/280
170
Q

Engine Failure on Final, what do you do?

A
  1. Quick! Rudder UP + Thrust UP + Trim
  2. Thrust UP - Maintain Above -Vref
  3. Trim
  4. IMC/VMC?
    1. If IMC and < 1000’ agl - G/A F15 (BU @ 1000’)
    2. If VMC - continue.Flaps?
      1. F30/40 - Maint Vref (if G/A - G/A F15, BU @ 1000) More Rudder
      2. F15 - Bug white bug (Vref+20) (if G/A - G/A F1, BU @ 1000’) More Rudder
  5. If time and if essential - memory items
171
Q

How do you calculate your drift?

A

Drift = TAS / SPD nm/min

  • 120 - 2
  • 150 - 2.5
  • 180 - 3
  • 210 - 3.5
  • 240 - 4
172
Q

Change of RoD - how do you calculate change of RoD with change in BAtt?

A

Change of RoD = chgBA*(TAS//Mach)

173
Q

How do you calculate your Roll out angle for turns?

A

Roll out = AoB / 3

174
Q

What AoB will you use to adjust your heading by a small amount?

A

AoB = Chg HDG required

175
Q

What’s the correct sequence for trimming in the 737?

A
  1. Change config (if reqd)
  2. Change Thrust
  3. Change pitch
  4. Recheck
  5. Trim
176
Q

What is the severe turbulence penetration procedure?

A
  1. CWS (no ALT HLD)
  2. N1 => CON (FMC)
  3. A/T OFF => Set Thrust from FMC
  4. 280//76 (lower)
  5. Trim , W/L and Leave
  6. Start switches CONT
177
Q

What speed are diversions flown at? What about other routes?

A

LRC

Other routes are flown at CI (eFL) or Fixed Mach (ATC)

178
Q

How do you do a OEI G/A?

A
  1. Press TO/GA, “G/A, F1”. Set thrust FWD
  2. “Set G/A Thr”
  3. Gear UP (+RoC on ALT, G/A att. set) PM checks TMA,FMA and PFD
  4. @ 400’ Roll mode - “LNAV or HDG sel”
  5. Maintain Vref15+5, VrefICE+10 and AoB 15* if < MFRA
  6. Tune radios for MAPP
  7. @ MFRA (1000’agl) - Bug UP (speed restrictions?)
  8. @ FUNL - LVL CHG, MCT, A/P + clb @ -UP to MSA/MAA
179
Q

What 7 things do you need before the OEI Land Cx?

A
  1. Memory Actions complete
  2. QRH complete
  3. ATOCx
  4. PIOSEE
  5. NITS
  6. PA
  7. Deffered items to OEI Land CX
180
Q

When would you configure if there’s a tailwind on base?

A

Early (late for H/wind)

181
Q

What should “Plan to land at the Nearest Suitable airport” trigger you to do?

A

Start a PIOSEE-NITS-PA-DALTA (if time=fuel available)

182
Q

ENG FIRE on Taxi In - what do you do?

A

CP - Stop + Set P/B + “CC SBY”

F/O - F40 (P/B) + ATC (mayday)

CP - State malfunction

As RTO from then on

183
Q

What are some of the APP + LDG implications of a Loss of HYD B?

A
  • Using ALTN Flaps - takes 2 minutes to extend to F15
  • Need 5 min cooldown period if you stop
  • Need to lower gear with other hand OR PF to lower it himself
  • Hence ask for 10nm final
184
Q

What are the APP + LDG implications of Loss of HYD A?

A
  • L/G freefall - cannot be retracted, hence
  • Lower flaps to F30 first to check for asymmetry (gera warning horn)
  • Then lower L/G.
185
Q

What NNC will you ask for an “IAS disagree” Alert on PFD?

A

“Airspeed Unrealiable” QRH + “My radios”

186
Q

What NNC will you ask for an “AoA disagree” Alert on PFD?

A

“Airspeed Unrealiable” QRH + “My radios”

187
Q

What airmanship considerations must you have for the “Airspeed Unreliable” QRH CX?

A

Don’t just compare all 3 indications. Compate them against known datums of Pitch + Thrust (QRH PI)

188
Q

What are the conditions for an orbit?

A
  1. >3000’ agl
  2. >10nm fm T/D
  3. VMC
  4. <=F10
189
Q

On the GND if there is an abnormal situation, who is PF/PM?

A

CP automatically becomes PF

190
Q

When and who will set the PRIM and SBY ALT to QNH?

What happens if you have to Level-off due ATC?

A

PF, when cleared to an ALT

Revert to STD

191
Q

What AFDS modes will you use for ATC Radar Vectoring ?

A

HDG Sel + LVL CHG / V/S

192
Q

How will you comply with ATC “Descend now instruction” if under VNAV?

A

MCP - lower ALT + ALT INTV

193
Q

What 3 things fo you need to do when cleared for an ILS APP?

A
  1. PROG 4/4
  2. Correct Sensing of LOC (+pointers shown)
  3. Arm APP
194
Q

What 3 things do you, as PF, need to check @ FUNL?

A
  1. Ask yourself “Am I clrd to FL?” when >3000’ agl
    1. Set cleared ALT on MCP (if CLRD FL)
    2. Clear SID ALT Restr
    3. “VNAV”
  2. Set STD
  3. ATOCx
195
Q

What 2 things do you need before the Landing Checklist?

A
  1. FRISC completed
  2. VSD ON (PM side)
196
Q

What is the VHF freq change procedure?

A
  1. PM on radios to ATC
  2. PF puts new freq in VHF 1 SBY - “Set”
197
Q

What would you do if you get a NNC in the climb?

A

Level off 1000-200’ above present altitude to start troubleshooting.

198
Q

What’s the Datum for

AEO

3* ILS at F40?

A

0*

63%

Flaps - Drag

Thrust-Attitude-Trim

199
Q

What’s the Datum for

AEO

3* ILS at F30?

A

1*

57%

Flaps - Drag

Thrust-Attitude-Trim

200
Q

What’s the Datum for

AEO

3* ILS at F15?

A

2.5*

52%

Flaps - Balooning

Thrust-Attitude-Trim

201
Q

What’s the Datum for

AEO

Level Flight at F15?

A

6*

70%

Flaps - Balooning

Thrust-Attitude-Trim

202
Q

What’s the Datum for

AEO

Level Flight at F5?

A

6*

60%

Flaps - Balooning

Thrust-Attitude-Trim

203
Q

What’s the Datum for

AEO

Level Flight at F1?

A

5.5*

60%

Flaps - Balooning

Thrust-Attitude-Trim

204
Q

What’s the Datum for

AEO

Level Flight at FU?

A

5.5*

58%

205
Q

What’s the Datum for

AEO

Level Flight at 250kts?

A

2-3*

58%

206
Q

What’s the datums for

OEI

ILS @ F15?

60t

A

1-2*

70(-73%)%

T 3-5

Flaps - Balooning

Thrust - Attitude - Trim

Catch trends on perf instruments first (IVSI, G/S, LOC) before they become visible on F/D

207
Q

What’s the datums for

OEI

Level flight @ F15?

60t

A

8*

92%

T 5

Flaps - Balooning

Thrust - Attitude - Trim

208
Q

What’s the datums for

OEI

Level flight @ F5?

60t

A

5.5*

78%

T 3-5

Flaps - Balooning

Thrust - Attitude - Trim

209
Q

What’s the datums for

OEI

Level flight @ F1?

60t

A

5.5*

80%

T 3-5

Flaps - Balooning

Thrust - Attitude - Trim

210
Q

What’s the datums for

OEI

Level flight @ FU?

60t

A

5.5*

73% (75-80%)

T 3-5

211
Q

What’s the OEI G/A datums?

A

12-13*

>90% (+Rudder)

212
Q

What’s the AEO G/A datums?

A

15-18*

85%

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