B737 (C&PF) Flows & Briefings.txt

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yann
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289967
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B737 (C&PF) Flows & Briefings.txt
Updated:
2014-11-24 16:20:20
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  1. 1- CDU PREFLIGHT (PF)
    • ATIS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Obtained
    • Initial Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Set
    • • IDENT page
    • • POS INIT page:

    • Navigation Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Set
    • • ROUTE page:
    • • DEPARTURES page:
    • • Select the ROUTE prompt:

    • PERF INIT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Set
    • • PERF INIT page:
  2. 2- COCKPIT SCAN (C)
    • *EFIS control panel . . . . . . . . . . . . . . .Set
    • *Mode control panel . . . . . . . . . .Set (PF)
    • *Oxygen . . . . . . . . . . . . . . . . .Test and Set
    • *Nose wheel steering sw . . .Guard closed
    • *Clock . . . . . . . . . . . . . . . . . . . . . . . . . ..Set (UTC)
    • *Display select panel . . . . . . . . . . . . . .Set
    • *Disengage lights . . . . . . . . . . . . . . . .Test
    • *Stab out of trim Lt. . . . . . ..Verify Extinguished
    • *Flight instruments . . . . . . . . . . . . .Check
    • *Standby instruments . . . . . . . . . .Check
    • *Integrated standby flight display . . .Set
    • *Standby RMI . . . . . . . . . . . . . . . . . . ..Set
    • *Speedbrake lever . . . . . . ..DOWN detent
    • • Verify that the SPEEDBRAKE ARMED light is extinguished.
    • • Verify that the SPEEDBRAKE DO NOT ARM light is extinguished.
    • • Verify that the SPEEDBRAKE EXTENDED light is extinguished.
    • *Reverse thrust levers . . . . . . . . . .Down
    • *Forward thrust levers . . . . . . . . .Closed
    • *Flap lever . . . . . . . . . . . . . . . . . . . . ..Set
    • *Parking brake . . . . . . . . . . . . . . . . . ..Set
    • *Engine start levers . . . . . . . . . .CUTOFF
    • *STABILIZER TRIM cutout sw . .NORMAL
    • *Radio tuning panel . . . . . . . . . . . . . ..Set
    • *VHF communications radios . . . . . ..Set
    • *VHF NAV radios . . . . ..Set for departure
    • *Audio control panel . . . . . . . . . . . . ..Set
    • *Seat . . . . . . . . . . . . . . . . . . . . . . . ..Adjust
    • *Rudder pedals . . . . . . . . . . . . . . . ..Adjust
    • *Seat belt and shoulder harness . .Adjust
  3. 3- INSTRUMENTS CHECK AND FINAL DATA (PF)
    • -INSTRUMENT CHECK
    • -Clearance (Set MCP and XPDR)

    • -X-Check Final Data
    • *PERF INIT page:
    • • Enter ZFW
    • • Verify that the FUEL on the CDU, the OPF, and the fuel qty indicators agree
    • • Verify that fuel is sufficient for the flight
    • • Perform a GROSS WEIGHT check by comparing the CDU and load and trim sheet are w/in 100 kgs.
    • • Enter takeoff CG
    • •EXECUTE

    • *N1 LIMIT page:
    • • Enter an assumed temperature if re-quired. OAT will only be entered if air-craft is not fitted with an aspirated TAT (Empty Data boxes).
    • • If required, select the appropriate DERATE TO. Note: Corresponding Reduced climb will be automatically selected by the FMC.
    • • Confirm correct engine thrust rating on TMD.

    • *TAKEOFF page:
    • • Enter TO flaps
    • • Enter takeoff CG
    • • Verify and set trim value as shown
    • • Enter the TO V speeds
    • • Set V2 on MCP
    • • Verify or enter thrust reduction altitude
  4. 4- TAKEOFF BRIEFING (PF)
    -Reduced or TOGA thrust takeoff from run-way ____, flaps____ .

    -Any malfunction before V1

    • -I will call REJECT or CONTINUE, if reject I will simultaneously:
    • • Close the thrust levers, disengage the auto-throttle.
    • • Deploy the speed brakes then
    • • Set max reverse thrust
    • • If required apply full manual braking.........

    • -At full stop:
    • • Set the parking brake
    • • Stow the speed brakes
    • • PA: “THIS IS THE CAPTAIN, ICI LE COMMANDANT, CREW STANDBY”
    • • Evaluate the situation, then I will call and carry out the appropriate drill

    -----ENGINE MALFUNCTION AFTER V1-----

    • -No actions before 400 ft AGL then:
    • • Engage HDG SEL
    • • Call for the appropriate drill
    • -At MFRA:
    • • Speed bug up
    • • Retract flaps on schedule
    • -At FLAPS UP:
    • • Set LVL change
    • • Set MCT
    • • Call for the appropriate C/L

    • ---SIC----
    • -I will :
    • • Monitor autobrake or call Autobrake disarmed,
    • • Call speed brake up or no speed brake
    • • Call reverse operative or no reverser no.___
    • • Call 60 kts
    • • Advise ATC
    • • Select flaps 40
    • • Depressurize the aircraft
    • • Locate the evacuation C/L
    • -----------------
    • • I will perform the appropriate drill

    ----NAVIGATION and CONSIDERATIONS-----

    • -Brief SID:
    • • Confirm: SID name, charts number, date
    • • Read from CDU all waypoints with constraints.
    • • Cleared initial altitude
    • • Transition altitude
    • • Radio set up
    • • NADP 1 or 2

    • -SPECIAL CONSIDERATIONS:
    • • MEL
    • • Anti-ice
    • • Route Taxi
    • • Radar
    • • Surrounding terrain
    • • EO procedure
    • • Cabin altitude warning briefing
    • • Aircraft differences
    • • Questions?
  5. 5- CABIN ALTITUDE WARNING TAKEOFF BRIEFING (PF)
    • ‘'-Whenever the intermittent warning horn sounds in flight at an airplane altitude above 10,000 feet MSL:
    • • We will immediately don oxygen masks and set regulators to 100%
    • • Established crew communications
    • • Complete the CABIN ALTITUDE WARNING / RAPID DEPRESSURIZATION DRILL
    • -We will both verify on the overhead Cabin Altitude Panel that the cabin altitude is stabilized at or below 10 000 ft before removing oxygen masks.''
  6. 6- FAMPACT (PF)
    • -FUEL (slip, verify: uplift, quantity, distribution and FUEL Panel (PUMPS ON))
    • -ATC (clearance received)
    • -MCP (set as per clearance)
    • -POWER N1 (On N1 Limit page: verify Assumed Temp. and Thrust Rating. Verify TMD.)
    • -AIRSPEEDS (Takeoff Ref page)
    • -CDU Set (Proper pages set)
    • -TRIM (x3) and TAKEOFF BRIEFING
  7. 7- BEFORE START FLOW (C) 1
    Fasten Belts switch . . . . . . . . . . . . . . . .ON


    Call “BEFORE START CHECKLIST TO THE LINE”
  8. 8- BEFORE START BELOW THE LINE FLOW (C) 4
    • Flight deck to Ground Com . . . . ..Establish
    • Door lights . . . . . . . . . . . . . . . . . . . . . .OUT
    • Flight deck door & window . . . . . . .Locked
    • Hydraulic pumps . . . . . . . . . . . . .“A pumps OFF” or “4 Pumps ON"
    • ................(4 ON, LO PRESS Lt OUT, Min 2800psi A&B + Brakes)..........

    • Get Clearance from ATC
    • ----------------

    • Anticollision light switch . . . . . . . . . . . . .ON
    • Relay push back instructions to ground crew
    • Parking Brake . . . . . . . . . . . . . . . .AS RQD

    Call:''BELOW THE LINE''
  9. 9- ENGINE START (C)
    • -At N2 25%:
    • Engine start lever . . . . . . . . .IDLE DETENT
    • Chronograph . . . . . . . . . . . . . . . . . . . .start (Light up within 10 sec).
    • Fuel flow . . . . . . . . . . . . . . . . . . . . .monitor
    • EGT . . . . . . . . . . . . . . . . . . . . . . . . .monitor

    • -When N2 is at 56%:
    • Call:“56%'', verify that the ENGINE START switch moves to OFF

    • -After the engine is stable at idle:
    • Call: “ENGINE #___STABLE''
    • Chronograph . . . . . . . . . . . . . . . .stop/reset
  10. 10- AFTER START (C) 5
    • Eng Start Levers . . . . . . . . . . . ..Idle detent
    • Generators 1 & 2 switches . . . . . . . . . .ON
    • Hydraulic Pumps switches . . . . . . . . . .ON (AFTER Bypass Pin Removal)
    • APU switch . . . . . . . . . . . . . . . . . . .As Req
    • Ground crew . . . . . . . ..order to disconnect

    Call: “ AFTER START CHECKLIST'
  11. 11- TAXI (C)
    • When clear of Ramp:
    • Call: “FLIGHT CONTROLS CHECK''

    • After Other Checks:
    • Call: “RUDDER CHECK''

    • NOSE WHEEL tiller . . . . . . . . . . . . . . .Hold
    • RUDDER pedals . . . . . . . . . . . . . . . .Move
    • Call: . . . . . . . . . . . . . . . . . . .“FULL LEFT''
    • Call: . . . . . . . . . . . . . . . . . .“FULL RIGHT''
    • Call: . . . . . . . . . . . . . . . . . . . .“NEUTRAL'

    Call: . . .. . . . . . . .. . "MINI-BRIEF"

    • Then:
    • Call: ‘'BEFORE TAKEOFF CHECKLIST TO THE LINE''

    • When complete:
    • Ask the SC to perform the PA.
  12. 12- LINE UP FLOW (C)
    • Call:“CLEAR LEFT''
    • TAXI light . . . . . . . . . . . . . . . . . . . . . . .ON
    • RUNWAY TURN OFF light . . . . . . . . . .ON

    Call: “BELOW THE LINE''

    • When cleared Takeoff:
    • FIXED LANDINGS lights . . . . . . . . . . .ON
    • Elapsed time . . . . . . . . . . . . . . . . . . ..RUN
  13. 13- TAKEOFF PROCEDURE (PF)
    • Call: "TAKEOFF". "N1, TOGA, SET THRUST"
    • -Verify 80 kts and call: “CHECK”
    • -Verify that A/T annunciation changes to THR HLD by 84 knots.
    • -At VR, rotate toward 15° pitch attitude.
    • -After lift-off, follow F/D commands.

    • Above 400 ft AAE:
    • -If no lateral mode engaged call “ENGAGE HDG SEL or LNAV”
    • -Call: “HDG SEL” or “LNAV”
    • -Engage A/P and verify FMA and Call: “COMMAND___” (A or B)

    • At Thrust Reduction Height 1 000 ft:
    • -Verify or set Climb Thrust and LVL CHG then call FMA.
    • CAUTION : Select N1 only when automatic thrust reduction has not occurred

    • At ACCEL ALTITUDE (1000 or 3000 AGL):
    • -Set MCP speed bug to “UP”
    • -Verify Acceleration.
    • -Call “FLAPS___” according to flap speed schedule.

    • When flaps are up and above 3 000 ft AGL:
    • -Engage VNAV or select normal en-route climb speed and call FMA.
    • -Call: ‘'AFTER TAKEOFF CHECKLIST''
  14. 14- CRUISE (PF) 1
    • Rudder trim . . . . . . . . . . . . . . . . . .adjust
    • • A/P engaged
    • • Fuel balanced
    • • Symetric thrust (N1)
    • • Rudder and aileron trims at 0
    • • Engage HDG SEL mode
    • • Slowly trim rudder only to reach 0 of aileron deflection
    • • Reengage appropriate lateral mode.

    Call: ‘' CRUISE CHECKLIST''
  15. 15- DESCENT PREPARATION (PF)
    • ATIS . . . . . . . . . . . . . . . . . . . . . . . . . .obtain
    • Approach ban . . . . . . . . . . . . . . . . . .review

    • Approach CDU . . . . . . . . . . . . . . . .program
    • *DEP/ARR page
    • • Select approach
    • • Select STAR
    • • Select transition
    • • Execute

    • *LEGS page
    • • Verify waypoints and constraints
    • • Set DA or DH
    • • Set RNP 0.3 NM for NPA

    • *DES page
    • • Adjust descent speed
    • • Insert current cruise Mach and 280 kts . ex: 0.78/280

    • *Bugs : Approach REF page
    • • Select Vref
    • • Insert wind correction

    • *NAV aids and course . . . . . . . . . .tune / set
    • • NAV accuracy as required
    • • VOR/ADF switch as required

    • *AUTO BRAKE . . . . . . . . . . . . . . . . . . ..set
    • • Verify landing distance with OPT

    *BRIEFING
  16. 16- APPROACH BRIEFING (PF)
    ATIS and approach ban . . . . . . . . . .review

    ‘'This will be a STAR_____ at _____airport, page__ effective date____ follow by an _____ approach____ runway ___ page__effective date____ TL___MSA____....'

    • *LEGS page
    • • Read from CDU all waypoints and constraints from the beginning of STAR until the DA or DH.

    • ---- ‘‘CALL ME 100 ABOVE AND MINIMUM
    • ---- I'LL CALL CONTINUE OR GO AROUND FLAPS
    • ---- AT POSITIVE CLIMB -- GEAR UP
    • ---- CHECK MISSED APPROACH ALTITUDE
    • ---- AT 400FT LNAV or HDG SEL''.

    • • Then read from CDU the missed approach.
    • • RNP set

    • *APPROACH REF page
    • • Vref (confirm display on PFD speed tape)

    • *NAV aids
    • • ILS/VOR/ADF frequencies and ident.
    • • Course

    • *Auto brake/Reversers usage
    • • Runway condition


    • *SPECIAL REQUIREMENTS
    • • MEL
    • • Auto pilot disconnection
    • • NOTAM
    • • Anti-ice
    • • Route Taxi
    • • Temperature corrections

    Then call "DESCENT CHECKLIST"

    Call:''ENGINE ANTI-ICE ON'' if req'd
  17. 17- ILS APPROACH (PF)
    • *At RA 2500 feet:
    • -"FLAPS 1"

    • *When on approach intercept heading and cleared for the approach:
    • • Select APP
    • • Engage 2nd autopilot ONLY when AutoLand is required (CAT II and III)

    • *At G/S ALIVE:
    • - Call: "GEAR DOWN,--- FLAPS 15--- LANDING CHECKLIST TO THE LINE"
    • - ARM Speedbrake; verify SPEED BRAKE ARMED light illuminated.
    • • Set MCP speed selector to flap speed schedule if required. (If not in VNAV)

    • *At G/S capture
    • - Call: “FLAPS ___” (as required for landing)
    • • Set MCP speed selector to flap speed schedule.
    • • Set Missed approach altitude on MCP
    • - Call: "BELOW THE LINE"

    *For autoland, call "FLARE ARMED" when it appears on FMA

    • *At 1 000 ft AGL
    • - Call: "CONTINUE--- SET MISSED APPROACH ALTITUDE" or "GO-AROUND FLAPS"
  18. 18- GO-AROUND AND MISSED APPROACH PROCEDURE (PF)
    • *Simultaneously:
    • • Press TO/GA switch
    • • Adjust /monitor pitch to follow flight director.
    • • Set TOGA Thrust and Call: "GO-AROUND FLAP".

    • *Verify Positive Rate of Climb
    • - Call: “GEAR UP---- CHECK MISSED APPROACH ALTITUDE”

    *If airspeed is below the top of the amber band, limit bank angle to 15°

    *Maintain a minimum of V2 +15 during initial climb

    • *Above 400 ft AAE
    • - Select or call: “HDG SEL” or “LNAV”

    • *At 1 000 ft AAE: acceleration altitude
    • - Call "FLAPS___" according to flap speed schedule.
    • - Verify Acceleration (If AP on, then Pitch mode is MCP SPD, manually select SPD BUG UP)
    • • Speed brake disarm (Captain)

    • *After flap retraction
    • • Select LVL CHG
    • • Confirm or set climb thrust
    • • Verify Missed App ALT captured
    • • Maintain Flaps Maneuvering Speed

    Call "AFTER TAKEOFF CHECKLIST"
  19. 19- AFTER LANDING (C)
    • *At Rollout
    • - Prior to 60 Kts, disarm the auto brake via manual braking or stowing SPD BRK.
    • - Call: "MANUAL BRAKING"

    • *At 60 knots:
    • - Gradually reduce thrust to IDLE Reverse Thrust (<30% N1) and slow to taxi speed.
    • - Then stow Reversers.

    • *Speedbrakes. . . . . . . . . . . . . . . . . . .STOW
    • *Landing and Taxi light switches . ..AS REQ
  20. 20- PARKING (C) 6
    • Parking Brake . . . . . . . . . . . . . . . . . . . SET
    • Start Levers . . . . . . . . . . . . . . . ..CUT-OFF
    • Fasten Belts switch . . . . . . . . . . . . . . .OFF
    • Anti-Collision Light . . . . . . . . . . . . . . .OFF
    • Fuel Pumps . . . . . . . . . . . . . . . . . . . . OFF (Leave one ON for APU)

    • After wheel chocks are in place:
    • Parking Brake. . . . . . . . . . . . . . . . RELEASED
  21. 21- SEQUENCE
    • 1- PRELIMINARY CHECKS
    • 2- CDU PREFLIGHT
    • 3- COCKPIT SCAN
    • 4- INSTRUMENTS CHECK & FINAL DATA
    • 5- TAKEOFF BRIEFING
    • 6- CABIN ALT WARNING BRIEFING
    • 7- FAMPACT
    • 8- BEFORE START..............

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