Procedures Flashcards
INSTRUMENT APPROACH USING V/S
Autopilot is recommended until suitable visual reference is established;
Tune and identify appropriate navaids. If additional waypoint references are desired
(VDP), use the FIX page;
Verify/enter the appropriate RNP;
The barometric minimums selector should be set at MDA(H)+50 ft (DA(H)/MDA(H)+50
ft) to ensure that if a missed approach is initiated, descent below the MDA(H) does not
occur during the missed approach;
Use of VSD (Vertical Situation Display) on ND is highly recommended.
“CABIN READY”………………………………………………………………………………………….Recieve
The recommended roll modes for the final approach are:
For an RNAV or GPS approach use LNAV;
For a LOC-BC, VOR or NDB approach use LNAV;
For a LOC, SDF or LDA approach use LNAV or VOR/LOC.
When on localizer / final approach course intercept heading:
Verify that the navigation radios are tuned and identified (as needed);
Verify that the deviation pointers are shown.
LNAV or other roll mode……………Select
APPROXIMATELY 2 NM BEFORE THE FINAL APPROACH FIX
Call: “GEAR DOWN”
“FLAPS 15”
Call: “APPROACHING GLIDEPATH”
LANDING GEAR lever ………………… Set DN
Verify that the green landing gear indicator
lights are illuminated.
FLAP lever………………………….Set to 15
ENGINE START switches …… Set to CONT
FASTEN BELTS ……….. twice OFF then ON
SPEEDBRAKE lever …………….. Set to ARM
SPEED BRAKE ARMED light is illuminated ………………………. Verify
MCP altitude window to the first altitude constraint, or MDA(H) if no altitude
constraint exists……………………………….Set
V/S armed on FMA ………………………. Verify
Note: If desired altitude is not at an even 100 foot increment, set the MCP altitude to the nearest 100 foot increment above the altitude constraint or MDA(H).
AT THE FINAL APPROACH FIX
Crossing altitude…………………………………………………………………………………………….Verify
Altimeters……………………………………………………………………………………………..Crosscheck
Call: “CROSSCHECKED”
Desired V/S……………………………………….Set
Set desired V/S to descend to MDA(H). Use
a V/S that results in no level flight segment at
MDA(H). Initial selection of an appropriate
V/S should be made considering the
recommended vertical speeds that are
published on the approach chart, if available.
If no recommended vertical speeds are
available, set approximately -700 to -800 fpm
(1/2 ground speed x 10).
Call:
“PASSING FAF (or FIX NAME), … FEET”
Call: “FLAPS ___ “ as needed for landing
Call: “SPEED CHECKED, FLAPS___”
FLAP lever ……………………. Set as directed
FLAPS extension…………………………………………………………………………………………Monitor
Verify flap position on flap position indicator and confirm numbered flap maneuvering speed
bugs on PFD are removed.
Call: “LANDING CHECKLIST”
LANDING checklist………………Perform
Approach…………………………………………………………………………………………………….Monitor
AT 1000 FT ABOVE AIRFIELD ELEVATION
Flight parameters…………………………………………………………………………….Verify
Call: “ONE THOUSAND – STABILIZED” or
If the A/C is not stabilized on the approach
path in landing configuration at minimum
stabilization height or below.
Call: “NOT STABILIZED – GO AROUND”
WHEN APPROXIMATELY 300 FEET ABOVE THE MDA(H) OR DA(H)
Missed approach altitude on MCP……Set
NOT BELOW MDA(H) or DA(H)
If suitable visual reference established and
made decision for landing, call:
“CONTINUE”
AT MDA(H)+80FT or DA(H)+80FT
Monitor or call:
“APPROACHING MINIMUMS”
AT MDA(H) or DA(H)
If suitable visual reference not established
or anytime when it’s lost, call:
“GO AROUND, FLAPS 15,
CHECK THRUST”
Monitor or call: “MINIMUMS”
If suitable visual reference is established:
A/T……………………………………….Disconnect
A/P………………………………………..Disengage
Call: “RECYCLE FD’S”
FD’s…………………………………..Recycle
Glidepath to landing………………….Maintain
Monitor approach, callout any deviations.
Exterior inspection – CM2
Before flight from the base airport or after maintenance action CM2 verify that:
- nose and main gear pins are removed;
- pitot probe covers are removed.
Preliminary preflight procedure – CM2
Nose and main gear pins are on board ………………………………………………………Check
IRS mode selectors…………………………………………………………………………………OFF, then NAV
ELT switch………………………………………………………………………………………………..Guard closed
PSEU light……………………………………………………………………………………….Verify extinguished
GPS light…………………………………………………………………………………………Verify extinguished
ILS light (if applicable)……………………………………………………………………..Verify extinguished
GLS light (if applicable)……………………………………………………………………Verify extinguished
SERVICE INTERPHONE switch………………………………………………………………………………..OFF
ENGINE panel ………………………………………………………………………………………………………….Set
OXYGEN panel …………………………………………………………………………………………………………Set
PASS OXYGEN switch – Guard closed
Landing gear indicator lights……………………………………………………………….Verify illuminated
FLIGHT RECORDER switch……………………………………………………………………….Guard closed
MACH AIRSPEED WARNING TEST switches………………………..Push and hold one at a time
STALL WARNING TEST switches……………………………………….Push and hold, one at a time
EMERGENCY EXIT LIGHTS switch……………………………………………………………..Guard closed
Verify that the NOT ARMED light is extinguished.
Circuit breakers (P6 panel)……………………………………………………………………………………Check
MANUAL GEAR EXTENSION ACCESS DOOR……………………………………………………….Closed
Circuit breakers (control stand, P18 panel)……………………………………………………………Check
EFB power on-off button (on Captain and First Officer sides)………………………………….Push
Emergency equipment………………………………………………………………………………………….Check
Aircraft documents………..……………………………………………………………………..Check
Flight deck access system test………………………………………………………………Perform
FLIGHT DECK ACCESS SYSTEM switch…………………………………………………………As needed
Preliminary preflight procedure – CM1
CREW OXYGEN pressure………………………………………………………………………………………Check
HYDRAULIC quantity……………………………………………………………………………..Check
Engine OIL QTY…………………………………………………………………………………..Check
WEATHER RADAR on both sides………………………………………………………..Check OFF
LIGHTS………………………………………………………………………………………………………………..Check
Master LIGHTS TEST and DIM switch – TEST
Aircraft technical status………………………………………………..………………………..Check
PARKING BRAKE…………………………………………………………………………………………..As needed
Overheat and fire protection panel……………………………………………………………………….Check
APU switch……………………………………………………………………………………………………..START
Air conditioning panel……………………………………………………………………………………………….Set
CDU preflight procedure CM2 and CM1
Electronic Flight Bag ………………………………………………………………………………………..Set CM2
Adjust display brightness (as required).
MENU key – Push.
On the MAIN MENU page:
Select INITIALIZE FLIGHT button.
Check/Clear all FAULT, MEMO, MSG items displayed.
Initial Data ………………………………………………………………………………………………………..Set СМ2
IDENT page:
Verify that the MODEL is correct.
Verify that the ENG RATING is correct.
Verify that the navigation data base ACTIVE date range is current.
POS INIT page:
Verify that the time is correct.
Enter the present position on the SET IRS POS line. Use the most accurate latitude and
longitude.
Navigation data ………………………………………………………………………………………………..Set СМ2
ROUTE page:
For route request via DATALINK:
Enter the FLIGHT NUMBER.
Push ROUTE REQUEST line select key.
When ROUTE UPLINK READY FMC Communication Message displays in the CDU
scratchpad:
Push LOAD line select key
Push EXEC key.
For manual route entry:
Enter the ORIGIN.
Enter the route (Company Route may be used).
Enter the FLIGHT NUMBER.
Activate and execute the route.
ATIS or WX INFO ……………………………………………………………….…………Recieve CM2
EFB CHART CLIP …………………………………………………………..…………….Prepare CM2
Prepare CHART CLIP for intended departure RWY (Taxi chart, SID, EOSID, emergency
return, takeoff alternate etc.).
Navigation data ………………………………………………………………………………………………..Set СМ2
DEPARTURES page:
Select the runway and departure routing.
Execute the runway and departure routing.
LEGS page:
Verify or enter the correct RNP for the departure.
Verify that the route is correct on the RTE pages. Check the LEGS pages as needed to
ensure compliance with the flight plan.
ROUTE 2 page: set with modification of RWY, SID, EO SID (if required and available).
Performance data ……………………………………………………………………………………………..Set СМ2
PERF INIT page:
Enter the ZFW
Note: Enter the actual or expected ZFW from data link loadsheet or OFP.
Enter RESERVES
Enter COST INDEX
Enter CRZ ALT
Enter CRZ WIND (mean equivalent cruise wind or received by ACARS)
Enter T/C OAT
Vеrify TRANS ALT
Verify that the FUEL on the CDU, the dispatch papers, and the fuel quantity indicators
agree.
Verify that the fuel is sufficient for flight.
Verify that the gross weight and cruise CG (GW/CRZ CG) on the CDU and the dispatch
papers agree.
Thrust mode display:
Verify that dashes are shown.
N1 LIMIT page:
Insert outside air temperature
TAKEOFF REF page:
Make data entries on page 2
Verify or enter an acceleration height
Verify or enter a thrust reduction altitude
ACARS ……………………………………………………………………………………………………..Initialize СМ2
COMPANY page – Select
FLIGHT INITIALIZATION page – Select
Verify/Enter:
FLIGHT NUMBER (AFL … )
DEPT (Departure station (ICAO))
ALT1 (Alternate station (ICAO))
FLIGHT PLAN TIME (HH:MM)
DAY (from OFP)
DEST (Destination station (ICAO))
ALT2 (Alternate station (ICAO))
Electronic Flight Bag ………………………………………………………………………………………..Set CM1
Adjust display brightness
Menu key – Push
On the MAIN MENU page:
Select INITIALIZE FLIGHT button
Check/Clear all FAULT, MEMO, MSG items displayed
ATIS or WX INFO ……………………………..……………………………………………Recieve CM1
EFB CHART CLIP …………………….…………………………………………….Prepare СМ1
Prepare CHART CLIP for intended departure runway (Taxi chart, SID, EOSID, emergency return,
takeoff alternate etc.).
CDU entries ………………………………………………………………………..………..Check CM1
SID, EOSID and ROUTE ………………………………………………..…………….Check BOTH
This procedure is regarded as part of the takeoff briefing.
CM2 reads aloud (from appropriate navigation chart) airfield code, page index, chart validation,
ATC (Radar) frequency, Transition Altitude, Current Transition Level and QNH, MSA, SID name,
initial climb clearance and routing (including altitude/speed constraints and fly-over waypoints)
and other significant information. CM1 checks departure routing using ND display in PLN mode
and the LEGS pages as needed to ensure compliance with navigation chart and checks/modifies
CDU, MCP and RNP entries.
Verify the route is correct on the LEGS pages versus the OFP. CM1 reads aloud flight plan
waypoints on the LEGS pages while CM2 checks versus the OFP.
PROG key on CDU……………………………………………………………………………….Push CM1
DTG and FUEL (distance to go and fuel remaining at destination)…………………………Call CM1
OFP ground distance and fuel remaining at destination ……………….……………..Call CM2
To ensure compliance with the flight plan, verify distance and FOB from CDU PROGRESS
page against OFP ground distance and fuel remaining for gross error check.
Preflight procedure - CM2
FLIGHT CONTROL panel …………………………………………………………………………………Check
FLIGHT CONTROL switches – Guards closed
Verify that the flight control LOW PRESSURE lights are illuminated.
Flight SPOILER switches – Guards closed
YAW DAMPER switch – ON
Verify that the YAW DAMPER light is extinguished.
Verify that the standby hydraulic LOW QUANTITY light is extinguished.
Verify that the standby hydraulic LOW PRESSURE light is extinguished.
Verify that the STBY RUD ON light is extinguished.
ALTERNATE FLAPS master switch – Guard closed
ALTERNATE FLAPS position switch – OFF
Verify that the FEEL DIFF PRESS light is extinguished.
Verify that the SPEED TRIM FAIL light is extinguished.
Verify that the MACH TRIM FAIL light is extinguished.
Verify that the AUTO SLAT FAIL light is extinguished.
NAVIGATION panel ……………………………………………………………………………………………….Set
VHF NAV transfer switch – NORMAL
IRS transfer switch – NORMAL
FMC source select switch – NORMAL
DISPLAYS panel ……………………………………………………………………………………………………Set
SOURCE selector – AUTO
CONTROL PANEL select switch – NORMAL
Fuel panel ……………………………………………………………………………………………………………..Set
Verify that the ENG VALVE CLOSED lights are illuminated dim.
Verify that the SPAR VALVE CLOSED lights are illuminated dim.
Verify that the FILTER BYPASS lights are extinguished.
CROSSFEED selector – Closed
Verify that the VALVE OPEN light is extinguished.
FUEL PUMPS switches – OFF
Verify that the center tank fuel pump LOW PRESSURE lights are extinguished.
Verify that the main tank fuel pump LOW PRESSURE lights are illuminated.
Electrical panel ………………………………………………………………………………………………………..Set
BATTERY switch – Guard closed
CAB/UTIL power switch – ON
IFE/PASS SEAT power switch – ON
STANDBY POWER switch – Guard closed
Verify that the STANDBY PWR OFF light is extinguished.
Verify that the BAT DISCHARGE light is extinguished.
Verify that the TR UNIT light is extinguished.
Verify that the ELEC light is extinguished.
Generator drive DISCONNECT switches – Guards closed
Verify that the DRIVE lights are illuminated.
BUS TRANSFER switch – Guard closed
Verify that the TRANSFER BUS OFF lights are extinguished.
Verify that the SOURCE OFF lights are extinguished.
Verify that the GEN OFF BUS lights are illuminated.
Overheat and fire protection panel ……………………………………………………………………….Check
Do this check if the flight crew did not do the Electrical Power Up supplementary
procedure.
This check is needed once per flight day.
Verify that the engine No. 1, APU, and engine No. 2 fire switches are in.
Alert ground personnel before the following test is accomplished:
OVERHEAT DETECTOR switches – NORMAL
TEST switch – Hold to FAULT/INOP
Verify that the MASTER CAUTION lights are illuminated.
Verify that the OVHT/DET annunciator is illuminated.
Verify that the FAULT light is illuminated.
If the FAULT light fails to illuminate, the fault monitoring system is inoperative.
Verify that the APU DET INOP light is illuminated.
Do not run the APU if the APU DET INOP light does not illuminate.
Note: The fire warning light flashes and the horn sounds on the APU ground control panel
when this test is done with the APU running. This can be mistaken by the ground
crew as an APU fire.
TEST switch – Hold to OVHT/FIRE
Verify that the fire warning bell sounds.
Verify that the master FIRE WARN lights are illuminated.
Verify that the MASTER CAUTION lights are illuminated.
Verify that the OVHT/DET annunciator is illuminated.
Master FIRE WARN light – Push
Verify that the master FIRE WARN lights are extinguished.
Verify that the fire warning bell cancels.
Verify that the engine No. 1, APU and engine No. 2 fire switches stay illuminated.
Verify that the ENG 1 OVERHEAT and ENG 2 OVERHEAT lights stay illuminated.
Verify that the WHEEL WELL light stays illuminated.
EXTINGUISHER TEST switch – Check
TEST switch – Position to 1 and hold
Verify that the three green extinguisher test lights are illuminated.
TEST switch – Release
Verify that the three green extinguisher test lights are extinguished.
Repeat for test position 2
APU switch (as needed) ……………………………………………………………………………………..START
Note: If extended APU operation is needed on the ground and the airplane busses are
powered by AC electrical power, position an AC powered fuel pump ON. This will
extend the service life of the APU fuel control unit.
Note: If fuel is loaded in the center tank, position the left center tank fuel pump switch
ON to prevent a fuel imbalance before takeoff.
CAUTION: Center tank fuel pump switches should be positioned ON only if the fuel quantity
in the center tank exceeds 453 kgs.
CAUTION: Do not operate the center tank fuel pumps with the flight deck unattended.
When the APU GEN OFF BUS light is illuminated:
APU GENERATOR bus switches – ON
Verify that the SOURCE OFF lights are extinguished.
Verify that the TRANSFER BUS OFF lights are extinguished.
Note: Run the APU for one full minute before using it as a bleed air source.
EQUIPMENT COOLING switches ………………………………………………………………………….NORM
Verify that the OFF lights are extinguished.
Passenger signs……………………………………………………………………………………………………….Set
FASTEN BELTS switch – ON
Windshield WIPER selectors ………………………………………………………………………………..PARK
Verify that the windshield wipers are stowed.
WINDOW HEAT switches ………………………………………………………………………………………….ON
Position switches ON at least 10 minutes before takeoff.
Verify that the OVERHEAT lights extinguish within 5 seconds.
Note: The master caution and ANTI-ICE system annunciator lights can illuminate.
Verify that the ON lights are illuminated (except at high ambient temperatures).
PROBE HEAT switches ………………………………………………………………………………………..AUTO
Verify that all lights are illuminated. Set to on if in icing conditions.
WING ANTI–ICE switch ……………………………………………………………………………………………OFF
Verify that the VALVE OPEN lights are extinguished.
Verify that the ICE DETECTOR light is extinguished.
ENGINE ANTI–ICE switches …………………………………………………………………………………….OFF
Verify that the COWL ANTI–ICE lights are extinguished.
Verify that the COWL VALVE OPEN lights are extinguished.
HYDRAULIC panel ……………………………………………………………………………………………………Set
ENGINE HYDRAULIC PUMPS switches – ON
Verify that the LOW PRESSURE lights are illuminated.
ELECTRIC HYDRAULIC PUMPS switches – OFF
Verify that the OVERHEAT lights are extinguished.
Verify that the LOW PRESSURE lights are illuminated.
Air conditioning panel ………………………………………………………………………………………………Set
AIR TEMPERATURE source selector – As needed
TRIM AIR switch – ON
Verify that the ZONE TEMP lights are extinguished.
Temperature selectors – As needed
Verify that the RAM DOOR FULL OPEN lights are illuminated.
RECIRCULATION FAN switches – AUTO
Air conditioning PACK switches – AUTO or HIGH
ISOLATION VALVE switch – OPEN
Engine BLEED air switches – ON
APU BLEED air switch – ON
Verify that the DUAL BLEED light is illuminated.
Verify that the PACK lights are extinguished.
Verify that the WING–BODY OVERHEAT lights are extinguished.
Verify that the BLEED TRIP OFF lights are extinguished.
Cabin pressurization panel ……………………………………………………………………………………….Set
Verify that the AUTO FAIL light is extinguished.
Verify that the OFF SCHED DESCENT light is extinguished.
FLIGHT ALTITUDE indicator – Cruise altitude
LANDING ALTITUDE indicator – Destination field elevation
Pressurization mode selector – AUTO
Verify that the ALTN light is extinguished.
Verify that the MANUAL light is extinguished.
Lighting panel ………………………………………………………………………………………………………Set
LANDING light switches – OFF
RUNWAY TURNOFF light switches – OFF
TAXI light switch – OFF
IGNITION select switch ……………………………………………………………………………….IGN R or L
Alternate the IGNITION SELECT switch position on subsequent starts. For the first
aircraft flight of the day set to R.
ENGINE START switches ……………………………………………………………………………………..OFF
LIGHTING panel …………………………………………………………………………………………………….Set
LOGO light switch – As needed
POSITION light switch – As needed
ANTI–COLLISION light switch – OFF
WING illumination switch – As needed
WHEEL WELL light switch – As needed
Mode Control Panel………………………………………………………………………………………………..Set
COURSE(S) – Set
FLIGHT DIRECTOR switch – ON
Move the switch for the pilot flying to ON first.
EFIS control panel …………………………………………………………………………………………………Set
MINIMUMS reference selector – RADIO or BARO
MINIMUMS selector – Set decision height or altitude reference
Flight Path Vector switch – As needed
METERS switch – As needed
BAROMETRIC reference selector – IN or HPA
BAROMETRIC selector – Set local altimeter setting
VOR/ADF switches – As needed
Mode selector – MAP
CENTER switch – As needed
Range selector – As needed
TRAFFIC switch – As needed
WEATHER RADAR – Off
Verify that the weather radar indications are not shown on the MAP.
Map switches – As needed
Oxygen ……………………………………………………………………………………………………Test and set
Note the crew oxygen pressure.
Oxygen mask – Stowed and doors closed
TEST/RESET switch – Push and hold
Verify that the yellow cross shows momentarily in the flow indicator.
EMERGENCY/Test selector – PUSH and HOLD
Continue to hold the TEST/RESET switch down and push the EMERGENCY/Test selector
for 5 seconds. Verify that the yellow cross shows continuously in the flow indicator.
Verify that the crew oxygen pressure does not decrease more than 100 psig.
If the oxygen cylinder valve is not in the full open position, pressure can:
decrease rapidly, or
decrease more than 100 psig, or
increase slowly back to normal.
Release the TEST/RESET switch and the EMERGENCY/Test selector. Verify that the yellow
cross does not show in the flow indicator.
Note: 5 second oxygen flow/pressure drop test is required once per flight day, following a
flight crew change or following any maintenance action.
Normal / 100% switch – 100 %
Crew oxygen pressure – Check
Verify that the pressure is sufficient for dispatch.
Clock ……………………………………………………………………………………………………………………….Set
TIME/DATE pushbutton - UTC time
Display select panel …………………………………………………………………………………………………Set
MAIN PANEL DISPLAY UNITS selector – NORM
LOWER DISPLAY UNIT selector – NORM
TAKEOFF CONFIG light (if installed and operative)……………………………Verify extinguished
CABIN ALTITUDE light (if installed and operative)……………………………..Verify extinguished
Disengage light TEST switch ……………………………………………………………………………Hold to 1
Verify that the A/P light is illuminated steady amber.
Verify that the A/T light is illuminated steady amber.
Verify that the FMC light is illuminated steady amber.
Disengage light TEST switch ……………………………………………………………………………Hold to 2
Verify that the A/P light is illuminated steady red.
Verify that the A/T light is illuminated steady red.
Verify that the FMC light is illuminated steady amber.
Do the Initial Data and Navigation Data steps from the CDU Preflight Procedure and verify
that the IRS alignment is complete before checking the flight instruments.
Flight instruments ……………………………………………………………………………………………….Check
Verify that the flight instrument indications are correct.
Verify that only these flags are shown:
TCAS OFF;
Verify that the flight mode annunciations are correct:
autothrottle mode is blank;
roll mode is blank;
pitch mode is blank;
AFDS status is FD.
Select the map mode.
GROUND PROXIMITY panel …………………………………………………………………………………Check
FLAP INHIBIT switch – Guard closed
GEAR INHIBIT switch – Guard closed
TERRAIN INHIBIT switch – Guard closed
RUNWAY INHIBIT switch – Guard closed
Verify that the GROUND PROXIMITY INOP light is extinguished.
Verify that the RUNWAY INOP light is extinguished.
The RUNWAY INOP light may be illuminated until the GPS accuracy is adequate for the
Runway Awareness and Advisory System requirements.
LANDING GEAR panel ……………………………………………………………………………………………..Set
LANDING GEAR lever – DN
Verify that the green landing gear indicator lights are illuminated.
Verify that the red landing gear indicator lights are extinguished.
AUTO BRAKE select switch ……………………………………………………………………………………RTO
Verify that the AUTO BRAKE DISARM light is extinguished.
ANTISKID INOP light ……………………………………………………………………….Verify extinguished
Engine display control panel ……………………………………………………………………………………Set
N1 SET selector – AUTO
SPEED REFERENCE selector – AUTO
FUEL FLOW switch – RATE
Move switch to RESET, then RATE.
Engine instruments …………………………………………………………………………………………….Check
Verify that the primary and secondary engine indications show existing conditions.
Verify that no exceedance is shown.
Verify that the hydraulic quantity indications do not show RF.
MFD Cancel / Recall switch – Push
Verify that the autoland status advisory messages are not shown.
CARGO FIRE panel …………………………………………………………………………………………….Check
This check is needed once per flight day.
DETECTOR SELECT switches – NORM
TEST switch – Push
Verify that the fire warning bell sounds.
Verify that the master FIRE WARN lights are illuminated.
Master FIRE WARN light – PUSH
Verify that the master FIRE WARN lights are extinguished.
Verify that the fire warning bell cancels.
Verify that the green EXTINGUISHER test lights stay illuminated.
Verify that the FWD and AFT lights stay illuminated.
Verify that the DETECTOR FAULT light stays extinguished.
Verify that the DISCH light stays illuminated.
Radio tuning panel …………………………………………………………………………………………………..Set
WARNING: Do not key the HF radio while the airplane is being fueled. Injury to
personnel or fire can occur.
Verify that the OFF light is extinguished.
VHF NAVIGATION radios ……………………………………………………………………..Set for departure
WEATHER radar control panel ………………………………………………………………………………….Set
Mode selector – AUTO
System control – NORM
Gain control – CAL
Transponder panel …………………………………………………………………………………………………..Set
Оnly transponder №1 is operative in case of all generators failure.
ADF radios ………………………………………………………………………………………………………………Set
Audio control panel ………………………………………………………………………………………………….Set
Check that the Push–to–Talk Switch on the ACP panel is in neutral position.
Stabilizer trim OVERRIDE switch ………………………………………………………………Guard closed
WARNING: Do not put objects between the seat and the aisle stand. Injury can occur
when the seat is adjusted.
Seat ……………………………………………………………………………………………………………………Adjust
Use the handhold above the forward window for assistance when pulling the seat forward.
Do not use the glareshield as damage can occur.
Adjust the seat for optimum eye reference.
Whenever the seat is adjusted, verify a positive horizontal (fore anaft) seat lock by pushing
against the seat.
Rudder pedals …………………………………………………………………………………………………….Adjust
Adjust the rudder pedals to allow full rudder pedal and brake pedal movement.
Seat belt and shoulder harness ……………………………………………………………………………Adjust
PREFLIGHT checklist on the Captain’s command………………………………….Accomplish
Preflight performance calculation
Preflight performance calculation
Start the Preflight Performance Calculation Procedure when data link loadsheet or paper
loadsheet is available.
This procedure is regarded as part of the takeoff briefing.
Note: Inform the ground staff (ramp agent or OCC) in case of:
the ACARS is unavailable, or
there is no datalink loadsheet 15 min prior to block-off time, or
cockpit printer failure.
Note: OFP EZFW Data may be used for preliminary calculation. After the final loadsheet
is available, if the actual GW for takeoff is less, than used for preliminary
calculations, the crew may not change the CDU entries. If more – recalculate
performance and enter data in the CDU. Saving engine’s life by reducing thrust for
takeoff should always be considered.
CM1 CM2
CDU performance data…..…………………..……………..…………………………………Insert
Zero Fuel Weight………..………………….Call
The CM1 calls ZFWA.
Zero Fuel Weight into CDU….………..Enter
Verify ZFWA against the loadsheet and insert
Cruise CG……………….………………………………………………………………………Check
Check the cruise CG is set 5%.
Fuel quantities….………………………………………………………………………………Check
Verify the FUEL on the CDU, OFP, and UPPER DU agree.
Verify that the fuel is sufficient for flight.
Gross Weight…..………………………Check
Compare the called CDU Gross Weight and
the ATOW from the loadsheet and OPT
allowing for taxi fuel.
Gross Weight………………….…………..Call
Call the CDU Gross Weight.
OPT EFB takeoff performance……………………………………………………………………….Calculate
CM1 and CM2 independently calculate the performance data for takeoff on respective EFB.
Note: Consider using larger flap settings to provide shorter takeoff distance and greater tail
clearance. Preferably Flaps 10 and 15 should be used for takeoff if performance allows.
Computed performance data…………………………………………………………………….Crosscheck
CM2 reads calculated performance data from the right EFB, CM1 checks data against the left.
Assumed temperature and N1%……….Call
Call the fixed derate takeoff or an assumed
temperature, or both, as needed, from the EFB
and check the CM2 entry.
N1 LIM page in CDU..………………………Set
Select a fixed derate takeoff or an assumed
temperature, or both as needed. Use “NO
ENG BLEED TAKEOFF”, if needed.
N1 reference on CDU………………………………………………………………………….Verify
CLIMB thrust…………………………….Verify
CLIMB thrust……..……………Verify / Select
Use automatically calculated CLB1 or CLB2
derated climb thrust. Select CLB climb thrust
only for safety or performance reason.
MIN ACCEL HT (EFB)…………………….Call
TAKEOFF 2/2 page…………………………Set
Verify / Enter:
EO ACCEL HT
THRUST RED
ACCEL HT
Note: EO ACCEL HT can not be less then MIN ACCEL HT computed by EFB.
Note: Set ACCEL HT and THRUST RED as required by local rules (NADP).
Takeoff flap setting (EFB)….……………Call TAKEOFF 1/2 page…………………….Select
Takeoff flap setting (CDU)……………….Enter
Takeoff CG……..………………….………Call
Call takeoff CG from the loadsheet / data link
loadsheet.
Takeoff CG………………..…………….Enter
STABILIZER TRIM…………………………Set
Takeoff speeds V1,VR,V2 (EFB)……….Call Takeoff speeds V1, VR, V2 (CDU)……Enter
CDU display…………………………………………………………………………………………………………..Set
Normally the PF selects the TAKEOFF REF page.
Normally the PM selects the LEGS page.
MCP…………………………………………Set
AUTOTHROTTLE……………..ARM
V2 on IAS/MACH selector……..Set
LNAV…….………………As needed
VNAV if needed…………As needed
Initial HEADING…..……………..Set
Initial ALTITUDE……………………Set
MCP settings……………………………..Verify
ATC clearance
Receive ATC clearance in accordance with local airport regulations.
This procedure is regarded as part of the takeoff briefing.
ATC clearance…………………………….………………………………………….……….Receive
ATC clearance……………………….…………….………………………………………………Check
ATC clearance should be read by CM2 and checked by all crewmembers
Takeoff briefing………………………………………….…………………………….Complete PF
Before start procedure
Flight deck door closed/locked……Verify
Verify that the LOCK FAIL light is
extinguished.
Exterior doors closed…………………….Verify
Flight deck windows closed and locked………………………………………………………………Verify
Clearance to pressurize hydraulic system
from ground handling personnel …..Obtain
If pushback is needed:
Nose gear steering lockout
pin is installed……………….………….Verify
FUEL panel……………………………………….Set
If the center tank fuel quantity exceeds 460
kilograms:
LEFT and RIGHT CENTER
FUEL PUMPS switches…………………..ON
Verify that the LOW PRESSURE lights
illuminate momentarily and then extinguish.
If the LOW PRESSURE light stays illuminated
turn off the CENTER FUEL PUMPS switch.
AFT and FORWARD
FUEL PUMPS switches………..….………ON
Verify that the LOW PRESSURE lights are
extinguished.
HYDRAULIC panel…………………………….Set
ANTI COLLISION light switch………….ON
Each trim freedom of movement……Check
TRIM……………………………………..……Set
STABILIZER TRIM check – ___ UNITS
Set the trim for takeoff.
Verify that the trim is in the green band.
AILERON trim – 0 units
RUDDER TRIM – 0 units
Transponder………………………………ALT ON
Call: “REQUEST PUSHBACK / START UP
CLEARANCE”
ATC pushback / start up
clearance ………………………………..Obtain
Call: “BEFORE START CHECKLIST”
To expedite departure the BEFORE START
checklist may be done during the pushback.
BEFORE START checklist………..Perform
Pushback or towing procedure
The Engine Start procedure may be done during pushback or towing.
Communications with ground handling
personnel ………….………………Establish
CAUTION: Do not hold or turn the nose wheel tiller during pushback or towing. This can
damage the nose gear or the tow bar.
CAUTION: Do not use airplane brakes to stop the airplane during pushback or towing. This
can damage the nose gear or the tow bar.
PARKING BRAKE.……………..Set or release
Set or release as directed by ground handling
personnel.
WHEN PUSHBACK OR TOWING IS COMPLETED
Tow bar is disconnected…..…………Verify
Nose gear steering
lockout pin is removed……………….Verify
System A HYD PUMPS switches……….ON
Verify that the system A pump LOW
PRESSURE lights are extinguished.
Verify that the system A pressure is 2800 psi
minimum.
Engine start procedure
Announce start sequence for the ground
personnel:
“STARTING ENGINE № ____”
Normally №2 then №1.
Secondary engine display……………..Select
Air conditioning PACK switches………OFF
Call “START ENGINE № ___ “ Elapsed Time……..……………………….Start
CHRONO…………………………………..Start
ENGINE START switch……………………GRD
Verify that the N2 RPM increases.
When N1 rotation is seen and N2 is at 25%, or (if 25% N2 is not possible), at maximum
motoring and a minimum of 20% N2.
Note: Maximum motoring occurs when N2 acceleration is less than 1% in approximately
5 seconds.
Engine start lever……………………………IDLE
CAUTION: Do not apply rotational force when
moving the engine start lever.
SPAR VALVE CLOSED light
transitions from dim to bright and then
extinguishes…………………..………..Verify
Note: The check is considered failed if the
SPAR VALVE CLOSED light (located on the
fuel control panel) fails to illuminate bright
during the check.
FUEL FLOW and EGT indications……………..…………..……………………………..Monitor
At 56% N2:
ENGINE START sw. moves to OFF….Verify
If not:
ENGINE START switch………..Move to OFF
When the engine start switch moves to OFF:
START VALVE OPEN extinguishes…Verify
Call: “STARTER CUTOUT”
Monitor the engine start until stable at idle.
CHRONO…………………………………..Stop
N1, N2, EGT, FUEL FLOW AND OIL PRESSURE
for normal indications while the engine accelerates to a stable idle..……………..Monitor
Before taxi procedure
When engines are stable at idle and start limit redline EGT indication has extinguished
Ground personnel……………………Release
GENERATOR 1 and 2 switches………….ON
PROBE HEAT switches…………………….ON
WING ANTI–ICE switch………….As needed
ENGINE ANTI-ICE switches…..As needed
PACK switches…………………………….AUTO
ISOLATION VALVE switch…………….AUTO
APU BLEED air switch…………………….OFF
APU switch……………………………………..OFF
Engine START SWITCHES……………CONT
Ground equipment is clear……………………………………………………………………..Verify
Call: “FLAPS ___ “ as needed
MFD SYS switch………….……..……….Push
Flight controls……………………………….Check
FLAP lever……………………….Set as needed
LE FLAPS EXT green
light is illuminated……………………….Verify
Note: For Flight control check push the MFD SYS switch to display the flight control surface
position indications on the lower display unit, if desired. Make slow and deliberate
inputs, one direction at a time. Hold the nose wheel steering wheel during the rudder
check to prevent nose wheel movement. Move the control wheel, the control column
and the rudder pedals to full travel in both directions and verify:
Freedom of movement
That the controls return to center
Correct flight control movement
Lower display unit…….………………..Blank
RECALL…………………………………………………………………………………………………………..Check
Verify that all system annunciator panel lights illuminate and then extinguish.
EFB AIRPORT MAP application…………………………………………………………………As desired
EFB map application should be selected at least on one side.
CAUTION: Do not use the Airport Map application as a primary navigation reference. The
Airport Map application is designed to aid flight crew positional awareness only.
Call: “BEFORE TAXI CHECKLIST”
BEFORE TAXI checklist…………..Perform
ATC taxi clearance..…..…..…………Obtain
Taxi briefing(if needed)………………Update
TAXI and TURNOFF lights…………………..ON
Hand signal from
ground staff (pin in hand)…………….Receive
Clear of obstacles….…………………..Check
Hand signal from ground
staff (pin in hand)…….…………….Receive
Clear of obstacles….…….…………..Check
Call: “LEFT SIDE CLEAR,
VISUAL SIGNAL RECEIVED”
Call: “RIGHT SIDE CLEAR”
PARKING BRAKE…………………….Release
Before takeoff procedure
AFTER LEAVING THE APRON
WX radar……………………………………On
Ensure there is ground or weather return on
ND. WX radar should be on before takeoff at
least on one side (PF or PM).
WX radar………………………………….…..On
Ensure there is ground or weather return on
ND. If the WX radar failure suspected – perform
WX radar test, according to FCOM SP. WX
radar should be on before takeoff at least on
one side (PF or PM).
Additional takeoff briefing (PF for the flight).………………………………………………..As needed
WXR or TERR switch…………..As needed WXR or TERR switch…………….As needed
“CABIN READY”…………………………………………….………………………………Receive
The “READY” light should be extinguished prior departure as a feedback to cabin crew.
FLAPS takeoff setting………………………………………………………………………….Verify
RTP 1 STANDBY window
airborne frequency………………….Set / Verify
AT HOLDING POINT
Call: “BEFORE TAKEOFF CHECKLIST”
BEFORE TAKEOFF checklist……….Perform
WHEN CLEARED TO LINE UP
Runway and runway entry point are correct……….………………………………………Verify
Notify the cabin crew to prepare for takeoff:
FASTEN BELTS…………..twice OFF then ON
POSITION light…………STROBE & STEADY
Transponder………….………..…………TA/RA
Prior to entering the departure runway check that the approach path is clear of traffic, visually
and using TCAS display on ND.
The pilot in view of the approach sector verifies and calls “APPROACH PATH CLEAR”. The
other pilot verifies and calls “CHECK”.
Both pilots should vеrifу RAAS calls.
When the airplane is aligned with the runway
centerline ensure the nose wheel steering
tiller is released.
Airplane heading agrees with the assigned runway heading…………………………..Verify
Engine run up (when engine anti-ice is required and the OAT is 3°C or below)………Perform
Takeoff procedure
WHEN CLEARED FOR TAKEOFF Elapsed Time……………..……..……….Start LANDING light switches…………………ON RETRACTABLE lights (if any)…As needed Call: "TAKE OFF" Call: "YOU HAVE CONTROL" if CM2 is PF Call: "I HAVE CONTROL" if CM2 is PF Brakes are released……………………………………………………………………………Verify Thrust levers to approx. 40% N1…Advance Allow the engines to stabilize. Thrust levers to min 70% N1……..Advance Allow the engines to spool-up to approximately target N1. Verify T/O configuration warning not present and without delay: TO/GA switch……….…………………...Push PF PM FMA mode changes……………...........Verify FMA mode changes……………..Verify/Call Correct takeoff thrust is set………………………………………………………………….Verify Monitor the engine instruments during the takeoff. Call out any abnormal indications. Adjust takeoff thrust before 60 knots as needed. During strong headwinds, if the thrust levers do not advance to the planned takeoff thrust, manually advance the thrust levers before 60 knots. Call: "THRUST SET" CM1’s hand must be on the thrust levers until V1. Monitor airspeed. Maintain light forward pressure on the control column. Monitor airspeed and call out any abnormal indications. AT 80 KNOTS AIRSPEED Verify 80 knots and call "CHECK" Call: "EIGHTY KNOTS" FMA mode changes…………….Verify/Call V1 speed………………………………...Verify Verify the automatic V1 callout or call: "V1" AT VR AIRSPEED Call: "ROTATE" Monitor airspeed and vertical speed. At VR, rotate toward 15° pitch attitude. After liftoff, follow F/D commands. Special attention should be focused on PFD pitch indication. When pitch reaches 8 degrees by PFD with main gears still on the runway call: "PITCH EIGHT" Positive rate of climb……………..Establish Positive rate of climb on the altimeter….....................Verify Call: "POSITIVE RATE" Positive rate of climb on the altimeter………………...Verify Call: "GEAR UP" LANDING GEAR lever.……..………..Set UP AT 400 FEET RADIO ALTITUDE Above 400 feet radio altitude call for a roll mode as needed. Call: "FOUR HUNDRED FEET" Roll mode……….……………..Select / Verify VNAV engaged……………….………...Verify AT THRUST REDUCTION ALTITUDE CLIMB thrust is set………………..…………………………………………..……………....Verify Call: "CLIMB/R-CLIMB/CLIMB1/CLIMB2" AT ACCELERATION ALTITUDE Call: "ACCELERATION" LANDING GEAR position…………….Verify Verify acceleration at the acceleration height. Call: "FLAPS \_\_\_" according to the flap retraction schedule. Call: "SPEED CHECKED, FLAPS \_\_\_" FLAP lever……………………Set as directed Monitor flaps and slats retraction Engage the autopilot when above the minimum altitude for autopilot engagement. AFTER FLAP AND GEAR RETRACTION All steps are done……………………..Verify Engine BLEEDS…………………………...Sеt PACKS are operating..........................Verify Verify that DIFF PRESS is positive. ENGINE START switches……....As needed AUTO BRAKE selector…………............OFF LANDING GEAR lever.…………............OFF (when landing gear retraction is complete) Call: "AFTER TAKEOFF CHECKLIST" AFTER TAKEOFF checklist………..Perform
