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Boeing 737-800

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MTOW

Maximum Takeoff Weight
79 016 kg
174 200 lbs

MZFW

Maximum Zero Fuel Weight
62 732 kg
138 300 lbs

MLW

Maximum Landing Weight
66 361 kg
146 300 lbs

OEW

Operating Empty Weight
41 413 kg
91 300 lbs

FLIGHT CEILING

41 000 ft

Flight ceiling

SEATING CAPACITY

Maximum Passenger Capacity
184 economy
160 two-class

MFC

Maximum Fuel Capacity
20 894 kg
46 063 lbs

FLIGHT CEILING

41 000 ft

Flight ceiling

RANGE

3 115 nm

RANGE

3 115 nm

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PRELIMINARY SAFETY INSPECTION 1/2

FP FILED IN SIMBRIEF
FP UPLOADED TO PDMG FOLDER
BATTERY ON
ELECTRIC HYDRAULIC PUMP
OFF
LANDING LEVER
OFF
GROUND POWER
FIRETEST
EMERGENCY EXIT LIGHTS
TEST CABIN ATTEND CALL
FLAPS
RETRACTED
TAKE OFF OPERATION WARNING TEST
CARGO FIRE SYSTEM TEST
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PRELIMINARY SAFETY INSPECTION 2/2

MANUAL GEAR EXT. ACCES DOOR
CLOSED
CIRCUIT BRAKERS
ALL IN
EMERCENCY ESCAPE ROPE
IN PLACE
FLIGHT RECORDER TEST
MACH AIRSPEED WARNING TEST (2X)
STALL WARNING TEST (2X)
ENGINE PANEL
NO LIGHTS
EEC PANEL
ON AND GUARDED
PASSSENGER OXYGEN SWITCH
GUARDED/NO LIGHT
OXYGEN PRESSURE
SUFFICIENT (>15)
SERVICE INTERPHONE SWITCH
OFF
GPS LIGHT
OFF
PSU LIGHT
OFF
IRS MODE SELECTOR TO NAV
ELEC. HYDR. PUMPS (BEFORE WALK AROUND)
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Loading aircraft (PMDG)

FS ACTIONS
FUEL
PAYLOAD
GROUND SERVICES > AIRPLANE SERVICES (2/4)
FUEL TRUCK
BLOCK FUEL
FUELING
GROUND SERVICES > PASSENGER SERVICES (3/4)
STAIRS 2L
PAX
PAX BUS
BOARDING
ROUND SERVICES > BAGGAGE HANDLING (4/4)
FWD LOADER
FWD CARTS
CARGO
LOADING
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FMC SETUP 1/2

IDENT PAGE
ENGINGE RATING
NAV DATA UP-TO-DATE
POS INIT PAGE
IRS POSITION
RTE PAGE (1/2)
DEPARTURE AIRPORT
DESTINATION AIRPORT
FLIGHT NUMBER
RUNWAY
DEPARTURE PAGE
RUNWAY
SID
RTE PAGE (2/2)
ROUTE
ARRIVAL PAGE
APPROACH
STAR
RTE PAGE
ROUTE
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FMC SETUP 2/2

PERF INIT PAGE
COST INDEX
RESERVES(+ALTN)
ZFW
FLIGHT LEVEL
CRZ WIND
T/C ISA TEMP (i.e. M007 in SB > subtract another 7)
TRANS ALTITUDE (+1)
FIX INFO PAGE (1/2)
DEPARTURE AIRPORT
HOLDING DISTANCE FOR ENGINE FAILURE
ECON DESC PAGE (1/2)
SPD RESTR. BELOW FL100 (EU: 250 knts)
DES FORECAST PAGE
TRANS LEVEL AT ARRIVAL
QNH
ISA DEV = TEMP -/- (15 -/- 2 x ALT ARR/1000)
3 x ALT (example 300-200-100)
3 x DIR/SPD (SIMBRIEF: WIND INF > DESCENT)
LEGS PAGE
DISCONTINUITY
BYPASS? (yes, reduce speed i.e. 220B/)
ROUTE
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PRE-FLIGHT 1/8

MAIN PANEL
LIGHT TEST (ON/OFF)
OXYGEN TEST
PRESS TEST BUTTON ONCE
PRESS RED BUTTON
PRESS TEST BUTTON 5sec
EFIS CONTROL PANEL
TFC - RANGE 10 NM
TFC ON
TERRAIN OVERLAYS ON
DISPLAY AIRPORT (ARPT) ON
BARO hPA (EU) or inHG (US)
QNH
MINIMUM FLAP RETRACTION ALTITUDE [MFRA - i.e. 1000ft above airfield, set with Baro selector]
WEATHER RADAR OFF
COPY TO RIGHT EFIS PANEL
MAIN PANEL
CLOCK AT UTC? (if neccessary push time/date button)
NOISE WHEEL STEERING SWITCH GUARDED (BELOW CLOCK)
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PRE-FLIGHT 2/8

OVERHEAD PANEL
// first left column:
FLT CONTROL SWITCH GUARDED
GUARDED
SPOILER SWITCH
GUARDED
ALTN FLAP EXTENSION
GUARDED/SWITCHED OFF
LIGHTS EXEPT YAW DAMPER
OFF
YAW DAMPER
NAVIGATION/DISPLAY SWITCHES
MIDDLE POSITION
SOURCE SWITCHES
AUTO POSITION
FUEL FOUR LIGHTS
DIM POSITION (NOT BRIGHT)
TEST CROSS FEED VALVE OPERATION
FUEL PUMPS ONWhen less 453 kg (1000 pounds) in center tankturn only wing tank in pre-flight
// second left column:
BATTERY SWITCH
GUARDED
GALLEY SWITCH
ON
STANDBY POWER SWITCH
GUARDED
IDG DISCONNECT SWITCHES
GUARDED
GENERATOR BUS TRANSFER
GUARDED
WIPER (L)
SET TO PARK
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PRE-FLIGHT 3/8

// middle column:
LIGHTS AS REQUIRED
EQUIPMENT COOLING SWITCHES
NORMAL (up position)
EMERGENCY EXIT LIGHT
GUARDED
SEAT BELT SIGN ON (when fueling is completed)
WIPER (R)
SET TO PARK
// next right column:
WINDOW HEAT SWITCHES ON (4X)
PROP HEAT SWITCHES
AUTO (up position) unless outside temp is 3 degree or less and there is visible precipitation
WING ANTI-ICE SWITCHES
OFF
ELECTRIC HYDRAULIC PUMP SWITCHES (4X)
ON
LOW PRESSURE ENGINE PUMP LIGHTS
ILLUMINATED
DIFFERENTIAL PRESSURE
AT ZERO
CABIN PRESSURE IN ALTITUDE
CHECKED
CABIN RATE OF CLIMB
AT ZERO
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PRE-FLIGHT 4/8

// most right column:
AIR TEMP SELECTOR TO FWD OR AFT POSITION
TRIM AIR
CONT CABIN TEMP TO POSITION A(UTO)
CABIN TEMP TO POSITION A(U)UTO
AFT CABIN TEMP TO POSITION AU(T)O
RECIRCULATION FAN
AUTO
PACKS TO AUTO
ISOLATIOM VALVE
OPEN
ENGINE BLEED
ON
APU BLEED
OFF
CRUISE FLIGHT LEVEL ON CABIN PRES. COMP.
LANDING ALTITUDE ON CABIN PRES. COMP.
PRESSURIZATION MODE SELECTOR
AUTO
ALTERNATE OR MANUAL LIGHT
NOT ILLUMINATED
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PRE-FLIGHT 5/8

// light switches (below-right):
POSITION LIGHT SWITCH TO STEADY
WHEEL WELL LIGHT ON (ONLY WHEN DARK)
LOGO LIGHT ON (ONLY WHEN DARK)
WING LIGHT
OFF
ANTI-COLLISION LIGHT
OFF
// engine switches (below-middle):
ENGINE START SWITCHES
OFF
IGNITER TO RIGHT POSITION (when maintaince available)
APU AS NEEDED
// light switches (below-left):
TAXI LIGHTS
OFF
RUNWAY TURNOFF LIGHTS
OFF
LANDING LIGHTS
OFF
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PRE-FLIGHT 6/8

MODE CONTROL PANEL (MCP):
FLIGT DIRECTOR ON (first left, then right)
COURSES AT DEPARTURE (inbound/outbond VOR)
SELECTOR SPEED: at 100 knots (V2 comes later)
SELECTOR HEADING: at runway heading
SELECTOR ALT: at expected first cleared alt. +100ft
RESET FUEL FLOW
AUTOBRAKE TO RTO
THRUST LEVER QUADRANT:
SPEEDBRAKER
DOWN DETENT
FLAP LEVER
UP
TAKE-OFF CONFIG CHECK
PARKING BRAKE
ENGINE START LEVERS
CUT OFF
STAB. TRIM CUT OFF SWITCHES
UP AND GUARDED
FIRE CONTROL PANEL:
OVERHEAT DETECTOR LOOPS
NORMAL POSITION
SWITCHES
NOT PULLED
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PRE-FLIGHT 7/8

PEDESTAL LEFT PANEL:
//radio control panel:
COM1-ACTIVE: FREQ. ATC DELIVERY
COM1-STANDBY: FREQ. ATC GROUND
COM2-ACTIVE: FREQ. EMERGENCY (121.5)
COM2-STANDBY: FREQ. ATIS
NAV1-ACTIVE: FREQ. DEP. RUNWAY ILS
NAV1-STANDY: FREQ. VOR1
NAV2-ACTIVE: FREQ. VOR1
NAV2-STANDBY: FREQ. DEP. RUNWAY ILS
//audio control panel:
VHF1 RADIO: INCREASE VOLUME (turn clockwise)
FLT (interphone): INCREASE VOLUME
SPRK: INCREASE VOLUME
PUSH TO TALK SWITCH
AT MIDDLE POSITION
MASK BOOM SELECTOR
AT BOOM POSITION
FILTER SWITCH
B POSITION
ALT/NORM SWITCH
NORM POSITION
//ADF panel:
ADF
SET AS NEEDED
//lights panel:
LIGHTS
SET AS NEEDED
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PRE-FLIGHT 8/8

PEDESTAL MIDDLE PANEL:
CARGO FIRE DETECTOR LOOPS
BOTH IN NORMAL
//weather radar:
WEATHER AND TURBULANCE MODE
GAIN AT MIDDLE POSITION (2X)
//transponder:
SQUAWK (STANDARD)
MODE SELECTOR TO STANDBY POSITION
LEFT TWO SELECTORS
SYSTEM 1 (LEFT SEAT)
//trim panel and trim indicator:
RUDDER TRIM INDICATOR
CENTERED
ELEVATOR TRIM INDICATOR
CENTERED
TEST AILORON TRIM SWITCH
TEST RUDDER TRIM SWITCH
PEDESTAL RIGHT PANEL:
RADIO PANEL
OK?
AUDIO CONTROL PANEL
OK?
THIRD RADIO PANEL
SET TO DATA MODE
STAB TRIM OVERRIDE SWITCH
GUARDED
FLIGHT DOOR SELECTOR
SET TO AUTO
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FINAL CDU PREFLIGHT AND TAKEOFF PERFORMANCE CALCULATION

N1 LIMIT PAGE
SELECT 22K RATING
SELECT ASSUMED TEMP (NORMAL: 30-55 DEG)
TAKE0FF REF PAGE
FLAPS (NORMAL: 5)
CENTER OF GRAVITY(CG)
TRIM
V1/VR/V2 SPEEDS
V2 ON MCP
REQUEST:
IFR CLEARANCE
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BEFORE REQUESTING PUSHBACK

SELECTOR ALT: at first cleared altitude
FMC ROUTING
CHECKED
TRANSPONDER
APU
REMOVE GROUND SERVICES (EXCEPT GPU)
APU GENERATOR SWITCHES (2X)
REMOVE GPU
PARKING BRAKE
ON
REMOVE WHEEL CHOCKS
PRE-PLAN PUSHBACK
CHECK:
TAXI ROUTE BRIEFED AND READY
DOORS CLOSED
GROUND EQUIPMENT CLEAR
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PREFLIGHT CHECKLIST

CHECKLIST:
alternatetext
REQUEST:
PUSHBACK CLEARANCE
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BEFORE PUSHBACK AND START

PACKS
APU BLEED
ANTI-COLLISION LIGHT
TRANSPONDER
ALT OFF
NO SMOKING SIGN
MASTER CAUTON WARNING
BEFORE START CHECKLIST:
alternatetext
PARKING BRAKE
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ENGINE START

ENGINE 2 START (AFTER PASSING GATE LINE):
ENGINE 2 START SWITCH
GND
AT 25% N2 - ENG 2 FUEL LEVER
ON
CHECK: VALVES STATUS (FIRST BRIGHT THEN OFF)
ENGINE 2 STATUS (2-4-6-3)
ENGINE 1 START:
ENGINE 1 START SWITCH
GND
AT 25% N2 - ENG 1 FUEL LEVER
ON
CHECK: VALVES STATUS (FIRST BRIGHT THEN OFF)
ENGINE 1 STATUS
ENGINE GENERATORS 1 & 2
APU
AFTER PUSHBACK
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BEFORE TAXI

ENGINE START SWITCHES
PROBE HEAT
ANTI-ICE
PACKS
ISOLATION VALVE
APU BLEED
ENGINE 1 & 2 BLEEDS
ON
FLAPS
ENGINE DISPLAYS MONITORED AND CLOSED
FLIGHT CONTROL CHECK
RECALL
alternatetext
CHECK:
REQUEST TAXI CLEARANCE
PREPARE TOWER FREQUENCY
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TAXI START

PREPARE DEPARTURE FREQUENCY
TAXI SPEED LIMIT:
APRONS
15 KNOTS
SHARP TURNS
10 KNOTS
STRAIGHT TAXIWAYS
30 KNOTS
BACKTRACK RUNWAY
50 KNOTS
CONTAMINATED SURFACE
5 KNOTS
TAXI LIGHTS
RWY TURN-OFF LIGHTS
PARKING BRAKE
TAKE-OFF CONFIG CHECK (70% N1)
START TAXI
FIRST 30-40 N1, THEN IDLE
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TAKE-OFF REVIEW

RUNWAY
XX
FLAPS
5
PAX
AUTO
BLEEDS
ON
ANTI-ICE
AS REQUIRED
TAKE-OFF SPEED
AS REQUIRED
INITIAL CLIMB ALTITUDE
AS REQUIRED
CONTACT DEPARTURE CONTROL
WHEN ADVISED BY ATC
alternatetext
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BEFORE TAKE-OFF

AT THE HOLD:
PARKING BRAKE
TAXI LIGHTS
CABIN LIGHTS
REQUEST TAKE-OFF / LINE UP CLEARANCE
AFTER LINE UP / TAKE-OFF CLEARANCE:
PREPARE CENTER FREQUENCY
STROBE LIGHTS
(FIXED) LANDINGS LIGHTS
AUTO THROTTLE
LNAV
TRANSPONDER
TAKE-OFF CONFIG CHECK (70% N1)
AFTER TAKE-OFF CLEARANCE:
TAXI LIGHTS
CLOCK TIMING (button left below)
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TAKE-OFF

TAKE-OFF PROCEDURE:
STABILIZE N1
40 PERCENT
TOGA
SET
SLIGHT FORWARD PRESSURE YOKE
UNTIL 80 KNTS
ROTATE
AT V1
WHEN POSITIVE RATE OF CLIMB
GEAR UP
INITIAL PITCH
7-9 DEGREES
AT 7.5 DEGR. PITCH
PULL MORE TO CONT. CLIMB
CLIMB OUT PITCH
15-18 DEGREES
LNAV ABOVE 400 FT
CHECKED
> 1000FT CLIMBING (ABOVE WHITE BAND)
AP ON
BUG UP
AT UP SPEED
PITCH DECREASES & TREND VECTOR VISIBLE & ABOVE WHITE DOT
FLAPS TO 1
PASSING FLAP 1 INDICATOR
FLAPS UP
LESS 1000FT TO LEVEL OFF ALTITUDE & NO FLAP LIGHT
REDUCE VS TO 1000
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AFTER TAKE-OFF

LANDING GEAR
AUTO BRAKES
ENGINE START SWITCHES
TAXI LIGHTS & RETR. LANDING LIGHTS
alternatetext
AFTER LEVEL OFF ALTITUDE
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CLIMB

AFTER FURTHER CLIMB CLEARANCE:
DIAL ALTITUDE UP
PRESS ALT. INV.
WHEN AIR TEMP LESS 10 DEGR.
ENGINE ANTI ICE ON
PASSING TRANSITION ALTITUDE:
SET ALTIMETER TO STD
+++
DIAL ALTITUDE UP
ALTIMETER
PASSING 10,000ft:
LANDING LIGHTS
CABIN PRESSURE
SEATBELT SIGNS
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CRUISE

ATIS
ARRIVAL DATA
LANDING ALTITUDE
RADIOS
LOCALIZER FREQ
LOCALIZER COURSE
RESET MCP ALTITUDE
RADIO ALT / BARO MIN
APPROACH & MISSED APPROACH
CHECK:
PREPARE LANDING & ARRIVAL PERF.
ARRIVAL TAXI ROUTE BRIEFED
PREPARE ARRIVAL FREQUENCY
ARRIVAL FREQUENCY STANDBY
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DESCENT

ANTI-ICE
ARRIVAL ALTIMETER
AUTOBRAKE
RECALL
PASSING TRANSITION ALTITUDE:
SET LOCAL QNH/QFE
ALTIMETER
PASSING 10,000ft:
MANUAL DESCENT BELOW 10.000:
- spd 220-flaps 5-spoilers on, or
- spd 180-flaps 10-spoilers on.
FLAPS:
-flaps 1 at UP indicator (13nm-10nm)
-flaps 5 at 1 indicator, appr. glidescope (10nm-9nm)
*** when glidescope start, set SPD af flap 5 speed ***
-flap 15 at 4/5nm and gear down.
*** set SPD af flap 15 speed ***
-flap 30
*** set SPD af vref+5 ***
LANDING
pitch around degrees;thrust 50%
*** when under glidescope, increase pitch slightly 3 degrees
flare at 30ft increase pitch to 5 degrees
LANDING LIGHTS
CABIN PRESSURE
PAX SIGNS
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BEFORE LANDING

ALTIMETER
LOCALIZER FREQ
LOCALIZER COURSE
ENGINE START SWITCHES
CHECK:
PREPARE TOWER FREQUENCY
TOWER FREQUENCY STANDBY
SPEED BRAKE
APP
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LANDING

GO-AROUND ALTITUDE
SPEED BRAKE
FLAPS
LANDING GEAR
AUTOPILOT
AUTOTHROTTLE
LANDING CLEARANCE RECIEVED
TAXI LIGHTS ON
TAXI LIGHTS
CHECK:
PREPARE GROUND FREQUENCY
GROUND FREQUENCY STANDBY
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AFTER LANDING

TRANSPONDER
FLAPS
SPEED BRAKE
LANDING LIGHTS
POSITION LIGHTS
TAXI LIGHTS
ANTI-ICE
APU
PROBE HEAT
ENGINE START SWITCHES
AUTO-BRAKE
APU GEN
TURNING INTO GATE
RUNWAY TURNOFF LIGHTS
OFF
TAXI LIGHTS
OFF
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SHUTDOWN

PARKING BRAKES
ENGINE FUEL LEVERS
PAX SIGNS
APU BLEED
ANTI COLLISION LIGHT
FUEL PUMPS
ANTI-ICE
ELEC. HYDRAULIC PUMPS
ISOLATION VALVE
FLIGHT DIRECTORS
GROUND POWER
EXTERIOR LIGHTS
DEBOARDING
REQUEST JETWAY/STAIRS
OPEN DOORS
DEBOARDING
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