A:Boeing 757-200
L:Initial Cockpit Inspection
Q:Aircraft Is Already Powered
R:Aircraft Powered
C:Battery Switch
R:ON
C:Standby Power Selector
R:AUTO
C:L/R Engine Hydraulic Pump Switches
R:ON
C:All Other Hydraulic Pump Switches
R:VERIFY OFF
C:APU Bleed Air Switch
R:OFF
C:APU Selector (see note)
R:START, THEN RELEASE TO ON
N:Only if required. Otherwise, skip to "Bus Tie Switches" check item.
B:            Aircraft Powered
C:Bus Tie Switches
R:AUTO
C:Utility Bus Switches
R:ON
C:L/R/Utility Bus Off Lights
R:VERIFY OFF
C:L/R Generator Control Switches
R:ON
C:Position and Wing Lights
R:ON
C:Cockpit Voice Recorder
R:TEST
N:Window illuminates and index needle deflects to far right side.
C:IRU Mode Selectors
R:NAV
N:Flight Displays will not function while IRU's are out of NAV mode. IRU's require approximately 10 minutes to align. Fly! II limitations do not permit this behavior to be modeled. If the IRU's are not in NAV mode, however, associated systems will be negatively affected.
C:FMC
R:ON, VERFIY, PROGRAM
L:FMS Initialization
C:Active NAV Database
R:VERIFY
N:Verify the active NAV database is current. See FMC Guide (Chapter 12) for detailed FMC instructions.
C:Reference Airport
R:ENTER
N:Enter the four letter ICAO airport code for the departure airport. See FMC Guide (Chapter 12) for detailed FMC instructions.
C:Gate
R:ENTER
N:Enter the departure gate. See FMC Guide (Chapter 12) for detailed FMC instructions.
C:IRS Position
R:SET, CONFIRM
N:Enter/confirm the current aircraft position location by downselect/upselect or manual entry. See FMC Guide (Chapter 12) for detailed FMC instructions.
C:UTC
R:VERIFY
N:Verify UTC/GMT time matches captains clock. See FMC Guide (Chapter 12) for detailed FMC instructions.
C:Flight Plan
R:ENTER, VERIFY
N:Use LOAD flight plan to load a saved flight plan, or use ORIGIN, DEST, and manual entry of waypoints to build route of flight on RTE 1 page. See FMC Guide (Chapter 12) for detailed FMC instructions.
L:Cockpit Preparation
C:R Electric Hydraulic Pump Switch
R:ON
C:R Electric Hydraulic PRESS Light
R:VERIFY OFF
C:Yaw Damper Switches
R:ON
C:Emergency Doors Light
R:OFF
C:Battery
R:CHECK
N:Rotate the standby power selector to BAT and observe the DISCH light comes on and the OFF light remains off. Rotate selector back to AUTO and verify that both lights remain off.
C:Fuel Quantity and Distribution
R:VERIFY
C:Fuel Pump Switches
R:ALL OFF
C:Crossfeed
R:VERIFY CLOSED
C:Engine Start Selectors
R:OFF
C:Ignition Selector
R:1 OR 2
N:If in 1, select 2. If in 2, select 1. This prevents wear on any single starter unit.
C:Emergency Lights Switch
R:ARMED
C:Window Heat Switches
R:ON
C:No Smoking Selector
R:ON
C:Seat Belts Selector
R:OFF
C:Pressurization Auto Rate Knob
R:AT INDEX MARK
C:Desitination Landing Altitude
R:SET
C:Mode Selector
R:VERIFY AUTO 1
C:Equipment Cooling Switch
R:NORMAL
N:Indicator is blank.
C:Engine Bleed Switches
R:VERIFY OFF
C:APU Bleed Switch
R:ON
N:Allow the APU to run for at least one minute before activating APU bleed air.
C:Isolation Switch
R:OPEN
N:Horizontal Bar
C:L/R Pack Selectors
R:AUTO
C:Trim Air Switch
R:ON
C:L/R Recirculation Fan Switches
R:ON
N:The Left Recirc fan must be ON to provide cooling to the Electronics Bay when the aircraft is not pressurized.
C:Flight Deck and Cabin Temp Control Selectors
R:AUTO
C:L/R flight Director Switches
R:ON
C:Autothrottle Arm Switch
R:VERIFY OFF
C:Bank Limit Selector
R:(Not operable this version)
C:Heading Selector
R:SET INITIAL HEADING
C:Altitude Selector
R:SET INITIAL ALTITUDE
C:Autopilot Disengage Bar
R:ARMED
N:The Autopilot Disengage Bar is armed when it is up.
C:Sliding Side Window
R:CLOSED AND LOCKED
C:Oxygen Mask/Regulator
R:TEST
C:Airspeed Indicator
R:CHECK
N:Observe that no flags are visible.
C:RMI
R:CHECK
N:Observe that no failure flags are visible in the face of the RMI.
C:ADI
R:CHECK
C:ADI Brightness
R:AS DESIRED
C:Decision Height
R:Remove
N:Remove by setting to a negative value. Located on throttle console.
C:Flight Director Attitude and Roll Bars
R:CHECK
C:FD and TO TO
R:ANNUNCIATED
C:HSI
R:CHECK
C:HSI Mode Selector
R:MAP
N:HSI Mode selector located on throttle console.
C:HSI Range Selector
R:AS DESIRED
C:HSI Brightness
R:CHECK
C:Heading and Track
R:CHECK
N:Observe the present heading and track appear at the top of the display and agree with the standby compass.
C:Autoland Status Annunciator
R:VERIFY BLANK
C:Altimeters
R:SET AND CROSSCHECKED
C:Vertical Speed Indicator
R:CHECK
C:Clock
R:CHECK
C:Reserve Brakes Switch
R:OFF
C:Standby Attitude Indicator
R:CHECK
N:Observe that no flags are showing and that a level attitude is displayed. Ensure Pitch Ladder setting matches current attitude displayed on ADI.
C:Standby Airspeed Indicator
R:CHECK
C:Standby Engine Indicator
R:VERIFY ON
C:Autobrakes Selector
R:SET TO RTO
C:EICAS Status Switch
R:PUSH
N:Located on throttle console.
C:EICAS Brightness
R:AS DESIRED
C:Oxygen Quantity
R:CHECK
C:Hydraulic Quantity
R:CHECK
C:Engine Switch
R:PUSH
N:Located on throttle console.
C:Engine Indicators
R:CHECK
N:Observe all indications are normal for shut-down conditions.
C:Engine Oil Quantity
R:CHECK
C:Alternate Flap System
R:OFF
C:Alternate Gear Extend Switch
R:GUARDED, OFF
C:Ground Proximity Flap/Gear/Config Setting Overrides
R:GUARDED, OFF
C:Speed Brake Lever
R:DOWN
C:Throttles
R:CLOSED
C:Fuel Control Switches
R:CUTOFF
C:Parking Brake
R:SET
N:The actual 747 parking brake is more complicated and does not twist. Not all users have toe-brake capability, so the modeling has been simplified.
C:Weather Radar
R:TEST
N:Weather Radar functionality not available in this version.
C:COMM Radios
R:SET
C:ADF
R:SET
C:VNF NAV Radios
R:SET
C:Aileron Trim
R:CENTERED
C:Rudder Trim
R:CENTERED
C:Transponder
R:STANDBY
C:SQUAWK CODE
R:ENTER
C:Seat and Rudder Pedals
R:ADJUST AS DESIRED
L:Final Cockpit Preparation
C:APU
R:START
N:Only if not running.
C:FMC PERF Runway and Departure Procedure
R:ENTER
C:FMC PERF Flight Plan Route
R:VERIFY
C:FMC PERF Zero Fuel Weight
R:VERIFY/ENTER
C:FMC PERF Reserve Fuel
R:VERIFY/ENTER
C:FMC PERF Cost Index
R:(Not Modeled)
C:FMC PERF Cruise Altitude
R:ENTER
C:FMC PERF OAT At Top Of Climb
R:ENTER
C:FMC VNAV CLB Page
R:PROGRAM
N:Program the Clean Maneuvering Speed restriction for VNAV used below 5000.
C:Takeoff Data
R:LOOK UP/SET
N:Use Flight Manual and Speed Cards (on throttle console) to determine V1, Vr, V2 and flap retraction speeds. Program V1, Vr and V2 into FMC to set speed bugs on airspeed indicator.
C:Trim Setting
R:LOOK UP/SET
N:Use Flight Manual to determine preferring Trim Setting.
C:IAS/MACH Speed Bug
R:SET V2 IN WINDOW
C:ILS
R:PARK
N:Rotate ILS frequency knob until dashes appear in tuner window.
C:EHSI
R:SET
N:Select MAP mode and set range as needed. Observe the display of the planned takeoof runway, any tuned VOR stations and the active flight plan on the display. Flight plan route should be solid magenta track unless discrepancies exit in FMC programmed route. Use the NAV AID, AIRPT, RTE DATA and WPT buttons to add additional information to the MAP screen to enhance situational awareness.
C:Hydraulic Pumps
R:ON
N:Turn on the center ELEC2 pump and observe the assoicated pressure lights extinguish. Then turn on the center ELEC1 pump and left ELEC pump and observe the associated pressure lights extinguish. Note: ELEC2 PRESS light illuminates when ELEC1 switch is activated.
C:Fuel Pumps
R:ON FOR ALL TANKS CONTAINING FUEL
N:Center tank PRESS lights will remain illuminated until associated engine is started.
C:Seat Belt Selector
R:ON
C:STAB Trim Setting
R:VERIFY IN GREEN ARC
Z:Before Start Checklist
L:Pushback and Start
C:Pushback/Start Clearance
R:OBTAIN
Z:Before Pushback Checklist
C:Red Anti-Collision Beacon
R:ON
C:Pack Selectors
R:OFF
L:Engine Start
C:Start Engine Number ___
R:ANNOUNCE
C:Engine Start Selector
R:ROTATE TO GROUND (GND)
N:At 25% N2 or stable N2, proceed to next.
C:Fuel Control Switch (Located behind Throttles)
R:RUN
N:(1) At approximately 50% N2, verify that START SELECTOR has returned to RUN. The START SELECTOR will make an audible 'click' when moving. (2) Verify engine reaches ground idle (N2 approximately 60-63%) within 90 seconds.
C:Start Engine Number ___
R:ANNOUNCE
C:Engine Start Selector
R:ROTATE TO GROUND (GND)
N:At 25% N2 or stable N2, proceed to next.
C:Fuel Control Switch (Located behind Throttles)
R:RUN
N:(1) At approximately 50% N2, verify that START SELECTOR has returned to RUN. The START SELECTOR will make an audible 'click' when moving. (2) Verify engine reaches ground idle (N2 approximately 60-63%) within 90 seconds.
L:After Start
C:Electrical Power Transfer
R:VERIFY
N:Observe that both GEN CONT OFF lights have extinguished, indicating that engine generators are producing electrical load.
C:APU
R:SHUTDOWN
C:ENG ANTI-ICE Switches
R:AS REQUIRED
N:If engine anti-ice is to be used for takeoff, or whenever taxiing through blowing snow, loose snow or visible moisture while OAT is < 10 C, activate engine anti-ice at start of taxi.
C:L/R Engine Bleed Switches
R:ON
C:APU Bleed Switch
R:OFF
C:Isolation Switch
R:CLOSE (NO BAR)
C:L/R Pack Selectors
R:AUTO
C:EICAS Display Assumed Temperature
R:SET
N:Note that if a takeoff is to be made using reduced takeoff thrust, the assumed temperature must be set after engine start. After setting, verify displayed EPR using FMC or flight manual.
C:EICAS Status/Alert Messages
R:CHECK
C:Release from Pushback/Ground Service
R:VERIFY
C:Flaps
R:SET
L:Taxi Out
C:Flight Controls
R:CHECK
N:Select STATUS mode on the lower EICAS and confirm flight control movements on all axes.
C:EICAS Engine Display
R:SET
Z:Before Takeoff Checklist 1
C:Takeoff Performance
R:CONFIRM
N:Verify takeoff performance speeds to determine if still acceptable. If aircraft weight changed during boarding/departure period, ensure that speeds are updated and accurate.
C:FMC Takeoff Settings for Pilot Flying
R:CLB PAGE
N:Verify that the ACT LIM SPD CLB page is displayed.
C:FMC Takeoff Settings for Pilot Not Flying
R:DIRECT/INTC PAGE
N:Push the DIR INTC key to display the ACT RTE 1 LEGS page with the DIRECT TO and INTC LEG prompts.
Z:Before Takeoff Checklist 2
C:Cabin Crew Takeoff Notification
R:PROVIDE
P:Cleared Onto Active Runway
C:Autothrottle Arm Switch
R:ARM
C:Transponder
R:SET TA OR TA/RA
Z:Before Takeoff Checklist 3
L:Takeoff
C:Wing Lights
R:ON FOR INCREASED VISIBILITY
C:Strobe Lights
R:ON
C:HDG Indicator
R:SET
N:Set assigned departure heading or runway heading.
C:Parking Brake
R:VERIFY RELEASED
C:Takeoff Thrust
R:SET
C:Engine Indications
R:MONITOR
C:Airspeed 80 knots
R:ANNOUNCE
C:Airspeed V1
R:ANNOUNCE
C:Airspeed Vr
R:ANNOUNCE
C:Initial Climb
R:ESTABLISH
C:Positive Rate of Climb
R:VERIFY
N:Target speed for climb is V2 + 15 KIAS. Rotate the airplane until this speed is achieved, but do not rotate over aggresively, as aft fuselage contact with the runway may occur.
C:Gear
R:UP
L:After Takeoff
C:Roll Mode
R:SET HDG OR LNAV
N:Select either the heading or Lateral Navigation modes to provide steering cues to the flight director. Verify expected mode annunciations on ADI.
P:800 Feet Above Takeoff Field Elevation
C:FLAPS
R:RETRACT ON SCHEDULE
C:PITCH MODE
R:SET VNAV OR FLCH
N:Verify CLB is displayed as the active thrust limit on the upper EICAS and that the throttles adjust to climb thrust. If seleting VNAV, observe the command airspeed bug responds and that EPR and VNAV SPD are annunciated on the ADI. If selecting FLCH, set the IAS/MACH indicator to clean maneuvering speed and verify that FLCH and SPD are annunciated. Note: if CLB does not activate automatically, press the CLB switch to the right of the upper EICAS to force the thrust limit mode in the CLB.
P:1200 Feet Above Takeoff Field Elevation
C:Autopilot
R:ON AS DESIRED
C:Engine Start Selectors
R:AUTO
N:If CONTINUOUS ignition was used for takeoff, select AUTO when no longer needed.
C:Anti-Ice Switches
R:AS REQUIRED
Z:After Takeoff Checklist
L:Climb
C:VNAV
R:SELECT AS DESIRED
N:Push the VNAV switch and verify VNAV SPD is displayed on the ADI.
C:Cleared Altitude
R:VERIFY SET IN MCP WINDOW
C:LNAV
R:SELECT AS DESIRED
N:When cleared to resume own navigation by the assigned flight route and the aircraft is on an intercept heading for the assigned route, push the LNAV switch and verify that LNAV is annunciated on the ADI.
C:Wing/Engine Anti-Ice
R:SELECT AS REQUIRED
P:10,000 Feet.
C:ECON CLB MODE
R:VERIFY ACTIVE
N:Observe the ACT ECON CLB page displayed on the FMC, or selected MCP speed if applicable. Ensure commanded speed agrees with the displayed values.
C:Cabin Signs
R:AS REQUIRED
P:Transition Altitude
C:Altimeters
R:SET AND ANNOUNCE QNE (29.92 in. Hg or 1013 hPa)
P:FL180
C:Landing Lights
R:OFF
C:Wing Lights
R:OFF
L:Cruise
C:Level Off
R:PERFORM
C:Flight Progress, Performance and Navigation
R:MONITOR
C:Fuel System
R:MONITOR
L:Initial Approach
C:ATIS
R:OBTAIN
C:Approach Briefing
R:ACCOMPLISH
C:ADI Decision Height/MDA Bug
R:CHECK AND SET
C:Landing Data
R:CHECK AND SET
N:Determine correct REF speed for the planned landing weight and flap setting. Verify values against FMC computed values, the adjust or acept FMC computed figures.
C:Seatbelt Selector
R:ON
P:FL180
C:Wing Lights
R:AS REQUIRED
P:Transition Altitude
C:Altimeters
R:SET AND ANNOUNCE QNH
C:Flaps
R:AS REQUIRED
N:Expect varying speed vectors during the approach phase of the flight. When a flap level is selected, set MCP speed to the flap maneuver speed + 10 knots. Do not use the flaps as air brakes to slow the aircraft; rather, slow the aircraft using appropriate throttle input and extend the flaps according to the flap deployment schedule.
Z:Approach Checklist
L:Final Approach
C:Autoflight Systems
R:AS REQUIRED
C:Localizer Capture
R:ANNOUNCE AS REQUIRED
C:Landing Gear
R:DOWN AND VERIFY
C:Speed Brake
R:VERIFY CLOSED
Z:Final Approach Checklist
C:Guide Slope Capture
R:ANNOUNCE AS REQUIRED
C:MCP Altitude
R:SET
N:If flying an ILS, set Missed Approach altitude after glideslope capture. If flying a non-precision approach, set the MDA altitude after aircraft has leveld at initial approach altitude, but BEFORE crossing the final approach fix. At FAF, use V/S as a descent mode to command the airplane down to MDA. Once reaching MDA, set the missed approach altitude in the MCP window.
C:Autoflight System
R:MONITOR AS REQUIRED
N:If flying an autoland approach, observe at 1500 radar altitude that LAND3 or LAND2 are annunciated, along with FLARE and ROLLOUT modes being displayed as armed.
L:Taxi In
C:Spoilers
R:VERIFY RETRACTED
P:Clear of the Active Runway
C:Landing Lights
R:OFF
C:White Anti-collision Lights
R:OFF
C:Flight Director Switch
R:OFF
C:Flaps
R:RETRACT
C:Stabilizer Trim
R:6 UNITS
C:Weather Radar
R:OFF
C:APU
R:AS REQUIRED
C:Engine And Window Anti-Ice Switches
R:OFF
L:Parking and Shutdown
C:Parking Brake
R:SET
C:Seatbelt Selector
R:OFF
C:Engine Bleed Switches
R:OFF
N:Observe VALVE lights illuminate.
C:Ground/External Power Generator
R:WHEN AVAILABLE, SELECT ON
N:Only if APU OFF. Otherwise, skip to next checklist item.
C:APU GEN CTRL Switch
R:CUTOFF
N:Only if APU ON. Otherwise, skip to next checklist item.
C:L/R Fuel Control Switch
R:CUTOFF
N:After completing APU ON/OFF checkitems proceed with checklist normally.
C:Hydraulic Pumps
R:OFF
C:Fuel Pump Switches
R:OFF
C:Red Anti-Collision Light Switch
R:OFF
C:Exterior Lights
R:AS REQUIRED
C:Pneumatics Panel APU Bleed Switch
R:ON
C:Pneumatics Panel Isolation Switches
R:OPEN
Z:Parking Checklist
L:Leaving Aircraft
C:Pneumatics Panel Pack Selectors
R:OFF
C:Pneumatics Panel UPR and LWR RECIRC FANS
R:OFF
C:Pneumatics Panel APU Bleed Switch
R:OFF
C:APU Selector
R:OFF
N:Allow APU to run without bleed or generator load for at least 1 minute before shutting down.
C:STBY Power Selector
R:OFF
C:BAT Switch
R:OFF
L:Before Start Checklist
X+
L:Before Pushback Checklist
L:Before Takeoff Checklist 1
L:Before Takeoff Checklist 2
L:Before Takeoff Checklist 3
L:After Takeoff Checklist
L:Approach Checklist
L:Final Approach Checklist
L:Parking Checklist
