Boeing 737-800 Procedure Checklist - Kennair Flight Simulator

Boeing 737-800 Procedure Checklist Page 2 of 4 [email protected] – March 2015 FLIGHT INSTRUMENTS CHECK NO FLAGS, FMA BLANK, FD ISOLATION VALVE...

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Boeing 737-800 Procedure Checklist ELECTRICAL POWER UP Procedure BATTERY SWITCH GUARD CLOSED STANDBY POWER GUARD CLOSED ALTERNATE FLAPS GUARD CLOSED WIPER SELECTOR PARK ELEC HYD PUMPS OFF LANDING GEAR LEVER DOWN If External Power is needed: GND PWR AVAIL GND PWR SWITCH ON If APU Power is needed: Verify ENG1, APU, ENG2 fire switch IN OVERHEAT DET SWITCH NORMAL TEST SWITCH Hold to FAULT/INOP OVHT/DET & APU DET Verify Illuminated INOP LIGHT TEST SWITCH Hold to OVHT/FIRE MASTER FIRE WARN PUSH EXTINGUISHER TEST CHECK TEST SWITCH POS TO 1 HOLD then RELEASE (repeat for 2) APU START APU GENERATOR BUS ON WHEEL WELL FIRE TEST FIRE BELL CUTOUT PUSH PRELIMINARY PREFLIGHT Procedure (Capt or FO) IRS MODE SELECTORS OFF, then NAV VOICE REC SWITCH ON PSEU LIGHT EXTINGUISHED GPS LIGHT VERIFY EXTINGUISHED SERVICE INTERPHONE OFF ENGINE PANEL SET OXYGEN PANEL SET LANDING GEAR LIGHTS VERIFY ILLUMINATED FLIGHT REC SWITCH GUARD CLOSED PARKING BRAKE ON CDU PREFLIGHT Procedure The initial data and Nav data entries must be completed before the Preflight Procedures. Performance Data entries must be complete before the Before Start Checklist CDU PREPARATION ENTER DATA PREFLIGHT Procedure - FO FLIGHT CTRL PANEL CHECK NAVIGATION PANEL SET DISPLAYS PANEL SET FUEL PANEL SET ELECTRICAL PANEL SET OVERHEAT AND FIRE CHECK PROTECTION PANEL APU SWITCH START EMERG EXIT LIGHT GUARD CLOSED Page 1 of 4

PASSENGER SIGNS WIPER SELECTORS WINDOW HEAT PROBE HEAT WING ANTI–ICE ENGINE ANTI–ICE HYDRAULIC PANEL AIRCON PANEL

SET PARK ALL ON OFF OFF OFF Set Set

PACKS=AUTO/HIGH, ISO VALVE=OPEN, ENG BLD=ON, APU BLD=ON

CABIN PRESS PANEL LIGHTING PANEL

SET SET

POSITION=ON, LOGO=ASREQ, ANTICOL=OFF, OTHERS=OFF

IGNITION SELECT SW

IGN L or R (ALTERNATE EACH FLIGHT)

ENGINE START SWITCH OFF TUNE ATIS AND NOTE DETAILS CALL FOR DEPARTURE CLEARANCE MODE CONTROL PANEL SET EFIS CONTROL PANEL SET SET MINS DEP AERO, SET QNH

OXYGEN CLOCK DISPLAY SELECT PANEL DISENGAGE LIGHT TEST FLIGHT INSTRUMENTS

TEST AND SET SET SET HOLD TO 1 (repeat 2) CHECK NO FLAGS, FMA BLANK, FD

GROUND PROXIMITY LANDING GEAR PANEL

CHECK SET DWN, 3 GRN, NO RED

AUTO BRAKE ANTISKID INOP ENG DISPLAY CONTROL

RTO VERIFY EXTINGUISHED SET AUTO, AUTO, RATE

ENGINE INSTRUMENTS CARGO FIRE PANEL

CHECK CHECK DET SW=NORM, PUSH TEST, PUSH MASTER FIRE, VFY ILLUM FWD AFT DET EXTINGUISHED

RADIO TUNING PANEL SET TRANSPONDER PANEL SET STAB TRIM OVERRIDE GUARD CLOSED SEAT/RUDDER PEDALS ADJUST PREFLIGHT Procedure - CAPTAIN LIGHTS TEST MODE CONTROL PANEL SET EFIS CONTROL PANEL SET SET MINS DEP AERO, SET QNH

OXYGEN CLOCK NOSE WHEEL STEERING DISPLAY SELECT PANEL DISENGAGE LIGHT TEST STAB OUT OF TRIM

TEST AND SET SET GUARD CLOSED SET HOLD TO 1 (repeat 2) LIGHT EXTINGUISHED

[email protected] – March 2015

Boeing 737-800 Procedure Checklist FLIGHT INSTRUMENTS

CHECK NO FLAGS, FMA BLANK, FD

STBY INSTRUMENTS STANDBY RMI SPEED BRAKE LEVER REVERSE THR LEVERS FORWARD THR LEVERS FLAP LEVER

CHECK SET DOWN DETENT DOWN CLOSED SET LEVER AGREES WITH POSITION

PARKING BRAKE SET ENGINE START LEVERS CUTOFF STABILIZER TRIM NORMAL RADIO TUNING PANEL SET SEAT/RUDDER PEDALS ADJUST SEAT BELT ADJUST Call “PREFLIGHT CHECKLIST” BEFORE START Procedure FLIGHT DECK DOOR CLOSED & LOCKED Do the Performance Data steps in the CDU Preflight before completing this procedure CDU DISPLAY PF – TAKEOFF PAGE PM – LEGS PAGE N1 & IAS BUGS CHECK & SET MCP SET V2 ARM LNAV/VNAV SET RWY HDG SET INIT ALTITUDE TAXI & TAKEOFF BRIEF COMPLETE EXTERIOR DOORS VERIFY CLOSED FUEL PUMPS ON CENTER FUEL PUMPS ON if < 460kg HYDRAULIC PANEL ALL ON ANTI COLLISION LIGHTS ON TRIM SET __ UNITS “0”&“0” PUSH & START OBTAIN CLEARANCE Call “BEFORE START CHECKLIST” ENGINE START Procedure ENGINE DISPLAY SELECT PACKS OFF START SEQUENCE ANNOUNCE CALL “START __ ENGINE” ENG START SWITCH GND N2 RPM VERIFY INCREASING ENGINE START LEVER IDLE AT 25% N2 MONITOR FUEL FLOW & EGT CALL “STARTER CUTOUT” BEFORE TAXI Procedure GENERATOR 1 & 2 ON PROBE HEAT ON WING ANTI-ICE AS REQUIRED ENGINE ANTI-ICE AS REQUIRED Page 2 of 4

PACKS AUTO ISOLATION VALVE AUTO APU BLEED OFF APU SWITCH OFF ENG START SWITCHES CONTINUOS ENG START LEVERS IDLE DETENT VERIFY GROUND EQUIPMENT IS CLEAR FLAPS SET FOR T/O FLIGHT CONTROLS CHECK BLANK LOWER DISPLAY LIGHTS TAXI/TURNOFF/WING – ON (LOGO at night) TRANSPONDER AS REQUIRED RECALL CHECK UPDATE CHANGES TO TAXI BRIEF AS REQUIRED Call “BEFORE TAXI CHECKLIST” BEFORE TAKEOFF Procedure CENTER FUEL TANK < 2300kg CABIN CREW SIGNAL WTHR RADAR DISP AS REQUIRED TERRAIN DISPLAY AS REQUIRED Call “BEFORE TAKEOFF CHECKLIST” TAKEOFF Procedure STROBE LIGHTS ON TRANSPONDER TA/RA RUNWAY HDG VERIFY WITH A/C HDG LANDING LIGHTS ALL ON (when cleared) CLOCK/TIMER START TAKEOFF TIME & FUEL NOTE ADVANCE THRUST LEVERS TO APPROX 40% N1 ALLOW ENGINES TO STABILIZE PRESS THE TO/GA SWITCH VERIFY T/O THRUST & MONITOR AT 80 KTS CALL “CHECK” AT V1 CALL “V1” AT VR CALL “ROTATE” ROTATE GENTLY TO 15⁰ NOSE UP AT POSITIVE RATE CALL “GEAR UP” CLIMB OUT V2+15-25 (is optimal) ABOVE 400FT RADIO VERIFY ROLL MODE AT ACCEL HEIGHT VERIFY CLIMB THRUST RETRACT FLAPS WHEN WITHIN 20 KTS OF FLAP SPEED MARKER. WHEN FLAPS ARE UP: AFTER FLAPS UP CALL VERTICAL MODE ENG BLD & PACKS ON ENG START SWITCHES AS REQUIRED AUTOBRAKE OFF LANDING GEAR OFF RETRACT/TAXI LIGHTS OFF Call “AFTER TAKEOFF CHECKLIST” [email protected] – March 2015

Boeing 737-800 Procedure Checklist CLIMB & CRUISE Procedure ABOVE 10,000FT (MSL or AGL): CENTER FUEL TANKS OFF < 460kg LIGHTS LANDING, TURNOFF, WING (LOGO) – OFF PASSENGER SIGNS AS REQUIRED AT TRANSITION ALT SET STD AND X-CHECK AT LEAST 10MINS PRIOR TO TOD: FMS/CDU LOAD STAR,RWY,MAP DESCENT Procedure CENTER FUEL TANKS OFF < 1400kg PRESSURIZATION CHECK LANDING ALT SYSTEM ANNUNC RECALL & REVIEW VREF SELECT IN CDU MINIMA SET BARO/RAD MINS NAVAIDS TUNE & SET APP CRS AUTOBRAKE SELECT APPROACH BRIEFING CONDUCT Call “DESCENT CHECKLIST” APPROACH Procedure BELOW 10,000FT (MSL or AGL): PASSENGER SIGNS ON LIGHTS FIXED LND, TURNOFF, WING (LOGO) - ON WHEN CLEARED BELOW TRANSITION LEVEL: ALTIMETERS SET QNH & X-CHECK RNP & APP PROCEDURE UPDATE AS REQUIRED Call “APPROACH CHECKLIST” LANDING Procedure - ILS CABIN CREW NOTIFY FLAPS LOWER ON SCHEDULE ON LOC INTERCEPT VERIFY ILS TUNED VERIFY LOC & G/S MARKERS SHOWN APPROACH MODE ARM SECOND AUTOPILOT ENGAGE IF REQUIRED IF NECESSARY USE HDG SEL TO INTERCEPT FINAL APP COURSE & VERIFY LOC IS CAPTURED AT GLIDESLOPE ALIVE “GEAR DOWN” “FLAPS 15” ENGINE START SWITCH CONT. LIGHTS RETRACT & TAXI - ON SPEEDBRAKE ARM VERIFY LIGHT ILLUMINATED

AT GLIDESLOPE SET FLAPS FOR CAPTURE LANDING MISSED APPROACH SET ALT IN MCP Call “LANDING CHECKLIST” AT FAF OR OM, VERIFY CROSSING ALTITUDE VERIFY AUTOLAND STATUS AT 500FT RADIO ALT Page 3 of 4

LANDING ROLL Procedure AUTOPILOT DISENGAGE THRUST LEVERS CLOSED SPEEDBRAKE LEVER VERIFY UP REVERSE THRUST APPLY AUTOBRAKE VERIFY OPERATION AT 60 KNOTS LOWER REVERSERS MANUAL BRAKING AS NEEDED AUTOBRAKES DISARM AFTER LANDING Procedure Start when clear of the active runway: SPEEDBRAKE CONFIRM DOWN APU START PROBE HEAT OFF LIGHTS LNDG, STROBES – OFF TAXI - ON ENG START SWITCHES OFF WEATHER RADAR OFF AUTOBRAKE OFF FLAP LEVER UP TRANSPONDER AS REQUIRED TURNING INTO GATE TAXI,RWY,WING - OFF SHUTDOWN Procedure PARKING BRAKE SET ELECTRICAL POWER APU GENS ON ENGINE START LEVERS CUTOFF SEAT BELTS SIGN OFF ANTI COLLISION LIGHT OFF FUEL PUMP SWITCHES OFF CAB/UTIL AS REQUIRED IFE/PASS SEAT AS REQUIRED WING ANTI-ICE OFF ENGINE ANTI-ICE OFF ENG HYD PUMPS ON ELEC HYD PUMPS OFF RECIRC FANS AS REQUIRED PACKS AUTO ENGINE BLEEDS ON APU BLEED ON EXTERIOR LIGHTS AS REQUIRED FLIGHT DIRECTORS OFF TRANSPONDER STBY Call “SHUTDOWN CHECKLIST” SECURE Procedure IRS MODE SELECTORS OFF EMERGENCY LIGHTS OFF WINDOW HEAT OFF PACKS OFF Call “SECURE CHECKLIST”

[email protected] – March 2015

Boeing 737-800 Procedure Checklist GO-AROUND MISSED APPROACH Procedure AT THE SAME TIME PRESS TO/GA CALL “FLAPS 15” THRUST VERIFY INCREASE & G/A ROTATION POSITIVE CLIMB GEAR UP LIMIT BANK TO 15⁰ IF AIRSPEED BELOW TOP OF AMBER BAND ABOVE 400FT VERIFY LNAV/HDG SEL VERIFY MISSED APP ROUTE IS TRACKED AT ACCEL HEIGHT CALL FOR FLAP RETRACT SCHED FLAPS RETRACT ON SCHED LVL CHG or VNAV SELECT AS NEEDED VERIFY CLIMB THRUST VERIFY MISSED APPROACH ALT IS CAPTURED LNDG GEAR LEVER OFF ENG START SWITCHES AS NEEDED Call “AFTER TAKEOFF CHECKLIST”

AUTOLAND LIMITS MAX GS ANGLE 3.25 degrees MIN GS ANGLE 2.5 degrees Automatic landings can be made using flaps 20 or 30, with both engines operative or one engine inoperative. The AFDS autoland status annunciation must display LAND 2 or LAND 3. MAXIMUM ALLOWABLE WIND SPEEDS HEADWIND 25 KNOTS TAILWIND 10-15 KNOTS CROSSWIND 25 KNOTS

OPERATIONAL LIMITATIONS RUNWAY SLOPE +/- 2% MAX T/O & LAND 10-15 KNOTS TAILWIND COMP MAXIMUM SPEEDS PLACARDED MAX OPERATING ALT 41,000 FT MAX T/O & LAND ALT 8,400 FT

Page 4 of 4

WEIGHT LIMITATIONS MAXIMUM TAXI WEIGHT 737-600 57,832 kg (127.5K lbs) 737-700 60,554 kg (133.5K lbs) 737-800 70,760 kg (156K lbs) 737-900 79,242 kg (174.2K lbs) MAXIMUM TAKEOFF WEIGHT 737-600 57,606 kg (127K lbs) 737-700 60,327 kg (133K lbs) 737-800 70,533 kg (155.5K lbs) 737-900 79,015 kg (174.2K lbs) MAXIMUM LANDING WEIGHT 737-600 54,657 kg (120.5K lbs) 737-700 58,059 kg (128K lbs) 737-800 65,317 kg (144K lbs) 737-900 66,360 kg (146.3K lbs) MAXIMUM ZERO FUEL WEIGHT 737-600 51,709 kg (114K lbs) 737-700 54,657 kg (120.5K lbs) 737-800 61,688 kg (136K lbs) 737-900 62,731 kg (138.3K lbs)

FMC CHEAT SHEET Add a fix at X nm before or after an existing waypoint on route Add waypoint that is off route Navigate to an intersection of 2 waypoints Add a distance ring round a waypoint (FIX page)

FFF/#DD PPPPPBBB/DDD XXXXXBBB/YYYYYBBB Enter fix name top left. Under BRG/DIST add /10 spd/FL190A

Speed and altitude constraint (up to 18000 then abv FL190). To intercept a specific inbound course to afix, (“Intercept the course 080 TO BOS,” for example.) the crewmember simply needs to enter the desired course TO the fix at the 6RLSK OFFSET command found in the INIT/REF LD.D or RD.D INDEX of the FMC/CDU

[email protected] – March 2015