NORMAL CHECKLIST B737 – 800W
Date: 15/04/2011 Rev: 03 Page 1 of 2
PREFLIGHT
AFTER TAKE OFF
Pins and covers……………......……………..REMOVED
Oxygen……………... …………..............TESTED, 100%
Nav transfer & display switches..…...NORMAL, AUTO
Window heat……………………………......................ON
Air cond & press............. _ _PACK , BLEEDS ON, SET
Flight Instruments….TRK___QNH___READING___ft
Parking brake………………………………………..SET
Engine Start levers………..…….……….…….CUTOFF
Rudder & aileron trim…………………FREE & ZERO
Taxi and Take off briefing….………..….COMPLETED
----- ----- ----- ----- ----- ----- ---------- ----- ----Fuel…………………………………...__kgs. PUMPS ON
Passenger signs……………………….........................SET
Autobrake…………………………………………....RTO
CDU Preflight and ACARS.…................COMPLETED
Take Off Speeds……………..……V1___,VR___,V2___
MCP………………….……....V2___, HDG___,ALT___
Engine Bleeds……………………….......................................ON
Packs………………………................................................AUTO
Landing gear………………………............................UP & OFF
Flaps…………………………………………...UP, NO LIGHTS
Altimeters.....……………………………..SET & X-CHECKED
DESCENT
Pressurization………………………...............LAND ALT____
Recall………………………………………………..CHECKED
Autobrake…………………………………………………....___
Landing data……………..............VREF___, MINIMUMS___
Approach Briefing………………………………COMPLETED
APPROACH
Altimeters.....…………………………….SET & X-CHECKED
BEFORE START
LANDING
Flight Deck Door………………….CLOSED & LOCKED
Doors and Windows…..…………..CLOSED & LOCKED
Anti Collision light………………...……........................ON
Transponder………….…………………………AS REQD
Cabin call………………………………………………..GIVEN
Engine start switches……………………….....................CONT
Speed brakes……….......................................................ARMED
Landing gear………………............................................DOWN
Flaps……………………………….............___GREEN LIGHT
BEFORE TAXI
SHUTDOWN
Generators……………………………….………….…..ON
Probe heat..……………………………….………….….ON
Anti-ice……………………............................................___
Air cond & press…………………………...PACKS AUTO
Isolation valve ……………………….………………AUTO
Engine Start switches…………….…………………CONT
Recall…………………….…………..………....CHECKED
Engine Start levers………………………..IDLE DETENT
Flight controls……….….……………..………CHECKED
Ground equipment…………..……………………CLEAR
APU…………………………….…….…..….………...____
BEFORE TAKEOFF
Flaps……………___PLANNED……___,GREEN LIGHT
Stabilizer trim………….……………...……….___UNITS
Cabin call…………………………………………..GIVEN
Fuel Pumps..…………….………………………………..OFF
Probe heat …………………………………….….AUTO/OFF
Hydraulic Panel…………………..…..…….…………….SET
Flaps………………………………………. ...AS REQUIRED
Parking brake…………………………….…AS REQUIRED
Engine Start levers………..………………….…….CUTOFF
Weather radar…………………………………………...OFF
Technical log…………………………............COMPLETED
SECURE
IRSs…………………………………………………...........OFF
Emergency exit lights………………………………...........OFF
Window heat…………………………….............................OFF
Packs…………………………….………………….............OFF
APU/ GPU………......................GND.SERVICE BUS or OFF
Battery………………………….…………………………..OFF
NORMAL CHECKLIST B737-800W
Date: 15/04/2011
Rev: 03
Page 2 of 2
SINGLE ENGINE LANDING CHECKLIST
(Immediate VMC Return)
Prerequisite: Memory items completed (if
any)/affected engine start lever CUTOFF:
AUTOTHROTTLE……………...DISENGAGE
APU………………………...…START/ON BUS
Autobrake…………………………………...SET
Flap Inhibit……………………………INHIBIT
Landing speed…………………………...Vref 15
Speedbrake…………………………....ARMED
Landing gear…………………………....DOWN
Flaps……………………….15, GREEN LIGHT
NO ENGINE BLEED TAKE-OFF
JUST PRIOR TO TAKE OFF
Right Pack Switch……………………..…AUTO
Isolation Valve Switch.........…….............CLOSE
Left Pack Switch………………………….AUTO
Engine No 1 BLEED air switch…..………..OFF
APU BLEED air switch……………………..ON
Engine No 2 BLEED air switch……………OFF
Trim Air Switch……………………………...ON
Wing ANTI ICE switch…………………….OFF
AFTER TAKE OFF (1500-2000 feet)
Engine No 2 BLEED air switch……………..ON
APU BLEED air switch…………………….OFF
When CABIN rate of CLIMB indic. Stabilizes.
Engine No 1 BLEED air switch…………….ON
ISOLATION VALVE switch……………AUTO
APU…………………...………..AS REQUIRED
EXTERIOR DE-ICING PROCEDURE
APU……………………………………..…………..AS REQ
FLAPS……………………………………………………UP
Stab. Trim……………………..…Full APL NOSE DOWN
Engine Bleed Air Switches……….……………………OFF
APU Bleed Air Switch…..…………………………..….OFF
Logo Light………………………..…………………….OFF
Row-44 (if installed)…………………………………...OFF
AFTER DE-ICING, PERFORM THE FOLLOWING
APU……………………………………..………….AS REQ
Stab. Trim………………………..…………..._____UNITS
Row-44 (if installed)……………………………….AS REQ
Engine Bleed air switches (after 1 min)...……………..ON
Exterior Lights……….…………...…..…………..AS REQ
Go-around directly followed by an
approach without flying above
transition altitude.
This procedure may replace the AFTER TAKE OFF,
DESCENT and APPROACH procedures, at
Commander's discretion to reduce flight deck workload.
Should a climb above transition altitude or a longer
holding be necessary, the Normal Checklist procedures
shall be used.
AUTO BRAKE………………………………..…...______
LANDING DATA........... VREF .........MINIMUMS_____
APPROACH BRIEFING........... ………….COMPLETED
NAV AIDS..... ……………..………………………….SET
ENGINE CROSSBLEED START
RVSM
Prior to using this procedure, ensure that the area
to the rear is clear.
Engine BLEED air switches………………....ON
APU BLEED air switch………………...…..OFF
PACK switches……………………………...OFF
ISOLATION VALVE switch…………....AUTO
(Ensures bleed air supply for engine start.)
Engine thrust lever (operating engine)
ADVANCE to 30 PSI
Non operating engine……………….…..START
Preflight:
Primary altimeters…………………………CHECK
Indicated altitude shall be within 75 ft of aerodrome
elevation. Difference between Capt and F/O
altimeters 50 feet (or 60 feet at AD above 5000’)
Prior to entering RVSM airspace:
Recheck altimeter setting and cross-check primary
altimeters. Record on Operational Flight Plan when
Aircraft is stable at cleared RVSM level.
Inflight:
At approximately one hour intervals, cross-check
primary altimeters. Maximum difference 200 ft.
Use normal start procedure with crossbleed air.
Note: FL 280 is the highest usable non-RVSM level.