NORMAL CHECKLIST B737 – 800W Date: 15/04/2011 Rev: Rev: 03 Page 1 of 2
PREFLIGHT
AFTER TAKE OFF
Pins and covers……………......……………..REMOVED Oxygen……………... Oxygen……………... …………..............TESTED, …………..............TESTED, 100% Nav transfer & display switches..…...NORMAL, switches..…...NORMAL, AUTO Window heat……………………… heat……………………………......................O ……......................ON N Air cond & press............. _ _PACK , BLEEDS ON, SET Flight Instruments….TRK___QNH___RE Instruments….TRK___QNH___READING___ft ADING___ft Parking brake………………………………………..SET Engine Start levers………..…….……….…….CUTOFF Rudder & aileron trim…………………FREE & ZERO Taxi and Take off briefing….………..….COMP briefing….………..….COMPLETED LETED ----- ----- ----- ----- ----- ----- ---------- ----- ----Fuel…………………………………...__kgs. PUMPS ON Passenger signs…………………… signs……………………….........................SET ….........................SET Autobrake…………………………………………....RTO CDU Preflight and ACARS.…................COMPLETED Take Off Speeds……………..… Speeds……………..……V1___,VR___,V2___ …V1___,VR___,V2___ MCP………………….…… MCP………………….……....V2___, ....V2___, HDG___,ALT___
Engine Bleeds………………………. Bleeds……………………….......................................ON ......................................ON Packs…………………… Packs………………………................................................AUTO …................................................AUTO Landing gear………………………............................UP gear………………………............................UP & OFF Flaps…………………………………………...UP, NO LIGHTS Altimeters.....……………………………..SET & X-CHECKED
DESCENT Pressurization………………… Pressurization………………………...............LAN ……...............LAND D ALT____ Recall………………………………………………..CHECKED Autobrake…………………………………………………....___ Landing data……………..............VREF___, 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………………...……........................O light………………...……........................ON N Transponder………….…………………………AS REQD
Cabin call………………………………………………..GIVEN Engine start switches…………………… switches……………………….....................CONT ….....................CONT Speed brakes……….......................................................ARM brakes……….......................................................ARMED ED Landing gear………………..................................... gear………………............................................DOWN .......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…………………… levers………………………..IDLE …..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………………………… log…………………………............COMPLET ............COMPLETED ED
SECURE IRSs…………………………………………………...........OFF Emergency exit lights………………………………...........OFF Window heat………………………… heat…………………………….............................OF ….............................OFF F Packs…………………………….………………….............OFF APU/ GPU………......................GND.SE GPU………......................GND.SERVICE RVICE 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 f ollowed by an approach with out fl ying 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 BRA KE………………………………..…...______ LANDING DATA........... VREF .........MINIMUMS_____ APPROACH B RIEFING........... ………….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.
