checklist_b737.pdf

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NORMAL CHECKLIST B737

PREFLIGHT

 AFTER TAK T AK EOFF

Oxyg en . . . . . . . . . . . . . . . . . . . . . . . . . Test ed, 100%

Eng in e bleed s . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON

Navigation Navigation t ransfer  and dis play s wit ches . . . . . . . . . . .NORMAL, .NORMAL, AUTO

Packs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A UTO

Win do w Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON Pressurization mode selec to r . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO Flight Inst ruments . . . . .Heading .Heading ___, ___, Altimeter ___  Parki ng Br ake . . . . . . . . . . . . . . . . . . . . . . . . . . . SET Engi ne st art l evers . . . . . . . . . . . . . . . . . . . CUTOFF BEFORE START Flight deck d oor . . . . . . . . . . . . .Closed and lock ed Fuel . . . . . . . . . . . . . . . . . . . . . . ___ KGS, Pump s ON Passen ger si gn s . . . . . . . . . . . . . . . . . . . . . . . . . .___ 

Landi ng g ear . . . . . . . . . . . . . . . . . . . . . UP and and OFF Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . UP, No lig ht s DESCENT Pressur ization . . . . . . . . . . . . . . . . . . LAND ALT ___  Recall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check ed  Au to br ake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___  Landi ng d ata . . . . . . . . . .VREF .VREF ___, ___, Mini Mini mum s ___   Ap pr oac h b ri efi ng . . . . . . . . . . . . . . . . . . Com pl eted  APPROACH  APP ROACH  Al ti met ers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___

Windo ws . . . . . . . . . . . . . . . . . . . . . . . . . . . . L ock ed MCP . . . . . . .V2 ___, HEADING ___, ALTITUDE ___ 

LANDING

Gros s Weig ht . . . . . . . . . . . . . . . . . CDU___, CDU___, OFP___  OFP___ 

Engin e start swi tch es . . . . . . . . . . . . . . . . . . . CONT

Takeof f s peeds . . . . . . . . . . V1 ___, VR ___, V2 ___ 

Speedb rake . . . . . . . . . . . . . . . . . . . . . . . . . .A RMED

CDU prefl igh t . . . . . . . . . . . . . . . . . . . . . . Com pleted

Land in g gear . . . . . . . . . . . . . . . . . . . . . . . . . . Down

Rudder and aileron tri m . . . . . . . . . . . . . .Free and 0

Green l ight ig ht Flaps . . . . . . . . . . . . . . . . . . . . . . ___, Green

Taxi and takeof f bri efing . . . . . . . . . . . . . Compl eted  An ti co ll is io n l ig ht . . . . . . . . . . . . . . . . . . . . . . . . . ON

SHUTDOWN Fuel p umps um ps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

BEFORE TAXI Generato rs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On

YF804-YV652 (SB chan ges YB521 - YF803)

Pro be heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . A UTO (SB Chang es YB521 - YF803)

Pro be heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Pro be heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

 An ti -ic e . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .___ 

Hydr auli c p anel . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Isolati on v alve . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Engin e start s wit ches . . . . . . . . . . . . . . . . . . . CONT CONT

Parki ng br ake . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___ 

Recall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked

Engin e start levers. . . . . . . . . . . . . . . . . . . . CUTOFF CUTOFF

 Au to br ake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RTO

Weather radar . . . . . . . . . . . . . . . . . . . . . . . . . .Off 

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . __, Green li gh t Engin e start levers . . . . . . . . . . . . . . . . .IDLE detent Fligh t co ntr ols . . . . . . . . . . . . . . . . . . . . . . . Checked Groun d equ ipm ent . . . . . . . . . . . . . . . . . . . . . . Clear  Clear 

SECURE IRSs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF Emergency exit l igh ts . . . . . . . . . . . . . . . . . . . . .OFF Win do w h eat. . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

BEFORE TAKEOFF

Packs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

Flaps . . . . . . . . . . . . . . . . . . . . . . . . .___ , Green li gh t

EFB . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

Stabilizer Stabilizer tri m  . . . . . . . . . . . . . . . . . . . . ___ Uni Units ts

March 31, 2016

REFERENCE CHECKLIST B737

TRANSAVIA.COM

WIND COMPONENT WIND ANGLE 0° 15° 30° 45° 60° 75° 90° 105° 120° 135° 150° 165° 180°

HEADWIND COMPONENT WIND SPEED 10 15 20 25 30 35 40 10 15 20 25 30 35 40 10 14 19 24 29 34 39 9 13 17 22 26 30 35 7 11 14 18 21 25 28 5 8 10 13 15 18 20 3 4 5 6 8 9 10 0 0 0 0 0 0 0 -3 -4 -5 -6 -8 -9 -10 -5 -7 -10 -13 -15 -18 -20 -7 -11 -14 -18 -21 -25 -28 -9 -13 -17 -22 -26 -30 -35 -10 -14 -19 -24 -29 -34 -39 -10 -15 -20 -25 -30 -35 -40

WIND ANGLE 45 45 43 39 32 23 12 0 -12 -23 -32 -39 -43 -45

0° 15° 30° 45° 60° 75° 90° 105° 120° 135° 150° 165° 180°

10 0 3 5 7 9 10 10 10 9 7 5 3 0

CROSSWIND COMPONENT WIND SPEED 15 20 25 30 35 40 0 0 0 0 0 0 4 5 6 8 9 10 8 10 13 15 18 20 11 14 18 21 25 28 13 17 22 26 30 35 14 19 24 29 34 39 15 20 25 30 35 40 14 19 24 29 34 39 13 17 22 26 30 35 11 14 18 21 25 28 8 10 13 15 18 20 4 5 6 8 9 10 0 0 0 0 0 0

AUTOPILOT/FLIGHT DIRECTOR SYSTEM 45 0 12 23 32 39 43 45 43 39 32 23 12 0

Maximum allowable wind speeds, when conducting a dual channel landing predicated on autoland operations, are: • Headwind 25 knots • Crosswind 20 knots • -700: Tailwind 15 knots • -800: Tailwind 15 knots (flaps 40 • -800: Tailwind 12 knots (flaps 30)

COLD TEMPERATURE ALTITUDE CORRECTIONS HEIGHT ABOVE ALTIMETER REFERENCE SOURCE AIRPORT TEMP °C 200 FT 300 FT 400 FT 500 FT 600 FT 700 FT 800 FT 900 FT 1000 FT1500 FT2000 FT3000 FT 0° 20 20 30 30 40 40 50 50 60 90 120 170 -10° 20 30 40 50 60 70 80 90 100 150 200 290 -20° 30 50 60 70 90 100 120 130 140 210 280 420 -30° 40 60 80 100 120 140 150 170 190 280 380 570 -40° 50 80 100 120 150 170 190 220 240 360 480 720 -50° 60 90 120 150 180 210 240 270 300 450 590 890 • No corrections are needed for reported temperatures above 0°C or if the airport temperature is at or above the minimum published temperature for the procedure being flown • Apply corrections to all published minimum departure, en route and approach altitudes, including missed approach altitudes

RUNWAY SURFACE CONDITION ASSESSMENT TABLE (RSCAT) and MAXIMUM TAKEOFF AND LANDING WIND COMPONENTS Condition

Dry

Coverage of 25% or lessa Wet

More than 25% coverage of the runway surface area within the reported length and width being used Wet (includes water less then 3 mm and damp)

Contaminated

Wet snow or dry snowb

Type

N/A

Any

Wet or Slippery Frost damp when wet

Standing water or slush

Depth

N/A

Any

Less than 3 mm

Less than 3 mm - Less than 3 mm 3 mmc 13 mmd 3 mmc 13 mmd

OAT

N/A

Any

N/A

N/A

N/A

N/A

N/A

N/A

RCC

6

5

5

3

5

5

2

Braking Action

N/A

GOOD

GOOD

MEDIUM to POOR

N/A

GOOD MEDIUM GOOD

Dry snow or Compacted snow wet snow (may include over comembedded ice) pacted snow

Ice

Wet ice, water over compacted snow, dry or wet snow over ice

Any

Any

Any

Any

Any

N/A

-15°C or colder

warmer than  -15°C

N/A

N/A

N/A

5

3

4

3

3

1e

0e

GOOD

MEDIUM

MEDIUM

POOR

NIL

GOOD to MEDIUM MEDIUM

Max crosswind T/O 25 T/O 25 T/O 25 T/O 25 T/O 25 15 10 15 20 15 15 5 0 componentf  (kts) 33 LDG 33 LDG 33 LDG 33 LDG 33 LDG 33  Rwy width > 40 m Max crosswind 15 15 10 15 15 5 15 10 12 10 10 0 0 componentf  (kts) 20 Rwy width 30-40m Max tailwind 15 15 15 5 15 15 5 15 5 10 5 5 0 0 componentf  (kts) a. When no more than 25% of the runway surface area within the reported length and width being used is covered by any contaminant, the runway is considered wet. b. For wet snow or dry snow use equivalent depth refer to 8.1.2-5-3. c. For equivalent contaminant depth less than 3 mm, the runway is considered wet. d. Takeoff and landing is not allowed with contaminant equivalent depth of more than 13 mm. e. RCCs 0 and 1 may be upgraded to 3 by the airport authorities under certain conditions, in this case wind limitations associated with RCC 3 are applicable. f. The maximum takeoff and landing wind components include gusts.

March 31, 2016