Verify takeoff data to include N1, V1, VR, V2, flap setting, zero fuel weight, temperature, altimeter setting, gross weight, and stabilizer trim setting.
Flight Deck Preparation – First Officer
Escape strap ................................................................................... Check
Ensure strap is connected to structure. Sun visor and smoke goggles .......................................................Stowed Oxygen and interphone.................................................................. Check
Audio selector panel – Set
Normal Procedures -Amplified Procedures 737 Operations Manual
Push FLT INT transmitter selector and receiver switch, and adjust volume controls on receiver switch and overhead speaker. Position microphone selector to MASK.
Oxygen panel – Set Check mask is properly stowed and NORMAL/100% switch is at 100%. RESET/TEST slide lever – Push down and hold Observe momentary yellow cross in flow indicator. EMERGENCY/TEST selector – Push and hold While holding RESET/TEST slide lever down, push EMERGENCY/TEST selector and observe constant yellow cross in flow indicator. Push–To–Talk switch – I/C While holding RESET/TEST slide lever down and pushing the EMERGENCY/TEST selector, simultaneously key microphone and listen for oxygen flow sound through the overhead speaker. Then release all switches and reposition microphone selector as desired. Oxygen pressure – Check Verify pressure meets dispatch requirements.
Audio Selector panel (as installed) ........................................................................................ Set Air conditioning system ................................... ____ pack(s), bleeds ON
AIR TEMPERATURE source selector – As desired
Temperature selectors – As desired
RAM DOOR FULL OPEN lights – Illuminated
RECIRCULATION FAN switch – AUTO
Air conditioning PACK switches – One AUTO or HIGH
ISOLATION VALVE switch – AUTO
Engine BLEED air switches – ON
Copyright . The Boeing Company. See title page for details.
NP.20.16 June 4, 2004
Normal Procedures -Amplified Procedures 737 Operations Manual
APU BLEED air switch – As required
ON unless external air is used for start.
Pressurization system ..........................................................................Set FLIGHT ALTITUDE indicator – Cruise altitude LANDING ALTITUDE indicator – Destination field elevation CABIN RATE selector – Index CABIN ALTITUDE indicator – 200 feet below destination field
elevation
FLT/GRD switch (as installed) – GRD
Pressurization mode selector – AUTO
AUTOMATIC FAIL light – Extinguished
NAV switch (as installed) ..........................................................................As required Mode control panel ..............................................................................Set
When selecting a value on the MCP, ensure the corresponding display on the instrument panel changes, if applicable.
COURSE(S) – Set and crosscheck FLIGHT DIRECTOR switches – ON Position the switch for the pilot flying to ON first. Air temp/True airspeed indicator (as installed) ............................. Check
Select TAT. Right flight instruments .......................................................................Set Note: IRS alignment must be complete.
EFIS – Correct
A/T, Pitch and ROLL FMA’s - Blank
A/P STATUS FMA - FD
Flight instrument indications are correct.
Normal Procedures -Amplified Procedures 737 Operations Manual
Verify no flags displayed.
Altimeter - Set
MAP – Correct
Verify no flags displayed.
Route - Displayed, correct.
Clock ................................................................................................... Set GROUND PROXIMITY warning SYSTEM
TEST switch ...............................................................Push momentarily Verify switch guards down. Verify proper operation of the following:
.
BELOW G/S, GPWS INOP and TERRAIN DISPLAY SELECT lights illuminate
.
PULL UP and WINDSHEAR alerts illuminate
.
“GLIDESLOPE,” “PULL UP,” “WINDSHEAR,” “TERRAIN, TERRAIN PULL UP,” “OBSTACLE, OBSTACLE PULL UP,” aurals sound
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本文鏈接地址：737-300機組操作手冊Flight Crew Operations Manual FCOM 1(37)
