Copyright . The Boeing Company. See title page for details.
SP.4.8  December 5, 2003

737 Operations Manual

Aircraft Communication Addressing and Reporting System (ACARS)
The following procedures are applicable to the noted ACARS functions from the company pages.
Pre-Departure Clearance
The flight crew shall manually verify (compare) the filed flight plan versus the digital pre-departure clearance and shall initiate voice contact with Air Traffic Control if any question/confusion exists between the filed flight plan and the digital pre-departure clearance.
Digital-Automatic Information Service
The flight crew shall verify that the D-ATIS altimeter setting numeric value and alpha value are identical. If the D-ATIS altimeter setting numeric value and alpha values are different, the flight crew must not accept the D-ATIS altimeter setting.
Oceanic Clearances
The flight crew shall manually verify (compare) the filed flight plan versus the digital oceanic clearance and initiate voice contact with Air Traffic Control if any questions/confusion exists between the filed flight plan and the digital oceanic clearance.
Weight and Balance
The flight crew shall verify the Weight and Balance numeric and alphabetical values are identical. If the Weight and Balance numeric and alphabetical values are different, the flight crew must not accept the Weight and Balance data.
Takeoff Data
The flight crew shall verify the Takeoff Data numeric and alphabetic values are identical. If the Takeoff Data numeric and alphabetic values are different, the flight crew must not accept the Takeoff Data message.
Supplementary Procedures -Communications 737 Operations Manual

Cockpit Voice Recorder Test
On airplanes with monitor indicator: Test switch .................................................................................. Push After a slight delay:
Monitor indicator .........................................................Green band A tone may be heard through a headset plugged into the headset jack. Test switch ..............................................................................Release On airplanes with STATUS light: Test switch .................................................................................. Push After a slight delay: STATUS light............................................................................ On A tone may be heard through a headset plugged into the headset jack. Test switch ..............................................................................Release On airplanes with LED monitor indicator: Test switch .................................................................................. Push After a slight delay: LED indicator ..............................................................Illuminated The LED indicator will illuminate twice. Test switch ..............................................................................Release
Copyright . The Boeing Company. See title page for details.
SP.5.2  June 4, 2004

737 Operations Manual

Standby Power Test
Battery switch .....................................................................................ON
AC–DC meter selectors ........................................................STBY PWR
APU GEN No. 2 switch or GRD PWR switch ................................. OFF

Turn OFF appropriate switch depending on power source in use. Removes power from TR 3. STANDBY POWER switch ............................................................. OFF Check STANDBY PWR OFF light illuminated. AC–DC voltmeters ...........................................................................Zero STANDBY POWER switch ............................................................. BAT Check STANDBY PWR OFF Light extinguished AC–DC voltmeters ........................................................................ Check AC voltmeter 115 +/- 5 volts DC voltmeter 26 +/- 4 volts Frequency meter ............................................................................ Check Check frequency meter for normal indication: 400 +/- 10 CPS. STANDBY POWER switch ..........................................................AUTO APU GEN No. 2 switch or GRD PWR switch...................................ON
Supplementary Procedures -Electrical 737 Operations Manual

Intentionally
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Copyright . The Boeing Company. See title page for details.
SP.6.2  December 1, 2000

737 Operations Manual

Battery Start
(With APU bleed or ground air available)
Prior to a battery start, accomplish the exterior safety inspection and the flight deck safety inspection. Accomplish interior/exterior inspections if required except for items requiring electrical or hydraulic power.
Accomplish the following preliminary flight deck preparation items:
Fault/Inop detection .................................................................. Check
　
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