曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Ensure the autopilots are OFF; that courses, altitude, heading, and speed are
set for the anticipated departure; that the bank limiter is set on 25 degrees;
that flight director switches are ON with the correct MA light illuminated.
> Select VOR/ILS or NAV as appropriate for the type of departure
anticipated.
When selecting a value on the MCP, ensure the corresponding display on
the instrument also changes.
737 Sec. 3 Page 49
Flight Manual Continental Rev. 11/15/02 #41
Flight Mode Annunciator (Flow)..................................................CHECKED
Check the Flight Mode Annunciator (FMA) for proper indications.
Altimeters & Flight Instruments............................ SET, CHECKED (F, C)
Note: IRS’s must be aligned for proper indications.
Verify that airspeed indicates >>@ zero or BCD 60, digital
readout indicates 45, and that no flags are in view. >>@ Verify
airspeed cursor control IN for automatic operation. Check ADI for proper
attitude and warning flags out of view. Check compass warning flags out of
view, cross-check heading of RMIs with (E) HSIs. Check vertical speed
indicator at zero with no flags.
Check Standby Horizon for proper attitude and warning flag out of view.
On >@BCD ensure that the ILS selector on the Standby Horizon
is ON. Check Standby altimeter / airspeed indicator. On BCD check
standby RMI for proper heading and Bearing Pointer switch in appropriate
position.
>>@ Set barometric pressure in all altimeters. Set altimeter bugs at
field elevation. Verify proper altitude and no flags.
>>@ Press to test the MARKER BEACON lights and adjust the intensity
by turning the light cap as required. Check GMT with ACARS.
The following instrument checks are required first flight of the day:
> INSTRUMENT COMPARATOR TEST:
Press the instrument comparator test switch. Observe the instrument
comparator lights illuminate. Release the instrument comparator test
switch and observe the instrument comparator lights extinguished. The
MON PWR light will not illuminate but may be tested by pulling the PWR
circuit breaker (ensure circuit breaker is reset P6-1, A-9).
> RADIO ALTIMETER TEST:
Press and hold the altimeter test button. Observe the altitude display moves
to 40 ± 5 feet. The DH light will illuminate when the test altitude is
indicated. Release the test button. Observe the altitude display returns to
zero and the DH light extinguishes.
On the >@BCD aircraft there is no Instrument Comparator /
Radio Altimeter Test.
Sec. 3 Page 50 737
Rev. 11/15/02 #41 Continental Flight Manual
The following tests are optional:
HSI/ILS TEST
Tune VHF navigation radio to an ILS frequency. Move UP/LEFT
DOWN/RIGHT test switch to the UP/LEFT position. Observe the glideslope
pointer is up one dot and the course deviation bar is left one dot. Check
navigation and glideslope failure flags are out of view. Release switch.
Move UP/LEFT DOWN/RIGHT test switch to the DOWN/RIGHT position. Observe
the glideslope pointer is down one dot and the course deviation bar is right
one dot. Check navigation and glideslope failure flags are out of view.
Release switch.
DME TEST
Tune VHF navigation radio to a VOR frequency.
Move VOR/DME test switch to DME. Check that both indicators for the DME
being tested are covered for two seconds; then display four dashes for three
seconds; then display 000.0 ± 0.5 until the test switch is released.
ADF AND RMI TEST
Position the ADF/VOR pointer switch on the RMI to ADF. On EFIS aircraft to
check the ADF pointers on the EHSI, select FULL NAV with the EHSI Mode
Selector.
Move the function selector to TEST and the ADF pointer on the RMI should
point to 45 degrees left of the lubber line. Place function selector to desired
mode.
HSI VOR RMI TEST
Select VOR/ILS on the HSI switch.
Tune in a VOR test station (VOT), if available, or any receivable VOR
frequency. Set course selector to 000. Select VOR on VOR/ADF switch (on
RMI).
Move VOR/DME test switch to VOR. Check that the course deviation bar is
centered; the to/from flag indicates FROM and the VOR pointer indicates 180
degrees. Release the test switch.
Note: The maximum permissible error is +4°.
>@BCD Nosewheel
Steering Switch (Flow) ...................................................................NORM
BCD Display Select Panel (Flow) .................................AS REQUIRED
737 Sec. 3 Page 51
Flight Manual Continental Rev. 11/15/02 #41
Warning & Operating Lights (Flow) ...........................................CHECKED
Ensure warning lights are checked.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737 FLIGHT MANUAL 737飛行手冊1(114)