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时间:2010-05-02 22:53来源:蓝天飞行翻译 作者:admin
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indicates the software options that are enabled. Each option has
a hexadecimal code. The codes for the enabled options are
summed, and this is shown on the software options page. These
are the software options your airline selected:
SHZ ALL
* Position Update - Runway offset in meters - This option
permits the entry of the airplane position as an offset
distance from the runway threshold.
* Manual takeoff speeds - This option lets the display of FMC
computed take off speeds on the TAKEOFF REF page be
turned on or off with the QRH ON or QRH OFF prompts.
* GPS with integrity - This option lets the FMC use GPS data as
the primary source for position update.
* Direct GPS input - This option permits the FMC to receive
GPS data from the MMRs.
* Manual RNP entry - This option lets the flight crew enter
different values for the RNP if they do not exceed the default
values.
* AOC datalink - This option lets the FMC uplink and downlink
data through ACARS.
* Alternate destination - This option lets the flight crew review
the distance, time, and fuel that remains for diversions to
alternate airports.
* Certified takeoff speeds - This option permits the use of FMC
computed take off speeds in the MEDB.
* Plan fuel entry - This option lets the flight crew input the final
fuel load before refueling has been completed. Thus, the
FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - SOFTWARE OPTIONS
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.147
D633A101-SHZ1 Jun 10/2007
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-064
FMC flight plan can be activated while the airplane is being
refueled. At engine start, in air, or entry of a new gross weight,
any entered plan fuel will be invalid.
* QFE altitude reference - This option lets the flight crew
change the SET LANDING ALTITUDE on the PFD between
QNH and QFE altitude references.
* Quiet climb system (QCS) - This option lets the flight crew
use noise abatement procedures during the climb out.
FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - SOFTWARE OPTIONS
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.148
D633A101-SHZ1 Jun 10/2007
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-064
FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - SOFTWARE OPTIONS
FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - SOFTWARE OPTIONS
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.149
D633A101-SHZ1 Jun 10/2007
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-064
FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - SOFTWARE OPTIONS
FMCS - TRAINING INFORMATION POINT - FMCS BITE PAGES - SOFTWARE OPTIONS
EFFECTIVITY
SHZ ALL POST SB 737-34-1918 34-61-00
Page 98.150
D633A101-SHZ1 Jun 10/2007
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-064
Purpose
The performance factors page permits the display and entry of
performance factors to optimize airplane performance for
individual operators or airplane characteristics.
Page Access
You use the PERF FACTR line select key (3R) on the FMCS BITE
page to get access to the performance factors page.
This page will automatically show if there is a performance
factors mismatch during power-up and it is the only mismatch.
Performance Factors Page
The aerodynamic and engine models in the performance data
base are from airplane design and flight test data. Since each
production airplane may be different, the FMCS PERF
FACTORS page lets the operator make adjustments for some
of the factors in the model/engine database.
SHZ ALL POST SB 737-34-1918
Line select key 1L shows the GEO DES mode. The geometric
path descent feature uses computed gradients for the entire
descent profile when FULL mode is selected. The FULL mode is
the default mode and can only be changed to the APP mode
with the Loadable Defaults Data Base. In the APP mode the
gradients are only used on approach or approach transistion
legs.
SHZ ALL
Line select key 2L shows the DRAG FACTOR value. This is a
correction factor applied to drag calculations and is a
percentage. The default value is 0.0 and the allowable entry
range is - 9.9 to + 9.9
Line select key 3L shows the fuel flow (F-F) value. This is a
correction factor applied to fuel flow calculations and is a
 
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