كيف استخدم الFMC في الطائرة

[ayoub318]

كيف استخدم ال:icon_arroFMC في الطائرة

[fly-iy]

اخى العزيز اذا كنت تقصد flight manangment computer
هناك معطيات وارقام يتم ا دخالها فى ال fmc انا الان مش ذاكرها قد استعنت باْحد الزملاء عن طريق الايميل اذا حصلت منه رد , ساتواصل معك من خلال هذه الصفحه.
واتمنى من احد الزملاء فى خط الطيران ان يتعاون معك .

[شهاب الجزيرة]

هذه مجموعة من مقاطع الفيديو

للطائرة التشبيهية لطريقة أستخدام

FMC


وأن شاء الله من خلال هذه المقاطع راح توضح لك الفكرة

نوع الطائرة 747-400

أف أم سي القسم الاول (http://www.hz-akc.com/malnajran/FMCpart1.wmv)

اف ام سي القسم الثاني (http://www.hz-akc.com/malnajran/FMCpart2.wmv)

اف ام سي القسم الثالث (http://www.hz-akc.com/malnajran/FMCpart3.wmv)

[fly-iy]

الاخ شهاب الجزيره , يعطيك العافيه الروابط لم يفتح معى خالص

[fly-iy]

هذه مجموعة من مقاطع الفيديو


للطائرة التشبيهية لطريقة أستخدام

FMC


وأن شاء الله من خلال هذه المقاطع راح توضح لك الفكرة

نوع الطائرة 747-400

أف أم سي القسم الاول (http://www.hz-akc.com/malnajran/FMCpart1.wmv)

اف ام سي القسم الثاني (http://www.hz-akc.com/malnajran/FMCpart2.wmv)


اف ام سي القسم الثالث (http://www.hz-akc.com/malnajran/FMCpart3.wmv)

الروابط لم يفتح

[Ehab Samy]

اخوى لم تحدد اى طائرة تقصد؟

[Sr.Flight Attendant]

اخي الكريم ريح بالك وتوجه لقسم الطيران التشبيهي او اكتب في البحث ( الفيديو التعليمي ) وسوف يظهر لك موضوع الاخ محمد النجران في شرحه للاف ام سي للبوينج 777 و 747 و البوينج 737 ايضاً .. شرح بالفيديو خطير جداً ولا يفوتك ..
لك مني كل التحية ..

[ykoheel]

FMCS - GENERAL DESCRIPTION

General

The flight management computing system shares data with the these systems or components:

Air data inertial reference system
Global positioning system
Navigation radios
Engine sensors
Fuel sensors
FMCF internal databases
Key entries into the control display units (CDUs).
The FMCS uses the data from the airplane systems to do these functions:

Navigation
Flight planning
Performance management
Guidance and control
Thrust management
Display and system control
Datalink interface.
FMCS Components

The FMCS has these components:

Flight management computing function (FMCF) (2) one in each AIMS cabinet
CDUs (3)
FMC selector
Instrument source select panel (ISSP) navigation source switches (2).
Also, the mode control panel (MCP) has an interface with the FMCS, but is not an FMCS component.
Flight Management Computing Function

Each FMCF has these two software partitions:

Flight management function (FMF) partition
Navigation function partition.
The FMF partition supplies these functions:

Flight planning
Lateral navigation (LNAV) guidance commands
Vertical navigation (VNAV) guidance commands
Thrust guidance commands
Performance data
Display control
ND MAP display
Manual, route, and procedure selection of navigation radios
BITE and fault monitoring.
The navigation function partition supplies these functions:

Position calculation
Navaid selection for radio position calculation
Navigation radio tuning command outputs.
The FMCFs use performance and navigation data bases and sensor inputs to calculate guidance commands. When the flight crew uses the MCP to select the LNAV and VNAV modes, the FMCF sends this data:

LNAV and VNAV guidance commands to the autopilot flight director computers (AFDCs)
Thrust guidance commands and thrust limit data to the thrust management computing function (TMCF)
Display and fault data to the primary display and central maintenance computing functions in the AIMS cabinets.
Automatic Dependent Surveillance Function

The automatic dependent surveillance function (ADSF) is a sub-function of the FMCF. The purpose of the ADSF is to let air traffic control (ATC) monitor the airplane in the air.
ATC sends automatic dependent surveillance (ADS) requests from the ground to the airplane. The ADSF in the airplane sends airplane position, heading, airspeed, and other data to the ground. ATC uses this data to manage air traffic. The ADSF is automatic and does not require flight crew action.
CDU - General

There are three CDUs in the flight deck. The CDUs are the primary control and display interface unit for the FMCF. The flight crew uses the left and right CDUs to enter flight plan data and interface with the FMCF and other systems. If the left or right CDU fails, the center CDU is the backup.
All CDUs can select a maintenance page format on a multifunction display (MFD) in the primary display system (PDS).
All CDUs can control the satellite communication (SATCOM) system.
The center CDU is the interface for the passenger address/cabin interphone (PA/CI) controller.
The CDU supplies these functions when the FMCFs fail:

Backup navigation radio tuning
Calculates LNAV guidance commands
Backup map data.
FMC Selector and Instrument Source Select Panel

The FMC selector is on the first officer display switching panel. It determines the active FMCF.
The FMC selector and ISSP switches supply analog inputs to the overhead panel ARINC 629 system (OPAS). The OPAS changes these inputs and sends them to the AIMS cabinet on the systems ARINC 629 buses.
The NAV ISSP switch determines the source of navigation display data.