+ activex/HKLM/HKCU startup, drop file to temp/windows/system32/system/drivers+ set file attribute to hidden, system and read only + clone pe icon, clone pe info, clone pe time. + change icon/null pe info/change pe entry point/add new pe section/fix pe checksum/null pe icon/anti padding/EOF data saver/Zero EntryPoint + add a custom stub/fake message/delayed execution + various anti methods by SqUeEzEr, Karcrack and me + command line/delayed execution for each binded/crypted file/url
#FLY CRYPTER V2.3 PASSWORD#
+ binded files and urls are hight crypted with your custom encryption-autogenerate random password for each binded file, you can also chose password level + multiple binder/crypter/packer/downloader/delayed execution/parameter support '11 Boeing B-777: Fly-By-Wire Flight Controls' (PDF). ^ Airbus A320 AFM (requires page number, publisher, etc).SmartCockpit – Airline training guides, Aviation, Operations, Safety. ^ a b c d e f g h i j 'Airbus 330 – Systems – Flight Controls'.^ 'Avionics Magazine :: Boeing 787: Integration's Next Step'.^ a b c 'The Boeing 777' (powerpoint).Archived from the original on 8 March 2009. ^ a b c d 'Crossing the Skies » Fly-by-wire and Airbus Laws'.^ 'Flight Control Laws - SKYbrary Aviation Safety'.Like the Airbus system, this state is entered when a number of failures occur in the EFCS or interfacing systems (e.g. However, EFCS functionality is reduced, including loss of flight envelope protection. īoeing secondary mode is comparable to the Airbus alternate law, with the PFCs supplying commands to the ACEs. Information from these computers is sent both to the pilot's primary flight display and also to the control surfaces. The computers also receive information from the control surfaces of the aircraft and from the pilot's aircraft control devices and autopilot. Information from the ADIRU is fed into one of several flight control computers (primary and secondary flight control). ADIRUs are part of the air data inertial reference system, which, on the Airbus is linked to eight air data modules: three are linked to pitot tubes and five are linked to static sources. This is fed along with GPS data, into three redundant processing units known as air data inertial reference units (ADIRUs) that act both as an air data reference and inertial reference. In addition there are two flight control data computers (FCDC) that read information from the sensors, such as air data (airspeed, altitude). The aircraft is controlled by three primary control computers (captain's, first officer's, and standby) and two secondary control computers (captain's and first officer's).
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