Commerce Control List Supplement No. 1 to Part 774 ... · PDF fileCommerce Control List...

Commerce Control List Supplement No. 1 to Part 774 Category 7—page 1

Export Administration Regulations July 16, 2001

CATEGORY 7 - NAVIGATION ANDAVIONICS

A. SYSTEMS, EQUIPMENT ANDCOMPONENTS

N.B.1: For automatic pilots for underwatervehicles, see Category 8. For radar, seeCategory 6.

N.B.2: For inertial navigation equipment forships or submersibles see item 9.e on theWassenaar Munitions List.

7A001 Accelerometers designed for use ininertial navigation or guidance systems andhaving any of the following characteristics (seeList of Items Controlled), and speciallydesigned components therefor.

License Requirements

Reason for Control: NS, MT, AT

Control(s) Country Chart

NS applies to entire entry NS Column 1

MT applies to entire entry MT Column 1

AT applies to entire entry AT Column 1

License Exceptions

LVS: N/AGBS: N/ACIV: N/A

List of Items Controlled

Unit: $ valueRelated Controls: See also 7A101 and 7A994.MT controls do not apply to accelerometers

that are specially designed and developed asMeasurement While Drilling (MWD) sensorsfor use in downhole well service applications.Related Definitions: N/A Items:

a. A "bias" "stability" of less (better) than 130micro g with respect to a fixed calibration valueover a period of one year;

b. A "scale factor" "stability" of less (better) than130 ppm with respect to a fixed calibration valueover a period of one year; or

c. Specified to function at linear accelerationlevels exceeding 100 g.

7A002 Gyros having any of the followingcharacteristics (see List of Items Controlled),and specially designed components therefor.







License Exceptions



Unit: $ valueRelated Controls: See also 7A102 and 7A994Related Definitions: N/AItems:



a. A "drift rate" "stability", when measured in a 1g environment over a period of three months andwith respect to a fixed calibration value, of:

a.1. Less (better) than 0.1° per hour whenspecified to function at linear acceleration levelsbelow 10 g; or

a.2. Less (better) than 0.5° per hour whenspecified to function at linear acceleration levelsfrom 10 g to 100 g inclusive; or

b. Specified to function at linear accelerationlevels exceeding 100 g.

7A003 Inertial navigation systems (gimballedor strapdown) and inertial equipment designedfor "aircraft", land vehicle or "spacecraft" forattitude, guidance or control, having any of thefollowing characteristics (see List of ItemsControlled), and specially designedcomponents therefor.







License Exceptions


!List of Items ControlledUnit: $ valueRelated Controls: See also 7A103 and 7A994.Inertial navigation systems and inertial

equipment, and specially designedcomponents therefor specifically designed,modified or configured for military use aresubject to the export licensing authority of theU.S. Department of State, Office of DefenseTrade Controls. (See 22 CFR part 121.)Related Definitions: N/AItems:

a. Navigation error (free inertial) subsequent tonormal alignment of 0.8 nautical mile per hour(50% Circular Error Probable (CEP)) or less(better); or

b. Specified to function at linear accelerationlevels exceeding 10 g.

Note: The parameters of 7A003.a areapplicable with any of the followingenvironmental conditions:

1. Input random vibration with an overallmagnitude of 7.7 g rms in the first half hour and atotal test duration of one and one half hour peraxis in each of the three perpendicular axes, whenthe random vibration meets the following:

a. A constant power spectral density(PSD) value of 0.04 g2/Hz over a frequencyinterval of 15 to 1,000 Hz; and

b. The PSD attenuates with frequencyfrom 0.04 g2/Hz to 0.01 g2/Hz over a frequencyinterval from 1,000 to 2,000 Hz; or

2. A roll and yaw rate of equal to or morethan +2.62 radian/s (150 deg/s); or

3. According to national standardsequivalent to 1. or 2. of this note.

Note: 7A003 does not control inertialnavigation systems that are certified for use on"civil aircraft" by civil authorities of a country inCountry Group A:1.



7A004 Gyro-astro compasses, and otherdevices which derive position or orientation bymeans of automatically tracking celestialbodies or satellites, with an azimuth accuracyof equal to or less (better) than 5 seconds ofarc.







License Exceptions



Unit: $ valueRelated Controls: See also 7A104 and 7A994Related Definitions: N/AItems:

The list of items controlled is contained in theECCN heading.

7A005 Global navigation satellite systems (i.e.GPS or GLONASS) receiving equipment, andspecially designed components therefor. (Theseitems are subject to the export licensingauthority of the U.S. Department of State,Office of Defense Trade Controls. See 22 CFR

part 121.)

7A006 Airborne altimeters operating atfrequencies other than 4.2 to 4.4 GHz inclusive,having any of the following characteristics (seeList of Items Controlled).







License Exceptions



Unit: $ valueRelated Controls: See also 7A106, 7A994and Category 6 for controls on radar. Related Definitions: N/AItems:

a. "Power management"; or

b. Using phase shift key modulation.

7A007 Direction finding equipment operatingat frequencies above 30 MHz and speciallydesigned components therefor. (These itemsare subject to the export licensing authority ofthe U.S. Department of State, Office of DefenseTrade Controls. See 22 CFR part 121.)



7A101 Accelerometers, other than thosecontrolled by 7A001, with a threshold of 0.05 gor less, or a linearity error within 0.25% of fullscale output, or both, which are designed foruse in inertial navigation systems or inguidance systems of all types and speciallydesigned components therefor.


Reason for Control: MT, AT




License Exceptions



Unit: $ valueRelated Controls: This entry does not controlaccelerometers which are specially designedand developed as MWD (Measurement WhileDrilling) sensors for use in downhole wellservice operations.Related Definitions: N/A Items:

The list of items is included in the entry heading.

7A102 All types of gyros, other than thosecontrolled by 7A002, usable in "missiles", witha rated "drift rate" "stability" of less than 0.5°(1 sigma or rms) per hour in a 1 g environmentand specially designed components therefor.






License Exceptions



Unit: $ valueRelated Controls: N/ARelated Definitions: 1.) Drift rate is definedas the time rate of output deviation from thedesired output. It consists of random andsystematic components and is expressed as anequivalent angular displacement per unit timewith respect to inertial space. 2.) Stability isdefined as standard deviation (1 sigma) of thevariation of a particular parameter from itscalibrated value measured under stabletemperature conditions. This can beexpressed as a function of time.Items:


7A103 Instrumentation, navigation equipmentand systems, other than those controlled by7A003, and specially designed componentstherefor.








License Exceptions



Unit: $ valueRelated Controls: 1.) Items described in7A103.b are subject to the export licensingauthority of the U.S. Department of State,Office of Defense Trade Controls (See 22CFR part 121). 2.) Inertial navigation systemsand inertial equipment, and specially designedcomponents therefor specifically designed,modified or configured for military use aresubject to the export licensing authority of theU.S. Department of State, Office of DefenseTrade Controls. (See 22 CFR part 121.)Related Definitions: N/AItems:

a. Inertial or other equipment usingaccelerometers or gyros controlled by 7A001,7A002, 7A101 or 7A102 and systemsincorporating such equipment;

Note: 7A103.a does not control equipmentcontaining accelerometers specially designed anddeveloped as MWD (Measurement WhileDrilling) sensors for use in down-hole wellservices operations.

b. Integrated flight instrument systems, whichinclude gyrostabilizers or automatic pilots,designed or modified for use in "missiles".

7A104 Gyro-astro compasses and otherdevices, other than those controlled by 7A004,

which derive position or orientation by meansof automatically tracking celestial bodies orsatellites and specially designed componentstherefor.






License Exceptions



Unit: $ valueRelated Controls: This entry controlsspecially designed components for gyro-astrocompasses and other devices controlled by7A004.Related Definitions: N/A Items:


7A105 Global Positioning Systems (GPS) orsimilar satellite receivers, other than thosecontrolled by 7A005, and designed or modifiedfor use in "missiles". (These items are subjectto the export licensing authority of the U.S.Department of State, Office of Defense TradeControls. See 22 CFR part 121.)

7A106 Altimeters, other than those controlledby 7A006, of radar or laser radar type,designed or modified for use in "missiles".



(These items are subject to the export licensingauthority of the U.S. Department of State,Office of Defense Trade Controls. See 22 CFRpart 121.)

7A115 Passive sensors for determining bearingto specific electromagnetic source (directionfinding equipment) or terrain characteristics,designed or modified for use in "missiles".(These items are subject to the export licensingauthority of the U.S. Department of State,Office of Defense Trade Controls. See 22 CFRpart 121.)

7A116 Flight control systems (hydraulic,m e c h a n i c a l , e l e c t r o - o p t i c a l , o relectro-mechanical flight control systems(including fly-by-wire systems) and attitudecontrol equipment) designed or modified for"missiles". (These items are subject to theexport licensing authority of the U.S.Department of State, Office of Defense TradeControls. See 22 CFR part 121.)

7A117 "Guidance sets" capable of achievingsystem accuracy of 3.33% or less of the range(e.g., a "CEP" of 10 km or less at a range of300 km). (These items are subject to the exportlicensing authority of the U.S. Department ofState, Office of Defense Trade Controls. See 22CFR part 121.)

7A994 Other navigation direction findingequipment, airborne communicationequipment, all aircraft inertial navigationsystems not controlled under 7A003 or 7A103,and other avionic equipment, including partsand components, n.e.s.


Reason for Control: AT



License Exceptions



Unit: $ valueRelated Controls: 1.) Global PositioningSatellite receivers having the followingcharacteristics are subject to the exportlicensing authority of the U.S. Department ofState, Office of Defense Trade Controls (22CFR part 121): (a) Designed for encryption ordecryption (e.g., Y-code) of GPS precisepositioning service (PPS) signal; (b) Designedfor producing navigation results above 60,000feet altitude and at 1,000 knots velocity orgreater; (c) Specifically designed or modifiedfor use with a null-steering antenna orincluding a null-steering antenna designed toreduce or avoid jamming signals; or (d)Designed or modified for use with unmannedair vehicle systems capable of delivering atleast a 500 kg payload to a range of at least300 km. (GPS receivers designed or modifiedfor use with military unmanned air vehiclesystems with less capability are considered tobe specially designed, modified or configuredfor military use are controlled by 22 CFR part121. 2.) This entry controls direction findingequipment that is not subject to the exportlicensing authority of the U.S. Department ofState, Office of Defense Trade Controls (22CFR part 121).Related Definitions: N/AItems:




B. TEST, INSPECTION ANDPRODUCTION EQUIPMENT

7B001 Test, calibration or alignmentequipment specially designed for equipmentcontrolled by 7A (except 7A994).







License Exceptions



Unit: $ valueRelated Controls: 1.) See also 7B102 and7B994. 2.) This entry does not control test,calibration or alignment equipment forMaintenance level I.Related Definition: 1.) Maintenance Level I:The failure of an inertial navigation unit isdetected on the aircraft by indications fromthe Control and Display Unit (CDU) or by thestatus message from the correspondingsub-system. By following the manufacturer'smanual, the cause of the failure may belocalized at the level of the malfunctioningline replaceable unit (LRU). The operatorthen removes the LRU and replaces it with aspare. 2.) Maintenance Level II: Thedefective LRU is sent to the maintenanceworkshop (the manufacturer's or that of the

operator responsible for level II maintenance).At the maintenance workshop, themalfunctioning LRU is tested by variousappropriate means to verify and localize thedefective shop replaceable assembly (SRA)module responsible for the failure. This SRAis removed and replaced by an operativespare. The defective SRA (or possibly thecomplete LRU) is then shipped to themanufacturer. Maintenance Level II does notinclude the removal of controlledaccelerometers or gyro sensors from the SRA.Items:


7B002 Equipment, as follows (see List of ItemsControlled), specially designed to characterizemirrors for ring "laser" gyros.







License Exceptions



Unit: $ valueRelated Controls: See also 7B102 and 7B994Related Definitions: N/AItems:



a. Scatterometers having a measurement accuracyof 10 ppm or less (better);

b. Profilometers having a measurement accuracyof 0.5 nm (5 angstrom) or less (better).

7B003 Equipment specially designed for the"production" of equipment controlled by 7A(except 7A994).







License Exceptions



Unit: $ valueRelated Controls: 1.) See also 7B103, (thisentry is subject to the licensing authority ofthe U.S. Department of State, Office ofDefense Trade Controls (see 22 CFR part121) 2.) This entry includes: inertialmeasurement unit tester (IMU module); IMUplatform tester; IMU stable element handlingfixture; IMU platform balance fixture; gyrotuning test station; gyro dynamic balancestation; gyro run-in/motor test station; gyroevacuation and filling station; centrifugefixtures for gyro bearings; accelerometer axisalign station; and accelerometer test station.

Related Definitions: N/A

Items:


7B101 "Production equipment", and othertest, calibration, and alignment equipment,other than that described in 7B003, 7B102 and7B104, designed or modified to be used withequipment controlled by 7A001-7A004 or7A101-7A104.






License Exceptions



Unit: $ valueRelated Controls: 1.) See also 7B003,7B102, 7B104 and 7B994. 2.) This entryincludes: inertial measurement unit tester(IMU module); IMU platform tester; IMUstable element handling fixture; IMU platformbalance fixture; gyro tuning test station; gyrodynamic balance station; gyro run-in/motortest station; gyro evacuation and fillingstation; centrifuge fixtures for gyro bearings;accelerometer axis align station; andaccelerometer test station.Related Definitions: N/AItems:




7B102 Equipment, other than those controlledby 7B002, designed or modified to characterizemirrors, for laser gyro equipment, as follows(see List of Items Controlled).






License Exceptions



Unit: $ valueRelated Controls: N/ARelated Definitions: N/AItems:

a. Scatterometers having a measurement accuracyof 10 ppm or less (better).

b. Reflectometers having a measurement accuracyof 50 ppm or less (better).

c. Prolifometers having a measurement accuracyof 0.5nm (5 Angstrom) or less (better).

7B103 Specially designed "productionfacilities" for equipment controlled by 7A117.(These items are subject to the export licensingauthority of the U.S. Department of State,

Office of Defense Trade Controls. See 22 CFRpart 121.)

7B104 Equipment, designed or modified to beused with equipment controlled by 7A001-7A004, or 7A101 - 7A104, as follows (see List ofItems Controlled).

License Requirements:





License Exceptions:


List of Items Controlled:

Unit: $ value

Related Controls: 1) See also 7B101 and7B994.Related Definitions: 1.) 7B104.a. does notcontrol balancing machines designed ormodified for dental or other medicalequipment. 2.) 7B104.c. and 7B104.d. do notcontrol rotary tables designed or modified formachine tools or for medical equipment. 3.)Rate tables not controlled by 7B104.c. andproviding the characteristics of a positioningtable are to be evaluated according to7B104.d. 4.) Equipment that has thecharacteristics specified in 7B104.d. whichalso meets the characteristics of 7B104.c. willbe treated as equipment specified in 7B104.c.Items:

a. Balancing machines having all the following



characteristics:

a.1. Not capable of balancingrotors/assemblies having a mass greater than 3Kgm;

a.2. Capable of balancing rotors/assemblies atspeeds greater than 12,500 rpm;

a.3. Capable of correcting unbalance in twoplanes or more; and

a.4. Capable of balancing to a residualspecific unbalance of 0.2 gram-mm per kg of rotormass;

b. Indicator heads (sometimes known asbalancing instrumentation) designed or modifiedfor use with machines specified in 7B104.a.

c. Motion simulators/rate tables (equipmentcapable of simulating motion) having all of thefollowing characteristics:

c.1. Two axes or more;

c.2. Slip rings capable of transmittingelectrical power and/or signal information; and

c.3. Having any of the followingcharacteristics:

c.3.a. For any single axis:

c.3.a.1. Capable of rates of rotationof 400 degrees/sec or more, or 30 degrees/sec orless, and

c.3.a.2. A rate resolution equal to orless than 6 degrees/sec and an accuracy equal toor less than 0.6 degrees/sec; or

c.3.b. Having a worst case rate stabilityequal to or better (less) than plus or minus 0.05%averaged over 10 degrees or more; or

c.3.c. A positioning accuracy equal to orbetter than 5 arc-second.

d. Positioning tables (equipment capable ofprecise rotary position in any axis) having thefollowing characteristics:

d.1. Two axes or more; and

d.2. A positioning accuracy equal to or betterthan 5 arc-second;

e. Centrifuges able to impart accelerations above100 g and having slip rings capable oftransmitting electrical power and signalinformation.

7B994 Other equipment for the test,inspection, or "production" of navigation andavionics equipment.





License Exceptions







C. MATERIALS [RESERVED]

D. SOFTWARE

7D001 "Software" specially designed ormodified for the "development" or"production" of equipment controlled by 7A(except 7A994) or 7B (except 7B994).


Reason for Control: NS, MT, RS, AT


NS applies to "software" NS Column 1for equipment controlledby 7A001 to 7A004, 7A006, 7B001, 7B002 or 7B003


RS applies to "software" RS Column 1for inertial navigationsystems inertial equipment,and specially designedcomponents therefor, for"civil aircraft"


License Exceptions

CIV: N/ATSR: N/A


Unit: $ valueRelated Controls: 1.) See also 7D101 and7D994. 2.) The "software" related to7A003.b, 7A005, 7A007, 7A103.b, 7A105,7A106, 7A115, 7A116, 7A117, or 7B103 are

subject to the export licensing authority of theU.S. Department of State, Office of DefenseTrade Controls. (See 22 CFR part 121.) 3.)"Software" for inertial navigation systems andinertial equipment, and specially designedcomponents therefor, not for use on civilaircraft are subject to the export licensingauthority of the U.S. Department of State,Office of Defense Trade Controls. (See 22CFR part 121.)Related Definitions: N/AItems:


7D002 "Source code" for the "use" of anyinertial navigation equipment or Attitude andHeading Reference Systems (AHRS) (exceptgimballed AHRS) including inertial equipmentnot controlled by 7A003 or 7A004.







License Exceptions

CIV: N/ATSR: N/A


Unit: $ valueRelated Controls: 1.) See also 7D102 and7D994. 2.) This entry does not control"source code" for the "use" of gimballed



AHRS.Related Definition: AHRS generally differfrom inertial navigation systems (INS) in thatan AHRS provides attitude and headinginformation and normally does not providethe acceleration, velocity and positioninformation associated with an INS.Items:


7D003 Other "software", as follows (see Listof Items Controlled).







License Exceptions

CIV: N/ATSR: N/A


Unit: $ valueRelated Controls: See also 7D103 and 7D994Related Definitions: N/AItems:

a. "Software" specially designed or modified toimprove the operational performance or reducethe navigational error of systems to the levelscontrolled by 7A003 or 7A004;

b. "Source code" for hybrid integrated systemsthat improves the operational performance orreduces the navigational error of systems to thelevel controlled by 7A003 by continuouslycombining inertial data with any of the followingnavigation data:

b.1. Doppler radar velocity;

b.2. Global navigation satellite systems (i.e.,GPS or GLONASS) reference data; or

b.3. Terrain data from data bases;

c. "Source code" for integrated avionics ormission systems that combine sensor data andemploy "expert systems";

d. "Source code" for the "development" of any ofthe following:

d.1. Digital flight management systems for"total control of flight";

d.2. Integrated propulsion and flight controlsystems;

d.3. Fly-by-wire or fly-by-light controlsystems;

d.4. Fault-tolerant or self-reconfiguring"active flight control systems";

d.5. Airborne automatic direction findingequipment;

d.6. Air data systems based on surface staticdata; or

d.7. Raster-type head-up displays or threedimensional displays;

e. Computer-aided-design (CAD) "software"specially designed for the "development" of"active flight control systems", helicopter



multi-axis fly-by-wire or fly-by-light controllersor helicopter "circulation controlled anti-torque orcirculation-controlled direction control systems"whose "technology" is controlled by 7E004.b,7E004.c.1 or 7E004.c.2.

7D101 "Software" specially designed for the"use" of equipment controlled by 7A001 to7A006, 7A101 to 7A106, 7A115, 7B001, 7B002,7B003, 7B101, 7B102, 7B103 or 7B104.






License Exceptions

CIV: N/ATSR: N/A


Unit: $ valueRelated Controls: 1.) The "software" relatedto 7A003.b, 7A005, 7A103.b, 7A105, 7A106,7A115, 7A116, 7A117, or 7B103 are subjectto the export licensing authority of the U.S.Department of State, Office of Defense TradeControls. (See 22 CFR part 121.) 2.)"Software" for inertial navigation systems andinertial equipment, and specially designedcomponents therefor, not designed for use oncivil aircraft by civil aviation authorities of acountry listed in Country Group A:1 is subjectto the export licensing authority of the U.S.Department of State, Office of Defense TradeControls. (See 22 CFR part 121.)Related Definitions: N/AItems:


7D102 Integration "software" for theequipment controlled by 7A003 or 7A103.






License Exceptions

CIV: N/ATSR: N/A


Unit: $ valueRelated Controls: The "software" related to7A003.b or 7A103.b are subject to the exportlicensing authority of the U.S. Department ofState, Office of Defense Trade Controls. (See22 CFR part 121.) Related Definitions: N/AItems:


7D103 "Software" specially designed formodelling or simulation of the "guidance sets"controlled by 7A117 or for their designintegration with "missiles". (This entry issubject to the export licensing authority of theU.S. Department of State, Office of DefenseTrade Controls. See 22 CFR part 121.)



7D994 "Software", n.e.s., for the"development", "production", or "use" ofnavigation, airborne communication and otheravionics.





License Exceptions

CIV: N/ATSR: N/A




E. TECHNOLOGY

7E001 "Technology" according to the GeneralTechnology Note for the "development" ofequipment or "software" controlled by 7A(except 7A994), 7B (except 7B994) or 7D(except 7D994).


Reason for Control: MT, NS, RS, AT


NS applies to "technology" NS Column 1for items controlled by7A001 to 7A004, 7A006,7B001 to 7B003, 7D001 to7D003


RS applies to "technology" RS Column 1for inertial navigation systems, inertial equipmentand specially designedcomponents therefor, forcivil aircraft


License Exceptions

CIV: N/ATSR: N/A


Unit: N/ARelated Controls: 1.) See also 7E101 and7E994. 2.) The "technology" related to7A003.b, 7A005, 7A007, 7A103.b, 7A105,7A106, 7A115, 7A116, 7A117, or 7B103 aresubject to the export licensing authority of theU.S. Department of State, Office of DefenseTrade Control (see 22 CFR part 121).Related Controls: N/ARelated Definitions: N/AItems:


7E002 "Technology" according to the GeneralTechnology Note for the "production" ofequipment controlled by 7A (except 7A994) or7B (except 7B994).




Reason for Control: NS, MT, RS, AT


NS applies to "technology" NS Column 1for equipment controlled by7A001 to 7A004, 7A006 or 7B001 to 7B003


RS applies to "technology" RS Column 1for inertial navigationsystems, inertial equipmentand specially designed components therefor, forcivil aircraft


License Exceptions

CIV: N/ATSR: N/A


Unit: N/ARelated Controls: 1.) See also 7E102 and7E994. 2.) The "technology" related to7A003.b, 7A005, 7A007, 7A103.b, 7A105,7A106, 7A115, 7A116, 7A117, or 7B103 aresubject to the export licensing authority of theU.S. Department of State, Office of DefenseTrade Controls (see 22 CFR part 121).Related Definitions: N/AItems:


7E003 "Technology" according to the General

Technology Note for the repair, refurbishing oroverhaul of equipment controlled by 7A001 to7A004.







License Exceptions

CIV: N/A TSR: N/A


Unit: N/ARelated Controls: See also 7E994. This entrydoes not control maintenance "technology"directly associated with calibration, removalor replacement of damaged or unserviceableLRUs and SRAs of a "civil aircraft" asdescribed in Maintenance Level I orMaintenance Level II.Related Definition: Refer to the RelatedDefinitions for 7B001. Items:


7E004 Other "technology", as follows (see Listof Items Controlled).









License Exceptions

CIV: N/ATSR: N/A


Unit: N/ARelated Controls: See also 7E104 and 7E994!Related Definitions: "Primary flightcontrol" means an "aircraft" stability ormaneuvering control using force/momentgenerators, i.e., aerodynamic control surfacesor propulsive thrust vectoring.Items:

a. "Technology" for the "development" or"production" of:

a.1. Airborne automatic direction findingequipment operating at frequencies exceeding 5MHz;

a.2. Air data systems based on surface staticdata only, i.e., that dispense with conventional airdata probes;

a.3. Raster-type head-up displays or threedimensional displays for "aircraft";

a.4. Inertial navigation systems or gyro-astrocompasses containing accelerometers or gyroscontrolled by 7A001 or 7A002;

a.5. Electric actuators (i.e., electromechanical,electrohydrostatic and integrated actuatorpackage) specially designed for "primary flightcontrol";

a.6. "Flight control optical sensor array"specially designed for implementing "active flightcontrol systems";

b. "Development" "technology", as follows, for"active flight control systems" (includingfly-by-wire or fly-by-light):

b.1. Configuration design for interconnectingmultiple microelectronic processing elements(on-board computers) to achieve "real timeprocessing" for control law implementation;

b.2. Control law compensation for sensorlocation or dynamic airframe loads, i.e.,compensation for sensor vibration environment orfor variation of sensor location from the center ofgravity;

b.3. Electronic management of dataredundancy or systems redundancy for faultdetection, fault tolerance, fault isolation orreconfiguration;

Note: 7E004.b.3. does not control"technology" for the design of physicalredundancy.

b.4. Flight controls that permit inflightreconfiguration of force and moment controls forreal time autonomous air vehicle control;

b.5. Integration of digital flight control,navigation and propulsion control data into adigital flight management system for "total controlof flight";

Note: 7E004.b.5 does not control:

1. "Development" "technology" forintegration of digital flight control, navigationand propulsion control data into a digital flightmanagement system for "flight path optimization";

2. "Development" "technology" for"aircraft" flight instrument systems integrated



solely for VOR, DME, ILS or MLS navigation orapproaches.

b.6. Full authority digital flight control ormultisensor mission management systemsemploying "expert systems";

N.B.: For "technology" for Full AuthorityDigital Engine Control ("FADEC"), see9E003.a.9.

c. "Technology" for the "development" ofhelicopter systems, as follows:

c.1. Multi-axis fly-by-wire or fly-by-lightcontrollers that combine the functions of at leasttwo of the following into one controlling element:

c.1.a. Collective controls;

c.1.b. Cyclic controls;

c.1.c. Yaw controls;

c.2. "Circulation-controlled anti-torque orcirculation-controlled directional controlsystems";

c.3. Rotor blades incorporating "variablegeometry airfoils" for use in systems usingindividual blade control.

7E101 "Technology", other than "technology"controlled by 7E003, according to the GeneralTechnology Note for the "use" of equipmentcontrolled by 7A001 to 7A006, 7A101 to 7A106,7A115 to 7A117, 7B001, 7B002, 7B003, 7B101,7B102, 7B103, 7B104, 7D101 to 7D103.


Reason for Control: MT, RS, AT



RS applies to "use" RS Column 1of inertial navigation systems, inertialequipment and speciallydesigned components therefor,for civil aircraft.


License Exceptions

CIV: N/ATSR: N/A


Unit: N/ARelated Controls: 1.) The "technology"related to 7A003.b, 7A005, 7A103.b, 7A105,7A016, 7A115, 7A116, 7A117, 7B103, or7D103 are subject to the export licensingauthority of the U.S. Department of State,Office of Defense Trade Controls. (See 22CFR part 121.) 2.) "Technology" for inertialnavigation systems and inertial equipment,and specially designed components therefor,not for use on civil aircraft are subject to theexport licensing authority of the U.S.Department of State, Office of Defense TradeControls. (See 22 CFR part 121.)Related Definitions: N/AItems:


7E102 "Technology" for protection of avionicsand electr ical subsystems aga inste lectromagnetic pulse (EMP) andelectromagnetic interference (EMI) hazards,from external sources, as follows (see List of



Items Controlled).






License Exceptions

CIV: N/ATSR: N/A


Unit: N/ARelated Controls: N/ARelated Definitions: N/AItems:

a. Design "technology" for shielding systems;

b. Design "technology" for the configuration ofhardened electrical circuits and subsystems;

c. Design "technology" for the determination ofhardening cri teria of .a and .b of this entry.

7E104 "Technology" for the integration of theflight control, guidance, and propulsion datainto a flight management system foroptimization of rocket system trajectory. (Thisentry is subject to the export licensing

authority of the U.S. Department of State,Office of Defense Trade Controls. See 22 CFRpart 121.)

7E994 "Technology", n.e.s., for the"development", "production", or "use" ofnavigation, airborne communication, and otheravionics equipment.





License Exceptions

CIV: N/ATSR: N/A


Unit: N/ARelated Controls: N/ARelated Definitions: N/AItems:


EAR99 Items subject to the EAR that are notelsewhere specified in this CCL Category or inany other category in the CCL are designatedby the number EAR99.

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