Commerce Control List Supplement No. 1 to Part 774 Category 7—page 1
CATEGORY 7 - NAVIGATION AND accelerometers that are “specially AVIONICS designed” and developed as Measurement While Drilling (MWD) sensors for use in downhole well service applications. A. “END ITEMS,” “EQUIPMENT,” Related Definitions: N/A “ACCESSORIES,” “ATTACHMENTS,” Items: “PARTS,” “COMPONENTS,” AND “SYSTEMS” a. Linear accelerometers having any of the following:
N.B.1: For automatic pilots for underwater a.1. Specified to function at linear vehicles, see Category 8. For radar, see acceleration levels less than or equal to 15 g and Category 6. having any of the following:
a.1.a. A “bias” “stability” of less 7A001 Accelerometers as follows (see List of (better) than 130 micro g with respect to a fixed Items Controlled) and “specially designed” calibration value over a period of one year; or “components” therefor. a.1.b. A “scale factor” “stability” of less License Requirements (better) than 130 ppm with respect to a fixed calibration value over a period of one year; Reason for Control: NS, MT, AT a.2. Specified to function at linear Country acceleration levels exceeding 15 g but less than Chart (See or equal to 100 g and having all of the following: Control(s) Supp. No. 1 to part 738) a.2.a. A “bias” “repeatability” of less NS applies to entire entry NS Column 1 (better) than 1,250 micro g over a period of one MT applies to commodities MT Column year; and that meet or exceed the 1 parameters of 7A101. a.2.b. A “scale factor” “repeatability” AT applies to entire entry AT Column 1 of less (better) than 1,250 ppm over a period of one year; or List Based License Exceptions (See Part 740 for a description of all license exceptions) a.3. Designed for use in inertial navigation or guidance systems and specified to function at LVS: N/A linear acceleration levels exceeding 100 g; GBS: N/A Note: 7A001.a.1 and 7A001.a.2 do not List of Items Controlled apply to accelerometers limited to measurement of only vibration or shock. Related Controls: (1) See USML Category XII(e) for accelerometers subject to the b. Angular or rotational accelerometers, ITAR. (2) See also ECCNs 7A101, specified to function at linear acceleration levels 7A611, and 7A994. (3) For angular or exceeding 100 g. rotational accelerometers, see ECCN 7A001.b. (4) MT controls do not apply to
Export Administration Regulations Bureau of Industry and Security December 4, 2020 Commerce Control List Supplement No. 1 to Part 774 Category 7—page 2
7A002 Gyros or angular rate sensors, having of the following: any of the following, and “specially designed” “components” therefor. a.1. An angular rate range of less than 500 degrees per second and having any of the License Requirements following:
Reason for Control: NS, MT, AT a.1.a. A “bias” “stability” of less (better) than 0.5 degree per hour, when Country measured in a 1 g environment over a period of Chart (See one month, and with respect to a fixed Control(s) Supp. No. 1 to calibration value; or part 738) NS applies to entire entry NS Column 1 a.1.b. An “angle random walk” of less MT applies to commodities MT Column 1 (better) than or equal to 0.0035 degree per that meet or exceed the square root hour; or parameters of 7A102. AT applies to entire entry AT Column 1 Note: 7A002.a.1.b does not control “spinning mass gyros”. License Requirement Note: For the purpose of MT controls only, the term ‘stability’ a.2. An angular rate range greater than or is defined as a measure of the ability of a specific equal to 500 degrees per second and having any mechanism or performance coefficient to remain of the following: invariant when continuously exposed to a fixed operating condition. (This definition does not a.2.a. A “bias” “stability” of less refer to dynamic or servo stability.) (IEEE STD (better) than 4 degrees per hour, when measured 528-2001 paragraph 2.247) in a 1 g environment over a period of three minutes, and with respect to a fixed calibration List Based License Exceptions (See Part 740 value; or for a description of all license exceptions) a.2.b. An “angle random walk” of less LVS: N/A (better) than or equal to 0.1 degree per square GBS: N/A root hour; or
Note: 7A002.a.2.b does not apply to List of Items Controlled “spinning mass gyros”.
Related Controls: (1) See USML Category b. Specified to function at linear acceleration XII(e) for gyros or angular rate sensors levels exceeding 100 g. subject to the ITAR. (2) See also ECCNs 7A102, 7A611, and 7A994. (3) For angular or rotational accelerometers, see 7A003 ‘Inertial measurement equipment or ECCN 7A001.b. systems’, having any of the following. Related Definitions: N/A Items: License Requirements a. Specified to function at linear acceleration Reason for Control: NS, MT, AT levels less than or equal to 100 g and having any
Export Administration Regulations Bureau of Industry and Security December 4, 2020 Commerce Control List Supplement No. 1 to Part 774 Category 7—page 3
Country Chart Arrangement Participating States, see Control(s) (See Supp. No. Supplement No. 1 to part 743 of the EAR.. 1 to part 738) NS applies to entire entry NS Column 1 Technical Note: ‘Positional aiding references’ MT applies to MT Column 1 independently provide position, and include: commodities in 7A003.d that meet or exceed the a. “Satellite navigation system”; parameters of 7A103 AT applies to entire entry AT Column 1 b.”Data-Based Referenced Navigation” (“DBRN”).
List Based License Exceptions (See Part 740 a. Designed for “aircraft”, land vehicles or for a description of all license exceptions) vessels, providing position without the use of ‘positional aiding references’, and having any of LVS: N/A the following “accuracies” subsequent to normal GBS: N/A alignment:
a.1. 0.8 nautical miles per hour (nm/hr) List of Items Controlled “Circular Error Probable” (“CEP”) rate or less (better); Related Controls: (1) See also ECCNs 7A103, 7A611, and 7A994. (2) See a.2. 0.5% distanced travelled “CEP” or less USML Category XII(d) for guidance or (better); or navigation systems subject to the ITAR. Related Definitions: N/A a.3. Total drift of 1 nautical mile “CEP” or Items: less (better) in a 24 hr period;
Note 1: ‘Inertial measurement equipment or Technical Note: The performance systems’ incorporate accelerometers or parameters in 7A003.a.1, 7A003.a.2 and gyroscopes to measure changes in velocity and 7A003.a.3 typically apply to ‘inertia orientation in order to determine or maintain measurement equipment or systems’ designed heading or position without requiring an for “aircraft”, vehicles and vessels, external reference once aligned. ‘Inertial respectively. These parameters result from the measurement equipment or systems’ include: utilization of specialized non-positional aiding references (e.g., altimeter, odometer, velocity - Attitude and Heading Reference log). As a consequence, the specified Systems (AHRSs); performance values cannot be readily converted - Gyrocompasses; between these parameters. Equipment designed - Inertial Measurement Units (IMUs); for multiple platforms are evaluated against - Inertial Navigation Systems (INSs); each applicable entry 7A003.a.1, 7A003.a.2, or - Inertial Reference Systems (IRSs); 7A003.a.3. - Inertial Reference Units (IRUs). b. Designed for “aircraft”, land vehicles or Note 2: 7A003 does not apply to ‘inertial vessels, with an embedded ‘positional aiding measurement equipment or systems’ which are reference’ and providing position after loss of all certified for use on “civil aircraft” by civil ‘positional aiding references’ for a period of up aviation authorities of one or more Wassenaar
Export Administration Regulations Bureau of Industry and Security December 4, 2020 Commerce Control List Supplement No. 1 to Part 774 Category 7—page 4 to 4 minutes, having an “accuracy” of less therefor, as follows (see List of Items (better) than 10 meters “CEP”; Controlled).
Technical Note: 7A003.b refers to systems License Requirements in which ‘inertial measurement equipment or systems’ and other independent ‘positional Reason for Control: NS, MT, AT aiding references’ are built into a single unit (i.e., embedded) in order to achieve improved Country Chart performance. Control(s) (See Supp. No. 1 to part 738) c. Designed for “aircraft”, land vehicles or NS applies to entire entry NS Column 1 vessels, providing heading or True North MT applies to entire entry MT Column 1 determination and having any of the following: AT applies to entire entry AT Column 1
c.1. A maximum operating angular rate less List Based License Exceptions (See Part 740 (lower) than 500 deg/s and a heading “accuracy” for a description of all license exceptions) without the use of ‘positional aiding references’ equal to or less (better) than 0.07 deg sec (Lat) LVS: N/A (equivalent to 6 arc minutes rms at 45 degrees GBS: N/A latitude); or List of Items Controlled c.2. A maximum operating angular rate equal to or greater (higher) than 500 deg/s and a Related Controls: (1) See USML Category heading “accuracy” without the use of XV for certain ‘star trackers’ that are ‘positional aiding references’ equal to or less “subject to the ITAR” (see 22 CFR parts (better) than 0.2 deg sec (Lat) (equivalent to 17 120 through 130). (2) See also 7A104 and arc minutes rms at 45 degrees latitude); 7A994. Related Definitions: N/A d. Providing acceleration measurements or Items: angular rate measurements, in more than one dimension, and having any of the following: a. ‘Star trackers’ with a specified azimuth “accuracy” of equal to or less (better) than 20 d.1. Performance specified by 7A001 or seconds of arc throughout the specified lifetime 7A002 along any axis, without the use of any of the equipment; aiding references; or b. “Components” “specially designed” for d.2. Being “space-qualified” and providing equipment specified in 7A004.a as follows: angular rate measurements having an “angle random walk” along any axis of less (better) than b.1. Optical heads or baffles; or equal to 0.1 degree per square root hour. b.2. Data processing units. Note: 7A003.d.2 does not apply to ‘inertial measurement equipment or systems’ that Technical Note: ‘Star trackers’ are also contain “spinning mass gyros” as the only type referred to as stellar attitude sensors or gyro- of gyro. astro compasses.
7A004 ‘Star trackers’ and “components”
Export Administration Regulations Bureau of Industry and Security December 4, 2020 Commerce Control List Supplement No. 1 to Part 774 Category 7—page 5
7A005 “Satellite navigation system” ITAR and USML Category XI(c)(10) for receiving equipment having any of the antennae that are subject to the ITAR. (3) following and “specially designed” Items that otherwise would be covered by “components” therefor. ECCN 7A005.a are “subject to the ITAR” (see 22 CFR parts 120 through 130). License Requirements Related Definitions: N/A
Items: Reason for Control: NS, MT and AT
a. Employing a decryption algorithm “specially Country Chart designed” or modified for government use to Control(s) (See Supp. No. 1 access the ranging code for position and time; or to part 738)
NS applies to NS Column 1 b. Employing ‘adaptive antenna systems’. 7A005.b
MT applies to MT Column 1 commodities in Note: 7A005.b does not apply to “satellite 7A005.b that meet navigation system” receiving equipment that or exceed the only uses “components” designed to filter, parameters of switch, or combine signals from multiple omni- 7A105. directional antennas that do not implement AT applies to AT Column 1 adaptive antenna techniques. 7A005.b
Technical Note: For the purposes of 7A005.b List Based License Exceptions (See Part 740 ‘adaptive antenna systems’ dynamically for a description of all license exceptions) generate one or more spatial nulls in an antenna array pattern by signal processing in the time
domain or frequency domain. LVS: N/A
GBS: N/A 7A006 Airborne altimeters operating at
frequencies other than 4.2 to 4.4 GHz List of Items Controlled inclusive and having any of the following (see List of Items Controlled). Related Controls: (1) See also ECCNs 7A105, 7A611 and 7A994. Commercially License Requirements available “satellite navigation system” receivers do not typically employ Reason for Control: NS, MT, AT decryption or adaptive antennae and are classified as 7A994. (2) See USML Country Control(s) Category XII(d) for “satellite navigation Chart (See system” receiving equipment subject to the
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Supp. No. 1 to Country Chart part 738) Control(s) (See Supp. No. NS applies to entire entry NS Column 1 1 to part 738) MT applies to commodities MT Column 1 NS applies to entire entry NS Column 2 in this entry that meet or AT applies to entire entry AT Column 1 exceed the parameters of 7A106 List Based License Exceptions (See Part 740 AT applies to entire entry AT Column 1 for a description of all license exceptions)
List Based License Exceptions (See Part 740 LVS: N/A for a description of all license exceptions) GBS: N/A
LVS: N/A List of Items Controlled GBS: N/A Related Controls: 7A008 does not control List of Items Controlled systems “specially designed” for installation on surface vessels or systems Related Controls: See also 7A106, 7A994 requiring acoustic beacons or buoys to and Category 6 for controls on radar. provide positioning data. See 6A001.a for Related Definitions: N/A acoustic systems, and 6A001.b for Items: correlation-velocity and Doppler- velocity sonar log equipment. See 8A002 for a. ‘Power management’; or other marine systems. Related Definitions: N/A Technical Note: ‘Power management’ is Items: changing the transmitted power of the altimeter signal so that received power at the “aircraft” The list of items controlled is contained in the altitude is always at the minimum necessary to ECCN heading. determine the altitude. b. Using phase shift key modulation. 7A101 Accelerometers, other than those controlled by 7A001 (see List of Items Controlled), and “specially designed” “parts” 7A008 Underwater sonar navigation systems and “components” therefor. using Doppler velocity or correlation velocity logs integrated with a heading source and License Requirements having a positioning “accuracy” of equal to or less (better) than 3% of distance traveled Reason for Control: MT, AT “Circular Error Probable” (“CEP”) and “specially designed” “components” therefor. Country Chart Control(s) (See Supp. No. License Requirements 1 to part 738) MT applies to entire entry MT Column 1 Reason for Control: NS, AT AT applies to entire entry AT Column 1
List Based License Exceptions (See Part 740 for a description of all license exceptions)
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7A002 (see List of Items Controlled), and LVS: N/A “specially designed” “parts” and GBS: N/A “components” therefor.
List of Items Controlled License Requirements
Related Controls: (1) See USML Category Reason for Control: MT, AT XII(e) for accelerometers subject to the ITAR. (2) See also ECCNs 7A101 and Country Chart 7A611. (3) This entry does not control Control(s) (See Supp. No. accelerometers that are “specially 1 to part 738) designed” and developed as MWD MT applies to entire entry MT Column 1 (Measurement While Drilling) sensors for AT applies to entire entry AT Column 1 use in downhole well service operations. Related Definitions: N/A List Based License Exceptions (See Part 740 Items: for a description of all license exceptions) a. Linear accelerometers designed for use in LVS: N/A inertial navigation systems or in guidance GBS: N/A systems of all types, usable in “missiles” having all of the following characteristics, and List of Items Controlled “specially designed” “parts” and “components” therefor: Related Controls: (1) See USML Category XII(e) for gyros or angular rate sensors a.1. ‘Scale factor’ “repeatability” less subject to the ITAR. (2) See also ECCNs (better) than 1250 ppm; and 7A002, 7A611, and 7A994. Related Definitions: 1.) Drift rate is defined a.2. ‘Bias’ “repeatability” less (better) than as the time rate of output deviation from 1250 micro g. the desired output. It consists of random and systematic components and is Note: The measurement of ‘bias’ and ‘scale expressed as an equivalent angular factor’ refers to one sigma standard deviation displacement per unit time with respect to with respect to a fixed calibration over a period inertial space. 2.) Stability is defined as of one year. standard deviation (1 sigma) of the variation of a particular parameter from its calibrated value measured under stable b. Accelerometers of any type, designed for use temperature conditions. This can be in inertial navigation systems or in guidance expressed as a function of time. systems of all types, specified to function at Items: acceleration levels greater than 100 g. a. All types of gyros, usable in rockets, Note to paragraph (b): This paragraph (b) missiles, or unmanned aerial vehicles capable of does not include accelerometers that are achieving a “range” equal to or greater than 300 designed to measure vibration or shock. km, with a rated “drift rate” ‘stability’ of less than 0.5 degrees (1 sigma or rms) per hour in a 1 g environment. 7A102 Gyros, other than those controlled by
Export Administration Regulations Bureau of Industry and Security December 4, 2020 Commerce Control List Supplement No. 1 to Part 774 Category 7—page 8 b. Gyros of any type, designed for use in inertial (see 22 CFR parts 120 through 130). navigation systems or in guidance systems of all Related Definitions: ‘Inertial measurement types, specified to function at acceleration levels equipment or systems’ specified in greater than 100 g. 7A103.a. incorporate accelerometers or gyros to measure changes in velocity and Technical Note: In this entry, the term orientation in order to determine or ‘stability’ is defined as a measure of the ability maintain heading or position without of a specific mechanism or performance requiring an external reference once coefficient to remain invariant when aligned. continuously exposed to a fixed operating Items: condition. (This definition does not refer to dynamic or servo stability.) (IEEE STD 528- a. ‘Inertial measurement equipment or systems’ 2001 paragraph 2.247) using accelerometers or gyros controlled by 7A001, 7A002, 7A101 or 7A102, and “specially designed” “parts” and “components” therefor; 7A103 Instrumentation, navigation equipment and systems, other than those Note 1: 7A103.a does not control equipment controlled by 7A003, and “specially containing accelerometers “specially designed” “parts” and “components” designed” and developed as MWD therefor, as follows (see List of Items (Measurement While Drilling) sensors for use in Controlled). down-hole well services operations.
License Requirements Note 2: 7A103.a does not control inertial or other equipment using accelerometers or gyros Reason for Control: MT, AT controlled by 7A001 or 7A002 that are only NS controlled. Country Chart Control(s) (See Supp. No. Note 3: 7A103.a. includes Attitude and 1 to part 738) Heading Reference Systems (AHRSs), MT applies to entire entry MT Column 1 gyrocompasses, Inertial Measurement Units AT applies to entire entry AT Column 1 (IMUs), Inertial Navigations Systems (INSs), Inertial Reference Systems (IRSs), and Inertial List Based License Exceptions (See Part 740 Reference Units (IRUs). for a description of all license exceptions) b. Integrated flight instrument systems, which LVS: N/A include gyrostabilizers or automatic pilots, GBS: N/A designed or modified for use in rockets, missiles, or unmanned aerial vehicles capable of List of Items Controlled achieving a “range” equal to or greater than 300 km, and “specially designed” “parts” and Related Controls: (1) See ECCN 7A003 “components” therefor. and 7A994. (2) Inertial navigation systems and inertial equipment, and c. Integrated Navigation Systems, designed or “specially designed” “parts” and modified for use in rockets, missiles, or “components” therefor specifically unmanned aerial vehicles capable of achieving a designed, modified or configured for “range” equal to or greater than 300 km and military use are “subject to the ITAR” capable of providing a navigational accuracy of
Export Administration Regulations Bureau of Industry and Security December 4, 2020 Commerce Control List Supplement No. 1 to Part 774 Category 7—page 9
200m Circular Error Probable (CEP) or less. are “subject to the ITAR” (see 22 CFR parts 120 through 130). (2) This entry Technical Note: An ‘integrated navigation controls “specially designed” “parts” and system’ typically incorporates the following “components” for gyro-astro compasses “parts” and “components”: and other devices controlled by 7A004. Related Definitions: N/A 1. An inertial measurement device (e.g., an Items: attitude and heading reference system, inertial reference unit, or inertial navigation system); The list of items controlled is contained in the ECCN heading. 2. One or more external sensors used to update the position and/or velocity, either periodically or continuously throughout the 7A105 Receiving equipment for ‘navigation flight (e.g., satellite navigation receiver, radar satellite systems’, having any of the following altimeter, and/or Doppler radar); and characteristics (see List of Items Controlled), and “specially designed” “parts” and 3. Integration hardware and software. “components” therefor.
License Requirements 7A104 Gyro-astro compasses and other devices, other than those controlled by Reason for Control: MT, AT 7A004, which derive position or orientation by means of automatically tracking celestial Country Chart bodies or satellites and “specially designed” Control(s) (See Supp. No. “parts” and “components” therefor. 1 to part 738) MT applies to entire entry MT Column 1 License Requirements AT applies to entire entry AT Column 1
Reason for Control: MT, AT List Based License Exceptions (See Part 740 for a description of all license exceptions) Country Chart Control(s) (See Supp. No. LVS: N/A 1 to part 738) GBS: N/A MT applies to entire entry MT Column 1 AT applies to entire entry AT Column 1 List of Items Controlled
List Based License Exceptions (See Part 740 Related Controls: (1) See also 7A005, for a description of all license exceptions) 7A611 and 7A994. (2) See USML Category XII(d) for GNSS receiving LVS: N/A equipment subject to the ITAR and USML GBS: N/A Category XI(c)(10) for antennae that are subject to the ITAR. (3) Items that otherwise would be covered by ECCN List of Items Controlled 7A105.b.2 are “subject to the ITAR” (see 22 CFR parts 120 through 130). (4) See Related Controls: (1) See USML Categories USML Category XII(d) for GPS receiving IV and XV for certain ‘star trackers’ that
Export Administration Regulations Bureau of Industry and Security December 4, 2020 Commerce Control List Supplement No. 1 to Part 774 Category 7—page 10
equipment in 7A105.a, b.1 and b.3 that are therefor. subject to the ITAR. Related Definitions: ‘Navigation satellite License Requirements systems’ include Global Navigation Satellite Systems (GNSS; e.g. GPS, Reason for Control: MT, AT GLONASS, Galileo or BeiDou) and Regional Navigation Satellite Systems Country Chart (RNSS; e.g. NavIC, QZSS). Control(s) (See Supp. No. Items: 1 to part 738) MT applies to entire entry MT Column 1 a. Designed or modified for use in “missiles”; or AT applies to entire entry AT Column 1 b. Designed or modified for airborne List Based License Exceptions (See Part 740 applications and having any of the following: for a description of all license exceptions)
b.1. Capable of providing navigation LVS: N/A information at speeds in excess of GBS: N/A 600 m/s; List of Items Controlled b.2. Employing decryption, designed or modified for military or governmental services, Related Controls: N/A to gain access to a ‘navigation satellite system’ Related Definitions: N/A secure signal/data; or Items:
b.3. Being “specially designed” to employ a. Internal tilt compensation in pitch (+/-90 anti-jam features (e.g., null steering antenna or degrees) and roll (+/-180 degrees) axes; electronically steerable antenna) to function in an environment of active or passive b. Azimuthal accuracy better (less) than 0.5 countermeasures. degrees rms at latitudes of +/-80 degrees, referenced to local magnetic field; and Note: 7A105.b.2 and 7A105.b.3 do not control equipment designed for commercial, civil or c. Designed or modified to be integrated with Safety of Life (e.g., data integrity, flight safety) flight control and navigation systems. 'navigation satellite system' services. Note: Flight control and navigation systems in 7A107 include gyrostabilizers, automatic 7A106 Altimeters, other than those pilots and inertial navigation systems. controlled by 7A006, of radar or laser radar type, designed or modified for use in “missiles”. (These items are “subject to the 7A115 Passive sensors for determining ITAR”. See 22 CFR parts 120 through 130.) bearing to specific electromagnetic sources (direction finding equipment) or terrain characteristics, designed or modified for use 7A107 Three axis magnetic heading sensors in “missiles”. (These items are “subject to the having all of the following characteristics (see ITAR”. See 22 CFR parts 120 through 130.) List of Items Controlled), and “specially designed” “parts” and “components”
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7A116 Flight control systems and “parts” c. Flight control servo valves designed of and “components”, as follows (see List of modified for the systems in 7A116.a or 7A116.b, Items Controlled). and designed or modified to operate in a vibration environment greater than 10 g rms License Requirements over the entire range between 20Hz and 2 kHz.
Reason for Control: MT, AT Note: This entry includes the systems, equipment and valves designed or modified to Country Chart enable operation of manned aircraft as Control(s) (See Supp. No. unmanned aerial vehicles. 1 to part 738) MT applies to entire entry MT Column 1 AT applies to entire entry AT Column 1 7A117 “Guidance sets” capable of achieving system accuracy of 3.33% or less of the range List Based License Exceptions (See Part 740 (e.g., a “CEP” of 10 km or less at a range of for a description of all license exceptions) 300 km). (These items are “subject to the ITAR”. See 22 CFR parts 120 through 130.) LVS: N/A GBS: N/A 7A611 Military fire control, laser, imaging, List of Items Controlled and guidance equipment, as follows (see List of Items Controlled). Related Controls: (1) See 9A610.r and 9A610.s for items designed or modified License Requirements for military UAVs. (2) See USML Category IV for items “specially Reason for Control: NS, MT, RS, AT, UN designed” for use in rockets or missiles that are “subject to the ITAR.” Country Chart Related Definitions: N/A Control(s) (See Supp. No. 1 Items: to part 738) NS applies to entire entry NS Column 1 a. Pneumatic, hydraulic, mechanical, electro- except 7A611.y optical, or electromechanical flight control MT applies to MT Column 1 systems (including fly-by-wire and fly-by-light commodities in 7A611.a systems) designed or modified for UAVs that meet or exceed the capable of delivering at least 500 kilograms of parameters in 7A103.b payload to a range of at least 300 km, other than or .c those controlled by either USML paragraph RS applies to entire entry RS Column 1 VIII(a) or ECCN 9A610.a; except 7A611.y RS applies to 7A611.y China, Russia, or b. Attitude control equipment designed or Venezuela (see modified for UAVs capable of delivering at least § 724.6(a)(7)) 500 kilograms of payload to a range of at least AT applies to entire entry AT Column 1 300 km, other than those controlled by either UN applies to entire entry See § 746.1(b) USML paragraph VIII(a) or ECCN 9A610.a; except 7A611.y for UN controls
List Based License Exceptions (See Part 740
Export Administration Regulations Bureau of Industry and Security December 4, 2020 Commerce Control List Supplement No. 1 to Part 774 Category 7—page 12 for a description of all license exceptions) 1. Enumerated or controlled in the USML or elsewhere within ECCN 7A611; LVS: $1500 GBS: N/A 2. Described in ECCNs 6A007, 6A107, 7A001, 7A002, 7A003, 7A101, 7A102 or 7A103; or Special Conditions for STA 3. Elsewhere specified in ECCN 7A611.y or STA: Paragraph (c)(2) of License 3A611.y. Exception STA (§ 740.20(c)(2) of the EAR) may not be used for any y. Specific “parts,” “components,” item in 7A611. “accessories,” and “attachments” “specially designed” for a commodity subject to control in List of Items Controlled this ECCN or a defense article in Category XII and not elsewhere specified on the USML or in Related Controls: (1) Military fire control, laser, the CCL, as follows, and “parts,” “components,” imaging, and guidance equipment that are “accessories,” and “attachments” “specially enumerated in USML Category XII, and designed” therefor: technical data (including software) directly related thereto, are subject to the ITAR. (2) y.1 [Reserved] See Related Controls in ECCNs 0A504, 2A984, 6A002, 6A003, 6A004, 6A005, 6A007, 6A008, 6A107, 7A001, 7A002, 7A994 Other navigation direction finding 7A003, 7A005, 7A101, 7A102, and 7A103. equipment, airborne communication (3) See ECCN 3A611 and USML Category XI equipment, all aircraft inertial navigation for controls on countermeasure equipment. systems not controlled under 7A003 or (4) See ECCN 0A919 for foreign-made 7A103, and other avionic equipment, “military commodities” that incorporate more including “parts” and “components,” n.e.s. than a de minimis amount of U.S. origin “600 series” controlled content. License Requirements Related Definitions: N/A Items: Reason for Control: AT a. Guidance or navigation systems, not Country Chart elsewhere specified on the USML, that are Control(s) (See Supp. No. 1 “specially designed” for a defense article on the to part 738) USML or for a 600 series item. AT applies to entire entry AT Column 1 b. to w. [Reserved] License Requirement Notes: Typically x. “Parts,” “components,” “accessories,” and commercially available GPS do not employ “attachments,” including accelerometers, gyros, decryption or adaptive antenna and are angular rate sensors, gravity meters classified as 7A994. (gravimeters), and inertial measurement units (IMUs), that are “specially designed” for List Based License Exceptions (See Part 740 defense articles controlled by USML Category for a description of all license exceptions) XII or items controlled by 7A611, and that are NOT: LVS: N/A
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GBS: N/A from the Control and Display Unit (CDU) or by the status message from the List of Items Controlled corresponding sub-system. By following the manufacturer’s manual, the cause of the Related Controls: See 7A005 and 7A105. failure may be localized at the level of the Related Definitions: N/A malfunctioning Line Replaceable Unit Items: (LRU). The operator then removes the LRU and replaces it with a spare. (2) The list of items controlled is contained in the ‘Maintenance Level II’: The defective LRU ECCN heading. is sent to the maintenance workshop (the manufacturer’s or that of the operator responsible for level II maintenance). At the B. TEST, INSPECTION AND maintenance workshop, the malfunctioning “PRODUCTION EQUIPMENT” LRU is tested by various appropriate means to verify and localize the defective Shop Replaceable Assembly (SRA) module 7B001 Test, calibration or alignment responsible for the failure. This SRA is equipment, “specially designed” for removed and replaced by an operative spare. equipment controlled by 7A (except 7A994). The defective SRA (or possibly the complete LRU) is then shipped to the License Requirements manufacturer. ‘Maintenance Level II’ does not include the disassembly or repair of Reason for Control: NS, MT, AT controlled accelerometers or gyro sensors. Items: Country Chart Control(s) (See Supp. No. The list of items controlled is contained in the 1 to part 738) ECCN heading. NS applies to entire entry NS Column 1 MT applies to entire entry MT Column 1 AT applies to entire entry AT Column 1 7B002 Equipment “specially designed” to characterize mirrors for ring “laser” gyros, List Based License Exceptions (See Part 740 as follows (see List of Items Controlled). for a description of all license exceptions) License Requirements LVS: N/A GBS: N/A Reason for Control: NS, MT, AT
List of Items Controlled Country Chart Control(s) (See Supp. No. Related Controls: (1) See also 7B101, 1 to part 738) 7B102 and 7B994. (2) This entry does not NS applies to entire entry NS Column 1 control test, calibration or alignment MT applies to entire entry MT Column 1 equipment for ‘Maintenance level I’ or AT applies to entire entry AT Column 1 ‘Maintenance Level II’. Related Definition: (1) ‘Maintenance Level List Based License Exceptions (See Part 740 I’: The failure of an inertial navigation unit for a description of all license exceptions) is detected on the “aircraft” by indications
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LVS: N/A IMU platform tester; IMU stable element GBS: N/A handling fixture; IMU platform balance fixture; gyro tuning test station; gyro List of Items Controlled dynamic balance station; gyro run- in/motor test station; gyro evacuation and Related Controls: See also 7B102 and fill station; centrifuge fixtures for gyro 7B994 bearings; accelerometer axis align Related Definitions: N/A stations; accelerometer test station; and Items: fiber optic gyro coil winding machines. Related Definitions: N/A a. Scatterometers having a measurement Items: “accuracy” of 10 ppm or less (better); The list of items controlled is contained in the b. Profilometers having a measurement ECCN heading. “accuracy” of 0.5 nm (5 angstrom) or less (better). 7B101 “Production equipment”, and other test, calibration, and alignment equipment, 7B003 Equipment “specially designed” for other than that described in 2B119 to 2B122, the “production” of equipment controlled by 7B003, and 7B102, designed or modified to be 7A (except 7A994). used with equipment controlled by 7A001 to 7A004 or 7A101 to 7A104. License Requirements License Requirements Reason for Control: NS, MT, AT Reason for Control: MT, AT Country Chart Control(s) (See Supp. No. Country Chart 1 to part 738) Control(s) (See Supp. No. NS applies to entire entry NS Column 1 1 to part 738) MT applies to entire entry MT Column 1 MT applies to entire entry MT Column 1 AT applies to entire entry AT Column 1 AT applies to entire entry AT Column 1
List Based License Exceptions (See Part 740 List Based License Exceptions (See Part 740 for a description of all license exceptions) for a description of all license exceptions)
LVS: N/A LVS: N/A GBS: N/A GBS: N/A
List of Items Controlled List of Items Controlled
Related Controls: (1) See also 7B103, (this Related Controls:1.) See also 2B119 to entry is “subject to the ITAR” (see 22 2B122, 7B003, 7B102, and 7B994. 2.) CFR parts 120 through 130)) and 7B994. This entry includes: inertial measurement (2) This entry includes: Inertial unit (IMU module) tester; IMU platform Measurement Unit (IMU module) tester; tester; IMU stable element handling
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fixture; IMU platform balance fixture; of 50 ppm or less (better). gyro tuning test station; gyro dynamic balance stations; gyro run-in/motor test c. Prolifometers having a threshold accuracy stations; gyro evacuation and filling of 0.5nm (5 angstrom) or less (better). stations; centrifuge fixtures for gyro bearings; accelerometer axis align stations; and accelerometer test stations. 7B103 “Specially designed” “production Related Definitions: N/A facilities” for equipment controlled by 7A117. Items: (These items are “subject to the ITAR”. See 22 CFR parts 120 through 130.) The list of items controlled is contained in the ECCN heading. 7B611 Test, inspection, and production commodities “specially designed” for 7B102 Equipment, other than those military fire control, laser, imaging, and controlled by 7B002, designed or modified to guidance equipment, as follows (see List of characterize mirrors, for laser gyro Items Controlled). equipment, as follows (see List of Items Controlled). License Requirements
License Requirements Reason for Control: NS, MT, RS, AT, UN
Reason for Control: MT, AT Country Chart Control(s) (See Supp. No. 1 Country Chart to part 738) Control(s) (See Supp. No. NS applies to entire entry NS Column 1 1 to part 738) MT applies to 7B611.a MT Column 1 MT applies to entire entry MT Column 1 commodities “specially AT applies to entire entry AT Column 1 designed” for 7A611.a commodities controlled List Based License Exceptions (See Part 740 for MT reasons for a description of all license exceptions) RS applies to entire entry RS Column 1 AT applies to entire entry AT Column 1 LVS: N/A UN applies to entire entry See § 746.1(b) GBS: N/A for UN controls
List of Items Controlled List Based License Exceptions (See Part 740 for a description of all license exceptions)
Related Controls: N/A LVS: $1500 Related Definitions: N/A GBS: N/A Items: Special Conditions for STA a. Scatterometers having a threshold accuracy of 10 ppm or less (better). STA: Paragraph (c)(2) of License Exception STA (§ 740.20(c)(2) of b. Reflectometers having a threshold accuracy the EAR) may not be used for any
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item in 7B611. Country Chart Control(s) (See Supp. No. 1 List of Items Controlled to part 738) AT applies to entire entry AT Column 1 Related Controls: N/A Related Definitions: N/A List Based License Exceptions (See Part 740 Items: for a description of all license exceptions) a. Test, inspection, and production end items LVS: N/A and equipment “specially designed” for the GBS: N/A “development,” “production,” repair, overhaul, or refurbishing of commodities controlled in List of Items Controlled ECCN 7A611 (except 7A611.y) or commodities in USML Category XII that are not enumerated Related Controls: N/A in USML Category XII or controlled by another Related Definitions: N/A “600 series” ECCN. Items: b. Environmental test facilities “specially The list of items controlled is contained in the designed” for the certification, qualification, or ECCN heading. testing of commodities controlled in ECCN 7A611 (except 7A611.y) or guidance equipment in USML Category XII that are not enumerated C. “MATERIALS” in USML Category XII or controlled by another [Reserved] “600 series” ECCN. c. Field test equipment “specially designed” to D. “SOFTWARE” evaluate or calibrate the operation of systems described in USML Category XII(a), (b), or (c). 7D001 “Software” “specially designed” or d. to w. [Reserved] modified for the “development” or “production” of equipment controlled by 7A x. “Parts,” “components,” “accessories,” and (except 7A994) or 7B (except 7B994). “attachments” that are “specially designed” for a commodity listed in this entry and that are not License Requirements enumerated on the USML or controlled by another “600 series” ECCN. Reason for Control: NS, MT, RS, AT
Country 7B994 Other equipment for the test, Chart (See Control(s) inspection, or “production” of navigation and Supp. No. 1 to avionics equipment. part 738) NS applies to software” for NS Column 1 License Requirements equipment controlled by 7A001 to 7A004, 7A006, Reason for Control: AT 7A008, 7B001, 7B002 or 7B003 MT applies to “software” for MT Column 1
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equipment controlled for Reason for Control: NS, MT, AT MT reasons. MT does not apply to “software” for Country Chart equipment controlled by Control(s) (See Supp. No. 7A008. 1 to part 738) RS applies to “software” for RS Column 1 NS applies to entire entry NS Column 1 inertial navigation systems MT applies to entire entry MT Column 1 and inertial equipment, and AT applies to entire entry AT Column 1 “components” therefor, for “9A991.b aircraft”. Reporting Requirements AT applies to entire entry AT Column 1 See § 743.1 of the EAR for reporting List Based License Exceptions (See Part 740 requirements for exports under License for a description of all license exceptions) Exceptions, and Validated End-User authorizations. TSR: N/A List Based License Exceptions (See Part 740 List of Items Controlled for a description of all license exceptions)
Related Controls: 1.) See also 7D101 and TSR: N/A 7D994. (2) The “software” related to 7A003.b, 7A005, 7A103.b, 7A105, List of Items Controlled 7A106, 7A115, 7A116, 7A117, or 7B103 is “subject to the ITAR” (see 22 CFR parts Related Controls: 1.) See also 7D102 and 120 through 130). (3) “Software” for 7D994. 2.) This entry does not control inertial navigation systems and inertial “source code” for the operation or equipment and “parts” or “components” maintenance of gimballed ‘AHRS’. “specially designed” therefor that are Related Definition: ‘AHRS’ generally differ directly related to defense articles and not from Inertial Navigation Systems (INS) in “specially designed” for use on civil that an ‘AHRS’ provides attitude and aircraft is “subject to the ITAR” (see 22 heading information and normally does CFR parts 120 through 130). not provide the acceleration, velocity and Related Definitions: N/A position information associated with an Items: INS. Items: The list of items controlled is contained in the ECCN heading. The list of items controlled is contained in the ECCN heading.
7D002 “Source code” for the operation or maintenance of any inertial navigation 7D003 Other “software” as follows (see List equipment, including inertial equipment not of Items Controlled). controlled by 7A003 or 7A004, or Attitude and Heading Reference Systems (‘AHRS’). License Requirements
License Requirements Reason for Control: NS, MT, AT
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Country Chart maps, magnetic maps or 3-D digital Control(s) (See Supp. No. 1 terrain maps. to part 738) Items: NS applies to entire entry NS Column 1 MT applies to “software” MT Column 1 a. “Software” “specially designed” or modified for equipment controlled to improve the operational performance or for MT reasons. MT reduce the navigational error of systems to the does not apply to levels controlled by 7A003, 7A004 or 7A008; “software” for equipment controlled by 7A008. b. “Source code” for hybrid integrated systems AT applies to entire entry AT Column 1 which improves the operational performance or reduces the navigational error of systems to the Reporting Requirements level controlled by 7A003 or 7A008 by continuously combining heading data with any See § 743.1 of the EAR for reporting of the following: requirements for exports under License Exceptions, and Validated End-User b.1. Doppler radar or sonar velocity data; authorizations. b.2. “Satellite navigation system” reference List Based License Exceptions (See Part 740 data; or for a description of all license exceptions) b.3. Data from ‘Data-Based Referenced Navigation’ (‘DBRN”) systems; TSR: N/A c. [Reserved] Special Conditions for STA d. [Reserved] STA: License Exception STA may not be used to ship or transmit software N.B. For flight control “source code,” see in 7D003.a or .b to any of the 7D004. destinations listed in Country Group A:6 (See Supplement No.1 e. Computer-Aided-Design (CAD) “software” to part 740 of the EAR). “specially designed” for the “development” of “active flight control systems”, helicopter multi- axis fly-by-wire or fly-by-light controllers or List of Items Controlled helicopter “circulation controlled anti-torque or circulation-controlled direction control Related Controls: See also 7D103 and systems”, whose “technology” is controlled by 7D994. 7E004.b.1, 7E004.b.3 to b.5, 7E004.b.7 to b.8, Related Definitions: ‘Data-Based 7E004.c.1 or 7E004.c.2. Referenced Navigation’ (‘DBRN’) systems are systems which use various sources of previously measured geo- 7D004 “Source code” incorporating mapping data integrated to provide “development” “technology” specified by accurate navigation information under 7E004.a.2, a.3, a.5, a.6 or 7E004.b, for any of dynamic conditions. Data sources include the following: (see List of Items Controlled). bathymetric maps, stellar maps, gravity License Requirements
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g. Three dimensional displays. Reason for Control: NS, AT Note: 7D004 does not apply to “source Country Chart code” associated with common computer Control(s) (See Supp. No. 1 elements and utilities (e.g., input signal to part 738) acquisition, output signal transmission, NS applies to entire entry NS Column 1 computer program and data loading, built-in AT applies to entire entry AT Column 1 test, task scheduling mechanisms) not providing a specific flight control system function. List Based License Exceptions (See Part 740 for a description of all license exceptions) 7D005 “Software” “specially designed” to TSR: N/A decrypt “Satellite navigation system” ranging signals designed for government use. Special Conditions for STA License Requirements STA: License Exception STA may not be used to ship or transmit “software” Reason for Control: NS, AT in 7D004.a to .d and .g to any of the destinations listed in Country Group Country Chart A:6 (See Supplement No.1 to part Control(s) (See Supp. No. 1 740 of the EAR). to part 738) NS applies to entire entry NS Column 1 List of Items Controlled AT applies to entire entry AT Column 1
Related Controls: See 7D103 and 7D994 List Based License Exceptions (See Part 740 Related Definitions: N/A for a description of all license exceptions) Items: TSR: N/A a. Digital flight management systems for “total control of flight”; List of Items Controlled b. Integrated propulsion and flight control Related Controls: N/A systems; Related Definitions: N/A Items: c. “Fly-by-wire systems” or “fly-by-light systems“; The list of items controlled is contained in the ECCN heading. d. Fault-tolerant or self-reconfiguring “active flight control systems”; 7D101 “Software” “specially designed” or modified for the “use” of equipment e. [Reserved]; controlled for missile technology (MT) reasons by 7A001 to 7A006, 7A101 to 7A107, f. Air data systems based on surface static data; 7A115, 7A116, 7A117, 7B001, 7B002, 7B003, or 7B101, 7B102, or 7B103.
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License Requirements List Based License Exceptions (See Part 740 Reason for Control: MT, AT for a description of all license exceptions)
Country Chart TSR: N/A Control(s) (See Supp. No. 1 to part 738) List of Items Controlled MT applies to entire entry MT Column 1 AT applies to entire entry AT Column 1 Related Controls: The “software” related to 7A003.b or 7A103.b is “subject to the List Based License Exceptions (See Part 740 ITAR” (see 22 CFR parts 120 through 130). for a description of all license exceptions) Related Definitions: N/A Items: TSR: N/A a. Integration “software” for the equipment List of Items Controlled controlled by 7A103.b.
Related Controls: (1) The “software” b. Integration “software” “specially designed” related to 7A003.b, 7A005, 7A103.b, for the equipment controlled by 7A003 or 7A105, 7A106, 7A115, 7A116, 7A117, or 7A103.a. 7B103 is “subject to the ITAR” (see 22 CFR parts 120 through 130). (2) “Software” for inertial navigation systems 7D103 “Software” “specially designed” for and inertial equipment and “parts” and modelling or simulation of the “guidance “components” “specially designed” sets” controlled by 7A117 or for their design therefor that are directly related to a integration with “missiles”. (This entry is defense article is “subject to the ITAR” “subject to the ITAR”. See 22 CFR parts120 (see 22 CFR parts 120 through 130). through 130.) Related Definitions: N/A Items: 7D611 “Software” “specially designed” for The list of items controlled is contained in the commodities controlled by 7A611 or ECCN heading. equipment controlled by 7B611, as follows (see List of Items Controlled).
7D102 Integration “software,” as follows (See License Requirements List of Items Controlled). Reason for Control: NS, MT, RS, AT, UN License Requirements Country Chart Reason for Control: MT, AT Control(s) (See Supp. No. 1 to part 738) Country Chart NS applies to entire entry NS Column 1 Control(s) (See Supp. No. except 7D611.y 1 to part 738) MT applies to 7D611.a MT Column 1 MT applies to entire entry MT Column 1 “software” “specially AT applies to entire entry AT Column 1 designed” for 7A611.a
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commodities controlled navigation, airborne communication and for MT reasons other avionics. RS applies to entire entry RS Column 1 except 7D611.y License Requirements RS applies to 7D611.y China, Russia, or Venezuela (see Reason for Control: AT § 724.6(a)(7)) AT applies to entire entry AT Column 1 Country Chart UN applies to entire See § 746.1(b) for Control(s) (See Supp. No. 1 entry except 7D611.y UN controls to part 738) AT applies to entire entry AT Column 1 List Based License Exceptions (See Part 740 for a description of all license exceptions) List Based License Exceptions (See Part 740 for a description of all license exceptions) TSR: N/A TSR: N/A Special Conditions for STA List of Items Controlled STA: Paragraph (c)(2) of License Exception STA (§ 740.20(c)(2) of Related Controls: N/A the EAR) may not be used for any Related Definitions: N/A software in 7D611. Items:
List of Items Controlled The list of items controlled is contained in the ECCN heading. Related Controls: “Software” directly related to articles enumerated in USML Category XII is subject of USML E. “TECHNOLOGY” paragraph XII(f). Related Definitions: N/A Items: 7E001 “Technology” according to the General Technology Note for the a. “Software” “specially designed” for the “development” of equipment or “software,” “development,” “production,” operation, or specified by 7A. (except 7A994), 7B. (except maintenance of commodities controlled by 7B994), 7D001, 7D002, 7D003 or 7D005. ECCNs 7A611 (except 7A611.y) or 7B611. License Requirements b. to x. [Reserved] Reason for Control: NS, MT, RS, AT y. Specific “software” “specially designed” for the “development,” “production,” operation, or Country Chart (See maintenance of commodities described in Control(s) 7A611.y. Supp. No. 1 to part 738) NS applies to technology” NS Column 1 7D994 “Software”, n.e.s., for the for items controlled by “development”, “production”, or “use” of 7A001 to 7A004, 7A006,
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7A008, 7B001 to 7B003, 7A106, 7A115, 7A116, 7A117, 7B103, 7D001 to 7D005. software in 7D101 specified in the Related MT applies to “technology” MT Column 1 Controls paragraph of ECCN 7D101, for equipment controlled for 7D102.a, or 7D103 is “subject to the MT reasons. MT does not ITAR” (see 22 CFR parts 120 through apply to “technology” for 130). equipment controlled by Related Definitions: N/A 7A008. MT does apply to Items: “technology” for equipment specified in 7A001, 7A002 The list of items controlled is contained in the or 7A003.d that meets or ECCN heading. exceeds parameters of 7A101, 7A102 or 7A103. Note: 7E001 includes key management RS applies to “technology” RS Column 1 “technology” exclusively for equipment for inertial navigation specified in 7A005.a. systems or inertial equipment, and “components” therefor, for 7E002 “Technology” according to the 9A991.b aircraft. General Technology Note for the AT applies to entire entry AT Column 1 “production” of equipment controlled by 7A (except 7A994) or 7B (except 7B994). Reporting Requirements License Requirements See § 743.1 of the EAR for reporting requirements for exports under License Reason for Control: NS, MT, RS, AT Exceptions, and Validated End-User authorizations. Country Chart (See Control(s) List Based License Exceptions (See Part 740 Supp. No. 1 to for a description of all license exceptions) part 738) NS applies to “technology” NS Column 1 TSR: N/A for equipment controlled by Special Conditions for STA 7A001 to 7A004, 7A006, 7A008 or 7B001 to 7B003 STA: License Exception STA may not be MT applies to MT Column 1 used to ship or transmit any “technology” for technology in this entry to any of the equipment controlled for destinations listed in Country Group MT reasons. MT does not A:6 (See Supplement No.1 to part apply to “technology” for 740 of the EAR). equipment controlled by 7A008. MT does apply to List of Items Controlled “technology” for equipment specified in Related Controls: 1) See also 7E101 and 7A001, 7A002 or 7A003.d 7E994. 2) The “technology” related to that meets or exceeds 7A003.b, 7A005, 7A103.b, 7A105, parameters of 7A101,
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7A102 or 7A103. refurbishing or overhaul of equipment RS applies to “technology” RS Column 1 controlled by 7A001 to 7A004. for inertial navigation systems or inertial License Requirements equipment, and “components” therefor, for Reason for Control: NS, MT, AT 9A991.b aircraft. AT applies to entire entry AT Column 1 Country Chart Control(s) (See Supp. No. Reporting Requirements 1 to part 738) NS applies to entire entry NS Column 1 See § 743.1 of the EAR for reporting MT applies to entire entry MT Column 1 requirements for exports under License AT applies to entire entry AT Column 1 Exceptions, and Validated End-User authorizations. List Based License Exceptions (See Part 740 for a description of all license exceptions) List Based License Exceptions (See Part 740 for a description of all license exceptions) TSR: N/A
TSR: N/A List of Items Controlled
Special Conditions for STA Related Controls: See also 7E994. This entry does not control “technology” for STA: License Exception STA may not maintenance directly associated with be used to ship or transmit any calibration, removal or replacement of technology in this entry to any of damaged or unserviceable LRUs and the destinations listed in Country SRAs of a “civil aircraft” as described in Group A:6 (See Supplement No.1 ‘Maintenance Level I’ or ‘Maintenance to part 740 of the EAR). Level II’. Related Definition: Refer to the Related List of Items Controlled Definitions for 7B001 for ‘Maintenance Level I’ or ‘Maintenance Level II’. Related Controls: (1) See also 7E102 and Items: 7E994. (2) The “technology” related to 7A003.b, 7A005, 7A103.b, 7A105, 7A106, The list of items controlled is contained in the 7A115, 7A116, 7A117, or 7B103 is “subject ECCN heading. to the ITAR” (see 22 CFR parts 120 through 130). Related Definitions: N/A 7E004 Other “technology” as follows (see Items: List of Items Controlled).
The list of items controlled is contained in the License Requirements ECCN heading. Reason for Control: NS, MT, AT
Country 7E003 “Technology” according to the Control(s) General Technology Note for the repair, Chart (See
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Supp. No. 1 to of an unmanned aerial vehicle. part 738) Related Definitions: “Primary flight NS applies to entire entry NS Column 1 control” means an “aircraft” stability or MT applies to MT Column 1 maneuvering control using force/moment “technology” generators, i.e., aerodynamic control for equipment or systems surfaces or propulsive thrust vectoring. controlled for MT reasons. Items: AT applies to entire entry AT Column 1 a. “Technology” for the “development” or List Based License Exceptions (See Part 740 “production” of any of the following: for a description of all license exceptions) a.1. [Reserved] TSR: N/A a.2. Air data systems based on surface static Special Conditions for STA data only, i.e., which dispense with conventional air data probes; STA: (1) Paragraph (c)(1) of License Exception STA (§ 740.20(c)(1) of a.3. Three dimensional displays for the EAR) may not be used for “aircraft”; 7E004, except for 7E004.a.7. (2) Paragraph (c)(2) of License a.4. [Reserved] Exception STA (§ 740.20(c)(2) of the EAR) may not be used for a.5. Electric actuators (i.e., 7E004, except for 7E004.a.7. electromechanical, electrohydrostatic and integrated actuator package) “specially List of Items Controlled designed” for ‘primary flight control’;
Related Controls: (1) See also 7E001, Technical Note: ‘Primary flight control’ is 7E002, 7E101, and 7E994. (2) In addition “aircraft” stability or maneuvering control to the Related Controls in 7E001, 7E002, using force/moment generators, i.e., and 7E101 that include MT controls, also aerodynamic control surfaces or propulsive see the MT controls in 7E104 for design thrust vectoring. “technology” for the integration of the flight control, guidance, and propulsion a.6. ‘Flight control optical sensor array’ data into a flight management system, “specially designed” for implementing “active designed or modified for rockets or flight control systems”; or missiles capable of achieving a “range” equal to or greater than 300 km, for Technical Note: A ‘flight control optical optimization of rocket system trajectory; sensor array’ is a network of distributed optical and also see 9E101 for design sensors, using “laser” beams, to provide real- “technology” for integration of air vehicle time flight control data for on-board processing. fuselage, propulsion system and lifting control surfaces, designed or modified for a.7. “DBRN” systems designed to navigate unmanned aerial vehicles capable of underwater, using sonar or gravity databases, achieving a “range” equal to or greater that provide a positioning “accuracy” equal to or than 300 km, to optimize aerodynamic less (better) than 0.4 nautical miles; performance throughout the flight regime
Export Administration Regulations Bureau of Industry and Security December 4, 2020 Commerce Control List Supplement No. 1 to Part 774 Category 7—page 25 b. “Development” “technology”, as follows, for 2. “Technology” for “aircraft” flight “active flight control systems” (including “fly- instrument systems integrated solely for VOR, by-wire systems” or “fly-by-light systems”): DME, ILS or MLS navigation or approaches.
b.1. Photonic-based “technology” for Technical Note: ‘Flight path optimization’ sensing “aircraft” or flight control component is a procedure that minimizes deviations from a state, transferring flight control data, or four-dimensional (space and time) desired commanding actuator movement, “required” for trajectory based on maximizing performance or “fly-by-light systems” “active flight control effectiveness for mission tasks. systems”; b.6. [Reserved] b.2. [Reserved] b.7. “Technology” “required” for deriving b.3. Real-time algorithms to analyze the functional requirements for “fly-by-wire component sensor information to predict and systems” having all of the following: preemptively mitigate impending degradation and failures of components within an “active b.7.a. ‘Inner-loop’ airframe stability flight control system”; controls requiring loop closure rates of 40 Hz or greater; and Note: 7E004.b.3 does not include algorithms for purpose of off-line maintenance. Technical Note: ‘Inner-loop’ refers to functions of “active flight control systems” that b.4. Real-time algorithms to identify automate airframe stability controls. component failures and reconfigure force and moment controls to mitigate “active flight b.7.b. Having any of the following: control system” degradations and failures; b.7.b.1. Corrects an Note: 7E004.b.4 does not include aerodynamically unstable airframe, measured at algorithms for the elimination of fault effects any point in the design flight envelope, that through comparison of redundant data sources, would lose recoverable control if not corrected or off-line pre-planned responses to anticipated within 0.5 seconds; failures. b.7.b.2. Couples controls in two or b.5. Integration of digital flight control, more axes while compensating for ‘abnormal navigation and propulsion control data, into a changes in aircraft state’; digital flight management system for “total control of flight”; Technical Note: ‘Abnormal changes in aircraft state’ include in-flight structural Note: 7E004.b.5 does not apply to: damage, loss of engine thrust, disabled control surface, or destabilizing shifts in cargo load. 1. “Technology” for integration of digital flight control, navigation and propulsion b.7.b.3. Performs the functions control data, into a digital flight management specified in 7E004.b.5; or system for ‘flight path optimization’; Note: 7E004.b.7.b.3 does not apply to autopilots.
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b.7.b.4. Enables ”aircraft” to have geometry airfoils’, for use in systems using stable controlled flight, other than during take- individual blade control. off or landing, at greater than 18 degrees angle of attack, 15 degrees side slip, 15 Technical Note: ‘Variable geometry degrees/second pitch or yaw rate, or 90 airfoils’ use trailing edge flaps or tabs, or degrees/second roll rate; leading edge slats or pivoted nose droop, the position of which can be controlled in flight. b.8. “Technology” “required” for deriving the functional requirements of “fly-by-wire systems” to achieve all of the following: 7E101 “Technology”, according to the General Technology Note for the “use” of b.8.a. No loss of control of equipment controlled by 7A001 to 7A006, the ”aircraft” in the event of a consecutive 7A101 to 7A107, 7A115 to 7A117, 7B001, sequence of any two individual faults within the 7B002, 7B003, 7B101, 7B102, 7B103, or “fly-by-wire system”; and 7D101 to 7D103 for MT reasons.
b.8.b. Probability of loss of control of License Requirements the ”aircraft” being less (better) than 1x10-9 failures per flight hour; Reason for Control: MT, RS, AT
Note: 7E004.b does not apply to Country “technology” associated with common Chart (See Control(s) computer elements and utilities (e.g., input Supp. No. 1 to signal acquisition, output signal transmission, part 738) computer program and data loading, built-in MT applies to entire entry MT Column 1 test, task scheduling mechanisms) not providing RS applies to “technology” RS Column 1 a specific flight control system function. required for the use of inertial navigation systems, c. “Technology” for the “development” of or inertial equipment, or helicopter systems, as follows: “specially designed” “parts” and “components” c.1. Multi-axis fly-by-wire or fly-by-light therefor, “specially controllers, which combine the functions of at designed” for 9A991.b least two of the following into one controlling aircraft. element: AT applies to entire entry AT Column 1
c.1.a. Collective controls; List Based License Exceptions (See Part 740 for a description of all license exceptions) c.1.b. Cyclic controls; TSR: N/A c.1.c. Yaw controls; List of Items Controlled c.2. “Circulation-controlled anti-torque or circulation-controlled direction control Related Controls: The “technology” related systems”; to 7A003.b, 7A005, 7A103.b, 7A105, 7A106, 7A115, 7A116, 7A117, 7B103, c.3. Rotor blades incorporating ‘variable software specified in the Related Controls
Export Administration Regulations Bureau of Industry and Security December 4, 2020 Commerce Control List Supplement No. 1 to Part 774 Category 7—page 27
paragraph of ECCN 7D101, 7D102.a, or 7E104 Design “Technology” for the 7D103 is “subject to the ITAR” (see 22 integration of the flight control, guidance, CFR parts 120 through 130). and propulsion data into a flight management Related Definitions: N/A system, designed or modified for rockets or Items: missiles capable of achieving a “range” equal to or greater than 300 km, for optimization of The list of items controlled is contained in the rocket system trajectory. (This entry is ECCN heading. “subject to the ITAR”. See 22 CFR parts 120 through 130.)
7E102 “Technology” for protection of avionics and electrical subsystems against 7E611 “Technology” “required” for the electromagnetic pulse (EMP) and “development,” “production,” operation, electromagnetic interference (EMI) hazards, installation, maintenance, repair, overhaul or from external sources, as follows (see List of refurbishing of commodities controlled by Items Controlled). 7A611, commodities controlled by 7B611, or software controlled by 7D611, as follows (see License Requirements List of Items Controlled).
Reason for Control: MT, AT License Requirements
Country Chart Reason for Control: NS, MT, RS, AT, UN Control(s) (See Supp. No. 1 to part 738) Country Chart MT applies to entire entry MT Column 1 Control(s) (See Supp. No. 1 AT applies to entire entry AT Column 1 to part 738) NS applies to entire entry NS Column 1 List Based License Exceptions (See Part 740 except 7E611.y for a description of all license exceptions) MT applies to MT Column 1 “technology” in 7E611.a TSR: N/A if “required” for items controlled for MT reasons List of Items Controlled in 7A611.a, 7B611.a, or 7D611.a Related Controls: N/A RS applies to 7E611.y China, Russia, or Related Definitions: N/A Venezuela (see Items: § 724.6(a)(7)) RS applies to entire entry RS Column 1 a. Design “technology” for shielding systems; except 7E611.y AT applies to entire entry AT Column 1 b. Design “technology” for the configuration of UN applies to entire entry See § 746.1(b) hardened electrical circuits and subsystems; except 7E611.y for UN controls c. Design “technology” for the determination of List Based License Exceptions (See Part 740 hardening criteria of .a and .b of this entry. for a description of all license exceptions)
TSR: N/A
Export Administration Regulations Bureau of Industry and Security December 4, 2020 Commerce Control List Supplement No. 1 to Part 774 Category 7—page 28
other avionics equipment. Special Conditions for STA License Requirements STA: Paragraph (c)(2) of License Exception STA (§ 740.20(c)(2) of Reason for Control: AT the EAR) may not be used for any technology in 7E611. Country Chart Control(s) (See Supp. No. 1 List of Items Controlled to part 738) AT applies to entire entry AT Column 1 Related Controls: Technical data directly related to articles enumerated in USML List Based License Exceptions (See Part 740 Category XII are subject to the control of for a description of all license exceptions) USML Category XII(f). Related Definitions: N/A TSR: N/A Items: List of Items Controlled a. “Technology” “required” for the “development,” “production,” operation, Related Controls: N/A installation, maintenance, repair, overhaul, or Related Definitions: N/A refurbishing of commodities or “software” Items: controlled by ECCN 7A611 (except 7A611.y), 7B611, or 7D611 (except 7D611.y). The list of items controlled is contained in the ECCN heading. b. through .x [Reserved] y. Specific “technology” “required” for the EAR99 Items subject to the EAR that are not “production,” “development,” operation, elsewhere specified in this CCL Category or installation, maintenance, repair, or overhaul of in any other category in the CCL are commodities or software controlled by ECCNs designated by the number EAR99. 7A611.y or 7D611.y.
7E994 “Technology,” n.e.s., for the “development,” “production” or “use” of navigation, airborne communication, and
Export Administration Regulations Bureau of Industry and Security December 4, 2020