i.1. Uses only published or commercial cryptographic standards;
and
    i.2. Is any of the following:
    i.2.a. Integral to a CPU that meets the provisions of Note 3 in
Category 5--Part 2;
    i.2.b. Integral to an operating system that is not specified by
5D002; or
    i.2.c. Limited to ``OAM'' of the equipment.

    b. Designed or modified for converting, by means of
``cryptographic activation'', an item not specified by Category 5--
Part 2 into an item specified by 5A002.a or 5D002.c.1, and not
released by the Cryptography Note (Note 3 in Category 5--Part 2), or
for enabling, by means of ``cryptographic activation'', additional
functionality specified by 5A002.a of an item already specified by
Category 5--Part 2;
    c. Designed or modified to use or perform ``quantum
cryptography'';

    Technical Note: ``Quantum cryptography'' is also known as
Quantum Key Distribution (QKD).

    d. Designed or modified to use cryptographic techniques to
generate channelizing codes, scrambling codes or network
identification codes, for systems using ultra-wideband modulation
techniques and having any of the following:
    d.1. A bandwidth exceeding 500 MHz; or
    d.2. A ``fractional bandwidth'' of 20% or more;
    e. Designed or modified to use cryptographic techniques to
generate the spreading code for ``spread spectrum'' systems, not
specified by 5A002.d, including the hopping code for ``frequency
hopping'' systems.

0
46. In supplement no. 1 to part 774, Category 5, part 2, ECCN 5D002 is
revised to read as follows:

5D002 ``Software'' as follows (see List of Items Controlled).

License Requirements

Reason for Control: NS, AT, EI

                                              Country chart  (see Supp.
                Control(s)                       No. 1  to part 738)

NS applies to entire entry................  NS Column 1
AT applies to entire entry................  AT Column 1
EI applies to ``software'' in 5D002.a.1,    Refer to Sec.   742.15 of
 a.3, .b, c.1 and c.3, for commodities or    the EAR
 ``software'' controlled for EI reasons in  Note: Encryption software is
 ECCNs 5A002, 5A004 or 5D002.                controlled because of its
                                             functional capacity, and
                                             not because of any
                                             informational value of such
                                             software; such software is
                                             not accorded the same
                                             treatment under the EAR as
                                             other ``software'; and for
                                             export licensing purposes,
                                             encryption software is
                                             treated under the EAR in
                                             the same manner as a
                                             commodity included in ECCN
                                             5A002

    License Requirements Note: See Sec.  744.17 of the EAR for
additional license requirements for microprocessors having a
processing speed of 5 GFLOPS or more and an arithmetic logic unit
with an access width of 32 bit or more, including those
incorporating ``information security'' functionality, and associated
``software'' and ``technology'' for the ``production'' or
``development'' of such microprocessors.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

CIV: N/A
TSR: N/A
ENC: Yes for certain EI controlled software, see Sec.  740.17 of the
EAR for eligibility.

List of Items Controlled

Related Controls: After classification or self-classification in
accordance with Sec.  740.17(b) of the EAR, mass market encryption
software that meet eligibility requirements are released from ``EI''
and ``NS'' controls. This software is designated as 5D992.c.
Related Definitions: 5D002.a controls ``software'' designed or
modified to use ``cryptography'' employing digital or analog
techniques to ensure ``information security''.
Items:

    a. ``Software'' ``specially designed'' or modified for the
``development'', ``production'' or ``use'' of any of the following:
    a.1. Equipment specified by 5A002 or ``software'' specified by
5D002.c.1;
    a.2. Equipment specified by 5A003 or ``software'' specified by
5D002.c.2; or
    a.3. Equipment specified by 5A004 or ``software'' specified by
5D002.c.3;
    b. ``Software'' designed or modified for converting, by means of
``cryptographic activation'', an item not specified by Category 5--
Part 2 into an item specified by 5A002.a or 5D002.c.1, and not
released by the Cryptography Note (Note 3 in Category 5--Part 2), or
for enabling, by means of ``cryptographic activation'', additional
functionality specified by 5A002.a of an item already specified by
Category 5--Part 2;
    c. ``Software'' having the characteristics of, or performing or
simulating the functions of, any of the following:
    c.1.Equipment specified by 5A002.a, .c, .d or .e;

    Note:  5D002.c.1 does not apply to ``software'' limited to the
tasks of ``OAM'' implementing only published or commercial
cryptographic standards.

    c.2. Equipment specified by 5A003; or
    c.3. Equipment specified by 5A004.
    d. [Reserved]

    N.B.: See 5D002.b for items formerly specified in 5D002.d.

0
47. In supplement no. 1 to part 774, Category 5, part 2, ECCN 5E002 is
revised to read as follows:

5E002 ``Technology'' as follows (see List of Items Controlled).

License Requirements

Reason for Control: NS, AT, EI

                                              Country chart  (see Supp.
                Control(s)                       No. 1  to part 738)

NS applies to entire entry................  NS Column 1
AT applies to entire entry................  AT Column 1
EI applies to ``technology'' in 5E002.a     Refer to Sec.   742.15 of
 for commodities or ``software''             the EAR
 controlled for EI reasons in ECCNs 5A002,
 5A004 or 5D002, and to ``technology'' in
 5E002.b.

    License Requirements Notes: (1) See Sec.  744.17 of the EAR for
additional license requirements for microprocessors having a
processing speed of 5 GFLOPS or more and an arithmetic logic unit
with an access width of 32 bit or more, including those
incorporating ``information security'' functionality, and associated
``software'' and ``technology'' for the ``production'' or
``development'' of such microprocessors.
    (2) When a person performs or provides technical assistance that
incorporates, or otherwise draws upon, ``technology'' that was
either obtained in the United States or is of US-origin, then a
release of the ``technology'' takes place. Such technical
assistance, when rendered with the intent to aid in the
``development'' or ``production'' of encryption commodities or
software that would be controlled for ``EI'' reasons under ECCN
5A002, 5A004 or 5D002, may require authorization under the EAR even
if the underlying encryption algorithm to be implemented is from the
public domain or is not of U.S.-origin.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

CIV: N/A
TSR: N/A
ENC: Yes for certain EI controlled technology, see Sec.  740.17 of
the EAR for eligibility.

List of Items Controlled

Related Controls: See also 5E992. This entry does not control
``technology'' ``required'' for the ``use'' of equipment excluded
from control under the Related Controls paragraph or the Technical
Notes in ECCN 5A002 or ``technology'' related to equipment excluded
from control under ECCN 5A002.
Related Definitions: N/A
Items:

    a. ``Technology'' according to the General Technology Note for
the ``development'', ``production'' or ``use'' of equipment
controlled by 5A002, 5A003, 5A004 or 5B002, or of ``software''
controlled by 5D002.a or 5D002.c.
    b. ``Technology'' for converting, by means of ``cryptographic
activation'', an item not specified by Category 5--Part 2 into an
item specified by 5A002.a or 5D002.c.1, and not released by the
Cryptography Note (Note 3 in Category 5--Part 2), or for enabling,
by means of ``cryptographic activation'', additional functionality
specified by 5A002.a of an item already specified by Category 5--
Part 2.

    Note:  5E002 includes ``information security'' technical data
resulting from procedures carried out to evaluate or determine the
implementation of functions, features or techniques specified in
Category 5 Part 2.

0
48. In supplement no. 1 to part 774, Category 6, ECCN 6A002 is revised
to read as follows:

6A002 Optical sensors and equipment, and ``components'' therefor, as
follows (see List of Items Controlled).

License Requirements

Reason for Control: NS, MT, CC, RS, AT, UN

                                            Country chart (see Supp. No.
                Control(s)                         1 to part 738).

NS applies to entire entry................  NS Column 2

MT applies to optical detectors in          MT Column 1
 6A002.a.1, or a.3 that are ``specially
 designed'' or modified to protect
 ``missiles'' against nuclear effects
 (e.g., Electromagnetic Pulse (EMP), X-
 rays, combined blast and thermal
 effects), and usable for ``missiles''.
RS applies to 6A002.a.1, a.2, a.3 (except   RS Column 1
 a.3.d.2.a and a.3.e for lead selenide
 based focal plane arrays (FPAs)), .c, and
 .f.
CC applies to police-model infrared         CC Column 1
 viewers in 6A002.c.
AT applies to entire entry................  AT Column 1
UN applies to 6A002.a.1, a.2, a.3 and .c..  See Sec.   746.1(b) of the
                                             EAR for UN controls.

Reporting Requirements

See Sec.  743.1 of the EAR for reporting requirements for exports
under License Exceptions, and Validated End-User authorizations.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

LVS: $500 for 6A002.f.
$3,000; except N/A for MT and for 6A002.a.1, a.2, a.3, .c, and .f.
GBS: N/A
CIV: N/A

List of Items Controlled

Related Controls: (1) See USML Category XII(e) for infrared focal
plane arrays, image intensifier tubes, and related parts and
components, subject to the ITAR. (2) See USML Category XV(e) for
space-qualified focal plane arrays subject to the ITAR. (3) See also
ECCNs 6A102, 6A202, and 6A992. (4) See ECCN 0A919 for foreign-made
military commodities that incorporate commodities described in
6A002. (5) Section 744.9 of the EAR imposes a license requirement on
commodities described in ECCN 6A002 if being exported, reexported,
or transferred (in-country) for use by a military end-user or for
incorporation into an item controlled by ECCN 0A919. (6) See USML
Categories XII(e) and XV(e)(3) for read-out integrated circuits
``subject to the ITAR.''
Related Definitions: N/A
Items:

    a. Optical detectors as follows:
    a.1. ``Space-qualified'' solid-state detectors as follows:

    Note:  For the purpose of 6A002.a.1, solid-state detectors
include ``focal plane arrays''.

    a.1.a. ``Space-qualified'' solid-state detectors having all of
the following:
    a.1.a.1. A peak response in the wavelength range exceeding 10 nm
but not exceeding 300 nm; and
    a.1.a.2. A response of less than 0.1% relative to the peak
response at a wavelength exceeding 400 nm;
    a.1.b. ``Space-qualified'' solid-state detectors having all of
the following:
    a.1.b.1. A peak response in the wavelength range exceeding 900
nm but not exceeding 1,200 nm; and
    a.1.b.2. A response ``time constant'' of 95 ns or less;
    a.1.c. ``Space-qualified'' solid-state detectors having a peak
response in the wavelength range exceeding 1,200 nm but not
exceeding 30,000 nm;
    a.1.d. ``Space-qualified'' ``focal plane arrays'' having more
than 2,048 elements per array and having a peak response in the
wavelength range exceeding 300 nm but not exceeding 900 nm;
    a.2. Image intensifier tubes and ``specially designed''
``components'' therefor, as follows:

    Note:  6A002.a.2 does not control non-imaging photomultiplier
tubes having an electron sensing device in the vacuum space limited
solely to any of the following:

    a. A single metal anode; or
    b. Metal anodes with a center to center spacing greater than 500
[mu]m.

    Technical Note:  `Charge multiplication' is a form of electronic
image amplification and is defined as the generation of charge
carriers as a result of an impact ionization gain process. `Charge
multiplication' sensors may take the form of an image intensifier
tube, solid state detector or ``focal plane array''.

    a.2.a. Image intensifier tubes having all of the following:
    a.2.a.1. A peak response in the wavelength range exceeding 400
nm but not exceeding 1,050 nm;
    a.2.a.2. Electron image amplification using any of the
following:
    a.2.a.2.a. A microchannel plate with a hole pitch (center-to-
center spacing) of 12 [mu]m or less; or
    a.2.a.2.b. An electron sensing device with a non-binned pixel
pitch of 500 [mu]m or less, ``specially designed'' or modified to
achieve `charge multiplication' other than by a microchannel plate;
and
    a.2.a.3. Any of the following photocathodes:
    a.2.a.3.a. Multialkali photocathodes (e.g., S-20 and S-25)
having a luminous sensitivity exceeding 350 [mu]A/lm;
    a.2.a.3.b. GaAs or GaInAs photocathodes; or
    a.2.a.3.c. Other ``III-V compound'' semiconductor photocathodes
having a maximum ``radiant sensitivity'' exceeding 10 mA/W;
    a.2.b. Image intensifier tubes having all of the following:
    a.2.b.1. A peak response in the wavelength range exceeding 1,050
nm but not exceeding 1,800 nm;
    a.2.b.2. Electron image amplification using any of the
following:
    a.2.b.2.a. A microchannel plate with a hole pitch (center-to-
center spacing) of 12 [mu]m or less; or
    a.2.b.2.b. An electron sensing device with a non-binned pixel
pitch of 500 [mu]m or less, ``specially designed'' or modified to
achieve `charge multiplication' other than by a microchannel plate;
and
    a.2.b.3. ``III/V compound'' semiconductor (e.g., GaAs or GaInAs)
photocathodes and transferred electron photocathodes, having a
maximum ``radiant sensitivity'' exceeding 15 mA/W;
    a.2.c. ``Specially designed'' ``components'' as follows:
    a.2.c.1. Microchannel plates having a hole pitch (center-to-
center spacing) of 12 [mu]m or less;
    a.2.c.2. An electron sensing device with a non-binned pixel
pitch of 500 [mu]m or less, ``specially designed'' or modified to
achieve `charge multiplication' other than by a microchannel plate;
    a.2.c.3. ``III-V compound'' semiconductor (e.g., GaAs or GaInAs)
photocathodes and transferred electron photocathodes;

    Note: 6A002.a.2.c.3 does not control compound semiconductor
photocathodes designed to achieve a maximum ``radiant sensitivity''
of any of the following:
    a. 10 mA/W or less at the peak response in the wavelength range
exceeding 400 nm but not exceeding 1,050 nm; or
    b. 15 mA/W or less at the peak response in the wavelength range
exceeding 1,050 nm but not exceeding 1,800 nm.

    a.3. Non-``space-qualified'' ``focal plane arrays'' as follows:

    N.B.:  `Microbolometer' non-``space-qualified'' ``focal plane
arrays'' are only specified by 6A002.a.3.f.

    Technical Note:  Linear or two-dimensional multi-element
detector arrays are referred to as ``focal plane arrays'';

    Note 1: 6A002.a.3 includes photoconductive arrays and
photovoltaic arrays.

    Note 2: 6A002.a.3 does not control:
    a. Multi-element (not to exceed 16 elements) encapsulated
photoconductive cells using either lead sulphide or lead selenide;
    b. Pyroelectric detectors using any of the following:
    b.1. Triglycine sulphate and variants;
    b.2. Lead-lanthanum-zirconium titanate and variants;
    b.3. Lithium tantalate;
    b.4. Polyvinylidene fluoride and variants; or
    b.5. Strontium barium niobate and variants.
    c. ``Focal plane arrays'' ``specially designed'' or modified to
achieve `charge multiplication' and limited by design to have a
maximum ``radiant sensitivity'' of 10 mA/W or less for wavelengths
exceeding 760 nm, having all of the following:
    c.1. Incorporating a response limiting mechanism designed not to
be removed or modified; and
    c.2. Any of the following:
    c.2.a. The response limiting mechanism is integral to or
combined with the detector element; or
    c.2.b. The ``focal plane array'' is only operable with the
response limiting mechanism in place.

    d. Thermopile arrays having less than 5,130 elements;

    Technical Note:  A response limiting mechanism integral to the
detector element is designed not to be removed or modified without
rendering the detector inoperable.

    a.3.a. Non-``space-qualified'' ``focal plane arrays'' having all
of the following:
    a.3.a.1. Individual elements with a peak response within the
wavelength range exceeding 900 nm but not exceeding 1,050 nm; and
    a.3.a.2. Any of the following:
    a.3.a.2.a. A response ``time constant'' of less than 0.5 ns; or
    a.3.a.2.b. ``Specially designed'' or modified to achieve `charge
multiplication' and having a maximum ``radiant sensitivity''
exceeding 10 mA/W;
    a.3.b. Non-``space-qualified'' ``focal plane arrays'' having all
of the following:
    a.3.b.1. Individual elements with a peak response in the
wavelength range exceeding 1,050 nm but not exceeding 1,200 nm; and
    a.3.b.2. Any of the following:
    a.3.b.2.a. A response ``time constant'' of 95 ns or less; or
    a.3.b.2.b. ``Specially designed'' or modified to achieve `charge
multiplication' and having a maximum ``radiant sensitivity''
exceeding 10 mA/W;
    a.3.c. Non-``space-qualified'' non-linear (2-dimensional)
``focal plane arrays'' having individual elements with a peak
response in the wavelength range exceeding 1,200 nm but not
exceeding 30,000 nm;

    N.B.:  Silicon and other material based `microbolometer' non-
``space-qualified'' ``focal plane arrays'' are only specified by
6A002.a.3.f.

    a.3.d. Non-``space-qualified'' linear (1-dimensional) ``focal
plane arrays'' having all of the following:
    a.3.d.1. Individual elements with a peak response in the
wavelength range exceeding 1,200 nm but not exceeding 3,000 nm; and
    a.3.d.2. Any of the following:
    a.3.d.2.a. A ratio of `scan direction' dimension of the detector
element to the `cross-scan direction' dimension of the detector
element of less than 3.8; or
    a.3.d.2.b. Signal processing in the detector elements;

    Note: 6A002.a.3.d does not control ``focal plane arrays'' (not
to exceed 32 elements) having detector elements limited solely to
germanium material.

    Technical Note:  For the purposes of 6A002.a.3.d, `cross-scan
direction' is defined as the axis parallel to the linear array of
detector elements and the `scan direction' is defined as the axis
perpendicular to the linear array of detector elements.

    a.3.e. Non-``space-qualified'' linear (1-dimensional) ``focal
plane arrays'' having individual elements with a peak response in
the wavelength range exceeding 3,000 nm but not exceeding 30,000 nm;
    a.3.f. Non-``space-qualified'' non-linear (2-dimensional)
infrared ``focal plane arrays'' based on `microbolometer' material
having individual elements with an unfiltered response in the
wavelength range equal to or exceeding 8,000 nm but not exceeding
14,000 nm;

    Technical Note:  For the purposes of 6A002.a.3.f,
`microbolometer' is defined as a thermal imaging detector that, as a
result of a temperature change in the detector caused by the
absorption of infrared radiation, is used to generate any usable
signal.

    a.3.g. Non-``space-qualified'' ``focal plane arrays'' having all
of the following:
    a.3.g.1. Individual detector elements with a peak response in
the wavelength range exceeding 400 nm but not exceeding 900 nm;
    a.3.g.2. ``Specially designed'' or modified to achieve `charge
multiplication' and having a maximum ``radiant sensitivity''
exceeding 10 mA/W for wavelengths exceeding 760 nm; and
    a.3.g.3. Greater than 32 elements;
    b. ``Monospectral imaging sensors'' and ``multispectral imaging
sensors'', designed for remote sensing applications and having any
of the following:
    b.1. An Instantaneous-Field-Of-View (IFOV) of less than 200
[mu]rad (microradians); or
    b.2. Specified for operation in the wavelength range exceeding
400 nm but not exceeding 30,000 nm and having all the following:
    b.2.a. Providing output imaging data in digital format; and
    b.2.b. Having any of the following characteristics:
    b.2.b.1. ``Space-qualified''; or
    b.2.b.2. Designed for airborne operation, using other than
silicon detectors, and having an IFOV of less than 2.5 mrad
(milliradians);

    Note: 6A002.b.1 does not control ``monospectral imaging
sensors'' with a peak response in the wavelength range exceeding 300
nm but not exceeding 900 nm and only incorporating any of the
following non-``space-qualified'' detectors or non-``space-
qualified'' ``focal plane arrays'':
    a. Charge Coupled Devices (CCD) not designed or modified to
achieve `charge multiplication'; or
    b. Complementary Metal Oxide Semiconductor (CMOS) devices not
designed or modified to achieve `charge multiplication'.

    c. `Direct view' imaging equipment incorporating any of the
following:
    c.1. Image intensifier tubes having the characteristics listed
in 6A002.a.2.a or 6A002.a.2.b;
    c.2. ``Focal plane arrays'' having the characteristics listed in
6A002.a.3; or
    c.3. Solid state detectors specified by 6A002.a.1;

    Technical Note:  `Direct view' refers to imaging equipment that
presents a visual image to a human observer without converting the
image into an electronic signal for television display, and that
cannot record or store the image photographically, electronically or
by any other means.

    Note:  6A002.c does not control equipment as follows, when
incorporating other than GaAs or GaInAs photocathodes:
    a. Industrial or civilian intrusion alarm, traffic or industrial
movement control or counting systems;
    b. Medical equipment;
    c. Industrial equipment used for inspection, sorting or analysis
of the properties of materials;
    d. Flame detectors for industrial furnaces;
    e. Equipment ``specially designed'' for laboratory use.

    d. Special support ``components'' for optical sensors, as
follows:
    d.1. ``Space-qualified'' cryocoolers;
    d.2. Non-``space-qualified'' cryocoolers having a cooling source
temperature below 218K (-55[deg] C), as follows:
    d.2.a. Closed cycle type with a specified Mean-Time-To-Failure
(MTTF) or Mean-Time-Between-Failures (MTBF), exceeding 2,500 hours;
    d.2.b. Joule-Thomson (JT) self-regulating minicoolers having
bore (outside) diameters of less than 8 mm;
    d.3. Optical sensing fibers specially fabricated either
compositionally or structurally, or modified by coating, to be
acoustically, thermally, inertially, electromagnetically or nuclear
radiation sensitive.

    Note: 6A002.d.3 does not apply to encapsulated optical sensing
fibers ``specially designed'' for bore hole sensing applications.

    e. [Reserved]
    f. `Read-Out Integrated Circuits' (`ROIC') ``specially
designed'' for ``focal plane arrays'' specified by 6A002.a.3.

    Note: 6A002.f does not apply to read-out integrated circuits
``specially designed'' for civil automotive applications.

    Technical Note: A `Read-Out Integrated Circuit' (`ROIC') is an
integrated circuit designed to underlie or be bonded to a ``focal
plane array'' (``FPA'') and used to read-out (i.e., extract and
register) signals produced by the detector elements. At a minimum
the `ROIC' reads the charge from the detector elements by extracting
the charge and applying a multiplexing function in a manner that
retains the relative spatial position and orientation information of
the detector elements for processing inside or outside the `ROIC'.

0
49. In supplement no. 1 to part 774, Category 6, ECCN 6A003 is revised
to read as follows:

6A003 Cameras, systems or equipment, and ``components'' therefor, as
follows (see List of Items Controlled).

License Requirements

Reason for Control: NS, NP, RS, AT, UN

                                            Country chart (see Supp. No.
                Control(s)                         1 to part 738)

NS applies to entire entry................  NS Column 2
NP applies to cameras controlled by         NP Column 1
 6A003.a.3 or a.4 and to plug-ins in
 6A003.a.6 for cameras controlled by
 6A003.a.3 or a.4.

RS applies to 6A003.b.3, 6A003.b.4.a,       RS Column 1
 6A003.b.4.c and to items controlled in
 6A003.b.4.b that have a frame rate
 greater than 60 Hz or that incorporate a
 focal plane array with more than 111,000
 elements, or to items in 6A003.b.4.b when
 being exported or reexported to be
 embedded in a civil product. (But see
 Sec.   742.6(a)(2)(iii) and (v) of the
 EAR for certain exemptions).
RS applies to items controlled in           RS Column 2
 6A003.b.4.b that have a frame rate of 60
 Hz or less and that incorporate a focal
 plane array with not more than 111,000
 elements if not being exported or
 reexported to be embedded in a civil
 product.
AT applies to entire entry................  AT Column 1
UN applies to 6A003.b.3 and b.4...........  See Sec.   746.1(b) of the
                                             EAR for UN controls

    License Requirement Note: Commodities that are not subject to
the ITAR but are of the type described in USML Category XII(c) are
controlled as cameras in ECCN 6A003 when they incorporate a camera
controlled in this ECCN.

Reporting Requirements

See Sec.  743.3 of the EAR for thermal camera reporting for exports
that are not authorized by an individually validated license of
thermal imaging cameras controlled by ECCN 6A003.b.4.b to
destinations in Country Group A:1 (see Supplement No. 1 to part 740
of the EAR), must be reported to BIS.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

LVS: $1,500, except N/A for 6A003.a.3 through a.6, b.1, b.3 and b.4
GBS: N/A
CIV: N/A

Special Conditions for STA

STA: License Exception STA may not be used to ship any commodity in
6A003.b.3 or b.4 to any of the destinations listed in Country Group
A:6 (See Supplement No.1 to part 740 of the EAR).

List of Items Controlled

Related Controls: (1) See ECCNs 6E001 (``development''), 6E002
(``production''), and 6E201 (``use'') for technology for items
controlled under this entry. (2) Also see ECCN 6A203. (3) See ECCN
0A919 for foreign made military commodities that incorporate cameras
described in 6A003. (4) Section 744.9 of the EAR imposes a license
requirement on cameras described in 6A003 if being exported,
reexported, or transferred (in-country) for use by a military end-
user or for incorporation into a commodity controlled by ECCN 0A919.
(5) See USML Category XII(c) and (e) for cameras subject to the
ITAR.
Related Definitions: N/A
Items:

    a. Instrumentation cameras and ``specially designed''
``components'' therefor, as follows:

    Note: Instrumentation cameras, controlled by 6A003.a.3 to
6A003.a.5, with modular structures should be evaluated by their
maximum capability, using plug-ins available according to the camera
manufacturer's specifications.

    a.1. [Reserved]
    a.2. [Reserved]
    a.3. Electronic streak cameras having temporal resolution better
than 50 ns;
    a.4. Electronic framing cameras having a speed exceeding
1,000,000 frames/s;
    a.5. Electronic cameras having all of the following:
    a.5.a. An electronic shutter speed (gating capability) of less
than 1[mu]s per full frame; and
    a.5.b. A read out time allowing a framing rate of more than 125
full frames per second;
    a.6. Plug-ins having all of the following characteristics:
    a.6.a. ``Specially designed'' for instrumentation cameras which
have modular structures and that are controlled by 6A003.a; and
    a.6.b. Enabling these cameras to meet the characteristics
specified by 6A003.a.3, 6A003.a.4 or 6A003.a.5, according to the
manufacturer's specifications;
    b. Imaging cameras as follows:

    Note: 6A003.b does not control television or video cameras
``specially designed'' for television broadcasting.

    b.1. Video cameras incorporating solid state sensors, having a
peak response in the wavelength range exceeding 10 nm, but not
exceeding 30,000 nm and having all of the following:
    b.1.a. Having any of the following:
    b.1.a.1. More than 4 x 10\6\ ``active pixels'' per solid state
array for monochrome (black and white) cameras;
    b.1.a.2. More than 4 x 10\6\ ``active pixels'' per solid state
array for color cameras incorporating three solid state arrays; or
    b.1.a.3. More than 12 x 10\6\ ``active pixels'' for solid state
array color cameras incorporating one solid state array; and
    b.1.b. Having any of the following:
    b.1.b.1. Optical mirrors controlled by 6A004.a.;
    b.1.b.2. Optical control equipment controlled by 6A004.d.; or
    b.1.b.3. The capability for annotating internally generated
`camera tracking data;'

    Technical Notes:
    1. For the purposes of this entry, digital video cameras should
be evaluated by the maximum number of ``active pixels'' used for
capturing moving images.
    2. For the purpose of this entry, `camera tracking data' is the
information necessary to define camera line of sight orientation
with respect to the earth. This includes: (1) The horizontal angle
the camera line of sight makes with respect to the earth's magnetic
field direction and; (2) the vertical angle between the camera line
of sight and the earth's horizon.

    b.2. Scanning cameras and scanning camera systems, having all of
the following:
    b.2.a. A peak response in the wavelength range exceeding 10 nm,
but not exceeding 30,000 nm;
    b.2.b. Linear detector arrays with more than 8,192 elements per
array; and
    b.2.c. Mechanical scanning in one direction;

    Note: 6A003.b.2 does not apply to scanning cameras and scanning
camera systems, ``specially designed'' for any of the following:
    a. Industrial or civilian photocopiers;
    b. Image scanners ``specially designed'' for civil, stationary,
close proximity scanning applications (e.g., reproduction of images
or print contained in documents, artwork or photographs); or
    c. Medical equipment.

    b.3. Imaging cameras incorporating image intensifier tubes
having the characteristics listed in 6A002.a.2.a or 6A002.a.2.b;
    b.4. Imaging cameras incorporating ``focal plane arrays'' having
any of the following:
    b.4.a. Incorporating ``focal plane arrays'' controlled by
6A002.a.3.a to 6A002.a.3.e;
    b.4.b. Incorporating ``focal plane arrays'' controlled by
6A002.a.3.f; or
    b.4.c. Incorporating ``focal plane arrays'' controlled by
6A002.a.3.g;

    Note 1: Imaging cameras described in 6A003.b.4 include ``focal
plane arrays'' combined with sufficient ``signal processing''
electronics, beyond the read out integrated circuit, to enable as a
minimum the output of an analog or digital signal once power is
supplied.

    Note 2: 6A003.b.4.a does not control imaging cameras
incorporating linear ``focal plane arrays'' with 12 elements or
fewer, not employing time-delay-and-integration within the element
and designed for any of the following:
    a. Industrial or civilian intrusion alarm, traffic or industrial
movement control or counting systems;
    b. Industrial equipment used for inspection or monitoring of
heat flows in buildings, equipment or industrial processes;
    c. Industrial equipment used for inspection, sorting or analysis
of the properties of materials;
    d. Equipment ``specially designed'' for laboratory use; or
    e. Medical equipment.

    Note 3: 6A003.b.4.b does not control imaging cameras having any
of the following:
    a. A maximum frame rate equal to or less than 9 Hz;
    b. Having all of the following:

    1. Having a minimum horizontal or vertical `Instantaneous-Field
-of-View (IFOV)' of at least 10 mrad (milliradians);
    2. Incorporating a fixed focal-length lens that is not designed
to be removed;
    3. Not incorporating a `direct view' display; and

    Technical Note: `Direct view' refers to an imaging camera
operating in the infrared spectrum that presents a visual image to a
human observer using a near-to-eye micro display incorporating any
light-security mechanism.
    4. Having any of the following:
    a. No facility to obtain a viewable image of the detected field-
of-view; or
    b. The camera is designed for a single kind of application and
designed not to be user modified; or

    Technical Note:
    `Instantaneous Field of View (IFOV)' specified in Note 3.b is
the lesser figure of the `Horizontal FOV' or the `Vertical FOV.'
    `Horizontal IFOV' = horizontal Field of View (FOV)/number of
horizontal detector elements
    `Vertical IFOV' = vertical Field of View (FOV)/number of
vertical detector elements.
    c. The camera is ``specially designed'' for installation into a
civilian passenger land vehicle and having all of the following:
    1. The placement and configuration of the camera within the
vehicle are solely to assist the driver in the safe operation of the
vehicle;
    2. Is operable only when installed in any of the following:
    a. The civilian passenger land vehicle for which it was intended
and the vehicle weighs less than 4,500 kg (gross vehicle weight); or
    b. A ``specially designed'', authorized maintenance test
facility; and
    3. Incorporates an active mechanism that forces the camera not
to function when it is removed from the vehicle for which it was
intended.

    Note: When necessary, details of the items will be provided,
upon request, to the Bureau of Industry and Security in order to
ascertain compliance with the conditions described in Note 3.b.4 and
Note 3.c in this Note to 6A003.b.4.b.

    Note 4: 6A003.b.4.c does not apply to `imaging cameras' having
any of the following characteristics:
    a. Having all of the following:
    1. Where the camera is ``specially designed'' for installation
as an integrated component into indoor and wall-plug-operated
systems or equipment, limited by design for a single kind of
application, as follows:
    a. Industrial process monitoring, quality control, or analysis
of the properties of materials;
    b. Laboratory equipment ``specially designed'' for scientific
research;
    c. Medical equipment;
    d. Financial fraud detection equipment; and
    2. Is only operable when installed in any of the following:
    a. The system(s) or equipment for which it was intended; or
    b. A ``specially designed'', authorized maintenance facility;
and
    3. Incorporates an active mechanism that forces the camera not
to function when it is removed from the system(s) or equipment for
which it was intended;
    b. Where the camera is ``specially designed'' for installation
into a civilian passenger land vehicle or passenger and vehicle
ferries and having all of the following:
    1. The placement and configuration of the camera within the
vehicle or ferry are solely to assist the driver or operator in the
safe operation of the vehicle or ferry;
    2. Is only operable when installed in any of the following:
    a. The civilian passenger land vehicle for which it was intended
and the vehicle weighs less than 4,500 kg (gross vehicle weight);
    b. The passenger and vehicle ferry for which it was intended and
having a length overall (LOA) 65 m or greater; or
    c. A ``specially designed'', authorized maintenance test
facility; and
    3. Incorporates an active mechanism that forces the camera not
to function when it is removed from the vehicle for which it was
intended;
    c. Limited by design to have a maximum ``radiant sensitivity''
of 10 mA/W or less for wavelengths exceeding 760 nm, having all of
the following:
    1. Incorporating a response limiting mechanism designed not to
be removed or modified; and
    2. Incorporates an active mechanism that forces the camera not
to function when the response limiting mechanism is removed; and
    3. Not ``specially designed'' or modified for underwater use; or
    d. Having all of the following:
    1. Not incorporating a `direct view' or electronic image
display;
    2. Has no facility to output a viewable image of the detected
field of view;
    3. The ``focal plane array'' is only operable when installed in
the camera for which it was intended; and
    4. The ``focal plane array'' incorporates an active mechanism
that forces it to be permanently inoperable when removed from the
camera for which it was intended.

    Note: When necessary, details of the item will be provided, upon
request, to the Bureau of Industry and Security in order to
ascertain compliance with the conditions described in Note 4 above.

    b.5. Imaging cameras incorporating solid-state detectors
specified by 6A002.a.1.

0
50. In supplement no. 1 to part 774, Category 6, ECCN 6A004 is revised
to read as follows:

6A004 Optical equipment and ``components'', as follows (see List of
Items Controlled).

License Requirements

Reason for Control: NS, AT

                                            Country chart (see Supp. No.
                Control(s)                         1 to part 738)

NS applies to entire entry................  NS Column 2
AT applies to entire entry................  AT Column 1

Reporting Requirements

See Sec.  743.1 of the EAR for reporting requirements for exports
under License Exceptions, and Validated End-User authorizations.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

LVS: $3,000
GBS: Yes for 6A004.a.1, a.2, a.4, .b, d.2, and .f.
CIV: Yes for 6A004.a.1, a.2, a.4, .b, d.2, and .f.

Special Conditions for STA

STA: Paragraph (c)(2) of License Exception STA may not be used to
ship any commodity in 6A004.c or .d to any of the destinations
listed in Country Group A:6 (See Supplement No.1 to part 740 of the
EAR).

List of Items Controlled

Related Controls: (1) For optical mirrors or `aspheric optical
elements' ``specially designed'' for lithography ``equipment'', see
ECCN 3B001. (2) See USML Category XII(e) for gimbals ``subject to
the ITAR''. (3) See also 6A994.
Related Definitions: An `aspheric optical element' is any element
used in an optical system whose imaging surface or surfaces are
designed to depart from the shape of an ideal sphere.
Items:

    a. Optical mirrors (reflectors) as follows:

    Technical Note: For the purpose of 6A004.a, Laser Induced Damage
Threshold (LIDT) is measured according to ISO 21254-1:2011.

    a.1. `Deformable mirrors' having an active optical aperture
greater than 10 mm and having any of the following, and specially
designed components therefor:
    a.1.a. Having all the following:
    a.1.a.1. A mechanical resonant frequency of 750 Hz or more; and
    a.1.a.2. More than 200 actuators; or
    a.1.b. A Laser Induced Damage Threshold (LIDT) being any of the
following:
    a.1.b.1. Greater than 1 kW/cm\2\ using a ``CW laser''; or
    a.1.b.2. Greater than 2 J/cm\2\ using 20 ns ``laser'' pulses at
20 Hz repetition rate;

    Technical Note: `Deformable mirrors' are mirrors having any of
the following:
    a. A single continuous optical reflecting surface which is
dynamically deformed by the application of individual torques or
forces to compensate for distortions in the optical waveform
incident upon the mirror; or
    b. Multiple optical reflecting elements that can be individually
and dynamically repositioned by the application of torques or forces
to compensate for distortions in the optical waveform incident upon
the mirror.

    `Deformable mirrors' are also known as adaptive optic mirrors.

    a.2. Lightweight monolithic mirrors having an average
``equivalent density'' of less than 30 kg/m\2\ and a total mass
exceeding 10 kg;
    a.3. Lightweight ``composite'' or foam mirror structures having
an average ``equivalent density'' of less than 30 kg/m\2\ and a
total mass exceeding 2 kg;

    Note: 6A004.a.2 and 6A004.a.3 do not apply to mirrors
``specially designed'' to direct solar radiation for terrestrial
heliostat installations.

    a.4. Mirrors specially designed for beam steering mirror stages
specified in 6A004.d.2.a with a flatness of [lambda]/10 or better
([lambda] is equal to 633 nm) and having any of the following:
    a.4.a. Diameter or major axis length greater than or equal to
100 mm; or
    a.4.b. Having all of the following:
    a.4.b.1. Diameter or major axis length greater than 50 mm but
less than 100 mm; and
    a.4.b.2. A Laser Induced Damage Threshold (LIDT) being any of
the following:
    a.4.b.2.a. Greater than 10 kW/cm2 using a ``CW laser''; or
    a.4.b.2.b. Greater than 20 J/cm2 using 20 ns ``laser'' pulses at
20 Hz repetition rate;

    N.B. For optical mirrors specially designed for lithography
equipment, see 3B001.

    b. Optical ``components'' made from zinc selenide (ZnSe) or zinc
sulphide (ZnS) with transmission in the wavelength range exceeding
3,000 nm but not exceeding 25,000 nm and having any of the
following:
    b.1. Exceeding 100 cm\3\ in volume; or
    b.2. Exceeding 80 mm in diameter or length of major axis and 20
mm in thickness (depth);
    c. ``Space-qualified'' ``components'' for optical systems, as
follows:
    c.1. ``Components'' lightweighted to less than 20% ``equivalent
density'' compared with a solid blank of the same aperture and
thickness;
    c.2. Raw substrates, processed substrates having surface
coatings (single-layer or multi-layer, metallic or dielectric,
conducting, semiconducting or insulating) or having protective
films;
    c.3. Segments or assemblies of mirrors designed to be assembled
in space into an optical system with a collecting aperture
equivalent to or larger than a single optic 1 m in diameter;
    c.4. ``Components'' manufactured from ``composite'' materials
having a coefficient of linear thermal expansion equal to or less
than 5 x 10-6 in any coordinate direction;
    d. Optical control equipment as follows:
    d.1. Equipment ``specially designed'' to maintain the surface
figure or orientation of the ``space-qualified'' ``components''
controlled by 6A004.c.1 or 6A004.c.3;
    d.2. Steering, tracking, stabilisation and resonator alignment
equipment as follows:
    d.2.a. Beam steering mirror stages designed to carry mirrors
having diameter or major axis length greater than 50 mm and having
all of the following, and specially designed electronic control
equipment therefor:
    d.2.a.1. A maximum angular travel of 26 mrad or
more;
    d.2.a.2. A mechanical resonant frequency of 500 Hz or more; and
    d.2.a.3. An angular ``accuracy'' of 10 [mu]rad (microradians) or
less (better);
    d.2.b. Resonator alignment equipment having bandwidths equal to
or more than 100 Hz and an ``accuracy'' of 10 [mu]rad or less
(better);
    d.3. Gimbals having all of the following:
    d.3.a. A maximum slew exceeding 5[deg];
    d.3.b. A bandwidth of 100 Hz or more;
    d.3.c. Angular pointing errors of 200 [mu]rad (microradians) or
less; and
    d.3.d. Having any of the following:
    d.3.d.1. Exceeding 0.15 m but not exceeding 1 m in diameter or
major axis length and capable of angular accelerations exceeding 2
rad (radians)/s\2\; or
    d.3.d.2. Exceeding 1 m in diameter or major axis length and
capable of angular accelerations exceeding 0.5 rad (radians)/s\2\;
    d.4. [Reserved]
    e. `Aspheric optical elements' having all of the following:
    e.1. Largest dimension of the optical-aperture greater than 400
mm;
    e.2. Surface roughness less than 1 nm (rms) for sampling lengths
equal to or greater than 1 mm; and
    e.3. Coefficient of linear thermal expansion's absolute
magnitude less than 3 x 10-6/K at 25 [deg]C;

    Technical Note:
    1. [See Related Definitions section of this ECCN]
    2. Manufacturers are not required to measure the surface
roughness listed in 6A004.e.2 unless the optical element was
designed or manufactured with the intent to meet, or exceed, the
control parameter.

    Note: 6A004.e does not control `aspheric optical elements'
having any of the following:
    a. Largest optical-aperture dimension less than 1 m and focal
length to aperture ratio equal to or greater than 4.5:1;
    b. Largest optical-aperture dimension equal to or greater than 1
m and focal length to aperture ratio equal to or greater than 7:1;
    c. Designed as Fresnel, flyeye, stripe, prism or diffractive
optical elements;
    d. Fabricated from borosilicate glass having a coefficient of
linear thermal expansion greater than 2.5 x 10-6/K at 25
[deg]C; or
    e. An x-ray optical element having inner mirror capabilities
(e.g., tube-type mirrors).

    f. Dynamic wavefront measuring equipment having all of the
following:
    f.1. `Frame rates' equal to or more than 1 kHz; and
    f.2. A wavefront accuracy equal to or less (better) than
[lambda]/20 at the designed wavelength.

    Technical Note: For the purposes of 6A004.f, `frame rate' is a
frequency at which all ``active pixels'' in the ``focal plane
array'' are integrated for recording images projected by the
wavefront sensor optics.

0
51. In supplement no. 1 to part 774, Category 6, ECCN 6A005 is revised
to read as follows:

6A005 ``Lasers'', ``components'' and optical equipment, as follows
(see List of Items Controlled), excluding items that are subject to
the export licensing authority of the Nuclear Regulatory Commission
(see 10 CFR part 110).

License Requirements

Reason for Control: NS, NP, AT

                                            Country chart (see Supp. No.
                Control(s)                         1 to part 738)

NS applies to entire entry................  NS Column 2
NP applies to lasers controlled by          NP Column 1
 6A005.a.2, a.3, a.4, b.2.b, b.3, b.4,
 b.6.c, c.1.b, c.2.b, d.2, d.3.c, or d.4.c
 that meet or exceed the technical
 parameters described in 6A205.
AT applies to entire entry................  AT Column 1

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

LVS: N/A for NP items; $3,000 for all other items
GBS: Neodymium-doped (other than glass) ``lasers'' controlled by
6A005.b.6.d.2 (except 6A005.b.6.d.2.b) that have an output
wavelength exceeding 1,000 nm, but not exceeding 1,100 nm, and an
average or CW output power not exceeding 2kW, and operate in a
pulse-excited, non-``Q-switched'' multiple-transverse mode, or in a
continuously excited, multiple-transverse mode; Dye and Liquid
Lasers controlled by 6A005.c.1, c.2 and c.3, except for a pulsed
single longitudinal mode oscillator having an average output power
exceeding 1 W and a repetition rate exceeding 1 kHz if the ``pulse
duration'' is less than 100 ns; CO ``lasers'' controlled by
6A005.d.2 having a CW maximum rated single or multimode output power
not exceeding 10 kW; CO2 or CO/CO2 ``lasers''
controlled by 6A005.d.3 having an output wavelength in the range
from 9,000 to 11,000 nm and having a pulsed output not exceeding 2 J
per pulse and a maximum rated average single or multimode output
power not exceeding 5 kW; CO2 ``lasers'' controlled by
6A005.d.3 that operate in CW multiple-transverse mode, and having a
CW output power not exceeding 15kW.
CIV: Neodymium-doped (other than glass) ``lasers'' controlled by
6A005.b.6.d.2 (except 6A005.b.6.d.2.b) that have an output
wavelength exceeding 1,000 nm, but not exceeding 1,100 nm, and an
average or CW output power not exceeding 2kW, and operate in a
pulse-excited, non-``Q-switched'' multiple-transverse mode, or in a
continuously excited, multiple-transverse mode; Dye and Liquid
Lasers controlled by 6A005.c.1, c.2 and c.3, except for a pulsed
single longitudinal mode oscillator having an average output power
exceeding 1 W and a repetition rate exceeding 1 kHz if the ``pulse
duration'' is less than 100 ns; CO ``lasers'' controlled by
6A005.d.2 having a CW maximum rated single or multimode output power
not exceeding 10 kW; CO2 or CO/CO2 ``lasers''
controlled by 6A005.d.3 having an output wavelength in the range
from 9,000 to 11,000 nm and having a pulsed output not

exceeding 2 J per pulse and a maximum rated average single or
multimode output power not exceeding 5 kW; CO2 ``lasers''
controlled by 6A005.d.3 that operate in CW multiple-transverse mode,
and having a CW output power not exceeding 15kW.

List of Items Controlled

Related Controls: (1) See ECCN 6D001 for ``software'' for items
controlled under this entry. (2) See ECCNs 6E001 (``development''),
6E002 (``production''), and 6E201 (``use'') for technology for items
controlled under this entry. (3) Also see ECCNs 6A205 and 6A995. (4)
See ECCN 3B001 for excimer ``lasers'' ``specially designed'' for
lithography equipment. (5) ``Lasers'' ``specially designed'' or
prepared for use in isotope separation are subject to the export
licensing authority of the Nuclear Regulatory Commission (see 10 CFR
part 110). (6) See USML Category XII(b) and (e) for laser systems or
lasers subject to the ITAR. (7) See USML Category XVIII for certain
laser-based directed energy weapon systems, equipment, and
components subject to the ITAR.
Related Definitions: (1) `Wall-plug efficiency' is defined as the
ratio of ``laser'' output power (or ``average output power'') to
total electrical input power required to operate the ``laser'',
including the power supply/conditioning and thermal conditioning/
heat exchanger, see 6A005.a.6.b.1 and 6A005.b.6; (2) `Non-repetitive
pulsed' refers to ``lasers'' that produce either a single output
pulse or that have a time interval between pulses exceeding one
minute, see Note 2 of 6A005 and 6A005.d.6.
Items:

    Note:
    1. Pulsed ``lasers'' include those that run in a continuous wave
(CW) mode with pulses superimposed.
    2. Excimer, semiconductor, chemical, CO, CO2, and
`non-repetitive pulsed' Nd:glass ``lasers'' are only specified by
6A005.d.

    Technical Note: `Non-repetitive pulsed' refers to ``lasers''
that produce either a single output pulse or that have a time
interval between pulses exceeding one minute.
    3. 6A005 includes fiber ``lasers''.
    4. The control status of ``lasers'' incorporating frequency
conversion (i.e., wavelength change) by means other than one
``laser'' pumping another ``laser'' is determined by applying the
control parameters for both the output of the source ``laser'' and
the frequency-converted optical output.
    5. 6A005 does not control ``lasers'' as follows:
    a. Ruby with output energy below 20 J;
    b. Nitrogen;
    c. Krypton.

    a. Non-``tunable'' continuous wave ``(CW) lasers'' having any of
the following:
    a.1. Output wavelength less than 150 nm and output power
exceeding 1W;
    a.2. Output wavelength of 150 nm or more but not exceeding 510
nm and output power exceeding 30 W;

    Note: 6A005.a.2 does not control Argon ``lasers'' having an
output power equal to or less than 50 W.

    a.3. Output wavelength exceeding 510 nm but not exceeding 540 nm
and any of the following:
    a.3.a. Single transverse mode output and output power exceeding
50 W; or
    a.3.b. Multiple transverse mode output and output power
exceeding 150 W;
    a.4. Output wavelength exceeding 540 nm but not exceeding 800 nm
and output power exceeding 30 W;
    a.5. Output wavelength exceeding 800 nm but not exceeding 975 nm
and any of the following:
    a.5.a. Single transverse mode output and output power exceeding
50 W; or
    a.5.b. Multiple transverse mode output and output power
exceeding 80 W;
    a.6. Output wavelength exceeding 975 nm but not exceeding 1,150
nm and any of the following;
    a.6.a. Single transverse mode output and output power exceeding
500 W; or
    a.6.b. Multiple transverse mode output and any of the following:
    a.6.b.1. `Wall-plug efficiency' exceeding 18% and output power
exceeding 500 W; or
    a.6.b.2. Output power exceeding 2 kW;

    Note 1: 6A005.a.6.b does not control multiple transverse mode,
industrial ``lasers'' with output power exceeding 2kW and not
exceeding 6 kW with a total mass greater than 1,200 kg. For the
purpose of this note, total mass includes all ``components''
required to operate the ``laser'', e.g., ``laser'', power supply,
heat exchanger, but excludes external optics for beam conditioning
or delivery.

    Note 2: 6A005.a.6.b does not apply to multiple transverse mode,
industrial ``lasers'' having any of the following:
     a. Output power exceeding 500 W but not exceeding 1 kW and
having all of the following:
    1. Beam Parameter Product (BPP) exceeding 0.7 mmmrad;
and
    2. `Brightness' not exceeding 1024 W/(mmmrad)\2\;
     b. Output power exceeding 1 kW but not exceeding 1.6 kW and
having a BPP exceeding 1.25 mmmrad;
     c. Output power exceeding 1.6 kW but not exceeding 2.5 kW and
having a BPP exceeding 1.7 mmmrad;
     d. Output power exceeding 2.5 kW but not exceeding 3.3 kW and
having a BPP exceeding 2.5 mmmrad;
     e. Output power exceeding 3.3 kW but not exceeding 4 kW and
having a BPP exceeding 3.5 mmmrad;
     f. Output power exceeding 4 kW but not exceeding 5 kW and
having a BPP exceeding 5 mmmrad;
     g. Output power exceeding 5 kW but not exceeding 6 kW and
having a BPP exceeding 7.2 mmmrad;
     h. Output power exceeding 6 kW but not exceeding 8 kW and
having a BPP exceeding 12 mmmrad; or
     i. Output power exceeding 8 kW but not exceeding 10 kW and
having a BPP exceeding 24 mmmrad;

    Technical Note: For the purpose of 6A005.a.6.b, Note 2 (a)(2),
`brightness' is defined as the output power of the ``laser'' divided
by the squared Beam Parameter Product (BPP), i.e., (output power)/
BPP\2\.

    a.7. Output wavelength exceeding 1,150 nm but not exceeding
1,555 nm and any of the following:
    a.7.a. Single transverse mode and output power exceeding 50 W;
or
    a.7.b. Multiple transverse mode and output power exceeding 80 W;
    a.8. Output wavelength exceeding 1,555 nm but not exceeding
1,850 nm and output power exceeding 1 W;
    a.9. Output wavelength exceeding 1,850 nm but not exceeding
2,100 nm, and any of the following:
    a.9.a. Single transverse mode and output power exceeding 1 W; or
    a.9. b. Multiple transverse mode output and output power
exceeding 120 W; or
    a.10. Output wavelength exceeding 2,100 nm and output power
exceeding 1 W;
    b. Non-``tunable'' ``pulsed lasers'' having any of the
following:
    b.1. Output wavelength less than 150 nm and any of the
following:
    b.1.a. Output energy exceeding 50 mJ per pulse and ``peak
power'' exceeding 1 W; or
    b.1.b. ``Average output power'' exceeding 1 W;
    b.2. Output wavelength of 150 nm or more but not exceeding 510
nm and any of the following:
    b.2.a. Output energy exceeding 1.5 J per pulse and ``peak
power'' exceeding 30 W; or
    b.2.b. ``Average output power'' exceeding 30 W;

    Note: 6A005.b.2.b does not control Argon ``lasers'' having an
``average output power'' equal to or less than 50 W.

    b.3. Output wavelength exceeding 510 nm, but not exceeding 540
nm and any of the following:
    b.3.a. Single transverse mode output and any of the following:
    b.3.a.1. Output energy exceeding 1.5 J per pulse and ``peak
power'' exceeding 50 W; or
    b.3.a.2. ``Average output power'' exceeding 50 W; or
    b.3.b. Multiple transverse mode output and any of the following:
    b.3.b.1. Output energy exceeding 1.5 J per pulse and ``peak
power'' exceeding 150 W; or
    b.3.b.2. ``Average output power'' exceeding 150 W;
    b.4. Output wavelength exceeding 540 nm but not exceeding 800 nm
and any of the following:
    b.4.a. ``Pulse duration'' less than 1 ps and any of the
following:
    b.4.a.1. Output energy exceeding 0.005 J per pulse and ``peak
power'' exceeding 5 GW; or
    b.4.a.2. ``Average output power'' exceeding 20 W; or
    b.4.b. ``Pulse duration'' equal to or exceeding 1 ps and any of
the following:
    b.4.b.1. Output energy exceeding 1.5 J per pulse and ``peak
power'' exceeding 30 W; or
    b.4.b.2. ``Average output power'' exceeding 30 W;
    b.5. Output wavelength exceeding 800 nm but not exceeding 975 nm
and any of the following:
    b.5.a. ``Pulse duration'' less than 1ps and any of the
following:
    b.5.a.1. Output energy exceeding 0.005 J per pulse and ``peak
power'' exceeding 5 GW; or

    b.5.a.2. Single transverse mode output and ``average output
power'' exceeding 20 W;
    b.5.b. ``Pulse duration'' equal to or exceeding 1 ps and not
exceeding 1 [mu]s and any of the following:
    b.5.b.1. Output energy exceeding 0.5 J per pulse and ``peak
power'' exceeding 50 W;
    b.5.b.2. Single transverse mode output and ``average output
power'' exceeding 20 W; or
    b.5.b.3. Multiple transverse mode output and ``average output
power'' exceeding 50 W; or
    b.5.c. ``Pulse duration'' exceeding 1 [mu]s and any of the
following:
    b.5.c.1. Output energy exceeding 2 J per pulse and ``peak
power'' exceeding 50 W;
    b.5.c.2. Single transverse mode output and ``average output
power'' exceeding 50 W; or
    b.5.c.3. Multiple transverse mode output and ``average output
power'' exceeding 80 W.
    b.6. Output wavelength exceeding 975 nm but not exceeding 1,150
nm and any of the following:
    b.6.a. ``Pulse duration'' of less than 1 ps, and any of the
following:
    b.6.a.1. Output ``peak power'' exceeding 2 GW per pulse;
    b.6.a.2. ``Average output power'' exceeding 30 W; or
    b.6.a.3. Output energy exceeding 0.002 J per pulse;
    b.6.b. ``Pulse duration'' equal to or exceeding 1 ps and less
than 1 ns, and any of the following:
    b.6.b.1. Output ``peak power'' exceeding 5 GW per pulse;
    b.6.b.2. ``Average output power'' exceeding 50 W; or
    b.6.b.3. Output energy exceeding 0.1 J per pulse;
    b.6.c. ``Pulse duration'' equal to or exceeding 1 ns but not
exceeding 1 [mu]s and any of the following:
    b.6.c.1. Single transverse mode output and any of the following:
    b.6.c.1.a. ``Peak power'' exceeding 100 MW;
    b.6.c.1.b. ``Average output power'' exceeding 20 W limited by
design to a maximum pulse repetition frequency less than or equal to
1 kHz;
    b.6.c.1.c. `Wall-plug efficiency' exceeding 12%, ``average
output power'' exceeding 100 W and capable of operating at a pulse
repetition frequency greater than 1 kHz;
    b.6.c.1.d. ``Average output power'' exceeding 150 W and capable
of operating at a pulse repetition frequency greater than 1 kHz; or
    b.6.c.1.e. Output energy exceeding 2 J per pulse; or
    b.6.c.2. Multiple transverse mode output and any of the
following:
    b.6.c.2.a. ``Peak power'' exceeding 400 MW;
    b.6.c.2.b. `Wall-plug efficiency' exceeding 18% and ``average
output power'' exceeding 500 W;
    b.6.c.2.c. ``Average output power'' exceeding 2 kW; or
    b.6.c.2.d. Output energy exceeding 4 J per pulse; or
    b.6.d. ``Pulse duration'' exceeding 1 [mu]s and any of the
following:
    b.6.d.1. Single transverse mode output and any of the following:
    b.6.d.1.a. ``Peak power'' exceeding 500 kW;
    b.6.d.1.b. `Wall-plug efficiency' exceeding 12% and ``average
output power'' exceeding 100 W; or
    b.6.d.1.c. ``Average output power'' exceeding 150 W; or
    b.6.d.2. Multiple transverse mode output and any of the
following:
    b.6.d.2.a. ``Peak power'' exceeding 1 MW;
    b.6.d.2.b. `Wall-plug efficiency' exceeding 18% and ``average
output power'' exceeding 500 W; or
    b.6.d.2.c. ``Average output power'' exceeding 2 kW;
    b.7. Output wavelength exceeding 1,150 nm but not exceeding
1,555 nm and any of the following:
    b.7.a. ``Pulse duration'' not exceeding 1 [mu]s and any of the
following:
    b.7.a.1. Output energy exceeding 0.5 J per pulse and ``peak
power'' exceeding 50 W;
    b.7.a.2. Single transverse mode output and ``average output
power'' exceeding 20 W; or
    b.7.a.3. Multiple transverse mode output and ``average output
power'' exceeding 50 W; or
    b.7.b. ``Pulse duration'' exceeding 1 [mu]s and any of the
following:
    b.7.b.1. Output energy exceeding 2 J per pulse and ``peak
power'' exceeding 50 W;
    b.7.b.2. Single transverse mode output and ``average output
power'' exceeding 50 W; or
    b.7.b.3. Multiple transverse mode output and ``average output
power'' exceeding 80 W;
    b.8. Output wavelength exceeding 1,555 nm but not exceeding
1,850 nm, and any of the following:
    b.8.a. Output energy exceeding 100 mJ per pulse and ``peak
power'' exceeding 1 W; or
    b.8.b. ``Average output power'' exceeding 1 W;
    b.9. Output wavelength exceeding 1,850 nm but not exceeding
2,100 nm, and any of the following:
    b.9.a. Single transverse mode and any of the following:
    b.9.a.1. Output energy exceeding 100 mJ per pulse and ``peak
power'' exceeding 1 W; or
    b.9.a.2. ``Average output power'' exceeding 1 W;
    b.9.b. Multiple transverse mode and any of the following:
    b.9.b.1. Output energy exceeding 100 mJ per pulse and ``peak
power'' exceeding 10 kW; or
    b.9.b.2. ``Average output power'' exceeding 120 W; or
    b.10. Output wavelength exceeding 2,100 nm and any of the
following:
    b.10.a. Output energy exceeding 100 mJ per pulse and ``peak
power'' exceeding 1 W; or
    b.10.b. ``Average output power'' exceeding 1 W;
    c. ``Tunable'' lasers having any of the following:
    c.1. Output wavelength less than 600 nm and any of the
following:
    c.1.a. Output energy exceeding 50 mJ per pulse and ``peak
power'' exceeding 1 W; or
    c.1.b. Average or CW output power exceeding 1W;

    Note: 6A005.c.1 does not apply to dye ``lasers'' or other liquid
``lasers'', having a multimode output and a wavelength of 150 nm or
more but not exceeding 600 nm and all of the following:
    1. Output energy less than 1.5 J per pulse or a ``peak power''
less than 20 W; and
    2. Average or CW output power less than 20 W.

    c.2. Output wavelength of 600 nm or more but not exceeding 1,400
nm, and any of the following:
    c.2.a. Output energy exceeding 1 J per pulse and ``peak power''
exceeding 20 W; or
    c.2.b. Average or CW output power exceeding 20 W; or
    c.3. Output wavelength exceeding 1,400 nm and any of the
following:
    c.3.a. Output energy exceeding 50 mJ per pulse and ``peak
power'' exceeding 1 W; or
    c.3.b. Average or CW output power exceeding 1 W;
    d. Other ``lasers'', not controlled by 6A005.a, 6A005.b, or
6A005.c as follows:
    d.1. Semiconductor ``lasers'' as follows:

    Note:
    1. 6A005.d.1 includes semiconductor ``lasers'' having optical
output connectors (e.g., fiber optic pigtails).
    2. The control status of semiconductor ``lasers'' ``specially
designed'' for other equipment is determined by the control status
of the other equipment.

    d.1.a. Individual single transverse mode semiconductor
``lasers'' having any of the following:
    d.1.a.1. Wavelength equal to or less than 1,510 nm and average
or CW output power, exceeding 1.5 W; or
    d.1.a.2. Wavelength greater than 1,510 nm and average or CW
output power, exceeding 500 mW;
    d.1.b. Individual, multiple-transverse mode semiconductor
``lasers'' having any of the following:
    d.1.b.1. Wavelength of less than 1,400 nm and average or CW
output power, exceeding 15 W;
    d.1.b.2. Wavelength equal to or greater than 1,400 nm and less
than 1,900 nm and average or CW output power, exceeding 2.5 W; or
    d.1.b.3. Wavelength equal to or greater than 1,900 nm and
average or CW output power, exceeding 1 W;
    d.1.c. Individual semiconductor ``laser'' `bars' having any of
the following:
    d.1.c.1. Wavelength of less than 1,400 nm and average or CW
output power, exceeding 100 W;
    d.1.c.2. Wavelength equal to or greater than 1,400 nm and less
than 1,900 nm and average or CW output power, exceeding 25 W; or
    d.1.c.3. Wavelength equal to or greater than 1,900 nm and
average or CW output power, exceeding 10 W;
    d.1.d. Semiconductor ``laser'' `stacked arrays' (two dimensional
arrays) having any of the following:
    d.1.d.1. Wavelength less than 1,400 nm and having any of the
following:
    d.1.d.1.a. Average or CW total output power less than 3 kW and
having average or CW output `power density' greater than 500 W/
cm\2\;
    d.1.d.1.b. Average or CW total output power equal to or
exceeding 3 kW but less than or equal to 5 kW, and having average or
CW output `power density' greater than 350W/cm\2\;
    d.1.d.1.c. Average or CW total output power exceeding 5 kW;

    d.1.d.1.d. Peak pulsed `power density' exceeding 2,500 W/cm\2\;
or

    Note: 6A005.d.1.d.1.d does not apply to epitaxially-fabricated
monolithic devices.

    d.1.d.1.e. Spatially coherent average or CW total output power,
greater than 150 W;
    d.1.d.2. Wavelength greater than or equal to 1,400 nm but less
than 1,900 nm, and having any of the following:
    d.1.d.2.a. Average or CW total output power less than 250 W and
average or CW output `power density' greater than 150 W/cm\2\;
    d.1.d.2.b. Average or CW total output power equal to or
exceeding 250 W but less than or equal to 500 W, and having average
or CW output `power density' greater than 50W/cm\2\;
    d.1.d.2.c. Average or CW total output power exceeding 500 W;
    d.1.d.2.d. Peak pulsed `power density' exceeding 500 W/cm\2\; or

    Note: 6A005.d.1.d.2.d does not apply to epitaxially-fabricated
monolithic devices.

    d.1.d.2.e. Spatially coherent average or CW total output power,
exceeding 15 W;
    d.1.d.3. Wavelength greater than or equal to 1,900 nm and having
any of the following:
    d.1.d.3.a. Average or CW output `power density' greater than 50
W/cm\2\;
    d.1.d.3.b. Average or CW output power greater than 10 W; or
    d.1.d.3.c. Spatially coherent average or CW total output power,
exceeding 1.5 W; or
    d.1.d.4. At least one ``laser'' `bar' specified by 6A005.d.1.c;

    Technical Note: For the purposes of 6A005.d.1.d, `power density'
means the total ``laser'' output power divided by the emitter
surface area of the `stacked array.'

    d.1.e. Semiconductor ``laser'' `stacked arrays,' other than
those specified by 6.A005.d.1.d., having all of the following:
    d.1.e.1. ``Specially designed'' or modified to be combined with
other `stacked arrays' to form a larger `stacked array;' and
    d.1.e.2. Integrated connections, common for both electronics and
cooling;

    Note 1: `Stacked arrays,' formed by combining semiconductor
``laser'' `stacked arrays' specified by 6A005.d.1.e, that are not
designed to be further combined or modified are specified by
6A005.d.1.d.

    Note 2: `Stacked arrays,' formed by combining semiconductor
``laser'' `stacked arrays' specified by 6A005.d.1.e, that are
designed to be further combined or modified are specified by
6A005.d.1.e.

    Note 3: 6A005.d.1.e does not apply to modular assemblies of
single `bars' designed to be fabricated into end to end stacked
linear arrays.

    Technical Notes:
    1. Semiconductor ``lasers'' are commonly called ``laser''
diodes.
    2. A `bar' (also called a semiconductor ``laser'' `bar,' a
``laser'' diode `bar' or diode `bar') consists of multiple
semiconductor ``lasers'' in a one dimensional array.
    3. A `stacked array' consists of multiple `bars' forming a two
dimensional array of semiconductor ``lasers''.

    d.2. Carbon monoxide (CO) ``lasers'' having any of the
following:
    d.2.a. Output energy exceeding 2 J per pulse and ``peak power''
exceeding 5 kW; or
    d.2.b. Average or CW output power, exceeding 5 kW;
    d.3. Carbon dioxide (CO2) ``lasers'' having any of
the following:
    d.3.a. CW output power exceeding 15 kW;
    d.3.b. Pulsed output with ``pulse duration'' exceeding 10 [mu]s
and any of the following:
    d.3.b.1. ``Average output power'' exceeding 10 kW; or
    d.3.b.2. ``Peak power'' exceeding 100 kW; or
    d.3.c. Pulsed output with a ``pulse duration'' equal to or less
than 10 [mu]s and any of the following:
    d.3.c.1. Pulse energy exceeding 5 J per pulse; or
    d.3.c.2. ``Average output power'' exceeding 2.5 kW;
    d.4. Excimer ``lasers'' having any of the following:
    d.4.a. Output wavelength not exceeding 150 nm and any of the
following:
    d.4.a.1. Output energy exceeding 50 mJ per pulse; or
    d.4.a.2. ``Average output power'' exceeding 1 W;
    d.4.b. Output wavelength exceeding 150 nm but not exceeding 190
nm and any of the following:
    d.4.b.1. Output energy exceeding 1.5 J per pulse; or
    d.4.b.2. ``Average output power'' exceeding 120 W;
    d.4.c. Output wavelength exceeding 190 nm but not exceeding 360
nm and any of the following:
    d.4.c.1. Output energy exceeding 10 J per pulse; or
    d.4.c.2. ``Average output power'' exceeding 500 W; or
    d.4.d. Output wavelength exceeding 360 nm and any of the
following:
    d.4.d.1. Output energy exceeding 1.5 J per pulse; or
    d.4.d.2. ``Average output power'' exceeding 30 W;

    Note: For excimer ``lasers'' ``specially designed'' for
lithography equipment, see 3B001.

    d.5. ``Chemical lasers'' as follows:
    d.5.a. Hydrogen Fluoride (HF) ``lasers'';
    d.5.b. Deuterium Fluoride (DF) ``lasers'';
    d.5.c. `Transfer lasers' as follows:
    d.5.c.1. Oxygen Iodine (O2-I) ``lasers'';
    d.5.c.2. Deuterium Fluoride-Carbon dioxide (DF-CO2)
``lasers'';

    Technical Note: `Transfer lasers' are ``lasers'' in which the
lasing species are excited through the transfer of energy by
collision of a non-lasing atom or molecule with a lasing atom or
molecule species.

    d.6. `Non-repetitive pulsed' Neodymium (Nd) glass ``lasers''
having any of the following:
    d.6.a. A ``pulse duration'' not exceeding 1 [mu]s and output
energy exceeding 50 J per pulse; or
    d.6.b. A ``pulse duration'' exceeding 1 [mu]s and output energy
exceeding 100 J per pulse;
    e. ``Components'' as follows:
    e.1. Mirrors cooled either by `active cooling' or by heat pipe
cooling;

    Technical Note: `Active cooling' is a cooling technique for
optical ``components'' using flowing fluids within the subsurface
(nominally less than 1 mm below the optical surface) of the optical
component to remove heat from the optic.

    e.2. Optical mirrors or transmissive or partially transmissive
optical or electro-optical ``components'', other than fused tapered
fiber combiners and Multi-Layer Dielectric gratings (MLDs),
``specially designed'' for use with controlled ``lasers'';

    Note to 6A005.e.2: Fiber combiners and MLDs are specified by
6A005.e.3.

    e.3. Fiber ``laser'' ``components'' as follows:
    e.3.a. Multimode to multimode fused tapered fiber combiners
having all of the following:
    e.3.a.1. An insertion loss better (less) than or equal to 0.3 dB
maintained at a rated total average or CW output power (excluding
output power transmitted through the single mode core if present)
exceeding 1,000 W; and
    e.3.a.2. Number of input fibers equal to or greater than 3;
    e.3.b. Single mode to multimode fused tapered fiber combiners
having all of the following:
    e.3.b.1. An insertion loss better (less) than 0.5 dB maintained
at a rated total average or CW output power exceeding 4,600 W;
    e.3.b.2. Number of input fibers equal to or greater than 3; and
    e.3.b.3. Having any of the following:
    e.3.b.3.a. A Beam Parameter Product (BPP) measured at the output
not exceeding 1.5 mm mrad for a number of input fibers less than or
equal to 5; or
    e.3.b.3.b. A BPP measured at the output not exceeding 2.5 mm
mrad for a number of input fibers greater than 5;
    e.3.c. MLDs having all of the following:
    e.3.c.1. Designed for spectral or coherent beam combination of 5
or more fiber ``lasers''; and
    e.3.c.2. CW ``Laser'' Induced Damage Threshold (LIDT) greater
than or equal to 10 kW/cm\2\;
    f. Optical equipment as follows:

    N.B.: For shared aperture optical elements, capable of operating
in ``Super-High Power Laser'' (``SHPL'') applications, see the U.S.
Munitions List (22 CFR part 121).

    f.1. [Reserved]

    N.B.: For items previously specified by 6A005.f.1, see 6A004.f.

    f.2. ``Laser'' diagnostic equipment ``specially designed'' for
dynamic measurement of ``SHPL'' system angular beam steering errors
and having an angular ``accuracy'' of 10 [mu]rad (microradians) or
less (better);
    f.3. Optical equipment and ``components'', ``specially
designed'' for coherent beam combination in a phased-array ``SHPL''
system and having any of the following:
    f.3.a. An ``accuracy'' of 0.1 [micro]m or less, for wavelengths
greater than 1 [micro]m; or
    f.3.b. An ``accuracy'' of [lambda]/10 or less (better) at the
designed wavelength, for wavelengths equal to or less than 1
[micro]m;
    f.4. Projection telescopes ``specially designed'' for use with
``SHPL'' systems;
    g. `Laser acoustic detection equipment' having all of the
following:
    g.1. CW ``laser'' output power greater than or equal to 20 mW;

    g.2. ``Laser'' frequency stability equal to or better (less)
than 10 MHz;
    g.3. ``Laser'' wavelengths equal to or exceeding 1,000 nm but
not exceeding 2,000 nm;
    g.4. Optical system resolution better (less) than 1 nm; and
    g.5. Optical Signal to Noise ratio equal or exceeding to 10\3\.

    Technical Note: `Laser acoustic detection equipment' is
sometimes referred to as a ``Laser'' Microphone or Particle Flow
Detection Microphone.

0
52. In supplement no. 1 to part 774, Category 6, ECCN 6A008 is revised
to read as follows:

6A008 Radar systems, equipment and assemblies, having any of the
following (see List of Items Controlled), and ``specially designed''
``components'' therefor.

License Requirements

Reason for Control: NS, MT, RS, AT

                                              Country chart  (see Supp.
                Control(s)                       No. 1  to part 738)

NS applies to entire entry................  NS Column 2
MT applies to items that are designed for   MT Column 1
 airborne applications and that are usable
 in systems controlled for MT reasons.
RS applies to 6A008.j.1...................  RS Column 1
AT applies to entire entry................  AT Column 1

Reporting Requirements

See Sec.  743.1 of the EAR for reporting requirements for exports
under License Exceptions, and Validated End-User authorizations.

List Based License Exceptions (See Part 740 for a Description of all
License Exceptions)

LVS: $5,000; N/A for MT and for 6A008.j.1.
GBS: Yes, for 6A008.b, .c, and l.1 only
CIV: Yes, for 6A008.b, .c, and l.1 only

Special Conditions for STA

STA: License Exception STA may not be used to ship any commodity in
6A008.d, 6A008.h or 6A008.k to any of the destinations listed in
Country Group A:6 (See Supplement No. 1 to part 740 of the EAR).

List of Items Controlled

Related Controls: (1) See also ECCNs 6A108 and 6A998. ECCN 6A998
controls, inter alia, the Light Detection and Ranging (LIDAR)
equipment excluded by the note to paragraph j. of this ECCN (6A008).
(2) See USML Category XII(b) for certain LIDAR, Laser Detection and
Ranging (LADAR), or range-gated systems subject to the ITAR.
Related Definitions: N/A
Items:

    Note: 6A008 does not control:

--Secondary surveillance radar (SSR);
--Civil Automotive Radar;
--Displays or monitors used for air traffic control (ATC);
--Meteorological (weather) radar;
--Precision Approach Radar (PAR) equipment conforming to ICAO
standards and employing electronically steerable linear (1-
dimensional) arrays or mechanically positioned passive antennas.
    a. Operating at frequencies from 40 GHz to 230 GHz and having
any of the following:
    a.1. An average output power exceeding 100 mW; or
    a.2. Locating ``accuracy'' of 1 m or less (better) in range and
0.2 degree or less (better) in azimuth;
    b. A tunable bandwidth exceeding 6.25% of the
`center operating frequency;'

    Technical Note:  The `center operating frequency' equals one
half of the sum of the highest plus the lowest specified operating
frequencies.

    c. Capable of operating simultaneously on more than two carrier
frequencies;
    d. Capable of operating in synthetic aperture (SAR), inverse
synthetic aperture (ISAR) radar mode, or sidelooking airborne (SLAR)
radar mode;
    e. Incorporating electronically scanned array antennae;

    Technical Note: Electronically scanned array antennae are also
known as electronically steerable array antennae.

    f. Capable of heightfinding non-cooperative targets;
    g. ``Specially designed'' for airborne (balloon or airframe
mounted) operation and having Doppler ``signal processing'' for the
detection of moving targets;
    h. Employing processing of radar signals and using any of the
following:
    h.1. ``Radar spread spectrum'' techniques; or
    h.2. ``Radar frequency agility'' techniques;
    i. Providing ground-based operation with a maximum
``instrumented range'' exceeding 185 km;

    Note: 6A008.i does not control:
    a. Fishing ground surveillance radar;
    b. Ground radar equipment ``specially designed'' for en route
air traffic control, and having all of the following:
    1. A maximum ``instrumented range'' of 500 km or less;
    2. Configured so that radar target data can be transmitted only
one way from the radar site to one or more civil ATC centers;
    3. Contains no provisions for remote control of the radar scan
rate from the en route ATC center; and
    4. Permanently installed;
    c. Weather balloon tracking radars.

    j. Being ``laser'' radar or Light Detection and Ranging (LIDAR)
equipment and having any of the following:
    j.1. ``Space-qualified'';
    j.2. Employing coherent heterodyne or homodyne detection
techniques and having an angular resolution of less (better) than 20
[mu]rad (microradians); or
    j.3. Designed for carrying out airborne bathymetric littoral
surveys to International Hydrographic Organization (IHO) Order 1a
Standard (5th Edition February 2008) for Hydrographic Surveys or
better, and using one or more ``lasers'' with a wavelength exceeding
400 nm but not exceeding 600 nm;

    Note 1: LIDAR equipment ``specially designed'' for surveying is
only specified by 6A008.j.3.

    Note 2: 6A008.j does not apply to LIDAR equipment ``specially
designed'' for meteorological observation.

    Note 3: Parameters in the IHO Order 1a Standard 5th Edition
February 2008 are summarized as follows:
    Horizontal Accuracy (95% Confidence Level) = 5 m + 5% of depth.
    Depth Accuracy for Reduced Depths (95% confidence level) =
[radic](a\2\ + (b * d)\2\) where:
    a = 0.5 m = constant depth error, i.e. the sum of all constant
depth errors
    b = 0.013 = factor of depth dependant error
    b * d = depth dependant error, i.e. the sum of all depth
dependant errors
    d = depth
    Feature Detection = Cubic features >2 m in depths up to 40 m;
10% of depth beyond 40 m.

    k. Having ``signal processing'' sub-systems using ``pulse
compression'' and having any of the following:
    k.1. A ``pulse compression'' ratio exceeding 150; or
    k.2. A compressed pulse width of less than 200 ns; or

    Note: 6A008.k.2 does not apply to two dimensional `marine radar'
or `vessel traffic service' radar, having all of the following:
    a. ``Pulse compression'' ratio not exceeding 150;
    b. Compressed pulse width of greater than 30 ns;
    c. Single and rotating mechanically scanned antenna;
    d. Peak output power not exceeding 250 W; and
    e. Not capable of ``frequency hopping''.

    l. Having data processing sub-systems and having any of the
following:
    l.1. `Automatic target tracking' providing, at any antenna
rotation, the predicted target position beyond the time of the next
antenna beam passage; or

    Note: 6A008.l.1 does not control conflict alert capability in
ATC systems, or `marine radar.'

    Technical Note: `Automatic target tracking' is a processing
technique that automatically determines and provides as output an
extrapolated value of the most probable position of the target in
real time.

    l.2. [Reserved]
    l.3. [Reserved]
    l.4. Configured to provide superposition and correlation, or
fusion, of target data within six seconds from two or more
`geographically dispersed' radar sensors to improve the aggregate
performance beyond that of any single sensor specified by 6A008.f,
or 6A008.i.

    Technical Note: Sensors are considered `geographically
dispersed' when each location is distant from any other more than
1,500 m in any direction. Mobile sensors are

always considered `geographically dispersed'.

    N.B.: See also the U.S. Munitions List (22 CFR part 121).

    Note: 6A008.l does not apply to systems, equipment and
assemblies designed for `vessel traffic services.'

    Technical Notes:
    1. For the purposes of 6A008, `marine radar' is a radar that is
used to navigate safely at sea, inland waterways or near-shore
environments.
    2. For the purposes of 6A008, `vessel traffic service' is a
vessel traffic monitoring and control service similar to air traffic
control for ``aircraft''.

0
53. In supplement no. 1 to part 774, Category 6, ECCN 6A203 is revised
to read as follows:

6A203 High-speed cameras, imaging devices and ``components''
therefor, other than those controlled by 6A003 (see List of Items
Controlled).

License Requirements

Reason for Control: NP, AT

                                              Country chart  (see Supp.
                Control(s)                       No. 1  to part 738)

NP applies to entire entry................  NP Column 1
AT applies to entire entry................  AT Column 1

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

LVS: N/A
GBS: N/A
CIV: N/A

List of Items Controlled

Related Controls: (1) See ECCNs 6E001 (``development''), 6E002
(``production''), and 6E201 (``use'') for technology for items
controlled under this entry. (2) Also see ECCN 6A003.a.3, and a.4.
Related Definitions: N/A
Items:

    a. Streak cameras and ``specially designed'' components
therefor, as follows:
    a.1. Streak cameras with writing speeds greater than 0.5 mm/
[micro]s;
    a.2. Electronic streak cameras capable of 50 ns or less time
resolution;
    a.3. Streak tubes for cameras described in 6A203.a.2;
    a.4. Plug-ins, ``specially designed'' for use with streak
cameras having modular structures, that enable the performance
characteristics described in 6A203.a.1 or .a.2;
    a.5. Synchronizing electronics units, and rotor assemblies
consisting of turbines, mirrors and bearings, that are ``specially
designed'' for cameras described in 6A203.a.1.
    b. Framing cameras and ``specially designed'' components
therefor, as follows:
    b.1. Framing cameras with recording rates greater than 225,000
frames per second;
    b.2. Framing cameras capable of 50 ns or less frame exposure
time;
    b.3. Framing tubes, and solid-state imaging devices, that have a
fast image gating (shutter) time of 50 ns or less and are
``specially designed'' for cameras described in 6A203.b.1 or .b.2;
    b.4. Plug-ins, ``specially designed'' for use with framing
cameras having modular structures, that enable the performance
characteristics described in 6A203.b.1 or .b.2;
    b.5. Synchronizing electronic units, and rotor assemblies
consisting of turbines, mirrors and bearings, that are ``specially
designed'' for cameras described in 6A203.b.1 or .b.2.
    c. Solid-state or electron tube cameras and ``specially
designed'' components therefor, as follows:
    c.1. Solid-state cameras, or electron tube cameras, with a fast
image gating (shutter) time of 50 ns or less;
    c.2. Solid-state imaging devices, and image intensifiers tubes,
that have a fast image gating (shutter) time of 50 ns or less and
are ``specially designed'' for cameras described in 6A203.c.1;
    c.3. Electro-optical shuttering devices (Kerr or Pockels cells)
with a fast image gating (shutter) time of 50 ns or less;
    c.4. Plug-ins, ``specially designed'' for use with cameras
having modular structures, that enable the performance
characteristics described in 6A203.c.1.

    Technical Note:  High speed single frame cameras can be used
alone to produce a single image of a dynamic event, or several such
cameras can be combined in a sequentially-triggered system to
produce multiple images of an event.

    d. Radiation-hardened TV cameras, or lenses therefor,
``specially designed'' or rated as radiation hardened to withstand a
total radiation dose greater than 5 x 10\4\ Gy (silicon) without
operational degradation.

    Technical Note:  The term Gy (silicon) refers to the energy in
Joules per kilogram absorbed by an unshielded silicon sample when
exposed to ionizing radiation.

0
54. In supplement no. 1 to part 774, Category 6, ECCN 6A990 is removed.

0
55. In supplement no. 1 to part 774, Category 6, ECCN 6D003 is revised
to read as follows:

6D003 Other ``software'' as follows (see List of Items Controlled).

License Requirements

Reason for Control: NS, RS, AT

                                              Country chart  (see Supp.
                Control(s)                       No. 1  to part 738)

NS applies to entire entry................  NS Column 1
RS applies to paragraph c.................  RS Column 1
AT applies to entire entry................  AT Column 1

Reporting Requirements

See Sec.  743.1 of the EAR for reporting requirements for exports
under License Exceptions, and Validated End-User authorizations.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

CIV: Yes for 6D003.h.1
TSR: Yes, except for 6D003.c and exports or reexports to
destinations outside of those countries listed in Country Group A:5
(See Supplement No. 1 to part 740 of the EAR) of ``software'' for
items controlled by 6D003.a.

Special Conditions for STA

STA: License Exception STA may not be used to ship or transmit
software in 6D003.a to any of the destinations listed in Country
Group A:6 (See Supplement No.1 to part 740 of the EAR).

List of Items Controlled

Related Controls: See also ECCNs 6D103, 6D991, and 6D993.
Related Definitions: N/A
Items:

Acoustics

    a. ``Software'' as follows:
    a.1. ``Software'' ``specially designed'' for acoustic beam
forming for the ``real-time processing'' of acoustic data for
passive reception using towed hydrophone arrays;
    a.2. ``Source code'' for the ``real-time processing'' of
acoustic data for passive reception using towed hydrophone arrays;
    a.3. ``Software'' ``specially designed'' for acoustic beam
forming for the ``real-time processing'' of acoustic data for
passive reception using bottom or bay cable systems;
    a.4. ``Source code'' for the ``real-time processing'' of
acoustic data for passive reception using bottom or bay cable
systems;
    a.5. ``Software'' or ``source code'', ``specially designed'' for
all of the following:
    a.5.a. ``Real-time processing'' of acoustic data from sonar
systems controlled by 6A001.a.1.e; and
    a.5.b. Automatically detecting, classifying and determining the
location of divers or swimmers;

    N.B.: For diver detection ``software'' or ``source code'',
``specially designed'' or modified for military use, see the U.S.
Munitions List of the International Traffic in Arms Regulations
(ITAR) (22 CFR part 121).

    b. Optical sensors. None.

Cameras

    c. ``Software'' designed or modified for cameras incorporating
``focal plane arrays'' specified by 6A002.a.3.f and designed or
modified to remove a frame rate restriction and allow the camera to
exceed the frame rate specified in 6A003.b.4 Note 3.a;

Optics

    d. ``Software'' specially designed to maintain the alignment and
phasing of segmented mirror systems consisting of mirror segments
having a diameter or major axis length equal to or larger than 1 m;
    e. Lasers. None.

Magnetic and Electric Field Sensors

    f. ``Software'' as follows:
    f.1. ``Software'' ``specially designed'' for magnetic and
electric field ``compensation systems'' for magnetic sensors
designed to operate on mobile platforms;

    f.2. ``Software'' ``specially designed'' for magnetic and
electric field anomaly detection on mobile platforms;
    f.3. ``Software'' ``specially designed'' for ``real-time
processing'' of electromagnetic data using underwater
electromagnetic receivers specified by 6A006.e;
    f.4. ``Source code'' for ``real-time processing'' of
electromagnetic data using underwater electromagnetic receivers
specified by 6A006.e;

Gravimeters

    g. ``Software'' ``specially designed'' to correct motional
influences of gravity meters or gravity gradiometers;

Radar

    h. ``Software'' as follows:
    h.1. Air Traffic Control (ATC) ``software'' application
``programs'' designed to be hosted on general purpose computers
located at Air Traffic Control centers and capable of accepting
radar target data from more than four primary radars;
    h.2. ``Software'' for the design or ``production'' of radomes
having all of the following:
    h.2.a. ``Specially designed'' to protect the ``electronically
scanned array antennae'' specified by 6A008.e; and
    h.2.b. Resulting in an antenna pattern having an `average side
lobe level' more than 40 dB below the peak of the main beam level.

    Technical Note: `Average side lobe level' in 6D003.h.2.b is
measured over the entire array excluding the angular extent of the
main beam and the first two side lobes on either side of the main
beam.

0
56. In supplement no. 1 to part 774, Category 6, ECCN 6D991 is revised
to read as follows:

6D991 ``Software,'' n.e.s., ``specially designed'' for the
``development'', ``production'', or ``use'' of commodities
controlled by 6A002, 6A003, 6A991, 6A996, 6A997, or 6A998.

License Requirements

Reason for Control: RS, AT

                                            Country chart (see Supp. No.
                Control(s)                         1 to part 738)

RS applies to ``software'' for commodities  RS Column 1
 controlled by 6A002, 6A003, or 6A998.b.
RS applies to ``software'' for commodities  RS Column 2
 controlled by 6A998.c.
AT applies to entire entry, except          AT Column 1
 ``software'' for commodities controlled
 by 6A991.
AT applies to ``software'' for commodities  AT Column 2
 controlled by 6A991.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

CIV: N/A
TSR: N/A

List of Items Controlled

Related Controls: (1) See ECCN 6D002 for ``software'' ``specially
designed'' for the ``use'' of commodities controlled under ECCN
6A002.b. (2) See ECCN 6D003.c for ``software'' ``specially
designed'' for cameras incorporating ``focal plane arrays''
specified by 6A002.a.3.f and ``specially designed'' to remove a
frame rate restriction and allow the camera to exceed the frame rate
specified in 6A003.b.4 Note 3.a.
Related Definitions: N/A
Items:

    The list of items controlled is contained in the ECCN heading.

0
57. In supplement no. 1 to part 774, Category 6, ECCN 6E001 is revised
to read as follows:

6E001 ``Technology'' according to the General Technology Note for
the ``development'' of equipment, materials or ``software''
controlled by 6A (except 6A991, 6A992, 6A994, 6A995, 6A996, 6A997,
6A998, or 6A999.c), 6B (except 6B995), 6C (except 6C992 or 6C994),
or 6D (except 6D991, 6D992, or 6D993).

License Requirements

Reason for Control: NS, MT, NP, RS, CC, AT, UN

                                            Country chart (see Supp. No.
                Control(s)                         1  to part 738)

NS applies to ``technology'' for items      NS Column 1
 controlled by 6A001 to 6A008, 6B004 to
 6B008, 6C002 to 6C005, or 6D001 to 6D003.
MT applies to ``technology'' for items      MT Column 1
 controlled by 6A002, 6A007, 6A008, 6A102,
 6A107, 6A108, 6B008, 6B108, 6D001, 6D002,
 6D102 or 6D103 for MT reasons.
NP applies to ``technology'' for items      NP Column 1
 controlled by 6A003, 6A005, 6A202, 6A203,
 6A205, 6A225, 6A226, 6D001, or 6D201 for
 NP reasons.
RS applies to ``technology'' for items      RS Column 1
 controlled by 6A002.a.1, .a.2, .a.3, .c,
 or .f, 6A003.b.3 or .b.4, or 6A008.j.1.
CC applies to ``technology'' for equipment  CC Column 1
 controlled by 6A002 for CC reasons.
AT applies to entire entry................  AT Column 1
UN applies to ``technology'' for equipment  See Sec.   746.1(b) of the
 controlled by 6A002 or 6A003 for UN         EAR for UN controls
 reasons.

Reporting Requirements

See Sec.  743.1 of the EAR for reporting requirements for exports
under License Exceptions, and Validated End-User authorizations.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

CIV: N/A
TSR: Yes, except for the following: (1) Items controlled for MT
reasons; (2) ``Technology'' for commodities controlled by 6A002,
6A004.e or 6A008.j.1; (3) ``Technology'' for 6A003 cameras, unless
for ``technology'' for the integration of 6A003 cameras into camera
systems ``specially designed'' for civil automotive applications;
(4) ``Technology'' for ``software'' ``specially designed'' for
``space qualified'' ``laser'' radar or Light Detection and Ranging
(LIDAR) equipment defined in 6A008.j.1 and controlled by 6D001 or
6D002; or (5) Exports or reexports to destinations outside of those
countries listed in Country Group A:5 (See Supplement No. 1 to part
740 of the EAR) of ``technology'' for the ``development'' of the
following: (a) Items controlled by 6A001.a.1.b, 6A001.a.1.e,
6A001.a.2.a.1, 6A001.a.2.a.2, 6A001.a.2.a.3, 6A001.a.2.a.5,
6A001.a.2.a.6, 6A001.a.2.b, 6A001.a.2.d, 6A001.a.2.e, 6A004.c,
6A004.d, 6A006.a.2, 6A006.c.1, 6A006.d, 6A006.e, 6A008.d, 6A008.h,
6A008.k, 6B008, or 6D003.a; (b) Equipment controlled by 6A001.a.2.c
or 6A001.a.2.f when ``specially designed'' for real time
applications; or (c) ``Software'' controlled by 6D001 and
``specially designed'' for the ``development'' or ``production'' of
equipment controlled by 6B008, or 6D003.a.

Special Conditions for STA

STA: License Exception STA may not be used to ship or transmit any
technology in this entry to any of the destinations listed in
Country Group A:6 (See Supplement No.1 to part 740 of the EAR).

List of Items Controlled

Related Controls: (1) Technical data directly related to satellites
and all other items described in USML Category XV are subject to the
ITAR under USML Category XV(f). (2) Technical data directly related
to laser systems, infrared imaging systems, and all other items
described in USML Category XII are subject to the ITAR under USML
Category XII(f). (3) Technical data

directly related to read-out integrated circuits described in USML
Categories XII(e) or XV(e)(3) is subject to the ITAR under USML
Categories XII(f) or XV(f), respectively. (4) See also 6E101, 6E201,
and 6E991.
Related Definitions: N/A
Items:

    The list of items controlled is contained in the ECCN heading.

0
58. In supplement no. 1 to part 774, Category 6, ECCN 6E002 is revised
to read as follows:

6E002 ``Technology'' according to the General Technology Note for
the ``production'' of equipment or materials controlled by 6A
(except 6A991, 6A992, 6A994, 6A995, 6A996, 6A997, 6A998 or 6A999.c),
6B (except 6B995) or 6C (except 6C992 or 6C994).

License Requirements

Reason for Control: NS, MT, NP, RS, CC, AT, UN

                                            Country chart (see Supp. No.
                Control(s)                         1 to part 738)

NS applies to ``technology'' for equipment  NS Column 1
 controlled by 6A001 to 6A008, 6B004 to
 6B008, or 6C002 to 6C005.
MT applies to ``technology'' for equipment  MT Column 1
 controlled by 6A002, 6A007, 6A008, 6A102,
 6A107, 6A108, 6B008, or 6B108 for MT
 reasons.
NP applies to ``technology'' for items      NP Column 1
 controlled by 6A003, 6A005, 6A202, 6A203,
 6A205, 6A225 or 6A226 for NP reasons.
RS applies to ``technology'' for items      RS Column 1
 controlled by 6A002.a.1, .a.2, .a.3, .c,
 or .f, 6A003.b.3 or .b.4, or 6A008.j.1.
CC applies to ``technology'' for equipment  CC Column 1
 controlled by 6A002 for CC reasons.
AT applies to entire entry................  AT Column 1
UN applies to ``technology'' for equipment  See Sec.   746.1(b) of the
 controlled by 6A002 or 6A003 for UN         EAR for UN controls
 reasons.

Reporting Requirements

See Sec.  743.1 of the EAR for reporting requirements for exports
under License Exceptions, and Validated End-User authorizations.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

CIV: N/A
TSR: Yes, except for the following:
(1) Items controlled for MT reasons;
(2) ``Technology'' for commodities controlled by 6A002, 6A004.e, or
6A008.j.1;
(3) ``Technology'' for 6A003 cameras, unless for ``technology'' for
the integration of 6A003 cameras into camera systems ``specially
designed'' for civil automotive applications; or
(4) Exports or reexports to destinations outside of those countries
listed in Country Group A:5 (See Supplement No. 1 to part 740 of the
EAR) of ``technology'' for the ``production'' of the following: (a)
Items controlled by 6A001.a.1.b, 6A001.a.1.e, 6A001.a.2.a.1,
6A001.a.2.a.2, 6A001.a.2.a.3, 6A001.a.2.a.5, 6A001.a.2.a.6,
6A001.a.2.b, 6A004.c, 6A004.d, 6A006.a.2, 6A006.c.1, 6A006.d,
6A006.e, 6A008.d, 6A008.h, 6A008.k, or 6B008; and (b) Items
controlled by 6A001.a.2.c or 6A001.a.2.f when ``specially designed''
for real time applications.

Special Conditions for STA

STA: License Exception STA may not be used to ship or transmit
``technology'' according to the General Technology Note for the
``production'' of equipment specified in the STA exclusion
paragraphs found in the License Exception sections of by ECCNs
6A001, 6A002, 6A003, 6A004, 6A006, 6A008, or 6B008 to any of the
destinations listed in Country Group A:6 (See Supplement No. 1 to
part 740 of the EAR).

List of Items Controlled

Related Controls: (1) Technical data directly related to satellites
and all other items described in USML Category XV are subject to the
ITAR under USML Category XV(f). (2) Technical data directly related
to laser systems, infrared imaging systems, and all other items
described in USML Category XII are subject to the ITAR under USML
Category XII(f). (3) Technical data directly related to read-out
integrated circuits described in USML Categories XII(e) or XV(e)(3)
is subject to the ITAR under USML Categories XII(f) or XV(f),
respectively. (4) See also 6E992.
Related Definitions: N/A
Items:

    The list of items controlled is contained in the ECCN heading.

0
59. In supplement no. 1 to part 774, Category 6, ECCN 6E201 is revised
to read as follows:

6E201 ``Technology'' according to the General Technology Note for
the ``use'' of equipment controlled by 6A003.a.3, 6A003.a.4;
6A005.a.2, 6A005.b.2.b, 6A005.b.3, 6A005.b.4.b.2, 6A005.b.6.c,
6A005.c.1.b, 6A005.c.2.b, 6A005.d.2, 6A005.d.3.c, or 6A005.d.4.c
(that meet or exceed the parameters of 6A205); 6A202, 6A203, 6A205,
6A225 or 6A226.

License Requirements

Reason for Control: NP, AT

                                              Country chart  (see Supp.
                Control(s)                       No. 1  to part 738)

NP applies to entire entry................  NP Column 1
AT applies to entire entry................  AT Column 1

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

CIV: N/A
TSR: N/A

List of Items Controlled

Related Controls: N/A
Related Definitions: N/A
ECCN Controls: This entry only controls ``technology'' for
``lasers'' in 6A005 that are controlled for NP reasons.
Items:

    The list of items controlled is contained in the ECCN heading.

0
60. In supplement no. 1 to part 774, Category 6, ECCN 6E990 is removed.

0
61. In supplement no. 1 to part 774, Category 7, ECCN 7A006 is revised
to read as follows:

7A006 Airborne altimeters operating at frequencies other than 4.2 to
4.4 GHz inclusive and having any of the following (see List of Items
Controlled).

License Requirements

Reason for Control: NS, MT, AT

                                              Country chart  (see Supp.
                Control(s)                       No. 1  to part 738)

NS applies to entire entry................  NS Column 1
MT applies to commodities in this entry     MT Column 1
 that meet or exceed the parameters of
 7A106.
AT applies to entire entry................  AT Column 1

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

LVS: N/A
GBS: N/A
CIV: N/A

List of Items Controlled

Related Controls: See also 7A106, 7A994 and Category 6 for controls
on radar.
Related Definitions: N/A
Items:

    a. `Power management'; or

    Technical Note: `Power management' is changing the transmitted
power of the altimeter signal so that received power at the
``aircraft'' altitude is always at the minimum necessary to
determine the altitude.

    b. Using phase shift key modulation.

0
62. In supplement no. 1 to part 774, Category 7, ECCN 7E004 is revised
to read as follows:

7E004 Other ``technology'' as follows (see List of Items
Controlled).

License Requirements

Reason for Control: NS, MT, AT

                                              Country chart  (see Supp.
                Control(s)                       No. 1  to part 738)

NS applies to entire entry................  NS Column 1
MT applies to ``technology ''for equipment  MT Column 1
 or systems controlled for MT reasons.
AT applies to entire entry................  AT Column 1

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

CIV: N/A
TSR: N/A

Special Conditions for STA

STA: (1) Paragraph (c)(1) of License Exception STA (Sec.
740.20(c)(1) of the EAR) may not be used for 7E004, except for
7E004.a.7. (2) Paragraph (c)(2) of License Exception STA (Sec.
740.20(c)(2) of the EAR) may not be used for 7E004, except for
7E004.a.7.

List of Items Controlled

Related Controls: (1) See also 7E001, 7E002, 7E101, and 7E994. (2)
In addition to the Related Controls in 7E001, 7E002, and 7E101 that
include MT controls, also see the MT controls in 7E104 for design
``technology'' for the integration of the flight control, guidance,
and propulsion data into a flight management system, designed or
modified for rockets or missiles capable of achieving a ``range''
equal to or greater than 300 km, for optimization of rocket system
trajectory; and also see 9E101 for design ``technology'' for
integration of air vehicle fuselage, propulsion system and lifting
control surfaces, designed or modified for unmanned aerial vehicles
capable of achieving a ``range'' equal to or greater than 300 km, to
optimize aerodynamic performance throughout the flight regime of an
unmanned aerial vehicle.
Related Definitions: ``Primary flight control'' means an
``aircraft'' stability or maneuvering control using force/moment
generators, i.e., aerodynamic control surfaces or propulsive thrust
vectoring.
Items:

    a. ``Technology'' for the ``development'' or ``production'' of
any of the following:
    a.1. [Reserved]
    a.2. Air data systems based on surface static data only, i.e.,
which dispense with conventional air data probes;
    a.3. Three dimensional displays for ``aircraft'';
    a.4. [Reserved]
    a.5. Electric actuators (i.e., electromechanical,
electrohydrostatic and integrated actuator package) ``specially
designed'' for `primary flight control';

    Technical Note: `Primary flight control' is ``aircraft''
stability or manoeuvring control using force/moment generators, i.e.
aerodynamic control surfaces or propulsive thrust vectoring.

    a.6. `Flight control optical sensor array' ``specially
designed'' for implementing ``active flight control systems''; or

    Technical Note: A `flight control optical sensor array' is a
network of distributed optical sensors, using ``laser'' beams, to
provide real-time flight control data for on-board processing.

    a.7. ``DBRN'' systems designed to navigate underwater, using
sonar or gravity databases, that provide a positioning ``accuracy''
equal to or less (better) than 0.4 nautical miles;
    b. ``Development'' ``technology'', as follows, for ``active
flight control systems'' (including ``fly-by-wire systems'' or
``fly-by-light systems''):
    b.1. Photonic-based ``technology'' for sensing ``aircraft'' or
flight control component state, transferring flight control data, or
commanding actuator movement, ``required'' for ``fly-by-light
systems'' ``active flight control systems'';
    b.2. [Reserved]
    b.3. Real-time algorithms to analyze component sensor
information to predict and preemptively mitigate impending
degradation and failures of components within an ``active flight
control system'';

    Note: 7E004.b.3 does not include algorithms for purpose of off-
line maintenance.

    b.4. Real-time algorithms to identify component failures and
reconfigure force and moment controls to mitigate ``active flight
control system'' degradations and failures;

    Note: 7E004.b.4 does not include algorithms for the elimination
of fault effects through comparison of redundant data sources, or
off-line pre-planned responses to anticipated failures.

    b.5. Integration of digital flight control, navigation and
propulsion control data, into a digital flight management system for
``total control of flight'';

    Note:  7E004.b.5 does not apply to:
    1. ``Technology'' for integration of digital flight control,
navigation and propulsion control data, into a digital flight
management system for `flight path optimization';
    2. ``Technology'' for ``aircraft'' flight instrument systems
integrated solely for VOR, DME, ILS or MLS navigation or approaches.

    Technical Note:  `Flight path optimization' is a procedure that
minimizes deviations from a four-dimensional (space and time)
desired trajectory based on maximizing performance or effectiveness
for mission tasks.

    b.6. [Reserved]
    b.7. ``Technology'' ``required'' for deriving the functional
requirements for ``fly-by-wire systems'' having all of the
following:
    b.7.a. `Inner-loop' airframe stability controls requiring loop
closure rates of 40 Hz or greater; and

    Technical Note:  `Inner-loop' refers to functions of ``active
flight control systems'' that automate airframe stability controls.

    b.7.b. Having any of the following:
    b.7.b.1. Corrects an aerodynamically unstable airframe, measured
at any point in the design flight envelope, that would lose
recoverable control if not corrected within 0.5 seconds;
    b.7.b.2. Couples controls in two or more axes while compensating
for `abnormal changes in aircraft state;';

    Technical Note:  `Abnormal changes in aircraft state' include
in-flight structural damage, loss of engine thrust, disabled control
surface, or destabilizing shifts in cargo load.

    b.7.b.3. Performs the functions specified in 7E004.b.5; or

    Note: 7E004.b.7.b.3 does not apply to autopilots.

    b.7.b.4. Enables ``aircraft'' to have stable controlled flight,
other than during take-off or landing, at greater than 18 degrees
angle of attack, 15 degrees side slip, 15 degrees/second pitch or
yaw rate, or 90 degrees/second roll rate;
    b.8. ``Technology'' ``required'' for deriving the functional
requirements of ``fly-by-wire systems'' to achieve all of the
following:
    b.8.a. No loss of control of the ``aircraft'' in the event of a
consecutive sequence of any two individual faults within the ``fly-
by-wire system''; and
    b.8.b. Probability of loss of control of the ``aircraft'' being
less (better) than 1x10\-9\ failures per flight hour;

    Note:  7E004.b does not apply to ``technology'' associated with
common computer elements and utilities (e.g., input signal
acquisition, output signal transmission, computer program and data
loading, built-in test, task scheduling mechanisms) not providing a
specific flight control system function.

    c. ``Technology'' for the ``development'' of helicopter systems,
as follows:
    c.1. Multi-axis fly-by-wire or fly-by-light controllers, which
combine the functions of at least two 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 or circulation-
controlled direction control systems'';
    c.3. Rotor blades incorporating `variable geometry airfoils',
for use in systems using individual blade control.

    Technical Note:  `Variable geometry airfoils' use trailing edge
flaps or tabs, or leading edge slats or pivoted nose droop, the
position of which can be controlled in flight.

0
63. In supplement no. 1 to part 774, Category 9, ECCN 9A002 is revised
to read as follows:

9A002 `Marine gas turbine engines' designed to use liquid fuel and
having all of the following (see List of Items Controlled), and
``specially designed'' assemblies and ``components'' therefor.

License Requirements

Reason for Control: NS, AT

                                              Country chart  (see Supp.
                Control(s)                       No. 1 to part 738)

NS applies to entire entry................  NS Column 2
AT applies to entire entry................  AT Column 1

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

LVS: $5,000
GBS: N/A
CIV: N/A

List of Items Controlled:

Related Controls: N/A
Related Definition: N/A
Items:

    a. Maximum continuous power when operating in ``steady state
mode'' at standard reference conditions specified by ISO 3977-2:1997
(or national equivalent) of 24,245 kW or more; and
    b. `Corrected specific fuel consumption' not exceeding 0.219 kg/
kWh at 35% of the maximum continuous power when using liquid fuel.

    Note: The term `marine gas turbine engines' includes those
industrial, or aero-derivative, gas turbine engines adapted for a
ship's electric power generation or propulsion.

    Technical Note: For the purposes of 9A002, `corrected specific
fuel consumption' is the specific fuel consumption of the engine
corrected to a marine distillate liquid fuel having a net specific
energy (i.e., net heating value) of 42 MJ/kg (ISO 3977-2:1997).

0
64. In supplement no. 1 to part 774, Category 9, ECCN 9A004 is revised
to read as follows:

9A004 Space launch vehicles and ``spacecraft'', ``spacecraft
buses'', ``spacecraft payloads'', ``spacecraft'' on-board systems or
equipment, and terrestrial equipment, as follows (see List of Items
Controlled).

License Requirements

Reason for Control: NS and AT

                                            Country chart (see Supp. No.
                Control(s)                         1 to part 738)

NS applies to 9A004.u, .v, .w and .x......  NS Column 1
AT applies to 9A004.u, .v, .w, .x and .y..  AT Column 1

    License Requirements Note: 9A004.b through .f are controlled
under ECCN 9A515.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

LVS: N/A
GBS: N/A
CIV: N/A

List of Items Controlled

Related Controls: (1) See also 9A104, 9A515, and 9B515. (2) See
ECCNs 9E001 (``development'') and 9E002 (``production'') for
technology for items controlled by this entry. (3) See USML
Categories IV for the space launch vehicles and XV for other
spacecraft that are ``subject to the ITAR'' (see 22 CFR parts 120
through 130).
Related Definition: N/A
Items:

    a. Space launch vehicles;
    b. ``Spacecraft'';
    c. ``Spacecraft buses'';
    d. ``Spacecraft payloads'' incorporating items specified by
3A001.b.1.a.4, 3A002.g, 5A001.a.1, 5A001.b.3, 5A002.c, 5A002.e,
6A002.a.1, 6A002.a.2, 6A002.b, 6A002.d, 6A003.b, 6A004.c, 6A004.e,
6A008.d, 6A008.e, 6A008.k, 6A008.l or 9A010.c;
    e. On-board systems or equipment, specially designed for
``spacecraft'' and having any of the following functions:
    e.1. `Command and telemetry data handling;';

    Note: For the purpose of 9A004.e.1, `command and telemetry data
handling' includes bus data management, storage, and processing.

    e.2. `Payload data handling;' or

    Note:  For the purpose of 9A004.e.2, `payload data handling'
includes payload data management, storage, and processing.

    e.3. `Attitude and orbit control;';

    Note:  For the purpose of 9A004.e.3, `attitude and orbit
control' includes sensing and actuation to determine and control the
position and orientation of a ``spacecraft''.

    N.B.: Equipment specially designed for military use is ``subject
to the ITAR''. See 22 CFR parts 120 through 130.

    f. Terrestrial equipment specially designed for ``spacecraft'',
as follows:
    f.1. Telemetry and telecommand equipment ``specially designed''
for any of the following data processing functions:
    f.1.a. Telemetry data processing of frame synchronization and
error corrections, for monitoring of operational status (also known
as health and safe status) of the ``spacecraft bus''; or
    f.1.b. Command data processing for formatting command data being
sent to the ``spacecraft'' to control the ``spacecraft bus'';
    f.2. Simulators ``specially designed'' for `verification of
operational procedures' of ``spacecraft''.

    Technical Note: For the purposes of 9A004.f.2, `verification of
operational procedures' is any of the following:
    1. Command sequence confirmation;
    2. Operational training;
    3. Operational rehearsals; or
    4. Operational analysis.

    g. through t. [Reserved]
    u. The James Webb Space Telescope (JWST) being developed,
launched, and operated under the supervision of the U.S. National
Aeronautics and Space Administration (NASA).
    v. ``Parts'', ``components'', ``accessories'' and
``attachments'' that are ``specially designed'' for the James Webb
Space Telescope and that are not:
    v.1. Enumerated or controlled in the USML;
    v.2. Microelectronic circuits;
    v.3. Described in ECCNs 7A004 or 7A104; or
    v.4. Described in an ECCN containing ``space-qualified'' as a
control criterion (See ECCN 9A515.x.4).
    w. The International Space Station being developed, launched,
and operated under the supervision of the U.S. National Aeronautics
and Space Administration.
    x. ``Parts'', ``components'', ``accessories'' and
``attachments'' that are ``specially designed'' for the
International Space Station.
    y. Items that would otherwise be within the scope of ECCN
9A004.v or .x but that have been identified in an interagency-
cleared commodity classification (CCATS) pursuant to Sec.  748.3(e)
of the EAR as warranting control in 9A004.y.

0
65. In supplement no. 1 to part 774, Category 9, ECCN 9D001 is revised
to read as follows:

9D001 ``Software'', not specified in 9D003 or 9D004, ``specially
designed'' or modified for the ``development'' of equipment or
``technology'' controlled by ECCN 9A001 to 9A004, 9A012, 9A101
(except for items in 9A101.b that are ``subject to the ITAR'', see
22 CFR part 121), 9A106.d. or .e, 9A110, or 9A120, 9B (except for
ECCNs 9B604, 9B610, 9B619, 9B990, and 9B991), or ECCN 9E003.

License Requirements

Reason for Control: NS, MT, AT

                                              Country chart  (see Supp.
                Control(s)                       No. 1  to part 738)

NS applies to ``software'' for equipment    NS Column 1
 controlled by 9A001 to 9A004, 9A012,
 9B001 to 9B010, and technology controlled
 by 9E003.
MT applies to ``software'' for equipment    MT Column 1
 controlled by 9B116 for MT reasons.
AT applies to entire entry................  AT Column 1

Reporting Requirements

See Sec.  743.1 of the EAR for reporting requirements for exports
under License Exceptions, and Validated End-User authorizations.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

CIV: N/A
TSR: N/A

Special Conditions for STA

STA: License Exception STA may not be used to ship or transmit
``software'' ``specially designed'' or modified for the
``development'' of equipment or ``technology'', specified by ECCNs
9B001.b. or 9E003.a.1, 9E003.a.2 to a.5, 9E003.a.8, or 9E003.h to
any of the destinations listed in

Country Group A:6 (See Supplement No.1 to part 740 of the EAR).

List of Items Controlled

Related Controls: ``Software'' that is ``required'' for the
``development'' of items specified in ECCNs 9A005 to 9A011, 9A101.b
(except for items that are subject to the EAR), 9A103 to 9A105,
9A106.a, .b, and .c, 9A107 to 9A109, 9A110 (for items that are
``specially designed'' for use in missile systems and subsystems),
and 9A111 to 9A119 is ``subject to the ITAR''.
Related Definitions: N/A
Items:

    The list of items controlled is contained in the ECCN heading.

0
66. In supplement no. 1 to part 774, Category 9, ECCN 9D002 is revised
to read as follows:

9D002 ``Software'', not specified in 9D003 or 9D004, ``specially
designed'' or modified for the ``production'' of equipment
controlled by ECCN 9A001 to 9A004, 9A012, 9A101 (except for items in
9A101.b that are ``subject to the ITAR'', see 22 CFR part 121),
9A106.d or .e, 9A110, or 9A120, 9B (except for ECCNs 9B604, 9B610,
9B619, 9B990, and 9B991).

License Requirements

Reason for Control: NS, MT, AT

                                              Country chart  (see Supp.
                Control(s)                       No. 1  to part 738)

NS applies to ``software'' for equipment    NS Column 1
 controlled by 9A001 to 9A004, 9A012,
 9B001 to 9B010.
MT applies to ``software'' for equipment    MT Column 1
 controlled by 9B116 for MT reasons.
AT applies to entire entry................  AT Column 1

Reporting Requirements

See Sec.  743.1 of the EAR for reporting requirements for exports
under License Exceptions, and Validated End-User authorizations.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

CIV: N/A
TSR: N/A.

Special Conditions for STA

STA: License Exception STA may not be used to ship or transmit
``software'' ``specially designed'' or modified for the
``production'' of equipment specified by 9B001.b to any of the
destinations listed in Country Group A:6 (See Supplement No.1 to
part 740 of the EAR).

List of Items Controlled

Related Controls: ``Software'' that is ``required'' for the
``production'' of items specified in ECCNs 9A005 to 9A011, 9A101.b
(except for items that are subject to the EAR), 9A103 to 9A105,
9A106.a, .b, and .c, 9A107 to 9A109, 9A110 (for items that are
``specially designed'' for use in missile systems and subsystems),
and 9A111 to 9A119 is ``subject to the ITAR''.
Related Definitions: N/A
Items:

    The list of items controlled is contained in the ECCN heading.

0
67. In supplement no. 1 to part 774, Category 9, ECCN 9D004 is revised
to read as follows:

9D004 Other ``software'' as follows (see List of Items Controlled).

License Requirements

Reason for Control: NS, AT

                                              Country chart  (see Supp.
                Control(s)                       No. 1  to part 738)

NS applies to entire entry................  NS Column 1
AT applies to entire entry................  AT Column 1

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

CIV: N/A
TSR: N/A.

Special Conditions for STA

STA: License Exception STA may not be used to ship or transmit
software in 9D004.a and 9D004.c to any of the destinations listed in
Country Group A:6 (See Supplement No.1 to part 740 of the EAR)

List of Items Controlled

Related Controls: See also 9D104.
Related Definitions: N/A
Items:

    a. 2D or 3D viscous ``software'', validated with wind tunnel or
flight test data required for detailed engine flow modelling;
    b. ``Software'' for testing aero gas turbine engines,
assemblies, ``parts'' or ``components'', having all of the
following:
    b.1. ``Specially designed'' for testing any of the following:
    b.1.a. Aero gas turbine engines, assemblies or components,
incorporating ``technology'' specified by 9E003.a, 9E003.h or
9E003.i; or
    b.1.b. Multi-stage compressors providing either bypass or core
flow, specially designed for aero gas turbine engines incorporating
``technology'' specified by 9E003.a or 9E003.h; and
    b.2. ``Specially designed'' for all of the following:
    a. Acquisition and processing of data, in real time; and
    b. Feedback control of the test article or test conditions
(e.g., temperature, pressure, flow rate) while the test is in
progress;

    Note: 9D004.b does not specify software for operation of the
test facility or operator safety (e.g., overspeed shutdown, fire
detection and suppression), or production, repair or maintenance
acceptance-testing limited to determining if the item has been
properly assembled or repaired.

    c. ``Software'' ``specially designed'' to control directional
solidification or single crystal material growth in equipment
specified by 9B001.a or 9B001.c;
    d. [Reserved]
    e. ``Software'' ``specially designed'' or modified for the
operation of items specified by 9A012;
    f. ``Software'' ``specially designed'' to design the internal
cooling passages of aero gas turbine engine blades, vanes and ``tip
shrouds'';
    g. ``Software'' having all of the following:
    g.1. ``Specially designed'' to predict aero thermal,
aeromechanical and combustion conditions in aero gas turbine
engines; and
    g.2. Theoretical modeling predictions of the aero thermal,
aeromechanical and combustion conditions, which have been validated
with actual turbine engine (experimental or production) performance
data.

0
68. In supplement no. 1 to part 774, Category 9, ECCN 9E003 is revised
to read as follows:

9E003 Other ``technology'' as follows (see List of Items
Controlled).

License Requirements

Reason for Control: NS, SI, AT

                                              Country chart  (see Supp.
                Control(s)                       No. 1  to part 738)

NS applies to entire entry................  NS Column 1
SI applies to 9E003.a.1 through a.8, .h,    See Sec.   742.14 of the EAR
 .i, and .k.                                 for additional information.
AT applies to entire entry................  AT Column 1

Reporting Requirements

See Sec.  743.1 of the EAR for reporting requirements for exports
under License Exceptions, and Validated End-User authorizations.

List Based License Exceptions (See Part 740 for a Description of All
License Exceptions)

CIV: N/A
TSR: N/A

Special Conditions for STA

STA: License Exception STA may not be used to ship or transmit any
technology in 9E003.a.1, 9E003.a.2 to a.5, 9E003.a.8, or 9E003.h to
any of the destinations listed in Country Group A:6 (See Supplement
No.1 to part 740 of the EAR).

List of Items Controlled

Related Controls: (1) Hot section ``technology'' specifically
designed, modified, or equipped for military uses or purposes, or
developed principally with U.S. Department of Defense funding, is
``subject to the ITAR'' (see 22 CFR parts 120 through 130). (2)
``Technology'' is subject to the EAR when actually applied to a
commercial ``aircraft'' engine program. Exporters may seek to
establish commercial application either on a case-by-case basis
through submission of documentation demonstrating application

to a commercial program in requesting an export license from the
Department Commerce in respect to a specific export, or in the case
of use for broad categories of ``aircraft'', engines, ``parts'' or
``components'', a commodity jurisdiction determination from the
Department of State.
Related Definitions: N/A
Items:

    a. ``Technology'' ``required'' for the ``development'' or
``production'' of any of the following gas turbine engine ``parts'',
``components'' or systems:
    a.1. Gas turbine blades, vanes or ``tip shrouds'', made from
directionally solidified (DS) or single crystal (SC) alloys and
having (in the 001 Miller Index Direction) a stress-rupture life
exceeding 400 hours at 1,273 K (1,000 [deg]C) at a stress of 200
MPa, based on the average property values;

    Technical Note: For the purposes of 9E003.a.1, stress-rupture
life testing is typically conducted on a test specimen.

    a.2. Combustors having any of the following:
    a.2.a. `Thermally decoupled liners' designed to operate at
`combustor exit temperature' exceeding 1,883K (1,610 [deg]C);
    a.2.b. Non-metallic liners;
    a.2.c. Non-metallic shells; or
    a.2.d. Liners designed to operate at `combustor exit
temperature' exceeding 1,883K (1,610 [deg]C) and having holes that
meet the parameters specified by 9E003.c;

    Note: The ``required'' ``technology'' for holes in 9E003.a.2 is
limited to the derivation of the geometry and location of the holes.

    Technical Notes:
    1. `Thermally decoupled liners' are liners that feature at least
a support structure designed to carry mechanical loads and a
combustion facing structure designed to protect the support
structure from the heat of combustion. The combustion facing
structure and support structure have independent thermal
displacement (mechanical displacement due to thermal load) with
respect to one another, i.e. they are thermally decoupled.
    2. `Combustor exit temperature' is the bulk average gas path
total (stagnation) temperature between the combustor exit plane and
the leading edge of the turbine inlet guide vane (i.e., measured at
engine station T40 as defined in SAE ARP 755A) when the engine is
running in a ``steady state mode'' of operation at the certificated
maximum continuous operating temperature.

    N.B.: See 9E003.c for ``technology'' ``required'' for
manufacturing cooling holes.

    a.3. ``Parts'' or ``components'', that are any of the following:
    a.3.a. Manufactured from organic ``composite'' materials
designed to operate above 588 K (315 [deg]C);
    a.3.b. Manufactured from any of the following:
    a.3.b.1. Metal ``matrix'' ``composites'' reinforced by any of
the following:
    a.3.b.1.a. Materials controlled by 1C007;
    a.3.b.1.b. ``Fibrous or filamentary materials'' specified by
1C010; or
    a.3.b.1.c. Aluminides specified by 1C002.a; or
    a.3.b.2. Ceramic ``matrix'' ``composites'' specified by 1C007;
or
    a.3.c. Stators, vanes, blades, tip seals (shrouds), rotating
blings, rotating blisks or `splitter ducts,' that are all of the
following:
    a.3.c.1. Not specified in 9E003.a.3.a;
    a.3.c.2. Designed for compressors or fans; and
    a.3.c.3. Manufactured from material controlled by 1C010.e with
resins controlled by 1C008;

    Technical Note: A `splitter duct' performs the initial
separation of the air-mass flow between the bypass and core sections
of the engine.

    a.4. Uncooled turbine blades, vanes or ``tip shrouds'' designed
to operate at a `gas path temperature' of 1,373 K (1,100 [deg]C) or
more;