a.9. Designed or modified to use or perform ``quantum
cryptography.''
    Technical Note: ``Quantum cryptography'' is also known as
Quantum Key Distribution (QKD).
    b. Systems, equipment and components, designed or modified to
enable, by means of ``cryptographic activation'', an item to achieve
or exceed the controlled performance levels for functionality
specified by 5A002.a that would not otherwise be enabled.

0
39. In Supplement No. 1 to part 774, ECCN 5D002 is amended by
0
a. Adding a Note to 5D002.c after Items paragraph c.2; and
0
b. Revising Items paragraph d.
    The revisions read as follows:

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

* * * * *
    List of Items Controlled
* * * * *
    Items: * * *
    c. * * *
    c.2. * * *
    Note: 5D002.c does not apply to ``software'' limited to the
tasks of ``OAM'' implementing only published or commercial
cryptographic standards.
    d. ``Software'' designed or modified to enable, by means of
``cryptographic activation,'' an item to achieve or exceed the
controlled performance levels for functionality specified by 5A002.a
that would not otherwise be enabled.

0
40. In Supplement No. 1 to part 774, ECCN 5E002 is amended by revising
Items paragraph b and the Note to 5E002 to read as follows:

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

* * * * *
    List of Items Controlled
* * * * *
    Items:* * *
    b. ``Technology'' to enable, by means of ``cryptographic
activation,'' an item to achieve or exceed the controlled
performance levels for functionality specified by 5A002.a that would
not otherwise be enabled.
    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
41. In Supplement No. 1 to part 774, ECCN 6A001 is amended by:

0
a. Revising Items paragraph a.1.a.2.a.2 and the Technical Note
following Items paragraph a.1.a.2.a.2;
0
b. Revising the introductory text of Items paragraph a.1.a.3;
0
c. Revising Note 1 after Items paragraph a.1.c;
0
d. Revising Items paragraph a.1.c.1;
0
e. Removing and reserving Items paragraph a.1.c.2 and removing the
Technical Note following Items paragraph a.1.c.2; and
0
f. Adding a N.B. after paragraph a.1.c.2.
    The revisions and additions read as follows:

6A001 Acoustic Systems, Equipment and ``Components'', as Follows
(see List of Items Controlled)

* * * * *
    List of Items Controlled
* * * * *
    Items: a. * * *
    a.1. * * *
    a.1.a. * * *
    a.1.a.2 * * *
    a.1.a.2.a. * * *
    a.1.a.2.a.2. `Sounding rate' greater than 3,800 m/s; or
    Technical Note: `Sounding rate' is the product of the maximum
speed (m/s) at which the sensor can operate and the maximum number
of soundings per swath assuming 100% coverage. For systems that
produce soundings in two directions (3D sonars), the maximum of the
`sounding rate' in either direction should be used.
* * * * *
    a.1.a.3. Side Scan Sonar (SSS) or Synthetic Aperture Sonar
(SAS), designed for seabed imaging and having all of the following,
and specially designed transmitting and receiving acoustic arrays
therefor:
* * * * *
    a.1.c. * * *
    Notes: 1. The control status of acoustic projectors, including
transducers, ``specially designed'' for other equipment not
specified by 6A001 is determined by the control status of the other
equipment.
* * * * *
    a.1.c.1. Operating at frequencies below 10 kHz and having any of
the following:
    a.1.c.1.a. Not designed for continuous operation at 100% duty
cycle and having a radiated `free-field Source Level (SLRMS)'
exceeding (10log(f) + 169.77)dB (reference 1 [mu]Pa at 1 m) where f
is the frequency in Hertz of maximum Transmitting Voltage Response
(TVR) below 10 kHz; or
    a.1.c.1.b. Designed for continuous operation at 100% duty cycle
and having a continuously radiated `free-field Source Level (SLRMS)'
at 100% duty cycle exceeding (10log(f) + 159.77)dB (reference 1
[mu]Pa at 1 m) where f is the frequency in Hertz of maximum
Transmitting Voltage Response (TVR) below 10 kHz; or
    Technical Note: The `free-field Source Level (SLRMS)' is defined
along the maximum response axis and in the far field of the acoustic
projector. It can be obtained from the Transmitting Voltage Response
using the following equation: SLRMS = (TVR + 20log VRMS) dB (ref
1[mu]Pa at 1 m), where SLRMS is the source level, TVR is the
Transmitting Voltage Response and VRMS is the Driving Voltage of the
Projector.
* * * * *
    N.B.: See 6A001.a.1.c.1 for items previously specified in
6A001a.1.c.2.
* * * * *

0
42. In Supplement No. 1 to part 774, ECCN 6A003 is amended by:
0
a. Remove the entry ``RS applies to 6A003.b.4.b'' from the table in the
License Requirements section;
0
b. Revising the Reporting Requirements in the License Requirements
section;
0
c. Revising Items paragraph a.3;
0
d. Revising paragraph b.4.c in Note 3 to 6A003.b.4.b; and
0
e. Revising paragraph b in Note 4 to 6A003.b.4.c.
    The revisions read as follows:

6A003 Cameras, Systems or Equipment, and ``Components'' Therefor,
as Follows (see List of Items Controlled)

* * * * *
    License Requirements
* * * * *
    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 of Items Controlled
* * * * *
    Items: a. * * *
    a.3. Mechanical or electronic streak cameras as follows:
    a.3.a. Mechanical streak cameras having writing speeds exceeding
10 mm/[mu]s;
    a.3.b. Electronic streak cameras having temporal resolution
better than 50 ns;
* * * * *
    b. ***
    b.4. ***
    b.4.c. ***
    Note 3: ***
    b. ***
    4. ***
    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: ***
    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;
* * * * *

0
43. In Supplement No. 1 to part 774, ECCN 6A004 is amended by:
0
a. Revising the GBS and CIV paragraphs under the List Based License
Exceptions section;
0
b. Adding a Technical Note after the introductory text of Items
paragraph a;
0
c. Revising Items paragraph a.1;
0
d. Revising Items paragraph a.4;
0
e. Revising Items paragraph d.2;
0
f. Removing and reserving Items paragraph d.4.
    The revisions and additions read as follows:

6A004 Optical Equipment and ``Components,'' as Follows (see List of
Items Controlled)

* * * * *
    List Based License Exceptions (See Part 740 for a description of
all license exceptions)
* * * * *
    GBS: Yes for 6A004.a.1, a.2, a.4, b, and d.2.
    CIV: Yes for 6A004.a.1, a.2, a.4, b, and d.2.
* * * * *
    List of Items Controlled
* * * * *
    Items: a. ***
    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;
* * * * *
    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.
* * * * *
    d. ***
    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;
    d.2.b. Resonator alignment equipment having bandwidths equal to
or more than 100 Hz and an accuracy of 10 [mu]rad or less;
* * * * *

0
44. In Supplement No. 1 to part 774, ECCN 6A005 is amended by:
0
a. Removing the Note to 6A005.c after Items paragraph c;
0
b. Revising Items paragraph e.2; and
0
c. Adding Items paragraph e.3.
    The revision and additions 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)

* * * * *
    List of Items Controlled
* * * * *
    Items:
* * * * *
    e. ***
    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\;
* * * * *

0
45. In Supplement No. 1 to part 774, ECCN 6C005 is amended by:
0
a. Revising the heading; and
0
b. Revising the Items paragraphs.
0
The revisions read as follows:

6C005 ``Laser'' Materials as Follows (see List of Items Controlled)

* * * * *
    List of Items Controlled
* * * * *
    Items: a. Synthetic crystalline ``laser'' host material in
unfinished form as follows:
    a.1. Titanium doped sapphire;
    a.2. [Reserved]
    b. Rare-earth-metal doped double-clad fibers having any of the
following:
    b.1. Nominal laser wavelength of 975 nm to 1,150 nm and having
all of the following:
    b.1.a. Average core diameter equal to or greater than 25 [mu]m;
and
    b.1.b. Core `Numerical Aperture' (`NA') less than 0.065; or
    Note to 6C005.b.1: 6C005.b.1 does not apply to double-clad
fibers having an inner glass cladding diameter exceeding 150 [mu]m
and not exceeding 300 [mu]m.
    b.2. Nominal laser wavelength exceeding 1,530 nm and having all
of the following:
    b.2.a. Average core diameter equal to or greater than 20 [mu]m;
and
    b.2.b. Core `NA' less than 0.1.
    Technical Notes: 1. For the purposes of 6C005, the core
`Numerical Aperture' (`NA') is measured at the emission wavelengths
of the fiber.
    2. 6C005.b includes fibers assembled with end caps.

0
46. In Supplement No. 1 to part 774, ECCN 6D003 is amended by:
0
a. Adding an undesignated center heading before Items paragraph d; and
0
b. Revising Items paragraph d.
    The addition and revision read as follows:

6D003 Other ``Software'' as Follows (see List of Items Controlled)

* * * * *
    List of Items Controlled
* * * * *
    Items:
* * * * *
    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;
* * * * *

0
47. In Supplement No. 1 to part 774, ECCN 7A003 is amended by revising
Note 2 in the Items paragraph to read as follows:

7A003 `Inertial Measurement Equipment or Systems', Having Any of
the Following (see List of Items Controlled)

* * * * *
    List of Items Controlled
* * * * *
    Items:
* * * * *
    Note 2: 7A003 does not apply to `inertial measurement equipment
or systems' which are certified for use on ``civil aircraft'' by
civil aviation authorities of one or more Wassenaar Arrangement
Participating States, see Supplement No. 1 to part 743 of the EAR.
* * * * *

0
48. In Supplement No. 1 to part 774, ECCN 7D004 is amended by:
0
a. Revising the Related Controls paragraph in the List of Items
Controlled section; and
0
b. Revising Items paragraph c.
    The revisions read as follows:

7D004 ``Source Code'' Incorporating ``Development'' ``Technology''
Specified by 7E004.a.1 to a.6 or 7E004.b, For Any of the Following:
(see List of Items Controlled)

* * * * *
    List of Items Controlled
    Related Controls: See also 7D103 and 7D994
* * * * *
    Items: ***
    c. ``Fly-by-wire systems'' or ``fly-by-light systems``;
* * * * *

0
49. In Supplement No. 1 to part 774, ECCN 7E001 is amended by revising
the heading to read as follows:

7E001 ``Technology'' According to the General Technology Note for
the ``Development'' of Equipment or ``Software'', Specified by 7A.
(except 7A994), 7B. (except 7B994), 7D001, 7D002, 7D003 or 7D005.

* * * * *

0
50. In Supplement No. 1 to part 774, ECCN 7E004 is amended by:
0
a. Revising the Related Controls paragraph in the List of Items
Controlled;
0
b. Revising Items paragraphs b introductory text and b.1;
0
c. Removing the Note after Items paragraph b.6;
0
d. Adding Items paragraphs b.7 and b.8.
    The revisions and additions read as follows:

7E004 Other ``Technology'' as Follows (see List of Items
Controlled)

* * * * *
    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.
* * * * *
    Items: ***
    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.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.
* * * * *

0
51. In Supplement No. 1 to part 774, ECCN 8A001 is amended by removing
the semicolon at the end of paragraph e.2. and adding in its place a
period and removing Items paragraph f through the Technical Note
following i.2.
0
52. In Supplement No. 1 to part 774, ECCN 8A002 is amended by removing
and reserving Items paragraphs k through n and o.1.
0
53. In Supplement No. 1 to part 774, ECCN 8A620 is amended by revising
Items paragraph f to read as follows:

8A620 Submersible Vessels, Oceanographic and Associated Commodities
(see List of Items Controlled)

* * * * *
    List of Items Controlled
* * * * *
    Items: ***
    f. Closed and semi-closed circuit (rebreathing) apparatus
``specially designed'' or modified for military use and not
enumerated elsewhere in the CCL or in the USML.
* * * * *

0
54. In Supplement No. 1 to part 774, ECCN 8E002 is amended by:
0
a. Revising the TSR paragraph in the List Based License Exceptions
section;
0
b. Adding a Note at the end of the List Based License Exceptions
section; and
0
c. Adding Items paragraph c.
    The revision and additions read as follows:

8E002 Other ``Technology'' as Follows (see List of Items
Controlled)

* * * * *
    List Based License Exceptions (See Part 740 for a description of
all license exceptions)
* * * * *
    TSR: N/A
    License Exceptions Note: License Exception TSU is not applicable
for the repair ``technology'' controlled by 8E002.a or .b, see
Supplement No. 2 to this part.
* * * * *
    List of Items Controlled
* * * * *
    Items: * * *
    c. ``Technology'' according to the General Technology Note for
the ``development'' or ``production'' of any of the following:
    c.1. Surface-effect vehicles (fully skirted variety) having all
of the following:
    c.1.a. Maximum design speed, fully loaded, exceeding 30 knots in
a significant wave height of 1.25 m or more;
    c.1.b. Cushion pressure exceeding 3,830 Pa; and
    c.1.c. Light-ship-to-full-load displacement ratio of less than
0.70;
    c.2. Surface-effect vehicles (rigid sidewalls) with a maximum
design speed, fully loaded, exceeding 40 knots in a significant wave
height of 3.25 m or more;
    c.3. Hydrofoil vessels with active systems for automatically
controlling foil systems, with a maximum design speed, fully loaded,
of 40 knots or more in a significant wave height of 3.25 m or more;
or
    c.4. `Small waterplane area vessels' having any of the
following:
    c.4.a. Full load displacement exceeding 500 tonnes with a
maximum design speed, fully loaded, exceeding 35 knots in a
significant wave height of 3.25 m or more; or
    c.4.b. Full load displacement exceeding 1,500 tonnes with a
maximum design speed, fully loaded, exceeding 25 knots in a
significant wave height of 4 m or more.
    Technical Note: A 'small waterplane area vessel' is defined by
the following formula: waterplane area at an operational design
draft less than 2x (displaced volume at the operational design
draft). \2\ / \3\

0
54. In Supplement No. 1 to part 774, ECCN 9A001 is amended by revising
Notes 1 and 2 to Items paragraph a to read as follows:

9A001 Aero Gas Turbine Engines Having Any of the Following (see
List of Items Controlled)

* * * * *
    List of Items Controlled
* * * * *
    Items: a. ***
    Note 1: 9A001.a does not control aero gas turbine engines which
meet all of the following:
    a. Certified by civil aviation authorities of one or more
Wassenaar Arrangement Participating States listed in Supplement No.
1 to Part 743; and
    b. Intended to power non-military manned aircraft for which any
of the following has been issued by civil aviation authorities of
one or more Wassenaar Arrangement Participating States listed in
Supplement No. 1 to Part 743 for the aircraft with this specific
engine type:
    b.1. A civil type certificate; or
    b.2. An equivalent document recognized by the International
Civil Aviation Organization (ICAO).

    Note 2: 9A001.a does not apply to aero gas turbine engines for
Auxiliary Power Units (APUs) approved by the civil aviation
authority of Wassenaar Arrangement Participating States (see
Supplement No. 1 to part 743 of the EAR).
* * * * *

0
55. In Supplement No. 1 to part 774, ECCN 9A003 is amended by:
0
a. Revising the heading; and
0
b. Revising Items paragraph b.
    The revisions read as follows:

9A003 ``Specially Designed'' Assemblies or ``Components,''
Incorporating Any of the ``Technologies'' Controlled by 9E003.a,
9E003.h or 9E003.i, For Any of the Following Aero Gas Turbine
Engines (see List of Items Controlled)

* * * * *
    List of Items Controlled
* * * * *
    Items: ***
    b. Whose design or production origins are either not from a
Wassenaar Participating State (see Supplement No. 1 to part 743 of
the EAR) or unknown to the manufacturer.

0
56. In Supplement No. 1 to part 774, ECCN 9A004 is amended by:
0
a. Revising the heading;
0
b. Revising the License Requirements section;
0
c. Redesignating Items paragraph a as paragraph w and adding new
paragraph .a;
0
d. Adding paragraphs b. through f.
    The revisions and addition 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.w and .x..............  NS Column 1
AT applies to 9A004.w, .x and .y..........  AT Column 1
------------------------------------------------------------------------

    License Requirement Note: 9A004.a through .f are controlled
under ECCN 9A515.
* * * * *

List of Items Controlled

* * * * *
    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.a.5, 5A002.a.9,
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;
    f.2. Simulators.
* * * * *

0
57. In Supplement No. 1 to part 774, ECCN 9A010 is revised to read as
follows:

9A010 ``Specially Designed'' ``Parts,'' ``Components,'' Systems and
Structures, for Launch Vehicles, Launch Vehicle Propulsion Systems
or ``Spacecraft''. (These items are ``subject to the ITAR.'' See 22
CFR parts 120 through 130.)

List of Items Controlled

    Items:
    a. ``Parts'', ``components'' and structures, each exceeding 10
kg and ``specially designed'' for launch vehicles manufactured using
any of the following:
    a.1. ``Composite'' materials consisting of ``fibrous or
filamentary materials'' specified by 1C010.e and resins specified by
1C008 or 1C009.b;
    a.2. Metal ``matrix'' ``composites'' reinforced by any of the
following:
    a.2.a. Materials specified by 1C007;
    a.2.b. ``Fibrous or filamentary materials'' specified by 1C010;
or
    a.2.c. Aluminides specified by 1C002.a; or
    a.3. Ceramic ``matrix'' ``composite'' materials specified by
1C007;
    Note: The weight cut-off is not relevant for nose cones.
    b. ``Parts'', ``components'' and structures, ``specially
designed'' for launch vehicle propulsion systems specified by 9A005
to 9A009, manufactured using any of the following:
    b.1. ``Fibrous or filamentary materials'' specified by 1C010.e
and resins specified by 1C008 or 1C009.b;
    b.2. Metal ``Matrix ``composites'' reinforced by any of the
following:
    b.2.a. Materials specified by 1C007;
    b.2.b. ``Fibrous or filamentary materials'' specified by 1C010;
or
    b.2.c. Aluminides specified by 1C002.a; or
    b.3. Ceramic ``matrix'' ``composite'' materials specified by
1C007;
    c. Structural components and isolation systems, specially
designed to control actively the dynamic response or distortion of
``spacecraft'' structures;
    d. Pulsed liquid rocket engines with thrust-to-weight ratios
equal to or more than 1 kN/kg and a response time (the time required
to achieve 90% of total rated thrust from start-up) of less than 30
ms.

0
58. In Supplement No. 1 to part 774, ECCN 9A012 is amended by:
0
a. Revising the heading;
0
b. Revising the second entry in the table under the License
Requirements section; and
0
c. Revising Items paragraphs a through b.2 and b.4.
    The revisions read as follows:

9A012 Non-military ``Unmanned Aerial Vehicles,'' (``UAVs''),
Unmanned ``Airships'', Related Equipment and ``Components'', as
Follows (see List of Items Controlled)

    License Requirements
* * * * *

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

                                * * * * *
MT applies to non-military Unmanned Air     MT Column 1
 Vehicle (UAVs) and Remotely Piloted
 Vehicles (RPVs) that are capable of a
 maximum range of at least 300 kilometers
 (km), regardless of payload.

                                * * * * *
------------------------------------------------------------------------

* * * * *
    List of Items Controlled
* * * * *
    Items: a. ``UAVs'' or unmanned ``airships'', designed to have
controlled flight out of the direct `natural vision' of the
`operator' and having any of the following:
    a.1. Having all of the following:
    a.1.a. A maximum `endurance' greater than or equal to 30 minutes
but less than 1 hour; and
    a.1.b. Designed to take-off and have stable controlled flight in
wind gusts equal to or exceeding 46.3 km/h (25 knots); or
    a.2. A maximum `endurance' of 1 hour or greater;
    Technical Notes: 1. For the purposes of 9A012.a, `operator' is a
person who initiates or commands the ``UAV'' or unmanned ``airship''
flight.
    2. For the purposes of 9A012.a, `endurance' is to be calculated
for ISA conditions (ISO 2533:1975) at sea level in zero wind.
    3. For the purposes of 9A012.a, `natural vision' means unaided
human sight, with or without corrective lenses.
    b. Related equipment and ``components'', as follows:
    b.1 [Reserved]
    b.2. [Reserved]
* * * * *

    b.4. Air breathing reciprocating or rotary internal combustion
type engines, ``specially designed'' or modified to propel ``UAVs''
or unmanned ``airships'', at altitudes above 15,240 meters (50,000
feet).
    Note: 9A012 does not control model aircraft or model
``airships''.

0
59. In Supplement No. 1 to part 774, ECCN 9B001 is amended by:
0
a. Revising the heading;
0
b. Revising the Special Conditions for STA section;
0
c. Revising Items paragraph b; and
0
d. Adding Items paragraph c.
    The revisions and addition read as follows:

9B001 Equipment, Tooling or Fixtures, ``Specially Designed'' for
Manufacturing Gas Turbine Engine Blades, Vanes or ``Tip Shrouds'',
as Follows (See List of Items Controlled)

* * * * *
    Special Conditions for STA
    STA: License Exception STA may not be used to ship commodities
in 9B001 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
* * * * *
    Items: * * *
    b. Cores or shells (moulds), specially designed for casting,
manufactured from refractory metals or ceramics;
    c. Directional-solidification or single-crystal additive-
manufacturing equipment.

0
60. In Supplement No. 1 to part 774, ECCN 9B010 is amended by revising
the heading to read as follows:

9B010 Equipment ``Specially Designed'' for the Production of Items
Specified by 9A012

* * * * *

0
61. In Supplement No. 1 to part 774, ECCN 9D003 is amended by revising
the heading to read as follows:

9D003 ``Software'' Incorporating ``Technology'' Specified by ECCN
9E003.h and Used in ``FADEC Systems'' for Systems Controlled by
ECCN 9A001 to 9A003, 9A101 (Except for Items in 9A101.b That Are
``Subject to the ITAR'', See 22 CFR Part 121), 9A106.d or .e, or 9B
(Except for ECCNs 9B604, 9B610, 9B619, 9B990, and 9B991).

* * * * *

0
62. In Supplement No. 1 to part 774, ECCN 9D004 is amended by revising
Items paragraphs c and e to read as follows:

9D004 Other ``Software'' as Follows (See List of Items Controlled).

* * * * *
    List of Items Controlled
* * * * *
    Items: * * *
    c. ``Software'' ``specially designed'' to control directional
solidification or single crystal material growth in equipment
specified by 9B001.a or 9B001.c;
* * * * *
    e. ``Software'' ``specially designed'' or modified for the
operation of items specified by 9A012;
* * * * *

0
63. In Supplement No. 1 to part 774, ECCN 9D005 is added to the
Commerce Control List after ECCN 9D004 to read as follows:

9D005 ``Software'' Specially Designed or Modified for the Operation
of Items Specified by 9A004.e or 9A004.f. (This ``Software'' Is
Controlled by ECCN 9D515)

0
64. In Supplement No. 1 to part 774, ECCN 9E003 is amended by:
0
c. Revising the second entry in the table in the License Requirements
section;
0
d. Revising Items paragraphs a.3 and a.4;
0
e. Revising the Note to 9E003.h after Items paragraph h.3;
0
f. Redesignating Items paragraph j as paragraph k; and
0
g. Adding new Items paragraph .j.
    The revisions and addition read as follows:

9E003 Other ``Technology'' as Follows (See List of Items Controlled).

    License Requirements
* * * * *

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

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

                                * * * * *
------------------------------------------------------------------------

* * * * *
    List of Items Controlled
* * * * *
    Items: a. * * *
    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;
* * * * *
    h. * * *
    h.3. * * *
    Note: 9E003.h does not apply to technical data related to
engine-aircraft integration required by civil aviation authorities
of one or more Wassenaar Arrangement Participating States (See
Supplement No. 1 to part 743 of the EAR) to be published for general
airline use (e.g., installation manuals, operating instructions,
instructions for continued airworthiness) or interface functions
(e.g., input/output processing, airframe thrust or shaft power
demand).
* * * * *
    j. ``Technology'' ``required'' for the ``development'' of wing-
folding systems designed for fixed-wing aircraft powered by gas
turbine engines.
    N.B.: For ``technology'' ``required'' for the ``development'' of
wing-folding systems designed for fixed-wing aircraft specified in
USML Category VIII (a), see USML Category VIII (i).
* * * * *

Supplement No. 5 to Part 774 [AMENDED]

0
65. Supplement No. 5 to part 774 is amended by:
0
a. Removing and reserving item No. 2 under the heading ``0D521.
Software''; and
0
b. Removing item No. 6 under the heading ``0E521. Technology''.
0
66. Supplement No. 6 to part 774 is amended by:
0
a. Revising paragraph (2);
0
b. Removing and reserving paragraph (5)(iv); and
0
c. Revising paragraph (9)(ii).
    The revisions read as follows:

Supplement No. 6 to Part 774--Sensitive List

* * * * *

(2) Category 2

    (i) 2D001--``Software'', other than that controlled by 2D002,
specially designed for the ``development'' or ``production'' of
equipment as follows:
    (A) Machine tools for turning (ECCN 2B001.a) having all of the
following:
    (1) ``Unidirectional positioning repeatability'' equal to or
less (better) than 1.1 [micro]m along one or more linear axis; and
    (2) Two or more axes which can be coordinated simultaneously for
``contouring control'';
    (B) Machine tools for milling (ECCN 2B001.b) having any of the
following:
    (1) Having all of the following:

    (a) ``Unidirectional positioning repeatability'' equal to or
less (better) than 1.1 [micro]m along one or more linear axis; and
    (b) Three linear axes plus one rotary axis which can be
coordinated simultaneously for ``contouring control'';
    (2) Specified by 2B001.b.2.a, 2B001.b.2.b or 2B001.b.2.c and
having a ``unidirectional positioning repeatability'' equal to or
less (better) than 1.1 [micro]m along one or more linear axis; or
    (3) A ``unidirectional positioning repeatability'' for jig
boring machines equal to or less (better) than 1.1 [micro]m along
one or more linear axis;
    (C) Electrical discharge machines (EDM) controlled under
2B001.d;
    (D) Deep-hole-drilling machines controlled under 2B001.f;
    (E) ``Numerically controlled'' or manual machine tools
controlled under 2B003.
    (ii) 2E001--``Technology'' according to the General Technology
Note for the ``development'' of ``software'' specified by 2D001
described in this Supplement or for the ``development'' of equipment
as follows:
    (A) Machine tools for turning (ECCN 2B001.a) having all of the
following:
    (1) ``Unidirectional positioning repeatability'' equal to or
less (better) than 1.1 [micro]m along one or more linear axis; and
    (2) Two or more axes which can be coordinated simultaneously for
``contouring control'';
    (B) Machine tools for milling (ECCN 2B001.b) having any of the
following:
    (1) Having all of the following:
    (a) ``Unidirectional positioning repeatability'' equal to or
less (better) than 1.1 [micro]m along one or more linear axis; and
    (b) Three linear axes plus one rotary axis which can be
coordinated simultaneously for ``contouring control'';
    (2) Specified by 2B001.b.2.a, 2B001.b.2.b or 2B001.b.2.c and
having a ``unidirectional positioning repeatability'' equal to or
less (better) than 1.1 [micro]m along one or more linear axis; or
    (3) A ``unidirectional positioning repeatability'' for jig
boring machines equal to or less (better) than 1.1 [micro]m along
one or more linear axis;
    (C) Electrical discharge machines (EDM) controlled under
2B001.d;
    (D) Deep-hole-drilling machines controlled under 2B001.f;
    (E) ``Numerically controlled'' or manual machine tools
controlled under 2B003.
    (iii) 2E002--``Technology'' according to the General Technology
Note for the ``production'' of equipment as follows:
    (A) Machine tools for turning (ECCN 2B001.a) having all of the
following:
    (1) ``Unidirectional positioning repeatability'' equal to or
less (better) than 1.1 [micro]m along one or more linear axis; and
    (2) Two or more axes which can be coordinated simultaneously for
``contouring control'';
    (B) Machine tools for milling (ECCN 2B001.b) having any of the
following:
    (1) Having all of the following:
    (a) ``Unidirectional positioning repeatability'' equal to or
less (better) than 1.1 [micro]m along one or more linear axis; and
    (b) Three linear axes plus one rotary axis which can be
coordinated simultaneously for ``contouring control'';
    (2) Specified by 2B001.b.2.a, 2B001.b.2.b or 2B001.b.2.c and
having a ``unidirectional positioning repeatability'' equal to or
less (better) than 1.1 [micro]m along one or more linear axis; or
    (3) A ``unidirectional positioning repeatability'' for jig
boring machines equal to or less (better) than 1.1 [micro]m along
one or more linear axis;
    (C) Electrical discharge machines (EDM) controlled under
2B001.d;
    (D) Deep-hole-drilling machines controlled under 2B001.f;
    (E) ``Numerically controlled'' or manual machine tools
controlled under 2B003.
* * * * *
    (9) Category 9
* * * * *
    (ii) 9B001
* * * * *

    Dated: May 1, 2015.
Kevin J. Wolf,
Assistant Secretary for Export Administration.
[FR Doc. 2015-10579 Filed 5-20-15; 8:45 am]
 BILLING CODE 3510-33-P


[Federal Register Volume 84, Number 211 (Thursday, October 31, 2019)]
[Notices]
[Pages 58379-58380]
[FR Doc No: 2019-23721]

=======================================================================
-----------------------------------------------------------------------

ENVIRONMENTAL PROTECTION AGENCY

[EPA-HQ-OAR-2004-0060; FRL-10001-77-OMS]

Information Collection Request Submitted to OMB for Review and
Approval; Comment Request; Certification and Compliance Requirements
for Nonroad Spark-Ignition Engines (Renewal)

AGENCY: Environmental Protection Agency.

ACTION: Notice.

-----------------------------------------------------------------------

SUMMARY: The Environmental Protection Agency (EPA) has submitted an
information collection request (ICR), Certification and Compliance
Requirements for Nonroad Spark-Ignition Engines (EPA ICR Number
1695.13, OMB Control Number 2060-0338) to the Office of Management and
Budget (OMB) for review and approval in accordance with the Paperwork
Reduction Act. This notice is a proposed extension of the ICR, which is
currently approved through October 31, 2019. Public comments were
previously requested via the Federal Register on July 2, 2019 during a
60-day comment period. This notice allows for an additional 30 days for
public comments. A fuller description of the ICR is given below,
including its estimated burden and cost to the public. An agency may
not conduct or sponsor and a person is not required to respond to a
collection of information unless it displays a currently valid OMB
control number.

DATES: Additional comments must be submitted on or before December 2,
2019.

ADDRESSES: Submit your comments, referencing the Docket ID No. EPA-HQ-
OAR-2004-0060, to the EPA: Online using www.regulations.gov (our
preferred method), or by mail to: EPA Docket Center, Environmental

Protection Agency, Mail Code 28221T, 1200 Pennsylvania Ave. NW,
Washington, DC 20460.
    EPA's policy is that all comments received will be included in the
public docket without change including any personal information
provided, unless the comment includes profanity, threats, information
claimed to be Confidential Business Information (CBI) or other
information whose disclosure is restricted by statute.

FOR FURTHER INFORMATION CONTACT: Julian Davis, Attorney Adviser,
Compliance Division, Office of Transportation and Air Quality, U.S.
Environmental Protection Agency, 2000 Traverwood, Ann Arbor, Michigan
48105; telephone number:<PHONE_NUMBER>; fax number<PHONE_NUMBER>; email
address<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION: Supporting documents, which explain in
detail the information that the EPA will be collecting, are available
in the public docket, EPA-HQ-OAR-2004-0060, for this ICR. The docket
can be viewed online at www.regulations.gov or in person at the EPA
Docket Center, EPA West, Room 3334, 1301 Constitution Ave. NW,
Washington, DC. The telephone number for the Docket Center is 202-566-
1744. For additional information about EPA's public docket, visit
http://www.epa.gov/dockets.
    Abstract: As required by the Clean Air Act, EPA has regulations
establishing emission standards and other requirements for various
classes of vehicles, engines, and evaporative emissions. These
regulations require that compliance be demonstrated prior to EPA
granting a ``Certificate of Conformity.'' EPA is charged with issuing
certificates of conformity for those engines which comply with
applicable emission standards. Such a certificate must be issued before
engines may be legally introduced into commerce. To apply for a
certificate of conformity, manufacturers are required to submit
descriptions of their planned production line, including detailed
descriptions of the emission control system, and test data. The
emission values achieved during certification testing may also be used
in the Averaging, Banking, and Trading (ABT) Program. The program
allows manufacturers to bank credits for engine families that emit
below the standard and use the credits for families that emit above the
standard. They may also trade banked credits with other manufacturers.
Participation in the ABT program is voluntary. Different categories of
spark-ignition engines may also be required to comply with production-
line testing (PLT) and in-use testing. There are also recordkeeping and
labeling requirements. This information is collected electronically by
the Gasoline Engine Compliance Center (GECC) at the U.S. Environmental
Protection Agency. GECC uses this information to ensure that
manufacturers comply with applicable regulations and the Clean Air Act
(CAA). It may also be used by the Office of Enforcement and Compliance
Assurance (OECA) and the Department of Justice for enforcement
purposes. Non-CBI may be disclosed on OTAQ's website or upon request
under the Freedom of Information Act (FOIA) to trade associations,
environmental groups, and the public. Any information submitted for
which a claim of confidentiality is made is safeguarded according to
EPA regulations at 40 CFR 2.201 et seq.
    Form Numbers: NR Small SI Bond Worksheet (5900-450); NR Small SI
Small Volume Bond Worksheet (5900-451); Altitude Worksheet (5900-452);
Annual Production Worksheet (5900-90); NR Small SI Production Line
Testing Report (5900-133); NR Small SI Averaging, Banking, and Trading
Report (5900-131); Evaporative Fuel Cap Test Data (5900-453);
Evaporative Fuel Line Test Data (5900-454); Evaporative Fuel Tank Data
Worksheet (5900-455); Marine and Large SI Diurnal System Data Worksheet
(5900-456); NR Small SI Equipment Worksheet (5900-457); Marine SI
Vessel Worksheet (5900-458); Marine SI Engine Data Map Sheet (5900-
459); Marine SI Averaging, Banking, and Trading Report (5900-92);
Marine SI Production Line Testing Report (5900-91); Large SI Production
Line Testing Report (5900-130); Large SI In-Use Testing Report (5900-
93); Marine SI In-Use Testing Report (5900-93); Snowmobile Production
Line Testing Report (5900-460); Rec Vehicle and ATV Production Line
Testing Report (5900-461); Rec Vehicle Averaging, Banking and Trading
Report (5900-462); Snowmobile Certification Template (5900-463); Rec
Vehicle Catalytic Converter Checklist (5900-464); Snowmobile Averaging,
Banking, and Trading Template (5900-465); Rec Vehicle Fuel Line Test
Data Worksheet (5900-466); Rec Vehicle Fuel Tank Test Data Worksheet
(5900-467).
    Respondents/affected entities: Manufacturers of nonroad engines and
evaporative components.
    Estimated number of respondents: 620 (total).
    Frequency of response: Yearly for certification, production, ABT,
and warranty reports.
    Total estimated burden: 281,351 hours (per year). Burden is defined
at 5 CFR 1320.3(b)
    Total estimated cost: $34,342,007 (per year), includes $12,374,111
annualized capital or operation & maintenance costs.
    Changes in Estimates: There is an increase of 15,876 hours (from
265,475 hours to 281,351) in the total estimated burden in this
collection from the burden currently identified in the OMB Inventory of
Approved ICRs. This increase in hours is primarily attributed to an
increase in the total number of respondents, though primarily from
evaporative components, and an adjustment in the hours required to file
a complete application for certification and conduct compliance
activities throughout a calendar year.

Courtney Kerwin,
Director, Collection Strategies Division.
[FR Doc. 2019-23721 Filed 10-30-19; 8:45 am]
BILLING CODE 6560-50-P