Office of Commercial Space Transportation: Millennium Engineering and Integration Company Safety Approval Performance Criteria, 7287 [2018-03399]
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Federal Register / Vol. 83, No. 34 / Tuesday, February 20, 2018 / Notices
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said North line a distance of 383.10 feet
to the point of beginning.
Parcel 57
A parcel of land being a part of the
Southwest Quarter of the Southeast
Quarter, the Southeast Quarter of the
Southwest Quarter of Section 14, the
Northwest Quarter of the Northeast
Quarter, the Northeast Quarter of the
Northwest Quarter, the Southwest
Quarter of the Northwest Quarter, the
Southeast Quarter of the Northwest
Quarter, the Northwest Quarter of the
Southwest Quarter, the Northeast
Quarter of the Southwest Quarter, the
Southwest Quarter of the Southwest
Quarter and the Southeast Quarter of the
Southwest Quarter of Section 23, T24N,
R8E, City of Stevens Point, Portage
County, Wisconsin more fully described
as follows:
Commencing at the West Quarter
Corner of Section 14; Thence S89°48′07″
E along the North line of the Southwest
Quarter of Section 14 a distance of
2630.42 feet to a 2″ Iron Pipe also being
the Center of Section 14; Thence
S00°24′38″ E along the East line of the
Southwest Quarter of Section 14 a
distance of 1314.25 feet to the
Northwest Corner of the Southwest
Quarter of the Southeast Quarter of
Section 14 also being the point of
beginning. Thence S89°50′51″ E along
the North line of the Southwest Quarter
of the Southeast Quarter of Section 14
a distance of 742.80 feet; Thence
S00°21′56″ E a distance of 1312.22 feet
to its intersection with the South line of
the Southwest Quarter of the Southeast
Quarter of Section 14; Thence
S89°59′49″ W along said South line a
distance of 622.73 feet; Thence
S29°39′41″ W a distance of 2807.79 feet
to the West line of the Southeast Quarter
of the Northwest Quarter of Section 23;
Thence S00°27′59″ E along said West
line a distance of 211.40 feet to the
Northwest Corner of the Northeast
Quarter of the Southwest Quarter of
Section 23; Thence S00°24′01″ E along
the West line of the Northeast Quarter
of the Southwest Quarter of Section 23
a distance of 1328.47 feet to the
Southwest Corner of the Northeast
Quarter of the Southwest Quarter of
Section 23; Thence N89°53′32″ E along
the South line of the Northeast Quarter
of the Southwest Quarter of Section 23
a distance of 1309.80 feet to the
Northeast Corner of the Southeast
Quarter of the Southwest Quarter of
Section 23; Thence S00°43′30″ E along
the East line of the Southeast Quarter of
the Southwest Quarter of Section 23 a
distance of 350.02 feet; Thence
S89°53′32″ W a distance of 877.14 feet;
Thence N57°30′33″ W a distance of
VerDate Sep<11>2014
17:55 Feb 16, 2018
Jkt 244001
618.84 feet; Thence N00°24′01″ W a
distance of 1344.59 feet; Thence
N00°27′59″ W a distance of 196.38 feet;
Thence N29°39′41″ E a distance of
2452.09 feet; Thence N38°12′00″ E a
distance of 1292.15 feet; Thence
N22°27′46″ W a distance of 602.03 feet;
Thence N89°50′51″ W a distance of
436.79 feet; Thence N89°48′28″ W a
distance of 675.78 feet;
Thence S40°22′20″ W a distance of
152.91 feet; Thence N49°37′40″ W a
distance of 99.84 feet to its intersection
with the Southeasterly Right-of-Way of
STH 66; Thence N40°23′54″ E along said
Southeasterly line a distance of 155.05
feet to its intersection with the North
line of the Southeast Quarter of the
Southwest Quarter of Section 14;
Thence S89°48′28″ E along said North
line a distance of 750.60 feet to the
point of beginning.
Issued in Des Plaines, IL, on January 25,
2018.
Deb Bartell,
Manager, Chicago Airports District Office,
FAA, Great Lakes Region.
[FR Doc. 2018–03423 Filed 2–16–18; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Office of Commercial Space
Transportation: Millennium
Engineering and Integration Company
Safety Approval Performance Criteria
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice.
AGENCY:
This is notification of criteria
used to evaluate the Millennium
Engineering and Integration Company
(MEI) safety approval application. This
Notice publishes the criteria that the
FAA used to evaluate the safety
approval application pursuant to FAA
regulations.
Background: MEI applied for, and
received, a safety approval for its ability
to provide its Flight Analyst
Workstation (FAWS) as a component of
the process to build flight rules,
generate the Mission Data Load (MDL),
and verify the MDL prior to loading it
onto a launch vehicle’s autonomous
flight safety unit (AFSU).
The FAA issued MEI the safety
approval, subject to the provisions of
Title 51 U.S.C. Subtitle V, ch. 509, and
the orders, rules and regulations issued
under it. This Notice is published
pursuant to Title 14 Code of Federal
Regulations (14 CFR 414.35).
MEI may offer FAWS as a component
of the process of generating and
SUMMARY:
PO 00000
Frm 00152
Fmt 4703
Sfmt 9990
7287
verifying MDLs for AFSUs to a
prospective launch or reentry operator
to meet the applicable requirements of
14 CFR 417.123(b), (d), and (e), and
§ 417.309(h).
Criteria Used To Evaluate Safety
Approval Application: The performance
criteria used to evaluate the FAWS as a
component of the process of generating
and verifying MDLs for AFSUs included
the following FAA regulations, NASA
standard, U.S. Air Force manuals or
instructions, industry standard, and
MEI-developed standards:
14 CFR 417.309(h) Flight Safety
System Analysis—Software and
Firmware and 14 CFR 417.123
Computing Systems and Software.
NASA–STD–8719.13C Software
Safety Standard.
AFSPCMAN 91–710 (v1) Range Safety
Policies and Procedures, AFSPCMAN
91–710 (v2) Range Safety User
Requirements Manual, Volume 2—
Flight Safety Requirements,
AFSPCMAN 91–712 Launch Safety
Software and Computing System
Requirements, and 45 SWI 91–701 45th
Space Wing Launch Safety Software
Management.
CMMI–Dev (ML3) Capability Maturity
Model Integration.
MEI–000071 Configuration
Management, MEI–000120
Requirements Development and
Management, MEI–000124 Technical
Solution, MEI–000149 Agile Software
Development Process, and MEI–000125
Verification and Validation.
For
questions about the performance
criteria, you may contact Randal Maday,
Licensing and Evaluation Division
(AST–200), FAA Office of Commercial
Space Transportation (AST), 800
Independence Avenue SW, Room 331,
Washington, DC 20591, telephone (202)
267–8652; Email randal.maday@
faa.gov.
FOR FURTHER INFORMATION CONTACT:
Issued in Washington, DC, on 9 February
2018.
George C. Nield,
Associate Administrator for Commercial
Space Transportation.
[FR Doc. 2018–03399 Filed 2–16–18; 8:45 am]
BILLING CODE 4910–13–P
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]]>Agencies
[Federal Register Volume 83, Number 34 (Tuesday, February 20, 2018)]
[Notices]
[Page 7287]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-03399]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Office of Commercial Space Transportation: Millennium Engineering
and Integration Company Safety Approval Performance Criteria
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice.
-----------------------------------------------------------------------
SUMMARY: This is notification of criteria used to evaluate the
Millennium Engineering and Integration Company (MEI) safety approval
application. This Notice publishes the criteria that the FAA used to
evaluate the safety approval application pursuant to FAA regulations.
Background: MEI applied for, and received, a safety approval for
its ability to provide its Flight Analyst Workstation (FAWS) as a
component of the process to build flight rules, generate the Mission
Data Load (MDL), and verify the MDL prior to loading it onto a launch
vehicle's autonomous flight safety unit (AFSU).
The FAA issued MEI the safety approval, subject to the provisions
of Title 51 U.S.C. Subtitle V, ch. 509, and the orders, rules and
regulations issued under it. This Notice is published pursuant to Title
14 Code of Federal Regulations (14 CFR 414.35).
MEI may offer FAWS as a component of the process of generating and
verifying MDLs for AFSUs to a prospective launch or reentry operator to
meet the applicable requirements of 14 CFR 417.123(b), (d), and (e),
and Sec. 417.309(h).
Criteria Used To Evaluate Safety Approval Application: The
performance criteria used to evaluate the FAWS as a component of the
process of generating and verifying MDLs for AFSUs included the
following FAA regulations, NASA standard, U.S. Air Force manuals or
instructions, industry standard, and MEI-developed standards:
14 CFR 417.309(h) Flight Safety System Analysis--Software and
Firmware and 14 CFR 417.123 Computing Systems and Software.
NASA-STD-8719.13C Software Safety Standard.
AFSPCMAN 91-710 (v1) Range Safety Policies and Procedures, AFSPCMAN
91-710 (v2) Range Safety User Requirements Manual, Volume 2--Flight
Safety Requirements, AFSPCMAN 91-712 Launch Safety Software and
Computing System Requirements, and 45 SWI 91-701 45th Space Wing Launch
Safety Software Management.
CMMI-Dev (ML3) Capability Maturity Model Integration.
MEI-000071 Configuration Management, MEI-000120 Requirements
Development and Management, MEI-000124 Technical Solution, MEI-000149
Agile Software Development Process, and MEI-000125 Verification and
Validation.
FOR FURTHER INFORMATION CONTACT: For questions about the performance
criteria, you may contact Randal Maday, Licensing and Evaluation
Division (AST-200), FAA Office of Commercial Space Transportation
(AST), 800 Independence Avenue SW, Room 331, Washington, DC 20591,
telephone (202) 267-8652; Email [email protected].
Issued in Washington, DC, on 9 February 2018.
George C. Nield,
Associate Administrator for Commercial Space Transportation.
[FR Doc. 2018-03399 Filed 2-16-18; 8:45 am]
BILLING CODE 4910-13-P
