Office of Commercial Space Transportation: Millennium Engineering and Integration Company Safety Approval Performance Criteria, 7287 [2018-03399]

Download as PDF Federal Register / Vol. 83, No. 34 / Tuesday, February 20, 2018 / Notices sradovich on DSK3GMQ082PROD with NOTICES 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 E:\FR\FM\20FEN1.SGM 20FEN1

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]


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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.

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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