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UFC 3-130-04 16 January 2025 UNIFIED FACILITIES CRITERIA (UFC) APPROVED FOR PUBLIC RELEASE; DISTRIBUTION UNLIMITED ARCTIC AND SUBARCTIC BUILDINGS UFC 3-130-04 16 January 2025 This Page Intentionally Left Blank UFC 3-130-04 16 January 2025 UNIFIED FACILITIES CRITERIA (UFC) ARCTIC AND SUBARCTIC BUILDINGS Any copyrighted material included in this UFC is identified at its point of use. Use of the copyrighted material apart from this UFC must have the permission of the copyright holder. U.S. ARMY CORPS OF ENGINEERS (Preparing Activity) NAVAL FACILITIES ENGINEERING SYSTEMS COMMAND AIR FORCE CIVIL ENGINEER CENTER Record of Changes (changes are indicated by \1\ ... /1/) Change No. Date Location This UFC supersedes UFC 3-130-07, dated 16 January 2004. UFC 3-130-04 16 January 2025 This Page Intentio
ENCES. Appendix C contains a list of references used in this document. The publication date of the code or standard is not included in this document. Unless otherwise specified, the most recent edition of the referenced publication applies. UFC 3-130-04 16 January 2025 4 This Page Intentionally Left Blank UFC 3-130-04 16 January 2025 5 CHAPTER 2 DESIGN CONSIDERATIONS 2-1 ENVIRONMENTAL FACTORS AND CONSIDERATIONS. The Arctic and Subarctic environment affects most stages of building design, construction, operation, and maintenance. UFC 3-130-01 and UFC 3-130-02 cover the important environmental considerations for the configuration and orientation of individual structures in Arctic and Subarctic locations. Reference UFC 3-130-03 for criteria and guidance on ground conditions, the presence of p
mixtures, solely or in combination. The ACI 306R Guide to Cold Weather Concreting provides recommendations for the use of these measures in varying cold weather conditions. Consider low temperature steels with high-notch toughness where UFC 3-130-04 16 January 2025 18 structural steel is exposed in arctic conditions. Design with proper joints to account for thermal expansion/contraction. 4-4 FOUNDATIONS. Comply with UFC 3-130-03. UFC 3-130-03 provides a complete discussion of foundations for freezing and thawing conditions. . UFC 3-130-04 16 January 2025 19 CHAPTER 5 MECHANICAL 5-1 GENERAL. Comply with UFC 1-200-01, UFC 3-401-01, and the government criteria referenced therein. Standardize components whenever possible to reduce the necessary inventory of repair materials. Employ redundant o
4 AFTTP 3-4.4, Contingency Airfield Operations, 2 November 2017 AFTTP 3-4.7, Contingency Response, 30 September 2017 MULTI-SERVICE PUBLICATIONS ETL 02-19, Airfield Pavement Evaluation Standards and Procedures, 12 November 2002 ETL 04-2, Standard Airfield Pavement Marking Schemes, with Change 2, 19 July 2004 ETL 09-6, c-130 and C-17 Landing Zone (LZ) Dimensional, Marking, and Lighting Criteria, 17 August 2009 ETL 94-01, Standard Airfield Pavement Marking Schemes, 4 May 1994 UFC 2-000-05N, Facility Planning Criteria for Navy/Marine Corps Shore Installations, Appendix E, Airfield Safety Clearances, January 1982 UFC 3-260-01, Airfield and Heliport Planning and Design, 17 November 2008 UFC 3-270-07, O&M: Airfield Damage Repair, 12 August 2002 UFC 3-535-01, Visual Air Navigation Facilities, 17 N
04 1.E-03 1.E-02 1.E-01 1.E+00 1.0E-05 1.0E-04 1.0E-03 1.0E-02 10 100 1000 Sine Tone, Peak g Vibration Schedule ASD, g2/Hz Frequency, Hz Vertical Transverse and Longitudinal Exaggeration Factor = 3.32 m = 5 Time Compression 20:1 (1 hour test is equivalent to 20 hour flight) Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:50Z Check the source to verify that this is the current version before use. MIL-STD-810H w/CHANGE 1 METHOD 514.8, ANNEX C 514.8C-25 Figure 514.8C-12. Category 8 - Propeller aircraft vibration exposure. 6-bladed C-130 Table 514.8C-XII. Category 8 - Propeller aircraft vibration exposure. 6-bladed C-130. Vertical Axis Broadband Random Vertical Axis Sinusoidal Components Longitudinal and Transverse Broadband Random Frequency, Hz ASD, g2/Hz Center Frequency, Hz (Bla
e (MEK) (I,T) U160 1338-23-4 2-Butanone, peroxide (R,T) U160 1338-23-4 Methyl ethyl ketone peroxide (R,T) U161 108-10-1 Methyl isobutyl ketone (I) U161 108-10-1 4-Methyl-2-pentanone (I) U161 108-10-1 Pentanol, 4-methyl- U162 80-62-6 Methyl methacrylate (I,T) U162 80-62-6 2-Propenoic acid, 2-methyl-, methyl ester (I,T) U163 70-25-7 Guanidine, -methyl-N'-nitro-N-nitroso- U163 70-25-7 MNNG U164 56-04-2 Methylthiouracil U164 56-04-2 4(1H)-Pyrimidinone, 2,3-dihydro-6-methyl-2-thioxo- U165 91-20-3 Naphthalene U166 130-15-4 1,4-Naphthalenedione U166 130-15-4 1,4-Naphthoquinone U167 134-32-7 1-Naphthalenamine U167 134-32-7 alpha-Naphthylamine U168 91-59-8 2-Naphthalenamine U168 91-59-8 beta-Naphthylamine U169 98-95-3 Benzene, nitro- U169 98-95-3 Nitrobenzene (I,T) U170 100-02-7 p-Nitrophenol U170
AMCN E0947 2-51 28,200 130 Logistics, TAMCN E0948 2-51 28,200 135 Mortar, TAMCN E0949 2-51 27,400 130 Recovery Unit, TAMCN E0950 2-51 23,400 135 Tow Anti-Tank, TAMCN E0942 2-51 27,650 130 Mobile Electronic Warfare Support System- Product Improvement Program (MEWSS-PIP) 2-51 29,480 130 M101A2 with Accompanying Load 3-2 3,000 100 Command Version 1 Trailer 3-2 1,958 100 Appendix C TM 4-48.11 (FM 4-20.199)/MCRP 4-11.3E, VOL III/NTTP 3-04.13/ C-8 AFMAN 11-223 (I), VOL III/COMDTINST M13482.4B 5 July 2013 Command Version 2 Trailer 3-2 1,981 100 Nomenclature Paragraph Number Max Weight (Pounds) Evaluated Air Speed (Knots) Len Cable Trailer 3-2 2,796 100 NC Support Trailer 3-2 2,643 100 Maintenance Trailer #2 3-2 1,430 100 Battalion Spares Trailer #1 3-2 1,594 100 Battalion Spares Trailer #2 3-2 2,
click on the Civil Reserve Air Fleet Capability link. Common Access Card and Air Force Portal access required. 4. Headquarters AMC/A3 retains runway criteria waiver authority for AMC organic aircraft. 5. See aircraft manuals for required tire pressure under specific conditions. Table 2. Aircraft Size. Aircraft Type Length (feet) Wing Span Width (feet)1 Maximum Weight (lbs) Landing Gear Type2 Width Required 180◦ Turn3 Required C-17 Parking Spots4 AMC Code FAA Code C-5M 247.8 222.7 840,000 TDT C5 150 1.9 C-130H/J 97.75 132.6 175,000 ST 2S 74 0.4 C-130J-30 112.75 132.6 175,000 ST 2S 78 0.5 C-17 173.92 169.75 585,000 TRT 2T 1435 1.04 KC-10A 181.6 165.3 593,000 SBTT 2D/D1 149.5 1.0 KC-46A 165.84 156.08 416,000 TT 2D 130 0.87 KC-135R/T 136.25 130.85 322,500 TT 2D 130 0.6 NOTES: 1. Wingtip cleara
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