B
HomeLibrariesCopilotSearchProjectsBookmarks
FeedbackHelp Desk
Libraries
Building Codes
Code LibraryIBC — BuildingIRC — ResidentialIFC — FireIPC — PlumbingIMC — MechanicalIFGC — Fuel GasIECC — EnergyNEC — ElectricalModel Codes
Specifications
CSI SpecificationsDOT SpecsTransit SpecsUSACE
Standards
TransportationRailroadFire SafetyAccessibilityStructural
Tools & References
DiagramsAssembliesProductsCalculatorsChecklistsPermits
PricingLog in
General Provisions (00100-00999)

836STRUCTURAL STEEL, FASTENERS AND MISCELLANEOUS METALS

AL · 2022 Standard SpecificationsBook pages 746762View official source ↗

836.01 General.

835.07 Use, Care, and Handling .

All reinforcement received on the project shall be placed in approved storage and shall be maintained clean, intact, and free from distortion. Reinforcement shall be free from loose or thick rust, which would impair bond of the steel with the concrete. R ust that produces only discoloration without reducing the cross section of the steel will not be considered objectionable. Only such reinforcement shall be distributed along the construction as needed for immediate use. STRUCTURAL STEEL, FASTENERS AND MISCELLANEOUS METALS

836.01 General.

a.Marking of Steels . Steels, when received from the mill shall be identified in accordance with ASTM A 6 {A 6M}. On steel piling the heat number and section size shall be legibly marked on each piece by stamp, paint, tag, sticker or other industry accepted method. Any piece that cannot be properly identified at time of use will be rejected until such time documentation or approved testing of the items in question can prove conformance to the requirements. Certified mill test reports or certified reports of tests made by other agencies which are recognized by the ALDOT, shall be furnished for each heat of steel verifying that the material meets the requirements of the type an d grade specified. The Department reserves the right to make its own test of any material, and the material may be rejected if these tests prove the material does not meet the requirements. For identification purposes, the fabricator shall utilize low stress stencils to dye stamp the mill heat numbers of the flanges and webs in the webs of welded members and in the webs of rolled members. The heat numbers shall be legible, located adjacent to piece marks, and placed centered between the top and bottom flang e in the first panel to the left end and near side of the member. All steel which is required to have a yield point greater than 36,000 psi {250 MPa} shall, at all times in the fabricator's plant, be color marked to identify its AASHTO, ASTM, or special sp ecification.
b.General Requirements .
1.Structural steel shall conform to the requirements of AASHTO M 270 Grade 36 {Grade 250} unless otherwise noted hereinafter in this Section or shown on the plans. AASHTO material specifications shall govern in lieu of ASTM material specifications where an AASHTO equivalent specification exists for all references within any referenced specification. With the approval of the Engineer, materials (other than web and flange material and web splice and flange splice m aterial) for members may be taken from stock, provided the fabricator provides all documentation which shows the material conforms to the required specifications, prior to use of such material. The term “main member”, as used hereinafter in this section or shown on the contract plans, is defined as any member requiring Charpy V -notch ( CVN) testing. Structural steel members requiring Charpy V -notch testing shall include, but not be limited to, the following: • All rolled beams in the superstructure and steel pier caps. • All flanges and webs of steel plate girders and steel pier caps. • All cover plates for beams and girders. • All flange and web splice plates for beams, girders, and floorbeams or stringer beams. • All connection plates welded to rolled beams, steel plate girders, and steel pier caps. • All diaphragms or cross frames for curved beams and girders, including their gusset and connection plates. • All stringer beams (floorbeams) and any connection plates welded thereto.

836.01 General.

• All floorbeam trusses (cross frames) w hich support stringer beams (floorbeams), including their gusset and connection plates. The material supplied shall meet the longitudinal Charpy V -notch test noted below. Sampling and testing shall be in accordance with AASHTO T 243 with the (H) frequency of heat testing used. All members requiring CVN testing shall have heat numbers legibly marked during fabrication. Steel Grade Thickness Test Requirements M 270 Grade 36 Up to 4" 15 ft. lb. @ 70°F. (Min. Ser. Temp. 0°F. and above) M 270 Grade 50 & Grade 50W Up to 4" Mech. Fastened Up to 2" Welded Over 2" to 4" Welded 15 ft. lb. @ 40°F. 15 ft. lb. @ 40°F. 20 ft. lb. @ 40°F. (Min. Ser. Temp. -1°F. to - 30°F.) {250} {Up to 102 mm} {20 J @ 21 °C} {Min. Ser. Temp. -18 °C and above} {345 & 345W} {Up to 102 mm Mech. Fastened} {Up to 51 mm Welded} {Over 51 mm to 102 mm Welded} {20 J @ 4 °C} {20 J @ 4 °C} {27 J @ 4 °C} {Min. Ser. Temp. -18 °C to - 34°C} If the yield point of the material exceeds 65 ksi {450 MPa}, the temperature of the CVN value for acceptability shall be reduced by 15 °F {8 °C} for each increment of 10 ksi {70 MPa} above 65 ksi {450 MPa}. When designated on the plans, the Contractor (Fabricator) shall furnish one main load carrying member (girder flange) 18 inches {460 mm} overlength per individual ALDOT bridge project, in order to provide an 18 inch {460 mm} sample for Departmental job control testing. Unless otherwise shown on the plans, steel plates for main members shall be cut a nd fabricated so that the primary direction of rolling is parallel to the direction of the main tensile and/or compressive stresses.

2.Fasteners, pins and rollers shall conform to the requirements of Articles 836.32, 836.33 and 836.42. Threads for all bol ts and pins for structural steel construction shall conform to the American National Standard for Unified Screw Threads, ANSI B1.1, Class 2A for external threads and Class 2B for internal threads, except that pin ends having a diameter of 1.375 inches {35 mm} or more shall be threaded six threads to the inch {25 mm}. All bolt heads and nuts shall be hexagonal shaped with dimensions conforming to the requirements for Hexagon Structural Bolts and Heavy Semi -Finished Hexagon Nuts of ANSI Standard B18.2.1 and B 18.2.2.
3.All cast and built -up bearings shall be shop assembled, checked for fit, securely packaged and shipped as a unit unless otherwise approved by the Engineer. The method of securing the bearing unit for shipment shall be as shown by the plan detail s or a method acceptable to the Engineer. The diameter of pins used in cast and built -up bearing shall be within 1/16 inch {1.6 mm} of the diameter specified by the plans with pin holes not in excess of the pin diameter by more than 1/16 inch {1.6 mm}.
4.Copper bearing structural steel, used for structural steel piling, shall conform to the requirements of Article 836.01, except that it shall contain not less than 0.20 percent of copper. Copper bearing steels for other structural uses shall be as specified .
5.High strength and alloy steel shall be in accordance with the following.
a.Special alloy steels to meet definite corrosion requirements shall be as specified on the plans.
b.High strength structural steel for bolted and welded construction shall con form to AASHTO M 270 of the Grade as shown on the contract plans (Grade 50 or Grade 50W). AASHTO M 270 Grade 50 {Grade 345} steel shall be limited to structural shapes in groups 1, 2 and 3 in ASTM A 6 {A 6M} and to plates and bars in thicknesses through 4 inches {102 mm}. Plates and bars over 3/4 inch {19 mm} through 4 inches {102 mm} in thickness shall be "killed -fine grain practice."
6.Corrosion -resistant iron chromium and iron chromium -nickel castings for general application shall conform to the requirements of ASTM A 296 of the grade specified on the plans.
7.Anchor bolt assemblies (anchor bolts, nuts, and washers) shall be in accordance with AASHTO M 314 (maximum tensile strength is waived). Galvanization of the anchor bolt from 3 inches {75

836.05 Gray Iron Castings.

mm} bel ow the top of the concrete to the top of the anchor bolt shall be required. The remaining length of the anchor bolt will not be required to be galvanized.

c.Full Size Testing of Members . When full size tests of structural members are required the methods and procedures shall be provided in the plans and specifications.

836.02 Steel Forging.

Carbon steel forgings shall, unless otherwise specified by plan details, conform to the requirements of AASHTO M 102 for Class C material. All forgings shall be annealed prior to being machined to form finished parts. A record of the annealing charges shall be furnished the Engineer by the manufacturer showing the forgings in each charge, the melt or melts from which they were secured, and the treatment they recei ved.

836.03 Blank.

836.04 Steel Castings.

Steel castings shall conform to the requirements of AASHTO M 103, Grade 70 -36, unless otherwise specified, and the following:

a.The dimensions of fillets shall not be less than the thickness of the thinnest adjoi ning section or member nor less than 1/2 inch {13 mm}.
b.All steel castings shall be annealed, unless otherwise provided, in accordance with AASHTO M 103 {M 103M}. Certification of annealing process shall be furnished by the manufacturer.
c.Steel casti ngs shall be true to pattern in form and dimension, free from pouring faults, sponginess, cracks, blow holes and other defects in positions affecting their strength and value for the service intended. No finished casting shall have visible blow holes so lo cated that a straight line laid in any direction will cut a total length of cavity greater than 1 inch {25 mm} in any 1 foot {300 mm}, nor shall any single blow hole exceed 1 inch {25 mm} in any dimension or have an area greater than 1/2 square inch {13 mm2}. Blow holes shall not have a depth injuriously affecting the strength of the casting. Minor defects which do not impair the strength may, if approved, be welded by the electric process. The defects shall be removed to solid metal by chipping, drilling o r other satisfactory methods and, after welding, the castings shall be annealed, if required. No cracks, flaws or other defects shall appear after such treatment. No sharp unfilleted angles or corners will be allowed. Castings that have been welded without the Engineer's permission shall be rejected.
d.All castings shall be blast cleaned of scale and sand so as to present a smooth, clean and uniform surface.
e.Castings shall be checked for soundness by comparing computed weight {mass} against actual weight {mass} (actual weight {mass} less than 95% of computed weight {mass} shall be cause for rejection of casting) and/or by suspending the casting and hammering it all over, comparing soundness of the ring.

836.05 Gray Iron Castings.

a.General . Gray iron castings shall be boldly filleted at angles and the arrises shall be sharp and perfect. They shall be true to pattern in form and dimensions. Castings will be classified under one of the following grades:
1.Grade "A". Grade "A" Castings shall conform to the requirements of Class No. 30 A for Gray Iron Castings, AASHTO M 105.
2.Grade "B". Grade "B" Castings shall conform to the requirements of Class No. 20 A for Gray Iron Castings, AASHTO M 105. All castings shall be of the Grade "A" classification unless otherwise noted.
b.Cleaning . All castings shall be blast cleaned of scale and sand so as to present a smooth, clean and uniform surface.

836.06 Malleable Iron Castings.

c.Weights {Masses }. Any casting weighing less than 95% of the weight {mass} computed from its dimensions shall be rejected.

836.06 Malleable Iron Castings.

Malleable iron castings shall conform to the requirements of ASTM A 47, Grade No. 35018. Castings shall be boldly filleted at angles and the arrises shall be sharp and perfect. The dimensions of fillets shall not be less than provided in Article 836.04. The surfaces shall have a workmanlike finish. Malleable castings shall be true to pattern in form and dimension, free from pouring faults, sponginess, cracks, blow holes and other defects in positions affecting thei r strength and value for the service intended. Cleaning shall be as provided in Subarticle 836.05(b). Soundness shall be checked as provided in Subarticle 836.04(e).

836.07 Ductile Iron Castings.

Ductile iron castings shall conform to the requirements of ASTM A 536, Grade 60 -40-18. Castings shall be boldly filleted at angles and the arrises shall be sharp and perfect. The dimensions of fillets shall not be less than provided in Article 836.04. The surfaces shall have a workmanlike finish. M alleable castings shall be true to pattern in form and dimension, free from pouring faults, sponginess, cracks, blow holes and other defects in positions affecting their strength and value for the service intended. Cleaning shall be as provided in Subartic le 836.04(d). Soundness shall be checked as provided in Subarticle 836.04(e).

836.08 Self -Lubricating Bronze Or PTFE Bearing Plates.

a.Self-Lubricating Bronze Bearing Plates . These bearing plates shall be an article of standard production by an establish ed manufacturer of such equipment. They shall be provided with trepanned or drilled recesses (not grooves) which shall be filled with a lubricating compound capable of withstanding the atmospheric elements and consisting of graphite and metallic substances with a lubricating binder. Such compound shall be pressed into the recesses by hydraulic presses so as to form dense non -plastic lubricating inserts. The lubricating area shall comprise not less than 25 percent of the total area. The manufacturer shall fu rnish additional lubrication and just prior to assembling, the entire sliding surfaces of members in contact with plates shall be thoroughly lubricated with the approved lubricant. The bearing plates shall be made of bronze conforming to the requirements f or Bronze Castings for Bridges and Turntables, AASHTO M 107, Alloy D, Copper Alloy 905, except that a maximum of 2 -1/2 percent lead will be permitted. This will modify minimum on copper to 84.5 percent, minimum on tin to 8.5 percent and maximum on zinc to 3.75 percent. The coefficient of friction shall not exceed one -tenth.
b.PTFE Bearing Plates . The structural steel portion of the bearing plate shall meet the requirements of AASHTO M 270 GRADE 36 {M 270M GRADE 250} unless shown otherwise on the plans. The material, fabrication and installation requirements for Polytetrafluoroethylene (PTFE) polymer shall be those given in SECTION 837. The coefficient of friction shall not exceed one -tenth.

836.09 Grounding Materials For Steel Bridges.

Standard stranded co pper grounding conductor shall be bare annealed Class B stranded electric conductor. Extra flexible grounding conductor shall be Class G bare annealed stranded electric conductor. Grounding rods shall be 5/8 inch x 8 feet {16 mm x 2.5 m}, minimum size, cop perclad steel grounding rods as manufactured by A.B. Chance, McGraw -Edison, Joslyn Manufacturing and Supply Company, or approved equal. Exothermic welding shall be by the Cadwell process or an approved equivalent method. All materials shall conform to the National Electrical Manufacturers' Association (NEMA) or the Underwriter's Laboratories, Inc. standards.

836.10 Lead Plates, Etc.

Lead used for plates, pipes, etc., shall conform to the requirements of ASTM B 29 for common desilverized lead.

836.16 Notice and Facilities For Inspection.

836.11 Hardwar e For Timber Bridges.

Machine bolts, nuts, washers, drift bolts, lag bolts and screws, dowels, nails, spikes, shear rings and plates and other miscellaneous hardware shall be common stock hardware items, either plain or galvanized. Galvanization when specified shall be in accordance with AASHTO M 232.

836.12 and 836.13 Blank.

836.14 Shop and Working Drawings.

The plans furnished the Contractor by the Department are not intended for use as shop or working drawings. Shop drawings and working drawings will be required as specified in Article 105.02. All applicable ALDOT specifications shall be referenced on the first shop drawing sheet by specification number and title. Shop drawings shall include camber and sweep diagrams covering steel portions of all stru ctures. Fabricators shall furnish verification certificates of the actual measurements of the camber placed in each beam, girder or truss.

836.15 Mill Orders and Shipping Statements.

The Contractor shall furnish the Engineer with as many copies of mill ord ers and shipping statements as may be directed. The weights {masses} of the individual members shall be shown.

836.16 Notice and Facilities For Inspection.

After the Bridge Engineer has received the fabricator notification required by 508.03(b) and as the fabrication begins, copies of the mill test reports and fabricators material information, for materials which require CVN testing, shall be supplied to the Bridge Engineer or his representative prior to completion and acceptance of fabrication. No mate rials or members will be accepted by the Bridge Engineer's representative on structural steel until the Department's form BBF -1 (available from the Bridge Engineer) and the supporting mill test reports for the materials have been furnished and approved by the Department. A complete package of this information shall be given to the ALDOT representative at the fabricator's plant, to be followed by a submittal to the ALDOT Materials & Tests' Certification office where official certification and approval is pro cessed. The BBF -1 form shall be signed by a company official and shall be notarized. The acceptance of members as fabricated may be noted by the affixing of the ALDOT S tamp on the member by the Bridge Engineer's representative. The Contractor /Fabricator shall provide ALDOT with adequate, suitable office facilities and equipment when required for the inspection of materials and workmanship in the fabrication plant . This office shall be conveniently located near the fabricating plant or work site, shall be private and not shared with the fabricator or any other agency, and shall be equipped so that it may be locked. It shall be climate controlled, water tight, and include necessary office furnishings such as a desk/table, chairs, and file cabinet. (Telephone i s optional). Inspectors shall be allowed free access to the necessary parts of the work. Refer to articles 105.09, 105.10, and 105.11 concerning the duties of the Inspector(s) and inspection of work. Unless otherwise provided, the Contractor shall furnish , without extra compensation, test specimens as provided herein. Fabrication shops shall have a master tape calibrated by the National Institute of Standards and Technology. All tapes used in fabrication measurements shall be calibrated with the master tape before being used on the project. Any master tape found damaged or with a certification over two years old shall be replaced or recalibrated. The quality control program for any fabrication work performed will be subject to the review of the Bridge Engin eer. A written current copy of the fabricator's Quality Control Manual and current copies of all nondestructive testing and Quality Control Inspection personnel certifications associated with fabrication work shall be on file with the Bridge Engineer prior to the beginning of work. Any bridge fabrication facility that is required to have an AISC Certification of Intermediate Bridge or Advanced Bridge shall have a Certified Welding Inspector (CWI) employed by, or retained by, and preferably working with the fabricator's quality control office. A CWI shall be present on all shifts and shall be available at any location that fabrication and welding are to take place. Quality Control guidelines and all welding code requirements shall conform to the AASHTO/AWS D1.5M/d1.5:2015, Bridge Welding Code, Seventh Edition. If the Bridge Engineer finds the fabricator's Quality Control Department is not providing sufficient inspection on the work in progress, he may suspend all or any portion of the work in progress (reference is made to Article 105.01 and Subarticle 108.07(a)).

836.17 Handling, Storage and Transporting Of Materials.

Work may resume only after necessary adjustments to the Quality Control Program are instituted which will assure conformance to the contract requirements. All nondestructive testing personnel shall m eet the requirements set forth in the "ASNT Standard for Qualification and Certification of Nondestructive Testing Personnel (ANSI/ASNT CP -105-2011)".

836.17 Handling, Storage and Transporting Of Materials.

The loading, unloading, handling and storing of m aterials shall be so conducted that the metal will not be injured or damaged. Structural material delivered at the bridge shop receiving yard shall be stored above the surface of the ground upon platforms, skids, or other supports and shall be protected fr om corrosion. It shall be kept free from accumulations of dirt, grease or foreign matter. During and after fabrication, proper lifting equipment with the capacity to handle members carefully at all times so that no member or part thereof will be bent, excessively stressed, deformed or otherwise damaged shall be used. Handling of members shall require the use of suitable clamps, plate hooks or other suitable devices. Chains or chokers will not be allowed without the use of a protective shield between the cha in and the member. Members longer than 50 feet {15 m} shall utilize a two or more point pickup method. Members shall be transported in such a manner that they will not be excessively stressed, deformed or otherwise damaged. Unless otherwise authorized for exceptionally deep girders, girders and beams shall be stored and transported in a "workway position" as used in the structure with appropriate shoring and blocking methods suitable to the Engineer. Chain tie downs shall be provided with protection shields . Multiple stacking of beams and girders may only be done in a manner acceptable to the Engineer. Any suspected damage from handling, storage or hauling shall be cause for the Engineer to order verification of design camber and/or repair of the beam or girder. All structural materials shall be examined by shop personnel and/or quality control, at the earliest possible time for evidence of any defects. If pitting or other defects are plainly visible during early stages of fabrication prior to any required su rface preparation (sand or shot blasting), evaluation shall be required. Information regarding actual material thickness, amount of area affected and end use of material being evaluated will be submitted to the Engineer for acceptability. Any required conditioning will be allowed only when in compliance with ASTM A 6 {A 6M}. The above shall also apply to pitting of fabricated material stored prior to shipment and to material delivered to the bridge site. Attention is called to Subarticle 106.05(b). Preparat ion and shipment of fabricated pieces shall conform to the following: Loose Members.

1.Parts not completely assembled in the shop shall be secured, insofar as practicable, to prevent damage in shipping or handling.
2.Projecting parts likely to be damaged during shipment shall be blocked with wood or otherwise protected. Packages.
1.Pins, small parts and small packages of bolts, rivets, washers, and nuts shall be shipped in boxes, crates, kegs, or barrels. A list and description of the contained material shall be plainly marked on the outside of each shipped container.
2.Anchor bolts, washers, and other anchorage or grillage materials, shall be shipped in time to suit the requirements of the masonry construction. Loading diagrams shall be provided to the Bridge Engineer for his review when Structural Steel items are to be shipped by barge or railcar.

836.18 Straightening Material.

Rolled material, before it is marked, laid out, or otherwise worked in the shop must be straight or cambered as shown on the p lans. Material with sharp kinks or bends may be rejected. If straightening is necessary it shall be done by methods that will not injure the metal and must be approved by the Engineer. Heat straightening will be permitted provided the metal is not heated a bove 1100°F {590 °C}. (controlled by the use of heat crayons furnished by the Fabricator or other approved means). After heating, the metal shall not be artificially cooled until after naturally cooling to 600 °F {315 °C} or less. The method of artificial cooling is subject to the approval of the Engineer. Water or water spray misting shall not be used as a means of artificial cooling. After straightening, the surface of the metal shall be carefully inspected for evidence of fracture.

836.19 Workmanship and Finish.

836.19 Workmanship and Finish.

a.General . Workmanship and finish shall be first class in every respect. Materials at the shop shall be kept clean and protected from the weather insofar as practical. Shearing, burning, chipping and grinding shall be neatly and accurately done in a workmanlike manner. Damage incurred to members or the surfaces of members for any reason shall be cause for the Engineer to order the damage repaired or to reject the member in accordance with the following:
1.Except as noted in parag raph 2 below, damage to surfaces of plates that does not reduce the plate thickness below the permissible minimum thickness allowed by ASTM A 6 {A 6 M} or the thickness of structural shapes in excess of 1/32 inch {0.8 mm} for material less than 3/8 inch {9 .5 mm} in thickness, 1/16 inch {3.2 mm} for materials 3/8 inch to 2 inches {9.5 mm to 50 mm} inclusive in thickness or 1/8 {3.2 mm} in for material over 2 inches {50 mm} thick are considered repairable. Damage in excess of the limits noted will be evaluate d by the Engineer as to whether to reject or allow repair of member.
2.Surface indentation of members caused by lifting devices shall be evaluated by the Bridge Engineer ’s representative to determine if the damage is repairable and if repairable, the repa irs necessary for acceptance. Continued use of lifting devices that cause damage, especially that which reduces the specified thickness by more than 1/16 inch {1.6 mm}, will be cause for the rejection of all such members so damaged.
3.In general, when allowed, repair work will consist of welding and/or grinding of the surfaces; however, when evaluation of base metal defects becomes necessary, such evaluation shall be done in the presence of the Bridge Engineer’s representative. The type of evaluation shall be determined by the fabricators quality control personnel subject to the approval of the Bridge Engineer's Representative. After evaluation of such defects and where welding is necessary on rolled surfaces, stringer beads shall be placed parallel to the direction of stress. All welding shall be performed by competent welders using low hydrogen welding electrodes and/or welding consumables listed in an ALDOT approved welding procedure (WPS). The Engineer shall be the sole judge as to the accepta bility of t he repair work; any unacceptable work shall be cause for rejection of a member.
4.A form of buffer and/or shield shall be utilized during fitting operations to protect base materials from damage caused by fitting tools or devices. If evidence of base met al damage appears due to misuse of such devices, the material may be deemed unacceptable.
b.Details .
1.Bends and crimps shall conform to wood or metal templates. All bending or crimping shall be done to the bend lines shown on the plans by a mechanicall y operated press without avoidable or unnecessary decrease in section.
2.All material shall be bent cold when practical. Cold bending of rolled steel plates shall conform to the following:
a.They shall be so taken from the stock plates that the bending l ine will be at right angles to the direction of rolling.
b.The radii of bends, measured to the concave face of the metal, shall not be less, and preferably shall be greater, than shown in the following table. Plate Thickness "t" Bend Radii For All Grades of Steel t ≤ 1/2 in {t ≤ 12 mm} 2t 1/2 in. < t ≤ 1 in. {12 mm < t ≤ 25 mm} 2.5t 1 in. < t ≤ 1.5 in. {25 mm < t ≤ 38 mm} 3t 1.5 in. < t ≤ 2.5 in. {38 mm < t ≤ 60 mm} 3.5t 2.5 in. < t ≤ 4 in. {60 mm < t ≤ 100 mm} 4t If a shorter radius is essential, the plates shall be bent hot. Hot -bent plates shall conform to requirement Item 1 above.
c.Before bending, the corners of the plate shall be rounded to a radius of 1/16 inch {1.6 mm} throughout that portion of the plate at whi ch the bending is to occur.

836.19 Workmanship and Finish.

3.When hot bending is necessary, the metal shall be carefully heated to a temperature not to exceed 1100 °F {590 °C}. as evidenced by heat crayons or other approved means. Material that has been heated shall be slowly cooled af ter the bending has been completed.
4.Material that is overheated, fractured, or otherwise injured or damaged shall be rejected.
c.Camber or Curving of Beams and Girders . Camber in rolled beams shall be accomplished by the heat up- set method utilizing t he lowest possible temperature not to exceed 1100 °F {590 °C}, as evidenced by infrared thermometers or heat crayons. The application of heat shall be carefully supervised using a method acceptable to the Engineer. Camber for built -up girders shall be accomplished by cutting the web to the prescribed camber with suitable allowance for shrinkage due to cutting and welding. However, moderate variation from the prescribed camber tolerance may be corrected by a carefully supervised application of heat not t o exceed 1100 °F {590 °C} as evidenced by infrared thermometers or heat crayons. Horizontal curving of rolled beams shall be accomplished by the heat up- set method which will require a written procedure approved by the Engineer. Said procedure shall utiliz e the lowest temperature possible but not in excess of 1100 °F {590 °C} as evidenced by infrared thermometers or heat crayons . Horizontal curving of built -up girders shall be accomplished by cutting flange plates to the radii shown by the plan details from wider plates, unless the heat up -set method is allowed by the plans or proposal. When the heat up- set method is allowed, such will require a written procedure approved by the Engineer. Said procedure shall utilize minimum temperatures not to exceed 1100°F {590 °C} as evidenced by infrared thermometers or heat crayons . After heating of metals as noted, the metal shall not be artificially cooled until after naturally cooling to 600°F {315 °C}. or less. The method of artificial cooling must be acceptable to t he Engineer. Water or water spray misting shall not be used as a means of artificial cooling. Any material that is heated above the temperature limit noted will be rejected until tests and investigations reveal the material is suitable for use. The Fabrica tor shall be solely responsible for providing any test data or other information deemed necessary by the Engineer to evaluate the acceptability of the material at no cost to the Department. The fabricator's Quality Control Inspector shall furnish verificat ion certificates of the actual measurements of the camber, overall length and horizontal sweep placed in each beam or girder. Actual measurements shall be verified and recorded by the Fabricator's Quality Control Inspector.
d.Straightness, Camber, and Sw eep in Welded Beams , Girders , and Ancillary Products .
1.Straightness of Welded Beams and Girders (No Required Camber or Sweep). If requirements for camber and sweep are not given in the contract, welded beams and girders shall be straight within a plus and minus tolerance for straightness. The straightness tolerance shall be +/ - 1/8 inches per foot times the number of feet from the nearest end of the beam or girder divided by 10 {+/ - 3 mm times the number of millimeters from the nearest end of the beam or girder divided by 3000}.
2.Tolerance for the Camber of Welded Beams , Girders , and Bridge Deck Joint Armor Plates . The camber of welded beams , girders , and armor plates shall be within a plus and minus tolerance measured in inches. The tolerance shall be + 1/8 inches and - 0 inches per foot times the number of feet from the nearest end of the beam , girder, or armor plate divided by 10 {+ 3 mm and - 0 mm times the number of millimeters from the nearest end of the beam, girder, or armor plate divided by 300 0}.
3.Tolerance for the Sweep of Welded Beams and Girders . The sweep of horizontally welded beams and girders shall be within a plus and minus tolerance measured in inches. The tolerance shall be +/ - 1/8 inches per foot times the number of feet from the nearest end of the beam or girder divided by 10 {+/ - 3 mm times the number of millimeters from the nearest end of the beam or girder divided by 3000}. The horizontal alignment of the sweep of the top and bottom flanges at any point along welded beam or girder shall be within 3/8 inch {10 mm).
e.Surface Profile at the Centerline of Structural Steel Finger Joints . The profile of the surface of a structural steel finger joint, measured along the centerline of the finger plate sections of the finger join t (transverse to the centerline of the roadway) shall be within a plus and minus tolerance. The tolerance shall be + 1/16 inch and - 0 inches per foot times the number

836.22 Fastener Holes.

of feet from the nearest end of the joint divided by 10 {+ 2 mm and - 0 mm times the number of millimeters from the nearest end of the joint divided by 3000}. When all fabrication is completed the flat surfaces of each finger plate section shall be straight edged for flatness and any area found exceeding 1/8 inch in 10 feet {3 mm in 3 m} shall be marked and corrected by approved methods. A 10 foot {3 m} straight -edge shall be used and lapped at least 5 feet {1.5 m} over the prior 10 foot {3 m} check.

836.20 Thermal Cutting.

Steel may be thermal cut, provided a smooth surface is secured by the use of a mechanical guide. Thermal cutting by hand shall be done only when approved, and the surface shall be made smooth by planing, chipping or grinding. Re -entrant cuts shall be filleted to a radius of not less than 3/4 inch {19 mm}. Defects in cut edges shall not be repaired by welding except with approval of the Engineer for occasional notches or gouges less than 7/16 inch {11 mm} deep for material up to 4 inches {100 mm} thick and less than 5/8 inch {16 mm} for material over 4 inches {100 mm} thick. S uch weld repairs shall be made by suitably preparing the defect, welding with low hydrogen electrodes not exceeding 5/32 inch {4 mm} in diameter, observing the applicable requirements of Departmental welding requirements and grinding the completed weld smo oth and flush with the adjacent surface to produce a workmanlike finish. Other methods of cutting steel may be acceptable provided the method will produce cut surfaces within the required tolerances for thermal cut surfaces.

836.21 Substitutions.

Substitut ions of sections having different dimensions than those shown on the plans shall be made only when approved in writing.

836.22 Fastener Holes.

a.General .
1.Required Size of Fastener Holes . In any one connection, all holes may be oversized or slotted by no more than 1/32 inch {0.8 mm}. In any one connection, a maximum of 10 % of the holes may be oversized or slotted by no more than 1/16 inch {1.6 mm} larger than the nominal diameter of the fastener.
2.Fastener Holes in Main Members . Holes for connections in structural steel "main members" ("main members" as defined in Article 836.01) shall be made in accordance with one or more of the following procedures: • Subdrilling and then reaming or drilling all members to full size holes with the members assembled; • Drilling full size holes in the assembled members by using a steel template with hardened steel bushings with the holes accurately dimensioned from the centerlines of the connection; • Drilled using Computer Numerically Controlled (CNC) machinery. Web and flange splice plates shall be match marked to the splice locations regardless of the method used for drilling the holes.
3.Fastener Holes in Members that are not Main Members . Holes in members other than "main members" ("main members" as defined in Article 836.01) may be punched with a full size die if the thickness of the member is not greater than: • The nominal diameter of the fastener and; • Not greater than 3/4 inch {20 mm} for carbon steel and; • Not greater than 5/8 inch {16 mm} for high strength steel and; • Not greater than 1/2 inch {13 mm} for quenched and tempered alloy stee l. The diameter of the die shall not exceed the diameter of the punch by more than 1/16 inch {1.6 mm}. Punched holes shall be clean cut and without torn or ragged edges.
4.Control of Drilling and Punching and Quality of Fastener Holes . Web and flange splice plates shall be match marked to the splice locations regardless of the method used for creating the fastener holes. Members drilled while assembled shall be securely held in the correct position while being drilled. Burrs on the metal surfaces shall be removed. Plug welding of any mis -located or mis -sized holes is not allowed.

836.22 Fastener Holes.

b.Accuracy of Punched Holes .
1.If the Engineer finds that the punched work does not comply with requirements hereinafter provided, it may be required that any or all holes be (1) subpunched (or subdrilled) and either reamed or drilled to full size or (2) drilled full size from the solid. All subpunched holes shall be 3/16 inch {4.8 mm} smaller than the nominal diameter of the fastener.
2.The punched holes shall be so accurately punched that after assembling (before any reaming is done) a cylindrical pin 1/8 inch {3 mm} smaller in diameter than the nominal size of the punched hole may be entered perp endicular to the face of the member, without drifting, in at least 75 percent of the contiguous holes in the same surface or in like proportion for any group of holes. If this requirement is not fulfilled, the badly punched pieces will be rejected. If any hole will not pass a pin 3/16 inch {4.8 mm} smaller in diameter than the nominal size of the punched hole, this will be cause for rejection.
c.Shop Assembly . Bolted trusses, arches, continuous beam spans and plate girders shall be assembled in the shop either in an upright position or on their side. After the members have been adjusted to line and fit with proper camber and rigidly fastened (i.e., drift pinned) together, the holes for field connections shall be reamed or drilled. Filler plates for bolted beam and girder splices have been based on theoretical dimensions. The thickness of the plates shall be adjusted in the shop to take care of any difference greater than 1/16 inch {1.6 mm} between the theoretical and actual dimensions. Splices in memb ers of the same theoretical size will require filler plates if the actual dimensions vary more than 1/16 inch {1.6 mm}. After assembling, sub -punched or sub -drilled holes shall be reamed to a diameter 1/16 inch {1.6 mm} larger than the nominal diameter of the fastener. Reaming shall be done after all the pieces to be connected are assembled and firmly fastened together. Reaming of fastener holes shall be done with twist drills or with short taper reamers. Where practicable, reamers shall be directed by mech anical means. Burrs resulting from reaming or drilling shall be removed.
d.Accuracy of Reamed or Drilled Holes . Reamed or drilled holes shall be cylindrical and perpendicular to the member and their accuracy shall be the same as provided for punched holes (Subarticle 836.22(b)) except that, after reaming or drilling, 85 percent of the contiguous holes in the same surface, or in like proportion for any group of holes, shall not show an offset greater than 1/32 inch {0.8 mm} between adjacent thickness of me tal. There shall be no drifting in the shop or field to enlarge mismatched holes. If any holes must be enlarged to admit the fastener, they shall be reamed.
e.Edge Distance of Fasteners .
1.The minimum distance from the center of any fastener to a sheare d or flame cut edge shall be: 1" Fastener: 1 -3/4" {45 mm}; 7/8" Fastener: 1 -1/2" {38 mm}; 3/4" Fastener: 1 -1/4" {32 mm}; 5/8" Fastener: 1 -1/8" {29 mm}. The minimum distance from the center of any fastener to a rolled or planed edge, except in flanges of beams and channels, shall be: 1" Fastener: 1 -1/2" {38 mm}; 7/8" Fastener: 1 -1/4" {32 mm}; 3/4" Fastener: 1 -1/8" {29 mm}; 5/8" Fastener: 1" {25 mm}. In the flanges of beams and channels the minimum distance from the center of the fastener to a edge shall be: 1" Fastener: 1 -1/4" {32 mm}; 7/8" Fastener: 1 -1/8" {29 mm}; 3/4" Fastener: 1" {25 mm}; 5/8" Fastener: 7/8" {22 mm}.
2.When enlarged or slotted holes are used the distance between edges of adjacent holes shall not be less than thr ee times the diameter of the fastener minus the nominal diameter of the hole. The distance to an edge shall not be less than the amount shown in Item 836.22(e)1. minus 1/2 the nominal diameter of the hole.

836.32 Bolts, and Bolted Connections.

836.23 Through 836.26 Blank.

836.27 Shop Assemblin g.

a.General . All surfaces of metal that will be in contact when assembled shall be cleaned before assembly but shall not be painted unless otherwise specified by plan details. No temporary welds for fitting aids or for other purposes will be allowed unless shown on the approved drawings. All welding (including stiffeners) shall be completed on beams or girders before they are put into laydown and/or assembled.
b.Assembling .
1.Before the reaming or drilling of any holes in a splice for conti nuous beam spans, continuous plate girder spans and stringer beams, is done, a "laydown", consisting of at least three contiguous shop sections or all members in at least three contiguous panels but not less than the number of panels associated with three contiguous chord lengths (lengths between field splices) and not less than 150 feet {46 m} in the case of structures longer than 150 feet {46 m}, shall be required. All individual members (girders and beams) which require horizontal curvature shall be proc essed in the laydown with the required curvature. Shop assembly may proceed so long as one section of the minimum size "lay down" has been satisfactorily assembled in a preceding "lay down." All trusses shall be assembled in the shop. All expansion dams (f inger joints) shall be assembled in the shop. Expansion dams shall be shipped assembled, including troughs, unless otherwise shown on the plans. For structures having curved girders, girders with integral steel caps, extreme skews in combination with seve re grade or camber, or other complex characteristics, the plans may direct that the entire structure, including the floor system, be assembled in the shop. The assembly, including camber, alignment, accuracy and fit of joints, shall be approved by the fabr icator's Quality Control Inspector before reaming or drilling is commenced.
2.The parts of a member shall be assembled, properly aligned with drift pins, and firmly drawn together with bolts before reaming or shop fastening is commenced. Assembled pieces shall be taken apart for the removal of burrs and shavings produced by reaming or drilling operation. The member shall be free from twists, bends and other deformations.
3.Preparatory to the shop fastening of full -sized punched material, the fastener holes, if necessary, shall be spear -reamed for the admission of the fastener. The reamed or drilled holes shall not be more than 1/16 inch {1.6 mm} larger than the nominal diameter of the fastener.
4.Abutting joints in compression members, where so specified on the drawings, shall be faced and brought to an even bearing. No milling shall be done until members are completely shop assembled, unless otherwise provided on the plans. Where joints are not faced (field splices in continuous steel girder lines), the o pening shall not exceed 3/8 inch {9.5 mm}.
5.Field splice plates and filler plates shall be bolted to girders and/or beams, at the locations shown on the approved shop drawings, in the fabrication shop after cleaning (blasting) and coating (painting) of b oth pieces to be joined.

836.28 Blank.

836.29 Match -Marking.

Connecting parts assembled in the shop for the purpose of reaming or drilling holes in field connections shall be match -marked with low stress stencils using figures and letters at least 3/8 inch {10 mm} high, and a diagram showing such marks shall be shown on approved shop drawings. Reamed parts shall not be interchanged.

836.30 Rivets.

In removing rivets, care shall be taken not to injure the adjacent metal, and, if necessary, they shall be dri lled out.

836.31 Blank.

836.32 Bolts, and Bolted Connections.

a.General .
1.This Article does not pertain to the use of high strength bolts.

836.33 High Strength Fasteners.

2.Unfinished and turned bolts and nuts shall conform to the requirements for Grade "A" bolts of ASTM A 307 unless otherwise specified.
3.The holes shall be truly cylindrical. Holes shall be at right angles to the surface of the metal so that both head and nut will bear squarely -against the metal.
4.The heads and nuts shall be drawn tight against the work with a suitable wrench. Where bolts are to be used in beveled surfaces, beveled washers shall be provided to give full bearing to the head or nut. All bolts shall have cut threads neatly and accurately finished.
5.Permanent unfinished or turned bolts shall ha ve single self -locking nuts or double nuts, unless otherwise shown on the plans.
b.Unfinished Bolts . Bolts transmitting shear shall be threaded to such a length that not more than one thread will be within the grip of the metal. The bolts shall be of such length that they will extend entirely through their nuts, but not more than 1/4 inch {6 mm} beyond them.
c.Turned Bolts .
1.Holes for turned bolts shall be carefully reamed and the bolts turned to a light driving fit with the threads entirely outside of the holes and under the washer, and a washer shall be used. The heads and nuts shall be hexagonal.
2.The surface of the body of turned bolts shall meet the ANSI roughness rating value of 125 {3.2 µm}
3.Bolts shall be driven accurately into the holes without damaging the thread. A snap shall be used to prevent damaging the threads.

836.33 High Strength Fasteners.

The components of high strength bolt assemblies shall meet the requirements of the following: ASTM A 325 {A 325M} - Bolts ASTM A 563 {A 563M} - Nuts ASTM F 436 {F 436M} - Washers ASTM F 959 - Direct Tension Indicators Unless otherwise noted by plan details, or approved by the Engineer, Type 1 bolts shall be used for standard construction and Type 3 bolts shall be used with weathering steel. Galvanization, where required shall be in accordance with the provisions of ASTM B 695 Class 50. When an Inorganic Zinc Paint Primer is specified on the contract plans, all bolts shall be galvanized. The producer, supplier a nd distributor shall submit the documentation required to certify that the bolt assembly components are in compliance with these specifications. These requirements shall be modified or supplemented as follows:

a.Quality Assurance . Acceptance of bolts, n uts, washers and direct tension indicator washers shall be based on the "Production Lot Method" of identification and quality assurance. A production lot is a group of bolts, nuts, washers or load indicator washers that are the same nominal size, are produ ced from the same heat of steel and are processed together through all operations to the shipping container. The manufacturer shall identify and maintain the integrity of each production lot from raw -material selection through all processing operations and treatments to final packing and shipment.
b.Manufacturing .
1.Bolts . Bolts shall meet the hardness requirements given in ASTM A 325 {A 325M}.
2.Nuts . Nuts to be galvanized shall be heat treated grade DH. Plain (ungalvanized) nuts shall be grades C, D or C3 with a minimum Rockwell hardness of 89 HRB (or Brinell hardness 180 HB), or heat treated grades DH or DH3. (The hardness requirements for grades C, D and C3 exceed the current AASHTO/ASTM requirements). Nuts that are to be galvanized shall be tapped oversize the minimum amount required for proper assembly. The amount of overtap in the nut shall be such that the nut will turn freely on the bolt in the coated condition. Galvanized nuts shall meet the mechanical requirements of ASTM A 563 {A 563M} and the rotational -capacity test herein (the overtapping requirements of ASTM A 563 {A 563M} paragraph 7.4 shall be considered maximum values instead of minimum, as currently shown).

836.33 High Strength Fasteners.

3.Marking . All bolts, nuts and washers shall be marked in accordance with the appropriate AASHTO/ASTM Specifications.
c.Testing .
1.Bolts . Proof load tests (ASTM F 606 Method 1) are required. Minimum frequency of tests shall be as specified in ASTM A 325 {A 325M} paragraph 9.5. Wedge tests on full size bolts (ASTM F 606 paragr aph 3.5) are required. If bolts are to be galvanized, tests shall be performed after galvanizing. Minimum frequency of tests shall be as specified in ASTM A 325 {A 325M} paragraph 9.5. If galvanized bolts are supplied, the thickness of the zinc coating sha ll be measured. Measurements shall be taken on the wrench flats or top of bolt head.
2.Nuts . Proof load tests (ASTM F 606 paragraph 4.2) are required. Minimum frequency of tests shall be as specified in ASTM A 563 {A 563M} paragraph 9.3. If nuts are to be galvanized, tests shall be performed after galvanizing, overtapping and lubricating. If galvanized nuts are supplied, the thickness of the zinc coating shall be measured. Measurements shall be taken on the wrench flats.
3.Washers . If galvanized washers are supplied, hardness testing shall be performed after galvanizing. (Coating shall be removed prior to taking hardness measurements). The thickness of the zinc coating shall be measured.
4.Assemblies . Rotational -capacity tests are required and shall be pe rformed on all plain and galvanized (after galvanizing) bolt, nut and washer assemblies by the manufacturer or distributor prior to shipping. Washers are required as part of the test. The following shall apply:
a.Except as modified herein, the rotational -capacity test shall be performed in accordance with the requirements of ASTM A 325 {A 325M}.
b.Each combination of bolt production lot, nut lot and washer lot shall be tested as an assembly. Where washers are not required by the installation procedures, t hey need not be included in the lot identification. A production lot change of either the bolt, nut, or washer shall require the testing of additional assemblies.
c.A rotational -capacity lot number shall be assigned to each combination of lots tested.
d.The minimum frequency of testing shall be two assemblies per rotational -capacity lot.
e.The bolt, nut and washer assembly shall be assembled in a Skidmore -Wilhelm Calibrator or an acceptable equivalent device (note - this requirement supersedes the curren t ASTM A 325 {A 325M} requirement that the test be performed in a steel joint). For short bolts which are too short to be assembled in the Skidmore- Wilhelm Calibrator, See Subitem 836.33(c)4.i.
f.The minimum rotation, from a snug tight condition (10% of t he specified proof load), shall be: 240° (2/3 turn) for bolt lengths < 4 diameters 360° (1 turn) for bolt lengths > 4 diameters and < 8 diameters 480° (1 1/3 turn) for bolt lengths > 8 diameters
g.The tension reached at the above rotation shall be equal to or greater than 1.15 times the required installation tension. The installation tension and the tension for the turn test are shown below: Diameter (In.) 1/2 5/8 3/4 7/8 1 1 1/8 1 1/4 1 3/8 1 1/2 Req. Installation Tension (kips) 12 19 28 39 51 56 71 85 103 Turn Test Tension (kips) 14 22 32 45 59 64 82 98 118 Diameter {mm} 16 20 22 24 27 30 36 Req. Installation Tension {kN} 94.2 147 182 212 275 337 490 Turn Test Tension {kN} 108.3 169.1 209.3 243.8 316.3 387.6 563.5
h.After the required installation tension listed above has been exceeded, one reading of tension and torque shall be taken and recorded. The torque value shall conform to the following:

836.34 Sheared Edges.

Torque < 0.25 PD Where: Torque = measured torque (foot -pounds); P = measured bolt tension (pounds) and D = bolt diameter (feet).

i.Bolts that are too short to test in a Skidmore -Wilhelm Calibrator may be tested in a steel joint. The tension requirement of Subitem 836.33(c)4.g. need not apply. The maximum torque requirement of Subitem 836.33(c)4.h. shall be computed using a value of P equal to the turn test tension shown in the table in Subitem 836.33(c)4.g.
5.Reporting . The results of all tests (including zinc coating thickness) required herein and in the appropria te AASHTO specifications shall be recorded. The location where tests are performed and the date of tests shall be recorded.
d.Documentation .
1.Mill Test Report(s ) (MTR). An MTR shall be furnished for all mill steel used in the manufacture of the bolts, nuts, and washers. The place where the material was melted and manufactured shall be shown on the MTR.
2.Manufacturer Certified Test Report (s) (MCTR). The manufacturer of the bolts, nuts and washers shall furnish test reports (MCTR) for the item furnished. Each MCTR shall show the relevant information required in accordance with Item 836.33(c)5. The manufacturer performing the rotational -capacity test shall include on the MCTR:
a.The lot number of each of the items tested.
b.The rotational -capacit y lot number as required in Subitem 836.33(c)4.c.
c.The results of the tests required in Item 836.33(c)4.
d.The pertinent information required in Item 836.33(c)5.
e.A statement that MCTR for the items are in conformance to this specification and the appropriate AASHTO specifications.
f.The location where the bolt assembly components were manufactured.
3.Distributor Certified Test Report(s ) (DCTR). The DCTR shall include MCTR above for the various bolt assembly components. The rotational -capacity test may be performed by a distributor (in lieu of a manufacturer) and reported on the DCTR. The results of the tests required in Item 836.33(c)4. shall be shown on the DCTR. The pertinent information required in Item 836.33(c)5. shall be shown on the DCTR. The rotational -capacity lot number as required in Subitem 836.33(c)4.c. shall be shown on the DCTR. The DCTR shall contain a statement that the MCTR are in conformance to this specification and the appropriate AASHTO specifications.
e.Shipping . Bolts, nuts and washers from each rotational -capacity lot shall be shipped in the same container. If there is only one production lot number for each size of nut and washer, the nuts and washers may be shipped in separate containers. Each container shall be permanentl y marked with the rotational - capacity lot number such that identification will be possible at any stage prior to installation.

836.34 Sheared Edges.

Sheared edges of plates more than 5/8 inch {16 mm} in thickness shall be planed to a depth of 1/4 inch {6 mm}. Plates 5/8 inch {16 mm} and less in thickness shall be ground to remove sharp corners and burrs. Re-entrants corners shall be filleted to a minimum radius of 3/4 inch {19 mm} before cutting.

836.35 Facing Of Bearing Surfaces.

The top and bottom surfaces of steel slabs and base plates and cap plates of columns and pedestals shall be planed, or else the plates or slabs hot -straightened. Parts of members in contact with them shall be faced and shall have full contact when assembled.

836.42 Pins and Rollers.

For fit -up of sole plates or bearing seats of beams or girders see Article 836.46. Sole plate and masonry plate corrections may be made by planing or hot -straightening. In planing the surface of expansion bearings, the cut of the tool shall be in the direction of expansion. Cast pedestals shall be planed on surfaces to be in contact with steel, and the surface to be in contact with masonry rough finished. The surface finish of bearing and base plates and other bearing surfaces that are to come in contact with each o ther or with concrete shall meet the ANSI surface roughness requirements as defined in ANSI B46.1, Surface Roughness, Waviness and Lay, Part I unless otherwise specified, Steel slab in contact with Masonry ANSI 2000 {50 µm} Steel slabs ANSI 2000 {50 µm} Heavy plates in contact in shoes to be welded ANSI 1000 {25 µm} Milled ends of compression members, milled or ground ends of stiffeners and fillers ANSI 500 {12.5 µm} Bridge rollers and rockers ANSI 250 {6.3 µm} Pins and pin holes ANSI 125 {3.2 µm} Sliding bearings ANSI 125 {3.2 µm} Surfaces of bronze bearing plates intended for sliding contact shall be carefully milled and polish finished.

836.36 Blank.

836.37 Blank.

836.38 Finished Members.

These shall be true to line and free from twists, bends, and other defects.

836.39 Blank.

836.40 Blank.

836.41 Stress Relieving.

Members such as bridge shoes or pedestals which are built -up by welding sections of plates together shall be stress relieved in accordance with the requirement s given in ANSI/AASHTO/AWS D1.5/D1.5M - 2008 for stress relieving unless an alternate method has the written approval of the Bridge Engineer.

836.42 Pins and Rollers.

a.General . Pins and rollers shall be accurately turned to the dimensions shown on the drawings and shall be straight, smooth, and free from flaws. Pins and rollers more than 9 inches {228 mm}in diameter shall be forged and annealed, pins and rollers 9 inches {228 mm}or less in diameter may be either forged and annealed or cold finished carbon steel shafting. Pins and roller material shall conform to one of the following unless a specific Grade or Class is specified by plan details: 4" { 100 mm} in Diameter or less........AASHTO M 169*, Grade 1016 to 1030, Inclusive 0" to 20" { 0 mm to 508 mm } in diameter.........AASHTO M 102, Class C, Class D or Class G** 0" to 10" { 0 mm to 254 mm} in diameter.........AASHTO M 102, Class F * This material shall provide the following minimum values: Yield - 36,000 psi {250 MPa} Stress in extreme Fiber - 29,000 psi {200 MPa} Shear - 14,000 psi {97 {MPa} Bearing on Pins not subject to rotation 29,000 psi {200 MPa} Bearing on Pins subject to rotation 14,000 psi {97 MPa} ** Rolled material with the same properties may be substituted for this class. In pins larg er than 9 inches {228 mm} in diameter, a hole not less than 2 inches {50 mm} in diameter shall be bored full length along the axis after the forging has been allowed to cool to a temperature below the critical range under suitable conditions to prevent inj ury by too rapid cooling, and before being annealed. Two pilot nuts and two driving nuts shall be furnished for each size pin, unless otherwise provided by plans or directed.

836.43 through 836.45 Blank.

The diameter of pins and rollers shall not exceed 1/16 inch {1.6 mm} plus or minu s from the diameter specified by the plans or ordered by the Engineer.

b.Boring Pin Holes . Pin holes shall be bored true to gage, smooth and straight, at right angles with the axis of the member and parallel with each other unless otherwise shown on the plans. Pins shall be parallel to each other unless otherwise shown on the plans. The final surface shall be obtained by a finishing cut. Boring of holes in built up members shall be done during the final lay down operation.
c.Pin Clearance . The diameter of the pin holes except as noted in Item 836.01(b)3 shall not exceed that of the pin by more than 1/50 inch {0.50 mm} for pins 5 inches {127 mm} or less in diameter or 1/32 inch {0.80 mm} for larger pins.

836.43 through 836.45 Blank.

836.46 Welds.

a.General . Shop welding shall be performed by Submerged Arc Welding (SAW) in accordance with the specification noted herein. In the event the above method cannot be used, approved manual welding or other approved and qualified automatic or semi -automati c methods may be authorized. Field Welding shall be performed by manual Shielded Metal Arc Welding (SMAW) using approved electrodes and procedures in accordance with the specifications noted herein. If a minimum of 3 inches (75 mm} of excess material beyon d the theoretical end cuts does not exist, extension bars or run -off tabs shall be used at girder ends to insure sound welds on web to flange welds. All welding shall be subject to the inspection and approval of the Engineer or his representative. During inspection of the work any workman, including welders and inspection technicians, who, in the opinion of the Engineer, produces inferior work, may under the provision of Article 108.06 be disqualified from performing Departmental work. All welding sh all be in accordance with the AASHTO/AWS D1.5M/D1.5:2015, Bridge Welding Code, Seventh Edition as modified by the following:

Article 3 — 1. A new sentence shall be added to paragraph 3.1.3 as follows:

"Shop welding, except for minor secondary members and mi nor repair welding, shall be done under a cover of a permanent structure and/or building capable of protecting the actual welding operation from inclement weather. Any standing water that would be dangerous to the welder or operator or to the integrity of the weld itself shall be cause for the welding to stop until such time as the situation is corrected." Paragraph 3.2.9. The original A.W.S. subclause was deleted but shall be replaced with the following : "Paragraph 3.2.9. All corners of thermal cut or sh eared edges, including edges of flanges of beams and girders along with splice material and other sharp edges deemed undesirable by the Engineer on structural members designated to be coated shall be slightly rounded. Said rounding shall be accomplished by light grinding to produce a satisfactory surface for painting (approximately 1/16 inch {1.6 mm} radius). The grinding shall be performed in such a manner as to produce a neat workmanship like product without nicks or notches in the metal." A new paragraph to 3.5.1.9 shall be added as follows: "Paragraph 3.5.1.9 Gaps shall not exceed 0.040 inches {1.0 mm) between the contact surfaces at the bottom flanges of beams or girders and steel bearing plates. There shall be no gap for at least 75% of this contact ar ea." New Paragraphs 4.9 and 4.10 shall be added as follows: "Paragraph 4.9 (SAW – single electrode), 4.10 (SAW – parallel and multiple electrodes). A properly operated heating torch shall run immediately ahead (about 12 inches {300 mm}, and on the same si de, in advance of the point of welding) of the submerged arc welding head to remove moisture from the steel in the vicinity of the weld when making web to flange fillet welds of plate girders. Gases produc ing moisture in welding operations are discouraged unless it can be shown that the resultant temperature of the metal is sufficient to vaporize any moisture that might be present."

836.46 Welds.

Paragraphs 6.7.1, 6.7.1.1, and 6.7.1.2 in regard to Nondestructive Testing (NDT) of Complete Joint Penetration groove welds sh all be deleted in their entirety and the following substituted in lieu thereof: "Paragraph 6.7.1 – Complete Joint Penetration (CJP) groove welds shall be tested by

A.W.S. D1.5 Bridge Welding Code requirements in regard to and mandating the use of either r adiographic testing (RT) or ultrasonic testing (UT) in accordance with the following: "6.7.1.1 - Shop Welds. 100% of all CJP butt weld splices in the following: all flanges (tension and compression) of beams and girders, all flanges of floorbeams, all members of floorbeam trusses which support stringer beams, all flanges of steel bent caps; and all chords, diagon als and verticals of trusses. 50% of all vertical CJP butt weld splices in webs of beams, girders, floorbeams, and steel bent caps. This requirement shall consist of 25% of the web depth beginning at the top of the web plate and 25% of the web depth beginn ing at the bottom of the web plate. If rejectable discontinuities are found in the vertical CJP butt welded splices, the remainder of the weld shall be tested. 15% of each longitudinal CJP butt weld splice in the webs of beams, girders, floorbeams, and ste el bent caps, and in truss members. This requirement shall consist of 5% of weld length at each end of each plate and 5% of the weld length at the center of the plate (each plate is defined as that portion of web between vertical splices either welded or bolted).If rejectable discontinuities are found in a partially NDT examined longitudinal joint, additional NDT examinations using the original NDT process of that joint shall be made as required by the Engineer. 100% of all CJP welds used at the ends of lon gitudinal stiffeners welded to girder webs and the CJP welds used to splice sections of the longitudinal stiffeners together. 100% of all CJP groove welds in T - and corner joints (girder stiffener/connection plate to flange welds) shall be tested by UT. All welded repairs of RT or UT examined joints shall be re- examined by the original NDT process for quality and acceptability in the area of the repair. 6.7.1.2. - Field Welds. 100% of all butt welds in beams, girders, floorbeams, steel bent caps; and chords , diagonals, and verticals of trusses. All repairs of radiographed joints shall be reradiographed in the repair area." A New Paragraph 6.7.2. 1. shall be added as follows: “Paragraph 6.7.2. 1. Magnetic particle examination of all fillet welds and/or reinforc ement welds used in bearing assembly fabrication and a minimum of 10% of all fillet welds in expansion dams is required. If defects are found which require repair they shall be re- examined with magnetic particle testing after the repairs are made. Magnetic particle examination shall follow the procedures and requirements as outlined in AWS Subsection 6.7. A New Paragraph 6.7.7 shall be added as follows: “Paragraph 6.7.7 Dye penetrant (PT) examination of all welded and finished plate edges of CJP butt weld s plices of girder web plate or girder flange plate weld splices in main members is required. This examination shall be performed in addition to the required radiographic testing (RT) or ultrasonic testing (UT). If defects are found which require repair thes e areas shall be re -examined with PT after repairs are made. Written documentation of all non -destructive testing performed on all welding which requires NDT testing shall be submitted to the ALDOT representative within 48 hours of completion of the tests.
b.Qualification of Welders . Field welders shall be prequalified according to the standard qualification procedure of the applicable AWS Specifications and amendments thereto as noted in Subarticle 836.46(a). A welder that passes the required test procedure without requiring a retest will then be qualified for the next three years with no test required provided his performance is satisfactory. During this three year period a new card will be issued for one- year periods when the welder presents evidence th at he has been welding during the previous six month period. Welders that require a retest to become qualified must take and pass the test each year. Field welders must have a current qualification card on his person at all times that he is doing field wel ding.

836.47 & 836.48 Blank.

c.Shop Welding .
1.The Contractor or his representative shall furnish to the Department a written report that shall cover the welding procedure specification (WPS) for each process and joint used in shop welding. This report shall be submitted in duplicate on a format approved by the Department.
2.All shop welds shall be properly identified so that it can be determined by the Engineer which welder performed the work.
3.The AWS joint designation shall appear in the tail of the weld symbol on the s hop drawing.
4.Each full penetration weld that is to be tested by ultrasonic or radiographic testing shall be assigned a unique number by the preparer of the shop drawing. This number shall serve to identify that particular weld and shall also appear on a ll nondestructive test reports and x -ray film.
5.Whenever there are members identified on bridge plans or structural shop drawings as fracture critical members, post weld heating shall be used to prevent cracking in the heat affected zone due to hydrogen embrittlement. The cost of post weld heating will be considered a subsidiary obligation of the fabrication process.
d.Field Welding . Only authorized welding shall be done in the field. Unauthorized indiscriminate welding shall not be done to attach temporary construction details to beams, girders, or other main members without approval of the Construction Bureau. Welding is strictly pro hibited in areas where this restriction is shown on the plans (tension flanges) and other critical areas (fractural critical members) noted in these specifications.
e.Non Destructive Testing . All non -destructive testing required by these Specifications shall be performed by the Contractor (Fabricator) at his expense.

836.47 & 836.48 Blank.

836.49 Painting.

Shop coating shall meet applicable requirements of Section 521.

836.50 Protection Of Machine Finished Surfaces.

Machine -finished surfaces in general shall be shop painted except for the following: Driven pins and pin holes; surfaces in sliding contact; bronze, and steel surfaces opposing bronze in sliding contact; other surfaces as noted on the plans. Machine surfaces of steel not requiring pai nt should receive a heavy shop coat of Petrolatum meeting the requirements of ASTM D 217, NLGI Grade 2 or 3 or Military Specification C -16173D, Grade 1. Other approved coating may be used. Surfaces opposing bronze in sliding contact, if shipped assembled w ith bronze, shall be coated and assembled with the lubricant supplied by the bronze manufacturer. If not shipped assembled with bronze, such surfaces shall receive a shop coating, which shall be removed before field assembly. The lubricant furnished by the bronze manufacturer shall then be applied. No paint or protective coating shall be applied to bronze. SECTION 837 ELASTOMERIC BEARING MATERIALS

837.01 Description.

Elastomeric bearings shall be classified by Type in accordance with the following:

Source: Alabama Standard Specifications for Highway Construction, 2022 Edition. Pages 746762 of 934.